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Aviation History
1959
1959 - 1066.PDF
Flight, 17 April 1959 185-4 HF COMM SYSTEM 618S-1 HF COMM SYSTEM 51R-4 8B0E-1 51Z-2 51V 3 FD-104 INTEGRATED FLIGHT SYSTEM FD-105 INTEGRATED FLIGHT SYSTEM FD-107 INTEGRATED FLIGHT SYSTEM Ever since the early days of commercial aviation the prestige of Collins communication and navigation equipment has thrived, nourished by an energetic research and development program dedicated to the advancement of aviation electronics. The result is evident on these pages-the most complete line of high quality avionics equipment bearing one trademark. And even this group portrait is incomplete, lacking the scores of servos, remote control units, shock- ,^_*__ • ^ mounts and test equipment associated with the major systems pictured. The Collins name ^^•^^^^^•^^^ is as important in military as it is in commercial aviation. In addition to the Collins com- munication and integrated electronics systems serving jet fighter and bomber squadrons throughout the world, Collins airline type equipment is widely used aboard military transports. DALLAS • BURBAIMKCOLLINS RADIO COMPANY • CEDAR RAPIDS • ror aircraft up to 200 nautical miles ssociated ground beacon. Provides 1 .. peak pulse power. Wt. 35 lbs. BEACON RECEIVER — One or ,.omati< *>'«. flight direc- NTATION OMNI«A«INO SELECTOR _ En obles selection of deitred track and provides to-from information. Wt. 2 lbs. 327A-2 MARKER LIGHT INDICATOR — Contains three press-to-test lights and Hi-Low sensi- tivity switch. Wt. 0 63 fbs. ID-48 DEVIATION INDICATOR — VOR/ILS dis- placement data. Flag service. Wt. 1.9 lbs. 331H-1 COURSE SELECTOR INDICATOR — Pro- vides cross-pointer, to-from, flag and digital course selector service. Wt. 4.0 lbs, 337A-2 OMNf-BEARfNG INDICATOR — Presents true bearing fa VOR station and drives RMI pointers. Wt. 2 5 lbs. 332C-1 RADIO MAGNETIC INDICATOR — Dual input for VOR or ADF. Provides heading and omni or ADF bearing. Wt. 2 lbs. 331E-2 ADF INDICATOR — Similar to 332C-1 indication except no magnetic heading indica- tion. Variation set knob sets card. Wt. 1.5 lbs. ANTENNAS 37J-3 VOR NAV ANTENNA — Receives VOR and IOC signals in the 106-122 me range. Drag of 2.6 lbs. at 250 mph. Wt. 4 lbs. 37R-2 VHF COMM ANTENNA — Receiving and transmitting antenna with maximum input capability of 125 watts. Frequency range; 116-152 me. Drag of 0.5 Ibt. at 250 mph, 1.3 lbs. at 400 mph. Wt. 2 lbs. 37R-1 VHF COMM ANTENNA — Receiving and transmitting antenna in 118-136 me frequency range. Drag is 1 Ib. at 250 mph. Wt. 3.5 lbs. 37P-4, -5 GLIDESLQPE ANTENNA — Accepts glides lope signals in the 329-336 me range. Negligible drag. 37P-5 hes two inputs for dual glideslope receiver installation. Wt, 0.7 lbs. 137X-1 VHF COMM/NAV ANTENNA — Com- bined unit for communication from 118 to 136 me and navigation from 108.0 to 127.0 me. Drag of 15.3 lbs. at 600 mph. Wt. 4.7 lbs. 37X-2 MARKER BEACON ANTENNA — Receives 75 me marker beacon signal. Drag of 3.5 ox. at 400 mph. Wt. T lbs. FLIGHT CONTROL AP-101E AUTOMATIC PILOT — Provides auto- matic pilot services in the heavy twin to four engine airliner range. Flies thfj aircraft in re- sponse to heading signols during cross country and loeaftzer-glideslope signals (including crosswlnd correction) during approach. AP-102 AUTOMATIC PILOT — Lightweight auto- matic pilot with services and installation rang* similar to the AP-101E. AP-103 AUTOMATIC PILOT — Collins newest version automatically control* all high per* formance commercial and executive aircraft including airline and executive jets. Offers continuous radio course cr&sswind correction, smooth. flight over VOR stations, included flight director steering computer circuitry. FD-104 INTEGRATED FLIGHT SYSTEM — Provides instrumentation for attitude control, flight along selected headings or VOR radicti, IL5 approaches and flight director steering. Com- plete plan view and forward view picture of flight is presented on two instruments. FD-105 INTEGRATED FLIGHT SYSTEM — Ad- vanced version of IFS with two-eofor horizon background, 4" instruments, integrated light- ing and iarger warning flogs. FD-107 INTEGRATED FLIGHT SYSTEM — Light- weight fFS utilizing 3" instruments of the FD-104. Computer amplifier in a 1/4 ATR short.
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