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B. Preliminary steps 601
C. Inspection of the wings 602
D. Final steps 606
2. CORROSION INSPECTION OF THE SPAR /
SKINS INTERFACE FROM N1 RIB TO N4 RIB 606
A. Tools and consumable materials 606
B. Visual examination 607
C. Thorough examination 607
ADAA
Validity : S/ N 1- 9999 Page 1
57-TC (EA) JUN 02
SOCATA
TB 20 MODEL
SUBJECT CHAPTER
WINGS 57-00-00 (CA)
REPAIR MAINTENANCE MANUAL
PAGE VALIDITY
801 1 - 9999
801
1. REPAIR - WRINKLED SKIN, LEADING EDGE BOX,
WING ROOT AREA 801
A. Tools and consumable materials 801
B. Procedure 801
2. PRINCIPLE OF BLANKING OFF A CORE SAMPLE 805
A. Tools and consumable materials 805
B. Procedure 805
3. PRINCIPLE OF CORROSION REPAIR ON THE
SPAR, FROM N1 RIB TO N4 RIB 806
A. Tools and consumable materials 806
B. Repair of the spar 807
C. Installation of the stiffener - Repairs A and B 807
D. Installation of the stiffener - Repairs C and D 808
WINGS 57-20-00 (EA) 1 1 - 9999
DESCRIPTION AND OPERATION 1
1. GENERAL 1
2. LOCATION 1
3. DESCRIPTION 1
A. Wing fittings 1
B. Landing gear attachment fittings 1
WINGS 57-20-00 (BA) 401 1 - 9999
REMOVAL / INSTALLATION 401
1. REMOVAL OF THE ARMS FITTED WITH FLAPS 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF THE ARMS FITTED WITH FLAPS 401
A. Tools and consumable materials 401
B. Procedure 402
3. REMOVAL OF THE ARMS FITTED WITH AILERONS 402
A. Tools and consumable materials 402
B. Procedure 402
4. INSTALLATION OF THE ARMS FITTED WITH AILERONS 403
A. Tools and consumable materials 403
B. Procedure 403
WING FITTINGS 57-20-03 (DA) 401 1 - 9999
REMOVAL / INSTALLATION 401
1. REMOVAL OF THE WING FRONT ATTACHMENT 401
A. Tools and consumable materials 401
B. Procedure 401
ADAA
Validity : S / N 1 - 9999 Page 2
57-TC (EA) SEP 04
SOCATA
TB 20 MODEL
SUBJECT CHAPTER
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