6-10-00 Page 6-7 Revised: February 28, 2002
Figure 6-1. Three View
6-10-00
Page 6-8
Revised: February 28, 2002
1C22
STATION REFERENCE LINES.
In order to facilitate the location of various components of the airplane which require maintenance and servicing, a method utilizing fuselage station, wing station or buttock line (BL), and waterline (WL) designations is frequently employed in this manual. (Refer to Figure 6-2.) Fuselage stations, buttock lines, and waterlines are reference points measured by inches in the vertical or horizontal direction from a given reference line which indicates station locations of structural members of the airplane.
Page 6-9 Revised: February 28, 2002
1C23
WEIGHT AND BALANCE DATA.
When figuring various weight and balance computations, the empty, static and gross weight, and center of gravity of the airplane may be found in the Weight and Balance Form of the Pilot's Operating Handbook.
SERIAL NUMBER PLATE.
The Serial Number Plate is located on the bottom of the fuselage forward of station 247.125. The Serial Number should always be included when referring to the airplane on service or warranty matters.
THIS SPACE INTENTIONALLY BLANK
Page 6-10 Revised: February 28, 2002
1C24
ACCESS PLATES AND INSPECTION PROVISIONS.
The access plates and inspection provisions for the airplane are shown in Figure 6-3. The component to be serviced or inspected through each opening is identified in the illustration. All access plates and panels are secured by either metal fasteners or screws. To enter the aft section of the fuselage, remove the rear trim panel.
THIS SPACE INTENTIONALLY BLANK
Page 6-11 Revised: February 28, 2002
1D1
STABILATOR TRIM DRIVE & LINKAGE AUTOPILOT TRIM SERVO
STABILATOR PUSH ROD ELECTRIC TRIM SERVO
2.
NAV ANTENNA 8. SUMP DRAINS
3.
Not Used 9. FLAP TORQUE TUBE
4.
ELT CONTROL SYSTEM PULLEY STABILATOR PUSH ROD & BELLCRANK FUEL SYSTEM RUDDER CONTROL CABLES FUEL SYSTEM VALVES STABILATOR CONTROL CABLES FUEL SYSTEM FILTER RUDDER TRIM CABLES HYDRAULIC LINES STABILATOR TRIM CABLES FLAP RETURN SPRINGS CONTROL SYSTEM PULLEYS AUTO PILOT ROLL SERVO
5.
LOWER RUDDER HINGE 10. FUEL SYSTEM CONTROL CABLES & ANCHORS RUDDER SECTOR CONTROL SYSTEM CABLES & PULLEYS
6.
COMBUSTION HEATER 11. FUEL SYSTEM CONTROL SELECTOR SLIDES BATTERY & BATTERY BOX 12. STABILATOR & RUDDER TRIM REGULATOR (2) FLAP HANDLE. DEFROSTERS CONTROL SYSTEM PULLEYS BRAKE RESERVOIR 13. ENGINE CONTROL CABLES FREE FALL VALVE CARBURETOR HEAT CONTROL LEVERS NOSE GEAR STEERING COWL FLAP CONTROL LEVERS AUTOPILOT 14. NOSE GEAR STARTER RELAYS NOSE GEAR ACTUATOR CYLINDER AUXILIARY POWER GEAR UP & GEAR DOWN SWITCHES
15.
CONTROL CABLE INSPECTION PANELS WING TIP LIGHTNING BONDING FUEL LINES AILERON BALANCE WEIGHT FINGER STRAINER PITOT STATIC HEAD 23. PROPELLER DOME PRESSURE
Figure 6-3. Access Plates and Panels
6-30-00
Page 6-12
Revised: February 28, 2002
1D2
16.
PITOT STATIC LINES 24. OIL SCREEN
17.
FUEL SYSTEM LINES 25. FUEL FILLER CAVITY DRAIN VACUUM SYSTEM LINES 26. WING INTERIOR SENDER FOR ANNUNCIATOR LIGHTS 27. WING INTERIOR
(VACUUM PRESS. & OIL PRESS.) 28. WING INTERIOR ENGINE CONTROL CABLES 29. AILERON BELLCRANK FUEL SYSTEM VENT LINE AILERON CONTROL CABLES ELECTRICAL SYSTEM 30. FUEL TANK VENT
18.
FUEL FILLER 31. WING / NACELLE INTERIOR
19.
FUEL QUANTITY SENDER 32. FUEL TANK VENT LINE BLADDER ACCESS HOLE 33. MAIN GEAR ATTACK BOLT
20.
OIL DIPSTICK & FILLER 34. MAIN GEAR
21.
PRIMER LINES HYDRAULIC ACTUATOR CYLINDER PITOT STATIC LINES GEAR LIMIT SWITCHES VACUUM SYSTEM LINES ENGINE CONTROL CABLES ELECTRICAL SYSTEM
Figure 6-3. Access Plates and Panels (cont)
6-30-00
Page 6-13
Revised: February 28, 2002
1D3
THIS PAGE INTENTIONALLY BLANK
6-30-00 Page 6-14 Revised: February 28, 2002
1D4
CHAPTER
7
LIFTING AND SHORING
THIS PAGE INTENTIONALLY BLANK
CHAPTER 7 - LIFTING AND SHORING
TABLE OF CONTENTS / EFFECTIVITY
CHAPTER/ SECTION SUBJECT GRID NO. EFFECTIVITY
7-10-00 JACKING 1D9 1R0202
7-Cont./Effec. Page 7-3 Revised: February 28, 2002
THIS PAGE INTENTIONALLY BLANK
7-Cont./Effec. Page 7-4 Revised: February 28, 2002
1D8
JACKING.
Jacking the airplane is necessary to service the landing gear and related systems. Jacking is normally performed with conventional tripod jacks, but in special situations, such as emergencies or post-accident, slings or air bags can be used.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：西门诺尔飞机维护手册 simenole PA-44-180 AMM 1(22)
