MODIFICATIONS OF H4 Aerospace (UK) Ltd. (47)

ADS-B OUT UPGRADE B777

ATC Transponder Upgrade for ADS-B for Boeing 777 Model: 777-200, 777-200R, 777-300, 777-300R, 777F    
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TCAS SYSTEM UPGRADE TO TPA-100B WITH VERSION 7.1 FOR HONEYWELL...

Installation of TCAS system upgrade from TPA-81A TCAS II with software version 7.0 or TPA-100A TCAS II to TPA-100B with software version 7.1 for Honeywell System
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MOD. H4A1804 ISSUE 1 - PALLETISED BUSINESS CLASS SEAT CONFIGURATIONS...

MOD. H4A1804 Issue 1 - Palletised Business Class Seat Configurations onAirbus A319:Initial configuration B: 48 BusinessClass SeatsFinal configuration A: 50 Business Class Seats
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AIRBUS A319 CABIN WIFI SYSTEM INSTALLATION FOR IFE STREAMING

Airbus A319 Cabin WiFi System Installation for IFE streaming
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INSTALLATION OF LED WASH LIGHTS

Installation of LED Wash Lights
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B757-200 CABIN WIFI SYSTEM INSTALLATION FOR IFE STREAMING

B757-200 Cabin WiFi System Installation for IFE streaming
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TCAS CHANGE 7.1 ON BOEING DC9/MD80 SERIES/HONEYWELL TPA-100B TCAS IITRAFFIC...

TCAS Change 7.1 on Boeing DC9/MD80 Series/Honeywell TPA-100B TCAS IItraffic computerinstalled in place of the existing Honeywell TPA-81A computer in thesame location. The originaltray remains. TPA-100B is fully compliant with ETSO-119c including bothRTCA/DO-185B forTCAS II change 7.1
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TCAS SYSTEM UPGRADE TO CHANGE 7.1 ON BOEING MD 90-30/B717-200...

TCAS System Upgrade to Change 7.1 on Boeing MD 90-30/B717-200 seriesAircraft
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HONEYWELL TCAS 7.1 SYSTEM UPGRADE ON BOEING 747 AIRCRAFT FOR...

Honeywell TCAS 7.1 System Upgrade on Boeing 747 Aircraft For HoneywellSystems.
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TCAS SYSTEM UPGRADE TO CHANGE 7.1 ON AIRBUS A340 SERIES...

TCAS System Upgrade to change 7.1 on Airbus A340 series aircraft
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A320/A321 BRAND PANEL AND MAGAZINE RACK INSTALLATION ON MONUMENTS

A320/A321 Brand Panel and Magazine Rack Installation on monuments
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TCAS SYSTEM UPGRADE TO CHANGE 7.1 ON BOEING 737 AIRCRAFT...

TCAS System Upgrade to Change 7.1 on Boeing 737 Aircraft for HoneywellSystems
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CHANGE OF WING FUEL TANK PUMP RELAYS TO GFI TYPE...

Change of Wing Fuel Tank Pump Relays to GFI type on Boeing 757-200Boeing SB -757-28A0078 changes the Wing and Centre Tank Fuel Pump relaysto a GFI type. This STC is dedicated to aircraft that have already hadthe Centre Tank Relays changed to the UFI type (per FAA approved TDGAerospace STC ST01950LA)...
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INSTALLATION OF TCAS SYSTEM UPGRADE FROM TPA-81A WITH SOFTWARE VERSION7.0...

Installation of TCAS system upgrade from TPA-81A with software version7.0 to TPA-100B with software version 7.1 on UralAirways Airbus A320and A321 a/c for Honeywell System
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INTRODUCTION OF LED BASED LOGO LIGHTS ON AIRBUS A330 AND...

Introduction of LED based logo lights on Airbus A330 and A340 aircraft.This STC replaces the original logo lights by LED logo lights. Limitations: Modification summary sheet, ref : H4A1391 Issue 2Instruction for Continued Airworthiness, ref : H4ADR611 Issue 1or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of this design change it must be determined that the interrelationship between this ...
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INSTALLATION OF ASTRONICS EMPOWER ISPS SYSTEM[INSTALLATION OF ASTRONICS EMPOWER ISPS...

Installation of Astronics EmPower ISPS system[Installation of Astronics EmPower ISPS system for European AviationC2C20755 seats into B757-200 aircraft] Limitations: - Modification Summary and Declaration of Compliance, H4 Aerospace document No. H4A1483, Issue 5, dated 10 May 2013- Aircraft Maintenance Manual Supplement, H4 Aerospace document No.H4AMS071, Revision 4, dated 10 May 2013or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of ...
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STRETCHER INSTALLATION AND AIRCRAFT CABIN RECONFIGURATION. LIMITATIONS: EASA STC 10043300H4...

Stretcher installation and Aircraft cabin reconfiguration. Limitations: EASA STC 10043300H4 Aerospace Modification Summary and Declaration of Compliance No. MODH4A1567 Issue 4 dated 10 March 2013H4 Airplane Flight Manual Supplement No. H4AFMS028H4 Instructions for Continued Airworthiness No. H4ADR739or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of this design change it must be determined thatthe interrelationship between this design change and ...
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CABIN RE-CONFIGURATION AND AIRVOD IFE SYSTEM INSTALLATION LIMITATIONS: NONE. CONDITIONS:...

Cabin Re-configuration and Airvod IFE System Installation 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 NEW CABIN INTERIOR AS DEFINED IN H4ACP075 LIMITATIONS:...

Installation of new cabin interior as defined in H4ACP075 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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INTRODUCTION OF AN AD AEROSPACE COCKPIT DOOR AND CABIN SURVEILLANCESYSTEM...

Introduction of an AD Aerospace Cockpit Door and Cabin SurveillanceSystem on Boeing B767 200/300. 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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PASSENGER CABIN RECONFIGURATION ON OPENSKIES B757 LIMITATIONS: NONE. CONDITIONS: NONE

Passenger cabin reconfiguration on Openskies B757 Limitations: None. Conditions: None
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INTRODUCTION OF COCKPIT DOOR SURVEILLANCE AND CABIN WITNESS SYSTEM LIMITATIONS:...

Introduction of Cockpit Door Surveillance and Cabin Witness System 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 GEVEN 'NOVA' & 'PUMA' SERIES PASSENGER SEATS 326YCONFIGURATION....

Installation of Geven 'Nova' & 'Puma' Series Passenger Seats 326Yconfiguration. Limitations: Limited to installation on B767-31K Serial Numbers 27205, 27206 and28865.. Conditions: None.
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INSTALLATION OF GEVEN PIUMA SEATS AS DEFINED IN H4ACP076 LIMITATIONS:...

Installation of Geven Piuma Seats as defined in H4ACP076 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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INTRODUCTION OF AN AEROSPACE COCKPIT DOOR AND CABIN SURVEILLANCE ONBOEING...

Introduction of an Aerospace Cockpit Door and Cabin Surveillance onBoeing 777-200. 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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ACTIVATION OF NICEMATE WLAN SYSTEM CERTIFICATION BASIS EASA.IM.A.009THE CERTIFICATION BASIS...

Activation of Nicemate WLAN System Certification Basis EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) Limitations H4 Aerospace Modification Summary No. MOD H4A1334 Issue 4 dated 05 May2011.H4 AFMS No. H4AFMS023H4 ICA No. H4ADR528or later revisions of the above listed documents approved by EASA ...
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INSTALLATION OF A CABINVU-123 COCKPIT DOOR MONITORING SYSTEM AND AFLIGHTVU...

Installation of a CabinVu-123 Cockpit Door Monitoring System and aFlightVu Witness Cabin Surveillance System in accordance with H4Aerospace Modification Summary document nr. H4A1333 Rev. 1, dated 18 052010 or later approved revision. Limitations: None. Conditions: H4AFMS022 Flight Manual Supplement shall be included in the AircraftFlight ManualH4ADR548 Instructions for Continued Airworthiness shall be included inthe aircraft maintenance instructionsPrior to installation of this modification it must be determined ...
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INSTALLATION OF A TWO-CLASS SEATING ARRANGEMENT LIMITATIONS: NOT APPLICABLE. CONDITIONS:...

Installation of a two-class seating arrangement Limitations: Not Applicable. 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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INTRODUCTION OF RECARO ECONOMY PASSENGER SEATS ON BOEING 737-800, INACCORDANCE...

Introduction of Recaro Economy Passenger Seats on Boeing 737-800, inaccordance with project H4A1239(Revision of STC 10027495 to remove EWIS Limitation) Limitations: None. Conditions: The STC is based upon cabin installations as approved under STCEASA.A.S.03836. Applicable documents must be considered.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previo
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INTRODUCTION OF INTERIOR WITH 56 RECARO BUSINESS CLASS SEATS ANDASSOCIATED...

Introduction of Interior with 56 Recaro Business class seats andassociated systems(Revison of STC EASA.A.S.03836 to remove EWIS Limitation) Limitations: - The STC is limited to MSN 33016 (YJ935) and MSN 33021 (YJ936).- Changes to MMEL or MEL are not covered under the STC approval andrequire an additional approval, if deemed necessary.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this ...
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INTERIOR RECONFIGURATION FROM 18 TO 22 PASSENGER CAPACITY ON BOEING737-700...

Interior Reconfiguration from 18 to 22 Passenger Capacity on Boeing737-700 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
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INSTALLATION OF RUNWAY TURNOFF AND LOGO LIGHTS. MINOR CHANGE TO...

Installation of Runway Turnoff and Logo Lights. Minor Change to EASA STC10029103, Rev.1 issue date 31.03.2010 granted to H4 Aerospace (UK) Ltd.Minor change approval is sought to reflect the up issue wording of theinstructions of continued airworthiness inc Limitations: Restricted to the aircraft listed in doc. N° H4ADR530 - MasterEffectivity List for Goodrich RTO and Logo Light Installation.. Conditions: Prior to installation of this modification it ...
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INSTALLATION OF LIFEPORT STRETCHER. LIMITATIONS: NONE.. CONDITIONS: PRIOR TO INSTALLATION...

Installation of Lifeport Stretcher. Limitations: None.. Conditions: Prior to installation of this modification the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product.The installatio
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GUEST/STAFF SEATING AREA RECONFIGURATION & MISC CABIN ITEMS FOR A320-232...

GUEST/STAFF SEATING AREA RECONFIGURATION & MISC CABIN ITEMS FOR A320-232 AIRCRAFT as defined in H4ACP057.Model: Airbus A320-232 MSN 2403, A6-DLM Limitations: Approval valid only for MSN 2403.The use of the aircraft is limited to non-commercial operation only. For other Limitations refer to Flight Manual Supplement H4AFMS019.. Conditions: n/a
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INSTALLATION OF GSM PHONE / SATCOM SYSTEM ON B737-800 AIRCRAFT....

Installation of GSM Phone / SATCOM system on B737-800 aircraft. Limitations: 1. 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.2.. Conditions: n/a
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IMPLEMENTATION OF INTERIOR CHANGES ASSOCIATED WITH THE CABINRECONFIGURATION FROM 124YC...

Implementation of Interior Changes associated with the cabinreconfiguration from 124YC to 126YC. Limitations: Prior to installation of this modification the installer must determine that theinterrelationship between this modification and any other previously installedmodification will introduce no adverse effect upon the airworthiness of theproduct.The installatio. Conditions: n/a
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INSTALLATION OF A SATCOM ANTENNA FOR A GSM SYSTEM ON...

Installation of a Satcom Antenna for a GSM system on B737-800 Limitations: As in Instrucions for Continued Airworthiness H4ADR259 Issue 1 or later EASA approved revision.. Conditions: n/a
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THE CABIN RECONFIGURATION OF B767-300 AIRCRAFT WITH BRICE B1000S SEATS...

The cabin reconfiguration of B767-300 Aircraft with Brice B1000S seats for TUI ARKEFLY/This modification removes the existing 260 economy class seats and installs 260 new Brice B1000s economy class seats in an identical passenger layout. Limitations: Continued Airworthiness Manual, Ref. No. ML3263, Rev. A.This approval is limited to only the installation made in the Boeing Models B767-300, S/N 24477, S/N 24847, S/N 24848 aircraft.. Conditions: n/a
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