BOEING 737
MAINTENANCE MANUAL
CHAPTER 10 TAB EFFECTIVE PAGES SEE LAST PAGE OF LIST FOR NUMBER OF PAGES CONTENTS 10 1 FEB 20/87 5052 BLANK PAGE DATE CODE 10- 12-0 (CONTINUED)* 228 SEP 01/02 500229 MAY 01/01 500230 MAY 01/00 500 10- 13-0 201 JUN 20/92 500202 FEB 01/96 501202A JUN 20/93 500202B BLANK 203 JUN 20/92 501204 BLANK PAGE DATE CODE PAGE DATE CODE PAGE DATE CODE
10- 11-0 * 201 MAY 01/03 500202 MAY 15/67 500202A JUN 20/86 501202B FEB 20/92 5C9202C FEB 20/92 5C9202D JUN 20/86 5C9202E JUN 20/86 5C9202F JUN 20/86 5C9202G JUN 20/86 5C9202H JUN 20/86 501203 MAY 01/99 539204 MAY 15/67 500* 205 MAY 01/03 501206 MAY 01/98 500* 207 MAY 01/03 500208 MAY 01/99 500209 MAY 01/98 500210 MAY 01/98 500* 211 MAY 01/03 500212 MAY 01/98 500 10- 20-0 201 NOV 15/68 500202 BLANK 10- 21-0 201 MAY 01/98 501202 MAY 01/98 500203 MAY 01/00 500204 MAY 01/98 500
10- 12-0 201 MAY 01/01 500* 202 MAY 01/03 500203 JUN 20/92 500* 204 SEP 01/02 500* 205 SEP 01/02 500* 206 SEP 01/02 500207 FEB 20/93 500* 208 SEP 01/02 500209 FEB 01/95 500* 210 MAY 01/03 500211 JUN 20/93 500* 212 MAY 01/03 500213 FEB 01/95 500214 JUN 20/92 500215 JUN 20/92 500* 216 MAY 01/03 500217 JUN 20/92 500218 MAY 01/01 500219 MAY 01/01 500220 JUN 20/92 500* 221 MAY 01/03 500* 222 MAY 01/03 500223 JUN 20/92 500224 FEB 20/94 500* 225 MAY 01/03 500* 226 MAY 01/03 500227 JUN 20/93 500
* = REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE
C8 CHAPTER 10 EFFECTIVE PAGES
MAY 01/03 PAGE 1
LAST PAGE
D6-37115
CHAPTER 10
PARKING AND MOORING
Subject TABLE OF CONTENTS Subject No.
PARKING
NORMAL PARKING.................................................................................................... Maintenance Practices 10-11-0
PROLONGED PARKING............................................................................................ Maintenance Practices 10-12-0
HIGH WIND CONDITIONS PARKING........................................................................ Maintenance Practices 10-13-0
MOORING ...................................................................................................................... Maintenance Practices 10-20-0
HIGH WIND CONDITIONS MOORING ................................................................... Maintenance Practices 10-21-0
505
Feb 20/87 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Contents 10 Page 1
NORMAL PARKING
1. General
A. The airplane is normally parked for short periods with chocks in front of and behind at least one main gear wheel, and with parking brakes off. The parking brake is used to hold the airplane until chocks are in place. Openings in the airplane structure such as vents and scoops shall be covered or plugged to keep out weather and foreign matter. Should very high winds be expected, refer to 10-21-0, High Wind Conditions, Mooring. For special procedures to park the airplane for engine operation refer to 71-09-100/201.
B. A static ground on the airplane is not necessary when the airplane is parked or is serviced during the turnaround operation. This does not include when the maintenance steps given below are done (Ref chapter 20-40-11).
(1)
A static ground on the airplane is not necessary when you pressure refuel the airplane. An electrical bond between the airplane and the refuel vehicle is recommended.
(2)
A static ground of the airplane when you fuel over the wing is recommended.
(3)
Do a static ground of the airplane when you do maintenance procedures. Do this when you use devices such as lights, power tools, and instruments powered from external cords that are attached to grounded electrical power sources.
C. Pitot probe covers and static port covers are recommended when the airplane is parked for more than a standard turnaround.
D. Failure to remove covers from pitot probes or coverings from static ports before flight may cause large errors in airspeed-sensing and altitude-sensing signals, which may lead to loss of safe flight.
E. A minimum distance of 15 feet should be maintained between airplanes being towed or parked to give adequate turning clearances (Fig. 201). If engine operation is anticipated, refer to Fig. 202 to ensure airplanes, maintenance personnel and equipment, and buildings, adequate protection from jet blast and heat at breakaway from standstill. Various thrust settings that will be required for breakaway from standstill are governed by airplane position, type of area, and surface conditions. A high initial thrust setting is required to start airplane movement. The setting is then reduced to idle, or slightly above, to continue the maneuver.
WARNING: DO NOT CROSS ENGINE EXHAUST AREA DURING ENGINE RUN-UP OR TAXIING. BE SURE AREAS IN FRONT OF ENGINES ARE CLEAR BEFORE ENGINE RUN-UP.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737 AMM 飞机维护手册 PARKING AND MOORING
