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B737-Series
Rockwell Collins High frequency communication system
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HFS700 & HFS900 Series systems;
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Single or dual system installations
- SelCal & Ships Audio integration
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B737-Series
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B737-Series
Elementary Navigation Enhanced mode S with flight ID
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Complete engineering data package
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Full integration material package
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Rockwell Collins and Honeywell mode S transponder change
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Gables/ Honeywell flight ID ATC control head installation
- EASA Approved STC
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B737-Series
406 MHz. Fixed ELT system.
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STC/Engineering
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All material including antenna structural package
- Wire harness, OEM Rotables and antenna
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B737-Series
Interior reconfiguration Engineering
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PAX reconfigurations LOPA design and approval
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Monument relocations and installation
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Structural modification design and approval
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Emergency equipment LOPA design and approval
- Floor Path and interior lighting installation and reconfigurations
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B737-300, 400, 500
Enhanced Ground Proximity Warning (EGPWS)
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Engineering and STC integration
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EFIS and non EFIS system kits
- Complete integration kits and engineering
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737-300, 400, 500
FM Immunity VHF Nav replacement
- Engineering and approval
- Provision for compliant components
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737-300, 400, 500 NG
8.33 KHz. Channel spacing expansion 118.00 - 136.975
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Engineering and approval
- Material kit
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737-Series
Fuel Quantity indication change
- Reconfigure aircraft fuel system units of measure to match the customer's requirements.
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737-Series
Cockpit voice recorder change to solid state version
- Addition of CVR power enable switch for JAR25-1301
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737-300, 400, 500
Flight Management Computer
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4MCU Replacement of 8MCU provisions
- System interface kits and engineering
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737-300, 400, 500
Parameter upgrade for flight data recording to comply with European JAR Ops requirements
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Installation of Flight Data Acquisition Management Unit (FDAM)
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Required position sensors to complete 34 parameter inputs
- Provisions include Engineering STC integration, complete wire harness system and
all required materials for install
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737-300, 400, 500
737-Series Installation of Aircraft Condition Monitoring System (ACMS)
- Integrated as part of the FDAM modification. Includes addition of sensors or wiring
for recording thrust reverser deployment, EGT, Fuel flow, N2, Engine oil pressure,
engine oil temp, fuel cut off and engine vibration
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737-Series
ACARS and VHF installation (Honeywell MK II)
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Engineering STC and material for full integration CMUII ACARS and VHF
- Wiring harness, Rotables, antenna structure for VHF antenna
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737-Series
Various modifications (operator specific)
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Mode S Address re-strapping
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EFIS Code strapping re configurations
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SELCAL Code change
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Cockpit instrument panel reconfigurations
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Operator specific equipment changes for fleet standardization
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Flight-VU cabin camera system.
- Interior reconfigurations
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