04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10033161 ANCRA INTERNATIONAL LLC FAA STC ST02319LA B737-400 Installation of main deck cargo loading system EASA validated equivalent to FAA STC This modification does not affect 21.12.2010
ST01827LA must be installed inconjunction Electrical Wiring InterconnectionSystems.
with this STC
Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair w
10038884 ANCRA INTERNATIONAL LLC FAA STC ST02414LA B757-200 Installation of Main Deck Cargo Loading
System.
10014603 APA AVIONES PIEZAS Y ACCESORIOS EASA.A.S.02726 CESSNA 421C Installation GNS-430 and DME KN62AGarmin
GNS-430 GPS/NAV/COMM system, Mid-
Continent MD41D Annunciation Control Unit
and Bendix King KN62 DME installed on
Cessna 421CS/N 0272 (GPS approved for IFR
and B-RNAV operations).
10016710 APICAL INDUSTRIES, Inc. EASA.IM.R.S.00619 FAA STC SR00470LA AS 350 B/D/BA/B1/B2/B3 Emergency Flotation Kit installation according
to FAA STC No. SR00470LA issued on
November 17, 1997 and reissued December
22, 1998.
10016719 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01013 FAA STC SR00780LA EC 120 B Installation of Apical Emergency Float Kit, p/n
10016772 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01107 REV. 1 FAA STC SR01779LA AB412, AB412EP
BELL 212, 412, 412EP/CF
BELL 412 EP
10016775 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01114 FAA STC SR00831LA AS 350 D/B/B1/B2/B3/BA,
AS 355 E/F/F1/F2/N
20498.The present STC is the validation of the
FAA STC n° SR00780LA issued on
19/03/1999.
STC EASA.IM.R.S.01107 applicability
extended to B212, 412 CF, AB412 and
AB412EP.
10016776 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01115 FAA STC SR01687LA EC 130 B4 Installation of Apical Emergency Float kit p/n
604-0018-100 or Emergency Float kit with
Liferaft p/n 604-0018-300.
10016788 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01135 FAA STC SR01535LA BELL 206A, 206B, 206L, 206L-1
BELL 206L-3, 206L-4, BELL 407
To be installed on a/c converted to a
Combination Passenger/ Freighterby ST
Aerospace Inc, EASA STC 10038822.
1. Restricted to aircraft CESSNA 421C S/N
0272.2. The aircraft is approved for dual pilot B-
RNAV operation, subjected to the conditions,
limitations and procedures contained in Doc N°
APA 018/03 "Supplement Flight Manual", Ed 2
Rev 0
1. This STC is approved only for the product
configuration as defined in the approved design
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
1. This STC is approved only for the product
configuration as defined in the approved design
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
1. Instruction for Continued Airworthiness ICA
412-41 Rev. B dated 12th July 2005 or later
approved revision.2. Bell Helicopter Textron,
Inc. High Skid Landing Gear with Lightweight
Flotation Skid Tubes, Part Number 412-050-
015-111/-112 or Aeronautic
Installation of Apical Emergency Float kit, Part 1. This approval requires the inspection and
Number 20416, in accordance with the overhaul schedules to be performed as
following FAA approved Apical Industries, Inc., mandated by the Apical Instructions for
Master Document List and Rotorcraft Flight Continued Airworthiness n° ICA 355-1, rev. G,
Manual Supplement :- For AS 350 series : dated December 3rd, 2004 or later FAA
MDL n° MD350(4) rev. I, dated Decemb approved revision.2. This installation should not
Installation of Apical Industries Inc. Emergency
Float Kits.
10016795 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01148 FAA STC SR00627LA AS 350 B, AS 350 B1, AS 350 B2 Installation of Utility floats in accordance with
AS 350 B3, AS 350 BA, AS 350 D FAA STC SR00627LA issued May 08, 1998,
reissued December 22, 1998 and amended
September 14, 1998.
10016829 APICAL INDUSTRIES, Inc. EASA.IM.R.S.01199 REV. 1 FAA STC SR01855LA EC 135 P1 (CDS)
EC 135 P1 (CPDS)
EC 135 P2 (CPDS), EC 135 P2+
EC 135 T1 (CDS)
EC 135 T1 (CPDS)
EC 135 T2 (CPDS), EC 135 T2+
Emergency Floats KitsInstallation of Apical
Industries, Inc. Emergency Floats Kits i.a.w.
FAASTC SR01855LA Apical MDL MD 135-1
provides for different installationseither with
liferats or without. Amendment of the STC in
order to add the EC135 Mid Height La
This StC is the EASA validation of FAA STC
n0 SR01687LA, dated March 22nd, 2005.
1. This installation of Apical Industries Inc.
Emergency Float Kit requires prior installation
of high landing gear with provision for float
installation as defined in Apical Industries Inc.
Approved Landing Gears for Apical
Emergency Float Kit, AIPHI-8
This approval requires the inspections and
overhaul schedules to be performed as
mandated by the Instruction for Continued
Airworthiness, ICA350-2 dated 2, 1997 or later
FAA approved revision.
1. The installation is not approved for
helicopters equipped with highskid landing
gear.2. Metro Aviation, Inc., Landing Gear Skid
Extensions, Part Number135M-110, must be
installed i.a.w. STC EASA.IM.R.S.01377 (FAA
STCSR09230RC) prior to the installation
Prior to installation of this modification it 21.03.2012
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.
Prior to installation of this modification it
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.
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