Shared Flashcard Set

Details

65 Emergencies 2
CG Aviation
12
Aviation
Not Applicable
12/20/2010

Additional Aviation Flashcards

 


 

Cards

Term

 

 

 

WHEELS FAIL TO EXTEND

Definition

Symptoms:

1. Amber light or absence of green lights with landing

gear handle in DOWN position

2. Gear visually checked not in down position

3. Blue landing gear indicator light not illuminated

4. LDG LOCKED not annunciated on the VEMD CAUTION/

FUEL page

 

Corrective Action:

1. LANDING GEAR INDICATOR − TEST

NOTE

This will reveal a bulb failure or loss of power to

the landing gear indicator. Power to the indicator

is provided through the GEAR IND circuit

breakers (pilot and copilot side).

If landing gear lights do not illuminate:

 

2. GEAR IND CIRCUIT BREAKERS − PULL, RESET

(pilot aft panel R5 #11 and copilot side panel R1 #8)

If landing gear lights do illuminate:

2. LANDING GEAR HANDLE − UP, THEN DOWN

If landing gear failure persists:

3. LANDING GEAR HANDLE − UP

4. GEAR CONT CIRCUIT BREAKER − PULL, RESET

(pilot aft panel R3 #9)

5. LANDING GEAR HANDLE − DOWN

If wheels extend:

6. SAFETY PIN − INSTALL (if available)

7. CONTINUE FLIGHT AS APPROPRIATE

If failure persists (and a Secondary Hydraulic System

low fluid level condition does not exist):

8. ELECTRIC PUMP − ACTIVATE (BKP position)

9. ELECTRIC PUMP − OFF

 

If wheels extend:

10. CONTINUE FLIGHT AS APPROPRIATE

 

 

If failure persists:

11. EMERGENCY LANDING GEAR EXTEN−

SION HANDLE − PULL

 

If wheels fail to extend:

12. CONSIDER EXTERNAL ACTIVATION OF LANDING

GEAR BLOW DOWN BOTTLE TO EXTEND

LANDING GEAR − ACTIVATE FROM THE

GROUND BY REMOVING FLAGGED SAFETY

PIN AND ACTUATOR PIN (located in chine panel

forward of the left main mount)

 

If wheels still fail to extend:

13. CONSIDER USE OF EXTERNAL NITROGEN

CANISTER VIA THE LANDING GEAR NITROGEN

LINE T−FITTING TO EXTEND LANDING

GEAR (located in chine panel forward of the left

main mount)

 

14. LAND AS SOON AS PRACTICABLE. (If loss of

fluid situation exists or is suspected − PERFORM

VERTICAL LANDING.)

 

 

 

 

 

 

 

 

 

Term

 

 

 

WHEELS FAIL TO RETRACT

Definition

Corrective Action:

1. LANDING GEAR HANDLE − RECYCLE

 

If failure persists:

2. LANDING GEAR HANDLE − DOWN

3. LAND

4. NOSEWHEEL − STRAIGHTEN

After takeoff:

 

5. LANDING GEAR HANDLE − UP

If failure persists:

6. LANDING GEAR HANDLE − DOWN

7. CONTINUE FLIGHT AS APPROPRIATE

Term

 

 

 

NOSEWHEEL SHIMMY DAMPER FAILURE

Definition

Symptom:

1. Lateral vibration when performing run on/off maneuvers

and during high speed taxiing. These vibrations

may be quite violent.

 

Corrective Action:

1. LIFT AIRCRAFT OFF GROUND IMMEDIATELY OR REDUCE TAXI SPEED

2. PERFORM VERTICAL LANDINGS OR TAKEOFFS

 

3. CONTINUE FLIGHT AS APPROPRIATE

Term

 

 

 

UPLOCK FAILURE

Definition

Symptom:

1. Amber GEAR UNSAFE light remains on or illuminates

intermittently with handle in UP position

 

Corrective Action:

1. LANDING GEAR HANDLE − RECYCLE

If failure persists:

2. LANDING GEAR HANDLE − DOWN

3. CONTINUE FLIGHT AS APPROPRIATE

Term

 

 

 

AUDIO SYSTEM FAILURE

Definition

Operation of both AUDIO BYPASS switches eliminates

the audio mixer and provides a power source directly

from the respective COMM radio. This eliminates all volume

control except for the MSTR VOL (master volume)

control on the applicable audio control panel.

For the pilot, copilot, and flight mechanic to communicate,

both AUDIO BYPASS switches should be in the

BYPASS position. During BYPASS operation the pilot

can only transmit/receive on COMM 1, the copilot on

COMM 2. All audio warnings are inoperative.

 

Possible Symptoms:

1. Complete loss of audio (all stations)

2. All ICS and transmit functions inoperative

3. Constant squeal or hum heard in headset

 

Corrective Action:

1. PILOT AND COPILOT AUDIO BYPASS

SWITCHES − BYPASS

2. ICS CIRCUIT BREAKERS (2) − PULL, RESET

(cockpit avionics panel R1 #5 and R5 #5)

3. CONTINUE FLIGHT AS APPROPRIATE

 

 

 

Term

 

 

 

EMERGENCY EGRESS PROCEDURES

Definition

1. WAIT FOR ALL VIOLENT MOTION TO STOP

 

2. REFERENCE POINT − HOLD

3. EMERGENCY RELEASE HANDLE − JETTISON

4. CORDS − DISCONNECT

5. SEATBELT/HARNESS − RELEASE AND MAINTAIN

REFERENCE

6. EGRESS

7. VEST − INFLATE WHEN CLEAR OF AIRCRAFT

Term

                     

                    MALFUNCTIONING CABIN

SLIDING DOOR

Definition

Symptom:

1. Cabin sliding door does not fully open or will not secure

in the closed position

Corrective Action:

1. FLIGHT MECHANIC − REMAIN SECURED TO

AIRCRAFT

2. DO NOT USE EXCESSIVE FORCE

3. DOOR ASSEMBLY − INSPECT:

a. RESCUE HATCH − SECURED

b. FORWARD UPPER ROLLER ASSEMBLY − IN

TRACKS

c. FORWARD LOWER ROLLER ASSEMBLY −

ATTACHED TO THE DOOR

4. AERODYNAMIC LOAD ON DOOR − REDUCE

(when ops permit); USING THE FOLLOWING:

a. DECREASE AIRSPEED

b. INDUCE LEFT SIDESLIP (right pedal)

c. OPEN PILOT WINDOW

If safe landing site is available:

5. LAND. REMOVE AND STOW DOOR

 

If safe landing site is not available:

5. JETTISON DOOR FROM A HOVER IN AN APPROPRIATE

MARKED LOCATION

6. CONTINUE FLIGHT AS APPROPRIATE

 

If appropriate location is not available:

5. DOOR − SECURE INTERIOR HANDHOLD ON

DOOR TO DECK TIEDOWN USING TRAIL LINE OR

STRAP

6. SPEED − 80 KIAS MAXIMUM

7. LAND AS SOON AS PRACTICABLE

Term

                         DITCHING/EGRESS

IMMEDIATE EMERGENCY LANDING/DITCHING

Definition

Corrective Action:

1. CREW AND PASSENGERS − ALERTED

2. WHEELS/FLOATS − AS REQUIRED

3. LAND/DITCH AIRCRAFT

4. EFSLS − BOTH OFF (after landing/water entry)

5. EMERGENCY ELECTRICAL CUTOFF − AS REQUIRED

6. ROTOR BRAKE (land only)

7. EMERGENCY EGRESS PROCEDURE − EXECUTE

Term

 

 

 

 

 

DIF/ N1

Definition

 

 

 

 

 

1. COMPLETE THE BIG 4"
2. ENGINE PARAMETERS − MONITOR
3. LAND AS SOON AS PRACTICABLE

Term

 

 

 

 

Minor Fadec Failure/Flashing or Steady GOV Light

Definition

 

 

 

1. COMPLETE THE BIG 4"
2. ABORT MISSION. URGENT MISSION MAY BE
COMPLETED

 

Term

 

 

 

 

Major Fadec Failure

Definition

 

 

1. COMPLETE THE BIG 4"
2. TRNG SWITCH − FLT

3. FADEC BACKUP SWITCH (affected engine) −
BACKUP

4. OEI − SET AS NECESSARY
5. LAND AS SOON AS PRACTICABLE

 

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