Picture of product MK VII

Part #:

Model: MK VII

OEM:

Honeywell

Desc:

GPWS Computer

Part Number :


 
Mark VII
FEATURES
  • Enhanced Ground Proxy Warning System (EGPWS)
  • Class A TAWS that provides protection against controlled flight into terrain (CFIT) as well as reactive windshear detection
  • CFIT warnings include excessive rate of descent, terrain closure rate, excessive altitude loss after takeoff or missed approach procedure, insufficient terrain clearance, descent below glideslope, and excessive bank angle
  • EGPWS incorporates features such as pin-selectable altitude callouts, envelope modulation, geometric altitude algorithm, turn extrapolation, auto display pop-up, auto tilt of weather radar, and the ability to host Honeywell's Runway Awareness and advisory System (RAAS)
  • Visual and aural warnings of impending windshear are provided via Honeywell's unique computer algorithms that can detect an increase in aircraft performance (a precursor to windshear)
  • System can be interfaced to Honeywell's optional bi-axial accelerometer if IRS or AHRS inputs are not available
  • FAA Certification:
    • TSO-C92c (GPWS)
    • TSO-C117a (Windshear)
    • TSO-C151a (Enhanced Functions)
    • TSO-C129a (Mercury GNSS)
    • UKCAA Certification: Specification 14

 

SPECIFICATIONS

Size: 2 MCU ARINC 600-6 form factor chassis Dimensions: 7.64"H x 2.43"W x 12.76"L (14.26" including handle)
Markings/Identification: per ARINC 723-1 Weight: 7.5 lbs.
Mounting: Rack mounted per ARINC 600-6 Vibration isolation or shock mounting not required Reliability: MTBF: ≥ 12,500 (operating) hours MTBUR: ≥ 11,250 (operating) hours
Power: See P/N Chart below Temperature Range: Operational: -40° to +70° C -55° to +70° (965-1076-040) Storage: -55° to +85° C
Altitude: High Altitude: 55,000 ft. Decompression: 8,000 to 55,000 ft. Overpressure: -15,000 ft. Cooling: Convection (no forced air cooling)
Shock: Operational: 6 G's for 11 msec Crash Safety: Impulse: 15 G's for 11 msec (20 G's for 965-1076-060) Sustained: 12 G's for 3 seconds (20 G's for 965-1076-060)
Radio Frequency Susceptibility: HIRF (radiated and conducted) (Category R)    
Part Number: Description:
965-1076-001-XXX-XXX Power Requirements: 115 VAC/400 HZ, 26 Watts with warning over 8Ω speaker
965-1076-020-XXX-XXX Power Requirements: 115 VAC/400 HZ, 31 Watts with warning over 8Ω speaker
965-1076-030-XXX-XXX Power Requirements: +28 VDC, 33 Watts with warning over 8Ω speaker
965-1076-040-XXX-XXX Power Requirements: +28 VDC, 25 Watts with warning over 8Ω speaker
965-1076-060-XXX-XXX Power Requirements: 115 VAC/400 HZ, 40 Watts with warning over 8Ω speaker
NOTE: X’s represent variable values defining a specific application and configuration software version

 

965-0876-001-B05-B08
- GPWS Computer
Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
965-0876-030-B04-B05
- Ground Prox Warn System
Price Condition Status
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965-0876-030-B05-B06
- Ground Prox Warn System
Price Condition Status
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965-0876-030-B05-B08
- GPWS Computer
Price Condition Status
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965-0876-030-B05-B12
- GPWS Computer
Price Condition Status
$2,500.00 SV OUTRIGHT REQUEST LEAD TIME
965-0876-030-B08-B11
- Ground Prox Warn System
Price Condition Status
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965-0876-040
- GPWS
Price Condition Status
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965-0876-041-B10-B14
- GPWS Computer
Price Condition Status
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965-0876-041-B10-B17
- GPWS Computer
Price Condition Status
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965-1076-001
- EGPWS Computer, 115VAC

NSN: 6340-01-518-8922

Price Condition Status
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965-1076-001-204-204
- EGPWS
Price Condition Status
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965-1076-001-217-217
- EGPWS
Price Condition Status
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965-1076-001-218-218
- EGPWS Computer
Price Condition Status
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965-1076-001-224-224
- Enhanced Ground Proximity Warning System
Price Condition Status
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965-1076-001-226-226
- EGPWS

NSN: 6340-01-469-8450

Price Condition Status
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965-1076-020-206-206
- EGPWS
Price Condition Status
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965-1076-020-208-208
- EGPWS Computer
Price Condition Status
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965-1076-020-213-213
- EGPWS Computer
Price Condition Status
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965-1076-020-214-214
- EGPWS Computer
Price Condition Status
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965-1076-020-218-218
- EGPWS Computer
Price Condition Status
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965-1076-030-204-204
- Enhanced Ground Prox
Price Condition Status
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965-1076-030-213-213
- EGPWS
Price Condition Status
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965-1076-040-204-204
- 28VDC EGPWS Computer
Price Condition Status
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965-1076-040-206-206
- Enhanced Ground Prox
Price Condition Status
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965-1076-040-208-208
- Enhanced Ground Prox
Price Condition Status
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965-1076-040-212-212
- Enhanced Ground Prox
Price Condition Status
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965-1076-040-213-213
- Enhanced Ground Prox
Price Condition Status
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965-1076-040-214-214
- Enhanced Ground Prox
Price Condition Status
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965-1076-040-218-218
- Enhanced Ground Prox

NSN: 5841-01-530-5537

Price Condition Status
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965-1076-040-224-224
- 28VDC EGPWS Computer
Price Condition Status
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965-1076-040-226-226
- 28VDC EGPWS Computer
Price Condition Status
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Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com


In relation to NE (New) parts, many OEMs change their prices and availability without any notice to dealers or the industry. Therefore, through the REQUEST or RFQ indication, we ask that customers contact us for the most accurate price and availability.

In relation to SV & OH parts, the used parts aftermarket in the aviation industry is not an infinite supply. It is a dynamic, constantly changing market that is significantly affected by and susceptible to highs and lows in supply and demand. Therefore, although we attempt to, at times, we are unable to predict the exact moment when an item may be available. Once again, through the REQUEST or RFQ indication on our website, we ask that customers contact us for the most current and accurate price and availability.

Many avionics systems require a configuration or setup process. This process is required to interface certain avionics systems to other systems in the aircraft that will be inputting or outputting information to and from these systems. Some examples of systems that require a configuration or setup process include:

Autopilot
EFIS
GPS
EGPWS
EHSI
RADAR
TAWS
TCAS


In addition, most newer technology or solid state systems require configuration via computer interface of some type. A qualified avionics technician should always refer to the appropriate manufacturer's installation manual for complete information and instructions.