04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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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 />
10<strong>01</strong>5853 PETERSEN AVIATION, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>956 FAA STC SA00328WI REIMS AVIATION CESSNA F- Operation of airplane on leaded and unleaded Limited to those airplanes equipped with<br />
24.<strong>04</strong>.2006<br />
172N<br />
automotive gasoline, 91 minimum antiknock gravity fuel feed to the carburetor and STC<br />
index (RON + MON) / 2 per ASTM<br />
certificated or approved engine installation. All<br />
SpecificationD-439. Intermixing with aviation engines must have separate approval for<br />
gasoline also approved.<br />
operation on automotive gasoline in the form of<br />
Supplemental or Type Certificte a<br />
10<strong>01</strong>5854 PETERSEN AVIATION, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>957 FAA STC SA2600CE CESSNA 172D<br />
Operation of airplane on leaded and unleaded Limited to those airplanes equipped with<br />
20.<strong>04</strong>.2006<br />
CESSNA 172E<br />
automotive gasoline, 91 minimum antiknock gravity fuel feed wing fuel tanks as the main<br />
CESSNA 172F<br />
index (RON + MON) / 2 per ASTM<br />
fuel supply to the carburetor and certificated<br />
CESSNA 172G<br />
SpecificationD-439. Intermixing with aviation (original or STC) or approved engine<br />
CESSNA 172H<br />
gasoline also approved.<br />
installations. All engines must have separate<br />
CESSNA 172I<br />
CESSNA 172K<br />
CESSNA 172L<br />
CESSNA 172M<br />
CESSNA 172N<br />
CESSNA 172P<br />
approval for operation on automative ga<br />
10<strong>01</strong>6291 PETERSEN AVIATION, INC. <strong>EASA</strong>.IM.A.S.02586 FAA STC SA2660CE PA-28-160, PA-28-161,<br />
Operation of Piper airplanes with automotive 1. Limitations as established in FAA STC<br />
10.09.2007<br />
PA-28-180, PA-28-181<br />
gasoline in accordance with FAA STC SA2660CE, dated April 29, 2005 are<br />
SA2660CE, dated April 29, 2005.<br />
applicable.2. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modification<br />
and any other previously installed<br />
10<strong>01</strong>6690 PETERSEN AVIATION, INC. <strong>EASA</strong>.IM.E.S.<strong>01</strong>002 FAA STC SE00663WI LYCOMING ENGINES O-540-<br />
F1B5<br />
1003<strong>04</strong>24 PETERSEN AVIATION, INC. P-<br />
<strong>EASA</strong>.IM.A.S.03224<br />
10033096 PETERSEN AVIATION, INC. FAA STC SA2670CE 1. A-1, A-1A, A-1B<br />
2. A-1C-180<br />
FAA STC SA00214WI CESSNA F182P Operation of airplane on unleaded automotive<br />
gasoline, 87 minimumantiknock index and<br />
leaded automotive gasoline, 88 minimum<br />
antiknockindex (RON + MON) /2 per ASTM<br />
Specification D-439 in acc. to FAA<br />
STCSA00214WI.<br />
Air Conditioning System for Agusta A 119FAA This approval should not be extended to<br />
STC SR0<strong>04</strong>63DE issued on 11th January 2002 rotorcraft of this model on which other<br />
and amended on 24th January 2006- Flight previously approved modifications are<br />
Manual Supplement Doc. N° A119-1 rev. 3 incorporated unless it is determinded that the<br />
dated 14th July 2005 or later approved interrelationship between this change and any<br />
revision.- Instruction for Continued<br />
of those other previously approved modificati<br />
Airworthiness<br />
Operation of airplanes using automotive<br />
gasoline according US STCSA2670CE<br />
1. Limited to those airplanes equipped with<br />
gravity fuel feed to thecarburettor and<br />
certificated (original or STC) <strong>EASA</strong> approved<br />
engineinstallations. All engines must have<br />
separate approval for operation onautomotive<br />
gasoline in the form of Supplemental or<br />
-According limitation section of AFM-S-Limited<br />
to those airplanes equipped with gravity fuel<br />
feed tocarburetor only-Not approved for 82UL<br />
23.02.2006<br />
Prior to installation of this modification it 15.06.2<strong>01</strong>0<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<br />
Conditions as indicated in FAA STC<br />
SA2670CE also apply. Prior to<br />
installation of this modification it must be<br />
or mixtures with 82UL-Limitation as indicated in determined thatthe interrelationship<br />
FAA STC SA2670CE also apply<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce no adv<br />
10<strong>01</strong>4378 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.<strong>01</strong>653 Installation of Dual GNS530 with Dual GI-106A This STC is approved only for the product<br />
10.02.2006<br />
& Dual KNI-582 RMI<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>4430 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.02478 BEECH A36 Installation of Skywatch Traffic Avoidance 07.06.2006<br />
10<strong>01</strong>4589 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.02696 REV. 1 BN2B-26 ISLANDER Installation of GNS530, GNS430 & GMA340. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
24.<strong>04</strong>.2007<br />
10<strong>01</strong>4732 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.02914 CESSNA 560 Installation of Honeywell EGPWSCessna 560 1. Restricted to G-PPLC ASN 560-00592.<br />
24.<strong>01</strong>.2007<br />
G-PPLC ASN 560-0059<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other aircr<br />
10<strong>01</strong>4979 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.03269 Installation of new Avionics. 30.<strong>01</strong>.2008<br />
10<strong>01</strong>5100 PHOENIX AEROSPACE LIMITED <strong>EASA</strong>.A.S.03443 PIPER PA-31 Installation of new Avionics Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
30.09.2008<br />
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