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1AD 14-09-007
SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, AS 332 C, AS332 C1, AS332 L, AS 332 L1, AS 332 L2, MBB-BK 117 C-2, AND AB 212, AB 412 AND AB 412EP HELICOPTERS, ALL SERIAL NUMBERS, 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 : / 25 September 2014
First Issued : 25 September 2014
2AD 14-09-010
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-200,-300,-400,AND-500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE SA037 DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH SA037 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 : / 25 September 2014
First Issued : 25 September 2014
3AD 14-07-022
HONEYWELL INTERNATIONAL INC. TFE731-50R TURBOFAN ENGINES WITH 2M STAGE LOW-PRESSURE TURBINE (LPT2)BLADES, PART NUMBER (P/N) 3075424-1, -2, OR -3 INSTALLED.
Legality : / 4 Agustus 2014
First Issued : 4 Agustus 2014
4AD 14-03-001
THIS AD APPLIES TO GENERAL ELECTRIC COMPANY (GE) GE90-110B1 AND GE90-115B TURBOFAN ENGINES WITH HIGH PRESSURE COMPRESSOR (HPC) ROTOR STAGE 2-5 SPOOLS, PART NUMBERS (P/NS) 351-103-106-0, 351-103-107-0, 351-103-141-0, 351-103-142-0, 351-103-144-0, 351-103-145-0, 351-103-148-0, 351-103-149-0, AND 351-103-151-0, WITH SPOOL SERIAL NUMBERS LISTED IN PARAGRAPH 4, APPENDIX A OF GE SERVICE BULLETIN (SB) NO. GE90-100 S/B 72-0499, DATED AUGUST 14, 2013.
Legality : / 16 April 2014
First Issued : 16 April 2014
5AD 14-03-031
THE BOEING COMPANY MODEL 737-200,-300,-400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY.INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) SA 037 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 14 CFR 39.17.
Legality : / 16 April 2014
First Issued : 16 April 2014
6AD 14-02-004
AS 332 C. AS 332 CL. AS 332 1. AS 332 11. AS 332 L2 HELICOPTERS. ALL SERIAL NUMBERS (S/N), IF EQUIPPED WITH MAIN GEAR BOX (MGB) BEVEL GEAR VERTICAL SHAFT PART NUMBER (P/N) 332A32-5 101-00 P/N 332A32-5101-05. P/N 332A32-5101-10 OR P/N 332A32-5101-15, ALL S/N.
Legality : / 15 April 2014
First Issued : 15 April 2014
7AD 13-10-016
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-600, -700, -700C, -800, AND - 900 SERIES AIRPLANES; CERTIFICATED IN ANY CATEGORY; AS IDENTIFIED IN BOEING SPECIAL ATTENTION SERVICE BULLETIN 737- 53-1294, REVISION 1, DATED JUNE 14, 2013. (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) ST00830SE (HTTP://RGL.FAA.GOV/REGULATORY_AND_GUIDANCE _LIBRARY/RGSTC.NSF/0/408E012E008616A786 2578880060 456C?OPENDOCUMENT&HIGHLIGHT=ST00830SE ) DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH STC ST00830SE 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. FOR ALL OTHER AMOC REQUESTS, THE OPERATOR MUST REQUEST APPROVAL FOR AN AMOC TO DGCA.
Legality : / 14 April 2014
First Issued : 14 April 2014
8AD 13-10-024
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-600, -700, -700C, -800, -900, AND -900ER SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY, WITH AN ORIGINAL AIRWORTHINESS CERTIFICATE OR ORIGINAL EXPORT CERTIFICATE OF AIRWORTHINESS ISSUED BEFORE APRIL 3, 2012. (2) THIS AD REQUIRES REVISIONS TO CERTAIN OPERATOR MAINTENANCE DOCUMENTS TO INCLUDE NEW INSPECTIONS. COMPLIANCE WITH THESE INSPECTIONS IS REQUIRED BY 14 CFR 91.403(C). FOR AIRPLANES THAT HAVE BEEN PREVIOUSLY MODIFIED, ALTERED, OR REPAIRED IN THE AREAS ADDRESSED BY THESE INSPECTIONS, THE OPERATOR MAY NOT BE ABLE TO ACCOMPLISH THE INSPECTIONS DESCRIBED IN THE REVISIONS. IN THIS SITUATION, TO COMPLY WITH 14 CFR 91.403(C), THE OPERATOR MUST REQUEST APPROVAL FOR AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) ACCORDING TO PARAGRAPH (J) OF THIS AD. THE REQUEST SHOULD INCLUDE A DESCRIPTION OF CHANGES TO THE REQUIRED INSPECTIONS THAT WILL ENSURE THE CONTINUED DAMAGE TOLERANCE OF THE AFFECTED STRUCTURE. THE FAA HAS PROVIDED GUIDANCE FOR THIS DETERMINATION IN FAA ADVISORY CIRCULAR (AC) 120-93, DATED NOVEMBER 20, 2007. (3) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) ST00830SE AFFECTS THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH STC ST00830SE IS INSTALLED, A 'CHANGE IN PRODUCT' AMOC APPROVAL REQUEST MIGHT BE NECESSARY TO COMPLY WITH THE REQUIREMENTS OF 14 CFR 39.17.
Legality : / 14 April 2014
First Issued : 14 April 2014
9AD 13-11-010
THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-600, -700, -800, -900, AND - 900ER SERIES AIRPLANES, WITH PASSENGER SEATS INSTALLED; CERTIFICATED IN ANY CATEGORY; AS IDENTIFIED IN BOEING SPECIAL ATTENTION SERVICE BULLETIN 737-53-1296, DATED JANUARY 11, 2011.
Legality : / 14 April 2014
First Issued : 14 April 2014
10AD 13-09-032
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-600, -700, -700C, - 800, -900, AND - 900ER SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY, AS IDENTIFIED IN BOEING ALERT SERVICE BULLETIN 737- 52A1167, DATED DECEMBER 1, 2011. (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) ST0083(HTTP://RGL.FAA.GOV/REGULATORY_AND_G UIDANCE_LIBRARY/RGSTC.NSF/0/408E012E00861 6A7862578880060 456C OPENDOCUMENT&HIGHLIGHT=ST00830SE) DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH STC ST00830SE 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 : / 8 April 2014
First Issued : 8 April 2014
11AD 13-08-010
GENERAL ELECTRIC COMPANY (GE) GE90- 110B1 AND GE90-115B TURBOFAN ENGINES WITH A TRANSFER GEARBOX ASSEMBLY (TGB) RADIAL GEARSHAFT, PART NUMBER 1995M24P02, SERIAL NUMBER (S/N) LISTED IN FIGURE 1 TO PARAGRAPH (C) OF THIS EMERGENCY AD, INSTALLED.
Legality : / 12 Maret 2014
First Issued : 12 Maret 2014
12AD 13-08-020
CFM56-5 (INCLUDING VARIANT CFM56-5-A1), CFM56-5-A1/F, CFM56-5A3, CFM56- 5A4, CFM56-5A4/F, CFM56-5A5 AND CFM56-5A5/F ENGINES, ALL SERIAL NUMBERS ON WHICH STAGE 1 LOW PRESSURE TURBINE WAS REPAIRED USING AIRFOIL REPLACEMENT REPAIR, CHROMALLOY NEVADA DER-N068 (04-CNV- 068-0). THESE ENGINES ARE KNOWN TO BE INSTALLED ON, BUT NOT LIMITED TO, AIRBUS A319 AND A320 AEROPLANES.
Legality : / 12 Maret 2014
First Issued : 12 Maret 2014
13SI 8900-2.13
PROSEDURE SERTIFIKASI, PERPANJANGAN, PENAMBAHAN UNTUK ORGANISASI PERAWATAN PESAWAT UDARA LUAR NEGERI
Legality : KP 464 TAHUN 2013 / 17 Oktober 2013
First Issued : 17 Oktober 2013
14SI 8900-2.11
PROSEDUR SERTIFIKASI, PERPANJANGAN, PENAMBAHAN UNTUK ORGANISASI PERAWATAN PESAWAT UDARA DALAM NEGERI
Legality : KP 463 TAHUN 2013 / 17 Oktober 2013
First Issued : 17 Oktober 2013
15AD 13-07-016
THIS AD APPLIES TO TRANSPORT CATEGORY AIRPLANES, IN PASSENGER-CARRYING OPERATIONS, AS SPECIFIED IN PARAGRAPH (C)(1) OR (C)(2) OF THIS AD. (1) AIRPLANES THAT ARE IN COMPLIANCE WITH THE REQUIREMENTS OF DGCA AD 11-03-15 (FAA AD 2011-04-09) (2) AIRPLANES EQUIPPED WITH ANY CHEMICAL OXYGEN GENERATOR INSTALLED IN ANY LAVATORY AND ARE: (I) OPERATING UNDER CASR PART 121; OR (II) INDONESIAN REGISTERED AND OPERATING UNDER CASR PART 129, WITH A MAXIMUM PASSENGER CAPACITY OF 20 OR GREATER.
Legality : / 2 Agustus 2013
First Issued : 2 Agustus 2013
16AD 13-07-009
THIS AD APPLIES TO TURBOCHARGED PIPER AIRCRAFT, INC. MODELS PA-31, PA-31-325, AND PA-31-350 AIRPLANES, ALL SERIAL NUMBERS, CERTIFICATED IN ANY CATEGORY.
Legality : / 25 Juli 2013
First Issued : 25 Juli 2013
17AD 13-06-001
GE AVIATION SYSTEMS LTD, TRADING AS DOWTY PROPELLERS, R334/4-82-F/13 PROPELLERS, IF FITTED WITH PART NUMBER (P/N) 660709201 HUB ASSEMBLIES. THESE PROPELLERS ARE KNOWN TO BE INSTALLED ON, BUT NOT LIMITED TO, CASA C-212 AIRPLANES.
Legality : / 7 Juni 2013
First Issued : 7 Juni 2013
18AD 12-10-019R1
(1) THIS AD APPLIES TO ALL THE BOEING COMPANY MODEL 737-100, -200, -200C, -300, -400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY. (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 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 : / 3 Juni 2013
First Issued : 3 Juni 2013
19AD 13-05-009
(1) THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-800 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY, AS IDENTIFIED IN BOEING SERVICE BULLETIN 737-53-1311, DATED OCTOBER 21, 2011. (2) INSTALLATION OF SUPPLEMENTAL TYPE CERTIFICATE (STC) ST00830SE DOES NOT AFFECT THE ABILITY TO ACCOMPLISH THE ACTIONS REQUIRED BY THIS AD. THEREFORE, FOR AIRPLANES ON WHICH STC ST00830SE 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 : / 3 Juni 2013
First Issued : 3 Juni 2013
20AD 13-05-013
(1) THIS AD APPLIES TO ALL THE BOEING COMPANY MODEL 737-100, -200, -200C, -300, -400, AND -500 SERIES AIRPLANES, CERTIFICATED IN ANY CATEGORY. (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 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 : / 3 Juni 2013
First Issued : 3 Juni 2013
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Agenda Kegiatan
Sosialisasi dan Bimbingan Reformasi dan Kelembagaan (Lokasi Makassar)
FGD Proses Penegakan Hukum Tindak Pidana Korupsi
Sosialisasi dan Bimbingan Reformasi dan Kelembagaan (Lokasi Surabaya)
Sosialisasi dan Bimbingan Reformasi dan Kelembagaan (Lokasi Medan)