04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015022 GOMOLZIG FLUGZEUG- UND EASA.A.S.03328 CESSNA 401 Alternative Supplemental Inspection Document 1. Alteration to A-SID is subject to written 05.12.2008 MASCHINENBAU CESSNA 401A (A-SID). permission of approval holder.2. This CESSNA 401B modification is only limited to S/N listed in CESSNA 402 EASA approved Gomolzig Document No. CESSNA 402A 17070_Master Aircraft Application Control CESSNA 402B CESSNA 402C CESSNA 411 CESSNA 411A CESSNA 414 CESSNA 414A CESSNA 421 CESSNA 421A CESSNA 421B CESSNA 421C CESSNA 425 List_01122008_ rev0, or later EASA approved 10015027 GOMOLZIG FLUGZEUG- UND EASA.A.S.03334 CESSNA 208B Installation of Camera Kit Cessna 208B 19.12.2007 MASCHINENBAU "System Gomolzig" C208B-812000 as defined by Equipmentlist AEL_17000_Rev0_11112007.XLS, dated 11.11.2007 10015031 GOMOLZIG FLUGZEUG- UND EASA.A.S.03343 REV. 1 DO 28 D-2 Turbine Conversion of Do 28 D-2 (model according limitation section of EASA STCDS Prior to installation of this modification it 06.12.2010 MASCHINENBAU marketing name: Do 28-G92 and Do28-G92- 10015031 must be determined thatthe EF) including new Propeller variantsMaster interrelationship between this modification Drawing List G92 for STC-Version G92-A- and any other previouslyinstalled 1900; G92-EF-A-1900;G92-A-1950 and G92- modification and/ or repair will introduce EF-A-1950Master Document List no adverse effectupon the airworthiness MDOCL_2023625_rev0_20101001 of the productIf the h 10015034 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10015040 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10015121 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10015261 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10017100 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10027347 GOMOLZIG FLUGZEUG- UND MASCHINENBAU EASA.A.S.03347 REV 1 BEECH 99 BEECH B99 EASA.A.S.03353 LEARJET 35A LEARJET 36A EASA.A.S.03470 EASA STC 2004-1522 CESSNA 402 CESSNA 402A CESSNA 402B CESSNA 402C EASA.A.S.03719 LBA STC 0279/2038 BRITTEN NORMAN BN-2A-21 ISLAND BRITTEN NORMAN BN-2A-26 ISLAND BRITTEN NORMAN BN-2A-27 ISLAND BRITTEN NORMAN BN-2B-20 ISLAND BRITTEN NORMAN BN-2B-26 ISLAND Installation of P&W PT6A-34 Engine This STC is limited to Beech 99 / B99 models equiped with Propeller McCauley 4HFR34C769/94LMA-4 i.a.w. FAA STC SA1351GL. Installation of Laser Reflector Dekagon Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install Use of Aerial Survey Camera Kit C402-812000 for installation of Zeiss RMK Top 15 and Top 30 cameras.Note: Change to the existing EASA STC 2004-1522 to enable optional operation of digital camera systems or laser scanners in accordance with MDL MDRWL_14631_ Installation of Exhaust System Gomolzig BN2- 606500. 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. EASA.R.S.01056 HUGHES 369D, HUGHES 369E Installation of Isolator Washing Platform Helicopter must be eqipped with- High Skid Landing Gear and- McDonnel Douglas Helicopter Cargo Hook Kit P/N 369H90072- 505 P-EASA.A.S.03887 SA 226T Installation of Wescam MX20 Camera Turret with ManualExtension/Retraction Mechanism and Operator Console Aircraft must be previously modified with camera hatches i.a.w.Swearingen Camera Plane Modification 19.12.2008 05.08.2008 08.02.2008 04.12.2008 06.12.2006 - The installation of this modification by 24.09.2009 third persons is subject towritten permission of the approval holder and disposal of the approvedappropriate documentation- Prior to installation of this modification it must be determined thatthe interrelationshi 04/01/2013 Page 238/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029335 GOMOLZIG FLUGZEUG- UND 310, 310A, 310B, 310C, 310D, Alternative Supplemenal Inspection Document As referred in limitations section of the 3A10_A- The installation of this modification by 19.03.2010 MASCHINENBAU 310E, 310F, 310G, 310H, 310I, (A-SID) SID_Maintenance ManualSupplement_21530 third persons is subject towritten 310J, 310J-1, 310K, 310L, 310N Alteration to A-SID is subject to written permission of the approval holder and 310P, 310Q, 310R permission of approval holder This modification holding and disposal ofthe approved E310H, E310J is only limited to S/N listed in EASA appropriate documentation. Prior to T310P, T310Q, T310R approvedGomolzig Document No. installation of this modification it must be 21530_Mast determined thatthe interr 10029380 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10029570 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10029736 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10030084 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10030085 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10031342 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10038775 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10040526 GOMOLZIG FLUGZEUG- UND MASCHINENBAU CESSNA 182, -A, -B, -C, -D, -E Camera Modification Kit As referred in limitations section of the AFM- The installation of this modification by 19.03.2010 CESSNA 182F, -G, -H, -J, -K, S:Airplane Flight Manual Supplement third persons is subject towritten CESSNA 182L, -M, -N, -P, -Q, SPOH_2022177_rev0_01022010 for permission of the approval holder and CESSNA 182R, -S, T, T182 Cessna182S, T and T182T Anhang zum holding and disposal ofthe approved CESSNA T182T Flughandbuch Kameraumrüstsatz C182- appropriate documentation Prior to 812000 Ausgabe 21.03.97for Cessna 182, -A, - installation of this modification it must be B, -C, -D, -E, -F, -G, -H, -J determined thatthe interre HUSKY A-1, A-1A, A-1B, A-1C Husky A1 Silencer STC Ext. To Variant A, B As referred in limitations section of the AFM- The installation of this modification by 01.04.2010 and C S:Airplane Flight Manual Supplement third persons is subject towritten SPOH_21750_rev0_20100301 permission of the approval holder and holding and disposal ofthe approved appropriate documentation. Prior to installation of this modification it must be determined thatthe interr P-EASA.A.S.03144 CESSNA 421B Installation of Silver Jodide Generators on Not Applicable Prior to installation of this modification it 16.04.2010 Cessna 421B 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. LBA STC 0060/549B REV. 1 SEE EASA APPROVED MODEL LIST LBA STC 0059/549B REV. 1 SEE EASA APPROVED MODEL LIST Upwards Opening Door for Parachutist Dropping.This STC revises and supersedes LBA STC 0060/549b. Dropping of max 4 Parachutists with Manual or Automatic Release. This STC revises and supersedes LBA STC 0059/549B. As referred in limitations section of the AFM- SSPOH_2022824_rev0_15042010For parachutist dropping As referred in limitations section of the AFM- SSPOH_2022926_rev0_15042010Max 4 parachutists The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation.Prior to installation of this modification it must be determined thatthe interre The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation.Prior to installation of this modification it must be determined thatthe interre 08.10.2010 08.10.2010 208B C208B Ferry Fuel Tank Installation in none The installation of this modification by 11.08.2010 accordance with Gomolzig Flugzeug-und third persons is subject towritten Maschinenbau GmbH MDOCL_2023163, Rev. permission of the approval holder.Prior to 0, dated 01/08/2010 installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinsta M6/91 PA-25-235, PA-25-260 Modification 2027423Low Noise Silencer Kit "System Gomolzig" PA-25-606500 PA-31T PA-31T Camera Hole ModificationChange Note CN_2025593_rev0_20120201 As referred in AFM-S Must be maintained iaw. Original MM and 13.03.2012 in addition iaw MaintenanceInstructions given in the above mentioned Installation Instructions orlater approved revisions.Prior to installation of this modification it must be determined thatthe interrelationship be as referred in AFM-S Must be maintained iaw. Original Piper MM and in addition iawII_2025593_rev0_20120201 or later approved revisions.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyi 04/01/2013 Page 239/462 09.07.2012
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04/01/2013 Page 1/462 - EASA

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