ALT 50A

Collins - Radio Alti
ALT 50A
ALT 50A


Part Number :
All prices are exclusive of VAT
Select part number to view pricing and availability.
Price Condition Delivery Action
1750.00 € OH OUTRIGHT In stock
850.00 € OH EXCHANGE On request
495.00 € SERVICE TEST EASA/FAA DUAL RELEASE On request
S.E.A.M.Repair Capabilities : Yes
Features
 
  • Lightweight, low-profile radio altimeter designed specifically for installation in light and medium, fixed-wing aircraft
  • Supplies altitude information to flight control/autopilot system during approach phase of flight
  • Typically used with 339H-3, 339H-4, 339H-4A (helicopter) analog indicators or DRI-55 digital display indicator, and two 437X-1/1A/1B or ANT-50A/51A/52 antennas depending on aircraft configuration
  • Provides decision height selection from 0 to 2000 feet
  • Provides four shop-adjustable altitude trips that can be adjusted to any altitude between 0 to 2000 ft. to provide switching to a flight director or other external system
  • Product improved version of the ALT-50/860F-2 transceiver (i.e. improved altitude accuracy, transmitter output power, etc.)
  • Versions available with altitude error reduction where unit will indicate lower altitude in the event of unit failure thus ensuring safe terrain separation
Specifications
 

TEMPERATURE RANGE

-54 to 71°C (operating)

ALTITUDE

Up to 45000 feet (operating)

ALTITUDE ACCURACY

more or less 2 feet (up to 2000 feet)

LOAD CAPABILITY

1 millimho maximum

RF TRANSMITTER POWER

210 mW nominal

FREQUENCY MODULATION (TRANSMIT

100 or 105 Hz

TIME CONSTANT

0.09s more or less 0.01 s

DC ANALOG SIGNAL

0 to 18 V dc, piecewise linear

ARINC

408

ENVIRONMENTAL CATEGORY

DO-138/AG/A/JN/AAAEXXXXX

RTCA

DO-138, DO-123

FAA TSO

C87

 
 
 
PART NUMBER DESCRIPTION

622-3201-001

0-2000 ft. range with 4 shop-adjustable altitude trips

622-3201-002

0-2000 ft. range, non-adjustable

622-3201-011

Same as -001 but with reduced altitude error product improvement mentioned above

622-3201-012

Same as -002 but with reduced altitude error product improvement mentioned above 

 
ALT 50A
'