Airframe Structural Components: RAC12321-1, RAC12356-1, RC1-116

Get a Quote

 
MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
RAC12321-1
RAC123211
1560-00-509-5057Plate, Hanger Lug, FuIII End Item Identification: Aircraft model F84
Northrop Grumman Systems Corporation (26512)

Quote

RAC12343-1
RAC123431
1560-00-509-5060Tube Assembly, VacuuIII End Item Identification: F-84 acft
General Characteristics Item Description: C/O tube and valve assy
Northrop Grumman Systems Corporation (26512)

Quote

RAC12354-1
RAC123541
1560-00-509-5062Ring, Seal JointGeneral Characteristics Item Description: Aluminum alloy, 26.752 in. dia
Northrop Grumman Systems Corporation (26512)

Quote

RAC12355-2
RAC123552
1560-00-546-1800Ring, Seal JointIII End Item Identification: Aircraft model F84
General Characteristics Item Description: Aluminum alloy, QQ-A-200/8, 26.909 in. min, 26.932 in. max od, 0.463 in. H
Northrop Grumman Systems Corporation (26512)

Quote

RAC12356-1
RAC123561
1560-00-509-5065Clamp Assembly, SealIII End Item Identification: Acft model F84
Northrop Grumman Systems Corporation (26512)

Quote

RAC12360-1
RAC123601
1560-00-509-5066Packing Assembly, sGeneral Characteristics Item Description: Rubber, synthetic, MIL-R-6855
Northrop Grumman Systems Corporation (26512)

Quote

RAC12361-1
RAC123611
1560-00-509-5067Bracket, Structural Component, AirAircraft Mission Design Series: F-84
Northrop Grumman Systems Corporation (26512)

Quote

RAC12362-1
RAC123621
1560-00-509-5068Pad, Fuel TankIII End Item Identification: Aircraft model F84
Northrop Grumman Systems Corporation (26512)

Quote

RAC12365-1
RAC123651
1560-00-345-4848Tank, Fuel, AircraftIII End Item Identification: U/O F87 acft
Capacity: 230.0 gallon, us measure
Northrop Grumman Systems Corporation (26512)

Quote

RAC12368-1
RAC123681
1560-00-546-1802Skin Assembly, Tail SectionGeneral Characteristics Item Description: Aluminum alloy, QQ-A-327
Northrop Grumman Systems Corporation (26512)

Quote

RAVE-JCC-3
RAVEJCC3
1560-01-552-1669Rave Server, Sm, AircRave Computer Association Inc. (0KYY5)

Quote

RAWMA11-223-037
RAWMA11223037
1560-01-378-8917EdgingSikorsky Aircraft Corporation (78286)

Quote

RAWMA16-466-015
RAWMA16466015
1560-01-340-4347Clean MeshFabrication Method: Woven
Diameter: 0.0021 inches nominal
Weave Type: Twilled plain
Sikorsky Aircraft Corporation (78286)

Quote

RAWMA16-466-C15
RAWMA16466C15
1560-01-340-4347Clean MeshFabrication Method: Woven
Diameter: 0.0021 inches nominal
Weave Type: Twilled plain
Sikorsky Aircraft Corporation (78286)

Quote

RAWMA16-981-001
RAWMA16981001
1560-01-340-4347Clean MeshFabrication Method: Woven
Diameter: 0.0021 inches nominal
Weave Type: Twilled plain
BE Aerospace Inc. (16827)
Sikorsky Aircraft Corporation (78286)

Quote

RB12404-1
RB124041
1560-00-919-7290Screen, Pump InletIII End Item Identification: Aircraft model UH1F
General Characteristics Item Description: Brass, 2.875 in. O/a lg, 2.234 in. min, 2.325 in. max O/a W, 0.250 in. in. min, 0.312 in. max O/a H, 2 mtg holes 0.187 in. dia
Crane Co. (51663)

Quote

RB1255 1560-01-560-6895Heat Shield, ExhaustIII Part Name Assigned BY Controlling Agency: Exhaust deflector
End Item Identification: 4930-01-114-9930, helicopter expedient refueling system
W.S. Darley & Co. (00299)

Quote

RB12582 1560-00-919-0164Plate, AircraftCrane Co. (51663)

Quote

RC1108-4
RC11084
1560-01-143-8020Receiver AssemblyIII End Item Identification: Acft model KC-135
General Characteristics Item Description: Corrosion resistant steel 17-4PH, heat treated to condition H900 per MIL-H-6875 and al alloy 6O61-T6, heat treated per MIL-H-6088; 2.470 in. lg, 1.250 in. W, 1.450 in. h; used on fan cowl-hold open mechanism
Marathonnorco Aerospace Inc. (08844)

Quote

RC1-116
RC1116
1560-00-027-1049Support, Structural Component, AirSpecial Features: Aluminum alloy, anodized
Marathonnorco Aerospace Inc. (08844)

Quote

  • We solve sourcing challenges for RAC12321-1, RAC12354-1, RAC12356-1, RAC12362-1, RAC12368-1, RAWMA11-223-037, RAWMA16-466-C15, RAWMA16-981-001, RB12404-1, RC1-116 - NSN parts, hard to find, long lead time and obsolete components.