Airframe Structural Components: M39184002-102, MA-182 TY 3, MA2106001-05
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
M39184002-102 M39184002102 | 1560-01-559-4151 | Aileron | Aircraft Mission Design Series: C-130J Side FOR Which Designed: Right side | Lockheed Martin Corporation (98897) | |
M4B | 1560-00-562-4699 | Pulley, Horizontal s | Atco Pulley Corp. (83451) General Aviation Equipment Co. Inc. (72652) | ||
M51,MODIFIED M51MODIFIED | 1560-01-305-6924 | Muffler, Aircraft | Electric Boat Corporation (96169) | ||
M5664-11 M566411 | 1560-01-282-3544 | Radome Assembly, Forward | III End Item Identification: BQM-74C drone acft General Characteristics Item Description: 0.060 in. thk; operating temperature -65 deg F to 165 deg f; weight 1.2 lbs III FSC Application Data: Nose cone assembly target drone | Northrop Grumman Guidance And (06481) | |
M61402-2 M614022 | 1560-01-053-4210 | Plate, Backup | III End Item Identification: Acft model F-16 General Characteristics Item Description: Steel 303 cres, 0.062 in.thick, 0.50 in.wide, 1.00 in.length | Transdigm Inc. (04638) | |
M61448-10 M6144810 | 1560-01-255-1386 | Former, Aircraft | III End Item Identification: F-16 Special Features: Main sleeve for push-pull control assembly | Transdigm Inc. (04638) | |
M62167-1 M621671 | 1560-01-053-2961 | Cover, Access | Material: Steel Peripheral Shape Style: Round, four ears and holes, one lobe Cross-Sectional Shape Style: Flat W/open center | Transdigm Inc. (04638) | |
M62171-1 M621711 | 1560-01-053-4212 | Guide Sleeve | III End Item Identification: Acft model F-16 | Transdigm Inc. (04638) | |
M62186-1 M621861 | 1560-01-053-4213 | Tube, Run out | III End Item Identification: Acft model F-16 General Characteristics Item Description: Steel 303 cres per QQ-S-763, 4.097 in.length, 0.39 in.dia., and 0.688 in.hex | Transdigm Inc. (04638) | |
M690-5 M6905 | 1560-01-150-6574 | Radome Assembly, Forward | General Characteristics Item Description: Weight maximum 1.2 pd; operating temperature -65 deg. F to 165 deg. F III FSC Application Data: Nose cone assembly target drone | Northrop Grumman Guidance And (06481) | |
M81714/29-2 M81714292 | 1560-01-415-5744 | Bracket, Structural Component, Air | III End Item Identification: Support of preprovisioning items which aso acts as point of entry | Military Specifications (81349) | |
M8271-7 M82717 | 1560-01-348-5401 | Stiffener, Aircraft | Northrop Grumman Guidance And (06481) | ||
M8271-8 M82718 | 1560-01-348-5402 | Stiffener, Aircraft | Northrop Grumman Guidance And (06481) | ||
M83413/8-A007BB M834138A007BB | 1560-01-477-5972 | Lead, Electrical, Air | Military Specifications (81349) | ||
M83798/2-6 M8379826 | 1560-01-528-0290 | Fitting, Structural Component, Air | III End Item Identification: UH1 aircraft III Part Name Assigned BY Controlling Agency: 45 degree swivel fitting Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
M922 | 1560-00-251-4621 | Screen Assembly, car | Metal Arts Co. Inc. (82804) | ||
M93A81 | 1560-01-316-1087 | Tube and Cone Assembly | Grimes Aerospace Company (72914) Kelly Aerospace Power Systems Inc. (0MJG0) | ||
MA1334A000 | 1560-01-033-0099 | Guard Screen | Honeywell Aerospace Yeovil (U1605) | ||
MA-182 TY 3 MA182TY3 | 1560-01-388-0218 | Covering, External Surface, Aircra | Northrop Grumman Systems Corporation (1W025) | ||
MA2106001-05 MA210600105 | 1560-01-571-5021 | Fuel Control Panel | Boeing Company, The (0PXV4) |