TB1-2840-248-20-21
7.
Parts to be Inspected. The engine records are to be inspected for the following components:
NOMENCLATURE
PART NUMBER
NATIONAL STOCK NUMBER
Stage 1 Forward Cooling Plate
6044T88P02
2840-01-140-6735
Stage 1 Forward Cooling Plate
6044T88P03
2840-01-236-4599
Stage 1 Aft Cooling Plate
6044T92P02
2840-01-140-6736
6044T92P03
2840-01-187-1558
Stage 2 Forward Cooling Plate
6055T25P01
2840-01-180-7667
6044T93P02
2840-01-140-6733
Stage 2 Aft Cooling Plate
6055T24P01
2840-01-180-7668
2840-01-299-2225
6044T94P02
2840-01-140-6734
8.
Inspection Procedures.
a. Prior to next flight, review DA Form 2408-16-1 (GG Rotor) to obtain the following cumulative component counts
(1) Engine serial number
(2) Component serial number
(3) Component operating hours
(4) LCF1 counts
(5) Unit Identification Code (UIC)
(6) Unit
(7) Station
(8) Point of contact/phone number/e-mail
9. Correction Procedures.
a. Remove all gas generator assemblies having stage 2 aft cooling plates (P/N 6055T24P01, NSN 2840-01-180-
7668) with more than 4,000 operating hours. Forward a Category I Deficiency Report (SF Form 368) per DA PAM 738-
c. Change the life limit of stage 2 aft cooling plates, P/N 6055T24P01, to 4,000 hours on DA Form 2408-16-1 in
accordance with TB 1-2840-248-20-21.
10. Supply/Parts and Disposition.
a. Parts Required. Turbine, Rotor, Turbine (also known as Gas Generator Rotor Assembly) Turbine, Rotor, Turbine,
P/N 6055T26G08, NSN 2840-01-298-0693; or Turbine, Rotor, Turbine, P/N 6055T26G09, NSN 2840-01-298-0693.
b. Requisitioning Instructions. Requisition replacement parts using normal supply procedures. All requisitions shall
use project code (CC 57-59) "XEG", "X-RAY-ECHO-GOLF".
NOTE
Project code "XEG", "X-RAY-ECHO-GOLF" is required to track and establish a data base of stock
fund expenditures incurred by the field as a result of Safety of Flight (SOF) actions.
c. Bulk and Consumable Materials.
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