Automatic Pilot Mechanisms and Airborne Gyro Components: SM55A1, SM-D-493408, ST4935038HE0003
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
SM55A1 | 6615-01-045-9770 | Indrive Module | III End Item Identification: Computer, 18749-1A | Honeywell Intl Inc. (55972) | |
SM-A-702316 SMA702316 | 6615-00-192-9617 | Gyroscope, Integrating | Overall Length: 3.250 inches nominal Overall Width: 1.590 inches nominal Overall Height: 13.590 inches nominal | US Army Communications (80063) | |
SM-C-498784 SMC498784 | 6615-00-400-2704 | Amplifier-Integrator | III End Item Identification: 6615-400-2705 General Characteristics Item Description: 0.370 in. dia, 0.700IN. lg | US Army Communications (80063) | |
SMD209322-1 SMD2093221 | 6615-00-649-8879 | Amplifier-Computer | III Fsc Application Data: Miscellaneous fire control equipment Overall Length: 2.188 inches nominal Overall Width: 3.625 inches nominal | US Army Communications (80063) | |
SM-D-493408 SMD493408 | 6615-01-368-7151 | Gyroscope, Displacement | III Fsc Application Data: GYR0SCOPE, displacem | US Army Communications (80063) | |
SM-D-498762 SMD498762 | 6615-00-167-9757 | Gyroscope, Displacement | Special Features: Self contained amplifier for continually slaving gyroscope to magnetic reference Overall Length: 7.562 inches nominal Overall Width: 5.812 inches nominal | US Army Communications (80063) | |
SM-D-703336 SMD703336 | 6615-01-151-4241 | Gyroscope, Rate | Dept of the Army (54490) US Army Communications (80063) | ||
SONO SITE M-TURBO SONOSITEMTURBO | 6615-01-577-4940 | Transducer, Ultrasound | Special Features: 10.4 inch diagonal lcd display; all-digital broadband and multifrequency; 128 channels; up to 165 db dynamic range; linear, curved and phased arrays; operates on ac power or rechargeable lithium-ion battery | Sonosite Inc. (1NQ76) | |
SP101 | 6615-00-397-3595 | Switch Asy | Triumph Mfg Co. (78806) | ||
SP175 | 6615-00-797-3967 | Integrant, Mechanica | Northrop Grumman Systems Corporation (95542) | ||
SP176 | 6615-00-797-6222 | Synchronizer, Automa | Northrop Grumman Systems Corporation (95542) | ||
SP-711 SP711 | 6615-01-287-1254 | Controller, Flight, Automatic Pilo | III End Item Identification: Bell 412 Frequency in Hertz: 400.0 Power Source: External | Honeywell Intl (55939) | |
SR3HNNV21FG-18B SR3HNNV21FG18B | 6615-00-680-6678 | Bearing, Rotor | III End Item Identification: Part number 652-0052-901 rotor housing assembly III Reference Data and Literature: Tech order 5N18-11-4 fig 7, index 9 | Barden Corporation, The (70854) | |
SR60-1018-10 SR60101810 | 6615-01-131-9135 | Ring, Electrical Contact | Overall Length: 0.690 inches nominal Mounting Configuration: 10 polytetrafluoroethylene insulated leads; 32 awg; 10.000 in. min lg; stripped 0.250 in. Material: GOLD | Bean Smith Burnett & Patton (11112) | |
SS18A1 | 6615-00-869-7424 | Switch Assy | Honeywell Intl Inc. (55972) | ||
SS9028 | 6615-00-967-0840 | Plate | Rotair Industries Inc. (54878) Sikorsky Aircraft Corporation (78286) | ||
ST1031 | 6615-00-544-6137 | Winding, Ac Pick-off | Parker-Hannifin Corporation (93835) | ||
ST4319001HE0001 | 6615-01-152-2253 | Accelerometer, Electrical, Linear | III Fsc Application Data: GBU-15(V)1/B aircraft Mounting Configuration: Two 0.135 to 0.150 in. dia. mtg holes | Boeing Company, The (51215) | |
ST4935036HE0005 | 6615-01-130-2296 | Gyroscope, Roll Axis | III End Item Identification: GBU-15(V) 1/B, rockwell General Characteristics Item Description: O/a dim. 4.700 in. lg; 2.522 in. w; 2.845 in. h; 4 holes 0.194 in. dia, porm 0.005 in.; weight, 1.70 lbs | Boeing Company, The (51215) | |
ST4935038HE0003 | 6615-01-357-7960 | Gyroscope, Displacement | III End Item Identification: WCU-14/B assembly of the AGM-130 missile Special Features: Unit spin is in a clockwise direction about the outer gimbal and vertical axes, unit marked to fwd for directional mounting, a 15 pin connecter mates with M24308/2-2 connecter or equivalent Overall Length: 3.750 inches nominal | Boeing Company, The (51215) |