MODIFICATIONS OF 1. Honeywell International Inc (151)

ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC) FOR AIRBUS A320 FAMILY

Installation of a Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) and Activation of the SmartRunway/SmartLanding Features in accordance with Honeywell Master Drawing List 756-0239-001, revision D, dated August 11, 2011, or later FAA approved revision.
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INSTALLATION OF HTE ALTERNATE PART NUMBER EFS 40/50 SG465 SYMBOL...

Installation of hte alternate part number EFS 40/50 SG465 Symbol Generator.
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MODELS PC-12, PC-12/45 AND PC-12/47 - INSTALLATION OF THE ALTERNATE...

Models PC-12, PC-12/45 and PC-12/47 - Installation of the alternate part number EFS 40/50 SG 465 Symbol Generator.
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INSTALLATION OF HONEYWELL KGP 560 GENERAL AVIATION ENHANCED GROUND PROXIMITY...

Installation of Honeywell KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS) with optional KMD 550/850 Multi-Function Display.
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REQUIREMENTS FOR INSTALLATION OF DUAL HONEYWELL/TRIMBLE HT9100 GLOBAL NAVIGATION SATELLITE...

Requirements for installation of Dual Honeywell/Trimble HT9100 global navigation satellite systems (GNSS).
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INSTALLATION OF CHADWICK HELMUTH PROPELLER BALANCE MONITORING SYSTEM (VIBRATION MANAGEMENT...

Installation of Chadwick Helmuth Propeller Balance Monitoring System (Vibration Management System II, VMS II).
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INSTALLATION OF A HONEYWELL ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)...

Installation of a Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) and Activation of the Smart Runway/Smart Landing Features.
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INSTALLATION OF A HONEYWELL CAS-100 TRAFFIC ALERT AND COLLISION AVOIDANCE...

Installation of a Honeywell CAS-100 Traffic Alert and Collision Avoidance System II (TCAS II)
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INSTALLATION OF A HONEYWELL ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)...

Installation of a Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) and Activation of the Smart Runway/Smart Landing Features in accordance with Honeywell Master Drawing List 756-0232-001, revision B, dated 11-17-2010 or later FAA approved revision.
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INSTALLATION OF THE MARK II AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING...

Installation of the Mark II Aircraft Communications Addressing and Reporting System (ACARS).
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INSTALLATION OF DUAL TRIMBLE TNL8100 GPS NAVIGATION SYSTEMS INTERFACED TO...

Installation of dual Trimble TNL8100 GPS Navigation Systems interfaced to existing instruments and autopilot.
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INSTALLATION OF A HONEYWELL ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)...

Installation of a Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) and Activation of the Smart Runway/Smart Landing Features in accordance with Honeywell Master Drawing List 756-0236-001, revision A, dated August 19, 2011, or later FAA approved revision.
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INSTALLATION OF A HONEYWELL ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)...

Installation of a Honeywell Enhanced Ground Proximity Warning Computer (EGPWC) and Activation of the Smart Runway/Smart Landing Features in accordance with Honeywell Master Drawing List 756-0233-001, revision B, dated February 14, 2011 or later FAA approved revision.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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INSTALLATION OF THE HONEYWELL TPA-100B TCAS II CHANGE 7.1 PROCESSOR

Installation of the Honeywell TPA-100B TCAS II Change 7.1 Processor
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ACTIVATION OF THE ENHANCED MODE S TRANSPONDER FUNCTION AND INSTALLATION...

Activation of the Enhanced Mode S Transponder function and installation of the Avionics Upgrade on the Lockheed 382G airplane
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INSTALLATION OF A HONEYWELL TPA-100 TCAS II PROCESSOR IN ACCORDANCE...

Installation of a Honeywell TPA-100 TCAS II Processor in accordance with Honeywell Master Drawing List 756-0238-001, revision B, dated 7-28-2011 or later FAA approved revision.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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ONE ONLY STC, S/N 468-58: INSTALLATION OF THE HONEYWELL EGPWS...

ONE ONLY STC, S/N 468-58: Installation of the Honeywell EGPWS with RAAS and Monitor Functions.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM.

Installation of a Honeywell Chadwick Model 15175 VXP system.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM.

Installation of a Honeywell Chadwick Model 15175 VXP System.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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INSTALLATION OF A CHADWICK-HELMUTH VIBRATION MONITORING SYSTEM, VXP.

Installation of a Chadwick-Helmuth Vibration Monitoring System, VXP.
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INSTALLATION OF A HONEYWELL CHADWICK MODEL 15175 VXP SYSTEM

Installation of a Honeywell Chadwick Model 15175 VXP System
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INSTALLATION OF A PERFORMANCE MANAGEMENT SYSTEM. (727-200 SERIES AIR CANADA...

Installation of a Performance Management System. (727-200 SERIES AIR CANADA CONFIGURATIONS)
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INSTALLATION OF PROVISIONS FOR SPERRY PERFORMANCE MANAGEMENT SYSTEM.

Installation of provisions for Sperry Performance Management System.
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ONE ONLY STC, SN 560-0004: INSTALLATION OF HONEYWELL DIFFERENTIAL GLOBAL...

ONE ONLY STC, SN 560-0004: Installation of Honeywell Differential Global Positioning System (DGPS) Airborne System (SLS-2000).
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INSTALLATION OF THE PRIMUS EPIC CONTROL DISPLAY SYSTEM-RETROFIT (CDS-R) WITH...

Installation of the Primus EPIC control Display System-Retrofit (CDS-R) with enhanced Ground Proximity Warning System (EGPWS) and Dual AZ-810 Air Data cmputers onto the Cessna 560 (Citation V)
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REQUIREMENTS FOR THE INSTALLATION OF THE HONEYWELL FMZ-2000 FMS AND...

Requirements for the installation of the Honeywell FMZ-2000 FMS and the HG2021 12 Channel GPS.
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INSTALLATION OF HONEYWELL HUD-2020 HEADS-UP DISPLAY SYSTEM FOR CATEGORY II...

Installation of Honeywell HUD-2020 heads-up display system for Category II approach criteria.
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ONE ONLY STC, SN 650-0005: INSTALLATION OF HONEYWELL TOTAL AIRCRAFT...

ONE ONLY STC, SN 650-0005: Installation of Honeywell Total Aircraft Information system (TAIS).
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MODIFICATION OF ELECTRICAL SYSTEM, INSTALLATION OF AVIONICS AND AUTOMATIC FLIGHT...

Modification of electrical system, installation of avionics and automatic flight control system for single pilot IFR.
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ONE ONLY STC, S/N 1005: INSTALLATION OF A SINGLE PILOT...

ONE ONLY STC, S/N 1005: Installation of a single pilot IFR configuration.
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INSTALLATION OF A SPERRY PRIMUS300SL OR 400SL WEATHER RADAR SYSTEM...

Installation of a Sperry Primus300SL or 400SL weather radar system and new nose radome.
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INSTALLATION OF A SPERRY AA-300 RADIO ALTIMETER SYSTEM.

Installation of a Sperry AA-300 radio altimeter system.
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INSTALLATION OF A SPERRY PRIMUS 500 WEATHER RADAR SYSTEM.

Installation of a Sperry Primus 500 weather radar system.
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INSTALLATION OF A SPERRY PRIMUS 300 SL WEATHER RADAR SYSTEM.

Installation of a Sperry Primus 300 SL weather radar system.
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INSTALLATION OF A SPERRY SINGLE PILOT IFR AFCS (CATEGORY 1).

Installation of a Sperry single pilot IFR AFCS (Category 1).
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INSTALLATION OF DUAL SPERRY EDZ-705 ELECTRONIC FLIGHT INSTRUMENT SYSTEMS, (EFIS).

Installation of dual Sperry EDZ-705 Electronic Flight Instrument Systems, (EFIS).
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INSTALLATION OF A SPERRY ONE OR TWO-PILOT IFR/VFR AVIONICS.

Installation of a Sperry one or two-pilot IFR/VFR avionics.
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INSTALLATION OF SPERRY DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS FOR ONE...

Installation of Sperry digital automatic flight control systems for one or two pilot IFR/VFR operation.
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INSTALLATION OF DUAL SPERRY SPZ-7000 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS.

Installation of dual Sperry SPZ-7000 digital automatic flight control systems.
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ONE ONLY, SN 31195 (N3910Y): INSTALL A SPERRY ONE-OR TWO-PILOT...

ONE ONLY, SN 31195 (N3910Y): Install a Sperry one-or two-pilot IFR/VFR avionics installation.
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INSTALLATION OF NAVIGATION COMPUTER P/N 7004402-875 OR P/N 7004402-975 AND...

Installation of navigation computer P/N 7004402-875 or P/N 7004402-975 and installation of auto tune wiring modification.
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ONE ONLY STC, SN 650-0005; INSTALLATION OF DUAL SPERRY EDZ-601...

ONE ONLY STC, SN 650-0005; Installation of dual Sperry EDZ-601 Electronic Flight Instrument Systems (EFIS) and a Global GNS-500A VLF/Omega Navigation System with a NDB-2 Data Base
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ONE ONLY STC, SN 550-0098; INSTALLATION OF DUAL SPERRY EDZ-601,...

ONE ONLY STC, SN 550-0098; Installation of dual Sperry EDZ-601, or EDZ-801, Electronic Flight Instrument Systems (EFIS)
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INSTALLATION OF SPERRY SP-40C AUTO FLIGHT CONTROL SYSTEM AND SPI-73B...

Installation of Sperry SP-40C auto flight control system and SPI-73B Sperry instrumentation system.
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INSTALLATION OF EPIC PHASE 4.2 SOFTWARE, ALTERNATE PART NUMBER AGM-200...

Installation of EPIC Phase 4.2 Software, alternate part number AGM-200 AFGS and alternate part number TR-865B CMF VDR
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INSTALLATION OF THE AGM-200 ADVANCED GRAPHICS MODULE AND ALTERNATE PART...

Installation of the AGM-200 Advanced Graphics Module and alternate part number Data Base Module.
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INSTALLATION OF DUAL HONEYWELL ENHANCED GNS-XLS FLIGHT MANAGEMENT SYSTEM. AIRCRAFT...

Installation of dual Honeywell enhanced GNS-XLS Flight Management System. Aircraft must have STC ST335CH-D installed.
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APPROVED FOR MODEL PC-12/45, S/N 101 AND AFTER, NOT TO...

Approved for model PC-12/45, S/N 101 and after, not to exceed S/N 540. Group airworthiness approval for Reduced Vertical Separation Minimum (RVSM).
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INSTALLATION OF ALLIEDSIGNAL CAS-67A TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM...

Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II) incorporating MOPS Change 7. Airplane must be previously equipped with STC ST333CH-D.
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INSTALLATION OF A BENDIX/KING CAS67A TCAS II SYSTEM WITH DUAL...

Installation of a Bendix/King CAS67A TCAS II System with dual MST-67 Mode S Transponders installed per Garrett Aviation Services.
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INSTALLATION OF A HONEYWELL AM-250 ALTIMETER.

Installation of a Honeywell AM-250 Altimeter.
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INSTALLATION OF DUAL HONEYWELL AM-250 ALTIMETERS TO INTERFACE WITH THE...

Installation of dual Honeywell AM-250 altimeters to interface with the Bendix/King KFC 325 autopilot system for Reduced Vertical Separation Minimum (RVSM) group airworthiness approval.
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INSTALLATION OF HONEYWELL ENHANCED GROUND PROXIMITY WARNING SYSTEM. LIMITED TO...

Installation of Honeywell Enhanced Ground Proximity Warning System. Limited to installation on NA-265-65, serial number 465-58 ONLY.
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INSTALLATION OF A BENDIX/KING VFR UTILITY AVIONICS PACKAGE (KCS 55A...

Installation of a Bendix/King VFR Utility Avionics Package (KCS 55A Compass System, KX 165 NavComm, KR 87 ADF, KRA 405 Radio Altimeter, Global Wulfsberg Flexcomm II, Artex Model 100 HM ELT, and Jet Model 510-22G Vertical Gyro.)
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INSTALL BENDIX/KING KAP 150H FLIGHT CONTROL SYSTEM.

Install Bendix/King KAP 150H Flight Control System.
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INSTALLATION OF BENDIX/KING EFS 40 FOUR OR TWO TUBE ELCTRONIC...

Installation of Bendix/King EFS 40 four or two tube elctronic flight instrument system.
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ONE-ONLY STC, SN 175: INSTALLATION OF DUAL BENDIX/KING KFC 400...

ONE-ONLY STC, SN 175: Installation of dual Bendix/King KFC 400 Automatic Flight Control Systems.
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INSTALLATION OF BENDIX 3 TUBE OR 5 TUBE EFS-10 ELECTRONIC...

Installation of Bendix 3 tube or 5 tube EFS-10 electronic flight instrument system.
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INSTALLATION OF BENDIX 3 TUBE OR 5 TUBE EFS-10 ELECTRONIC...

Installation of Bendix 3 tube or 5 tube EFS-10 electronic flight instrument system.
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INSTALLATION OF BENDIX/KING EFS-10 ELECTRONIC FLIGHT INSTRUMENT SYSTEMS (3 TUBE),...

Installation of Bendix/King EFS-10 Electronic Flight Instrument Systems (3 tube), single or dual KFC 400 Automatic Flight Control System (Category I and II), single or dual KAD 480 Air Data System, KNS 660 Flight Management System, KHF 950 HF Comm System, RDS 86 Color Weather Radar and Series III Radios.
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ONE-ONLY STC, SN 465-058: INSTALLATION OF BENDIX/KING CAS 80A TRAFFIC...

ONE-ONLY STC, SN 465-058: Installation of Bendix/King CAS 80A Traffic Alert and Collision Avoidance System.
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INSTALLATION OF BENDIX/KING EFS-10 ELECTRONIC FLIGHT INSTRUMENT SYS (5 TUBE)...

Installation of Bendix/King EFS-10 electronic flight instrument sys (5 tube) dual KFC-400 automatic flight control sys, dual KAD-480 air data sys, dual KNS-660 flight mgmt sys, KHF-950HF Comm System and MLS-21 microwave landing system.
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INSTALLATION OF BENDIX/KING 2 OR 3 TUBE EFS 50 EFIS...

Installation of Bendix/King 2 or 3 Tube EFS 50 EFIs and KFC 325 Automatic Flight Control System.
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INSTALLATION OF BENDIX/KING KLN 90B GPS (GLOBAL POSITIONING SYSTEM) FOR...

Installation of Bendix/King KLN 90B GPS (Global Positioning System) for IFR enroute and approach operation. For serial numbers UE-156 and above.
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INSTALLATION OF PROVISIONS FOR ALLIEDSIGNAL AIRSAT 1 IRIDIUM AERONAUTICAL SATELITE...

Installation of provisions for AlliedSignal AIRSAT 1 IRIDIUM Aeronautical Satelite Communication System.
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INSTALLATION OF BENDIX/KING 4-TUBE EFS-10 EFIS, DUAL BENDIX/KING KFC 400...

Installation of Bendix/King 4-tube EFS-10 EFIS, dual Bendix/King KFC 400 automatic flight control systems, dual Bendix/King series III VHF COMM/NAV, dual Bendix/King RMS 555 radio management system, Bendix/King DFS 43A, DMS 44A, MST 67A mode S transponder , KRA 405 radar altimeter, Motorola ARC-164 UHF COMM, Bendix/King KRT-707 TACAN, RDS 82 VP radar, MLS 21 MLS, CAS 81A TCAS, KHF 950 HF, KNS 660 FMS with ...
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INSTALLATION OF DUAL BENDIX/KING KFC 400 AUTOMATIC FLIGHT CONTROL SYSTEMS,...

Installation of dual Bendix/King KFC 400 automatic flight control systems, Bendix/King CNI equipment, 5 tube Bendix/King EFS 10 with KAH460 AHRS and dual Bendix/King KAD480 air data systems for category II approach operation.
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INSTALLATION OF ALLIEDSIGNAL AVIONICS, INC., KAD-481 ADAPTOR MODULE, PART NUMBER...

Installation of AlliedSignal Avionics, Inc., KAD-481 adaptor module, part number 065-05041-28E1 (software part number 125-00981-00E1). Approved for installation on NA-265-65, serial number 465-58 ONLY.
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INSTALLATION OF DUAL GLOBAL GNS-1000 FLIGHT MANAGEMENT SYSTEM, A GLOBAL...

Installation of dual Global GNS-1000 flight management system, a Global NDB-2 Navigation Database and a Global Airborne Flight Information System (AFIS).
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TRANSCEIVERS KY90, KY90E, KY90H, KY95, KY95E, AND KY95H.

Transceivers KY90, KY90E, KY90H, KY95, KY95E, and KY95H.
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