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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />

10026943 DECRANE AEROSPACE PATS<br />

P-<br />

B737-800 Installation of Auxiliary Fuel System in the None. - Prior to installation of this modification 26.08.2009<br />

AIRCRAFT,<br />

<strong>EASA</strong>.IM.A.S.03257<br />

forward and aft cargocompartments.Validation<br />

the installer mustdetermine that the<br />

of STC ST<strong>01</strong>713NY-D as amended June 29,<br />

interrelationship between this modification<br />

2009<br />

and anyother previously installed<br />

modification will introduce no adverse<br />

effectupon the airworthiness of the<br />

product.- The install<br />

10027297 DECRANE AEROSPACE PATS<br />

AIRCRAFT,<br />

10027298 DECRANE AEROSPACE PATS<br />

AIRCRAFT,<br />

10027299 DECRANE AEROSPACE PATS<br />

AIRCRAFT,<br />

10028092 DECRANE AEROSPACE PATS<br />

AIRCRAFT,<br />

10028093 DECRANE AEROSPACE PATS<br />

AIRCRAFT,<br />

<strong>EASA</strong>.IM.A.S.03026 REV. 3 FAA STC ST<strong>01</strong>727NY-D ERJ 190-100ECJ Major Change to FAA STC ST<strong>01</strong>727NY-D:<br />

Project DAS-GED-P072 / ODA-GED-0<strong>01</strong>-<br />

Installation of Executive Interior (A/C #4)<br />

<strong>EASA</strong>.IM.A.S.03027 REV. 1 FAA STC ST<strong>01</strong>728NY-D ERJ 190-100ECJ Major Change to FAA STC ST<strong>01</strong>728NY-D:<br />

DAS-GED-P067 - Modification of theClass C<br />

Forward Cargo Compartment<br />

<strong>EASA</strong>.IM.A.S.03028 REV. 1 FAA STC ST<strong>01</strong>729NY-D ERJ 190-100ECJ ST<strong>01</strong>729NY-D: Installation of a Passenger<br />

Gaseous Oxygen Supply System<br />

10<strong>01</strong>5980 DEL-AIR <strong>EASA</strong>.IM.A.S.02132 FAA STC SA5733SW CESSNA 150<br />

CESSNA 150A<br />

CESSNA 150B<br />

CESSNA 150C<br />

CESSNA 150D<br />

CESSNA 150E<br />

CESSNA 150F<br />

CESSNA 150G<br />

CESSNA 150H<br />

CESSNA 150L<br />

CESSNA 150M<br />

CESSNA 152<br />

CESSNA A152<br />

FAA STC ST0<strong>04</strong>05LA-D 737-700 IGW Alteration of Fire Protection Systems, Lower<br />

Cargo Compartments. This STC revises and<br />

supersedes LBA STC LBA.21NE1.TA0682.<br />

The revisionwas issued to reflect the transfer<br />

from Hollingshead International toDecrane<br />

Aerospace PATS Aircraft.<br />

FAA STC ST<strong>01</strong>184LA B737-800 Alteration of Fire Protection Systems, Lower<br />

Cargo Compartments. This STC revises and<br />

supersedes LBA STC LBA.21NE1.TA0511.<br />

The revisionwas issued to reflect the transfer<br />

from Hollingshead International toDecrane<br />

Aerospace PATS Aircraft.<br />

Configuration 1: - Concurrent installation of<br />

STC ST<strong>01</strong>728NY-D (Class "C"<br />

CargoCompartment) iaw. Master Drawing List<br />

6071-0000-MDL Rev. IR dtd.7.October 2008 is<br />

required. -Commercial operation under <strong>EASA</strong><br />

rules requires installation of PATS<br />

SBST<strong>01</strong>72NY-D-25-S<br />

Configuration 1: - Concurrent installation of<br />

STC ST<strong>01</strong>727NY-D (Installation of<br />

anExecutive Interior) iaw. Master Drawing List<br />

5950-0000-MDL revision Gdtd. 16.April 2009 is<br />

required Configuration 2: - Concurrent<br />

installation of STC ST<strong>01</strong>727NY-D (Installation<br />

Not Applicable 26.03.2<strong>01</strong>0<br />

Not Applicable 18.09.2009<br />

- Concurrent installation of STC's ST<strong>01</strong>727NY- Not Applicable<br />

D (Installation of anExecutive Interior) and<br />

ST<strong>01</strong>728NY-D (Class "C" Cargo<br />

Compartment) isrequired - For aircraft under<br />

FAA jurisdiction this modification may not<br />

beinstalled after 30.August 2<strong>01</strong>0 unless:(1)<br />

previ<br />

18.09.2009<br />

None. Prior to installation of this modification it<br />

must be determined thatthe<br />

interrelationship between this modification<br />

and any other previouslyinstalled<br />

modification and/ or repair will introduce<br />

no adverse effectupon the airworthiness<br />

of the product.The ins<br />

18.11.2009<br />

Installation of Longe Range Wing Fuel Tanks 1. If the holder agrees to permit another<br />

person to use this certificate to alter the<br />

product, the holder shall give the other person<br />

written evidence of that permission.2. This<br />

STC is approved only for the product<br />

configuration as defined in the app<br />

None. Prior to installation of this modification it<br />

must be determined thatthe<br />

interrelationship between this modification<br />

and any other previouslyinstalled<br />

modification and/ or repair will introduce<br />

no adverse effectupon the airworthiness<br />

of the product.The ins<br />

18.11.2009<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 182/<strong>462</strong><br />

14.08.2006

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