Airborne Maintenance & Engineering Services offers Automatic Dependent Surveillance-Broadcast (ADS-B) modifications on Boeing 757, 767-200, and 767-300 aircraft.
The Airborne solution includes many cost-saving features while minimizing aircraft downtime and upgrade expense to comply with Satellite Based Augmentation System (SBAS) requirements mandated by the FAA for 2025.
Installation of an ACSS Surveillance Processor, Mode-S Datalink Transponders and associated components with ADS-B Out provisions
Installation of a seat-back In-Flight-Entertainment (IFE) system
Relocation of the Auxiliary Power Unit (APU) Electronic Control Unit (ECU) from the E6 rack in the A
Modification to the flap control system to provide a maximum landing flap of 40 degrees in the norma
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)
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...
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.
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, Revision C, dated January 18, 2006, or later EASA approv.
Conditions: n/a
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, is also a.
Conditions: n/a