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• For Left REV UNLOCK: WARN LTS PWR #4: Pilot’s Aft Panel, F-4
• For Right REV UNLOCK: WARN LTS PWR #8: Pilot’s Aft Panel, G-3
CAUTION
OBSERVE STARTER DUTY CYCLE.
CAUTION
DO NOT ATTEMPT TO START ENGINES IF T/R
DOORS ARE NOT ENGAGED BY THE SECONDARY
LOCK LATCH. PERFORM NEXT STEP IF T/R DOORS
ARE NOT ENGAGED.
IF T/R DOORS ARE NOT ENGAGED:
2. Engine Crank Cycle................PERFORM WITH REVERSER LEVER IN STOW
POSITION
See Section 03-08-40, Engine Cranking Cycle. T/R doors will engage secondary
lock latch.
NOTE:
Engine crank cycle will not lock T/R actuator.
3. Normal Engine Start...............PERFORM WITH REVERSER LEVER IN STOW
POSITION
AFTER ENGINE REACHES IDLE:
4. Circuit Breaker(s) ......................................................................................CLOSE
REV UNLOCK and REV DEPLOY lights should be extinguished.
ALTERNATE METHOD:
NOTE:
As an alternate method to the engine crank cycle, the
T/R doors may be brought through the secondary lock
latch as follows.
5. Electrical / Hydraulic Power................................REMOVED FROM AIRPLANE
6. Flight Controls ....CYCLE TO DISSIPATE ANY RESIDUAL PRESSURE FROM
SYSTEMS
7. Hand Pressure ............APPLY TO LOWER DOOR UNTIL SECONDARY LOCK
LATCH ENGAGES T/R DOORS
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-24-00
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WINDSHIELDS / DOOR SYSTEMS
05-25-10: Windshield Failure
WINDSHIELD HEAT:
If windshield heat failure is detected, cycle the windshield heat control switch(es)
OFF, then ON. If windshield heat cannot be regained, flight may be continued, but
flight into icing conditions should be avoided. If failure involves a front window, pull
the appropriate circuit breaker:
• L FRONT POWER: Copilot’s Aft Panel, J-8
• R FRONT POWER: Copilot’s Aft Panel, L-8
• L SIDE WSHLD: Copilot’s Aft Panel, J-10
• R SIDE WSHLD: Copilot’s Aft Panel, K-10
WINDSHIELD CRACKS:
UPON DETECTING A CRACK IN OUTER HEATING / PROTECTIVE PLY:
1. Windshield Heat..................SELECT AFFECTED WINDOW OFF BY PULLING
APPROPRIATE CIRCUIT BREAKERS
Pull appropriate circuit breaker for affected window. Observe icing restrictions.
• L FRONT POWER: Copilot’s Aft Panel, J-8
• R FRONT POWER: Copilot’s Aft Panel, L-8
• L SIDE WSHLD: Copilot’s Aft Panel, J-10
• R SIDE WSHLD: Copilot’s Aft Panel, K-10
UPON DETECTING A CRACK IN EITHER MAIN STRUCTURAL WINDSHIELD PLY,
THE FOLLOWING IS RECOMMENDED:
2. Cabin Pressure Differential ..........REDUCE TO 7.5 PSI FOR REMAINDER OF
FLIGHT
3. Airspeed / Mach.......................MAINTAIN CURRENT AIRSPEED / MACH FOR
REMAINDER OF FLIGHT
4. GIV Configuration Deviation Listing - Appendix B..................CONSULT FOR
SUBSEQUENT TAKEOFF CONSIDERATIONS
WARNING
IF CRACKING IS TO THE INNER GLASS PLY, IT IS
RECOMMENDED THAT THE PILOT ADJACENT TO
THE CRACK WEAR EYE PROTECTION SUCH AS
SMOKE GOGGLES.
OPERATING MANUAL
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CHAPTER 06 - GROUND / FLIGHT CHARACTERISTICS AND PROCEDURES
LIST OF EFFECTIVE PAGES
ATA PAGE DATE
06-00-00 1 May 31/00
06-00-00 2 May 31/00
06-01-00 1 May 31/00
06-01-00 2 May 31/00
06-02-00 1 May 31/01
06-02-00 2 May 31/01
06-02-00 3 May 31/01
06-02-00 4 May 31/01
06-02-00 5 May 31/01
06-02-00 6 May 31/01
06-02-00 7 May 31/01
06-02-00 8 May 31/01
06-02-00 9 May 31/01
06-02-00 10 May 31/01
06-03-00 1 May 30/02
06-03-00 2 May 30/02
06-03-00 3 May 30/02
06-03-00 4 May 30/02
06-03-00 5 May 30/02
06-03-00 6 May 30/02
06-03-00 7 May 30/02
06-03-00 8 May 30/02
06-04-00 1 May 31/01
06-04-00 2 May 31/01
06-04-00 3 May 31/01
06-04-00 4 May 31/01
*06-05-00 1 October 11/02
*06-05-00 2 October 11/02
*06-05-00 3 October 11/02
*06-05-00 4 October 11/02
*06-05-00 5 October 11/02
*06-05-00 6 October 11/02
*06-05-00 7 October 11/02
*06-05-00 8 October 11/02
*06-05-00 9 October 11/02
*06-05-00 10 October 11/02
*06-05-00 11 October 11/02
*06-05-00 12 October 11/02
　
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