(2)
An inspection of the horizontal stabilizer
(3)
The installation of the horizontal stabilizer.
TASK 27-41-11-206-001
2. Horizontal Stabilizer Inspection (Fig. 601)________________________________
A. Standard Tools and Equipment
(1)
Micrometer - 0-1 inch
(2)
Vernier Caliper
B.
References
(1)
27-41-11/401, Horizontal Stabilizer
C.
Access
(1)
Access Panels
3801 Tail Cone Access Door, LH
3802 Tail Cone Access Door, RH
D.
Procedure
S 026-002
(1)
Do this task: "Horizontal Stabilizer Removal" (Ref 27-41-11/401).
S 216-003
(2)
Examine the parts for worn areas:
(a)
Use a micrometer or a vernier caliper to measure the parts for the worn areas.
(b)
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601.
(c)
Replace the parts that are not in the tolerance.
(d)
Install the parts.
S 426-004
(3) Do this task: "Horizontal Stabilizer Installation"
(Ref 27-41-11/401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-11
ALL ú ú 01 Page 601 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
REAR SPAR FITTINGS
SEE B
HINGE SUPPORT
FWD
A 737-300/400/500MAINTENANCE MANUAL
FRONT SPAR FITTINGS
SEE A
JACKSCREW SUPPORT
1. BUSHING/BOLT
3. BUSHING/BOLT
UPPER FITTING
4. BUSHING/BOLT
CENTER FITTING
5. BUSHING/BOLT
2. BUSHING/BOLT
LOWER FITTING
B
A
Horizontal Stabilizer Wear Limits Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-11
ALL ú ú 01 Page 602 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS PARTWORN REPLACE PART WORN REPAIR INSTR REPAIR
DIAMETER PER-MITTED WEAR DIM. ANCE CLEAR-MAX DIA
MIN MAX
1 BUSHING ID 1.0030 1.0045 1.0090 .010 1
BOLT OD .9985 .9990 .9930 1
2 BUSHING ID .8780 .8795 .8840 .010 1
BOLT OD .8735 .8740 .8680 1
3 BUSHING ID 1.3781 1.3791 1.3840 .010 1
BOLT OD 1.3725 1.3740 1.3681 1
4 BUSHING ID 1.3781 1.3791 1.3840 .010 1
BOLT OD 1.3725 1.3740 1.3681 1
5 BUSHING ID 1.5031 1.5041 1.5090 .010 1
BOLT OD 1.4975 1.4990 1.4931 1
REPLACE WITH NEW PART HAVING SAME PART NUMBER
Horizontal Stabilizer Wear Limits
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-11
ALL ú ú 01 Page 603 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
HORIZONTAL STABILIZER LEADING EDGE - REMOVAL/INSTALLATION
_________________________________________________________
1. General
_______
A. This procedure has two tasks, one for the removal and one for the installation of the horizontal stabilizer leading edge (which is referred to as the leading edge). The procedure has these parts:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(94)