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1AD 16-01-017
THIS AD APPLIES TO SIKORSKY MODEL S-76A, S-76B, AND S-76C HELICOPTERS WITH A MAIN GEARBOX (MGB) PART NUMBER (P/N) 76351-09000 SERIES, 76351-09500 SERIES, AND 76351-09600 SERIES INSTALLED THAT HAS BEEN REPAIRED IN ACCORDANCE WITH "APPLICABILITY" SECTION IN REFERENCED AD
Legality : / 2 Pebruari 2016
First Issued : 2 Pebruari 2016
2AD 16-01-006-U
AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AND AS 332 L2 HELICOPTERS, ALL MANUFACTURER SERIAL NUMBERS, IF EQUIPPED WITH EMERGENCY FLOTATION GEAR
Legality : / 22 Januari 2016
First Issued : 22 Januari 2016
3SI 8900-2.11 Amandement 1
PROSEDUR SERTIFIKASI, PERPANJANGAN, PENAMBAHAN UNTUK ORGANISASI PERAWATAN PESAWAT UDARA DALAM NEGERI
Legality : KP 576 TAHUN 2015 / 6 Oktober 2015
First Issued : 17 Oktober 2013
Latest Amandement (1) : 6 Oktober 2015
4EAD 15-09-11
THIS EAD WAS PROMPTED BY AN ACCIDENT OF A SIKORSKY AIRCRAFT CORPORATION MODEL S-76C HELICOPTER. DURING PRELIMINARY INVESTIGATION, A FAILED SERVO INPUT CONTROL PUSHROD (PUSHROD) ASSEMBLY WAS IDENTIFIED. SEPARATION OF THE PUSHROD TUBE AND THE CONTROL ROD END WITH BEARING WAS FOUND. THIS EAD REQUIRES INSPECTING THE MAIN ROTOR (M/R) FORWARD, AFT, AND LATERAL PUSHROD ASSEMBLIES, THE TAIL ROTOR (T/R) PUSHROD ASSEMBLY, AND THE JAMNUTS, AND APPLYING SLIPPAGE MARKS ACROSS THE PUSHROD TUBES AND JAMNUTS. THESE EAD ACTIONS ARE INTENDED TO PREVENT LOSS OF M/R OR T/R FLIGHT CONTROL AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER. WE ARE ISSUING THIS EAD BECAUSE WE EVALUATED ALL THE RELEVANT INFORMATION AND DETERMINED THE UNSAFE CONDITION DESCRIBED PREVIOUSLY IS LIKELY TO EXIST OR DEVELOP IN OTHER PRODUCTS OF THESE SAME TYPE DESIGNS.
Legality : / 17 September 2015
First Issued : 17 September 2015
5EAD 15-09-011
THIS EAD WAS PROMPTED BY AN ACCIDENT OF A SIKORSKY AIRCRAFT CORPORATION MODEL S-76C HELICOPTER. DURING PRELIMINARY INVESTIGATION, A FAILED SERVO INPUT CONTROL PUSHROD (PUSHROD) ASSEMBLY WAS IDENTIFIED. SEPARATION OF THE PUSHROD TUBE AND THE CONTROL ROD END WITH BEARING WAS FOUND. THIS EAD REQUIRES INSPECTING THE MAIN ROTOR (M/R) FORWARD, AFT, AND LATERAL PUSHROD ASSEMBLIES, THE TAIL ROTOR (T/R) PUSHROD ASSEMBLY, AND THE JAMNUTS, AND APPLYING SLIPPAGE MARKS ACROSS THE PUSHROD TUBES AND JAMNUTS. THESE EAD ACTIONS ARE INTENDED TO PREVENT LOSS OF M/R OR T/R FLIGHT CONTROL AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER. WE ARE ISSUING THIS EAD BECAUSE WE EVALUATED ALL THE RELEVANT INFORMATION AND DETERMINED THE UNSAFE CONDITION DESCRIBED PREVIOUSLY IS LIKELY TO EXIST OR DEVELOP IN OTHER PRODUCTS OF THESE SAME TYPE DESIGNS.
Legality : / 17 September 2015
First Issued : 17 September 2015
6AD 15-08-004
A300-600 AND A310 PASSENGER AEROPLANES, ALL MODELS, ALL SERIAL NUMBERS (EXCEPT ALL-CARGO AEROPLANES), IF EQUIPPED WITH ONE-FRAME OVERHEAD STOWAGE COMPARTMENTS (OHSC).
Legality : / 4 September 2015
First Issued : 4 September 2015
7AD 15-09-004
A300-600 AND A310 PASSENGER AEROPLANES, ALL MODELS, ALL SERIAL NUMBERS (EXCEPT ALL-CARGO AEROPLANES), IF EQUIPPED WITH ONE-FRAME OVERHEAD STOWAGE COMPARTMENTS (OHSC).
Legality : / 4 September 2015
First Issued : 4 September 2015
8AD 15-08-14
EC 155 B AND B1 HELICOPTERS, ALL MANUFACTURER SERIAL NUMBERS, IF EQUIPPED WITH AN EXTRACTION TAPE FITTED WITH PRESS-STUDS ON THE EMERGENCY EXIT WINDOWS.
Legality : / 24 Agustus 2015
First Issued : 24 Agustus 2015
9AD 15-08-04
SA 365 N, SA 365 N1, AS 365 N2, AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 AND EC 225 LP, MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK 117 C-1, AB 212 AND AB 412 HELICOPTERS, IF EQUIPPED WITH EMERGENCY FLOTATION SYSTEM, ALL PART NUMBERS, AS APPROVED OPTIONAL KIT FOR DITCHING PROVISION FROM THE HELICOPTER MANUFACTURER OR BY A SUPPLEMENTAL TYPE CERTIFICATE (STC).
Legality : / 19 Agustus 2015
First Issued : 19 Agustus 2015
10AD 15-07-005
AIRBUS A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 AND A321-232 AEROPLANE MODELS, ALL MANUFACTURER SERIAL NUMBERS, EXCEPT THOSE THAT HAVE EMBODIED AIRBUS MODIFICATION 33125 (GASEOUS SYSTEM FOR ALL OXYGEN CONTAINERS) IN PRODUCTION
Legality : / 15 Juli 2015
First Issued : 15 Juli 2015
11AD 15-07-009
AIRBUS A330-201, A330-202, A330-203, A330-243,A330-341, A330-342 AND A330-343 AEROPLANES, ALL MANUFACTURER SERIAL NUMBERS (MSN), EXCEPT THOSE THAT HAVE EMBODIED AIRBUS MODIFICATION 33125 (GASEOUS SYSTEM INSTALLED FOR ALL OXYGEN CONTAINERS) IN PRODUCTION
Legality : / 15 Juli 2015
First Issued : 15 Juli 2015
12AD 15-06-008
THIS AD APPLIES TO ALL LYCOMING TIO-540-AJ1A RECIPROCATING ENGINES LISTED BY ENGINE SERIAL NUMBER (S/N) IN FIGURE 1 TO PARAGRAPH (C) OF THIS AD AND TO ANY TIO-540-AJ1A RECIPROCATING ENGINE WITH A REPLACEMENT TURBOCHARGER MOUNTING BRACKET INSTALLED THAT WAS PURCHASED BETWEEN APRIL 5, 2012 AND MAY 29, 2014
Legality : / 16 Juni 2015
First Issued : 16 Juni 2015
13AD 15-06-003
AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 AND EC 225 LP HELICOPTERS, ALL SERIAL NUMBERS, IF EQUIPPED WITH AN INTERMEDIATE GEAR BOX (IGB) FAIRING PART NUMBER (P/N) 332A24-0303-05XX OR P/N 332A24-0303-06XX OR P/N 332A08-1391-00 OR P/N 332A08-1391-01
Legality : / 8 Juni 2015
First Issued : 8 Juni 2015
14PKPS 91 Amandement 4
GENERAL OPERATING AND FLIGHT RULES
Legality : PM 94 / 20 Mei 2015
First Issued : 22 Juli 1997
Latest Amandement (4) : 20 Mei 2015
15AD 15-05-010
AIRBUS A330-201, A330-202, A330-203, A330-243, A330-341, A330-342 AND A330-343 AEROPLANES, ALL MANUFACTURER SERIAL NUMBERS (MSN), EXCEPT AEROPLANES ON WHICH AN UPPER CARDAN PIN ON A MAIN LANDING GEAR (MLG) HAS NEVER BEEN REPLACED OR RE-INSTALLED SINCE FIRST ENTRY INTO SERVICE OF THE AEROPLANE.
Legality : / 19 Mei 2015
First Issued : 19 Mei 2015
16AD 15-05-007
AS 332L1, AS 332L2, EC 225LP, SA 365N, AS 365 N3, AND EC 155B1 HELICOPTERS, ALL SERIAL NUMBERS, IF EQUIPPED WITH HR SMITH EMERGENCY LOCATOR TRANSMITTER (ELT) PART NUMBER (P/N) CPI 503-16 INSTALLED IN ACCORDANCE WITH AN AIRBUS HELICOPTERS DESIGN CHANGE AS SPECIFIED ON THE REFERENCE AD
Legality : / 18 Mei 2015
First Issued : 18 Mei 2015
17AD 14-09-007R2
SA 365, AS 365, EC 155, AS 332 C, AS 332, EC 225, MBB-BK 117, AB 212 AND AB 412 HELICOPTERS, IF EQUIPPED WITH EMERGENCY FLOTATION SYSTEM, ALL PART NUMBERS, AS APPROVED OPTIONAL KIT FOR DITCHING PROVISION FROM THE HELICOPTER MANUFACTURER OR BY A SUPPLEMENTAL TYPE CERTIFICATE (STC)
Legality : / 20 April 2015
First Issued : 20 April 2015
18AD 15-04-006
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-100, -200, -200C, -300, -400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY, AS IDENTIFIED IN BOEING SPECIAL ATTENTION SERVICE BULLETIN 737-53-1083, REVISION 5, DATED JULY 22, 2014. (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) ST01219SE DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH FAA STC ST01219SE IS INSTALLED A 'CHANGE IN PRODUCT' ALTERNATIVE METHOD OF COMPLIANCE (AMOC) APPROVAL REQUEST IS NOT NECESSARY TO COMPLY WITH THE REQUIREMENTS OF 14 CFR 39.17.
Legality : / 14 April 2015
First Issued : 14 April 2015
19AD 13-12-017R1
AS 350 BA, AS 350 BB, AS 350 B2, AS 350 B3 AND AS 355 NP HELICOPTERS, ALL S/N, IF MODIFIED IN PRODUCTION WITH (OPTIONAL) MODIFICATION OP0811 AND EQUIPPED WITH A GRIMES-HONEYWELL POWER SUPPLY UNIT, PART NUMBER (P/N) 60-1431-3, IN THE BAGGAGE COMPARTMENT AS PART OF THAT OPTIONAL MODIFICATION, EXCEPT HELICOPTERS THAT HAVE EMBODIED AT LEAST ONE OF THE MODIFICATIONS AS LISTED IN APPENDIX1 OF THE REFERENCE AD
Legality : / 27 Pebruari 2015
First Issued : 27 Pebruari 2015
20AD 15-02-013
THIS AIRWORTHINESS DIRECTIVE (AD) APPLIES TO TRANSPORT CATEGORY AIRPLANES, IN PASSENGER-CARRYING OPERATIONS, AS SPECIFIED IN PARAGRAPH (A) AND (B) OF THIS AD. (A) REGISTERED IN INDONESIA AND OPERATING UNDER CASR 129, WITH A MAXIMUM PASSENGER CAPACITY OF 20 OR GREATER (B) AIRPLANES EQUIPPED WITH ANY CHEMICAL OXYGEN GENERATOR INSTALLED IN ANY LAVATORY AND ARE OPERATING UNDER CIVIL AVIATION SAFETY REGULATIONS (CASR) 121
Legality : / 27 Pebruari 2015
First Issued : 27 Pebruari 2015
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