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1AD 16-06-002
BOMBARDIER INC. DHC-8-400 SERIES, MODELS -400, -401 AND -402, SERIAL NUMBERS 4001, 4003 THRU 4325, EQUIPPED WITH MAIN LANDING GEAR (MLG) RETRACT ACTUATOR ROD END PART NUMBER (P/N) P3A2750 OR P3A2750-1
Legality : / 17 Juni 2016
First Issued : 17 Juni 2016
2AD 16-05-025
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-300, -400, AND -500 SERIES AIRPLANE, CERTIFICATED IN ANY CATEGORY, AS IDENTIFIED IN BOEING ALERT SERVICE BULLETIN 737-53A1339, DATED AUGUST 12, 2014. (2) INSTALLATION OF SUPPLEMENT TYPE CERTIFICATED (STC) SA037 DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANE ON WHICH STC SA037 IS INSTALLED, A “CHANGE IN PRODUCT” ALTERNATIVE METHOD OF COMPLIANCE (AMOC) APPROVAL REQUEST IS NOT NECESSARY TO COMPLY WITH THE REQUIREMENTS OF CASR 39.15.
Legality : / 1 Juni 2016
First Issued : 1 Juni 2016
3AD 16-05-026
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-200, -300, -400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY, AS IDENTIFIED IN BOEING SPECIAL ATTENTION SERVICE BULLETIN 737-53-1159, REVISION 1, DATED OCTOBER 20, 2014. (2) INSTALLATION OF SUPPLEMENT TYPE CERTIFICATED (STC) SA037 DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANE ON WHICH STC SA037 IS INSTALLED, A “CHANGE IN PRODUCT” ALTERNATIVE METHOD OF COMPLIANCE (AMOC) APPROVAL REQUEST IS NOT NECESSARY TO COMPLY WITH THE REQUIREMENTS OF CASR 39.15.
Legality : / 1 Juni 2016
First Issued : 1 Juni 2016
4AD 16-05-020
THIS AD APPLIES TO ALL GENERAL ELECTRIC COMPANY (GE) CF6-80C2B1F, CF6-80C2D1F, CF6-80E1A2, CF6-80E1A3, CF6-80E1A4, AND CF6-80E1A4/B TURBOFAN ENGINES
Legality : / 23 Mei 2016
First Issued : 23 Mei 2016
5AD 16-05-007
A300, A300-600 AND A310 AEROPLANES, ALL CERTIFIED MODELS, ALL MANUFACTURER SERIAL NUMBERS (MSN). NOTE: THIS AD APPLIES TO ALL A300, A310 AND A300-600 AEROPLANES AS AN AFFECTED FORWARD PASSENGER DOOR COULD HAVE BEEN REMOVED AND INSTALLED IN SERVICE ON ANY MSN
Legality : / 4 Mei 2016
First Issued : 4 Mei 2016
6AD 16-04-028
BELL HELICOPTER TEXTRON CANADA LIMITED MODEL 429, SERIAL NUMBERS 57001 THROUGH 57265 WHERE THE HELICOPTER IS EQUIPPED WITH WHEELED LANDING GEAR.
Legality : / 28 April 2016
First Issued : 28 April 2016
7AD 16-04-011
THIS EMERGENCY AIRWORTHINESS DIRECTIVE (EAD) APPLIES TO EMBRAER S.A. MODEL ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR, AND ERJ190-200 IGW AIRPLANES
Legality : / 15 April 2016
First Issued : 15 April 2016
8AD 16-04-017
THIS AD APPLIES TO THE BOEING COMPANY MODEL 747-400 SERIES AIRPLANES HAVING A STRETCHED UPPER DECK; CERTIFICATED IN ANY CATEGORY; EXCLUDING AIRPLANES THAT HAVE BEEN CONVERTED TO A LARGE CARGO FREIGHTER CONFIGURATION
Legality : / 15 April 2016
First Issued : 15 April 2016
9SI 8900-3.552
PETUNJUK TEKNIS BAGIAN 8900-3.552 (STAFF INSTRUCTION 8900-3.552) TENTANG ADMINISTRASI DAN PENGENDALIAN PENGELASAN PESAWAT UDARA DAN UJI TAK RUSAK (UTR) (ADMINISTRATION AND CONTROL OF AIRCRAFT WELDING AND NON DESTRUCTIVE TESTING (NDT)
Legality : KP 137 Tahun 2016 / 11 April 2016
First Issued : 11 April 2016
10AC 8900-3.552
PEDOMAN TEKNIS OPERASIONAL BAGIAN 8900-3.552 (ADVISORY CIRCULAR 8900-3.552) TENTANG ADMNISTRASI DAN PENGENDALIAN PESAWAT UDARA DAN UJI TAK RUSAK (UTR) (ADMINISTRATION AND CONTROL OF AIRCRAFT WELDING AND NON DESTRUCTIVE TESTING (NDT)
Legality : KP 122 Tahun 2016 / 8 April 2016
First Issued : 8 April 2016
11AD 16-03-007
(1) THIS AD APPLIES TO ALL THE BOEING COMPANY MODEL 737-100, -200, -300, -400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY. (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) SA037 DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH STC SA037 IS INSTALLED, A 'CHANGE IN PRODUCT' ALTERNATIVE METHOD OF COMPLIANCE (AMOC) APPROVAL REQUEST IS NOT NECESSARY TO COMPLY WITH THE REQUIREMENTS OF CASR 39.15
Legality : / 18 Maret 2016
First Issued : 18 Maret 2016
12AD 16-02-008
AS 350 B1, B2 AND AS 355 E, F, F1, F2, N HELICOPTERS, ALL SERIAL NUMBERS, IF EQUIPPED WITH MAIN GEARBOX (MGB) BOTTOM CASING (SUMP) P/N 350A32-3119-03 OR P/N 350A32-3119-05
Legality : / 15 Pebruari 2016
First Issued : 15 Pebruari 2016
13AD 16-02-009
AS 355 NP HELICOPTERS, ALL SERIAL NUMBERS, IF EQUIPPED WITH MAIN GEARBOX (MGB) MAIN CASING PART NUMBER (P/N) 350A32-3121-07, OR EQUIPPED WITH MGB BOTTOM CASING (SUMP) P/N 350A32-3119-03 OR P/N 350A32-3119-05
Legality : / 15 Pebruari 2016
First Issued : 15 Pebruari 2016
14AD 16-02-010
EC 130 B4 HELICOPTERS, ALL SERIAL NUMBERS, IF EQUIPPED WITH MAIN GEARBOX (MGB) MAIN CASING PART NUMBER (P/N) 350A32-3156-21 (FITTED ON ASSEMBLY 350A32-3156-01) OR P/N 350A32-3156-22 (FITTED ON ASSEMBLY 350A32-3156-02) OR EQUIPPED WITH MGB BOTTOM CASING (SUMP) P/N 350A32-3119-05
Legality : / 15 Pebruari 2016
First Issued : 15 Pebruari 2016
15AD 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
16AD 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
17SI HRD-01 Amandement 2
HUMAN RECOURSES DEVELOPMENT OF DIRECTORATE GENERAL OF CIVIL AVIATION PERSONNEL
Legality : KP 621 TAHUN 2015 / 28 Oktober 2015
First Issued : 1 Nopember 2000
Latest Amandement (2) : 28 Oktober 2015
18SI 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
19EAD 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
20EAD 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
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