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Catalog item

BLADE,COMPRESSOR,AIRCRAFT GAS TU

2840FSC
01NCB code
455-4979Item number
NIIN 01-455-4979
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DEMIL code
Q

Identification

Item name code
50531
PINC
0050531
Criticality code
Y
II
M
DEMIL code
Q
DEMIL integrity code
3
NIIN assigned
05-MAY-98
Precious metals indicator
A
ADP equipment code
0
Hazardous material indicator
N
Schedule B export code
8411997050
Last known source of supply
FHZ

Part numbers

Part number
572901
CAGE
77445
RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY
CAGE status
A
RNCC
3
RNVC
2
Document availability code
B
RNAAC
ZZ

Characteristics

OVERALL HEIGHTINCHES MINIMUM 3.870 AND INCHES MAXIMUM 3.880
OVERALL WIDTHINCHES NOMINAL 0.839
END ITEM IDENTIFICATIONTF33-PW-102C AIRCRAFT GAS TURBINE ENGINE
DESIGN TYPEAXIAL COMPRESSOR
BLADE ATTACHMENT METHODDOVETAIL
CRITICALITY CODE JUSTIFICATIONFEAT AND ABKW AND ABMK AND CZBJ
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME BLADE,COMPRESSOR ROTOR
ENGINE SECTION LOCATIONCOMPRESSOR
STAGE NUMBER1
SPECIAL FEATURESTHIS ITEM COMES OFF A JT3D-7 COMMERCIAL ENGINE; IT REPLACES P/N 430401; THE FORM, FIT, FUNCTION IS EXACTLY THE SAME, THE ONLY DIFFERENCE IS THE ANGLE OF THE BLADE; BLADE WILL PROVIDE 1200 POUNDS MORE THRUST WHEN IN USE; ONCE REPLACED WILL MODIFY THE TF33-PW-102B TO THE 102C; JOINT STAR AIRCRAFT PROJECT
MATERIALOVERALL TITANIUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATIONOVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S4928
PROPRIETARY CHARACTERISTICSPACS
REFERENCE DATA AND LITERATURET.O. 2J-TF33-34, FIG 5, IND 8

MOE rules

MOE rule
YA01
MOE CD
YA
Date assigned
01-APR-09
PICA
YA
PICA LOA
81
Auth collab
YA

Freight

ACTY CD
TK

Related items

Standardization

Item standardization code
5
Orig stdzn dec
97
Dt stdzn dec
05-MAY-1998
NIIN status code
0

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