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 />
100320<strong>01</strong> STC TWENTY ONE LIMITED DC-9-11, DC-9-12, DC-9-13, Introduction of Cabin Vu-123 Cabin<br />
None Prior to installation of this modification it 30.09.2<strong>01</strong>0<br />
DC-9-14, DC-9-15, DC-9-15F, Surveillance System<br />
must be determined thatthe<br />
DC-9-21, DC-9-31, DC-9-32,<br />
interrelationship between this modification<br />
DC-9-32 (VC-9C), DC-9-32F,<br />
and any other previouslyinstalled<br />
DC-9-32F (C-9A, C-9B),<br />
modification and/or repair will introduce<br />
DC-9-33F, DC-9-34, DC-9-34F,<br />
no adverse effectupon the airworthiness<br />
DC-9-41, DC-9-51,<br />
DC-9-81(MD-81),DC-9-82(MD-82),<br />
DC-9-83(MD-83),DC-9-87(MD-87),<br />
MD-88, MD-90-30, 717-200<br />
of the product<br />
10032098 STC TWENTY ONE LIMITED BOMBARDIER CL600-2B19 Removal of Divan Seating Restriction This design change will allow the removal of an<br />
existing limitation onoccupation of the<br />
forwardmost seating position on the installed<br />
divan(<strong>EASA</strong> STC No. <strong>EASA</strong>.A.S.03452 and<br />
<strong>EASA</strong>.A.S.03022 refers). If the arrester block<br />
installation assembly becomes unservic<br />
10032232 STC TWENTY ONE LIMITED CESSNA 206H, T206H Introduction of Stand-By Battery Power Supply<br />
in accordance withS21.MDL-0770, issue 2,<br />
dated 14/10/2<strong>01</strong>0<br />
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 />
07.10.2<strong>01</strong>0<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 />
19.10.2<strong>01</strong>0<br />
10033452 STC TWENTY ONE LIMITED B757-200 Carriage of Horses & Grooms in Freighter a/c This design change is applicable to Boeing 757- Prior to installation of this modification it 21.<strong>01</strong>.2<strong>01</strong>1<br />
200 aircraft convertedunder Boeing's Special must be determined thatthe<br />
Freighter Programme, approved by the UK interrelationship between this modification<br />
CAA underAirworthiness Approval Note AAN and any other previouslyinstalled<br />
27308 (acceptable to <strong>EASA</strong> under the modification and/ or repair will introduce<br />
<strong>EASA</strong>Grandfather provisions).<br />
no adverse effectupon the airworthiness<br />
of the product<br />
10034641 STC TWENTY ONE LIMITED REV. 3 PA-31 Introduction of Chin Mount and re-located Pitot<br />
tubes.<br />
10034714 STC TWENTY ONE LIMITED REV. 1 PA-31 Introduction of an Enlarged Window and<br />
Sensor Turret<br />
Not to be flown in icing conditions with the chin<br />
mount and aerodynamicfairing installed.The<br />
installation of a sensor turret is<br />
prohibited.Limitations as defined in AFMS<br />
S21.FMS-0072 Issue 3.<br />
Limited to aircraft serial numbers 31-7712054<br />
& 31-815 onlyNot to be flown in icing<br />
conditionsLimitations as defined in AFMS<br />
S21.FMS-0077 Issue 1 dated 20/<strong>04</strong>/2<strong>01</strong>1<br />
10034734 STC TWENTY ONE LIMITED REV. 1 PA-31 Introduction of a Belly Pod Not to be flown in icing conditions with the belly<br />
pod installedLimitations as defined in AFMS<br />
S21.FMS-0080 Issue 2 dated 31/10/2<strong>01</strong>2<br />
Prior to installation of this modification it 29.05.2<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 />
Prior to installation of this modification it 27.<strong>04</strong>.2<strong>01</strong>1<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 22.11.2<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 />
10035173 STC TWENTY ONE LIMITED B737-300 Introduction of Number 2 Galley Assembly 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 />
<strong>01</strong>.06.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 424/<strong>462</strong>
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