APR 11

SOCATA MAINTENANCE MANUAL

TBM 700 MODEL

Validité : N / S 93 Page 1 00-LETR (BA) TR040.27

AAAA

LIST OF EFFECTIVE TEMPORARY REVISIONS

Revision

No.

Date of

revision

Date of

insertion by

user

Signature Revision

No.

Date of

revision

Date of

insertion by

user

Signature

TR001.05 Dec. 1992 Incorporated at a previous

revision

TR002.24 Dec. 1992 Incorporated at a previous

revision

TR002A.05 Dec. 94 Incorporated at a previous

revision

TR003.24 Feb. 95 Incorporated at a previous

revision

TR004.27 May 95 Incorporated at a previous

revision

TR005.05 APR 99 Incorporated at R23

TR006.52 JUL 99 Incorporated at R22

TR007.27 AUG 99 Incorporated at R21

TR008.53 N/A

TR009.52 DEC 99 Incorporated at R22

TR010.04 DEC 99 Incorporated at R24

TR011.05 DEC 99 Incorporated at R23

TR012.05 MAR 00 Incorporated at R23

TR013.52 MAR 00 Incorporated at R23

TR014.53 N/A

TR015.71 JUN 00 Incorporated at R22

TR016.04 NOV 01 Incorporated at R24

TR017.27 NOV 03 Incorporated at R28

TR018.20 JUL 04 Incorporated at R30

TR019.22 JUL 04 Incorporated at R33

TR020.27 JUL 04 Incorporated at R28

TR021.05 JUN 04 Incorporated at TR024.05

TR022.53 JUL 04 Incorporated at R33

TR023.04 N/A

TR024.05 NOV 05 Incorporated at R32

TR025.05 SEP 06 Incorporated at R34

TR026.00 DEC 06 Incorporated at R34

TR027.34 DEC 06 Incorporated at R37

TR028.73 FEB 07

TR029.77 FEB 07 Incorporated at R37

TR030.79 FEB 07

TR031.20 FEB 07 Incorporated at R34

TR032.05 APR 07 Incorporated at R34

TR033.32 APR 07 Incorporated at R34

TR034.71 APR 08 Incorporated at R37

TR035.77 APR 08 Incorporated at R37

TR036.05 MAY 08 Incorporated at R36

TR037.77 OCT 08 Incorporated at R37

TR038.25 FEB 10 Incorporated at R39

TR039.53 APR 10

TR040.27 APR 11

Page 1/2
SOCATA MAINTENANCE MANUAL

TBM 700 MODEL

TR040.27

APR 11

TEMPORARY REVISION No. TR040.27

CAUTION : KEEP THIS PAGE AND POSITION IT BEFORE THE LIST OF EFFECTIVE PAGES OF

CHAPTER 27.

FILING INSTRUCTIONS : Insert this Temporary Revision dated APR 11.

Retain this TR until it is CANCELLED by a normal revision or until replaced by

a new TR.

SUBJECT : Aileron control cables.

REASON : To define the correct installation direction of aileron cables.

CONCERNED PAGES :

TOPICS PAGES DATE NOTE

27--10--02 (BA) 410 APR 11

27--10--03 (CA) 403, 405 APR 11
APR 11

SOCATA MAINTENANCE MANUAL

TBM 700 MODEL

Validity : All Page 410 27-10-02 (BA) TR040.27

ABAB

Spoiler mechanism cables -- Removal / Installation

Figure 402

38 -- Immobilization tool

41 -- Pulley

42 -- Cable guard

43 -- Washer

44 -- Bolt

45 -- Bolt

46 -- Washer

47 -- Cable end

48 -- Safetying pin

49 -- Turnbuckle

50 -- Cable end
APR 11

SOCATA MAINTENANCE MANUAL

TBM 700 MODEL

Validity : All Page 403 27-10-03 (CA) TR040.27

ABAB

-- Mastinox (TB 05--002A)

-- Stainless steel lockwire, dia. 0.032 in. (0.8 mm)

B. Installation of aileron cable assembly

1) Inspect the interfaces for cleanliness and condition.

2) Inspect the teflon cable--guide, cables and the pulleys for condition -- refer to 20--10--04 and 20--10--05.

3) If pulley assembly (7) has been removed, proceed as follows

a) Position rod (43) onto pulley assembly (7) equipped with lever (62).

b) Install bolt (41) lubricated with grease (TB 04--004A), washer (61) and nut (60).

c) Safety with a new cotter pin (59).

d) Position the pulley assembly on the spar.

CAUTION : DO NOT INVERT THE TWO CABLES, THE LONGEST ONE IS TO BE INSTALLED ON

WING TIP SIDE, WITH L.H. THREADED END IN UPPER SECTION.

4) Coat peg (6) of aileron cable with Mastinox (TB 05--002A).

5) Insert peg (6) into pulley (7), with L.H. threaded cable end positioned in upper section.

NOTE : L.H. threaded end is marked by a notch on the hexagonal section.

6) Install cable guard (1) with bolts (3) and (4) and washers (2) and (5).

7) Insert peg (33) coated with Mastinox (TB 05--002A) into pulley (34) with L.H. threaded cable end

positioned in lower section.

NOTE : L.H. threaded end is marked by a notch on the hexagonal section.

8) Install spoiler mechanism assembly (21) with bolts (28) and (23) and washers (29) and (22).

9) Engage rod (31) into fitting (27).

10) Install bolt (30) lubricated with grease (TB 04--004A), washer (26) and nut (25).

11) Safety with a new cotter pin (24).

12) Position the cables on the two pulleys (15) and install cable guards (12) with bolts (14) and washers (13).

13) Lubricate cable ends (8) and (11) with grease (TB 04--004A).

14) Link aileron cables with the two turnbuckles (10).

NOTE : Turnbuckles (10) and cable ends (8) and (11) are L.H. threaded and R.H. threaded ; the

L.H. threaded end is marked by a notch on the hexagonal section of cable ends (8) and

(11), and by a groove on one end of turnbuckles (10).

15) Immobilize cable ends (8) and (11) while tightening turnbuckles (10) with immobilization tool (32).

16) Screw each turnbuckle by the same number of turns, including the spoiler cables.

CAUTION : IF THE STORAGE INSTRUCTIONS DEFINED BY THE MANUFACTURER IN SERVICE

LETTER LS 70--010--27 ”FLIGHT CONTROL CABLES” ARE NOT COMPLIED WITH,

CHECK THE TENSION OF THE CABLES AFTER THE FIRST FLIGHT FOLLOWING

CABLE REPLACEMENT.

17) Check the tension of the cables -- refer to 27--10--00.
APR 11

SOCATA MAINTENANCE MANUAL

TBM 700 MODEL

Validity : All Page 405 27-10-03 (CA) TR040.27

ABAB

Aileron control -- Removal / Installation

Figure 401

1 -- Cable guard

2 -- Washer

3 -- Bolt

4 -- Bolt

5 -- Washer

6 -- Peg

7 -- Pulley

8 -- Cable end

9 -- Safetying pin

10 -- Turnbuckle

11 -- Cable end

12 -- Cable guard

13 -- Washer

14 -- Bolt

15 -- Pulley