cessna 208 c208 675hp 1998 poh cessna-caravan-updated-to
TRANSCRIPT
FAA ,APPROVED AIRPLANE FLIGHT MANUALS
THIS TEMPORARY REVISION REVISES FUEL QUANTITY VERSUS DEPTH INFORMATION WHEN USING THE DIPSTICK REQUIRED BY CAB04-1 ON BOTH LEFT AND RIGHT WING L.EADING EDGE IN THE PILOT'S OPERATING HANDBOOK.
( INSERT THE , PROVIDED LIST OF TEMPORARY REVISIONS, AND
( ,r-" THE TEMPORARY REVISION INTO THE PILOT'S OPERATING ( \0~')' HANDBOOK 'IN ACCORDANCE WITH ' THE FILING
,INSTRUCTIONS IN EACH REVISION.
For Training Purposes Only
3 February 2004 208PHTR .
LIST OF TEMPORARY REVISIONS MODEL ~eERIES208 (
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Following is the List of Temporary Revisions that may be inserted into this " ( Pilot's Operating Handbook. . i (
Insert this page opposite the first page of the Log of Effective Pages in the front of the Pilot's Operating Handbook.
TEMPORARY MANUAL ISSUE
REVISION SECTION/ DATE
208PHTR02 208PHTR02
208PHTR02 3/EMERGENCY 23 September
TEMPORARY REVISION 208PHTR03 APPROVED BY
'AA APPROVED UNDER FAR 21SUBPART J rl\lj Ceqn. Aircraft Co
0010g81100 Option' Authonzalion 00A·230428-Ce
SERVICE BULLETIN
208PHTR
Section 4, NORMAL PROCEDURES
Insert this temporary revision into the Pilot's Operating Handbook.
( In Section 4, NORMAL PROCEDURES, insert the temporary revIsion
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208PHTR03
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For Training Purposes Only
PILOT'SOPERATING HANDBOOK TEMPORARY REVISION
Cessna 208 MODEL SERIES
SECTION 4 - NORMAL PROCEDURES
A WARNING
It is essential in cold weather to remove even small accumulations of frost, ice, or snow from the wing and control surfaces. Also, make sure the control surfaces contain no internal accumulations of ice or debris. Prior to any flight in icing ' conditions, check that pitot/static source and stall warning heaters are warm to touch after turning pitot/static and stall heat switches on for 30 seconds, then off. Make sure the pitot covers are removed.
1. Wing Strut Deice Boots -- CHECK for tears, abrasion and cleanliness. 2. Wing Tie-Down -- DISCONNECT. 3. Wing Deice Boots -- CHECK for tears, abrasions and cleanliness. 4. Stall Warning Vane -- CHECK freedom of movement, audible warning
and warmth. (For aircraft equipped with a stall warning ground disconnect switch, check audible warning with elevator off forward stop).
5. PitoVStatic Tube -- CHECK security, openings for stoppage and warmth. ,
6. Landing and Taxi Lights ~- CHECK condition and cleanliness. 7. Fuel Quantity -- USE DIPSTICK required by CAB04-1 to check fuel
level. See Figure TC-l for fuel quantity versus depth.
A CAUTION
8. Fuel Filler Cap -- SECURE.
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9. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and airplane parked with one wing low on a sloping ramp) -- DRAIN (using fuel sampler) to check for water, sediment, and proper fuel before each flight and after each refueling. If water is observed, take further ( samples until clear. Take repeated samples from all fuel drain points ( .(, until all contamination has been removed. \.
10; NaVigation and Strobe Lights -- CHECK for condition and cleanliness.
3 February 2004 208PHTR03 For Training Purposes Only
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Universal XL Fuel Gage Fuel Quantity Gage Scale Gal lbs
0.50 87.4 585 0.75 91 .1 610 1.00 94.7 634 1.25 98.2 658 1.50 101.8 682 1.75 105.2 705 2.00 108.6 727 2.25 111.9 750 2.50 115.1 771 2.75 118.3 793 3.00 121.5 814 3.25 124.5 834 3.50 127.5 855 3.75 130.5 874 4.00 133.4 894 4.25 136.2 912 4.50 138.9 931 4.75 141.6 949 5.00 144.3 966 5.25 146.8 984 5.50 149.3 1000 5.75 151 .8 1017 6.00 154.1 1Q33 6.25 156.5 1048 6.50 158.7 1053 6~75 160.9 1078 7.00 163.0 1092 7.25 165.0 1106
Figure TC-1. Measure
Generic Fuel Gage - Inches Fuel Quantity ncnes Gal . Lbs
0.50 88.4 592 0.75 92.6 . 621 1.00 96.7 648 1.25 100.8 675 1.50 104.7 702 1.75 108.6 727 2.00 112.4 753 2.25 116.1 778 2.50 119.7 802 2.75 123.2 826 3.00 126.7 849 3.25 130.1 871 3.50 133.4 894 3.75 136.G 915 4.00 139.7 936 4.25 142.8 956 4.50 145.7 976 4.75 148.6 996 5.00 151.4 1015 5.25 154.1 . 1033 5.50 156 .. 8 1050 5.75 159.3 1068 6.00 161.8 1084 6.33 · 165.0 1105
d Fuel Depth vs Fuel Quantity
For Training P\Jrposes On'y 3 February 2004
208PHTR03
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VRIGHT WING Leading Edge
A WARNING It is essential in cold weather ,to remove even small accumulations of frost, ice, or snow from the wing and control surfaces. Also, make sure the control surfaces contain no internal accumulations of ice or debris.
1. Navigation and Strobe Lights -- CHECK condition and cleanliness. 2. Fuel Quantity -- USE DIPSTICK required by QAB04-1 to check fuel
level. See Figure TC-1 for fuel quantity verSus depth.
A CAUT10N
3. F'uel Filler Cap-- SECURE.
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5. PitoVStatic Tube -- CHECK security, . openings 'for stoppage , and warmth.
6. Landing and Taxi Lights -~ CHECK conditibn .~nd cleanliness. 7. Wing Deice Boots-- CHECK for tears, abrasl9~ and cleanliness. 8. Radome -- CHECK condition and security. :' \ . 9. Wing Tie-Down -- DISCONNECT. ' '~
10 .. Wing Strut Deice Boots -- CHECK for tears, abrasion,and cleanliness. 11 . Inboard Fuel Tank Sump and External Sump Quick-Drain Valves -
DRAIN (using fuel sampler) to check for water, sediment, arid proper fuel before each flight and after each refueling. If water is observed. take further samples until clear. Take repeated samples from aliluel drain pOints until all contamination has been removed.
12. Main Landing Gear -- CHECK proper tire inflation and gear condition.
3 February 2004 208PHTR03 For Training Purposes Only
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THIS TEMPORARY REVISION REPLACES TEMPORARY . REVISION 208PHTR01 DATED 8 SEPTEMBER 2003 AND REVISES
FLAP USAGE INFORMATION IN ·SECTIONS 2, 3, 4 AND 5 OF THE PILOT'S OPERATING HANDBOOK.
INSERT THE PROVIDED LIST OF TEMPORARY REVISIONS, AND THE TEMPORARY REVISION INTO THE PILOT'S OPERATING HANDBOOK· IN ACCORDANCE WITH THE FILING INSTRUCTIONS IN EACH REVISION.
For Training Purposes Only
For Training Purposes Only
23 September 2003 208PHTR
All Cessna Model 208 Series
The following List of . Temporary Revisions must be inserted into this Pilot's Operating Handbook. (
Insert this page opposite the first page of the Log of Effective Pages in the frontof the Pilot's Operating Handbook.
TEMPORARY MANUAL ISSUE REVISION . . SECTIONI DATE
NUMBER TOPIC
208PHTR02 .. 208PHTR02
20BPHTR02 3/EMERGENCY 23 September
TEMPORARY REVISION 208PHTR02 APPROVED BY
FAA APPROVED UNDER FAR 21 SUBPART J The C_ 1.ircr8ft co.
Del"llation Option Authoriulion DOA-23042B-CE
~. ~3 SE..PTEM&R. :l003
208PHTR
Section 2, LIMITATIONS, . EMERGENCY PROCEDURES, NORMAL PROCEDURES, and PERFORMANCE.
Section Section Section
3, 4, 5,
Insert this temporary revision into the Pilot's Operating Handbook.
In Section 2, LIMITATIONS, insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 2 pages containing the information that is shown in this -temporary revision. .
_ In Section 3, EMERGENCY PROCEDURES; insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 3 pages containing the information that is shown in this temporary revision.
In Section 4, NORMAL PROCEDURES, insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 4 pages containing the information that is shown in this temporary revision.
In Section 5, PERFORMANCE, insert the. temporary revision pages adjacent to the current Pilot's Operating Handbook Section 5 pages containing the information that is shown in this temporary revision.
Discard any pages of this temporary revision that are not applicable to your model/serial airplane.
For Training Purposes Only 23 September 2003
20BPHTR02
For Training Purposes Only
PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
The flap motor and STBY flap motor circuit breakers must be pulled and collared. (place a tie wrap or equivalent around the pulled circuil breaker.)
• The following placard must be displayed in the cockpit, in clear view 01 the pilot, on the lower right hand portion of the center instrument panel:
I· USE OF FLAPS IS PROHIBITED
NOTE
Use 0° Flap Takeoff and . Landing performance and procedures from Section 5.
23 September 2003 For Training Purposes Only 208PHTRm
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For Training Purposes Only
'KINDS OF OPERATION LIMITS
This airplane is equipped for day VFR, and may be equipped for night VFR and/or IFR operations and for f1ight-into-known icing conditions. The operating limitations placard reflects the limits applicable at the time of Airworthiness Certificate issuance.
The following equipment list identifies the systems and equipment upon which type certification for each kind of operation was ' predicated, These systems and equipment items must be installed and operable for the particular kind of operation indicated. Reference should also be made to the Equipment List furnished with the airplane for additional equipment information. The pilot is responsible for determining the airworthiness of his airplane for each flight and for assuring compliance with curr~nt operating FAR's.
REQUIRED EQUIPMENT
DAVVFR:
Airspeed Indicator (1) Altimeter (1)* Auxiliary Boost Pump System BA TIERY HOT And SA TIERY
OVERHEAT·Annunciators (NiCad Batteries Only)
Elevator Trim System (Manual) Engine Ignition System (Flap Motor Disabled) Flap Position Indicator FUEL PRESS LOW Annunciator Fuel Quantity Indicators (2) Fuel Selectors Off Warning
System Generator Inertial Separator System In Indicator Magnetic Compass
Ng% RPM Indicator . OIL PRESS LOW Annunciator Oil Pressure Gage Oil Temperature Gage Outside Air Temperature Gage Overspeed (Airspeed) Warning
System Overspeed Governor Pilots Operating HandbookiAFM Pitot-Static System (1)
. Propeller APM Indicator
Seat Belts (Each Occupant) Shoulder Harnesses (Front Seats) Slip-Skid Indicator (1) Stall Warning System Torque Indicator ' Trim Position Indicators (3) VolVAmmeter
. When a servoed altimeter is installed, a functioning pneumatic altimeter is also required.
23 September 2003 For Training Purposes Only 208PHTA02
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For Training Purposes Only
PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
1. Airspeed •• 95 KIAS with 0° flaps. 2. Propeller-- FEATHER. 3. Fuel Condition Lever -- CUTOFF. 4. Fuel Shutoff -- OFF (pull out). 5. Fuel Tank Selectors -- OFF (warning horn will sound), 6. Battery -" OFF.
23 September 2003 for Tr~ining Pqrposes Only 208PHTR02
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For Training Purposes Only
SECTION 3 - EMERGENCY PROCEDURES
EMERGENCY LANDING WITHOUT .ENGINE POWER
1, Seats, Seat Belts, Shoulder Harnesses -- SECURE, 2. Airspeed -- 100 KIAS (flaps UP) 3. Power Lever --IDLE. 4. Propeller Control Lever -- FEATHER. 5. Fuel condition Lever -- CUTOFF. 6. Fuel Boost Switch -- OFF. 7. Ignition Switch -- NORM, 8. Standby Power Switch (if installed) -~ OFF. 9. . Non-essential Equipment (if Installed) -- OFF.
10. Fuel Shutoff -- OFF (pull out). 11. Fuel Tank Selectors -- OFF (warning horn will sound). 12. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 13. Ba~tery Switch -- OFF when landing is assured. 14. Touchdown -- SLIGHTLY TAIL LOW. 15. Brakes -- APPLY HEAVILY.
PRECAUTIONARY LANDING WITH ENGINE POWER
1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2 . . Wing Flaps -- 0°. 3. Airspeed -- 95 KIAS. 4. Selected Field -- FL YOVER, noting terrain and obstructions. 5. All Electrical Switches (except Battery and Generator) -- OFF. 6. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 7. Generator Switch (if installed) -- OFF. 8. Battery Switch -- OFF. 9. Touchdown -- SLIGHTLY TAIL LOW.
10. Fuel Condition Lever -- CUTOFF. 11. Brakes -- APPLYHEAVIL Y.
23 September 2003 For Training Purposes Only 208PHTR02
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For Training Purpos~s Only
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PILOT'S OPERATING HANDBOOK TEMPORARY'REVISION
1. Radio·· TRANSMIT MAYDAY on 121.5 MHz,giving location and intentions and SQUAWK 7700 if transponder is installed.
2. Heavy Objects in Cabin •• SECURE if passenger is available to assist.
3. Seats, Seat Belts, Shoulder Harnesses •• SECURE. 4. , Wing Flaps •• 0°. , 5. Power·· ESTABLISH 300 FT/MIN DESCENT AT 100 KIAS. 6. Approach·· High Winds .. INTO THE WIND.
light Winds, Heavy Swells •• PARALLEL TO SWELLS. 7. FACE •• CUSHION at touchdown with folded coat or similar object. 8. Touchdown •• NO FLARE, maintain descent attitude. 9. Airplane·· EVACUATE.
10. Life Vests and Raft·· INFLATE when outside cabin.
23 September 2003 ForTraining Purposes Only 208PHTRm
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For Training Purposes Only
PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
ENGINE FIRE IN FLIGHT (Red ENGINE FIRE Annunciator On Or Off)
1. Power Lever -- IDLE. 2. Propeller Control Lever -- FEATHER. 3. Fuel Condition Lever - CUTOFF. 4. Fuel Shutoff -- OFF. 5. Cabin Heat Firewall Shutoff Coritrol-- PULL OFF. 6. Forward Side Vents -- CLOSE. 7. Overhead Vents -- OPEN. 8. Ventilation Fans (if installed) -- ON. 9. , Wing Flaps -- 0°.
10. Airspeed _. 100 KIAS. 11. Forced Landing -- EXECUTE (as described in Emergency Landing
Without Engine Power)
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For Training Purposes Only
LANDING GEAR MALFUNCTION PROCEDURES
LANDING WITH FLAT MAIN TIRE
1. Airplane -- FLY as desired to lighten fuel load. ~. Fuel Selectors _. POSITION ONE SIDE OFF TO LIGHTEN LOAD ON
SIDE OF FLAT TIRE (maximum fuel unbalance of 200 pounds). 3. Approach -- NORMAL W flaps). 4. Touchdown .- INFLATED TIRE FIRST. Hold airplane off flat tire as
long as possible with aileron control. 5. Directional Control·· MAINTAIN using brake on wheel with inflated
tire as required.
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For Training Purposes Only
EMERGENCY DESCENT PROCEDURES
SMOOTH AIR
1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2. Power Lever -- IDLE. 3. Propeller Control Lever -- MAX (full forward). 4. Wing Flaps -- 0°. 5. Airspeed -- 175 KIAS.
23 September 2003 For Training Purposes Only 208PHTRO~
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For Training Purposes Only
INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT
UPPER HALF OF CARGO DOOR OR UPPER HALF OF PASSENGER AIRSTAIR DOOR OPEN (Red DOOR WARNING Annunciator On) .
1. Airspeed -- MAINTAIN LESS THAN 100 KIAS. 2. If available or practical. have a second crew member go aft to close
and latch door. 3. If landing is required with door open:
a. Approach and Landing NORMAl.
LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN
1. Airspeed -- MAINTAIN 100 KIAS. 2. Flight Controls -- MANEUVER for return for landing. 3. Wing Flaps -- 0°. 4. Approach -- NORMAL. 5. Landing -- SLIGHTLY TAIL LOW; avoid nose high flare.
23 September 2003 For Training Purposes Only 208PHTR02
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For Training Purposes Only
LANDING WITHOUT ELEVATOR CONTROL
Using power lever and elevator trim control, trim for approximately 500 fpm descent with 0° flaps at 100 KIAS. Then control the glide angle by adjusting power. If required,make small trim changes to maintain approximately 85KIAS as power is adjusted during the approach.
The landing ' flare can be accomplished by a gentle power reduction accompanied by nose up trim.' At forward C.G. loadings, it may be necessary to make a small power increase in the final flare stage to bring the nose up and prevent touchdown ' on the nose first. After touchdown, mov.e the power lever to idle:
23 September 2003 For Trai"ingPurp(Jses Oply 208PHTR02
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For Training Purposes Only
SECTION 3 - EMERGENCY PROCEDURES
INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT
If any of the airplane doors should inadvertently. open in flight, the airplane should be slowed to 100 KIAS tei reduce buffeting of the doors. On the Passenger Version, closing the upper cargo door or upper half of the passenger airstair door can be accomplished after airspeed has been reduced by pulling the door forcefully closed and latching the door. If the door cannot be closed · in flight, a landing should be made as soon as practical in accordance with the checklist procedures. On Cargo · Versions. an open cargo door cannot be closed in flight since the inside of the upper door has no handle. .
If any cargo pod doors inadvertently open in flight. the airplane should be slowed to 100 KIAS or less and landed as soon as practical. During the landing. avoid a nose-high flare to prevent dragging an . open rear cargo pod door on the runway. .
23 Septertlber2003 For Training Purposes Only 208PHTRO~
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PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
1. Pilot's Operating Handbook and Other Required Documents -- AVAILABLE IN THE AIRPLANE.
2. Control Locks --REMOVE (DISENGAGE rudder lock, if installed). 3. Parking Brake -- SET. 4. All Switches -- OFF. 5. All Circuit Breakers -- IN. 6. Static Pressure Alternate Source Valve -- OFF (full in) .
. 7. Inertial Separator T-Handle -- NORMAL. 8. Standby Flap Motor Switch (Overhead) -- GUARDED NORM. 9. Oxygen Supply Pressure -- CHECK.
10. Oxygen Masks -- CHECK AVAILABLE. 11. Fuel Selector Valves -- CHECK ON and FEEL AGAINST STOPS. 12. Radar -- OFF. 13. Air Conditioner (if installed) -- OFF. 14. inverier Switch (if instaiied) -- OFF. 15. Bleed Air Heat Switch -- OFF. 16. Emergency ' Power Uwer -- NORMAL, and if applicable, copper
witness wire present and intact. 17. Trim Controls -- SET .
. 18. Fuel Shutoff -- ON. 19. Cabin Heat Firewall Shutoff Control -- CHECK IN. 20. Battery Switch -- ON. 21 . Avionics Power Switch No. 2 -- ON. Check audibly that avionics
cooling fan is operating. 22. Avionics Power Switch No. 2 .- OFF. 23. Fuel Quantity Indicators -- CHECK QUANTITY. 24. Wing Flaps -- UP. . 25. Pilot/Static and Stall Heal Switches -- ON for 30 seconds, then OFF.
(Ensure pitot/static tube covers are removed.) . 26. . Battery Switch -- OFF.
: CD LEFT SIDE
1. Fuel Reservoir Drain (bottom . of fuselage or left side of . cargo pod) - DRAIN (using fuel sampler) to check for water, sediment, and proper fuel before each flight and after each refueling. If water is observed, take further samples until. clear. Take repeated samples from all fuel drain points (see Section 7 Fuel System Schematic for all nine drain locations) until all contamination has been removed.
23 September 2003 For Training Purpo~es Only 208PHTR02
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Cessna 208 MODEL SERIES
PILOT'S OPERATINGHANDBOOK TEMPORARY REVISION
SECTION 4 • NORMAL PROCEDURES
BEFORE TAKEOFF 1. Parking Brake·· SET. 2. Seats, Seat Belts, Shoulder Harnesses -- CHECK SECURE.
A WARNING
Failure to properly utilize seat belts and shoulder harnesses could result in SERIOUS or FATAL injury in the event of an accident.
3. Flight Controls _. FREE and CORRECT. 4. Flight Instruments -- CHECK and SET. 5. Fuel Boost Switch .- RECHECK NORM. 6. Fuel Tank Selectors -- RECHECK BOTH ON. 7. Fuel Quantity -- RECHECK. 8. Fuel Shutoff -- RECHECK FULLY ON. 9. Elevator, Aileron, and Rudder Trim Controls -- SET for takeoff.
10. Power Lever -- 400 FT -LBS. a. Suction Gage _. CHECK. b. Volt/Ammeter -- CHECK and return selector to BATT position. c. Inertial Separator -- CHECK. Turn control counterclockwise, pull
to BYPASS position and check torque drop; move control back to NORMAL position and check that original torque is regained.
d. Engine Instruments .- CHECK (See Section 2, Limitations for minimum oil temperature required for flight).
11 . Overspeed Governor -- CHECK (stabilized at 1750 ±60 RPM) (See Systems Checks) .
12. Power Lever --IDLE. 13. Quadrant Friction Lock -- ADJUST. 14. Standby Power (if installed) _. CHECK (See Systems Checks). 15. Autopilot .- PREFLIGHT TEST (See Systems Checks). 16. Known Icing System -~ PREFLIGHT COMPLETE (See Systems
Checks) prior to any flight in icing conditions. 17. Pitot/Static Heat -- On when OAT is below 4°C (40°F). 18. Ice Protection -- AS REQUIRED. 19~ Avionics and…
THIS TEMPORARY REVISION REVISES FUEL QUANTITY VERSUS DEPTH INFORMATION WHEN USING THE DIPSTICK REQUIRED BY CAB04-1 ON BOTH LEFT AND RIGHT WING L.EADING EDGE IN THE PILOT'S OPERATING HANDBOOK.
( INSERT THE , PROVIDED LIST OF TEMPORARY REVISIONS, AND
( ,r-" THE TEMPORARY REVISION INTO THE PILOT'S OPERATING ( \0~')' HANDBOOK 'IN ACCORDANCE WITH ' THE FILING
,INSTRUCTIONS IN EACH REVISION.
For Training Purposes Only
3 February 2004 208PHTR .
LIST OF TEMPORARY REVISIONS MODEL ~eERIES208 (
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Following is the List of Temporary Revisions that may be inserted into this " ( Pilot's Operating Handbook. . i (
Insert this page opposite the first page of the Log of Effective Pages in the front of the Pilot's Operating Handbook.
TEMPORARY MANUAL ISSUE
REVISION SECTION/ DATE
208PHTR02 208PHTR02
208PHTR02 3/EMERGENCY 23 September
TEMPORARY REVISION 208PHTR03 APPROVED BY
'AA APPROVED UNDER FAR 21SUBPART J rl\lj Ceqn. Aircraft Co
0010g81100 Option' Authonzalion 00A·230428-Ce
SERVICE BULLETIN
208PHTR
Section 4, NORMAL PROCEDURES
Insert this temporary revision into the Pilot's Operating Handbook.
( In Section 4, NORMAL PROCEDURES, insert the temporary revIsion
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208PHTR03
{ \ \
For Training Purposes Only
PILOT'SOPERATING HANDBOOK TEMPORARY REVISION
Cessna 208 MODEL SERIES
SECTION 4 - NORMAL PROCEDURES
A WARNING
It is essential in cold weather to remove even small accumulations of frost, ice, or snow from the wing and control surfaces. Also, make sure the control surfaces contain no internal accumulations of ice or debris. Prior to any flight in icing ' conditions, check that pitot/static source and stall warning heaters are warm to touch after turning pitot/static and stall heat switches on for 30 seconds, then off. Make sure the pitot covers are removed.
1. Wing Strut Deice Boots -- CHECK for tears, abrasion and cleanliness. 2. Wing Tie-Down -- DISCONNECT. 3. Wing Deice Boots -- CHECK for tears, abrasions and cleanliness. 4. Stall Warning Vane -- CHECK freedom of movement, audible warning
and warmth. (For aircraft equipped with a stall warning ground disconnect switch, check audible warning with elevator off forward stop).
5. PitoVStatic Tube -- CHECK security, openings for stoppage and warmth. ,
6. Landing and Taxi Lights ~- CHECK condition and cleanliness. 7. Fuel Quantity -- USE DIPSTICK required by CAB04-1 to check fuel
level. See Figure TC-l for fuel quantity versus depth.
A CAUTION
8. Fuel Filler Cap -- SECURE.
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9. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and airplane parked with one wing low on a sloping ramp) -- DRAIN (using fuel sampler) to check for water, sediment, and proper fuel before each flight and after each refueling. If water is observed, take further ( samples until clear. Take repeated samples from all fuel drain points ( .(, until all contamination has been removed. \.
10; NaVigation and Strobe Lights -- CHECK for condition and cleanliness.
3 February 2004 208PHTR03 For Training Purposes Only
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Universal XL Fuel Gage Fuel Quantity Gage Scale Gal lbs
0.50 87.4 585 0.75 91 .1 610 1.00 94.7 634 1.25 98.2 658 1.50 101.8 682 1.75 105.2 705 2.00 108.6 727 2.25 111.9 750 2.50 115.1 771 2.75 118.3 793 3.00 121.5 814 3.25 124.5 834 3.50 127.5 855 3.75 130.5 874 4.00 133.4 894 4.25 136.2 912 4.50 138.9 931 4.75 141.6 949 5.00 144.3 966 5.25 146.8 984 5.50 149.3 1000 5.75 151 .8 1017 6.00 154.1 1Q33 6.25 156.5 1048 6.50 158.7 1053 6~75 160.9 1078 7.00 163.0 1092 7.25 165.0 1106
Figure TC-1. Measure
Generic Fuel Gage - Inches Fuel Quantity ncnes Gal . Lbs
0.50 88.4 592 0.75 92.6 . 621 1.00 96.7 648 1.25 100.8 675 1.50 104.7 702 1.75 108.6 727 2.00 112.4 753 2.25 116.1 778 2.50 119.7 802 2.75 123.2 826 3.00 126.7 849 3.25 130.1 871 3.50 133.4 894 3.75 136.G 915 4.00 139.7 936 4.25 142.8 956 4.50 145.7 976 4.75 148.6 996 5.00 151.4 1015 5.25 154.1 . 1033 5.50 156 .. 8 1050 5.75 159.3 1068 6.00 161.8 1084 6.33 · 165.0 1105
d Fuel Depth vs Fuel Quantity
For Training P\Jrposes On'y 3 February 2004
208PHTR03
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VRIGHT WING Leading Edge
A WARNING It is essential in cold weather ,to remove even small accumulations of frost, ice, or snow from the wing and control surfaces. Also, make sure the control surfaces contain no internal accumulations of ice or debris.
1. Navigation and Strobe Lights -- CHECK condition and cleanliness. 2. Fuel Quantity -- USE DIPSTICK required by QAB04-1 to check fuel
level. See Figure TC-1 for fuel quantity verSus depth.
A CAUT10N
3. F'uel Filler Cap-- SECURE.
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5. PitoVStatic Tube -- CHECK security, . openings 'for stoppage , and warmth.
6. Landing and Taxi Lights -~ CHECK conditibn .~nd cleanliness. 7. Wing Deice Boots-- CHECK for tears, abrasl9~ and cleanliness. 8. Radome -- CHECK condition and security. :' \ . 9. Wing Tie-Down -- DISCONNECT. ' '~
10 .. Wing Strut Deice Boots -- CHECK for tears, abrasion,and cleanliness. 11 . Inboard Fuel Tank Sump and External Sump Quick-Drain Valves -
DRAIN (using fuel sampler) to check for water, sediment, arid proper fuel before each flight and after each refueling. If water is observed. take further samples until clear. Take repeated samples from aliluel drain pOints until all contamination has been removed.
12. Main Landing Gear -- CHECK proper tire inflation and gear condition.
3 February 2004 208PHTR03 For Training Purposes Only
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THIS TEMPORARY REVISION REPLACES TEMPORARY . REVISION 208PHTR01 DATED 8 SEPTEMBER 2003 AND REVISES
FLAP USAGE INFORMATION IN ·SECTIONS 2, 3, 4 AND 5 OF THE PILOT'S OPERATING HANDBOOK.
INSERT THE PROVIDED LIST OF TEMPORARY REVISIONS, AND THE TEMPORARY REVISION INTO THE PILOT'S OPERATING HANDBOOK· IN ACCORDANCE WITH THE FILING INSTRUCTIONS IN EACH REVISION.
For Training Purposes Only
For Training Purposes Only
23 September 2003 208PHTR
All Cessna Model 208 Series
The following List of . Temporary Revisions must be inserted into this Pilot's Operating Handbook. (
Insert this page opposite the first page of the Log of Effective Pages in the frontof the Pilot's Operating Handbook.
TEMPORARY MANUAL ISSUE REVISION . . SECTIONI DATE
NUMBER TOPIC
208PHTR02 .. 208PHTR02
20BPHTR02 3/EMERGENCY 23 September
TEMPORARY REVISION 208PHTR02 APPROVED BY
FAA APPROVED UNDER FAR 21 SUBPART J The C_ 1.ircr8ft co.
Del"llation Option Authoriulion DOA-23042B-CE
~. ~3 SE..PTEM&R. :l003
208PHTR
Section 2, LIMITATIONS, . EMERGENCY PROCEDURES, NORMAL PROCEDURES, and PERFORMANCE.
Section Section Section
3, 4, 5,
Insert this temporary revision into the Pilot's Operating Handbook.
In Section 2, LIMITATIONS, insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 2 pages containing the information that is shown in this -temporary revision. .
_ In Section 3, EMERGENCY PROCEDURES; insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 3 pages containing the information that is shown in this temporary revision.
In Section 4, NORMAL PROCEDURES, insert the temporary revision pages adjacent to the current Pilot's Operating Handbook Section 4 pages containing the information that is shown in this temporary revision.
In Section 5, PERFORMANCE, insert the. temporary revision pages adjacent to the current Pilot's Operating Handbook Section 5 pages containing the information that is shown in this temporary revision.
Discard any pages of this temporary revision that are not applicable to your model/serial airplane.
For Training Purposes Only 23 September 2003
20BPHTR02
For Training Purposes Only
PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
The flap motor and STBY flap motor circuit breakers must be pulled and collared. (place a tie wrap or equivalent around the pulled circuil breaker.)
• The following placard must be displayed in the cockpit, in clear view 01 the pilot, on the lower right hand portion of the center instrument panel:
I· USE OF FLAPS IS PROHIBITED
NOTE
Use 0° Flap Takeoff and . Landing performance and procedures from Section 5.
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'KINDS OF OPERATION LIMITS
This airplane is equipped for day VFR, and may be equipped for night VFR and/or IFR operations and for f1ight-into-known icing conditions. The operating limitations placard reflects the limits applicable at the time of Airworthiness Certificate issuance.
The following equipment list identifies the systems and equipment upon which type certification for each kind of operation was ' predicated, These systems and equipment items must be installed and operable for the particular kind of operation indicated. Reference should also be made to the Equipment List furnished with the airplane for additional equipment information. The pilot is responsible for determining the airworthiness of his airplane for each flight and for assuring compliance with curr~nt operating FAR's.
REQUIRED EQUIPMENT
DAVVFR:
Airspeed Indicator (1) Altimeter (1)* Auxiliary Boost Pump System BA TIERY HOT And SA TIERY
OVERHEAT·Annunciators (NiCad Batteries Only)
Elevator Trim System (Manual) Engine Ignition System (Flap Motor Disabled) Flap Position Indicator FUEL PRESS LOW Annunciator Fuel Quantity Indicators (2) Fuel Selectors Off Warning
System Generator Inertial Separator System In Indicator Magnetic Compass
Ng% RPM Indicator . OIL PRESS LOW Annunciator Oil Pressure Gage Oil Temperature Gage Outside Air Temperature Gage Overspeed (Airspeed) Warning
System Overspeed Governor Pilots Operating HandbookiAFM Pitot-Static System (1)
. Propeller APM Indicator
Seat Belts (Each Occupant) Shoulder Harnesses (Front Seats) Slip-Skid Indicator (1) Stall Warning System Torque Indicator ' Trim Position Indicators (3) VolVAmmeter
. When a servoed altimeter is installed, a functioning pneumatic altimeter is also required.
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PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
1. Airspeed •• 95 KIAS with 0° flaps. 2. Propeller-- FEATHER. 3. Fuel Condition Lever -- CUTOFF. 4. Fuel Shutoff -- OFF (pull out). 5. Fuel Tank Selectors -- OFF (warning horn will sound), 6. Battery -" OFF.
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SECTION 3 - EMERGENCY PROCEDURES
EMERGENCY LANDING WITHOUT .ENGINE POWER
1, Seats, Seat Belts, Shoulder Harnesses -- SECURE, 2. Airspeed -- 100 KIAS (flaps UP) 3. Power Lever --IDLE. 4. Propeller Control Lever -- FEATHER. 5. Fuel condition Lever -- CUTOFF. 6. Fuel Boost Switch -- OFF. 7. Ignition Switch -- NORM, 8. Standby Power Switch (if installed) -~ OFF. 9. . Non-essential Equipment (if Installed) -- OFF.
10. Fuel Shutoff -- OFF (pull out). 11. Fuel Tank Selectors -- OFF (warning horn will sound). 12. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 13. Ba~tery Switch -- OFF when landing is assured. 14. Touchdown -- SLIGHTLY TAIL LOW. 15. Brakes -- APPLY HEAVILY.
PRECAUTIONARY LANDING WITH ENGINE POWER
1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2 . . Wing Flaps -- 0°. 3. Airspeed -- 95 KIAS. 4. Selected Field -- FL YOVER, noting terrain and obstructions. 5. All Electrical Switches (except Battery and Generator) -- OFF. 6. Crew Doors -- UNLATCH PRIOR TO TOUCHDOWN. 7. Generator Switch (if installed) -- OFF. 8. Battery Switch -- OFF. 9. Touchdown -- SLIGHTLY TAIL LOW.
10. Fuel Condition Lever -- CUTOFF. 11. Brakes -- APPLYHEAVIL Y.
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1
PILOT'S OPERATING HANDBOOK TEMPORARY'REVISION
1. Radio·· TRANSMIT MAYDAY on 121.5 MHz,giving location and intentions and SQUAWK 7700 if transponder is installed.
2. Heavy Objects in Cabin •• SECURE if passenger is available to assist.
3. Seats, Seat Belts, Shoulder Harnesses •• SECURE. 4. , Wing Flaps •• 0°. , 5. Power·· ESTABLISH 300 FT/MIN DESCENT AT 100 KIAS. 6. Approach·· High Winds .. INTO THE WIND.
light Winds, Heavy Swells •• PARALLEL TO SWELLS. 7. FACE •• CUSHION at touchdown with folded coat or similar object. 8. Touchdown •• NO FLARE, maintain descent attitude. 9. Airplane·· EVACUATE.
10. Life Vests and Raft·· INFLATE when outside cabin.
23 September 2003 ForTraining Purposes Only 208PHTRm
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For Training Purposes Only
PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
ENGINE FIRE IN FLIGHT (Red ENGINE FIRE Annunciator On Or Off)
1. Power Lever -- IDLE. 2. Propeller Control Lever -- FEATHER. 3. Fuel Condition Lever - CUTOFF. 4. Fuel Shutoff -- OFF. 5. Cabin Heat Firewall Shutoff Coritrol-- PULL OFF. 6. Forward Side Vents -- CLOSE. 7. Overhead Vents -- OPEN. 8. Ventilation Fans (if installed) -- ON. 9. , Wing Flaps -- 0°.
10. Airspeed _. 100 KIAS. 11. Forced Landing -- EXECUTE (as described in Emergency Landing
Without Engine Power)
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LANDING GEAR MALFUNCTION PROCEDURES
LANDING WITH FLAT MAIN TIRE
1. Airplane -- FLY as desired to lighten fuel load. ~. Fuel Selectors _. POSITION ONE SIDE OFF TO LIGHTEN LOAD ON
SIDE OF FLAT TIRE (maximum fuel unbalance of 200 pounds). 3. Approach -- NORMAL W flaps). 4. Touchdown .- INFLATED TIRE FIRST. Hold airplane off flat tire as
long as possible with aileron control. 5. Directional Control·· MAINTAIN using brake on wheel with inflated
tire as required.
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EMERGENCY DESCENT PROCEDURES
SMOOTH AIR
1. Seats, Seat Belts, Shoulder Harnesses -- SECURE. 2. Power Lever -- IDLE. 3. Propeller Control Lever -- MAX (full forward). 4. Wing Flaps -- 0°. 5. Airspeed -- 175 KIAS.
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INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT
UPPER HALF OF CARGO DOOR OR UPPER HALF OF PASSENGER AIRSTAIR DOOR OPEN (Red DOOR WARNING Annunciator On) .
1. Airspeed -- MAINTAIN LESS THAN 100 KIAS. 2. If available or practical. have a second crew member go aft to close
and latch door. 3. If landing is required with door open:
a. Approach and Landing NORMAl.
LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN
1. Airspeed -- MAINTAIN 100 KIAS. 2. Flight Controls -- MANEUVER for return for landing. 3. Wing Flaps -- 0°. 4. Approach -- NORMAL. 5. Landing -- SLIGHTLY TAIL LOW; avoid nose high flare.
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LANDING WITHOUT ELEVATOR CONTROL
Using power lever and elevator trim control, trim for approximately 500 fpm descent with 0° flaps at 100 KIAS. Then control the glide angle by adjusting power. If required,make small trim changes to maintain approximately 85KIAS as power is adjusted during the approach.
The landing ' flare can be accomplished by a gentle power reduction accompanied by nose up trim.' At forward C.G. loadings, it may be necessary to make a small power increase in the final flare stage to bring the nose up and prevent touchdown ' on the nose first. After touchdown, mov.e the power lever to idle:
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SECTION 3 - EMERGENCY PROCEDURES
INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT
If any of the airplane doors should inadvertently. open in flight, the airplane should be slowed to 100 KIAS tei reduce buffeting of the doors. On the Passenger Version, closing the upper cargo door or upper half of the passenger airstair door can be accomplished after airspeed has been reduced by pulling the door forcefully closed and latching the door. If the door cannot be closed · in flight, a landing should be made as soon as practical in accordance with the checklist procedures. On Cargo · Versions. an open cargo door cannot be closed in flight since the inside of the upper door has no handle. .
If any cargo pod doors inadvertently open in flight. the airplane should be slowed to 100 KIAS or less and landed as soon as practical. During the landing. avoid a nose-high flare to prevent dragging an . open rear cargo pod door on the runway. .
23 Septertlber2003 For Training Purposes Only 208PHTRO~
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PILOT'S OPERATING HANDBOOK TEMPORARY REVISION
1. Pilot's Operating Handbook and Other Required Documents -- AVAILABLE IN THE AIRPLANE.
2. Control Locks --REMOVE (DISENGAGE rudder lock, if installed). 3. Parking Brake -- SET. 4. All Switches -- OFF. 5. All Circuit Breakers -- IN. 6. Static Pressure Alternate Source Valve -- OFF (full in) .
. 7. Inertial Separator T-Handle -- NORMAL. 8. Standby Flap Motor Switch (Overhead) -- GUARDED NORM. 9. Oxygen Supply Pressure -- CHECK.
10. Oxygen Masks -- CHECK AVAILABLE. 11. Fuel Selector Valves -- CHECK ON and FEEL AGAINST STOPS. 12. Radar -- OFF. 13. Air Conditioner (if installed) -- OFF. 14. inverier Switch (if instaiied) -- OFF. 15. Bleed Air Heat Switch -- OFF. 16. Emergency ' Power Uwer -- NORMAL, and if applicable, copper
witness wire present and intact. 17. Trim Controls -- SET .
. 18. Fuel Shutoff -- ON. 19. Cabin Heat Firewall Shutoff Control -- CHECK IN. 20. Battery Switch -- ON. 21 . Avionics Power Switch No. 2 -- ON. Check audibly that avionics
cooling fan is operating. 22. Avionics Power Switch No. 2 .- OFF. 23. Fuel Quantity Indicators -- CHECK QUANTITY. 24. Wing Flaps -- UP. . 25. Pilot/Static and Stall Heal Switches -- ON for 30 seconds, then OFF.
(Ensure pitot/static tube covers are removed.) . 26. . Battery Switch -- OFF.
: CD LEFT SIDE
1. Fuel Reservoir Drain (bottom . of fuselage or left side of . cargo pod) - DRAIN (using fuel sampler) to check for water, sediment, and proper fuel before each flight and after each refueling. If water is observed, take further samples until. clear. Take repeated samples from all fuel drain points (see Section 7 Fuel System Schematic for all nine drain locations) until all contamination has been removed.
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Cessna 208 MODEL SERIES
PILOT'S OPERATINGHANDBOOK TEMPORARY REVISION
SECTION 4 • NORMAL PROCEDURES
BEFORE TAKEOFF 1. Parking Brake·· SET. 2. Seats, Seat Belts, Shoulder Harnesses -- CHECK SECURE.
A WARNING
Failure to properly utilize seat belts and shoulder harnesses could result in SERIOUS or FATAL injury in the event of an accident.
3. Flight Controls _. FREE and CORRECT. 4. Flight Instruments -- CHECK and SET. 5. Fuel Boost Switch .- RECHECK NORM. 6. Fuel Tank Selectors -- RECHECK BOTH ON. 7. Fuel Quantity -- RECHECK. 8. Fuel Shutoff -- RECHECK FULLY ON. 9. Elevator, Aileron, and Rudder Trim Controls -- SET for takeoff.
10. Power Lever -- 400 FT -LBS. a. Suction Gage _. CHECK. b. Volt/Ammeter -- CHECK and return selector to BATT position. c. Inertial Separator -- CHECK. Turn control counterclockwise, pull
to BYPASS position and check torque drop; move control back to NORMAL position and check that original torque is regained.
d. Engine Instruments .- CHECK (See Section 2, Limitations for minimum oil temperature required for flight).
11 . Overspeed Governor -- CHECK (stabilized at 1750 ±60 RPM) (See Systems Checks) .
12. Power Lever --IDLE. 13. Quadrant Friction Lock -- ADJUST. 14. Standby Power (if installed) _. CHECK (See Systems Checks). 15. Autopilot .- PREFLIGHT TEST (See Systems Checks). 16. Known Icing System -~ PREFLIGHT COMPLETE (See Systems
Checks) prior to any flight in icing conditions. 17. Pitot/Static Heat -- On when OAT is below 4°C (40°F). 18. Ice Protection -- AS REQUIRED. 19~ Avionics and…