LogiQuest® Lite - NSN 1560-01-728-9692 FLAP,WING LANDING

National Stock Number(NSN): 1560-01-728-9692 (1560017289692, 017289692)

( Historical )

NIIN:

01-728-9692

Item Name:

FLAP,WING LANDING

INC:

60494

FSC:

1560

Assignment Date:

Apr-24-2025

CRIT:

X

IIG:

60494

ISC:

5

Date Standardized:

Apr-24-2025

HMIC:

P

DODIC:

NSC:

0

Cancellation Date:

PMIC:

A

FIIG:

A11500

ESD:

A

Schedule B:

8803.90.9060

DEMIL:

Q

DEMIL INT:

3

TIIC:

4

Originator:

97

ADPEC:

0

RPDMRC:

3

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The full version of LogiQuest has information related to NSN 1560-01-728-9692 in each of the following databases.

• CAGE - Commercial And Government Entity

• H6 - Federal Item Name Directory

• FSC - Federal Supply Class

• Schedule B - Export Commodity Classifications

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Part Information

Part Number	CAGE	Company	Status	RN CC	RN VC	DAC	RN AAC	RN FC	RN SC	RN JC	SADC	HCC	MSDS
20397-1-AOW	1YF28	AIR TRACTOR, INC.	C	3	2	5	ZZ

Management Information

MOEC	SOS	A A C	R C	S L C	CIIC	U P Q	U S C	Unit Price	UI	UICF	MCD	Action Date	C/H
DA	H9D	J	L	0	U	1	A	$20,897.52	EA		W3100X-	Apr-01-2025	C
DF	H9D	J	T	0	U	1	F	$20,897.52	EA		--C---N	Apr-01-2025	C
DJ	H9D	J	L	0	U	1	L	$20,897.52	EA		F31ZBX9	Apr-01-2025	C
DM	H9D	J	L	0	U	1	M	$20,897.52	EA		2-55---	Apr-01-2025	C
DN	H9D	J	H	0	U	1	N	$20,897.52	EA		6S--XE-	Apr-01-2025	C

Technical Characteristics Information

MRC	Requirement Statement	Reply Statement
CXCY	PART NAME ASSIGNED BY CONTROLLING AGENCY	FLAP ASSEMBLY
FEAT	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 Information

MOE Rule	Former MOER	Effective	AMC	AMSC	IMC	IMCA	Collaborators	Receivers
A102		Apr-01-2025	0	0	E		TO\|TU\|AQ\|SO	AQ\|SO
NJQ4		Apr-01-2025	0	0	E		JQ\|SO\|GG\|GH	JQ\|SO\|GG\|GH
MS22		Apr-01-2025	0	0	E		PA\|PQ\|SO	PA\|PQ\|SO
F8SQ		Apr-01-2025	0	0	E		SQ\|SO\|TU	SQ\|SO\|TU
SC01		Apr-01-2025	0	0	E		SO	SO

LogiQuest® Lite A Commercial Alternative to WebFLIS

LogiQuest^® Lite A Commercial Alternative to WebFLIS