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>7005 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>417 FAA STC SR0<strong>01</strong>25BO MD HELICOPTERS 369A Installation of a Pratt & Whitney Engine 1. Aircraft must have Engine modified in<br />
14.03.2008<br />
MD HELICOPTERS 369D Services. Inc.-Honeywell IntelliStart Plus+TM accordance with <strong>EASA</strong> STC<br />
MD HELICOPTERS 369E Electronic Control System P/N DPU-K- <strong>EASA</strong>.IM.E.S.<strong>01</strong><strong>01</strong>9, FAA STC<br />
MD HELICOPTERS 369F <strong>01</strong>0Note: This STC reflects the transfer from SE00027EN.2. Pratt & Whitney Engine<br />
MD HELICOPTERS 369FF Altair Avionics Corporation to Pratt & Whitney Services, Inc. Rotorcraft Flight Manual DPPU-<br />
MD HELICOPTERS 369H Engine Services, Inc.<br />
T-250-2 dated July 27, 2000 or later approved<br />
MD HELICOPTERS 369HE<br />
MD HELICOPTERS 369HM<br />
MD HELICOPTERS 369HS<br />
MD HELICOPTERS 500N<br />
revision, is required.3. Th<br />
10<strong>01</strong>7006 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>418 FAA STC SR0<strong>01</strong>13BO BELL 206A<br />
Installation of a Pratt & Whitney Engine 1. Aircraft must have engine modified in<br />
14.03.2008<br />
BELL 206B<br />
Services, Inc. - AlliedSignal Aerospace accordance with <strong>EASA</strong> STC<br />
BELL 206L<br />
IntelliStart Plus + TM Electronic Control <strong>EASA</strong>.IM.E.S.<strong>01</strong><strong>01</strong>7, FAA STC<br />
BELL 206L-1<br />
System P/N DPU-K-<strong>01</strong>0Note: This STC SE00026EN.2. Compatibility of this design<br />
BELL 206L-3<br />
reflects the transfer from Altair Avionics change with previously approved modifications<br />
BELL 206L-4<br />
Corporation to Pratt & Whitney Engine must be determined by the installer.3. Pratt &<br />
Services, Inc.<br />
Whitney Engine Serv<br />
10<strong>01</strong>7007 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>419 REV. 1 FAA STC SR0<strong>01</strong>69BO, LBA RC1237 EUROCOPTER DEUTSCHLAND Installation of Pratt & Whitney Engine Services, 1. Required maintenance, as prescribed in the<br />
25.03.2008<br />
BO-105<br />
Inc. SmartCycle+ monitoring and recording applicable airframe or engine Instructions for<br />
EUROCOPTER DEUTSCHLAND system<br />
Continued Airworthiness, shall not be predicted<br />
BO-105D<br />
on the data obtained from the Pratt & Whitney<br />
EUROCOPTER FRANCE AS 350<br />
Engine Services, Inc. monitoring/recording<br />
B<br />
EUROCOPTER FRANCE AS 350<br />
B1<br />
EUROCOPTER FRANCE AS 350<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
EUROCOPTER FRANCE AS<br />
355N<br />
system.2. This system sha<br />
10<strong>01</strong>7008 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>420 FAA STC SR0<strong>01</strong>26BO AND LBA RC 1 BELL 205A-1 Installation of a Pratt & Whitney Engine 1. Pratt & Whitney Engine Services, Inc.<br />
03.03.2008<br />
Services, Inc. SmartCycle Plus System P/N Rotorcraft Flight Manual EMU-T-250-1 dated<br />
EMU-K-<strong>01</strong>0-2<br />
August 31, 2000 or later approved revision, is<br />
required.2. This system is designed as an<br />
electronic aid for recording engine trend and<br />
cycle data. This system does not elim<br />
10<strong>01</strong>7009 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>421 FAA STC SR0<strong>01</strong>18BO, LBA STC RC EUROCOPTER FRANCE AS 350<br />
B<br />
EUROCOPTER FRANCE AS 350<br />
B1<br />
EUROCOPTER FRANCE AS 350<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
10<strong>01</strong>7<strong>01</strong>0 PRATT & WHITNEY <strong>EASA</strong>.IM.R.S.<strong>01</strong>423 FAA STC SR0<strong>01</strong>36BO, LBA RC1176<br />
BA<br />
EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
EUROCOPTER FRANCE AS<br />
355N<br />
Installation of Pratt & Whitney Engine Services,<br />
Inc. SmartCycle Engine Monitoring<br />
System,Part no. CYCLE-K-<strong>01</strong>0<br />
Installation of a Pratt & Whitney Engine<br />
Services, Inc. SmartCycle Twin Engine<br />
Monitoring System Part No. CYCLE-K-<strong>01</strong>0-4<br />
for AS355N and -5 for AS355E, AS355-F,<br />
AS355F1, AS355F2<br />
1. Pratt & Whitney Engine Services, Inc.<br />
Aircraft Flight Manual Supplement for<br />
Eurocopter France, Models, AS-350B, AS-<br />
350B1, AS-350B2, AS-350BA, and AS-<br />
350B3, Doc. No. Cycle-T-250-1, Revision-,<br />
approved April 11, 2000, or later approved<br />
revision, is requ<br />
1. Pratt & Whitney Engine Services, Inc.,<br />
Aircraft Flight Manual Supplement for<br />
Eurocopter France, Models AS355E, AS355-<br />
F, AS355-F1, AS355F2, and AS355N, Doc.<br />
No. CYCLE-T-250-2, Revision-, approved May<br />
22, 20<strong>01</strong>, or later approved revision, is required<br />
with<br />
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