Catalog item
Request a quoteFLAP,WING LANDING
1560FSC
01NCB code
728-9692Item number
NIIN 01-728-9692
- Unit price
- $20,897.52
- Unit of issue
- EA
- Source of supply
- H9D
- DEMIL code
- Q
Identification
- Item name code
- 60494
- PINC
- 0060494
- Criticality code
- X
- II
- 0
- DEMIL code
- Q
- DEMIL integrity code
- 3
- NIIN assigned
- 24-APR-25
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- P
- ESD/EMI code
- A
- Schedule B export code
- 8803909060
Management
| Effective date | Major organizational entity | Acquisition advice code | Source of supply | Unit of issue | Unit of measure quantity | Unit price | Quantity per unit pack | Controlled inventory item code | Shelf-life code | Recoverability code | Management control | Net price | USC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 01-APR-2025 | DA | J | H9D | EA | 0.0000 | $20,897.52 | 1 | U | 0 | L | W3100X- | $0.00 | A |
| 01-APR-2025 | DF | J | H9D | EA | 0.0000 | $20,897.52 | 1 | U | 0 | T | --C---N | $0.00 | F |
| 01-APR-2025 | DJ | J | H9D | EA | 0.0000 | $20,897.52 | 1 | U | 0 | L | F31ZBX9 | $0.00 | L |
| 01-APR-2025 | DM | J | H9D | EA | 0.0000 | $20,897.52 | 1 | U | 0 | L | 2-55--- | $0.00 | M |
| 01-APR-2025 | DN | J | H9D | EA | 0.0000 | $20,897.52 | 1 | U | 0 | H | 6S--XE- | $0.00 | N |
Part numbers
- Part number
- 20397-1-AOW
- CAGE
- 1YF28AIR TRACTOR, INC.
- CAGE status
- A
- RNCC
- 3
- RNVC
- 2
- Document availability code
- 5
- RNAAC
- ZZ
Characteristics
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP ASSEMBLY |
|---|---|
| SPECIAL FEATURES | WING MOUNTED FLAP INTENDED TO AID AIRCRAFT LANDINGS; THE FLAPS ARE CATEGORIZED AS "SECONDARY FLIGHT CONTROL STRUCTURES". A FLAP IS A HIGH-LIFT DEVICE USED TO REDUCE THE STALLING SPEED OF AN AIRCRAFT WING AT A GIVEN WEIGHT. THE WING FLAPS INSTALLED ON THE OA-1K ARE MOUNTED ON THE WING TRAILING EDGES, AND ARE PARTIAL-SPAN FLAPS; SPANWISE FROM NEAR THE WING ROOT TO THE INBOARD END OF THE AILERONS. WHEN EXTENDED, THE FLAPS ARE DESIGNED SO THAT THEY ALTER THE SPANWISE LIFT DISTRIBUTION ON THE WING BY CAUSING THE INBOARD HALF OF THE WING TO SUPPLY AN INCREASED PROPORTION OF THE LIFT, AND THE OUTBOARD HALF TO SUPPLY A REDUCED PROPORTION OF THE LIFT. THE FLAPS ARE USED TO REDUCE THE TAKE-OFF DISTANCE AND THE LANDING DISTANCE. FLAPS ALSO CAUSE AN INCREASE IN AERODYNAMIC DRAG, SO THEY ARE RETRACTED WHEN NOT NEEDED. |
MOE rules
| MOE rule | MOE CD | AMC | AMSC | NIMSC | Date assigned | IMC | PICA | PICA LOA | SICA | SICA LOA | Auth collab | DSOR |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| A102 | DA | 0 | 0 | 0 | 01-APR-25 | E | XJ | 22 | AQ | 8D | TO TU AQ SO | CN |
| F8SQ | DF | 0 | 0 | 0 | 01-APR-25 | E | XJ | 22 | SQ | 8D | SO SQ TU | CN |
| MS22 | DM | 0 | 0 | 0 | 01-APR-25 | E | XJ | 22 | PQ | 8D | SO PQ PA | CN |
| NJQ4 | DN | 0 | 0 | 0 | 01-APR-25 | E | XJ | 22 | JQ | 8D | SO JQ GH GG | CN |
| SC01 | DJ | 0 | 0 | P | 01-APR-25 | E | XJ | 22 | SO | CN |
Service data
Army
- Matcat 1
- W
- Matcat 2
- 3
- Matcat 3
- 1
- Matcat 4 5
- 00
- ARC
- X
Navy
- COG
- 6S
- IRRC
- XE
Air Force
- Budget
- C
- PVC
- N
- ERRC
- T
Marine Corps
- SAC
- 2
- MEC
- 55
SOCOM
- ICP
- F
- A L
- 3
- REP
- 1
- W ESDC
- ZB
- AR
- X
- COS
- 9
Freight
- ACTY CD
- XJ
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 24-APR-2025
- NIIN status code
- 0
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