aircraft status forecast report asfr asfr...

ASFR DEC 2013

AIRCRAFT STATUS FORECAST REPORT

"ASFR"ASFR

Next

Due

4 mth

200hrs1-3-2014 14300,0

A/C REG A/C TYP YEAR OF MFG A/C S/N LOG NO DATE T.T HRS A/C OPERATOR TELE A/C BASE

SE-HZZ AGUSTA BELL 206B2 1978 8554 RDB 1-12-2013 14150,3 GUSTAF DIEDEN

Component Mfg Status Service Action

ATA Name Part No. Serial No. HRS CYCLES DATE Remarks Hrs/Cyc. Date Auth Lic.

8000 Starter-Generator 23032-010 10973 14176,8OH

505 50 Hr or 6 Month Insp Airframe Greasing 8554 14200,3 2-6-2014Insp MP-AB206B, Appx.. 5-4, 5-5

516 1500 /50 Hrs Insp Comp. SWPL. Support8554 14200,3Insp. MP-AB206B, Appx. 5-22

510E 100 Hrs Insp Engine RR250-C20 CAE-822933 14250,3 4-6-2014OIL Change Mobil Oil 254

506 100 Hrs Insp Airframe 8554 14250,3 1-12-2014Insp MP-AB206B, Appx. 5-6A, 5-6B

509 100 Hrs or 12 Month, InspAirframe Greasing 8554 14250,3 1-12-2014Insp MP-AB206B, Appx. 5-4

512 100 Hrs/ 12 Month Insp GILL G641 G02770844 14250,3 1-12-2014Insp. Battery IAW Gill Manual Q01-

1101 Rev. 27-10-2007

510E 100 Hr Insp Engine RR250-C20 CAE-822933 14250,3EASA AD 2004-0009 Rev. 2, CSL-

1066 MAC TI-005, B-Nut Tubing Insp

510E 100 Hr Insp Engine RR250-C20 CAE-822933 14250,3 17-12-2013EASA AD 2007-0043 , AW SB 206-

242, Exhaust Clamp Insp.

510E 100 Hr Insp Engine RR250-C20 CAE-822933 14250,3Insp. MP-AB206B, Appx. 6-1

Due A/C Time Action Performed

CALENDER LIFE ITEMS HELICOPTER AGUSTA BELL AB 206B

REG A/C TYPE YEAR OF MFG A/C S/N AC TCDS NR Rev L.NO AC DATE T.T HRS Ldgs A-Start ENG TSN CSN

SE-HZZ AB 206B II 1978 8554 ENAC SO/A140 8 RDB 7-1-2014 14210,1 UNK 14721 14084,4 14721 13-078 DATE:

PAGE: 1 OF 4

AIRFRAME COMPONENT: LIFE/TBO Sign: ORG NO:

Component Mfg Status Installed. A/C Time Component Time Due A/C Time Available To Go Component Cond Work Complied With

ATA Name Part No. Serial No. Life Tbo Insp Days Rins Date Hrs Rins Tsn/Tso Rins Days Hrs Rins Date Hrs Rins Days Remarks WO A/C Hrs Date Sign/Lic No

8000 Starter-Generator 23032-010 10973 1000 10-3-2009 13678,0 501,2 14176,8 -33,3OH

505 50 Hr or 6 Month Insp Airframe Greasing 8554 50 183 17-12-2013 14150,3 0,0 0 14200,3 18-6-14 -9,8 162Insp MP-AB206B, Appx.. 5-4, 5-5

MAC

13-078

516 1500 /50 Hrs Insp Comp. SWPL. Support 8554 50 17-12-2013 14150,3 0,0 0 14200,3 -9,8Insp. MP-AB206B, Appx. 5-22

MAC

13-078

510E 100 Hrs Insp Engine RR250-C20CAE-822933 100 185 17-12-2013 14150,3 0,0 14250,3 20-6-14 40,2 164OIL Change Mobil Oil 254

MAC

13-078

506 100 Hrs Insp Airframe 8554 100 365 17-12-2013 14150,3 0,0 0 14250,3 17-12-14 40,2 344

Insp MP-AB206B, Appx. 5-6A, 5-

6B

MAC

13-078

509 100 Hrs or 12 Month, InspAirframe Greasing 8554 100 365 17-12-2013 14150,3 0,0 0 14250,3 17-12-14 40,2 344Insp MP-AB206B, Appx. 5-4

MAC

13-078

512 100 Hrs/ 12 Month Insp GILL G641 G02770844 100 365 17-12-2013 14150,3 0,0 0 14250,3 17-12-14 40,2 344

Insp. Battery IAW Gill Manual Q01-

1101 Rev. 27-10-2007

MAC

13-078

510E 100 Hr Insp Engine RR250-C20CAE-822933 100 17-12-2013 14150,3 0,0 14250,3 40,2

EASA AD 2004-0009 Rev. 2, CSL-

1066 MAC TI-005, B-Nut Tubing

Insp

MAC

13-078

510E 100 Hr Insp Engine RR250-C20CAE-822933 100 17-12-2013 14150,3 0,0 14250,3 17-12-13 40,2

EASA AD 2007-0043 , AW SB 206-

242, Exhaust Clamp Insp.

MAC

13-078

510E 100 Hr Insp Engine RR250-C20CAE-822933 100 17-12-2013 14150,3 0,0 14250,3 40,2Insp. MP-AB206B, Appx. 6-1

MAC

13-078

521 1200 Hr Insp Cyclic Control Stick 8554 1200 13105,3 0,0 0 14305,3 95,2Insp. MP-AB206B, Appx. 5-8

6310 M/R Transmission 206-040-002-025 BKW11380 200 365 17-12-2013 14150,3 0,0 0 14350,3 17-12-14 140,2 344Oil &Filter Change, Mobil Oil 254

MAC

13-078

6510 TGB, Oil Change 206-040-400-5 B13-483 200 365 17-12-2013 14150,3 0,0 0 14350,3 17-12-14 140,2 344Oil Change, Mobil Oil 254

MAC

13-078

530 300 Hr Insp Airframe 8554 300 14061,2 0,0 14361,2 151,1Insp. MP-AB206B, Appx.5-7

530E 300 Hr Insp Engine RR250-C20CAE-822933 300 14061,2 0,0 0 14361,2 151,1Insp. MP-AB206B, Appx. 6-3

2810 Airframe Fuel Filter KD651510 NSN 300 14061,2 0,0 14361,2 151,1LIFE

6740 Lower Collective Tube 206-001-194-001 TYFS-4097 4800 12-10-2000 12437,4 2808,4 14429,0 218,9LIFE

510 300 Hrs or 12 Month Airframe Greasing 8554 300 365 17-12-2013 14150,3 0,0 0 14450,3 17-12-14 240,2 344Insp. MP-AB206B, Appx. 5-4

MAC

13-078

6250 M/R S/P & Support Assy 206-010-450-7 JIJG-09270 4800 15-5-2012 14027,3 4234,0 14593,3 383,2OH

6250 M/R S/P Duplex Brg 206-010-443-001 NSN 4800 15-5-2012 14027,3 4234,0 14593,3 383,2OH

6250 M/R S/P Sleeve Assy 206-010-454-005 A19-01581 4800 26-11-2001 12695,4 2901,6 14593,8 383,7LIFE

6360 Main Drive Shaft 206-040-015-103 A247 600 365 17-12-2013 14150,3 0,0 0 14750,3 17-12-14 540,2 344Insp. MP-AB206B, Appx. 5-18

MAC

13-078

6210 M/R Blade 206-010-200-033 T22604 5000 17-12-2013 14150,3 4117,8 15032,5 822,4LIFE

MAC

13-078

6210 M/R Blade 206-010-200-033 T22603 5000 17-12-2013 14150,3 4117,8 15032,5 822,4LIFE

MAC

13-078

6230 MRH Assy 206-011-100-021 EM0038 1200 14-9-2011 13986,3 0,0 15186,3 976,2OH

6230 MRH Pin Ret.Strap. Red 206-011-123-003 DIFS22387 1200 14-9-2011 13986,3 0,0 15186,3 976,2LIFE

6230 MRH Pin Ret.Strap. White206-011-123-003 DIFS22453 1200 14-9-2011 13986,3 0,0 15186,3 976,2LIFE

6230 MRH Ret. Strap Fitting. White206-011-140-001 DIFS3239 1200 14-9-2011 13986,3 0,0 15186,3 976,2LIFE

6230 MRH Ret. Strap Fitting. Red206-011-140-001 DIFS3590 1200 14-9-2011 13986,3 0,0 15186,3 976,2LIFE

6230 MRH Ret Strap 206-011-154-105 LPFS34053 1200 730 16-5-2013 14149,7 0,0 0 15349,7 16-5-15 1139,6 494LIFE

Wo No: 16-Aug-13

MAC SE.145.0113

1 Komponentlista airframe SE-HZZ ny




PAGE: 1 OF 4




Wo No: 16-Aug-13

MAC SE.145.0113

6230 MRH Ret Strap 206-011-154-105 LPFS34056 1200 730 16-5-2013 14149,7 0,0 0 15349,7 16-5-15 1139,6 494LIFE

515 1200 Hrs/24 Month Insp T/R Ctr Tube Nylatron Tubes8554 1200 730 17-12-2013 14150,3 0,0 0 15350,3 17-12-15 1140,2 709Insp. MP-AB206B, Appx. 5-20

MAC

13-078

6330 M/R Mast Assembly 206-040-002-007 NJE-08835 1500 27-8-2010 13879,4 0,0 15379,4 1169,3Insp. MP-AB206B, Appx.5-21

6310 M/R Transmission 206-040-002-025 BKW11380 4500 31-3-2011 13906,3 3023,4 15382,9 1172,8OH

6310 M/R Transmission 206-040-002-025 BKW11380 1500 31-3-2011 13906,3 0,0 15406,3 1196,2Insp. MP-AB206B, Appx.5-21

6350 FreeWheeling Assy 206-040-270-117 BMB11247 1500 11-3-2011 13906,3 0,0 15406,3 1196,2Insp. MP-AB206B, Appx.5-21

6350 FreeWheeling Assy 206-040-270-117 BMB11247 3000 11-3-2011 13906,3 1468,9 15437,4 1227,3OH

6510 TGB 206-040-400-5 B13-483 3000 12-10-2000 12437,4 0,0 15437,4 1227,3LIFE Duplex Brg 206-040-408-1

6350 FreeWheel Clutch Assy CL42250-1 FD13579 3000 11-3-2011 13906,3 1468,9 15437,4 1227,3LIFE

518 3000 Hrs Insp Comp. TGB-TRD 8554 3000 11-3-2011 13906,3 1468,9 0 15437,4 11-3-11 1227,3Insp. MP-AB206B, Appx. 5-23

6420 T/R Trunnion 206-011-812-005 NSN 2400 8-2-2008 13493,7 0,0 15893,7 1683,6LIFE

6420 T/R Yoke 206-011-819-105 AFS-7079 5000 8-2-2008 13493,7 2581,1 15912,6 1702,5LIFE, ref SB 206-89-47

6420 T/R Hub Assy 206-011-810-139 A-6087 2500 8-2-2008 13493,7 0,0 15993,7 1783,6OH

6250 M/R S/P Support 206-010-452-109 EA-944 4800 8-2-2010 13767,6 2209,3 16358,3 2148,2LIFE(ref ASB206-93-74)

6230 MRH Latch Bolt 206-011-260-103 DI26694 2500 14-9-2011 13986,3 0,0 16486,3 2276,2LIFE

6230 MRH Latch Bolt 206-011-260-103 DI26856 2500 14-9-2011 13986,3 0,0 16486,3 2276,2LIFE

6421 T/R Blade 206-016-201-103M-A C6-814 2500 15-10-2012 14121,7 0,0 16621,7 2411,6LIFE

6421 T/R Blade 206-016-201-103M-A C6-773 2500 15-10-2012 14121,7 0,0 16621,7 2411,6LIFE

2950 Hydralic Servo Act. Coll 206-076-031-013 5979 3600 9-10-2003 13105,4 0,0 16705,4 2495,3OH

2950 Hydralic Servo Act. LH 206-076-031-013 5981 3600 20-2-2008 13493,7 388,3 16705,4 2495,3OH

2950 Hydralic Servo Act. RH 206-076-031-013 3952 3600 9-10-2003 13105,4 0,0 16705,4 2495,3OH

6330 M/R Mast Assembly 206-040-002-007 NJE-08835 3000 27-8-2010 13879,4 0,0 16879,4 2669,3OH

6230 MRH Grip 206-010-102-121A AFS-7498 4800 14-9-2011 13986,3 1575,6 17210,7 3000,6LIFE

6230 MRH Grip 206-010-102-121A AFS-7391 4800 14-9-2011 13986,3 1575,6 17210,7 3000,6LIFE

6250 M/R S/P Lever Collective 206-010-467-1 REFS-1237 4800 26-11-2011 12695,4 258,0 17237,4 3027,3LIFE

2940 Hyd Pump&Reservoir 206-076-022-005 6106 3600 11-4-2011 13906,3 0,0 17506,3 3296,2OH

6250 M/R S/P Link Coll. Idler 206-010-407-001 REFS-4367 4800 23-7-2004 13202,5 0,0 18002,5 3792,4LIFE

6510 TGB 206-040-400-5 B13-483 6000 12-10-2000 12437,4 0,0 18437,4 4227,3OH

6230 MRH Trunnion 206-011-113-105 HB3657 4800 14-9-2011 13986,3 0,0 18786,3 4576,2LIFE

522 Airworthiness SE-HZZ 8554 * 365 19-12-2013 14150,3 0,0 0 14150,3 19-12-14 346ARC-0 Renewal

MAC

13-078





PAGE: 1 OF 4




Wo No: 16-Aug-13

MAC SE.145.0113

2550 First Aid Kit APOTEKET 8554 365 17-12-2013 14150,3 0 17-12-14 344Check Cond.

MAC

13-078

2630 Fire Exting. Halon 1211 BA23792-1 074360 365 17-12-2013 14150,3 0 17-12-14 344

Check Cond. & Weight, Original

Weight: 1179 gram

MAC

13-078

6330 M/R Mast Assembly 206-040-002-007 NJE-08835 365 17-12-2013 14150,3 0 17-12-14 344Insp. MP-AB206B, Appx. 5-24

MAC

13-078

2430 Battery "Lead-Acid" Gill G-641 G02770844 365 17-12-2013 14150,3 0 17-12-14 344Insp. MP-AB206B, Appx.5-11

MAC

13-078

2805 Fuel Tank Cell 206-061-675-001 NSN 365 17-12-2013 14150,3 0 17-12-14 344Insp. MP-AB206B, Appx.5-11

MAC

13-078

500 12 Month Inspection Airframe 8554 365 17-12-2013 14150,3 0 17-12-14 344Insp. MP-AB206B, Appx.5-11

MAC

13-078

2350 ELT KANNAD 406 AF-H 1202503 KA2625223001 365 17-12-2013 14150,3 0 17-12-14 344

Test Function & Check Instl. Ref

KANNAD OMM

MAC

13-078

3450 Airspeed Ind. 8000 NSN 730 17-12-2013 14150,3 0 17-12-15 709

Insp Ref: BCL-M, kap 4.3 para. 7.3

& bilaga 2

MAC

13-078

3450 Altimeter 5934M NSN 730 17-12-2013 14150,3 0 17-12-15 709

Insp Ref: BCL-M, kap 4.3 para. 6.3

& bilaga 1

MAC

13-078

500 24 Month Inspection Airframe 8554 730 17-12-2013 14150,3 0 17-12-15 709Insp. MP-AB206B, Appx. 5-12

MAC

13-078

3460 Compass Stby-Dir.Gyro C2300DL4B NSN 730 17-12-2013 14150,3 0 17-12-15 709Deviation Check

MAC

13-078

2630 Fire Exting. Halon 1211 BA23792-1 074360 3650 8-2-2008 13493,7 0 5-2-18 1490LIFE

2350 ELT KANNAD 406 AF-H 1202503 KA2625223001 2100 17-12-2013 14150,3 0 17-9-19 2079Life Battery

MAC

13-078

6730 Support Servo Actuator 206-001-520-005 NSN O/C 1-1-1978 0,0 0,0 0 O/C O/CC.M

3430 Clock 8 Days Digital LC-2 NSN O/C 1-1-1978 0,0 0,0 0 O/C O/CC.M

7900 E/G Oil Cooler Assy 8534998 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

6311 MR Trans Oil Cooler 8538312 NSN O/C 31-3-2011 13906,3 5593,4 0 O/C O/CC.M

6600 T/M Oil Cooler 8538312 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2330 TXPD, KING 76A 066-1062-10 126850 O/C 3-4-1978 0,0 0 O/C O/CC.M. REC. EASA SIB: 2011-15R1

2320 VHF COM "King KY96A" 064-1052-70 6971 O/C 3-4-1978 0,0 0 O/C O/CC.M

3430 GPS KING 8553 O/C 3-4-1978 0,0 0 O/C O/CC.M

2320 VHF Com/Nav "King KX12569-01028-1101 8553 O/C 3-4-1978 0,0 0 O/C O/CC.M

2430 Voltage Regulator 1589-1F NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3420 Directional Gyro Ind. 200DC NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

6230 MRH Yoke 206-010-101-125 O/C 14-9-2011 13986,3 0,0 0 O/C O/CC.M INSP AT HUB OH

6330 M/R Mast Pole 206-010-332-17 FAJF-57778 O/C 27-8-2010 13879,4 8005,1 0 O/C O/CC.M

6240 MRH Blade Bolt 206-011-119-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

6240 MRH Blade Bolt 206-011-119-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

6420 T/R Assy 206-011-810-825 NSN O/C 8-2-2008 13493,7 2581,1 , O/C O/CC.M

5500 Tail Fin Assy 206-020-113-11 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M





PAGE: 1 OF 4




Wo No: 16-Aug-13

MAC SE.145.0113

5500 Horizontal Stabilizer 206-020-123-011 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

5500 Horizontal Stabilizer 206-020-123-012 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

5500 Fuselage Assy, Fwd 206-031-002-107A 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

5500 Tail Boom Assy 206-031-004-115 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

6520 T/R Fan Shaft Assy 206-040-301-015 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

7900 E/G Oil Tank Assy 206-061-505-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2820 Fuel Press Transducer 206-061-535-007 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 N1 Tacho-Gene 206-062-627-003 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 N2 Tacho-Gene 206-062-627-003 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2820 Fuel Boost Pump "Aft" 206-062-681-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2820 Fuel Boost Pump "Fwd" 206-062-681-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

7630 Linear Actuator Assy 206-062-721-011 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 Dual Tacho Ind. 206-070-265-007 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 N1 Tacho Ind. 206-070-266-009 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3450 Turn & Slip Ind 206-070-274-101 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3420 VSI 206-070-278-005 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 Fuel Press & Load Meter 206-075-186-003 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 E/G Oil Temp& Press Ind 206-075-187-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 T/M Oil Temp & Press Ind206-075-188-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 Fuel Qty Ind. 206-075-189-101 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 TOT Ind 206-075-190-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 OAT Ind 206-075-624-001 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3300 High Landing Gear Assy 206-321-431 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 NR Tacho-Gene 22A690 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2820 Pump Cartridge "Aft" 2C27-10 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

2820 Pump Cartridge "Fwd" 2C27-10 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3130 Torque Meter Ind 4308 3018 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

500 Weight & Balance Check Airframe 8554 O/C 3-4-1978 0,0 0,0 0 O/C O/CNew Weight & balance Check

2805 Fuel Tank Unit "Upper" EA470-3587 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CCheck Daily

2805 Fuel Tank Unit "Lower" EA470-3588 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CCheck Daily





PAGE: 1 OF 4




Wo No: 16-Aug-13

MAC SE.145.0113

3480 Audio Selector IC "King" KA134 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3450 Audio IC Unit PM3000 NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

3450 Attitude Gyro "AIM" NSN O/C 3-4-1978 0,0 0,0 0 O/C O/CC.M

501 Weekly Insp Airframe "Corrosiv" 8554 * 7 17-12-2013 14150,3 0,0 0 14150,3 24-12-13Insp. MP-AB206B, Appx. 5-9

MAC

13-078 NA SE-HZZ

503 6 Month Insp Airframe "Floats" 8554 * 180 0,0 0 0,0 28-6-00Insp. MP-AB206B, Appx. 5-10

NA SE-HZZ

513 3 Years Insp Airframe "Floats" 8554 * 1095 0,0 0 0,0 30-12-02Insp. MP-AB206B, Appx. 5-14

NA SE-HZZ

520 600 Hrs Insp Comp. MGB 8554 600 0,0 0 600,0 0-1-00Insp. MP-AB206B, Appx. 5-17

NA SE-HZZ

511 300 Hrs/ 6 Month Insp Comp. MD Shaft 8554 300 180 0,0 0 300,0 28-6-00Insp. MP-AB206B, Appx. 5-15

NA SE-HZZ

514 1200 Hrs Insp Components Insp 8554 1200 * 0,0 0 1200,0Insp. MP-AB206B, Appx. 5-19

NA SE-HZZ


ASB AC

MANDATORY SERVICE BULLETINES & EASA/ENAC AD AB 206B II

REG: SE-HZZ SN: 8554 ADs & ASB AIRFRAME PAGE Of 12 BW 2013-25 MAC Wo.No: 13-078 DATE: 17-Dec-13

ASB Rev AB-BT EASA-AD ENAC-AD CF-AD ACTION PARTREC REPT QAT REMARK ACTION TAKEN WO NoDATE MECH

00-93 A 2000-343 2000-13 Collective Lever Assy PN 206-010-467-001, Modification I, IINO ASB

Check, Non raised bossC.W, PART II, RAISED FORGED

BOSS REMOVED 2013-05-11 CAA-145

01-96 A 2001-401 2001-33Tedeco B3188B and B4093 chip detector assembly Insp.

and testing I NO ASB

PERF. TEST PROCEDURE I.A.W.

PROC. B OF ASB206-01-96 REV AC.W. INSP CHECK 2013-05-11 CAA-145

AA, high fwd crosstube, P/N 206-321-001,SN 1001 through

1152, and high aft crosstube, P/N 206-321-002 S/N 2001-

2152, I NO ASB

AERONAUTICAL HIGH GEAR, STC

SH1392SONA DUE TO PN INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

04-101 04-09 2004-25T/R BLADES 206-016-201-131 CHECK AND REMOVAL

FROM SERVICE OF.I, II

NO ASB

BLADES 131 WITH SN CS-4820 TO

CS4845NA DUE TO PN INSTALLED 2013-05-11 CAA-145

04-100 C 07-01 2004-05R2T/R BLADES 206-016-201-131/-133, CHECK INSPECTION

OFI, II, III, IV

YES ASBBLADES 131 & -133 WITH SUFFIX CS NA DUE TO PN INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

2007-078R1 2007-02R1205 series hcp that have the following Transmission Pylon

Support Spindle Part Number (P/N) 206-031-554 (Spindle) I NO ASB

Concerns specific serialised

components, see AD for details.

NA DUE TO SPINDLE INSTALLED

BY REPAIR OR SN2008-03-13 CAA-145

2007-349 2007-02R1206 series hcp that have the following Transmission Pylon

Support Spindle Part Number (P/N) 206-031-554 (Spindle)I

NO ASB


components, see AD for details.


BY REPAIR OR SN2008-03-13 CAA-145

06-109 206-241 2006-0371-E 2006-483 2006-23R1Removal of M/R latch bolts, P/N 206-010-169-001/-003 and

206-011-122-003, Bell 206B S/N 0 - 3216 I NO ASBNA BY LATCH BOLT PN 2008-03-13 CAA-145

06-109 206-241 2006-0371-E 2007-104 2006-23R1

Removal of M/R latch bolts, P/N 206-010-169-001/-003 and

206-011-122-003, Bell 206B S/N 0 - 3216, REMOVE

FROM SERVICE I NO ASB

NA BY LATCH BOLT PN 2008-03-13 CAA-145

06-107 A 05-02 2006-12VERTICAL FIN SUPPORTS 206-031-417-003/-007 AND

206-031-418-001/-005, INSPECTION OFI

NO ASBNEW TYPE PN; 206-033-426 C.W INSP 2008-07-17 CAA-145

06-110 06-09 2007-044 2007-01Identification and Insp. of steel tailboom filting, P/N 407-

030-750-103I, II

NO ASBNA, DUE TO INSTALLED PARTS 2008-03-13 CAA-145

09-121 C 09-08 2009-10R1CYCLIC CONTROL LEVER, (P/N) 206-001-401-111, 206-

001-400-115, 206-001-400-111 AND 206-001-339-015I

NO ASBC.W. INSP CHECK 2009-03-31 CAA-145

07-116 B 206-248 2010-0272-E 2010-423 2007-21R1

T/R BLADES 206-016-201-127/131/-133/-135/-137,

REPAIRED BY RBI CHECK AND REMOVAL FROM

SERVICE OF. SNS

INO ASB

Future servicability of tall rotor blades

governed by SINNA DUE TO BLADE PN SN INSTL. 2010-12-22 CAA-145

07-116 B 206-248 2010-0272-E 2010-453 2007-21R1

T/R BLADES 206-016-201-127/131/-133/-135/-137,


SERVICE OF. SNS

INO ASB



08-01 A

Emergency Float Kit with a part number (P/N) and serial

number (S/N), installed by a supplemental type certificate

(STC), as follows:I

NO ASBSTC-KIT NA STC NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

10-11Night Vision Imaging System (NVIS) lighting installed per

Supplemental Type Certificate (STC) SR01383SEI

NO ASBNA STC NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

80-07 B 1997-156 1997-03MRTrunnion, P/N: 206-010-136-001, 206-010-136-003,and

206-011-113-001, Insp. Req, SERVICE LIFEI

NO ASB

Ref. to FAA AD 81-18-01 Bell (ASB)

206L-94-99 Rev.ANA DUE TO AC MODEL 2013-05-11 CAA-145

2001-263R1 2001-03R1Mand instal of part sep/intaks deflector on all Bell 206B,

RFM Limits, IN SNOW AND ICY CONDITIONS I NO ASBThis supercedes FAA AD 89-10-11R1.

C.W. AT WINTER FLYING,

INCORP IN RFM CHAPTERS2013-05-11 CAA-145

93-74 BSwashplate Support Assembly 206-010-452-001/-005/-109,

Inspection ofI

YES ASB109 INSTL. 50 hrs after 1500 tsn

C.W INSP. CHECK, INSTRUCTION

INCORP IN MP-AB206B2 APPX. 6

MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

93-75Trunnion 206-011-113-103 Master Spline Mislocation of

I NO ASBC.W CHECK CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

92-69 ABracket, Bearing Support206-030-407-007/-009 and 206-

030-433-005/-007/-Oll/-013/-015and -017, One Time

InspectionI NO ASB

C.W CHECK CAMO 2013-12-17MAC, SE MG

0095 ASR-1

90-54 Fuel Valve Switch Guard, Installation ofI NO ASB

C.W CHECK CAMO 2013-12-17MAC, SE MG

0095 ASR-1

79-05 1996-115 1995-19Insp. intervall for main input driveshaft assembly, P/N 206-

040-100-013 I YES ASB

Ref. Bell(ASB) 206-79-05, FM (AD) 81-

04-08 and TC (AD) CF-95-19 (300

hours)

NA DUE TO PN INSTALLED 2013-05-11 CAA-145

93-76 B 1996-115 1995-19

Main Driveshaft Grease Lubricated Couplings 206-040-108

and 206-040-118, Over-Temperature Indicators, Installation

of

I, II, IIINO ASB

600 HRS / 1YR GRAESING INCORP.

IN MM CL

C.W. INCORP IN AB MM CHAP 12

& 52000-10-12 CAA-145

Page 6

ASB AC




206-1 1967-117Insp. of engine droop compensator control, P/N 206 061

701 I NO ASB

AB 206A S/N 8002 8007 and 8018 only,

Ref. Bell(SB) 206A-1 and BT 206-1 (10

hours until compliance with Part II)

PERFORMED AT FACTORY AT

MFG1978-01-01 AGUSTA

206-1 1967-117Modification of engine droop compensator control, P/N 206-

061-701 II YES ASB

AB 206A S/N 8002 - 8007 and 8018

only



206-3 1967-123 Insp. and safety wiring of exhaust stack clamp, P/N N3657I YES ASB

AB 206A S/N 8002 - 8008, 8011, 8013

and 8018 only, Ref. BT 206-003 (daily)



206-2 1967-124Insp. of cyclic control system lever assembly, P/N 206-001-

339-11, and addition of shield, P/N 206-001-340-1 I NO ASB

AB 206A (delivered) with single controls

only and/or manufactured before 8th

November 1967, Ref. BT 206-002



206-8 1968-010Insp. of swaged ends of cyclic andc ollective control tubes,

P/N 206-001-524-3 and 206-001-524-7 I NO ASB

AB 206A S/N 8001 - 8021 and 8026

only, see AD for details, Ref. BT 206-

008



206-7 1968-011Insp. and addition of support bracket kit, P/N 206-704-005-

1, at the forward engine mount attachment points I NO ASB

AB 206A S/N 8001 8021 and 8026 only,

Ref. BT 206-007



206-10 1968-048Modification of bellcrank, P/N 206-001-702-1, and/or

installation of modified bellcrank,P/N 206-001-702-5 I NO ASB

AB 206A S/N 8001 - 8008, 8011, 8013,

8014, 8018, 8019, 8020 and 8026 only,

Ref. BT 206-010



206-15 1968-101 Installation of new fuel system check valve, P/N 496 4D1 2I NO ASB

AB 206A S/N 8001 8050 only, Ref.

Bell(Memo) No. 206A-17 and BT 206-

015



206-14 1968-106Replacement of exhaust stack clamp, P/N 4656AA, with

modified exhaust stack clamp, P/N N3657 I NO ASB

AB 206A S/N 8001 - 8040 only, Ref.

Bell(SL) No. 38 Rev. A and BT 206-014



206-17 1968-117 Installation of lower R.P.M. limit stop on engine governorI NO ASB

AB 206A S/N 8001 - 8036 only, Ref.

Bell(SL) No. 206A-7 and BT 206-017



206-19 1968-156Modification of instrument console with stiffeners, P/N 206-

031-110-251 and 206-031-110-252 I NO ASB

AB 206A S/N 8001 8018 only, Ref. BT

206-019



206-20 1968-157 Insp. and torque check of tall rotor blade retention bottsI NO ASB

AB 206A S/N 8001 - 8068 only, Ref. BT

206-020



206-21 1968-162 Insp. of M/R blade retention botts, P/N 206 010 152 1I NO ASB

AB 206A S/N 8001 8079 only, Ref.

Bell(SL) No. 206A-55 and BT 206-021



206-22 1968-167Insp. of magnesium tall boom , P/N 206031 004 1 and 206

031 004 3 I NO ASB

BT applies to specific airframe and

tailboom configurations, see BT for

details, Ref. Bell(SB) No. 206A-7 and



206-27 1968-201 Interim operating restrictions of the Allison 250C18I NO ASB

AB 206A S/N 1 8094 (except those with

modified powerplants), Ref. Bell(SL)

206A-103, Ref. BT 206-027



206-29 1969-016 Insp. of pitch link assembly, P/N 206-010-330 9I NO ASB


206-029



206-30 1969-019

Insp. of the fan shaft assembly, P/N 206-040-301-5, to

assess condition and alignement of bearings, P/N 206-040-

339-1I NO ASB

Insp. applies only to AB 206A where fan

shaft assembly has been disturbed, Ref.

BT 206-030



206-25 1969-020 Insp. of tall rotor control tube assembly, P/N 206-001-021-9I YES ASB

AB 206A only, Ref. Bell(SL) No. 206A-

97 and BT 206-025



1969-058Insp. and replacement of magnesium cyclic pitch mixing

lever supports, P/N 206-001-521 I YES ASB

AB 206A only, Ref. FAA (AD) 1969 7-3

(daily)



1969-059 AD Cancelled AD Cancelled 1978-01-01 AGUSTA

206-6 1969-084Modification of tall rotor pedal control by addition of fridlon

slamp, P/N 206-001-710-1, and spring, P/N 206-001-721-1 I NO ASB

AB 206A S/N 8001 - 8025 only, Ref. BT

206-006



1969-112Replacement of instrument console Insp. panel(s)

attachment hardware I NO ASB

AB 206A S/N 8001 - 8170 only, Ref.

Bell(SB) 206A-120



206-12 206-12 1969-116Establishment of mandatory retirement life of hydraulic

cylinder wire drive, P/N 30000649 I NO ASB

BT concerns hydraulic cylinders P/N

41103750, 41103750-2 and 41103650-

005, Ref. Bell(SB) No. 206A-12



206-33 1969-117 Addition of exhaust stack clips , P/N 206-1202 C1 2I NO ASB

BT applies to specific airframe and

exhaust config., see BT for details, Ref.

Bell(SL) No. 206A-123



Page 7

ASB AC




206-32 1969-172

Replacement of cyclic control bellcrank support, P/N 206-

001-521-5, with modified assemblies, P/N 206-001-544-5

and -6I NO ASB AB 206A S/N 8001 - 8147 only



206-38 1970-037Insp. of the tall rotor gear box bevel case, P/N 206-040-412-

1 and 206-040-425-1, mounting surface I NO ASB

AB 206A S/N 8001 8189 only, Ref.

Bell(SB) 206A-15 and BT 206-038



206-37 1970-064Reduction in service life of transmission spider, P/N 206-

040-041-1 I NO ASB

AB 206A only, Ref. Bell(SB) No. 206A-

14 Rev. B and BT 206-037



206-40 1970-091A Introduction of corrosion protection at M/R blads buff endI NO ASB

AB 206 with specified M/R blades, see

AD for setails, Ref. Bell(SL) 206A-86

Rev. A and BT 206-040



206-41 1970-119Insp. of M/R mast boot, P/N 206-010-439-1, for installation

and condition of attachment rings I YES ASB


206-041 (daily)



206-43 1970-146AInstallation of improved firewall seal , P/N 206062 224 5

(Kit P/N 206 704 026 1) I NO ASB

AB 206 S/N 8001 8210 only, Ref.

Bell(SL) 206-142 Rev. A and BT 206-

043



206-44 1970-147AReplacement of solid voltage regulators , P/N 206 075 027

3, with carbon pile type I NO ASB

BT applies to specific airFrame S/N

only, see BT for details, Ref. Bell(SL)

206A-139 Rev. B and BT 206-044



206-46 1970-167Insp. and modification of snow winterization kit, P/N 206-

706-027-1 I NO ASB

AB 206A S/N 8001 8192 with snow

winterization kit installed, Ref. Bell(SB)

206A-16 and BT 206-046



206-45 1970-168

Installation of improved transmission drain plug and

modification of Insp. procedurs of transmission magnetit

pluqI NO ASB

AB 206A with early type magnetic plug,

P/N B734, installed, Ref. Bell(SB) 206A-

17 and BT 206-045




206-18 1970-219Replacement of aluminum fuel fines with corrosion resistant

steel fines I NO ASB

AB 206A S/N 8001 - 8244 only, Ref.

Bell(SB) 206A-18



206-50 1971-042Insp. and/or installation of collective lever ground cable,

P/N 206-075-357-13 I NO ASB

AB 206A S/N 8001 - 8247 only, Ref. BT

206-050




206-51 1972-061Modification of particle seperator installation with kit, P/N

206 704 078 1 I NO ASB

BT applies to specific particle seperator

configurations, Ref. Bell(SI) 206-89 and

BT 206-051 (Optional)




206-53 1972-175AFunctional check for high skid gear emergency floatation

kit, P/N MV254, valve assembly, P/N 800853 I YES ASB

AB 206 equipped with high skid gear

emergency floatation kit, Ref. Bell(SB)

206-21 Rev. A and BT 206-053 (90



206-54 1973-003Insp. and modification of idler assembly, P/N 206-001-746-

5, to post-mod status, P/N 206-001-746-9 I NO ASB

AB 206 S/N 8260 - 8329, 8331 and

8332 only, Ref. Bell(SB) 206-22 and BT

206-054



206-55 1973-004Insp. of M/R hub latch and retention bott nuts, P/N

NAS1022A14 or MS21245-L14 I NO ASB

AB 206 only, Ref. Bell(SB) 206- 24 and

BT206-055



206-56 1973-005One time Insp. of M/R mast, P/N

206-010-332 I NO ASB

AB 206 S/N 8001 - 8332 only, Ref.

Bell(SB) 206-23 and BT 206-056



1973-028Insp. of heater fuel line, P/N 206-070 705 1, for evidence of

chafing I NO ASB



206-57 1973-051B

Identification and Insp. of vertical fin P/N 206-020-113-3,

206-020-113-5, 206-020-113-7 and 206-020-113-9 inboard

skinI NO ASB

AB 206 S/N 8001 - 8335 without

doublers installed, Ref. Bell(SB) 206-01-

73-1 and BT 206-057



206-61 1973-069One time Insp. of hydraulic servo actuator valve drive

lovknut, P/N MS20364-1032C or MS21042 I NO ASB

AB 206 manufactured before 21 May

1973 only, Ref. Bell(SB) 206-06-73-2

and BT 206-061



206-64 1973-076Insp. of M/R pitch link tubel, P/N 206-010-330 and 206-

010-342 I NO ASB

AB 206 only, Ref. Bell(SB) 206-04-2-73-

1 and BT 206-064



206-66 1973-085Insp. of heater fuel line, P/N 206-070-231-1, for evidence of

interference with airframe at station 3429, W/L 1618 I NO ASB

AB 206 S/N 8001 - 8355 only, Ref.

Bell(SB) 206-12-73-1 and BT 206-066



Page 8

ASB AC




206-63 1973-086AInsp. and replacement of hydraulic servo

actuator assembly, P/N 41000005 I YES ASB

BT applies to specific servo actuators

only, see BT for details, Ref. Bell(SB)

206-06-73-1 and BT 206-063 (100



206-65 1973-090 Insp. of M/R swashplate hearing, P/N 206-010-420I YES ASB

AB 206 only, Ref. Bell(SB) 206-04-2-73-2 and BT

206-065 (300 hours)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

206-67 1973-094Insp. and replacement of vertical fin support forgings, P/N

206-031-417 and 206-031-418 I NO ASB

AB 206 S/N 8001 - 8380 only, Ref.

Bell(SB) 206-01-73-5 and BT 206-067




206-69 1973-117Introduction of mandatory retirement life for M/R retention

strap filtings, P/N 206-010-155, and pins, P/N 206-010-123 I NO ASB

AB 206 only, Ref. Bell(SB) 206-04-1-73-

1 and BT 206-069



206-60 1973-140AMagnetit particle Insp. of rotor brake assembly, P/N

4000071, and rework of relief holes in diss stots I YES ASB

AB 206 with rotor brake P/N 206-706-

021-1 installed, Ref. Bell(SB) 206-50-73-

2 Rev. A and BT 206-060 (300 hours)



206-71 1973-141 Insp. of tall rotor gearbox assembly, P/N 206 040 400I NO ASB

AB 206 S/N 8260 8355 only,Ref.

Bell(SB) 206-04-73-1 and BT 206-071



206-59,

206-68,

206-72

1973-158DInsp. of transmission mount links , P/N 206 031 508 5 and

206 031 508 7 I YES ASB

AB 206 with specified links filted, Ref.

Bell(SB) 206-01-73-2, BT 206-59, BT

206-68 and BT 206-72 (5 hours)




1974-023B Insp. of M/R blade, P/N 206-010-200 29I YES ASB

AB 206 with M/R blade P/N 206 010

200 29 installed , Ref. Bell(SB) 206A-19

(100 hours/daily)








1974-111Insp. and replacement of cyclic and collective control

system hardware with special bolt, P/N NAS1305-18D I NO ASB

AB 206 S/N 8001 8429 only, Ref.

Bell(SB) 206-04-2-74-1



206-78 1974-128Replacement of tube assemblies , P/N 206-070-444 1 and

206 070 448 1 I NO ASB

AB 206 S/N 8001 8329, 8372 8417, Ref.

Bell(SB) 206-08-74-1 and BT 206-078



206-79 1974-129Installation of horizontal stabilzer stop kit, P/N 206 704 096

3 I NO ASB

AB 206 S/N 8001 8417 only, Ref.

Bell(SB) 206-01-74-1 Rev. B and BT

206-079



206-80 1974-130Insp. and replacement of cyclic and collective control

system hardware with special bolt, P/N NAS1305-18D I NO ASB

AB 206 S/N 8001 - 8429 only, Ref.

Bell(SB) 206-04-2-74-1 and BT 206-080



206-82 1974-159Replacement of hearing hanger screw, P/N 206-040-323-3,

with improved screw, P/N 206-040-323-3 I NO ASB

AB 206 S/N 8001 - 8355 only, Ref.

Bell(SB) 206-04-74-1 Rev. B and BT

206-082



206-83 1974-160Insp. of particle seperator , P/N 206-062

818 5 I NO ASB

AB 206 equipped with specified particle

seperator only, Ref. Bell(TB) 206-01-74-

2



206-76 1974-161AModification of fuel cell cavity and vent live, P/N 206-061-

699-1 I NO ASB

AB 206 S/N 8001 - 8372 and 8381 8382

only, Ref. BT 206-076




206-84 1974-179Insp. and rework of M/R hub yoke,P/N 206-010-101-1, 206-

010-101-5, 206-010-101-9 and 206-010-101-13 I NO ASB

AB 206 S/N 8001 - 8422 only, Ref.

Bell(SB) 204-04-1-74-1 and BT 206-

084



Page 9

ASB AC





206-86 1974-197Modification of pressure regulator valve

assembly, P/N 206 076 015 1 I NO ASB

AB 206 S/N 8001 8370 only, Ref.

Bell(TB) 206-06-74-1 and BT 206-086




206-87 1974-226BRemoval from service of rotor brake disc

assembly, P/N 4000071 or 4000071 1 I NO ASB

AB 206 equipped with rotor brake kit

P/N 206-706-032-1 only, Ref. Bell(SB)

206-50-74-1 and BT 206-087




206-88 1975-002Insp. of transmission mount spindle, P/N

206 031 554 1 or 206 031 554 3 I NO ASB

BT supercedes BT206 31 Rev.A, AB

206 only, Ref. Bell(SB) 206-01-74-3 and

BT 206-088



206-92 1975-050 Insp. of the M/R grip assembly, P/N 206 010 102 9I YES ASB

AB 206 fitted with specified M/R ASSY only, Ref.

Bell(SB) 206-04-1-74-

2 and BT 206-092 (1200 hours)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1



206-74 1975-091BInsp. and replacement of starter generator retaining clamp

'T' bolt I NO ASB

AB 206 S/N 8001 8365 and 83818384

only, Ref. Bell(SB) 206-03-73-1 and BT

206-074



206-95 1975-115Insp. of tall rotor drive shaft clamp type bearing hangers,

P/N 206-040-338-5, 206-040- 345-9 and 206-040-346-9 I NO ASB

BT applies to specific airframe and tall

rotor driveshaft bearing configuration,

Ref. Bell(SB) 206-75-1 and BT 206-095




206-85 1975-117BInsp. of hydraulic system and hydraulic

servo actuators I NO ASB

AB 206 S/N 8001 8468 with specific

actuators only, Ref. Bell(SB) 206-06-74-

1 Rev. A and BT 206-085



206-85 1975-117B Modification of sequence valveII YES ASB

AB 206 S/N 8001 - 8468 with specific

actuators only, Ref. Bell(SB) 206-06-74-

1 Rev. A and BT 206-085



206-94 1975-142AInsp. of tall rotor control tube assembly,

P/N 206-010-743-13 I NO ASB

AB 206 S/N 8001 - 8259 only, Ref.

Bell(SB) 206-75-2 and BT 206-094



206-91 1975-155AReplacement of sabin roof straps, P/N 206-031-200-23 and

-24 with modified straps, P/N 206-032-200-37 and -38 I NO ASB

AB 206 S/N 8001 - 8371 and 8381 -

8385, Ref. Bell(SB) 206-01-74-2 and

BT206-091



206-96 1975-165Introduction of mandatort' retirement ffc fortall rotor yokes,

P/N 206-010-788-1 and 206-011-802-1 I NO ASB

AB 206 fitted with specified tall rotor

yokes only, Ref. Bell(SB) 206-75-4 and

BT 206-096





206-98 1975-201 Modification of externa) hoist assembly, P/N BL-16600-11I NO ASB

AB 206B S/N 8330 and sub. Equipped

with specified hoist, Ref. Bell(SB) 206-

75-5 and BT 206-098



206-100 1975-251Insp. of upper and lower passenger door hinge rivets, P/N

206-031-535, 206-031-536, 206-031-537 and 206-031-538 I NO ASB

AB 206 S/N 8001 - 8172 , Ref. Bell(SB)

206-75-7 and BT 206-100



206-79 1975-266AInsp. of pitch fink assemblies, P/N 206-010-330 and 206-

010-342 I NO ASB

AB 206 fitted with specified pitch fink

assemblies only, Ref. BT 206-79





Page 10

ASB AC




206-102 1975-295Introduction of mandatory retirement life for M/R blades,

P/N 206 010 200 29 I NO ASB

AB 206 filted with specific M/R blade

only, Ref. Bell(SB) 206-75-10 and BT

206-102



206-103 1976-031 Installation of 10 micron filter in fuel purge fineI NO ASB

AB 206 S/N 8051 - 8532 only, Ref.

Bell(SB) 206-75-8 and BT 206-103




206-104 1976-098

Installation of scupper, P/N 206-072-912-1 to fuel drain

valve when cargo hook kit, P/N 206-706-104-1 or -3, is

installedI NO ASB

AB 206 S/N 8001 - 8371 equipped with

specified cargo hook kit only, Ref. Bell

(TB) 206-50-73-1 and BT 206-104



206-107 1976-114Restrictions on grease, P/N 204-040-755-3 (Andero) L

786), batch nutuber 12111 I YES ASB

AB 206 and spares delivered between 1

Feb 1975 and 1 July 1976 only, Ref. BT

206-107 (3 months)



206-109 1976-123 Insp. of fuel systemI NO ASB

AB 206 only, Ref. Bell(SB) 206 76-3

and BT 206-109



206-75 1976-128CInsp. of horizontal stabilzer, P/N 206-020-119 and 206-020-

123 1 I NO ASB

AB 206 S/N 8001 8417 only, Ref.

Bell(SB) 206-01-73-7 Rev. D and BT

206-075



206-101 1976-161AInsp. of hydraulic servo actuator support assembly, P/N

206-001-520-5, forward webs I YES ASB

AB 206 only, Ref. Bell(SB) 206- 76-1 and BT 206-

101 (100 hours)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

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MAC AT-1

206-97 1976-168BCheck torque of pillow block attaching balt

torque II YES ASB

AB 206 only, Ref. Bell(SB) 20675-3 and FAA AD

75-18-07 and BT 206-097(100 hours)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

206-97 1976-168BInstallation of epoxy renin coated flanged bushings, P/N

206-011-128-1, inta M/R hub pillow blocks I NO ASB

AB 206 S/N 8001 - 8153 only, Ref.

Bell(SB) 206-75-3 and FAA AD 75-18-

07 and BT 206-097



206-110 1976-172Insp. of hydraulic servo actuators, P/N 206-076-031, -9 or -

13 (Modet No. 41000670-1, -003 or -005) I NO ASB

AB S/N 8313 and sub. equipped with

servos manuf. by Hydraulic Research

only,



206-112 1976-173Modification of linear actuators, P/N 206-062-721-1 or 206-

062-721-11 (General Design P/N 7185-1) I NO ASB

AB 206 fited with specific actuators

only, Ref. Bell(SB) 206-76-6, BT 206-

112 and General Design (SB)



206-113 1976-187AInstallation of taper washers under hydraulic servo actuator

support assembly, P/N 206-001-520-5 I NO ASB

AB 206 S/N 8001 - 8531 only, Ref.

Bell(SB) 206-76-8 Rev. A and BT 206-

113



206-108 1976-190AInsp. of mein rotor hub tension/torsion strap assembly, P/N

206 010 105 3 I NO ASB

AB 206 fitted with specified TT strap

assembly, see AD for details Ref.

Bell(SB) 206-76-4 Rev. B and BT 206-




206-115 1976-240AInstallation of improved lifter door striker

housing assemblies to lifter door post I NO ASB

AB 206 in lifter configuration only, Ref.

Bell(SI) 206-68 and Bell (SB) 206-76-10

Rev. B and BT 206-115



206-116 1977-042AInstallation of improved tall rotor drive shaft bearings, P/N

206-040-339-9 I NO ASB

AB 206 S/N 8001 - 8259 only, Ref.

Bell(SB) 206-76-12 and BT 206-116




206-040-339-9 II NO ASB

AB 206 S/N 8001 - 8259 only,

Ref. Bell(SB) 206-76-12 and BT 206-

116




206-040-339-9 III NO ASB

AB 206 S/N 8001 - 8259 only, Ref.

Bell(SB) 206-76-12 and BT 206-116





206-117 1977-115Replacement of rotor brake kit, P/N 206-706-009-1, 206-

706-032-1 or 206-706-034, Ilning retention screws I NO ASB

AB 206 equipped with specified rotor

brake kit only, Ref. Bell(SB) 206-77-2

and



206-118 1977-116One time Insp. of tube assembly, P/N 206-061-522-1 or

206-061-541-1 I NO ASB

AB 206 S/N 8001 - 8531 only, Ref.

Bell(SB) 206-77-3 and BT 206-118




Page 11

ASB AC




206-121 1977-173Introduction of reduced mandatory retirement lite for

tension/torsion siraps and improved limit free strap filtings I NO ASB

AB 206 operating in corrosive

atmosphere conditions, Ref. Bell(SB)

206-77-7 and BT 206-121



77-9 206-122 1978-029Replacement of tall rotor drive shaft clamp

type bearing hangers with shims I NO ASB

AB 206 S/N 8260 - 8371 only, Ref.

Bell(SB) 206-77-9 and BT 206-122NA 2013-05-11 CAA-145

77-9 206-123 1978-130Modification of tall rotor drive shaft clamp type bearing

hangers with shims, P/N 206-040-345-1, -346-5 and -338-1 I NO ASB

AB 206 S/N 8260 - 8371 only,

Ref. Bell(SB) 206-77-7 and BT 206-123

(Optional)NA 2013-05-11 CAA-145

1978-154 AD Cancelled AD Cancelled 2013-05-11 CAA-145

206-127 1978-208Insp. of flight control lever assembly, P/N 206 001 339 23,

hearing for adequate stake I NO ASB

AB 206 S/N 8026 8553 not filted with

specified dual controls, Ref. Bell(TB)

206-78-1 and BT 206-127


MFG2013-05-11 CAA-145

1979-004T AD Cancelled AD Cancelled 2013-05-11 CAA-145

206-140 1980-172Torque check and Insp. of tall rotor gearbox, P/N 206-040-

400 (all dash numbers), attachment hardware I YES ASB

AB 206 S/N 8001 8594 only, Ref. BT 206-140

(100 hours)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1



80-7 206-139 1981-019Insp. and replacement of M/R tension trunnion, P/N 206-

010-104-1 and 206-011-113-1 I NO ASB

AB 206 fitted with specified

M/Rtrunnion, Ref. Bell(ASB) 206-80-7

Rev. A and BT 206-139 (600 hours)NA 2013-05-11 CAA-145



80-6 206-148 1981-102Introduction of new retirement life for tall rotor blades, P/N

206-010-750-5 and 206-010-750-7 I NO ASB

AB 206 equipped with specified tall

rotor blades, Ref. Bell(ASB) 206-80-12

and BT 206-146NA DUE TO PN INSTALLED 2013-05-11 CAA-145







1982-161Installation of Flow Monitoring Kit, P/N C-22-FM, to aircraft

fitted with Chadwick Auxiliary Fuel System, P/N C-22 II NO ASB

AB 206 fitted with specified fuel system

only, Ref. FAA (AD) 82-16-12 and

Chadwick (SB) 20-81-01NA EQUIPMENT NOT INSTALLED 2013-05-11 CAA-145

1982-161Installation of warning decal to aircraft fitted with Chadwick

Auxiliary Fuel System, P/N C 22 I NO ASB

AB 206 fitted with specified fuel system

only, Ref. FAA (AD) 82-16-12 and

Chadwick (SB) 20-81-01NA EQUIPMENT NOT INSTALLED 2013-05-11 CAA-145


206-153 1983-075Insp. of engine to transmission driveshaft, P/N 206-040-100-

13 I YES ASB

AB 206 S/N 8001 - 8668 only, (100

hours)NA DUE TO PN INSTALLED 2013-05-11 CAA-145


Page 12

ASB AC




83-21 A 1984-073 One time Insp. of M/R mast, P/N 206-010-332I NO ASB AB 206 S/N 8001 - 8674

C.W. 2013-05-11 CAA-145

1984-073 Introduction of periodis Insp. to M/R mast, P/N 206 010 332II YES ASB

AB 206 S/N 8001 - 8674, Ref. Bell(ASB) 206 83

21 Rev. A (12 months)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1


206-168 1985-170Insp. of M/R blade retaining nuts, P/N 206-011-119-1, with

non metallic locking feature I NO ASB

AB 206 fitted with nuts P/N 206-011-119-

1 equipped with non metallic locking

feature, Ref. BT 206-168NA DUE TO PN INSTALLED 2013-05-11 CAA-145

85-29 206-169 1986-013AInsp. of pilots cyclic control stick assembly and co-pilots

stick I YES ASB

AB 206 only, Ref. Bell(ASB) 206-206-85-29 and

BT 206-169 (600 hour Insp./24months)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

85-28 206-170 1986-024Insp. and replacement of T/R blade ,P/N 206 016 201 1

and 103, tip block rivets I NO ASB

AB 206 S/N 8001 8681 fitted with

specified bladel, Ref. Bell(ASB) 206-85-

28 Rev. B and BT 206-170 (100 hours)NA DUE TO PN INSTALLED 2013-05-11 CAA-145


1987-002

Identification and removal of tall rotor yoke, P/N 206-011-

819-101, combined with crosshead, P/N 206-010-741-001/-

003I NO ASB

AB 206 with specific tall rotor

configurations only, see AD for details,

Ref. FAA (AD) 86-24-01NA DUE TO PN INSTALLED 2013-05-11 CAA-145


87-37 1987-120 Identification of M/R mast, P/N 206-010-332-121I NO ASB

Future servicability of M/R mast

governed by S/N, see AD for details,




1988-215 Indentification of tall rotor yoke, P/N 206-011-819 101I NO ASB

Future servicability of tall rotor yoke

governed by S/N, see AD for details,


1989-019TI NO ASB

C.W. 2013-05-11 CAA-145

78-1 206-126 1989-029Replacement of M/R tension/torsion strap, P/N 206 010 105

3 and 206 010 105 5 I NO ASB

AB 206 equipped with specified M/R

tension/torsion strap, Ref. BT 206-126NA DUE TO PN INSTALLED 2013-05-11 CAA-145


89-43 A 206-189 1989-259AOne time Insp. and replacement of Aeroquip 601 hose

assemblies I NO ASBC.W. INSP 2008-03-13 CAA-145

1989-272R1Mandatory installation of particle separator/intake deflector

on all Bell 206B Jet Ranger I NO ASBC.W. IN WINTER CLIMATE 2013-05-11 CAA-145


1990-006TI NO ASB

C.W. 2013-05-11 CAA-145



COMP 1991-285 AD Cancelled AD Cancelled 2013-05-11 CAA-145


Page 13

ASB AC










91-60 206-202 1992-256 Insp.and addition of mounting spacers for vertical fin

assembly, P/N 206-020-113-5, -7, -9 and -107 II NO ASB AB 206 S/N 8001- 8442 onlyNA DUE TO AC SN 2013-05-11 CAA-145

91-60 206-202 1992-256Insp. and modification of vertical fin supports, P/N 206-031-

417 and 206-031-418 I NO ASB AB 206 S/N 8001 - 8442 onlyNA DUE TO AC SN 2013-05-11 CAA-145

206-194 1992-332A Installation of emergency float bag inflation valve restrictorsI NO ASB

AB 206 equipped with specified

emergency Floats only, see AD for

details.

NA DUE TO EQUIP. NOT

INSTALLED2013-05-11 CAA-145


90-56 A 1993-040Identification of main transmission sungear, P/N 206-040-

662-101 I NO ASB

Future servicability of sungear governed

by S/N, see AD for details.C.W. 2013-05-11 CAA-145

1993-248

Revision of aircraft literature for aircraft filted with Allison

250-C2OR engine power-out warninq sensors, P/N 206-

075-545-001I NO ASB

Ref. Soloy Corporation (SB) No. 02-680

and FAA (AD) 94-15-07

NA DUE TO ENGINE MODEL NOT




06-107 206-211 1994-253A 2006-12Insp. of swashplate support assembly, P/N 206-010-452-1,

206-010-452-5 and 206-010-452-109 I, II YES ASB50 HRS INSP. AFTER 1500 HRS LIFE



MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

93-77 1994-260Insp. of M/R blade, P/N 206-010-200-133, with ' A ' S/N

prefix I NO ASBNA DUE TO PN INSTALLED 2013-05-11 CAA-145

92-69 1995-058Insp. of tall rotor drive skaft hanger hearing support

brackets, P/N 206-030-407, 206-030-433 and 206-033-412 I NO ASBC.W. 2013-05-11 CAA-145

90-54 1995-154Modification of fuel valve switch to add a protective

mechanical switch guard I NO ASBC.W. MOD. 2008-03-13 CAA-145

96-103 1996-163 1996-10Rework of tube assemblies, P/N 206-064-228-001 and 206-

054-229 001 I NO ASB

AD applies to spec. B206L 1, L 3 and L

4 only, see AD, NA DUE TO AC MODEL CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

206-172 1996-193Insp. of tall rotor gearbox, P/N 206-011-810 (all dash

numbers), attachment area I NO ASB

AB 206 equipped with specified T/R

HUB Assy PN: 206-011-810NA DUE TO PN INSTALLED 2013-05-11 CAA-145

1996-281 1996-13

Identification and removal from service of Kratos Turbins

Outlet Temperaturs indicators, P/N 124.444-6 or 124.444-

20I NO ASB

AD applies to Bell 206L-1 fitted with

spec. TOT ind. only, ref. Bell (ASB) No.

206L-94-94

NA DUE TO AC MODEL 2013-05-11 CAA-145

206-223 1997-021 2013-28Fuel cell vent tube decal installation to prevent water

ingestion I YES ASB

(ASB) No. 206 95 156 and 206-95-180, BT 206-

223 Rev. A & TC (AD) CF-96-11 (300

hour/annual)



MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

206-229 1998-283 Insp. of M/R blades, PIN 206-010-200 33I YES ASB

BT applies to M/R blades S/N M3-1501

M3-2057 & EM-0001 - EM-0154 only,

Ref. BT 209-229 (50 hours)

NA DUE TO SN INSTALLED 2013-05-11 CAA-145

206-1 1998-344Removal of hydraulic relief valves, P/N 206-076-036-101,

and replacement with modified item, PIN 206-076-036-105 I NO ASB

AD applies to Bell 407 S/N 53000 -

53266 only, Ref. Bell(ASB) No. 407-98-

20 and TC (AD) CF-98-28


Page 14

ASB AC




206-1 1998-416 Modification and Insp. of tailboomI YES ASB

Ref. Bell(ASB) No. 206L-97-107 Rev. A,

(ASB) No. 206L-87-47 Rev. C and TC

(AD) CF-98-27 (100 hour Insp.)


206-1 1998-453Removal of hydraulic relief valves, P/N 206-076-036-101,

and replacement with modified item, P/N 206-076-036-105 I NO ASB

AD applies to Bell 206L-4 S/N 52001 -

52208 only, Ref. Bell(ASB) No. 206L-98-

111 and TC (AD) CF-98-34


AIRBORNE 1999-102 1998-43AIRBORNE Crosstube assembly identification and fixing

lorations, PN: AB206-050-XXX I NO ASB

Concerns assemblies mfg by AA Inc.,

Bell and any approved P/N .NA, NEW TYPE INSTALLED 2013-05-11 CAA-145

206-232 2000-356 Insp. and verification of fuel hose conigurationII NO ASB

AB 206 S/N 8054 8312 equipped with

specified fuel boost pump(s) only, refer

to Agusta BT 206-232

NA DUE TO AC SN 2000-10-12 CAA-145

COMP 2000-356 Insp. of fuel boost pumps, P/N 206-062-681I NO ASB

AB 206 S/N 8054 - 8312 equipped with

specified fuel boost pump(s) only, Ref.

Parker Airborne SL-50

NA DUE TO AC SN 2000-10-12 CAA-145

206-234 2000-394One time Insp. of tall rotor blades, P/N 206-016-201 (all

dash numbers) I NO ASB

AB 206 fitted with specified tall rotor

blades with less than 25 flight hours.NA DUE TO COMP PN 2013-05-11 CAA-145

206-236 2001-524 Insp. of magnetit brake , P/N 204-001-376 3I NO ASB

AB 206 equipped with specific magnetic

brake only, Ref. Agusta BT 206-236

NA DUE TO EQUIPMENT NOT


2002-217One time Insp. of Kaflex engine to transmission driveshaft

assembly, P/N 206-340-300-105 I NO ASB

Bell 427, 407 and 206L only, Ref. TC

(AD) CF 2002 03 R2NA DUE TO AC MODEL 2013-05-11 CAA-145

206-237 2004-141Insp. of T/R blade, P/N 206-016-201-131 and 206-016-201-

131, skin and balance weight I YES ASB

BT applies to specific serialised

components, Ref. Agusta BT 206-237

and Bell (ASB) 206-04-100 Rev. A (100 NA DUE TO PN INSTALLED 2013-05-11 CAA-145

2004-315Inspection of tail rotor blades, P/N 206-016-201-131 and

206-016-201-133, for cracks on blade(s) trailing edge I YES ASB

Reference (ASB) No. 206-04-100 Rev.

B and TC (AD) CF-2004-05R2 (100

hour/annual)NA DUE TO PN INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

2004-503Removal from service of tall rotor blades, P/N

206-016-201-131 S/N CS4820 - 4825 I NO ASB

Ref. (ASB) No. 206-04-101 and No.

206L-04-131NA DUE TO PN INSTALLED 2013-05-11 CAA-145

2004-512Door handfe Insp., Bell 206B Jet Ranger

S/N 3567 - 4577, 5101 - 5284 I NO ASB

Ref. (ASB) No. 206-04-102 and TC (AD)

CF-2004-27NA DUE TO AC SN 2013-05-11 CAA-145

2005-112Identification and replacement of freewheel aft bearing cap,

P/N 406 040 509 101 I NO ASB

Applies to bearing cap S/N A1833

A1912 only, Bell 407 and 206L only,

Ref. TC (AD) CF-2004-17R1NA DUE TO AC MODEL 2013-05-11 CAA-145

02-99 206-239 2005-406Insp. and rework of M/R blades , P/N 206 010 200 (all dash

nutubers) I NO ASB

BT applies to any M/R blade S/N A

xxxx, Ref. Bell(ASB) 206-02-99 Rev. A

and BT 206-239

NA DUE TO BLADE SN

INSTALLED IS TXXXXCAMO 2013-12-17

MAC, SE MG

0095 ASR-1

05-103 A 2005-496 2005-10R3 Fuel Distribution Electrical Grounding check for complianceI NO ASB

C.W. MOD & INSP 2008-03-13 CAA-145

06-107 206-240 2006-0275 2006-231

Insp. of two piece vertical fin support, P/N 206-031-417-

003/-007 and 206-031-418-001/-005 , Bell 206B S/N 004 -

3906I NO ASB

Intitial Insp. of vertical fin and tailboom

mating surfaces.C.W. 2007-07-17 CAA-145

06-107 206-240 2006-0275 2006-231

Insp. of two piece vertical fin support, P/N 206-031-417-

003/-007 and 206-031-418-001/-005 , Bell 206B S/N 004 -

3906II YES ASB

Repetitive Insp. and torque check of attachment

hardware. (100Hrs)C.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

206-242 2007-0043 2007-058

INSP TO GROOVED CLAMPS & EXHAUST STACK

CLAMP P/N 4656AA OR 4606AC, Insp. AND SAFETY

WIRINGI YES ASB 100 HRS/ANNUAL



MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

2007-123 2007-03Insp. of horizontal stabilizers 206-023 119 167 and 407 023

801 109 I NO ASB

Future servicability of horizontal

stabilizer governed by S/N, Bell 407 and

206L only, Ref. TC (AD) CF-2007-03NA DUE TO AC MODEL 2013-05-11 CAA-145

2007-125Identification of transmission pylon support spindle, P/N

206 031 554 I NO ASB


components manufactured by Cadorath

Aerospace Inc. And H-S Tools & Parts C.W. INSP 2008-03-13 CAA-145

206-243 2007-324Insp. of tall rotor drive disc assembly, P/N 32721-1,

manufactured between 01/11/05 - 30/11/06 I NO ASB

AB 206 filted with specified tall rotor

drive assembly only.C.W. INSP 2008-03-13 CAA-145

07-116 B 206-248 2010-0272-E 2007-347 2007-21R1

T/R BLADES 206-016-201-127/131/-133/-135/-137,


SERVICE OF. SNSI NO ASB



07-115 C 206-244 2009-0022-E 2007-353 2007-13R2Power Turbine RPM Operational Warning, Bell 206 S/N 0-

4366I

NO ASB

R&R CEB-A-1400, PLACARD P/N 230-

075-213-125

C.W PART I, PART II RFM REV 8.,

AGUSTA RFM, AND PLACARD

INSTALLATION

2008-03-13 CAA-145

07-114 07-03 2007-357 2007-16 DISC ASSEMBLY P/N 32721-1, INSPECTION OF I, IINO ASB

DISC MFG BETWEEN NOV 1-2005

AND NOV 30-2006C.W CHECK 2008-03-13 CAA-145

Page 15

ASB AC




2007-359Identification of transmission pylon support spindle, P/N

206 031 554 I NO ASB


components manufactured by Cadorath

Aerospace Inc. And H-S Tools & Parts C.W CHECK 2008-03-13 CAA-145

05-103 A 2007-373 2005-10R3 Fuel distribution system Insp. and modification I,II, III, IV1 YES ASB

Ref. (ASB) No. 206-05-103 Rev. A and

TC 2005-10 R3 (24 month Insp./clean,

Part IV)C.W. MOD & INSP. CHECK INSTL 2008-03-13 CAA-145


4366I

NO ASB


075-213-125



INSTALLATION

2008-03-13 CAA-145

07-115 C 206-244 2009-0022-E 2009-033 2007-13R2Introduction Power Turbine RPM (N2) steady state

operation avoidanceI

NO ASB


075-213-125



INSTALLATION

2009-03-23 CAA-145

09-121 2009-084One time Insp. of cyclic control lever assembly, P/N 206-

001-401-111, 206-001-400-115 and 206-001-400-111I

NO ASB

AD requires Insp. of cyclic control lever

bearing P/N 206-301-501-101 staking, C.W CHECK 2009-03-31 CAA-145

206-245 2009-096One time Insp. of M/R pitch horn trunnion bearing, P/N 206

011 105 001I

NO ASB

AD requires visual Insp. and purge

lubrication of bearing to verify

lubrication passage.C.W CHECK 2009-03-26 CAA-145

09-122 04-sep 2009-264 2009-32 STAKED BEARINGS, ONE-TIME INSPECTION OF INO ASB

AD requires Insp. of component bearing

staking.C.W CHECK 2009-09-09 CAA-145

09-120 2009-313One time Insp. of M/R pitch horn trunnion bearing, P/N 206

Oll 105 001I

NO ASB

AD requires Insp. and purge lubrication

of bearing to verify lubrication passage.C.W CHECK 2009-03-26 CAA-145

09-121 2009-343One time Insp. of cyclic control lever assembly, P/N 206-

001-401-111, 206-001-400- 115 and 206-001-400-111I

NO ASB

AD requires Insp. of cyclic control lever

bearing P/N 206-301-501-101 staking.C.W CHECK 2009-03-31 CAA-145


4366I

NO ASB


075-213-125



INSTALLATION

2008-03-13 CAA-145

2009-435Introduction of additional fight control check before engine

shut downI

NO ASB

AD requires addition of the Bell

Helicopters Flight Manual revision D-45

(206A), revision B-51 (206B) or revision C.W. LATEST RFM REV CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

09-123 2010-073 2007-16 Identification and removal of disc assembly, P/N 101584-2 I, IINO ASB

DISC MFG BETWEEN NOV 1-2005

AND NOV 30-2006C.W CHECK 2010-02-22 CAA-145

63 2007-0089206 series hcp that have the following Transmission Pylon


P.C.W. PART I , AT AC DATE

2007.4.18


BY REPAIR OR SN INSTALLEDCAMO 2013-12-17

MAC, SE MG

0095 ASR-1

63 2007-0257206 series hcp that have the following Transmission Pylon


P.C.W. PART I , AT AC DATE

2007.10.2


BY REPAIR OR SN INSTALLEDCAMO 2013-12-17

MAC, SE MG

0095 ASR-1

206-244 2009-0022-EPOWER TURBINE RPM (N2) STEADY STATE

OPERATION AVOIDANCE, INTRODUCTION OFI, II

NO ASBR&R CEB-A-1400

C.W PART I, PART II RFM REV 50

& DECAL, NA DUE TO WHEEL NO

3 PN

CAMO 2013-12-17MAC, SE MG

0095 ASR-1

206-245 2009-0067-EM/R PITCH HORN TRUNNION, BEARING 206-011-105-

001, ONE TIME CHECK,I

NO ASB

CHECKED IN LOCATION WITH

GREASE GUNCAMO 2013-12-17

MAC, SE MG

0095 ASR-1

206-247 2009-0226

ONE TIME INSPECCTION OF BEARINGS P/N 206-301-

051-101, INSTALLED ON LEVER ASSY P/N 206-001-339-

015

INO ASB

P.C.W BT 206-247 CAMO 2013-12-17MAC, SE MG

0095 ASR-1

2013-0020EQUIPMENT & FURNISHING-SAFETY BELTS CHECK

REMANUFACTURER STATUS W/O ETCI

NO ASB

NA DUE TO INSTALLATION

MISSING, LEAD ACID BATT G-641

INSTALLED


0095 ASR-1

2013-0040-EELECTRICAL POWER - BATTERY OVERHEAT SENSOR

INSPI

NO ASB

NA DUE TO INSTALLATION

MISSING, LEAD ACID BATT G-641

INSTALLED


0095 ASR-1

206-239 IT-2005-406M/R BLADES, P/N206-010-200-ALL Insp. AND REWORK

OF, BLADES WITH SUFFIX A-XXX I, II, III NO ASB

C.W PART I, PART II & III NA DUE TO

STATUS OF P I

NA DUE TO BLADE PN-SN

INSTALLEDCAMO 2013-12-17

MAC, SE MG

0095 ASR-1

04-102 05-02 2004-27INSIDE DOOR HANDLE ASSEMBLY P/N 206-031-620-

101, INSPECTION AND REWORK OFI

NO ASBAC SN 3567 UP TO 4577 NA DUE TO AC SN 2013-05-11 CAA-145

05-104 05-05 2005-22 TORQUE INDICATOR 206-075-739-125, RECALL OF INO ASB

206-075-185-1, INSTL. NA DUE TO PN INSTALLED 2013-05-11 CAA-145

09-120 09-02 2009-34MAIN ROTOR PITCH HORN TRUNNION, BEARING 206-

011-105-001, ONE TIME CHECK,I

NO ASB

C.W CHECKED IN LOCATION

WITH GREASE GUN2009-03-26 CAA-145

09-123 A 09-06 2010-07 DISC ASSEMBLY 101584-2, RECALL OF INO ASB

PN 32721-1 IS OK C.W PN VERIFICATION CONTROL 2010-02-24 CAA-145

Page 16

ASB AC




11-127 2012-19CONTROL BOX ASSEMBLY P/N 206-375-017-101,

RECALL OF.I

NO ASB

NA AUTO RELIGT INSTALLATION

MISSING2012-02-20 CAA-145

95-165 2013-28FUEL CELL VENT TUBE WATER INVESTIGATION,

INSTAL FUEL VENT TUBE DECAL AT OUTLET OF TUBEI

YES ASBC.W ANUALLY OR 300 HRS, SS AD CF-96-11



MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

95-84 1995-11R2Hydraulic Servo Actuators (HR Textron) Shoulder Bolts,

One Time Inspection ofI

NO ASBNA DUE TO P/N INSTALLED 2008-03-13 CAA-145

AA-94045 1995-17R2AA - PN 206-320-101, BELL LANDING GEAR

CROSSTUBE INSPECTIONI

YES ASBC.W ANUALLY OR 300 HRS NA DUE TO PN INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

GEN 1972-09Blade retention fittings, P/N 206-010-155-7 installed shall

have these fittings replaced by P/N 206-010-155-11 or -15 I

NO ASBPERFORMED AT FACTORY AT MFG 1978-01-01 AGUSTA

GEN 1978-09206B helicopters fitted with front seat belt Support

Assemblies, P/N 206-030-126-7 or -007I

NO ASBPERFORMED AT FACTORY AT MFG 1978-01-02 AGUSTA

GEN 1991-35

The cabin roof boxbeam assembly (P/N 206-031-200-all

dash numbers) is a primary load bearing member subject to

fatigue.

IYES ASB

C.W ANUALLYC.W INSP. CHECK, INSTRUCTION


MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

GEN 1998-15 EXTERNAL RESCUE SYSTEM BREEZE EASTERN INO ASB

NA NOT INSTALLED 2013-05-11 CAA-145

206-11-

197M/R BLADE 206-010-200-033/-133/-137/-139/-141 I

NO ASB OPTIONALC.W INSTALLATION

206-219I NO ASB

C.W INSP 2013-05-11 CAA-145

206-226 INSPECTION OF WINDSHIELDI NO ASB



MAC

13-0782013-12-01

SE.145.0113

MAC AT-1

2009-43HYD SYS: BHT-206B-FM-1, Rev B-51, DATED 2 July

2009, or FM Supplement Rev.12 Dated 2 July 2009I

NO ASB REV RFM STATUS C.W RFM REV CHECK 2013-05-11 CAA-145

(Apical), emergency float kit installed under Supplemental

Type Certificate (STC) Number SR01535LA, I NO ASBNA NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

89-49

emergency float bags, part numbers (P/N) 206-050-248-

107, -109 and -111 manufactured prior to September 1,

1989.I NO ASB

NA NOT INSTALLED CAMO 2013-12-17MAC, SE MG

0095 ASR-1

If the tail rotor blade assembly installed is P/N 206-016-201-

113 or P/N 206- 016-201-127 I NO ASBNA NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

MR blades (P/N) 206-015-001-001, 206-015-001-103, 206-

015-001-105, or 206-010-200-033 insta I NO ASBNA NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

with tail rotor blade assembly, P/N 206-016-201-125 or -

127. I NO ASBNA NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

To prevent failure and separation of the main rotor blades,

and subsequent loss of the helicopter, accomplish the

followingI NO ASB

NA SN NOT INSTALLED CAMO 2013-12-17MAC, SE MG

0095 ASR-1

250-C20R engine power-out warning sensors,(P/N) 206-

075-545-001, in accordance with (STC) No. SH4169NM I NO ASB STCNA NOT INSTALLED CAMO 2013-12-17

MAC, SE MG

0095 ASR-1

Page 17

CYCLES LIFE ITEMS HELICOPTER AGUSTA BELL AB206B

REG A/C TYPE YEAR OF MFG A/C S/N ENG TC Rev L. NO DATE T.T HRS AC Ldgs AC Starts ENG. CSN TSN

SE-HZZ AB 206B II 1978 8554 IM.E.052 Issue 1 22.6.11 7-1-2014 14210,1 UNK 14721 ##### 14084,4

Wo No: DATE:

ENGINE INSTALLATION : LIFE / TBO / CYCLES PAGE: 1 OF 1

E-Type Eng.S/N Install. Date A/C Hrs A Starts E.TSN CSN CSO DIFF AC-ENGINE HRS126, 1 PLUS TO AIRFRAME Sign: LIC No:

250-C20 822933 17-nov-03 13105,4 13178 12979,7 13178 NEW Installed Engine Time Component Time Due Eng Time Available To Go Service.Action Work Action Complied With

ATA Name Part No. Serial No. Life Tbo Days Cycle Date Hrs CSN TSN/TSOCycle Days Hrs Cycle Hrs Cycle DaysRemarks Wo No A/C Hrs Date Lic No.

7230 Comp. Coupling 6898561 48506 3500 15-5-2012 13901,7 3121,9 14279,8 195,4 OH

7230 Comp. Tiebolt 6871259 46082 3500 15-5-2012 13901,7 3121,9 14279,8 195,4 OH

7230 Compressor Assy 6890550 CAC-24466 3500 16-5-2012 13902,7 3121,9 14280,8 196,4 OH

7530 Bleed Valve 23053176 FF38515 1500 28-3-2003 12801,3 0,0 14301,3 216,9 OH

7230 Compr. Impeller 6876873 KR82790 3550 9150 15-5-2012 13901,7 14545 3121,9 3395 14329,8 20300 245,4 5579 LIFE

7325 FCU High Press Filter 1730791-02-41 NSN 200 24-1-2013 14141,0 0,0 14341,0 256,6 LIFE

7240 Turbine "HMI" 23038241 CAT-36727 1750 15-5-2012 13901,7 1229,6 14422,1 337,7 HMI

7240 Turbine Whl. No 2 6898782 HX111463 1775 3000 15-5-2012 13901,7 14545 1229,6 2407 14447,1 15138 362,7 417 LIFE

7240 Turbine Whl. No 1 6886407 X128273 1775 3000 15-5-2012 13901,7 14545 1229,6 2407 14447,1 15138 362,7 417 LIFE

7230 Compressor Case 23057142 15892 500 730 24-1-2013 14141,0 0,0 0 14641,0 556,6 CORRO/CRACK INSP.

7240 Turbine "OH" 23038241 CAT-36727 3500 15-5-2012 13901,7 2659,6 14742,1 657,7 OH


7230 Compressor Case 23057142 15892 1750 24-1-2013 14141,0 0,0 15891,0 1806,6 HMI INSP. MAND.

7310 Fuel Nozzle 23077068 AG54525 2500 26-6-2006 13576,0 145,8 15930,2 1845,8 OH

7620 Governor "CECO" 23006259 3AAD2451 4000 12-10-2000 12310,6 0,0 16310,6 2226,2 OH

7320 Fuel Control "CECO" 23061824 3AAC2424 4000 17-9-2004 13106,6 43,9 17062,7 2978,3 OH


7330 Fuel Pump TRW 6899253 T2852 4000 30-11-2011 13878,0 0,0 17878,0 3793,6 OH

7240 Turbine Nozzle Shield 23073533 NSN 1000 15-5-2012 13901,7 14545 23,7 50 15495 774 INSP CEB 1370R6

7240 Turbine Tie Bolt 23068265 NC85704 9000 15-5-2012 13901,7 14545 23,7 50 23495 8774 LIFE CEB 1371R2

7210 Gearbox 6877180 CAG-20749 BA O/C 15-5-2012 13901,7 0,0 O/C C.M

CAMO SE.MG0095, ASR-1

16-Aug-1313-078

ENGINE STATUS LIST "ESL" 1 Komponentlista airframe SE-HZZ ny

ESB Engine

MANDATORY SERVICE BULLETINES "ESB" W:O RECOMMENDED OPTIONAL

ENG.SN: EASA TCDS EASA & FAA ADs Page 1 of 1 PRE COMPLIED WITH PARTIALLY PERFORMED CANCELLED

822933 IM.E.052 Rolls Royce 250-C20B Bi-Weekly NOT PERFORMED PERFORMED NOT APPLICABLE

MO sb SB rev FAA-AD EASA/ENA

C

ACTION PAR

TREP DUE CAT REMARK CODE MTD. OF COMPLIANCE WO NODATE INSP

FC A

CSL-

1166 2004-0009R2

TORQUE LOAD ON "B" NUTS

I 100 1 ASB100 HRS INSP, REF

EASA ADX

C.W TORQUE CHECK ITEMS LISTED

IN MAC TI-005, MAC WO 13-047

MAC

13-078

EGCSL-

1005 13

TIME LIMETED PARTS

I 300 100 ASB XC.W RESEARCH NEXT DUE 2014-11-

15CAMO 30-Nov-13

SE.MG.0095

MAC-ASR-1

EGCSL-

1004 20

TIME BETWEEN OVERHAUL

I 300 100 ASB XC.W RESEARCH NEXT DUE 2014-11-

15CAMO 30-Nov-13

SE.MG.0095

MAC-ASR-1

SE-HZZ

A/C REG:

13-078

2013-25

PCW___

CODE

ASB - 1 2 3-7

CAT

NA

Page 2

EMPTY WEIGHT & EQUIPMENT BALANCE RECORDAIRCRAFT MODEL SERIAL NUMBER REGISTRATION PAGE of

AB 206B II 8554 SE-HZZ 2

WEIGING COMPANY REPORT DATE W/O LOADING VERSION

LOADMASTERS 12MA6632 5-11-11 5 Seat & High Skid

Load Cells Location Scale Tare Net Tare Long C.G Moment Lat C.G Moment

Fwd Jackpoints L/H Main 0,0 55,16 0 -17,00 0

Fwd Jackpoints R/H Main 0,0 55,16 0 16,82 0

Aft Jackpoints 0,0 179,92 0 0,00 0

Total Weight lb 1883,0 115,78 218022 0,00 0

Required Equipment Installed at

WeighingPN SN WEIGHT LONG C.G MOMENT LAT C.G MOMENT

Standard Equipment

Altimeter & Encoder B4515210011 2,0 37,0 74 11,0 22,0

Airspeed Ind "8000" 206-075-725-001 0,8 38,0 30 4,3 3,4

Dual Tachometer 206-075-681-115 1,9 38,0 72 4,3 8,2

Gas Producer Tachometer 206-075-682-105 0,7 38,0 27 1,3 0,9

Fuel Pressure & Loadmeter 206-075-676-107 1,0 38,0 38 -1,3 -1,3

Fuel Quantity Ind. 206-075-740-107 0,8 38,0 30 -1,3 -1,0

Torque Meter Ind. 206-075-739-107 0,6 38,0 23 1,3 0,8

Turbine Outlet Temperature Ind 206-375-005-101 1,0 38,0 38 1,3 1,3

Engine Oil Pressure/Temperature 206-075-677-103 0,6 38,0 23 -1,3 -0,8

XMSN Oil Pressure/Temperature 206-075-678-105 0,6 38,0 23 -1,3 -0,8

Outside Air Temp Ind. 206-075-624-001 0,2 53,0 11 3,0 0,6

Compass Magnetic Standby MC-NS51A 0,7 33,0 23 23,0 16,1

Clock 8 Days 206-070-275-005 0,5 38,0 19 1,2 0,6

Caution Panel 75-0286-13 1,4 42,0 59 3,0 4,2

Anti-Collision Light - Strobe 01-0770019-21 0,5 341,0 171 6,0 3,0

Anti-Collision Light - Power supply A490ATS-DF 1,5 160,8 241 11,2 16,8

Position Lights LH&RH AN3033-12/13 0,6 263,0 158 0,0 0,0

Landing Lights (2) 206-075-303-001 1,6 12,0 19 0,0 0,0

Tail Light A-2064-1683 0,2 363,0 73 0,0 0,0

Map Light 90-004-4 0,3 80,5 24 0,0 0,0

Starter Generator 2308-027 17,6 145,0 2552 5,0 88,0

Safety Belts - Pilot 222-320-823-125 1,5 67,0 101 14,0 21,0

Safety Belts - Copilot/Fwd Passenger 222-320-823-125 1,5 67,0 101 -11,0 -16,5

Safety Belts - Aft Passenger L.H 222-320-841-111 1,5 108,0 162 -17,0 -25,5

Safety Belts - Aft Passenger Center 222-320-841-115 1,5 108,0 162 0,0 0,0

Safety Belts - Aft Passenger R.H 222-320-841-111 1,5 108,0 162 17,0 25,5

Flight Manual BHT-206B3-FM-1 1,7 37,0 63 -24,0 -40,8

Fire Extinguisher "Halon 1211" 3,1 85,0 264 -1,1 -3,4

First Aid Kit BCL D 1.10 1,8 160,0 288 0,0 0,0

Battery,Gill G-641 206-706-330 26,5 15,0 398 1,0 26,5

Tubular High Skid Gear 206-706-031-001 62,0 95,2 5902 0,0 0,0

Optional Equipment Installed at

WeighingPN SN WEIGHT LONG C.G MOMENT LAT C.G MOMENT

AF Fuel Filter 206-706-603-003 4,3 150,4 647 -4,5 -19,4

Audio Panel KMA24H 1,7 43,5 74 6,8 11,5

Paravion Bleed Air Heater 33,2 108,6 3606 -1,0 -33,2

ILS KN63 1,5 43,5 65 0,0 0,0

ELT Antenna CI318-1 0,3 88,0 26 0,0 0,0

Flap Restraint 206-706-013 2,7 107,1 289 0,0 0,0

Flight Instruments 206-706-323-019 10,1 37,6 380 5,3 53,5

Flite Steps 0 0,0 0,0

EMPTY WEIGHT & EQUIPMENT BALANCE RECORDAIRCRAFT MODEL SERIAL NUMBER REGISTRATION PAGE of

AB 206B II 8554 SE-HZZ 2

WEIGING COMPANY REPORT DATE W/O LOADING VERSION

LOADMASTERS 12MA6632 5-11-11 5 Seat & High Skid

Floor Protectors 0 0,0 0,0

4ea Wedge Windows 0 0,0 0,0

Range Extender 0 0,0 0,0

Hobbs Meter 206-706-102-1 0,2 20,0 4 0,0 0,0

Maintenance Step L/H STC SH1281SO 1,5 120,8 181 -27,0 -40,5

Night Flying 206-706-340 11,2 117,7 1318 3,6 40,3

Pass. Door Locks 206-706-011 0,4 92,9 37 0,0 0,0

Rotor Brake, "Dual Caliper" 206-706-034 0 0,0 0,0

NAV KN53 2,8 39,6 111 0,0 0,0

Transponder Equipment KT 79 206-705-008-117 2,8 39,6 111 0,0 0,0

Transponder Provisions 206-075-008-115 1,0 43,7 44 -1,2 -1,2

VHF Antenna 206-898-653-101 1,5 283,0 425 0,0 0,0

COM/NAV KX165 7,7 41,6 320 0,0 0,0

5 ea Headsets Bose 41,6 0 0,0 0,0

VHF COMM KY-196B 0 0,0 0,0

Windshield Defog 206-706-131- 1,3 68,0 88 0,0 0,0

VOR & IND KN53 0 0,0 0,0

Cargo Hook Provision 206-706-335-005 4,1 81,8 335 -2,3 -9,4

Helicopter as Weighed 1883,0 115,78 218022 0,00 0,0

WEIGHT EMPTY DERIVATION Remove:

Undrainable Fuel (Jet A-1) 0,0 130,0 0 0,0 0,0

Ballast 0,0 13,0 0 -2,5 0,0

Useable Oil 0,0 179,0 0 0,0 0,0

WEIGHT EMPTY DERIVATION Add:

Unusable Fuel (Jet A-1) 0,0 120,1 0 0,0 0,0

Ballast 0,0 13,0 0 -2,9 0,0

Ballast 0,0 18,6 0 4,7 0,0

Ballast 0,0 35,8 0 -3,0 0,0

Helicopter Delivery Empty Weight 1883,0 115,78 218022 0,00 0,0

TS: TILÄGG TILL GRUNDSPECIFIKATIONEN BASIC WEIGHT AND BALANCE RECORD(CONTINUOUS HISTORY OF CHANGES IN STRUCTURE OR EQUIPMENT AFFECTING WEIGHT AND BALANCE)

AIRCRAFT MODEL SERIAL NUMBER REGISTRATION NUMBER PAGE OF LOADING VERSION MTO

AB 206B II 8554 SE-HZZ 1 1 5 Seat & High Skid 3200

WEIGHT CHANGES RUNNING TOTAL

DATE ITEM NO. DESCRIPTION OF ARTICLE OR MODIFICATION LB ADDED (IN ) LB/IN REMOVED (-) LB IN BASIC AIRCRAFT

Item IN OUT WEIGHT LONG C.G MOMENT LAT C.G MOMENT WEIGHT LONG C.G MOMENT LAT C.G MOMENT

0 11-May-12 X Brought Forward From. LOADMASTERS 1883,0 115,78 218022 0,0 0

1 15-Nov-13 X ELT KANNAD 406AF-H 2,62 37,20 97 0,0 0

2 15-Nov-13 X ELT KANNAD 406AF-HMounting Bracket 1,94 37,20 72 0,0 0

3 15-Nov-13 X ELT KANNAD 406AF-HRC200 RCP 0,22 50,00 11 0,0 0

4 15-Nov-13 X ELT KANNAD 406AF-HAntenna 0,33 61,00 20 0,0 0

5 0 0,0 0

6 0 0,0 0

7 0 0,0 0

8 0 0,0 0

9 0 0,0 0

10 0 0,0 0

11 0 0,0 0

12 0 0,0 0

15-Nov-13 X New Calculated Weight & Balance 5,1 103 0 1888,1 115,5 218125 0,0 0

*MALMSKOGENS AEROCENTER" CERTIFIES THAT THE WORK SPECIFIED EXCEPT AS OTHERWISE SPECIFIED WAS CARRIED OUT IN ACCORDANCE WITH PART-145, AND IN RESPECT TO THAT WORK THE AIRCRAFT IS CONSIDERED READY FOR RELEASE TO SERVICE.

W.O NO: 13-078 DATE: 2013-11-15 LIC NO: SE.145.0113, AT-01 SIGN:....................................

ITEM NO DATE LOCATION ORGANISATION NAME SIGN

1-4 2013-11-15 Linköping MAC,SE.145.0113, AT-01 Lasse Dahlberg _______________

TS: L1 LASTPLAN LOADING EXAMPLE FWD & AFT

WEIGHT BROUGHT FWD.TO THE PILOT FLIGHT MANUAL WEIGHT BROUGHT FWD.TO THE PILOT FLIGHT MANUAL

WEIGHT 1888,1 LB 849,6 KG WEIGHT 1888,1 LB

LONG ARM C.G 115,5 IN 293,44 CM LAT ARM C.G 0,0 IN Lat CG Limit, Left 3in, Right 4in

MOMENT 218125 LB.IN 249317 KG.CM LAT MOMENT 0,0 LB.IN

FORWARD CG LOAD EXAMPLE AFT CG LOAD EXAMPLE AFT CG Limit with Fwd Door Off 110 in

MOST FORWARD CG; IN 106 1,2 Longitudinal Lateral MOST AFT C.G Inch 111,6 -0,2 Longitudinal Lateral

Most Fwd Load Items Each Weight Long CG Moment Lat CG Moment Most Aft Load Items Each Weight Long CG Moment Lat CG Moment

Weight Empty 1888,1 115,5 218125 0,0 0 Weight Empty 1 1888,1 115,5 218125 0,0 0

Pilot 1 180 180,0 65,0 11700 14,0 2520 Pilot 1 180 180,0 65,0 11700 14,0 2520

Passenger Fwd 1 170 170,0 65,0 11050 -11,0 -1870 Passenger Aft 3 170 510,0 104,0 53040 0,0 0

Passenger Aft 3 170 510,0 104,0 53040 0,0 0 Oil Engine 8 1 8,0 179,0 1432 0,0 0

Oil Engine 8 1 8,0 179,0 1432 0,0 0 Fuel Max LB 618,8 1 618,8 117,7 72833 0,0 0

MTO 3200 lb Total 2756,1 107,2 295347 0,2 650 MTO 3200 lb Total 3204,9 111,4 357130 0,8 2520

*MALMSKOGENS AEROCENTER" CERTIFIES THAT THE WORK SPECIFIED EXCEPT AS OTHERWISE SPECIFIED WAS CARRIED OUT IN ACCORDANCE WITH PART-145, AND IN RESPECT TO THAT WORK THE AIRCRAFT IS CONSIDERED READY FOR RELEASE TO SERVICE.

W.O NO: 13-078 DATE: 2013-11-15 LIC NO: SE.145.0113, AT-01 SIGN:.......................................

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