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6) Carry out the same operations on the struts.
7) Remove the wheels :
a) Carry out a dye penetrant inspection on rims and check for distortion.
b) Remove the tires for internal inspection.
c) Carry out a detailed inspection of the axles using a 10 X magnifying glass. If there is any doubt, carry out a dye penetrant or magnetic particle inspection.
8) If the main landing gear lateral slack is significant, remove the wings to carry out a detailed inspection and check for crack and out-of-roundness of the holes concerning :
- wing attachments, on wing and fuselage sides ; carry out a detailed and dye penetrant inspection on all wing attachment brackets and carry out a magnetic particle inspection on the attachment pins (or replace them),
- frame No. 1 under floor,
- wing front small spar (check via lower surface access door and rib N1),
- rear small spar, rear attachment and rear rib N1.
9) Depending on the cases, apply repair procedures recommended by the manufacturer.
10) In all cases, contact the manufacturer for additional investigations and, if necessary, definition or approval of a proposal for rework.
11) Lower the aircraft to ground and remove the jacks - refer to 07-10-00.
ACAA
Validity : S / N 1 - 9999 05-50 01Page 604
(DA) JUN 01
 
INSPECTION AFTER FLIGHT IN SEVERE AIR TURBULENCE
OR WITH SEVERE MANEUVERS
INSPECTION / CHECK
1. GENERAL
This inspection is implemented :
- upon request of the pilot in the flight report,
- after observation during a workshop inspection which would tend to indicate that the airplane has been flown in severe air turbulence.
Checks are broken down into two categories, the first described in Paragraph 2.C. "First-level" investigation, the second is implemented as per conditions described in Paragraph 2.D. "Second-level" investigation.
CAUTION : EVEN IF EVIDENCE OF WRINKLES AND WAVINESS ON FUSELAGE OR WING SKINS MAY SEEM MINOR ENOUGH TO BE CONSIDERED AS NEGLIGIBLE, A CAREFUL AND METICULOUS INSPECTION OF THE INTERNAL STRUCTURE COULD REVEAL MAJOR DAMAGE.
2. DETAILED INSPECTION
A. Tools and consumable materials None
B. Preliminary operations
With the airplane on a flat and, if possible, horizontal area, check whether the various components are in their normal configuration.
C. "First-level" investigation
1) Wings
a) Inspect the central structure of the wing. Particularly check for the following on the lower and upper skins :
- wavinesses in the skin level with the spars, between the rivets,
- wavinesses in the panels,
- missing or slack rivets.
b) Carefully inspect the spar via the inspections doors.
c) Visually inspect the attachment brackets in the feed-through structure ; check for any cracks or riveting faults.
　
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本文鏈接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飛機維護手冊 05 時間限制維護檢查 2(89)