kamov ka 32 procedures - vih cd/vih/pilot/ka32_emergency.pdf · ka‐32 emergency procedures...

AMENDMENT: 1 AMENDMENT DATE: 29 APRIL, 2014

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KAMOV Ka‐32 EMERGENCY PROCEDURES

SUBJECT PAGEApplication 4Definitions 4Emergency Actions 5Emergency Procedures Checklist

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VIH HELICOPTERS LTD.

Copy No.: SN 000

Assigned to: Enhanced CD / Electronic Copy

VIH HELICOPTERS LTD. Ka‐32 EMERGENCY PROCEDURES


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1. RECORD OF AMENDMENTS Amendment No. Date Date Entered Amended by

Original (Reissue) 04 September, 2009 J. Neill #1 (Reissue) 04 March, 2014 S. Palmer #2 29 April, 2014 S. Palmer

VIH HELICOPTERS lTD. Ka-32 EMERGENCY PROCEDURES

2. LIST OF EFFECTIVE PAGES

This manual includes the pages listed below at the revision status indicated.

Page Revision Effective Date 1 2 29 April, 2014 2 2 29 April, 2014 3 2 29 April, 2014 4 1 04 March, 2014

FIRES

Page Revision Effective Date 9 1 04 March, 2014 10 1 04 March, 2014

ENGINES

Page Revision Effective Date 12 1 04 March, 2014 13 1 04 March, 2014 14 1 04 March, 2014 15 1 04 March, 2014 16 1 04 March, 2014

HYDRAULICS

Page Revision Effective Date 22 1 04 March, 2014 23 1 04 March, 2014 24 1 04 March, 2014 25 1 04 March, 2014

ELECTRICAL

Page Revision Effective Date 30 1 04 March, 2014 31 1 04 March, 2014 32 1 04 March, 2014

GEAR BOX

Page Revision Effective Date 36 37

Signature:

Page 5 6 7 8

Page 17 18 19 20 21

Page 26 27 28 29

3 34 35

LATEST CHANGED PAGES IN BOLD

Revision Effective Date 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014 2 29 April, 2014

Effective Date 04 March, 2014

Revision Effective Date 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014

Revision Effective Date 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014

Revision Effective Date 1 04 March, 2014 1 04 March, 2014 1 04 March, 2014

Effective Date 04 March, 2014

29 April, 2014 Date

AMENDMENT: 2 AMENDMENT DATE: 29 APRil, 2014

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AMENDMENT: 1 AMENDMENT DATE: 04 MARCH, 2014

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3. EMERGENCY PROCEDURES 3.1. APPLICATION

This section contains emergency procedures for the Kamov Ka32. The list of emergencies is not all inclusive and is meant to be used in conjunction Section 3 of the Ka32 Flight Manual. Normally Company procedures will be followed over those in the AFM. However, where differences exist between the SOPs, RFM, and CAR’s, the more stringent shall prevail.

Because of the single engine flight capability of the Ka32, it is rarely necessary to act hastily in the event of an emergency, exceptions being engine failures on departures, and some servo malfunctions. All other failures/malfunctions allow the pilots time to think and analyse the situation. The Ka32 is certified as a single pilot aircraft except for external load operations. All pilots should be able to handle emergencies that require initial actions before referring to the check list as they may be single pilot.

3.2. DEFINITIONS LAND IMMEDIATELY / DITCH The urgency of the landing is paramount.

The primary consideration is to assure the survival of the occupants.

LAND AS SOON AS POSSIBLE Land without delay at the nearest suitable area (i.e. open field) at which a safe approach and landing is reasonably assured.

LAND AS SOON AS PRACTICAL The duration of the flight and landing site are at the discretion of the pilot. Extended flight beyond the nearest approved landing area is not recommended.



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3.3. EMERGENCY ACTIONS

The following sequence shall be carried out in all emergencies: 1) Fly Control the aircraft

Power Adjust to maintain Rotor RPM, and/or single

engine limits.

External Cargo Released from Belly Hook (Electrical or manual)

Airspeed Single engine minimum (70 kts)

Altitude Minimum 500 ft AGL. Lower at pilot’s discretion

2) Identify Caution light, bad engine, handling problem, vibrations, etc.

3) Verify Confirm the failure with secondary indications (gauges, lights, flight instruments).

4) Rectify The emergency procedures are divided into two parts:

Initial Actions - which must be memorized, and

Subsequent Actions - which should be carried out using the Checklist.

Note: 1. The Master Warning light, if illuminated, should be reset as soon as possible

after identifying the malfunction. This will also cancel the Audio. (Normally by the NFP).

2. Radio calls / Squawk 7700 / Passenger advisories shall be made at the

appropriate time depending on the severity of the emergency. 3. During an emergency the flying pilot (FP) will normally continue flying while the

non flying pilot (NFP) identifies the malfunction. Verification and Rectification will be confirmed and agreed upon after consideration of input from both pilots. Checklist actions will be completed using the Challenge and Response procedure.

Continued on next page



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4. During any emergency that requires switching OFF a system, closing a fuel shutoff lever, throttle to idle or closing a fuel valve the (FP) will ask the (NFP) to identify that switch, throttle or valve before giving instructions on its activation.

5. RESETTING OF TRIPPED CIRCUIT BREAKERS

The Rotorcraft Flight Manual (RFM) and the Maintenance Manual (MM) procedures and limitations shall be the basis for Circuit Breaker (CB) resetting procedures. General: There is a latent danger in resetting a CB tripped by an unknown cause because the tripped condition is a signal that something may be wrong in the related circuit. Until it is determined what has caused a trip to occur, crewmembers have no way of knowing the consequences of resetting a tripped CB. CB Associated with Fuel Pump Circuit of Fuel Quantity Indicating System (FQIS) Special caution is appropriate where fuel pumps and/or FQIS are involved, because of the possibility that arcing might lead to the ignition of fuel of fuel vapors. The resetting of the fuel boost pump and/or the Fuel Quantity Indicator CBs in-flight is not recommended unless authorized by the aircraft manufacturer, and then only when authorized by the pilot-in-command. The resetting of fuel boost pump and/or Fuel Quantity Indicator CBs on the ground, without first identifying the source of the electrical fault is not recommended. On-the-Ground: A CB tripped by an unknown cause may only be reset on the ground after maintenance has determined the cause of the trip and has determined that the CB may be safely reset. A CB may be cycled (tripped, pulled or reset) where it is required to be performed within approved maintenance inspection criteria, or as part of an approved trouble-shooting procedure, unless doing so is specifically prohibited. If an air operator’s minimum equipment list contains procedures that allow a tripped CB to be reset, then the same cautions with reference to resetting tripped CBs identified elsewhere in this manual also applies. Resetting a CB tripped by an unknown cause should normally be a maintenance function conducted on the ground. In-flight: A tripped CB shall not be reset in flight unless doing so is consistent with explicit procedures specified in the approved rotorcraft flight manual, SOPs, and checklists used by the crew members or unless, in the judgment of the pilot-in-command, resetting the CB is necessary for the safe completion of the flight. Crewmembers should limit resetting of CBs to one in-flight reset where this action is required. No attempt should be made to reset a CB if it trips a second time.



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4. KA32 EMERGENCY PROCEDURES CHECKLIST

TABLE OF CONTENTS

1. RECORD OF AMENDMENTS................................................................................................................. 2

2. LIST OF EFFECTIVE PAGES.................................................................................................................... 3

3. EMERGENCY PROCEDURES ................................................................................................................. 4

3.1. APPLICATION ........................................................................................................................................... 4 3.2. DEFINITIONS ............................................................................................................................................ 4 3.3. EMERGENCY ACTIONS ............................................................................................................................... 5



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4. KA32 EMERGENCY PROCEDURES CHECKLIST ....................................................................................... 7

TABLE OF CONTENTS ................................................................................................................................ 7/8

FIRES ............................................................................................................................................. 9

ENGINE FIRE ON GROUND ................................................................................................................ 9 ENGINE FIRE IN FLIGHT .................................................................................................................. 10 SMOKE FUMES IN CABIN ................................................................................................................. 11

ENGINES ...................................................................................................................................... 12

ENGINE FAILURE IN HOVER OR FLIGHT WITH EXTERNAL LOAD ................................................... 12 ENGINE FAILURE IN FLIGHT ............................................................................................................ 13 DUAL ENGINE FAILURE (AUTOROTATION) ..................................................................................... 14 ENGINE VIBRATION .......................................................................................................................... 15 ENGINE OIL SYSTEM FAILURE ........................................................................................................ 16 CHIPS IN ENGINE OIL ...................................................................................................................... 17 ENGINE ELECTRONIC GOVERNOR .................................................................................................. 18 GAS GENERATOR CIRCUIT EEG FAILURE ..................................................................................... 19 FREE TURBINE CONTROL CIRCUIT FAILURE .................................................................................. 20 FREE TURBINE RPM GOVERNOR FAILURE ................................................................................... 21

HYDRAULICS ................................................................................................................................ 22

MAIN HYDRAULIC SYSTEM PRESSURE BELOW LIMITS ................................................................. 22 MAIN HYDRAULIC OIL TEMPERATURE ABOVE LIMITS ................................................................... 23 STANDBY HYDRAULIC SYSTEM PRESSURE BELOW LIMITS .......................................................... 24 STANDBY HYDRAULIC SYSTEM PRESSURE ABOVE LIMITS ........................................................... 25 AUXILIARY HYDRAULIC SYSTEM FAILURE ...................................................................................... 26 MAIN/STANDBY SYSTEM PRIMARY CONTROL VALVES JAMMING ................................................. 27 HYDRAULIC SYSTEM PRESSURIZATION FAILURE .......................................................................... 28 AUTO PILOT FAILURE ...................................................................................................................... 29

ELECTRICAL .................................................................................................................................. 30

AC GENERATOR FAILURE ............................................................................................................... 30 DUAL AC GENERATOR FAILURE ................................................................................................... 31 RECTIFIER FAILURE ......................................................................................................................... 32 DUAL RECTIFIER FAILURE ............................................................................................................. 33 MAIN TRANSFORMER FAILURE ....................................................................................................... 34 BATTERY HOT .................................................................................................................................. 35

GEARBOX ..................................................................................................................................... 36 MAIN GEARBOX OIL PRESSURE BELOW LIMITS ............................................................................ 36 MAIN GEARBOX OIL TEMPERATURE ABOVE LIMIT ........................................................................ 37 CHIPS IN MAIN GEARBOX OIL ......................................................................................................... 38



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FIRES ENGINE FIRE ON GROUND

INDICATIONS:

Master warning light and audio signal on, LH or RH engine fire light on, possible erratic engine indications, high ITT etc. Smoke or flames visible in mirror. Fumes.

IMMEDIATE ACTIONS: Reset Master warning light (this will also cancel audio) 1. Both fuel shutoff levers ........................................................................... Closed 2. Check engine fire lights .......................................................................... Identify 3. Both fuel valves ............................................................................................ Off 4. A.P.U. ........................................................................................................... Off 5. A.P.U. fuel valve ........................................................................................... Off 6. Check No.1 fire bottle light out ................................................................. Verify

If No.1 fire bottle has failed to operate automatically.

7. Extinguisher button affected engine ......................................................... Press 8. No.1 fire bottle light off ............................................................................. Verify If check fire light remains on 1. Fire bottle switch to No.2 position ............................................................ Press 2. Extinguisher button affected engine ......................................................... Press 3. Rotor brake .................................................................................................. On 4. Emergency de-energized switch .................................................................. Off 5. Evacuate aircraft 6. If fire persists, fight externally.



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ENGINE FIRE IN FLIGHT INDICATIONS:

Master warning light and audio signal on, LH or RH check fire light on, possible erratic engine indications, high ITT etc. Smoke or flames visible in mirror. Fumes.

IMMEDIATE ACTION: (When hovering land immediately if able) Reset Master warning light (this will also cancel audio) 1. Establish safe airspeed for O.E.I.. ................................................. Climb/Cruise 2. Check engine fire lights .......................................................................... Identify 3. Check No.1 fire bottle light ........................................................................... out 4. Confirm correct fuel shutoff lever ........................................................... Closed 5. Confirm correct engine throttle ....................................................... Idle position 6. Confirm correct fuel valve............................................................................. Off 7. Good engine throttle ...................................................................... Full Forward

If No.1 fire bottle has failed to operate automatically. (From item 3.)

8. Extinguisher button affected engine ........................................................ Press 9. No.1 fire bottle light out ............................................................................ Verify If check fire light remain on

10. Extinguisher bottle switch to No. 2 position ............................................. Select 11. Fire button affected engine....................................................................... Press 12. If fire persists and check fire light remains on land or ditch immediately. SUBSEQUENT ACTIONS: 1. Cabin\cockpit heat and engine anti ice ......................................................... Off 2. Firex warn system switch .............................................................. Cycle Off/On 3. Radio calls ....................................................................................... As required 4. Crew ...................................................................................................... Advised 5. Land as soon as possible CAUTION: If temperature is 5 deg or below with visible moisture engine anti ice

should remain on.



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SMOKE FUMES IN CABIN

INDICATIONS: Smoke, smell of burning, toxic fumes, etc., in cabin IMMEDIATE ACTIONS: 1. Airspeed .................................................................................................. 70 Kts 2. Commence emergency descent to landing if possible. 3. Cockpit windows and vents ...................................................................... Open 4. Oxygen bottle and mask ......................................................................... Ready SUBSEQUENT ACTIONS:

If time and altitude permit and source is suspected to be electrical attempt to identify and isolate the effected system. If identified, de-energize the instruments and units in the area of the fire.

1. Smoke and protection mask ............................................................ As required 2. Fight fire with extinguisher 3. Radio calls ....................................................................................... As required 4. Land as soon as possible



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ENGINES

ENGINE FAILURE IN HOVER OR FLIGHT WITH EXTERNAL LOAD

INDICATIONS:

Master warning light and audio signal on, change in engine sound., engine fail light on, ITT and N1 decrease, Oil press, low RPM light if rotor drops below 85% NR. Audio signal will change if NR below 85%, Loss of generators and Autopilot if NR below 83%, Control problems and increased roughness if NR continues to drop. Affected overspd light on.

IMMEDIATE ACTION: Reset Master warning light (this will also cancel audio) 1. External Load. ...................................................................................... Release 2. Collective. ....................................................................... Reduce to maintain Nr 3. Establish safe airspeed for O.E.I. .................................................. Climb/Cruise 4. Failed engine ................................................................. Identified by both crew 5. Good engine ................................................................................... Within limits 6. Good engine throttle ........................................................................ Full forward SUBSEQUENT ACTIONS: 1. Check Auto Pilot On ............................................................ Reset if Necessary 2. Confirm correct fuel shutoff lever ........................................................... Closed 3. Confirm correct engine throttle ....................................................... Idle position 4. Confirm correct fuel valve............................................................................. Off 5. Radio Calls ...................................................................................... As required 5. Land as soon as practical NOTE: Consider fuel remaining on good engine tank system. For lowest fuel

consumption, airspeed 97 Kts. CAUTION: It is forbidden to start the failed engine if fail light is illuminated after

engine over speed.



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ENGINE FAILURE IN FLIGHT

INDICATIONS:

Master warning light and audio signal on, change in engine sound., engine fail light on, ITT and N1 decrease, Oil press, low RPM light if rotor drops below 85% NR. Audio signal will change if NR below 85%, affected overspd light on.

IMMEDIATE ACTION: Reset Master warning light (this will also cancel audio) 1. Establish safe airspeed for O.E.I. .................................................. Climb/Cruise 2. Failed engine ................................................................. Identified by both crew 3. Good engine ................................................................................... Within limits 4. Good engine throttle ........................................................................ Full forward SUBSEQUENT ACTIONS: 1. Confirm correct fuel shutoff lever ........................................................... Closed 2. Confirm correct engine throttle ....................................................... Idle position 3. Confirm correct fuel valve............................................................................. Off 4. Radio Calls ...................................................................................... As required 5. Land as soon as practical NOTE: Consider fuel remaining on good engine tank system. For lowest fuel

consumption, airspeed 97 Kts. CAUTION: It is forbidden to start the failed engine if fail light is illuminated after

engine over speed.



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DUAL ENGINE FAILURE (AUTOROTATION)

INDICATIONS: Master warning light and audio signal on, engine fail lights on, low RPM light on, , engine sound stopped! ITT decreasing both engines, engine oil pressures lights on, battery bus light on. IMMEDIATE ACTIONS: Reset Master warning light (this will also cancel audio) 1. Collective ........................................................................................... Full Down 2. Rotor speed .......................................................................................... 68-92 % 3. Airspeed ......................................................................................... 55 to 70 Kts 4. Radio ..................................................................................................... Mayday 5. Crew ....................................................................................................... Briefed

If time permits before landing shut down engines as follows: 6. Fuel shut off levers ................................................................................. Closed 7. Fuel valves ................................................................................................... Off FULL STOP LANDING: Initiate flare at 160 – 100 ft. AGL depending on airspeed. 25 degree nose up and 2/3 full travel on collective pitch. Maintain flare up to complete deceleration and 10 ft. AGL. Apply forward cyclic to achieve landing attitude. Collective full up to cushion landing on main wheels. NOTE: 10 degree maximum pitch up for landing. 15 degree maximum pitch up for ditching. RUN ON LANDING: Initiate flare at 160 – 100 ft. AGL at approximately 3 ft. AGL. Reduce flare to 8-10 deg. and airspeed to 21 kts. for run on landing. Apply collective to cushion landing on main wheels. After landing move collective full down (slowly). Cyclic neutral and apply brakes.



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ENGINE VIBRATION INDICATIONS: Master warning light and audio signal on, LH or RH engine vibration lights on red, amber or both. IMMEDIATE ACTIONS: Reset Master warning light (this will also cancel audio) 1. Collective down to reduce power. 2. Engine parameters .............................................................................. Checked If red and amber engine vibration lights remain on. Shut down affected engine 3. Establish safe airspeed for O.E.I. ................................................. Climb/Cruise 4. Confirm correct fuel shut off lever .......................................................... Closed 5. Confirm correct engine throttle ....................................................... Idle position 6. Confirm correct fuel valve............................................................................. Off 7. Good engine throttle ........................................................................ Full forward 8. Radio calls ....................................................................................... As required 9. Land as soon as possible. If red engine vibration light extinguished, but amber engine vibration light remains on. Monitor engine parameters. Land as soon as practical. NOTE: When engine vibration lights are illuminated, engine operating parameters may be out of limits. If only the amber or the red engine vibration light illuminates the system should be tested by pressing the VIBR METER test button and the WARN CHECK button. If the red engine vibration light does not illuminate when the system is being tested the system could be faulty and the engine should be shut down if a vibration is suspected.



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ENGINE OIL SYSTEM FAILURE

INDICATIONS: Master warning light on, LH or RH engine oil pressure light on, engine oil pressure 2Kg./sq.cm or less. possible engine oil temperature is higher than other engine and climbing. IMMEDIATE ACTIONS: 1. Establish safe airspeed for O.E.I ................................................... Climb/Cruise 2. Master warning light ................................................................................. Reset SUBSEQUENT ACTIONS: 1. Confirm correct fuel shut off lever ............................................................ Close 2. Confirm correct engine throttle ....................................................... Idle position 3. Confirm correct fuel valve............................................................................. Off 4. Good engine throttle ...................................................................... Full Forward 5. Radio calls ...................................................................................... As Required 6. Land as soon as possible. NOTE: If only one out of three indications occurs and oil temperature does not

exceed 150 C do not shut down the affected engine. Monitor oil system parameters. Test all warning lights. Land as soon as practical.



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CHIPS IN ENGINE OIL

INDICATIONS: Master warning light on, LH or RH engine chip light on. Oil pressure below 2Kg./sq.cm. possible oil temperature above 150 C. IMMEDIATE ACTIONS: Establish safe airspeed for O.E.I............................................................. Climb/Cruise Master warning light ............................................................................................ Reset SUBSEQUENT ACTIONS: Check oil pressure and temperature. If oil pressure or temperature beyond limits shut down engine. 1. Confirm correct fuel shut off lever ............................................................ Close 2. Confirm correct engine throttle ....................................................... Idle position 3. Confirm correct fuel valve............................................................................. Off 4. Good engine throttle ...................................................................... Full Forward 5. Radio calls ....................................................................................... As required 6. Land as soon as possible. NOTE: If oil pressure and temperature normal and chip light on, consider retarding

affected engine to idle. Monitor pressure and temperature.



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ENGINE ELECTRONIC GOVERNOR E.E.G. FAILURE: EEG Automatic cutout INDICATIONS: Master warning light on, EEG LH or RH fail light on. IMMEDIATE ACTIONS: Master warning light ............................................................................................ Reset SUBSEQUENT ACTIONS: 1. Cycle affected EEG off/on. If EEG light remains on keep EEG switch on. 2. Radio calls. 3. Land as soon as practical CAUTION: Do not exceed take off power limits.



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GAS GENERATOR CIRCUIT EEG FAILURE INDICATIONS: LH or RH engine power limit light on. N1 affected engine decreases to 85% IMMEDIATE ACTIONS: Establish safe airspeed for O.E.I. … ........................................................ Climb/Cruise SUBSEQUENT ACTIONS: 1. Cycle affected EEG off/on. If N1 affected engine has not restored switch EEG

off. 2. Engine operating parameters have restored ......................................... Monitor 3. Radio Calls 4. Land as soon as practical. NOTE: This occurs when EEG is not able to recognize its own failure in gas generator control circuit. CAUTION: Do not exceed take off power limits.



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FREE TURBINE CONTROL CIRCUIT FAILURE INDICATIONS: Master warning light and audio signal on, LH or RH engine over speed light on, affected engine operating parameters within limits. IMMEDIATE ACTIONS: Nil SUBSEQUENT ACTIONS: 1. Cycle affected EEG switch off/on.

If engine over speed light is still on switch EEG off 2. Master warning light ................................................................................. Reset 3. Radio calls 4. Land as soon as practical CAUTION: Do not exceed takeoff power limits. No over speed protection on affected

engine.



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FREE TURBINE RPM GOVERNOR FAILURE INDICATIONS: Master warning light and audio signal on, spontaneous rise of the rotor RPM, high RPM light at 99.4 NR (flickers on). Gas generator RPM N1 affected engine maximum. EEG 2.5 min light affected engine may be on. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset 2. Control rotor RPM ......................................................................... Collective up 3. If 2.5 min power light affected engine on ........................................ Switch Off SUBSEQUENT ACTIONS: Check the synchronization system cut out as follows: Move collective smoothly downward, maintain rotor RPM within limits. 1. Indications that synchronization system has been cut out. The power of the normally operating engine decreases and power of affected engine does not change in response to collective pitch reduction, rotor RPM remains close to normal. In this case proceed as follows: Shift the throttle lever of the affected engine to position marked by red line. Move collective smoothly to control engine power and rotor RPM. 2. Indications that synchronization system has not been cut out: The power of both engines changes slightly in response to collective pitch reduction, rotor RPM rises. In this case proceed as follows: Move collective smoothly downward to increase the rotor RPM to (99%…103%).Do not exceed the 3 second time limit between 98% and 103%. When synchronization system is cut out the normally operating engine N1 and rotor RPM should decrease. Shift the throttle lever of the affected engine to position marked by red line. Move collective smoothly to control power and rotor RPM. Radio Calls. Land as soon as practical. NOTE: Difference between gas generator RPM of both engines is not limited.



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HYDRAULICS

MAIN HYDRAULIC SYSTEM PRESSURE BELOW LIMITS INDICATIONS: Master warning light on, main hydraulic light on, auxiliary pump on, hydraulic pressure in main system is lower than 50 Kg/sq.cm. Actuator indicator zero. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset 2. Auto Pilot ...................................................................................................... Off 3. Standby Hydraulic press .............................................. Check 64..90 kg/sq.cm. 4. Auxiliary Pump and System Pressure .................................... On and Checked 200-220 kg/sq.cm. 75-90 kg./sq.cm. SUBSEQUENT ACTIONS: (If auxiliary pump fails to engage automatically) Open cap and switch emergency auxiliary pump switch from auto to on. Check pressure 200-220 Kg/sq.cm. Verify hydraulic pressure in auxiliary system 75-90 Kg/sq.cm. 1. Monitor the standby hydraulic system indicators. 2. Radio Calls 3. Land as soon as possible.



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MAIN HYDRAULIC OIL TEMPERATURE ABOVE LIMITS INDICATIONS: Master warning light on, Main Hyd light on, main hydraulic system oil temperature 88.5 to 96 C. Pressure 64 to 90 kg./sq.cm. IMMEDIATE ACTIONS: Master warning light ............................................................................................ Reset SUBSEQUENT ACTIONS: 1. Standby hydraulic press and temperature ............................................... Check 64-90 Kg/sq.cm. not above 85 C 2. Radio Calls NOTE: if oil temperature does not exceed 100 C land as soon as practical. if oil temperature exceeds 100 C land as soon possible.



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STANDBY HYDRAULIC SYSTEM PRESSURE BELOW LIMITS INDICATIONS: Master warning light on, standby hydraulic light on, pressure in standby hydraulic system below 50 kg/sq.cm. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset 2. Main hydraulic pump pressure ............................................................... Check 64-90 Kg/sq.cm. SUBSEQUENT ACTIONS: 1. Radio Calls. 2. Land as soon as possible.



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STANDBY HYDRAULIC SYSTEM PRESSURE ABOVE LIMITS INDICATIONS: Master warning light on, Stby Hyd light on, standby hydraulic system oil temperature 88.5 to 96 C. Pressure 64 to 90 kg./sq.cm. IMMEDIATE ACTIONS: Master warning light ............................................................................................ Reset SUBSEQUENT ACTIONS: 1. Main hydraulic pressure and temperature ............................................... Check 64-90 Kg/sq.cm. not above 85 C 2. Radio Calls NOTE: if oil temperature does not exceed 100C land as soon as practical. if oil temperature exceeds 100C land as soon as possible.



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AUXILIARY HYDRAULIC SYSTEM FAILURE

INDICATIONS: Master warning light on, auxiliary hydraulic light on. Pressure in auxiliary hydraulic system below 50 Kg/sq.cm. IMMEDIATE ACTIONS: Master Warning Light .......................................................................................... Reset SUBSEQUENT ACTIONS: 1. Before landing open cap and switch auxiliary pump emergency switch from

auto to on. 2. Radio Calls. 3. Land as soon as practical. NOTE: In the case of an auxiliary hydraulic system failure, the Aux Hyd Fail light is

on only in the following cases: In flight with the main hydraulic system failed and pressure below 50 kg./sq.cm. On the ground with the hydraulic tanks are pressurized and pressure below 50

kg./sq.cm. CAUTION: With main and auxiliary hydraulic failure, there is not wheel brakes.

Chock wheels before engine shut down.



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MAIN/STANDBY SYSTEM PRIMARY CONTROL VALVES JAMMING INDICATIONS: Master Warning Light on. Main/Stby Hyd Ctrl valve light on. IMMEDIATE ACTIONS: Master Warning Light .......................................................................................... Reset Main/Stby Hyd. Pressures ................................................................................. Check 64-90 kg./sq.cm. SUBSEQUENT ACTIONS 1. Monitor the hydraulic systems instruments. 2. Land as soon as possible.



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HYDRAULIC SYSTEM PRESSURIZATION FAILURE INDICATIONS: Master Warning Light on. No Hyd Tnk Press light on. IMMEDIATE ACTIONS: 1. Master Warning Light ............................................................................... Reset SUBSEQUENT ACTIONS: 1. Before landing open cap and switch auxiliary pump emergency switch from

auto to on. 2. Radio Calls. 3. Land as soon as practical. CAUTION: After landing with no Hyd Tnk. Press light on the auxiliary pump will cut

out automatically.



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AUTO PILOT FAILURE INDICATIONS: Helicopter abruptly changes attitude. Check Panel Ap light on. Indication of actuator indicators on stop limit or move from stop to stop limits. IMMEDIATE ACTIONS: Auto Pilot ................................................................................................................ Off Maintain level attitude. SUBSEQUENT ACTIONS: 1. Reset Auto pilot ................................................................. Check 3 green lights

If one or more green lights do not illuminate switch off the affected channels. 2. Radio Calls. 3. Land as soon as practical. NOTE: There are no flight restrictions with auto pilot off. However, you may have to

depress cyclic trim button more frequently. Fly at airspeeds that are comfortable.



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ELECTRICAL

AC GENERATOR FAILURE INDICATIONS: Master warning light on, LH or RH AC generator light on. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset 2. Cycle affected AC Generator switch Off/On

If AC Generator fails to come on line continue with the checklist. SUBSEQUENT ACTIONS: 1. AC Amps ............................. Monitor and verify in accordance with circuit load. 2. AC Volts ............................................................. Monitor. 115-119 volts verify. 3. Radio Calls. 4. Land as soon as practical.



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DUAL AC GENERATOR FAILURE INDICATIONS: Master warning light on, both generator lights on, 36V inverter light on. 115V inverter light on. Both rectifier lights on. Main TRNS OFF light on Battery bus light on. AC ammeter zero. AC voltmeter zero. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset 2. Inverter ............................................................................................. To Manual 3. 36V inverter light ................................................................................ Verify On 4. 115V inverter light .............................................................................. Verify On 5. Cycle generators switches off/on SUBSEQUENT ACTIONS: 1. Radio Calls. 2. Land as soon as possible. NOTE: To prolong flight time to 30 min switch off fuel transfer pumps and

transponder. Emergency cabin lighting switch to neutral. (All unnecessary DC power).

CAUTION: When transfer pumps are switched off the only fuel available is from

No2 and 5 tanks.



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RECTIFIER FAILURE INDICATIONS: Master warning light on, LH or RH rectifier light on. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset SUBSEQUENT ACTIONS: 1. Check DC volts ............................................................................ 27-30V verify 2. Radio Calls 3. Land as soon as practical.



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DUAL RECTIFIER FAILURE INDICATIONS: Master warning light and audio signal on, both rectifier lights on. Battery bus light on. IMMEDIATE ACTIONS: Reset Master warning light (this will also cancel audio) SUBSEQUENT ACTIONS: 1. Radio Calls. 2. Land as soon as possible. NOTE: To prolong flight time to 30 min switch off fuel transfer pumps and

transponder. Emergency cabin lighting switch to neutral. (All unnecessary DC power.)

CAUTION: When transfer pumps are switched off the only fuel available is from

No2 and 5 tanks.



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MAIN TRANSFORMER FAILURE INDICATIONS: Master warning light on, main transformer light on. IMMEDIATE ACTIONS: 1. Master warning light ................................................................................. Reset SUBSEQUENT ACTIONS: 1. Main transformer/standby transformer switch .............To Standby Transformer 2. Continue flight.



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BATTERY HOT INDICATIONS: Master warning light and audio signal on, LH or RH battery hot lights on IMMEDIATE ACTIONS: 1. Reset Master warning light ( this will also cancel audio) 2. Affected battery ............................................................................................ Off SUBSEQUENT ACTIONS: 1. Monitor battery hot lights 2. Radio Calls 3. Land as soon as possible.



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GEARBOX

MAIN GEARBOX OIL PRESSURE BELOW LIMITS INDICATIONS: Master warning light and audio signal on, gearbox oil pressure low light on, oil pressure less than 1.3 kg/sq.cm., possible oil temperature increase. IMMEDIATE ACTIONS: 1. Reduce power and commence emergency descent 2. Reset Master warning light. ( this will also cancel audio) 3. Main gearbox temperature and pressure .............................................. Monitor 4. Radio calls. 5. Descend to the lowest possible safe altitude for flight. 6. Land as soon as possible. SUBSEQUENT ACTIONS: NOTE: Airspeed maximum 70kts. If pressure continues to decrease or noises heard

from the main gearbox area land or ditch immediately.



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MAIN GEARBOX OIL TEMPERATURE ABOVE LIMIT INDICATIONS: Master warning light on, gearbox oil hot light on, gearbox oil temperature above 100 C. IMMEDIATE ACTIONS: 1. Reduce power and commence emergency descent 2. Reset Master warning light. (this will also cancel audio) 3. Main gearbox temperature and pressure .............................................. Monitor 4. Radio calls. 5. Descend to the lowest possible altitude for flight. 6. Land as soon as possible. SUBSEQUENT ACTIONS: NOTE: Airspeed maximum 70kts. If main gearbox temperature and pressure beyond

limits, be prepared to land or ditch immediately.



PAGE 38

CHIPS IN MAIN GEARBOX OIL INDICATIONS: Master warning light and audio signal on, gearbox chip light on. Possible low oil pressure and high oil temperature. IMMEDIATE ACTIONS: 1. Reduce power and commence emergency descent 2. Reset Master warning light. ( this will also cancel audio) 3. Main gearbox temperature and pressure .............................................. Monitor 4. Radio calls. 5. Descend to the lowest possible altitude for flight. 6. Land as soon as possible. SUBSEQUENT ACTIONS: NOTE: Airspeed maximum 70kts. If main gearbox temperature and pressure

beyond limits or noises heard from the main gearbox area, land or ditch immediately.

kamov ka 32 procedures - vih cd/vih/pilot/ka32_emergency.pdf · ka‐32 emergency procedures...

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