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Correction Procedures
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TB-1-1520-238-20-77 Removal and Replacement of Main Rotor Blade Tip Weight Retention Nuts on All AH-64 Helicopters Manual
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References

TB 1-1520-238-20-77
NOTE
Project code - XB8 - is required to track and establish a data base of
stock fund expenditures incurred by the field as a result of ASAM/SOF
actions.
c. Bulk and Consumable Materials. N/A.
NOMENCLATURE
PART NUMBER
NSN
Thread Anti-Seize Compound,
MIL-T-83483
8030-00-243-3285
Molybdenum Disulfide-Petrola
turn (8 oz. Tube)
Thread Anti-Seize Compound,
MIL-T-83483
8030-00-087-8630
Monybdenum Disulfide-Petrola
tum (1 lb. can)
Corrosion Preventative Com-
MIL-C-16173
8030-00-118-0666
pound, Class 1, Grade 2 (Soft
Film), 11 oz. Tube
Corrosion Preventative Com-
MIL-C-16173
8030-01 -149-1731
pound, Class 1, Grade 2 (Soft
Film), 1 qt.
Corrosion Preventative Com-
MIL-C-16173
8030-00-244-1297
pound, Class 1, Grade 2 (Soft
Film), 1 gal.
d. Disposition. Dispose of removed parts/components in accordance with normal supply procedures. A
QDR is not required.
e. Disposition of Hazardous Material. N/A.
11. Special Tools, Jigs and Fixtures Required. Wrench, Torque, 3/8 Drive, 0-300 Inch-Pounds, NSN
5120-00-776-1 841.
12. Application.
a. Category of Maintenance. AVUM. Aircraft downtime will be charged to AVUM.
b. Time Required.
(1) Total of one and one-half (1 1 /2) man-hours using one (1) person for each Main Rotor Blade.
(2) Total of six (6) hours downtime per Aircraft.
c. Estimated Cost Impact of Stock Fund Items to the Field.
NOMENCLATURE
PART NUMBER/
QUANTITY
COST EACH
TOTAL$
NATIONAL
STOCK NUMBER
Nut, Self-locking,
NAS1291C6M
2
$.88
$ 1.76
Aft Fitting
5310-00-879-0669
Nut, Self-locking,
NAS1291C5M
3
$.58
$ 1.74
Fwd Fitting
5310-00-882-6479
Screw, Close
HS4396-3T4 5305-
5
$.78
$3.90
Tolerance
01-224-6693
Screw, Close
HS4396-3T5 5305-
AR (Max. 42)
$ .99
$ .99
Tolerance
01-219-8718
Maximum total cost per Blade = $8.39
4

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