Navigational Instruments: 34084500-502, 34084600-003, 34200750-3042
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
34084500-502 34084500502 | 6605-01-339-9252 | Inertial Reference unit, Navigati | Honeywell International Inc. (0BFA5) | ||
34084500-503 34084500503 | 6605-01-339-9252 | Inertial Reference unit, Navigati | Honeywell International Inc. (0BFA5) | ||
34084574 | 6605-01-339-9252 | Inertial Reference unit, Navigati | Honeywell International Inc. (0BFA5) | ||
34084600-003 34084600003 | 6605-01-340-4784 | Power Adapter, Rotor Support | III End Item Identification: Inertial navigational system, F-117-A aircraft General Characteristics Item Description: Basic unit 34084631-003 rotor support power assembly; 28 volts dc; overall dim: 4.82 in. W by 5.91 in. ht III Functional Description: Provides emergency despin voltage for spindown of ins gyros upon loss of aircraft power | Honeywell International Inc. (0BFA5) | |
34200600-2CS5-SM-US 342006002CS5SMUS | 6605-01-532-9821 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
34200600-3057 342006003057 | 6605-01-415-9079 | Inertial Navigation System | III End Item Identification: Preprovisioning support navicp is poe | Honeywell International Inc. (0BFA5) | |
34200600-3057SM 342006003057SM | 6605-01-415-9079 | Inertial Navigation System | III End Item Identification: Preprovisioning support navicp is poe | Honeywell International Inc. (0BFA5) | |
34200600-30H4 3420060030H4 | 6605-01-426-8522 | Inertial Navigation unit | III End Item Identification: C/KC-135 aircraft Special Features: 2/3A C-cell gps battery installed;front connector panel:built in test; electrostatic discharge sensitive Overall Width: 7.000 inches nominal | Honeywell International Inc. (0BFA5) | |
34200600-30H4-SM 3420060030H4SM | 6605-01-426-8522 | Inertial Navigation unit | III End Item Identification: C/KC-135 aircraft Special Features: 2/3A C-cell gps battery installed;front connector panel:built in test; electrostatic discharge sensitive Overall Width: 7.000 inches nominal | Honeywell International Inc. (0BFA5) | |
34200600-30S5-SM-US 3420060030S5SMUS | 6605-01-532-9825 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
34200600-H035-GR 34200600H035GR | 6605-01-553-1902 | Inertial Navigation unit | III End Item Identification: C27-J aircraft III Part Name Assigned By Controlling Agency: Egi computer | Lockheed Martin Corporation (98897) | |
34200601 | 6605-01-445-0200 | Inertial Navigation System | Honeywell International Inc. (0BFA5) | ||
34200601-3067 342006013067 | 6605-01-445-0200 | Inertial Navigation System | Honeywell International Inc. (0BFA5) | ||
34200602-3057 342006023057 | 6605-01-522-2012 | Inertial Navigation unit | III End Item Identification: UH-1 4 blade rotor head upgrade Overall Width: 7.030 inches nominal Overall Length: 11.130 inches nominal | Honeywell International Inc. (0BFA5) | |
34200602-3SRB 342006023SRB | 6605-01-503-7056 | Inertial Navigation unit | III End Item Identification: F-5 acft avionics systems upgrade; T38 program | Honeywell International Inc. (0BFA5) Rivets Unlimited (0BSA5) | |
34200650-3004 342006503004 | 6605-01-421-0076 | Inertial Navigation unit | III End Item Identification: AH-64, OH-58D Special Features: Weight 18 lbs nom.;this item is the core egi unit which has the potential to be multiapplication based on theinternal cca configuration provided Overall Width: 7.020 inches maximum | Honeywell International Inc. (0BFA5) | |
34200650-300J 34200650300J | 6605-01-421-0076 | Inertial Navigation unit | III End Item Identification: AH-64, OH-58D Special Features: Weight 18 lbs nom.;this item is the core egi unit which has the potential to be multiapplication based on theinternal cca configuration provided Overall Width: 7.020 inches maximum | Honeywell International Inc. (0BFA5) | |
34200650-30P7 3420065030P7 | 6605-01-457-2789 | Inertial Navigation System | III End Item Identification: Preprovisioning support navicp is poe | Honeywell International Inc. (0BFA5) | |
34200650-30Q7 3420065030Q7 | 6605-01-487-8451 | Inertial Navigation System | III End Item Identification: 34200650-30Q7, egi ins system Special Features: Angular rate, roll, pitch, YAW-420 deg/sec; passive cooling per 40 watts ; neg 54 to pos 71 deg C Current Type: DC | Honeywell International Inc. (0BFA5) | |
34200750-3042 342007503042 | 6605-01-449-4965 | Inertial Navigation unit | III End Item Identification: F-15S Special Features: Electrostatic discharge sensitive; includes embedded global positioning system Overall Width: 10.950 inches minimum and 11.050 inches maximum | Honeywell International Inc. (0BFA5) |