MODIFICATIONS OF ALOFT AeroArchitects (261)

DEMONSTRATE ELECTROMAGNETIC COMPATIBILITY (EMC) TO TRANSMITTING PORTABLE ELECTRONIC DEVICES

Demonstrate Electromagnetic Compatibility (EMC) to Transmitting Portable Electronic Devices
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INSTALLATION OF A ROCKWELL COLLINS STAGE IN FLIGHT ENTERTAINMENT SYSTEM

Installation of a Rockwell Collins STAGE In Flight Entertainment System
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INSTALLATION OF A VIASAT KA CABIN DISTRIBUTION SYSTEM

Installation of a ViaSat KA Cabin Distribution System
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INSTALLATION OF A VIASAT KA SATCOM SYSTEM ON BOEING MODEL...

Installation of a ViaSat KA SATCOM System on Boeing Model 737-800 series per ViaSat Installation Master Data List 1246982, revision 005, dated June 08, 2017, or later FAA-approved revision
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INSTALLATION OF AUTOMATIC DEPENDENT SURVEILLANCE – BROADCAST OUT (ADS-B OUT)...

Installation of Automatic Dependent Surveillance – Broadcast Out (ADS-B Out) system
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INSTALLATION OF MAINTENANCE SWITCHES AND REDUNDANT OVERHEAT SENSORS FOR APU

Installation of Maintenance Switches and Redundant Overheat Sensors for APU
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INSTALLATION OF AN FANS CAPABLE AND NON-FANS CAPABLE IRIDIUM ANTENNAS

Installation of an FANS capable and Non-FANS capable Iridium Antennas
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INSTALLATION OF A EXECUTIVE INTERIOR

Installation of a Executive Interior
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INSTALLATION OF A FORWARD CARGO ELECTRONIC EQUIPMENT RACK

Installation of a Forward Cargo Electronic Equipment Rack
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INSTALLATION OF TWO FORWARD AND FOUR AFT TANK AUXILIARY FUEL...

Installation of two forward and four aft tank auxiliary fuel systemconfiguration in the forward and aft cargo compartments.
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INSTALLATION OF AUXILIARY FUEL SYSTEMS IN THE FORWARD AND AFT...

Installation of auxiliary fuel systems in the forward and aft cargocompartment.Configurations 1-E, 1-F, 1-G, 1-H, 1-J, 1-K, 1-L, 1-M, 1-N, 1-P, 1-R,1-S, 1-T, 1-U, 1-V, 1-W, 1-X and 1-Y.Rev1: List of AFMS corrected
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INSTALLATION OF A SUNDSTRAND TURBOMACH T-62T-40C7B GAS TURBINE AUXILIARY POWER...

Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator.
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INSTALLATION OF A SUNDSTRAND TURBOMACH T-62T-40C7B GAS TURBINE AUXILIARY POWER...

Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator
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INSTALLATION OF A FIVE-TANK AUXILIARY FUEL SYSTEMS IN THE AFT...

Installation of a Five-Tank Auxiliary Fuel Systems in the aft cargo compartment.
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INSTALLATION OF A 250-GALLON SUPPLEMENTAL WATER TANK AND PLUMBING.

Installation of a 250-gallon supplemental water tank and plumbing.
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INSTALLATION OF A FIVE-CELL AUXILIARY FUEL SYSTEM I THE FORWARD...

Installation of a Five-Cell Auxiliary Fuel System i the forward and aft cargo compartments.
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INSTALLATION OF AN EXECUTIVE INTERIOR. APPROVED FOR INSTALLATION ON BOEING...

Installation of an executive interior. Approved for installation on Boeing 737-800, serial number 32450 ONLY.
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INSTALLATION OF UNS-1E FLIGHT MANAGEMENT SYSTEM. APPROVED FOR INSTALLATION IN...

Installation of UNS-1E Flight Management System. Approved for installation in Boeing 737-600, 737-700, 737-800.
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INSTALLATION OF A THREE CELL AUXILIARY FUEL SYSTEM IN FORWARD...

Installation of a Three Cell Auxiliary Fuel System in forward and aft cargo compartments. Approved for serial numbers 32438, 32450, 32451, 32777, 32806, 32915, 32971, 33079, and 33361 ONLY.
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INSTALLATION OF A SIX-CELL AUXILIARY FUEL SYSTEM IN THE FORWARD...

Installation of a Six-Cell Auxiliary Fuel System in the forward and aft cargo compartments.
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DESCRIPTIVE DATA PERTAINING TO THIS DESIGN CHANGE ARE CONSIDERED INADEQUATE...

Descriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Boeing, 737-700 IGW, Serial Number 29749. Removal of the existing EROS Flight Crew Oxygen Masks P/N MF 20-003 and installation of EROS Full Face Flight Crew Oxygen Masks/goggles P/N MF 20-503.
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INSTALLATION OF HONEYWELL ONE VIEW AIS2000 (AIRBORNE DIRECT-TV) SYSTEM PER...

Installation of HOneywell ONE VIEW AIS2000 (Airborne Direct-TV) System per DeCrane Aircraft Master Drawing List 5059-0000-MDL latest revision. STC ST01340NY required with this mod.
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INSTALLATION OF AN EXECUTIVE INTERIOR PER DECRANE AIRCRAFT MASTER DRAWING...

Installation of an executive interior per DeCrane Aircraft Master Drawing List 5046-0000-MDL latest revision. Limited to installation on serial number 32628 ONLY.
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INSTALLATION OF STRUCTURAL PROVISIONS FOR A THREE CELL, FOUR CELL,...

Installation of structural provisions for a Three Cell, Four Cell, and Five Cell Auxiliary Fuel System, in forward and aft cargo compartments. For 737-700 (IGW).
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INSTALLATION OF PROVISIONS FOR A FIVE (5) CELL AUXILIARY FUEL...

Installation of provisions for a Five (5) Cell Auxiliary Fuel System. Limited to installation on aircraft that have STC SA714NE previously installed. Life-limited to 250 aircraft cycles.
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INSTALLATION OF AN EXECUTIVE PASSENGER CABIN INTERIOR IN ACCORDANCE WITH...

Installation of an executive passenger cabin interior in accordance with Jormac Aerospace Master Drawing List No.HOR1-MDL-000, Revision B, dated May 8, 2002, or later FAA approved revision. Limited to installation on serial number 21474 ONLY.
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INSTALLATION OF ONE MAGNASTAR C-2000 TERRESTRIAL TELEPHONE SYSTEM AND THREE...

Installation of one MagnaStar C-2000 Terrestrial Telephone System and three 60Hz Avionics Frequency Converters. Approved for 727-200 serial number 21474.
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INSTALLATION OF 100-GALLON SUPPLEMENTAL POTABLE WATER TANK, PLUMBING AND WATER...

Installation of 100-gallon supplemental potable water tank, plumbing and water sterilization system.
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INSTALLATION OF A PATS DECEASED DISTINGUISHED VISITOR (DDV) RESTRAINT SYSTEM.

Installation of a PATS Deceased Distinguished Visitor (DDV) restraint system.
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A. INSTALLATION OF A FOUR FORWARD, FOUR AFT TANK AUXILIARY FUEL...

a. Installation of a Four Forward, Four Aft Tank Auxiliary Fuel System on a Boeing 757-200 that is 14 CFR 25.981, amendment 102 and 14 CFR 26 compliant, in accordance with PATS Aircraft, LLC Master Drawing List 5936-0001-MDL revision P dated June 7, 2010. b. PATS Aircraft LLC, Airplane Flight Manual Supplement No. 202 revision IR, dated March 31, 2011. c. The aircraft must be maintained ...
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INSTALLATION OF PROVISIONS FOR A TWO FORWARD/TWO AFT CELL AUXILIARY...

Installation of provisions for a Two Forward/Two Aft Cell Auxiliary Fuel System in the forward and aft cargo compartment
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CONFIGURATION A: INSTALLATION OF 5,520 GALLON, TANK AUXILIARY FUEL SYSTEM...

Configuration A: Installation of 5,520 gallon, tank auxiliary fuel system in the forward and aft cargo compartment Configuration B: Installation of 2-722 gallon, tank auxiliary fuel system in the aft cargo compartment
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INSTALLATION OF CONTROL COLUMN AND RUDDER PEDAL, POSITION SENSORS FOR...

Installation of control column and rudder pedal, position sensors for Flight Data Recorder Expanded Parameters.
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INSTALLATION OF PROVISIONS FOR CONTROL COLUMN AND RUDDER PEDAL, POSITION...

Installation of provisions for Control Column and Rudder Pedal, Position Sensors for Flight Data Recorder Expanded Parameters.
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INSTALLATION OF SCANDINAVIAN BELLYLOADING CO SLIDING CARPET LOADING SYSTEM. (DC-9-81...

Installation of Scandinavian Bellyloading Co Sliding Carpet Loading System. (DC-9-81 (MD-81) Applicable to FSN 49912 only)
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INSTALLATION OF COLLINS COMMUNICATIONS MANAGEMENT UNIT AND VHF DATA RADIO...

Installation of Collins Communications Management Unit and VHF Data Radio Transceiver (ACARS/VDR)
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ONE-ONLY STC: INSTALLATION OF SCANDINAVIAN BELLYLOADING COMPANY SLIDING CARPET LOADING...

ONE-ONLY STC: Installation of Scandinavian Bellyloading Company Sliding Carpet Loading System, S/N 49912.
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INSTALLATION OF UNIVERSAL AVIONICS SYSTEMS CORPORATION TERRAIN AWARENESS AND WARNING...

Installation of Universal Avionics Systems Corporation Terrain Awareness and Warning System (TAWS) with dual Universal Avionics Systems Corporation MFD-640 multi-functional displays
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RECONFIGURATION OF FIRST CLASS SEATING TO ACCOMMODATE INSTALLATION OF A...

Reconfiguration of first class seating to accommodate installation of a first class closet.
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ONE-ONLY STC: INTERIOR RECONFIGURATION INVOLVING GALLEYS, LAVATORIES, VIDEO INSTALLATION, AND...

ONE-ONLY STC: Interior reconfiguration involving galleys, lavatories, video installation, and seats, S/N 24957.
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INSTALLATION OF ROCKWELL COLLINS SATELLITE COMMUNICATIONS (SATCOM) SYSTEM SAT-906 HIGH...

Installation of Rockwell Collins Satellite Communications (Satcom) system SAT-906 High Gain Aero H+
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INSTALLATION OF AN ADDITIONAL TAPE REPRODUCER AND SWITCHING UNIT.

Installation of an additional tape reproducer and switching unit.
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ONE-ONLY STC: CONVERSION OF A PASSENGER AIRPLANE WITH SIDE CARGO...

ONE-ONLY STC: Conversion of a passenger airplane with side cargo door to a freighter configuration, S/N 20713.
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INSTALLATION OF ROCKWELL COLLINS CMU-900 ACARS AND VHF-700 #3 VHF...

Installation of Rockwell Collins CMU-900 ACARS and VHF-700 #3 VHF Radio Provisions.
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INSTALLATION OF ROCKWELL COLLINS FPI-930 5 ATI LCD EADI &...

Installation of Rockwell Collins FPI-930 5 ATI LCD EADI & EHSI, WXR-700X Basic Turbulence Weather Radar System, and Honeywell Compass System
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ONE-ONLY STC: RECONFIGURATION OF AN INTERIOR ARRANGEMENT AND INSTALLATION OF...

ONE-ONLY STC: Reconfiguration of an interior arrangement and installation of entertainment system, S/N 21595.
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INSTALLATION OF CONTROL COLUMN AND RUDDER PEDAL, POSITION SENSORS FOR...

Installation of control column and rudder pedal, position sensors for Flight Data REcorder Expanded Parameters.
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INSTALLATION OF SPIRENT SYSTEMS HAMMERHEAD 3 DOCK AND SUMMIT AVIONICS...

Installation of Spirent Systems Hammerhead 3 Dock and Summit Avionics MIPS-312 Printer.
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INSTALLATION OF CABIN VIDEO SURVEILLANCE CAMERAS, VIDEO SERVER, WIRELESS LAN...

Installation of cabin video surveillance cameras, video server, wireless LAN unit, cabin wireless antenna, power supplies, thermal motion detectors, and structural mounting provisions for video display units.
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INSTALLATION OF PASSENGER ENTERTAINMENT SYSTEM PROVISIONS, ELECTRONIC FLIGHT BAG PROVISIONS,...

Installation of passenger entertainment system provisions, electronic flight bag provisions, and miscellaneous minor modifications. Approved for installation on Boeing 737-700 IGW serial number 29251.
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INSTALLATION OF AN EXECUTIVE INTERIORMAJOR CHANGE TO FAA STC ST01727NY-DUPDATE...

Installation of an Executive InteriorMajor Change to FAA STC ST01727NY-DUpdate of EASA STC 10027297 Rev 3: Compliance with EWIS ICA SpecialCondition H-01 Limitations: Configuration 1:-Master Drawing List 5950- 0000-MDL Rev. G dtd. 16.April 2009 (*)- Airplane Flight Manual Supplement No. 215, Rev. D dtd. 12. March 2010(*)-Maintenance Manual Supplement TO-3163 Rev. IR dtd. 1.May 2008 (*) withTR20-1001 dtd. 10.April 2 (...) Conditions: Configuration 1:- Concurrent installation ...
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INSTALLATION OF A PASSENGER GASEOUS OXYGEN SUPPLY SYSTEMMAJOR CHANGE TO...

Installation of a Passenger Gaseous Oxygen Supply SystemMajor Change to FAA STC ST01729NY-DUpdate of EASA STC 10027299 Rev 1: Compliance with EWIS ICA SpecialCondition H-01 Limitations: - Master Drawing List 6072-0000MDL Rev. A dtd. 15.December 2008 (*)- Airplane Flight Manual Supplement No. 226, Rev. IR dtd. 17.April 2009(*)- Maintenance Manual Supplement TO-3163 Rev. IR dtd. 1.May 2008 (*) withTR20-1001 dtd. 10.April 2009(*) or la (...) Conditions: ...
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MODIFICATION OF THE CLASS C FORWARD CARGO COMPARTMENT TO ACCOMMODATE...

Modification of the Class C Forward Cargo Compartment to accommodate anAuxiliary Fuel Tank and Installation of a new Class C Cargo Compartmentat the Rear of the Main CabinMajor Change to FAA STC ST01728NY- DUpdate of EASA STC 10027298 Rev 1: Compliance with EWIS ICA SpecialCondition H-01 Limitations: Configuration 1:Modification of the Class C Forward Cargo Compartment to accommodate an Auxiliary Fuel Tank and Installation of a ...
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REVISIONS TO AUXILIARY FUEL SYSTEM STRUCTURAL PROVISIONS CERTIFICATION BASIS IM.A.023THE...

Revisions to Auxiliary Fuel System Structural Provisions Certification Basis IM.A.023The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H- 01The requirements for environmental protection and the associatedcertif (...) Limitations EASA STC No. 10027222 dated 15 September 2009.FAA STC No. ST00365NY- D dated 14 January 2011.Configuration 6. Installation of a two tank Auxiliary Fuel System withinthe fuselage ...
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REVISIONS TO AUXILIARY FUEL SYSTEM STRUCTURAL PROVISIONS LIMITATIONS: PATS AIRCRAFT,...

Revisions to Auxiliary Fuel System Structural Provisions Limitations: PATS Aircraft, LLC. Airplane Flight Manual Supplement No. 200, RevisionB, FAA approved 11 June 2009, is required with configurations 5 and 6.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF AN EXECUTIVE INTERIOR LIMITATIONS: IN THIS INSTALLATION THE...

Installation of an Executive Interior Limitations: In this installation the maximum passenger seating capacity is limitedto 15.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF AN EXECUTIVE INTERIOR CERTIFICATION BASIS EASA IM.A.023THE CERTIFICATION...

Installation of an Executive Interior Certification Basis EASA IM.A.023The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCRI H- 01The requirements for environmental protection and the associatedce (...) Limitations Configuration 1:EASA STC No. 10027223 Revision 1 dated 08 February 2010.FAA STC No. ST01730NY-D dated 14 January 2011.PATS Aircraft, LLC Master Drawing List 6049-0001-MDL, revision F dated01 July ...
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INSTALLATION OF TEN AUXILIARY FUEL TANK SYSTEM CONFIGURATIONSVALIDATION OF STC...

Installation of ten auxiliary fuel tank system configurationsValidation of STC ST01725NY-D Approved configurations are the following: Configuration 1: ,,Installation of a Five-Cell Auxiliary Fuel System inthe forward and aft cargo compartments in accorda Limitations: Configurations 1 & 5:,,PATS Aircraft, LLC. Airplane Flight ManualSupplement No. 221 for a Five-Cell (1 Fwd/4 Aft) Auxiliary Fuel System,revision IR dated January 30, 2009 is required. Approved for aircraftwith NGS. Configurations ...
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MAJOR CHANGE TO FAA STC ST01727NY-D: PROJECT DAS-GED-P072 / ODA-GED-001-...

Major Change to FAA STC ST01727NY-D: Project DAS-GED-P072 / ODA-GED-001- Installation of Executive Interior (A/C #4) Limitations: Configuration 1: - Concurrent installation of STC ST01728NY-D (Class "C" CargoCompartment) iaw. Master Drawing List 6071-0000-MDL Rev. IR dtd.7.October 2008 is required. -Commercial operation under EASA rules requires installation of PATS SBST0172NY-D-25-S. Conditions: Not Applicable
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ALTERATION OF FIRE PROTECTION SYSTEMS, LOWER CARGO COMPARTMENTS. THIS STC...

Alteration of Fire Protection Systems, Lower Cargo Compartments. This STC revises and supersedes LBA STC LBA.21NE1.TA0511. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.The ...
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ALTERATION OF FIRE PROTECTION SYSTEMS, LOWER CARGO COMPARTMENTS. THIS STC...

Alteration of Fire Protection Systems, Lower Cargo Compartments. This STC revises and supersedes LBA STC LBA.21NE1.TA0682. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.The ...
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INSTALLATION OF ELECTRONIC EQUIPMENT RACK IN AFT BULK CARGO COMPARTMENT....

Installation of Electronic Equipment Rack in Aft Bulk Cargo Compartment. This STC revises and supersedes EASA STC EASA.IM.A.S.03093. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of ...
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INSTALLATION OF CANADIAN MARCONI CMA-2101 HIGH GAIN SATCOM ANTENNA. THIS...

Installation of Canadian Marconi CMA-2101 High Gain SATCOM Antenna. This STC revises and supersedes EASA STC EASA.IM.A.S.02513. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the ...
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INSTALLATION OF A TWO-CELL (ONE FORWARD, ONE AFT) AUXILIARY FUEL...

Installation of a Two-Cell (One Forward, One Aft) Auxiliary Fuel System in the forward and aft cargo compartment.
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ST01729NY-D: INSTALLATION OF A PASSENGER GASEOUS OXYGEN SUPPLY SYSTEM LIMITATIONS:...

ST01729NY-D: Installation of a Passenger Gaseous Oxygen Supply System Limitations: - Concurrent installation of STC's ST01727NY- D (Installation of anExecutive Interior) and ST01728NY-D (Class "C" Cargo Compartment) isrequired - For aircraft under FAA jurisdiction this modification may not beinstalled after 30.August 2010 unless:(1) previ. Conditions: Not Applicable
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MAJOR CHANGE TO FAA STC ST01728NY-D: DAS-GED-P067 - MODIFICATION OF...

Major Change to FAA STC ST01728NY-D: DAS-GED-P067 - Modification of theClass C Forward Cargo Compartment Limitations: Configuration 1: - Concurrent installation of STC ST01727NY-D (Installation of anExecutive Interior) iaw. Master Drawing List 5950-0000-MDL revision Gdtd. 16.April 2009 is required Configuration 2: - Concurrent installation of STC ST01727NY-D (Installation. Conditions: Not Applicable
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INSTALLATION OF VARIOUS PROVISIONS FOR A FIVE CELL AUXILIARY FUEL...

Installation of various provisions for a Five Cell Auxiliary Fuel System.
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INSTALLATION OF AUXILIARY FUEL SYSTEM IN THE FORWARD AND AFT...

Installation of Auxiliary Fuel System in the forward and aft cargocompartments.Validation of STC ST01713NY-D as amended June 29, 2009 Limitations: None.. Conditions: - Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.- The install
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INSTALLATION OF PROVISIONS FOR SMOKE DETECTION AND FIRE SUPPRESSION SYSTEMS,...

Installation of provisions for smoke detection and fire suppression systems, lower cargo compartments. Approved for 737-700 IGW and 737-700C Series.
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ONE ONLY STC - BOEING 737-700 IGW SERIAL NUMBER 29251....

ONE ONLY STC - Boeing 737-700 IGW Serial Number 29251. Installation of Passenger Entertainment System components, Electronic Flight Bag Provisions, and Miscellaneous Minor Modifications.
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INSTALLATION OF ALLIEDSIGNAL GNS-XLS FLIGHT MANAGEMENT SYSTEM WITH DUAL COLLINS...

Installation of AlliedSignal GNS-XLS Flight Management System with Dual Collins EHSI-74B electronic HSI.
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INSTALLATION OF A TWO TANK AUXILIARY FUEL SYSTEM WITHIN FUSELAGE...

Installation of a two tank auxiliary fuel system within fuselage pressure vessel forward of baggage compartment.
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INSTALLATION ECE SUBSTITUTE HALOGEN LAMP AS A REPLACEMENT FOR NOSE...

Installation ECE Substitute Halogen Lamp as a replacement for nose gear and/or wing landings and nose gear taxi lights
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INSTALLATION OF A SUNDSTRAND (GEMINI) T-20G-10C3/-10C3A APU.

Installation of a Sundstrand (Gemini) T-20G-10C3/-10C3A APU.
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INSTALLATION OF B/E AEROSPACE AIR CHILLER P/N 470-1 LIMITATIONS: APPLICABLE...

Installation of B/E Aerospace air Chiller P/N 470-1 Limitations: Applicable only to A/C with C&D Zodiac pantry installation P/N C801001-101 and C801001- 103 covered by FAA STC ST02144LA and EASA STC P-EASA.A.S.02421.. Conditions: n/a
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INSTALLATION OF MOUNTING PROVISIONS AND ELECTRICAL PROVISIONS FOR ELECTRONIC FLIGHT...

Installation of mounting provisions and electrical provisions for electronic flight bags. Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.. Conditions: n/a
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INSTALLATION OF A FOUR-CELL AUXILIARY FUEL SYSTEM IN THE FORWARD...

Installation of a four-cell auxiliary fuel system in the forward and aft cargo compartments.
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INSTALLATION OF SMOKE DETECTION AND FIRE SUPPRESSION SYSTEMS PROVISIONS, LOWER...

Installation of Smoke Detection and Fire Suppression Systems Provisions, Lower Cargo Compartments. Limitations: n/a. Conditions: n/a
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INSTALLATION OF SMOKE DETECTION AND FIRE SUPPRESSION SYSTEMS PROVISIONS, LOWER...

Installation of Smoke Detection and Fire Suppression Systems Provisions, Lower Cargo Compartments. Limitations: n/a. Conditions: n/a
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INSTALLATION OF THE KLM B747-200/-300 AVIONICS UPGRADE - ELECTRONIC FLIGHT...

Installation of the KLM B747-200/-300 Avionics Upgrade - Electronic Flight Instrument System (EFIS). Approval of this change in type design applies to the above model aircraft only, serial numbers 21110, 21111, 21549, 21550, 21659, 21660, 21848, 22376, 22379, 22380, 23056, 23137, and 23508.
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INSTALLATION OF THE KLM B747-200/300 AVIONICS UPGRADE – PHASE 1...

Installation of the KLM B747-200/300 Avionics Upgrade – Phase 1 (Analog Instruments).
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INSTALLATION OF A TWO TANK AUXILIARY FUEL SYSTEM. CERTIFICATION BASIS...

Installation of a two tank Auxiliary Fuel System. Certification Basis Limitations -FAA STC No. ST00365NY-D dated 29 January 2007.-Configuration 3. Installation of structural provisions only, for a two(2) Cell Auxiliary Fuel System within the fuselage pressure vesselforward of the baggage compartment in accordance with PATS Aircr (...) Conditions 1. PATS Aircraft, LLC Airplane Flight Manual Supplement No.200, Rev. IRFAA approved January 5, 2007 is required with ...
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INSTALLATION OF B/E AEROSPACE AIR CHILLER P/N 470-1 LIMITATIONS: THIS...

Installation of B/E Aerospace Air Chiller P/N 470-1 Limitations: This approval is limited to airplanes on which C&D Zodiac Pantry P/N C481001-101 has been installed in accordance with STC ST01880LA. Conditions: n/a
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INSTALLATION OF A TWO TANK AUXILIARY FUEL SYSTEM WITHIN FUSELAGE...

Installation of a two tank auxiliary fuel system within fuselage pressure vessel forward of baggage compartment.
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INSTALLATION OF A THREE CELL AUXILIARY FUEL SYSTEM AND A...

Installation of a three cell auxiliary fuel system and a four cell auxiliary fuel system.
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INSTALLATION OF A GARRETT AIRESEARCH GTCP 36-100(A) APU.

Installation of a Garrett AiResearch GTCP 36-100(A) APU.
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INSTALLATION OF PROVISIONS FOR A 5-CELL AUXILIARY FUEL SYSTEM IN...

Installation of provisions for a 5-cell auxiliary fuel system in cargo compartment per configuration 5005-2800-300 of Decrane/Pats, Inc. master drawing list no. 5005-2800-001 latest FAA approved revision. Life-limited to 50 aircraft flight cycles.
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INSTALLATION OF A SUNDSTRAND TURBOMACH T-62T-40C7B GAS TURBINE AUXILIARY POWER...

Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator.
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INSTALLATION OF EXECUTIVE INTERIOR. THIS APPROVAL IS LIMITED TO THE...

Installation of executive interior. This approval is limited to the installation made in Boeing Aircraft Company Model 757-2M6, Serial Number 23454 only.
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INSTALLATION OF SOLAR T-62T-40C APU WHEN GARRETT AIRESEARCH TFE-731-3-1H ENGINES...

Installation of Solar T-62T-40C APU when Garrett AiResearch TFE-731-3-1H engines are installed in accordance with STC SA3925WE.
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INSTALLATION OF GARRETT AIRESEARCH GTCP36-100(H) AUXILIARY POWER UNIT.

Installation of Garrett AiResearch GTCP36-100(H) auxiliary power unit.
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INSTALLATION OF SOLAR T-62T-40C APU WITH 400 AMPERE STARTER-GENERATOR.

Installation of solar T-62T-40C APU with 400 ampere starter-generator.
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INSTALLATION OF AUXILIARY POWER UNIT GARRETT MODEL GTCP36-150 FOR GROUND...

Installation of auxiliary power unit Garrett Model GTCP36-150 for ground use only.
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INSTALLATION OF TURBOMECH AUXILIARY POWER UNIT. LIMITED TO INSTALLATION ON...

Installation of Turbomech auxiliary power unit. Limited to installation on serial number NA758 ONLY.
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REPLACEMENT OF GARRETT AIRESEARCH GTCP-36-6 APU WITH SOLAR T-62T-40C2 APU.

Replacement of Garrett AiResearch GTCP-36-6 APU with Solar T-62T-40C2 APU.
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INSTALLATION OF A GARRETT GTCP 36-150W AUXILIARY POWER UNIT FOR...

Installation of a Garrett GTCP 36-150W auxiliary power unit for ground use only.
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INSTALLATION OF SOLAR T-62T-39Y, -39 OR -40C APU MODIFICATIONS.

Installation of Solar T-62T-39Y, -39 or -40C APU modifications.
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REPLACEMENT OF GARRETT GTCP 36-6 AUXILIARY POWER UNIT BY GARRETT...

Replacement of Garrett GTCP 36-6 auxiliary power unit by Garrett GTCP 36-100G auxiliary power unit.
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INSTALLATION OF SOLAR T-62T-39 GAS TURBINE AUXILIARY POWER UNIT.

Installation of Solar T-62T-39 gas turbine auxiliary power unit.
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INSTALLATION OF SOLAR T-62T-40C7. LIMITED TO INSTALLATION ON SERIAL NUMBER...

Installation of Solar T-62T-40C7. Limited to installation on serial number 013 ONLY.
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INSTALLATION OF A SOLAR GAS TURBINE MODEL APU. LIMITED TO...

Installation of a Solar Gas Turbine Model APU. Limited to installation on serial number 135 ONLY.
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INTEGRATED AUXILIARY POWER UNIT AND AIR CONDITIONING SYSTEM USING SOLAR...

Integrated auxiliary power unit and air conditioning system using Solar T-62T-29A gas turbine.
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REPLACEMENT OF SOLAR T-62T-39 APU. LIMITED TO INSTALLATION ON FALCON...

Replacement of Solar T-62T-39 APU. Limited to installation on Falcon Series F serial numbers 428 and 426.
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INSTALLATION OF 225 AMPERE CURRENT LIMITER IN THE BATTERY GROUND...

Installation of 225 ampere current limiter in the battery ground circuit.
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INSTALLATION OF AIRESEARCH GTCP 36-100(H) AUXILIARY POWER UNIT. LIMITED TO...

Installation of AiResearch GTCP 36-100(H) auxiliary power unit. Limited to installation on serial number 1329-23E, serial number 5112 ONLY.
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INSTALLATION OF SOLAR GAS TURBINE AUXILIARY POWER UNIT T-62T-40C.

Installation of Solar gas turbine auxiliary power unit T-62T-40C.
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INSTALLATION OF SOLAR MODEL T-62T-39 GAS TURBINE AUXILIARY POWER UNIT....

Installation of Solar Model T-62T-39 Gas Turbine Auxiliary Power Unit. Limited to installation on serial number 140 ONLY.
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INSTALLATION OF SOLAR MODEL T-62T-39 GAS TURBINE AUXILIARY POWER UNIT....

Installation of Solar Model T-62T-39 gas turbine auxiliary power unit. Limited to installation on serial number 19 and serial number 68.
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REWORK OF SOLAR T-62T-39 APU INSTALLED BY STC SA674CE WHEN...

Rework of Solar T-62T-39 APU installed by STC SA674CE when Garrett AiResearch TFE-731-3-1H engines are installed per STC SA3870WE.
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INSTALLATION OF AN AUXILIARY POWER UNIT GARRETT MODEL GTCP 36-150W...

Installation of an auxiliary power unit Garrett model GTCP 36-150W for ground and flight use.
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INSTALLATION OF BITE OR FAULT INDICATOR UNIT CONNECTED TO ELECTRONIC...

Installation of bite or fault indicator unit connected to electronic sequencing unit of Garrett 36-100(A) aux. power unit.
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INSTALLATION OF HAMILTON STANDARD R72-3W AIR CYCLE MACHINE, P/N 750660-3...

Installation of Hamilton Standard R72-3W air cycle machine, P/N 750660-3 or 78790-2, Model DHC 7/10 heat exchanger, P/N 753355.
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INSTALLATION OF A GARRETT GTCP 36-150RJ GAS TURBINE AUXILIARY POWER...

Installation of a Garrett GTCP 36-150RJ gas turbine auxiliary power unit.
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INSTALLATION OR TURBOMACH (SOLAR) T-62T-40C APU. LIMITED TO INSTALLATION ON...

Installation or Turbomach (Solar) T-62T-40C APU. Limited to installation on model BH.125-400A, serial number 755 ONLY.
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INSTALLATION OF SECURAPLANE TECHNOLOGIES BC-1306 BATTERY CHARGER AND HAWKER 40...

Installation of Securaplane Technologies BC-1306 Battery Charger and Hawker 40 amp-hour sealed lead acid battery.
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INSTALLATION OF AN AUXILIARY POWER UNIT GARRETT MODEL GTCP 36-150W...

Installation of an auxiliary power unit Garrett Model GTCP 36-150W for ground and flight use.
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