04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10039114 PARKER HANNIFIN CORPORATION FAA STC SA619GL 1. C90A, C90GT, C90GTI EASA Validation of FAA STC
None Prior to installation of this modification it 10.04.2012
2. 65-90, 65-A90
SA619GLInstallation of Parker Hannifin Main
must be determined thatthe
2. 65-A90-1 (JU-21A)
Wheel and Brake Conversion Kit PartNumbers
interrelationship between this modification
2. 65-A90-4 (RU-21E, RU-21H) 199-90 in accordance with Parker Hannifin
and any other previouslyinstalled
2. B90, C90, E90, H90 (T-44A) Conversion KitInstallation Manual IM 199-90,
modification and/ or repair will introduce
Revision J, dated January 7, 2009, orlater FAA
no adverse effectupon the airworthiness
approved
of the product.
10033420 PARMA-TECHNIK, S.R.O. 1. M 137A, M 137AZ
2. M 332, M 332A, M 332AK
3. M 337, M 337A, M 337AK
Prolongation of TBO for the M137, M332 and
M337 engines in serviceaccording to the
procedure No. WMS - OS/09/04 (Definition
document)under the AP DOA Parma Technik
organization No. M332, 137, 337/001
10037491 PATS AIRCRAFT L.L.C. FAA STC ST01725NY-D B737-900ER Installation of ten auxiliary fuel tank system
configurationsValidation of STC ST01725NY-D
Approved configurations are the following:
Configuration 1: ,,Installation of a Five-Cell
Auxiliary Fuel System inthe forward and aft
cargo compartments in accorda
10027222 PATS AIRCRAFT LLC P-
EASA.IM.A.S.03142
10027223 PATS AIRCRAFT LLC P-
EASA.IM.A.S.03235
REV. 1 FAA STC ST00365NY-D CL-600-2B19 Revisions to Auxiliary Fuel System Structural
Provisions
none none 19.01.2011
Configurations 1 & 5:,,PATS Aircraft, LLC.
Airplane Flight ManualSupplement No. 221 for
a Five-Cell (1 Fwd/4 Aft) Auxiliary Fuel
System,revision IR dated January 30, 2009 is
required. Approved for aircraftwith NGS.
Configurations 2 & 6:,,PATS Aircraft, L
PATS Aircraft, LLC. Airplane Flight Manual
Supplement No. 200, RevisionB, FAA
approved 11 June 2009, is required with
configurations 5 and 6.
REV. 2 FAA STC ST01730NY-D CL-600-2B19 Installation of an Executive Interior In this installation the maximum passenger
seating capacity is limitedto 15.
10016198 PEMCO WORLD AIR SERVICES EASA.IM.A.S.02438 REV. 2 FAA STC SA2968SO BOEING 737-400 Modification of floor in accordance with Pemco
World Air Services, Inc. Master Data list,
Report No. 2316, revision “K”, dated June15,
2006, or later EASA approved revision.
10016199 PEMCO WORLD AIR SERVICES EASA.IM.A.S.02439 REV. 2 FAA STC SA2969SO BOEING 737-400 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.
10016200 PEMCO WORLD AIR SERVICES EASA.IM.A.S.02440 FAA STC SA2970SO BOEING 737-400 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.
10035332 PEMCO WORLD AIR SERVICES EASA STC 2004-
3750
REV. 1 FAA STC SA2971SO B737-300 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
10016480 PENTASTAR AVIATION, L.L.C. EASA.IM.A.S.02832 FAA STC ST01759CH FALCON 50
FALCON 900
FALCON 900EX
Instructions for Continued Airworthiness (ICA),
Pemco Report No 2917, Revision C, dated
January 18, 2006, or later EASA approved
revision, is a required part of this STC, and
must be incorporated into the operator’s
maintenance program.
- 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
- 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
EASA Validation of FAA approved STC 1. See those of original FAA STC
ST01759CHUpgrade of a Rockwell Collins ST01759CH.2. Prior to installation of this
SAT-906 SATCOM system by modification of modification the installer must determine that
Rockwell Collins SDU-906 Satellite Data Unit the interrelationship between this modification
and HPA-901A High Power Amplifier and the and any other previously installed modification
installation of a Rockwell Collins HST-900 High will introduce no adverse effec
Speed
Prior to installation of this modification it 12.12.2011
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.
Prior to installation of this modification it 12.07.2012
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.
Prior to installation of this modification it 12.07.2012
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.
24.06.2008
24.06.2008
07.05.2007
None 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.
16.06.2011
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