BOEING 747 MODIFICATIONS (19)

SBAS / GNSS Aircraft Integration by Fokker Services

Global Navigation Satellite System (GNSS) refers to a constellation of satellites providing signals from space that transmit positioning and timing data to GNSS receivers. The receivers then use this data to determine position, altitude, time, and velocity. This performance can be improved by regional satellite-based augmentation systems (SBAS).

SBAS improves the accuracy and reliability of GPS information by correcting signal measurement errors and by providing information about the integrity of its signals.  SBAS is essential for applications where accuracy and integrity are critical. SBAS is a key enabler of Performance Based Navigation (PBN) usage for Automatic Dependent Surveillance-Broadcast (ADS-B) and Localizer Performance with Vertical Guidance (LPV).

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Underwater Locator Device - ULD - Fokker Services

Events related to aircraft missing over oceanic areas have led to several new requirements, amongst which is the introduction of a long-range Underwater Locator Device (ULD).

The ULD low frequency (8.8kHz) technology is used to increase the range at which aircraft submerged wreckage can be located.

It will be mounted on the aircraft structure free of sound absorbent materials and not in wing sections or empennage. The installation is in accordance with ARINC specification 667, which describes the removal, installation and maintenance aspects of an ULD installation.

Note that the ULD is not to be confused with the Underwater Locator Beacons (ULB) as installed on the CVR and FDRs. The ULD is complementary to the ULB and is mounted to the aircraft structure.

ICAO states that by January 1st 2018 aircrafts flying long range over water with a MTOW>27.000 kg must be equipped with an ULD. Long range over water is determined by the exceedance of the distance from a suitable emergency landing spot. The distance corresponds to 120 min at cruise speed or 400NM whichever is the lesser.

EASA states that by January 1st 2019 Passenger aircraft flying long range over water with a MTOW>27.000 kg and cargo aircraft with MTOW > 45.500kg must be equipped with an ULD. Long range over water is determined by a distance >180 NM from shore.

CARS 121 MOS 11.64 states that aircraft with a MTOW>27.000 kg carrying a life raft should have an ULD by December 2, 2023.

Other authorities have accepted similar rules.

Contact Fokker Services for other aircaft types.

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Conditions for the Permit to Fly

Under certain circumstances, special conditions are required to operate the aircraft, for example maintenance reposition flight. A non EASA aircraft manufacturer may issue a No Techical Objection (NTO) or similar statement.

This may need to be processed by a DOA organisation before it can be presented to EASA or local office for the application for a Permit to Fly.

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Conditions for the Permit to Fly

Under certain circumstances, special conditions are required to operate the aircraft for for example maintenance reposition fligth. A non EASA aircraft maufacturer may issue No techical objection orsimilar statement.

this may need to be processed by a DOA organisation before it can be presented to EASA or local office for the application for a Permit to Fly.

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Installation of Aerocon On-Board Airstairs

Installation of Aerocon On-Board Airstairs provide a VIP-class boarding experience without the need for ground support equipment.

Aircraft: Boeing 747-400

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EAD installed Honeywell Weight and Balance System (WBS) on B747-400...

EAD installed Honeywell Weight and Balance
System (WBS) on B747-400 in accordance
with EAD Master Data List 01021-FAA-A-MDL, rev. E, or later EASA-approved revision.This STC is a validation of FAA STC ST02267CH
Limitations: 1. This on board weight and balance system is considered an advisory systeem and is not certified as the primary means of calculating the aircraft's weight and balance.2. EASA approved Airplane Flight Manual Supplement, EAD document 01021-FAA-A-AFM-01, Rev.
Conditions: n/a

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Installation of a Solid State Cockpit Voice Recorder and Control...

Installation of a Solid State Cockpit Voice Recorder and Control Unit in Boeing 747-100 and –200 series aircraft per ATL Master Document List MDL-11053-00001 at Issue 1 or later approved revisions. EASA.A.S.03698

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Installation of Precise Flight Pulselite Control Unit in landing/taxi system....

Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)

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Integrator

Automatically exchanging information between systems is of great operational advantage as people have all information available at any time. ExSyn Integrator is designed to create the interfaces required between systems in order to exchange this information between different systems and platforms.

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