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 />
10029679 WIPAIRE Inc. FAA STC SA1470GL 1) CESSNA 206H, T206H Installation of right front cabin door in None Prior to installation of this modification it 12.<strong>04</strong>.2<strong>01</strong>0<br />
2) CESSNA 206, P206, P206A, accordance with Wipaire, Inc.installation<br />
must be determined thatthe<br />
P206B, P206D, P206E, U206, drawing number 3D1-11<strong>01</strong><br />
interrelationship between this modification<br />
TP206C, TP206D, TU206C,<br />
and any other previouslyinstalled<br />
TU206D<br />
modification and/ or repair will introduce<br />
TU206E, TU206F, TU206G<br />
no adverse effectupon the airworthiness<br />
U206A, U206B, U206C, U206D,<br />
U206E, U206F, U206G, TP206A,<br />
of the product.<br />
10030272 WIPAIRE Inc. FAA STC SA00059WI CESSNA 208, 208B Installation of the Wipaire Single Point Fueling None Prior to installation of this modification it 08.06.2<strong>01</strong>0<br />
System on Cessna 208i.a.w. FAA STC<br />
must be determined thatthe<br />
SA00059WI<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 />
10031133 WIPAIRE Inc. FAA STC SA02808CH DHC-6-200, -300 Installation of nine passenger executive seating<br />
system in accordancewith FAA STC<br />
SA02808CH<br />
10032352 WIPAIRE Inc. P-<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>058<br />
FAA STC SA<strong>01</strong>916CH AIR TRACTOR AT-802, AT-802A Installation of vortex generators. Installation of<br />
Wipaire stallimprovement array in accordance<br />
with Wipaire installation drawing No.7A1-4407<br />
Revision B, dated April 27,2<strong>01</strong>0 for the AT-<br />
802A model andinstallation drawing No.<br />
10<strong>04</strong>245, Revision B, dated April<br />
10<strong>04</strong>1960 WIPAIRE Inc. FAA STC SA1311GL CESSNA 208 Modification of Cessna 208 in accordance with<br />
FAA STC SA1311GL:1) Installation of Wipaire<br />
Model 8000 Amphibian/Seaplane floats or2)<br />
Installation of Wipaire Model 8750<br />
Amphibian/Seaplane floats andinstallation of<br />
vortex generators iaw. Wipaire STC SA270CH<br />
(<br />
10<strong>01</strong>5702 WORLDWIDE AIRCRAFT SERVICES Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>69 REV. 1 AEROSPATIALE ATR 42-200<br />
AEROSPATIALE ATR 42-300<br />
AEROSPATIALE ATR 42-320<br />
AEROSPATIALE ATR 42-500<br />
AEROSPATIALE ATR 72-1<strong>01</strong><br />
AEROSPATIALE ATR 72-102<br />
AEROSPATIALE ATR 72-2<strong>01</strong><br />
AEROSPATIALE ATR 72-202<br />
AEROSPATIALE ATR 72-211<br />
AEROSPATIALE ATR 72-212<br />
AEROSPATIALE ATR 72-212A<br />
10<strong>01</strong>5808 WORLDWIDE AIRCRAFT SERVICES Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>877 FAA STC ST00798WI FAIRCHILD SWEARINGEN SA<br />
227-AC<br />
FAIRCHILD SWEARINGEN SA<br />
227-AT<br />
FAIRCHILD SWEARINGEN SA<br />
227-BC<br />
FAIRCHILD SWEARINGEN SA<br />
227-CC<br />
FAIRCHILD SWEARINGEN SA<br />
227-DC<br />
Passenger to all cargo conversion of ATR-42/-<br />
72 series aircraft.ATR-42 is modified in<br />
accordance with Worldwide Aircraft Services<br />
Master Drawing List DL42-25-0<strong>01</strong> Rev G dated<br />
JAN 22, 20<strong>04</strong>.ATR-72 is modified in<br />
accordance with Worldwide Aircraft Services<br />
Ma<br />
Installation of Fairchild Digital Flight Data<br />
Recorder F800 or F1000 in Fairchild aircraft<br />
SA227-AT, -AC, BC, CC, DC in accordance<br />
with Worldwide Aircraft Services Certification<br />
Drawing list No; DL227-31-06 Revision A,<br />
dated May 14, 1999 or later approved<br />
100319<strong>01</strong> WORLDWIDE AIRCRAFT SERVICES Inc. FAA STC SA4872SW SA226-T, SA226-AT Installation of 2 Garrett AiResearch engines<br />
Model TPE 331-10UA-5<strong>01</strong>G orTPE 331-10UA-<br />
511G<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.<br />
28.07.2<strong>01</strong>0<br />
FAA STC No. SA<strong>01</strong>916CH "Limitations and<br />
conditions”, amended May 24, 2<strong>01</strong>0<br />
1.,,Airplanes not incorporating STC SA270CH,<br />
with Model 8000 floats: Airspeed Limits:,,VA at<br />
8000 lbs. = 143 KIAS Maximum Weight:,,8000<br />
lbs. ,,Take off and Flight ,,7800 lbs. ,,Landing<br />
(Water and Land) ,,8035 lbs.,,Ramp ,,,, C.G.<br />
Range,,Take off and Flight<br />
The FAA approved Airplane Flight Manual<br />
Supplement must be on board the aircraft at all<br />
times.This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
othe<br />
Prior to installation of this modification it 05.11.2<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 />
Prior to installation of this modification it 26.10.2<strong>01</strong>2<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 />
24.11.2005<br />
02.11.2007<br />
according limitation section of AFM-S 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.If the<br />
21.09.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 461/<strong>462</strong>
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