W DOC AIRBUS | AMM A320F

Check for the Self-Locking Feature [PW11]


TASK 70-26-00-910-803-A
Check for the Self-Locking Feature


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the Job
NOTE: Always obey the specific procedures and limits in the specific AMM maintenance tasks.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
SOCKET STANDARD
No specific
1
WRENCH - TORQUE, STANDARD
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P03-001)
lubricant, aircraft turbine engine
 C. Referenced Information
REFERENCE
DESIGNATION
3. Job Set-up
Subtask 70-26-00-869-050-A ** ON A/C NOT FOR ALL
A. Not Applicable
4. Procedure
Subtask 70-26-00-911-050-A ** ON A/C NOT FOR ALL
A. General
   (1) Self-locking fasteners are designed for a limited number of reuses to keep the quality of their self-locking function. Free-spinning fasteners have other features for locking.
F Check For Self Locking Feature ** ON A/C NOT FOR ALL
   (2) Discard the fastener if the self-locking function is not correct.
   (3) Do not pinch, squeeze or deform a fastener to repair the self-locking feature.
Subtask 70-26-00-280-050-A ** ON A/C NOT FOR ALL
B. Procedure - Feel Method
   (1) Use feel to test the self-locking function of each fastener during the final assembly by the assembly mechanic.
   (2) The assembly mechanic must get experience in the usual or new part feel for run-on torques of the applicable fasteners.
   (3) If there is too much run-on torque, or insufficient run-on torque, during the installation of a fastener, the mechanic must replace the fastener with one which is acceptable.
   (4) Discard any fastener which does not feel acceptable.
Subtask 70-26-00-280-051-A ** ON A/C NOT FOR ALL
C. Procedure - Test Method
   (1) You can use a statistically valid sampling inspection program to test some of the parts as an alternative to testing every part.
     (a) Use the limits in the table that follows for:
       1 Self-locking nuts on bolts, screws or studs
       2 Bolts or screws into self-locking helical inserts.
     (b) Lubricate the fastener with P03-001lubricant, aircraft turbine engine or the applicable antigallant.
     (c) Install the fastener on the mating fastener and fully engage the self-locking feature without any axial load (do not seat the fastener).
     (d) Use a WRENCH - TORQUE, STANDARD and the table that follows to test the "Break Away Torque" of the fastener:
       1 Install a beam or digital WRENCH - TORQUE, STANDARD and SOCKET STANDARD on the fastener.
       2 Monitor the amount of torque necessary to initially start the fastener turning.
       3 Compare the "Break Away Torque" indication with the limits in the table that follows.
       4 Discard any fastener that is not in the limits.
   (2) Use a torque wrench and the table that follows to test the "Run-On Torque" of the fastener:
     (a) Install a beam or digital WRENCH - TORQUE, STANDARD and SOCKET STANDARD on the fastener.
     (b) After the initial "Break Away Torque", monitor the amount of torque necessary to turn the fastener to the thread "Run-On Torque".
     (c) Compare the "Run-On Torque" indication with the limits in the table that follows.
     (d) Discard any fastener that is not in the limits.
Thread Size
Minimum Breakaway Torque lbf.in (m.daN)
Maximum Locking (Run- On) Torque lbf.in (m.daN)
0.112-40
0.5 lbf.in (0.006 m.daN)
3.0 lbf.in (0.034 m.daN)
0.112-48
0.5 lbf.in (0.006 m.daN)
3.0 lbf.in (0.034 m.daN)
0.138-32
1.0 lbf.in (0.011 m.daN)
6.0 lbf.in (0.068 m.daN)
0.138-40
1.0 lbf.in (0.011 m.daN)
6.0 lbf.in (0.068 m.daN)
0.164-32
1.5 lbf.in (0.017 m.daN)
9 lbf.in (0.102 m.daN)
0.164-36
1.5 lbf.in (0.017 m.daN)
9 lbf.in (0.102 m.daN)
0.190-24
2.0 lbf.in (0.023 m.daN)
13 lbf.in (0.147 m.daN)
0.190-32
2.0 lbf.in (0.023 m.daN)
13 lbf.in (0.147 m.daN)
1/4 Inch:


0.250-20
4.5 lbf.in (0.051 m.daN)
30 lbf.in (0.339 m.daN)
0.250-28
3.5 lbf.in (0.040 m.daN)
30 lbf.in (0.339 m.daN)
5/16 Inch:


0.3125-18
7.5 lbf.in (0.085 m.daN)
60 lbf.in (0.678 m.daN)
0.3125-24
6.5 lbf.in (0.073 m.daN)
60 lbf.in (0.678 m.daN)
3/8 Inch:


0.375-16
12.0 lbf.in (0.136 m.daN)
80 lbf.in (0.904 m.daN)
0.375-24
9.5 lbf.in (0.107 m.daN)
80 lbf.in (0.904 m.daN)
7/16 Inch:


0.4375-14
16.5 lbf.in (0.186 m.daN)
100 lbf.in (1.130 m.daN)
0.4375-20
14 lbf.in (0.158 m.daN)
100 lbf.in (1.130 m.daN)
1/2 Inch:


0.500-14
24 lbf.in (0.271 m.daN)
150 lbf.in (1.695 m.daN)
0.500-20
18 lbf.in (0.203 m.daN)
150 lbf.in (1.695 m.daN)
9/16 Inch:


0.5625-12
30 lbf.in (0.339 m.daN)
200 lbf.in (2.260 m.daN)
0.5625-18
24 lbf.in (0.271 m.daN)
200 lbf.in (2.260 m.daN)
5/8 Inch:


0.625-11
40 lbf.in (0.452 m.daN)
300 lbf.in (3.390 m.daN)
0.625-18
32 lbf.in (0.362 m.daN)
300 lbf.in (3.390 m.daN)
3/4 Inch:


0.750-10
60 lbf.in (0.678 m.daN)
400 lbf.in (4.520 m.daN)
0.750-16
50 lbf.in (0.565 m.daN)
400 lbf.in (4.520 m.daN)
7/8 Inch:


0.875-9
82 lbf.in (0.927 m.daN)
600 lbf.in (6.780 m.daN)
0.875-14
70 lbf.in (0.791 m.daN)
600 lbf.in (6.780 m.daN)
1 Inch:


1.000-8
110 lbf.in (1.243 m.daN)
800 lbf.in (9.040 m.daN)
1.000-14
92 lbf.in (1.040 m.daN)
800 lbf.in (9.040 m.daN)
[Rev.10 from 2021] 2026.04.02 06:31:42 UTC