Navigational Instruments: 4977096-3, 4V10066-101A, 4V10067-107A
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4977096-3 49770963 | 6605-01-582-4313 | Bean Splitter Assembly | Raytheon Company (96214) | ||
| 49DM272 | 6605-00-346-1686 | Drive, Speed Transmi | Canadian Commercial Corporation (98247) MIL-Vickers Inc. (88311) Unison Industries LLC (59501,83311) | ||
| 49J100 | 6605-00-312-6398 | Commutator Assy | RAM Meter Inc. (99246) | ||
| 4D19058-107A 4D19058107A | 6605-01-077-3424 | Box Assembly, Instrument | III End Item Identification: C5A acft General Characteristics Item Description: W/relay assembly 12; capacitor 3 III Fsc Application Data: Triple inertial navigation system | Lockheed Martin Corporation (98897) | |
| 4D19058-107B 4D19058107B | 6605-01-077-3424 | Box Assembly, Instrument | III End Item Identification: C5A acft General Characteristics Item Description: W/relay assembly 12; capacitor 3 III Fsc Application Data: Triple inertial navigation system | Lockheed Martin Corporation (98897) | |
| 4E12309-101A 4E12309101A | 6605-00-084-7188 | Shim Assembly | General Characteristics Item Description: Consists of plate, 4E12309-103A and spacer, 4E12309-105A, 1EA; O/a dia 5.000 in.; cement per stp 60-505, type 5D; 2 sets of 12/0.220 to 0.226 dia holes/spaced 30 deg apart on 2 dia, 1ST dia 4.600 in., 2ND dia 4.250 in., 15 degbetween each hole of 1ST and 2ND dia | Lockheed Martin Corporation (98897) | |
| 4F19101-101B 4F19101101B | 6605-01-077-3427 | Pad Assembly | III End Item Identification: C5A acft General Characteristics Item Description: Material aluminum, QQ-A-250/12, 7075-T6; O/a lg 5.000 in. nom; O/a W 2.500 in. nom; O/a ht 1.250 in. nom; 1 hole 1.000 in. nom dia; W/insert III Fsc Application Data: Triple inerial navigational system | Lockheed Martin Corporation (98897) | |
| 4F19103-103B 4F19103103B | 6605-01-077-3430 | Filler, Mount pad | III End Item Identification: C5A acft General Characteristics Item Description: Material aluminum alloy, QQ-A-250, 7075-T6; O/a lg 4.310 in. nom; O/a W 1.190 in. nom; O/a ht 5.090 in. nom III Fsc Application Data: Triple inertial navigational system | Lockheed Martin Corporation (98897) | |
| 4F9101-103B 4F9101103B | 6605-01-077-3428 | PAD | III End Item Identification: C5A acft General Characteristics Item Description: Material aluminum alloy, QQ-A-250, 7075-T6; O/a lg 5.000 in. nom; W 2.500 in. nom; ht 0.380 in. nom; 1 hole 1.000 in. nom dia III Fsc Application Data: Triple inertial navigational system | Lockheed Martin Corporation (98897) | |
| 4K12130-101A 4K12130101A | 6605-01-078-1727 | Nossle Assembly | III End Item Identification: C5A acft General Characteristics Item Description: O/a dia 3.000 in. nom; O/a lg 16.050 in. nom; 18 plain holes equally spaced 1.570 in. nom; 5 plain holes on flanges; W/3 flanges one 1.620 in. nom lg, 0.650 in. nom W, 0.560 in. ht on one end two flanges 0.560 in. W, 0.500 in. ht other end III Fsc Application Data: Triple ins | Lockheed Martin Corporation (98897) | |
| 4K90027-111A 4K90027111A | 6605-01-077-3426 | Control unit, Navigation set | Special Features: Panel lighting power 3.5 va, instrument source power 28 vdc; width 8 inches, height 3.250 inches, depth 5.250 inches; weight 5 lbs; 3 connectors End Item Identification: C-5A aircraft III Part Name Assigned By Controlling Agency: Navigation selector panel | Lockheed Martin Corporation (98897) | |
| 4K90058-101A 4K90058101A | 6605-00-084-7211 | Indicator, Bearing-Distance-Headi | Special Features: Dimensions 7.250 in. by 3.250 in. by 3.250 in.; presentation type: synchro motor Phase: Single Color: Black background overall | Lockheed Martin Corporation (98897) | |
| 4K90075-103A 4K90075103A | 6605-01-078-1701 | Coupler, Heading | III End Item Identification: C5A acft General Characteristics Item Description: Comonentscapacitor 5, connector shell 1, transformer 1, diode 8; O/a lg 14.337 in. nom; O/a W 7.688 in. nom; O/a ht 2.375 in. nom; W/handle | Lockheed Martin Corporation (98897) | |
| 4K95000-165A 4K95000165A | 6605-00-110-9499 | Mode Selector unit | III End Item Identification: EC135J aircraft III Fsc Application Data: Inertial navigation system, aircraft III Reference Data and Literature: To 5N1-4-8-42 | Delco Electronics Corp. (99974) | |
| 4L244 | 6605-01-155-4037 | Cover, Underwater log | General Characteristics Item Description: Aluminum iaw QQ-R-601 | Dynalec Corporation (12763) The Electric Tachometer Corp. (20049) | |
| 4LCD1N | 6605-01-233-5221 | Indicator, Course | Dynalec Corporation (12763) The Electric Tachometer Corp. (20049) | ||
| 4MB219N | 6605-01-393-0486 | Control-Indicator Subassembly | End Item Identification: Indicator transmitter eor | Dynalec Corporation (12763) The Electric Tachometer Corp. (20049) | |
| 4SE01600 | 6605-01-543-3754 | Adf Test set Antenna | End Item Identification: SH-2G helicopter | Technology Program Services (04VM1) | |
| 4V10066-101A 4V10066101A | 6605-01-077-3423 | Panel Assembly, Instrument Select | III End Item Identification: C5A acft General Characteristics Item Description: W/circuit card assy 1, connector 3, switch 2 III Fsc Application Data: Triple inertial navigation system | Lockheed Martin Corporation (98897) | |
| 4V10067-107A 4V10067107A | 6605-01-077-3425 | Panel Assembly, Status | III End Item Identification: C5A acft General Characteristics Item Description: Includes circuit card assy 1, connector 1, indicator light ASSY1 III Fsc Application Data: Triple inertial navigation system | Lockheed Martin Corporation (98897) |