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时间:2011-10-21 11:52来源:蓝天飞行翻译 作者:航空
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I VARNISH PROTECTION I  
  

ASSEMBLY OR
CONNECTION OF BONDING
ELEMENT
DEGREASING
I VARNISH PROTECTION I
Electrical bonding — Procedure flow sheet
Table 201
AAAA
Validity : S / N 1 — 9999 20-00 12Page 203
(sA) DEC 98
 
PAGE INTENTIONALLY LEFT BLANK
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Validity : S / N 1 — 9999 20-00-12Page 204
(BA) OCT 97
 
UTILIZATION OF CLINOMETER
MAINTENANCE PRACTICES
1. SERVICING (Figure 201) A. Procedure
NOTE : Quoted from the "Maintenance Manual for use by the Maintenance and Repair Shops" —Airframe Manual — DGAC — SFACT — N° AC 65-15.
1) With the rim / disk locking device being engaged in the deep slot, rotate the disk setting device so as to lock the disk onto the rim.
2) Put the control surface to neutral position. Position the clinometer on the control surface and rotate the rim setting device so as to bring the bubble of the center level between the marks (the rim should be unlocked from the frame).
3) Lock the ring on the frame using the ring lock on the frame.
4) Bring the control surface to its maximum travel limit.
5) Unlock the disk from the rim using the rim / disk locking device.
6) Rotate the disk setting device so as to bring the bubble of the center level between the marks.
7) Read the control surface travel, expressed in degrees on the disk and in tenths of degree on the vernier.
I AAAA
Validity : S / N 1 — 9999 20-00-13Page 201
(BA) DEC 98
 
Utilization of clinometer
Figure 201
AAAA
Validity : S / N 1 — 9999 20-00-13Page 202
(BA) DEC 98
 
NON-DESTRUCTIVE INSPECTION
DESCRIPTION AND OPERATION
1. GENERAL
The purpose of non—destructive inspection consists in detecting structural defects without altering the area or adjacent equipment.
It mainly consists in an inspection for cracks and corrosion. The main methods used are :
— visual inspection,
— penetrant inspection as a complement to the visual inspection.
2. DESCRIPTION
A. Visual inspection
This method consists in visually inspecting suspicious parts. This requires a thorough cleaning of the incriminated area.
Visual inspection is the oldest and most common form of non—destructive inspection. It provides a means of detecting and examining a wide variety of material surface discontinuities such as cracks, corrosion, contamination, surface finish, weld joints, solder connections and adhesive disbonds.
This method can be used by any person but requires, nevertheless, the knowledge, skills and abilities to understand where flaws are likely to occur in the aircraft.
The use of optical aids for visual inspection is beneficial and recommended.
 
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本文链接地址:TB20 MAINTENANCE MANUAL 20 STANDARD PRACTICES AIRFRAME TB20飞机维护手册 20 标准施工机体(54)