MODIFICATIONS OF Airborne Maintenance & Engineering Services (74)

INSTALLATION OF AN ACSS SURVEILLANCE PROCESSOR, MODE-S DATALINK TRANSPONDERS AND...

Installation of an ACSS Surveillance Processor, Mode-S Datalink Transponders and associated components with ADS-B Out provisions
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RELOCATION OF THE AUXILIARY POWER UNIT (APU) ELECTRONIC CONTROL UNIT(ECU)...

Relocation of the Auxiliary Power Unit (APU) Electronic Control Unit(ECU) from the E6 rack in the Aft Equipment Center (AEC) to the E2 rackin the thermally-controlled Main Equipment Center (MEC)
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RELOCATION OF THE AUXILIARY POWER UNIT (APU) ELECTRONIC CONTROL UNIT...

Relocation of the Auxiliary Power Unit (APU) Electronic Control Unit (ECU) from the E6 rack in the A
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INSTALLATION OF DUAL HONEYWELL XK516D 400W HIGH FREQUENCY (HF) VOICERADIO...

Installation of dual Honeywell XK516D 400W High Frequency (HF) VoiceRadio Systems:- configuration 1: installation of provisions on aircraft without HFprovisioned or aircraft provisioned for ferry kit-configuration 2: installation of provisions on aircraft with a singleBoeing HF Voice Radio System ins...
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MODIFICATION TO THE FLAP CONTROL SYSTEM TO PROVIDE A MAXIMUM...

Modification to the flap control system to provide a maximum landing flap of 40 degrees in the norma
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INSTALLATION OF A UNIVERSAL AVIONICS TERRAIN AWARENESS WARNING SYSTEM (TAWS)...

Installation of a Universal Avionics Terrain Awareness Warning System (TAWS) and a Universal Avionics GPS-1000 Global Positioning System.
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INSTALLATION OF PROVISIONS FOR DUAL HONEYWELL XK516D HIGH FREQUENCY (HF)...

Installation of provisions for dual Honeywell XK516D High Frequency (HF) radio systems.
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REPLACE TELEDYNE DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) P/N 2227000-1...

Replace Teledyne Digital Flight Data Acquisition Unit (DFDAU) P/N 2227000-1 with Teledyne DFDAU P/N 2233000-816.
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CONVERSION OF A BOEING 757-200 SERIES PASSENGER CONFIGURATION TO A...

Conversion of a Boeing 757-200 series passenger configuration to a freighter configuration incorporating a new main deck cargo door, interior, and associated systems
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INSTALLATION OF ELECTRONIC STANDBY INSTRUMENT SYSTEM (ESIS) LIMITATIONS: ONLY TO...

Installation of Electronic Standby Instrument System (ESIS) Limitations: Only to be installed on a/c with EASA STC 10036223 installed.. 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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UPGRADE OF TELEDYNE DIGITAL FLIGHT DATA ACQUISITION UNIT LIMITATIONS: NONE....

Upgrade of Teledyne Digital Flight Data Acquisition Unit 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.
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INSTALLATION OF THE WINGSPEED SATELLITE COMMUNICATION (SCS) AND TWO DAC...

Installation of the WingSpeed Satellite Communication (SCS) and two DAC international Cockpit Display Devices (CDD) Class II
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INSTALLATION OF UNIVERSAL AVIONICS SYSTEMS, EFI-890R, UNS1LW, ASU, SSDTU, AND...

Installation of Universal Avionics Systems, EFI-890R, UNS1Lw, ASU, SSDTU, and RCU, Cobham Audio Control Panels, L3 Communications ESIS, WSI AV-350 and Astro-Med. Printer in accordance with AMES, Inc. Master Data List, Report No. 46220MDL01, Revision E, dated August 09, 2011, or later FAA approved revision.
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INSTALLATION OF A CARGO LOADING SYSTEM IN ACC WITH MDL...

Installation of a Cargo Loading System in acc with MDL 2337 rev X dated12/07/2010Modification of the STC FAA SA2971SO to increase from 121 pax to 148 paxaccording to drawing 90945-507/607 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.
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INSTALLATION OF AN INTERIOR MODIFICATION INCLUDING GALLEY AND LAVATORY AND...

Installation of an interior modification including galley and lavatory and passenger seat rearrangement.
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INSTALLATION OF A SUNDSTRAND MARK V GROUND PROXIMITY WARNING SYSTEM...

Installation of a Sundstrand Mark V ground proximity warning system with reactive windshear.
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INSTALLATION OF AN INTERIOR MODIFICATION INCLUDING GALLEY, DIVIDERS, STOWAGE CLOSETS,...

Installation of an interior modification including galley, dividers, stowage closets, and passenger seat rearrangement.
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APPROVAL OF MAXIMUM ZERO FUEL WEIGHT INCREASE. (737-200 SERIES S/N'S...

Approval of maximum zero fuel weight increase. (737-200 SERIES S/N'S 20549, 22002, 22540)
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MODIFICATION OF FLOOR IN ACCORDANCE WITH PEMCO WORLD AIR SERVICES,...

Modification of floor in accordance with Pemco World Air Services, Inc. Master Data list, Report No. 2316, revision “K”, dated June15, 2006, or later EASA approved revision. Limitations: Instructions for Continued Airworthiness (ICA), Pemco Report No 2917, Revision C, dated January 18, 2006, or later EASA approved revision, is a required part of this STC, and must be incorporated into the operator’s maintenance program.. Conditions: n/a
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INSTALLATION OF A CARGO DOOR IN ACCORDANCE WITH PEMCO WORLD...

Installation of a cargo door in accordance with Pemco World Air Services, Inc. Master Data list, Report No. 2373, revision “T”, dated June 15, 2006, or later EASA approved revision. Limitations: - Airplane Flight manual Supplement (AFMS), Report P03-003FM Rev 7, or later EASA approved revision.- Instructions for Continued Airworthiness (ICA), Pemco Report No 2917, Revision C, dated January 18, 2006, or later EASA approved revision, ...
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INSTALLATION OF A CLASS “E” CARGO COMPARTMENT AND PASSENGER INTERIOR...

Installation of a Class “E” Cargo Compartment and passenger interior configuration in accordance with with Pemco World Air Services, Inc. Master Data list, Report No. 2374, revision “S”, dated June 15, 2006, or later EASA approved revision. Limitations: - Airplane Flight manual Supplement (AFMS), Report P03-003FM Rev 7, dated April 27th 2007 or later EASA approved revision.- Instructions for Continued Airworthiness (ICA), Pemco Report No 2917, ...
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INSTALLATION OF CLASS 'E' CARGO COMPARTMENT AND 9G RESTRAINT BARRIER,...

Installation of class 'E' cargo compartment and 9g restraint barrier, a 170 passenger interior, and six passenger/cargo combinations.
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MODIFICATION TO THE FLAP CONTROL SYSTEM TO PROVIDE A MAXIMUM...

Modification to the flap control system to provide a maximum landing flap of 40 degrees in the normal case and an optional stop in the flap position quadrant to restrict the full landing position to 40 degrees.
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INSTALLATION OF NOISE ATTENUATION EQUIPMENT IN EITHER OR BOTH ENGINE...

Installation of noise attenuation equipment in either or both engine nacelles. (DC-9-10 SERIES w/P&W JT8D-7, -9, or -11 engines)
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