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时间:2011-03-31 15:30来源:蓝天飞行翻译 作者:航空
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(2)  
Tilt vertical gyro No. 1 until captain's ADI indicates 10 degrees pitch down (attitude assembly moves toward top of indicator). 

NOTE:  ADI should follow displacements of vertical gyro smoothly with no sluggishness or overshoot.

(3)  
Tilt vertical gyro No. 1 until captain's ADI indicates 10 degrees pitch up.


5C8
Jun 20/85 34-22-0 Page 501
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(4)  
Tilt vertical gyro No. 1 until captain's ADI indicates 20 degrees right roll (attitude tape rotates counterclockwise).

(5)  
Tilt vertical gyro No. 1 until captain's ADI indicates 20 degrees left roll.

(6)  
Repeat steps (2) thru (5) using vertical gyro No. 2 and first officer's ADI.

(7)  
Place VERTICAL GYRO transfer switch in BOTH ON 2 position and repeat steps (2) thru (5) using vertical gyro No. 2 and captain's ADI.

(8)  
Place VERTICAL GYRO transfer switch in BOTH ON 1 position and repeat steps (2) thru (5) using vertical gyro No. 1 and F/O's ADI.

(9)  
Return vertical gyros to level and install mounting bolts.


C.  Attitude Warning Flag Circuit Test
(1)  
Check warning circuits as tabulated below.

(2)  
Circuit breakers shall be opened one at a time and closed at completion of each test.

(3)  
Check that flag appears when breaker is opened, disappears when breaker is closed.


TEST  VG TRANSFER SWITCH POSITION  OPEN CIRCUIT BREAKER  GYRO FLAG APPEARS ON ADI 
1  NORMAL  VERT GYRO-1  Captain’s 
2  NORMAL  CAPT HORIZ  Captain’s 
3  NORMAL  VERT GYRO-2  F/O’s 
4  NORMAL  F/O HORIZ  F/O’s 
5  BOTH ON 2  VERT GYRO-2  Captain’s * 
F/O’s 
6  BOTH ON 2  CAPT’S HORIZ (ALT  Captain’s 
7  BOTH ON 2  F/O’S HORIZ  Captain’s & 
F/O’s 

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VG TRANSFER  GYRO FLAG 
SWITCH  OPEN  APPEARS 
TEST  POSITION  CIRCUIT BREAKER  ON ADI 

8
BOTH ON 2 INST XFMR-2  Captain’s
9
BOTH ON 1 VERT GYRO-1 Captain’s & F/O’S 10 BOTH ON 1 F/O’S HORIZ (ALT) F/O’s
11 BOTH ON 1 CAPT’S HORIZ  Captain’s & F/O’s
12 BOTH ON 1 INST XFMR-1  F/O’S
13 BOTH ON 1  PLACE INVERTER SWITCH F/O’S TO ON
(4) Place VERTICAL GYRO transfer switch in NORMAL position.
D. Vertical Gyro Transfer Relay Monitor Test
(1)
Check transfer relay monitor as tabulated below.

(2)
Open instrument transfer circuit breaker for test and reclose at the completion of each test.


VG TRANSFER  REPOSITION VG 
SWITCH  OPEN  TRANSFER  FLAG APPEARS 
TEST  POSITION  CIRCUIT BREAKER  SWITCH TO  ON ADI 

1  NORMAL  INSTR TRANS  BOTH ON 2 BOTH ON 1  Captain’s F/O’s 
2  BOTH ON 2  INSTR TRANS  NORMAL BOTH ON 1  Captain’s Captain’s & F/O’s 
3  BOTH ON 1  INSTR TRANS  NORMAL BOTH ON 2  F/O’S Captain’s & F/O’s 
E.  Remove electrical power from airplane 

May 01/76  34-22-0
Page 503
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

3.  System Test
A.  Equipment and Materials
(1)  
Calibrated tilt tables (2 required)

(2)  
Gyro extension cables suitably terminated to extend airplane wiring to tilt tables (2 required)


B.  Prepare for System Test
(1)  
Remove vertical gyros from mountings and install on calibrated tilt tables (oriented as installed in airplane).

(2)  
Connect jumper cables between gyros and their respective airplane connector.

(3)  
Adjust tilt tables to zero degrees roll and pitch.

(4)  
Connect electrical power to airplane and close GND PWR switch on panel P5. Energize No. 1 and 2 electronics buses by closing ac and dc circuit breakers on panel P6 and placing master switches in ON position.

(5)  
Check that following circuit breakers are closed: VERT GYRO-2, F/O HORIZ (ALT), INST XFMR-2, F/O's HORIZ and INV CONT on panel P6; VERT GYRO-1, CAPT'S HORIZ (ALT), INST XFMR-1, CAPT'S HORIZ, and INSTR TRANS on panel P18.
 
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