NSN 2840-01-448-7038 · NIIN 014487038 · FSC 2840
NO DASHES 2840014487038
In Stock
LINER,COMBUSTION CHAMBER,AIRCRAF
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
9 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 6.157 AND INCHES MAXIMUM 6.269 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 1.456 |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER DUCT |
| CZBJ | ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 100, IND 20; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABILITY LINER SEGMNET THRU NORMAL ATTRITION OF PARTS |
| MATT | MATERIAL | OVERALL NICKEL ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MFR REF SINGLE MATERIAL RESPONSE WA1475 |