Navigational Instruments: HG1700AG19, HG1700AG-43, HG9740CH2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| HG1700AG19 | 6605-01-482-0896 | Inertial Navigation System | III End Item Identification: First pbl; F/A-18E elect. flt. contr; arr list code - MX11884/ASW57, 34206718-001 III Part Name Assigned By Controlling Agency: (Inavy): inertial measurement | Honeywell International Inc. (0BFA5) | |
| HG1700AG-43 HG1700AG43 | 6605-01-518-1716 | Subassembly, Inertia | Honeywell International Inc. (0BFA5) | ||
| HG1700AG73 | 6605-01-536-9218 | Inertial Navigation System | III End Item Identification: P5CTS Special Features: Mounting ring diameter 5.0 in.; +/- 15VDC, +/- 5VDC input voltages; hermetically sealed; unit weight approx. 1.6 lb.; output data rate 100HZ/600HZ;GYRO input range +/- 1000 deg/sec; gyro rate scale factor 150 ppm; accelerometer range +/- 50 g; accelerometer linearity 500 ppm; accelerometer scale 300 ppm; programmable, expandable serial I/O with RS422 interface Overall Height: 2.900 inches nominal | DRS C3 Systems Inc. (12339) Honeywell International Inc. (0BFA5) | |
| HG2001AC20 | 6605-01-521-8694 | Inertial Reference unit, Navigati | III End Item Identification: Astor airborne radar | Honeywell Intl (55939) | |
| HG2011AC03 | 6605-01-500-0499 | Computer, Aircraft Attitude | III End Item Identification: Aircraft, embraer, model ERJ135 and ERJ145 Special Features: Uses digital ring-laser gyros andquartz accelerometers to keep track ofchanges in aircraft heading and attitude III Part Name Assigned By Controlling Agency: Attitude heading reference syste m | Honeywell Intl (55939) | |
| HG2021GD02 | 6605-01-521-4472 | Inertial Navigation unit | III End Item Identification: Falcon 900 aircraft | Honeywell International Inc. (94580) | |
| HG2030AE22 | 6605-01-542-9726 | Inertial Navigation unit | III End Item Identification: Airbus A319, A320 | Honeywell International Inc. (65507) | |
| HG2100AB02 | 6605-01-500-6802 | Inertial Navigation unit | III End Item Identification: C-5 Special Features: Esd sensitive III Part Name Assigned By Controlling Agency: Inertial ref unit | Honeywell International Inc. (65507) | |
| HG2101AB02 | 6605-01-500-6802 | Inertial Navigation unit | III End Item Identification: C-5 Special Features: Esd sensitive III Part Name Assigned By Controlling Agency: Inertial ref unit | Honeywell International Inc. (65507) | |
| HG2195AB02 | 6605-01-582-4465 | Inertial Navigation unit | Special Features: Attitude 0.1 degree; heading 0.4 degree; inertial position 2 nmph; hybrid position 25M; inertial velocity 8 knots; hybrid velocity 0.25 knots; 25, 000 hours operating time; power consumption 20W; passive cooling; quartz accelerometer technology; accuracy two sigma or 95 percent; integrated gps; tray mounted Overall Width: 6.400 inches nominal Overall Length: 6.500 inches nominal | Honeywell International Inc. (97896) | |
| HG9715A1 | 6605-01-422-0715 | Dynamic Reference unit | III End Item Identification: M109A6 paladin sp howitzer | Honeywell International Inc. (0BFA5) | |
| HG9715A2 | 6605-01-422-0715 | Dynamic Reference unit | III End Item Identification: M109A6 paladin sp howitzer | Honeywell International Inc. (0BFA5) | |
| HG9715B1 | 6605-01-444-8045 | Dynamic Reference unit | III End Item Identification: N109A6 palidin sp howitzer | Honeywell International Inc. (0BFA5) | |
| HG9740AH3 | 6605-01-533-8754 | Inertial Navigation unit | III End Item Identification: 155 lightweight howitzer Special Features: Interface requirements in accordance with OBFA5-34205000-004, 3CONNECTORSTYPE D38999/24WD15PN power, D38999/24WH35PN I/O, D38999/24WB35PN 1553 | Honeywell International Inc. (0BFA5) | |
| HG9740AH6 | 6605-01-533-8754 | Inertial Navigation unit | III End Item Identification: 155 lightweight howitzer Special Features: Interface requirements in accordance with OBFA5-34205000-004, 3CONNECTORSTYPE D38999/24WD15PN power, D38999/24WH35PN I/O, D38999/24WB35PN 1553 | Honeywell International Inc. (0BFA5) | |
| HG9740AJ3 | 6605-01-522-1649 | Inertial Navigation unit | III End Item Identification: M1064 W/XM95 mortar | Honeywell International Inc. (0BFA5) | |
| HG9740BA2 | 6605-01-529-0542 | Inertial Navigation unit | III End Item Identification: M1A1 abrams fov | Honeywell International Inc. (0BFA5) | |
| HG9740BU4 | 6605-01-558-3399 | Inertial Navigation unit | III End Item Identification: Fennek armored vehicle Special Features: Talin 4000 | Honeywell International Inc. (0BFA5) | |
| HG9740CB2 | 6605-01-552-7419 | Inertial Navigation unit | III End Item Identification: AN/TPQ-37(V) III Part Name Assigned By Controlling Agency: Talin (tactical advanced land inertial navigator) | Honeywell International Inc. (0BFA5) | |
| HG9740CH2 | 6605-01-560-3408 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) |