MODIFICATIONS OF GDCTechnics (17)

HONEYWELL KA-BAND JETWAVE HARDWARE

The GDC Group has announced her progress on its development of the Supplemental Type Certificates (STC) for the installation of the Honeywell’s Ka-Band JetWave hardware on different Boeing and Airbus aircraft. The FAA/EASA STC's will be finalized during the 1st quarter of 2017 and the aircraft types that are involved include those in Boeing Business Jet, Airbus Corporate Jet and Commercial configuration. 
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INTERIOR CHANGE

This modification has a Minor Change approval and consists of: Replacement of carpets in the cockpit and cabin area Replacement of upper cabin RH side panel Limitations/Conditions: This modification is MSN limited
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EXCHANGE OF SEAT COVERS

This modification has a Minor Change approval and includes: Exchange of seat covers from fabric to leather cover. Limitations/Conditions: This modification is MSN limited
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INSTALLATION OF WATER TANK RACK

This modification has a Minor Change approval and includes: Installation of an water tank rack in the aft bulk cargo compartment   Limitations/Conditions: This modification is MSN limited
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SATCOM SYSTEM UPGRADE AND INSTALLATION OF NEW CORDLESS PHONES

This modification has an minor change approval and includes: Replacement of existing High Gain Antenna and Diplexer/Low Noise Amplifier (D/LNA) Replacement of High Power Amplifier (HPA) Replacement of High Speed Data Unit (HSU) Replacement of Satellite Data Unit (SDU) Replcement of Cabin Telecommunication Unit Installation of Remote Ethernet Switch Installation of ePhone docking station and handset Modification of wiring Modification of furniture Installation of Interface Panel ...
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INTERIOR CHANGE

This modification has a Minor Change approval and consists of: Replacement of carpets in the cockpit and cabin area Replacement of upper cabin RH side panel Limitations/Conditions: This modification is MSN limited
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CABIN INTERIOR CHANGE

This Cabin Interior Change includes: A new LOPA in the economy class only, including ETSO seats with ebedded LCD and in-seat power supply A new In-Flight Entertainment System for the whole aircraft including a control monitor unit for the cabin attendants, extra fixed LCD monitors for passenger addressing also in business class Various other items in the cabin (carpet, tedlar, curtains, blinds) Limitations/Conditions: This STC is ...
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STRUCTURAL PROVISIONS OF PATIENT TRANSPORT COMPARTMENT (PTC)

This modification includes: Structural provisions of Patient Transport Compartment (PTC) Installation of a Oxygen Discharge Indicator   Limitations/Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/or repair will introduce no adverse effect upon the airworthiness of the product. 
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INSTALLATION OF A WLAN SYSTEM

The STC installs a new WLAN system in replacement of an existing one. The system includes: An airborne unit WLAN access points  Indication panel in the cabin Switch in the cockpit Limitations/Conditions: This STC is MSN limited
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INTEGRATION OF A FLIGHT INSPECTION SYSTEM

This modification includes: Installation of an additional set of antennas, Installation of an Observer Console in the cabin Installation of additional controls and displays in the cockpit dedicated to Flight Inspection Mission Limitations/Conditions: This STC is MSN limited
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STRUCTURAL PROVISIONS FOR VIP CABIN COMPLETION AND FOR INSTALLATION OF....

This modification includes: Structural provisions for VIP Cabin Completion Installation of fin camera Installation of belly camera Installation of iridium sat antenna Installation of door locks Installtion of a avionic rack   Limitations/Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/or repair will introduce no adverse effect upon ...
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STRUCTURAL PROVISIONS FOR 747-8I BELLY CAMERA INSTALLATION BETWEEN THE NLG...

Structural provisions for 747-8i belly camera installation between the NLG bay and the belly fairing at the lowest point of the fuselage. It contains: Attachment to the aircraft structure through brackets Outside fairing Installation of a wiring feed-through Limitations/Conditions: none
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GENERAL FIN CAMERA INSTALLATION ON AIRBUS A319

General Fin Camera Installation on Airbus A319 Limitations/Conditions: This design change approval is MSN limited
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GENERAL FIN CAMERA INSTALLATION ON AIRBUS A319

General Fin Camera Installation on Airbus A319 Limitations/Conditions: This design change approval is MSN limited
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STRUCTURAL PROVISIONS FOR 747-8I BELLY CAMERA INSTALLATION BETWEEN THENLG BAY...

Structural provisions for 747-8i belly camera installation between theNLG bay and the belly fairing at the lowest point of the fuselage. Itcontains:- Attachment to the aircraft structure through brackets- Outside fairing- Installation of a wiring feed-thro 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 ...
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