(b)
Make sure that the MACH TRIM FAIL light on the Pilots' Overhead Panel is off.
(c)
Push the master caution annunciators below the MASTER CAUTION light.
(d)
Make sure that these lights come on: 1) MASH TRIM FAIL light on the P5-3 overhead panel 2) Master Caution FLT CONT Annunciator (P7) 3) Left and right MASTER CAUTION lights (P7).
(e)
Push the MASTER CAUTION light.
(f)
Make sure that these lights are OFF: 1) MASH TRIM FAIL light on the P5-3 overhead panel 2) Master Caution FLT CONT Annunciator (P7) 3) Left and right MASTER CAUTION lights (P7).
(g)
Close the A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.
(h)
Open the B FCC DC circuit breaker on the P6-2 Circuit Breaker Panel.
(i)
Make sure that the MACH TRIM FAIL light stays off.
(j)
Push the master caution annunciators.
(k)
Make sure that these light are ON: 1) MASH TRIM FAIL light on the P5-3 overhead panel 2) Master Caution FLT CONT Annunciator (P7) 3) Left and right MASTER CAUTION lights (P7).
(l)
Push the MASTER CAUTION light.
(m)
Make sure that these light are OFF: 1) MASH TRIM FAIL light on the P5-3 overhead panel
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 08 Page 548 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
2) Master Caution FLT CONT Annunciator (P7)
3) Left and right MASTER CAUTION lights (P7).
(n)
Open the A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.
(o)
Make sure that these light are ON: 1) MASH TRIM FAIL light on the P5-3 overhead panel 2) Master Caution FLT CONT Annunciator (P7) 3) Left and right MASTER CAUTION lights (P7).
(p)
Push the MASTER CAUTION light.
(q)
Make sure that the MACH TRIM FAIL light stays on.
(r)
Make sure that the MASTER CAUTION light and master caution annunciators are off.
(s)
Close the A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.
(t)
Close the B FCC DC circuit breaker on the P6-2 Circuit Breaker Panel.
(u)
Make sure that the MACH TRIM FAIL light is off.
TASK 22-11-00-835-064
4. Rigging Tests_____________
A. General
(1) The BITE rigging test makes sure that the surfaces are correctly aligned. The rigging test includes the pitch and roll actuators, LVDT feedback, aileron and elevator position signals, and neutral shift sensor rigging. The authority checks are for the pitch, roll, and stabilizer actuators.
NOTE: Use the rigging limits shown in this section for the
____ latest engineering values. The CDU display can show incorrect limits.
(2) The BITE rigging test includes:
(a)
Elevator Rigging Test
(b)
Aileron Rigging Test
(c)
Flaps Rigging Test
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
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ú ú 11 Page 549 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B.
C.
D.
A
737-300/400/500MAINTENANCE MANUAL
(d)
Stabilizer Rigging Test
(e)
Pitch Control Wheel Steering Rigging Test
(f)
Roll Control Wheel Steering Rigging Test
(g)
Mach Trim Rigging Test
(h)
Alpha Vane Rigging Test
Standard Tools and Equipment
(1)
Adapter Assemblies - Control Wheel Torque Tool; F72867-1
(2)
Torque Wrenches - 10 lb-ft and 50 lb-ft (two are necessary)
(3)
Spring Scale - Chatillion Model; DPP-50
(4)
Trammel Bar - Stabilizer Actuator; F80055-1 or Measurement Tape - Steel
(5)
Pressure Source - Dry air; 0 to 5 psi, F72928-33 with gage and fittings (to connect to the feel system pitot tubes)
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航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(66)
