A4O-AT AIRWORTHINESS COMPLIANCE STATUS (AIRFRAME AND APPLIANCE)

Transcription

1 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) AIRFRAME (RLD) ATC TRANSPONDER - TEST//REPAIR. NOT APPLICABLE DUE TO AC INPUT OPERATIONAL TEST OF TOILET WASTE BIN FLAP FOR PROPER CLOSING OPERATIONAL TEST / 29166:00/ EVERY 120 DAYS OPEN/REPETITIVE COMPLIED DURING C1/P14 CHECK WO: (B)R1 FLAPS 45 CONFIGURATION (B)R2 FLIGHT CONTROLS (B) AUTO-PILOT (B)R1 STRUCTURE - RESULT OF FATIGUE TEST. CANCELLED BY R3 DTD 26 JUL 2000, REPLACED BY AD (B) (B)R2 FLIGHT IN FREEZING DRIZZLE OR RAIN. CANCELLED CANCELLED AND REPLACED BY AD (B) (B)R0 MAIN LANDING GEAR SIDE BRACE PIN NOT APPLICABLE DUE TO AFFECTED: MSN 121 TO (B)R0 PROTECTION OF THE ELECTRICAL HARNESS IN FRONT AREA (B)R R1 / TIME LIMITS REVISION COMPLIED TIME LIMIT DOC PER LATEST REV. OF MPD (B) TIME LIMITS SPI 1301 REVISION COMPLIED TIME LIMIT DOC PER LATEST REV. OF MPD (B)R0 WINDSHIELD FRAME-NODE (B)R0 CORROSION ON WING REAR SPAR. NUMBER (B)R0 DE-ICING PROCEDURES & PROTECTION IMPROVEMENTS CANCELLED CANCELLED BY R1 DATED 9 OCT Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 1 of 18

2 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) (B)R0 ENGINE NACELLE DRAIN SYSTEM (B)R0 MAIN LANDING GEAR PINS MAGNETIC. SB ATR SB ATR NOT APPLICABLE AS PER A/C SATUS AT DELIVERY (B)R0 FUSELAGE STRINGER 6 TO FRAME 34 JUNCTION. SB ATR COMPLIED AS PER A/C LIST AT DELIVERY (B)R1 DE-ICING PROCEDURES & PROTECTIONS IMPROVEMENTS (ATA30) ATR R REPLACED BY AD NO (B)R (B)R0 STANDBY HORIZON POWER SUPPLY (B)R0 STICK SHAKER/PUSHER SYSTEM NUMBER (B)R1 FORWARD CARGO DOOR COMPARTMENT NETS (B)R4 BARREL SWINGING LEVER HINGE (B)R () / FUSELAGE MAIN LANDING GEAR ACTUATOR FITTING. SB ATR SB ATR COMPLIED AS PER A/C LIST AT DELIVERY (B)R0 KARMN FAIRING PANEL FASTENERS (B)R1 FLIGHT CONTROLS - RUDDER NOT APPLICABLE DUE TO MSN AFM UPDATE POWER LEVEL POSITIONING ALREADY ACCOMPLISHED BY MANUFACTURER (B)R () / ENGINE MOUNT AND UPPER ENGINE FAIRING STIFFENER FOULING. COMPLIED AS PER A/C LIST AT DELIVERY (B)R () / ROTOR RECIRCULATION FAN. SB ATR SB ATR SB ATR COMPLIED AS PER A/C LIST AT DELIVERY () (B)R1 / RUDDER AND VERTICAL STABILIZER SB ATR ALREADY ACCOMPLISHED BY MANUFACTURER. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 2 of 18

3 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) (B)R0 EXT WINGS-INNER SKIN SURFACE/REAR SPAR JUNCTION (b)R (B)R (B)R1 F R () ELECTRICAL SYSTEM DC GENERATOR (ATA 24) CANCELLED / ICING CONDITIONS - REVISE THE AIRPLANE FLIGHT MANUAL (ATA30). CANCELS THE ORIGINAL AD T TELEGRAPHICALLY ISSUED ON AD COPY INSERTED TO AFM () (B) WING AND TAIL LEADING EDGE PNEUMATIC DE- ICING BOOT SYSTEM. SI/ / 2358:29/ 2552 COMPLIED DURING YRLY RAMP CHECK. AD COPY INSERTED TO AFM (B)R (B)R () / SEVERE ICING CONDITIONS - IMPLEMENT AIRCRAFT DESIGN ENHANCEMENTS (ATA30). SB ATR R01 REMOVAL INSTALLATION / 4404:30/ 4945 CHECK (B) AIR TRAFFIC CONTROL MODE A/C AND 5 ON BOARD TRASNPONDER SYSTEM SI/ 1264 TEST / 3065:13/ 3403 COMPLIED DURING C CHECK (AB)R (AB)R /3(RLD) SEAT BELT ATTACHMENT FITTING. SI/ 1273 SB / 4495:24/ / 4829:12/ 5454 CHECK. CHECK. SUPERSEDED BY (B)R () / FIRE PROTECTION - FIRE HANDLES (ATA26) ATR R01 SI/ / 6682:06/ 7532 COMPLIED DURING WEEKLY CHECK WO: (B)R0 STRUCTURE - RESULT OF FATIGUE TESTS (ATA 52) (B)R () / ENGINE CONTROLS - FLIGHT MANUAL PROCEDURES ASSOCIATED WITH REVERSE APPLICATION. AD COPY INSERTED TO AFM (B)R () / TAKE-OFF AFTER USE OF TYPE-II OR IV FLUIDS - APPENDIX TO THE FLIGHT MANUAL (ATA 04) SI/ 1305 UPDATE / 4254:24/ 4768 CHECK. AD COPY INSERTED TO AFM (B)RO ELECTRICAL SYSTEM - ENGINE START SELECTOR (ATA 24, 80) () (B)R1 / LANDING GEARS - INSTALL MODIFIED UP-LOCK BOXES (ATA 32) SB SI/ / 4259:24/ 4772 CHECK. CARRIED OUT ON NOSE, LH AND RH (AB)R1 ROCKWELL COLLINS CTL-92 TRANSPONDER. Collins SBCTL dtd 05 Apr THE AD NOT AFFECTED DUE TO SERIAL NO. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 3 of 18

4 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) (AB)R (AB)R2 VHF RADIO NAVIGATION AND LANDING RECEIVERS FM IMMUNITY (ATA 34) NOT APPLICABLE TO PN INSTALLED (B) PROP FEATHERING ATPCS TEST SELECTOR SWITCH (ATA 24, 61) SI/ / 7331:23/ 8285 CHECK WO: (B)R1 FLIGHT CONTROLS - NORMAL PITCH TRIM SWITCHES (ATA 27) SI/ 1374 SB ATR SI/ 1372 SB ATR INSTALLATION RESTORATION / 7331:23/ / 6723:48/ 7586 CHECK WO: CHECK WO: (B) (B)R1 MAIN LANDING GEAR - SWINGING LEVER SPACER (ATA32) ATR Mod 5338 CANCELLED REPLACED BY AD (B) (AB) (RLD) BACKREST LINK (9G SEATS (ATA 05, 25) EO T C SB SWI ST R / 23283:03/ COMPLIED DURING WEEKLY CHECK WO: (B) MAIN LANDING GEAR - SWINGING LEVER SPACER (ATA32) SB ATR R02 SB / 16506:58/ COMPLIED AS PER SINGAPORE PRECISION REPAIR AND OVERHAUL PTE LTD. CARRIED OUT ON LH AND RH (B) F / THERMAL/ACOUSTICAL INSULATION MATERIALS (ATA 25). SB ATR R02 ACCOMPLISHMENT THROUGH AD F R1 / NOTIFICATION OF CANCELLATION OF AD NO ACTION REQUIRED ATC TRANSPONDER(S) () BLA INERTIAL REFERENCE UNIT (IRU) P/N HG1075AB (AB) ROCKWELL COLLINS AIR DATA COMPUTER COFFEE MAKER, WATER BOILER/BEV MAKER WIRING (AB) NAVIGATION - FLIGHT MANAGEMENT COMPUTERS. NOT APPLICABLE DUE TO TYPE & MANUF. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 4 of 18

5 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) EQUIPMENT/FURNISHINGS - RESTRAINT SYSTEMS /. / (B) PROP PITCH CHANGE SYSTEM COMPONENT. NOT APPLICABLE DUE TO A/C & PROP MODEL (B) WIRE BUNDLE ROUTING ON AND 95VU CARBON SHELVES (ATA 92). SB ATR MOD EO T R / 7428:33/ 8406 CHECK WO: (AB)R (AB)R (AB)R /2(RLD) /3 (RLD) EQUIPMENT/FURNISHINGS RESTRAINT SYSTEMS -/ - SAFETY BELTS AND RESTRAINT SYSTEMS TYPE Anjou Aeronautique SB EO T C R00 / / 7338:34/ 8291 CHECK WO: (AB)R (AB)R /2(RLD) /3(RLD) BLA /2(RLD) (AB)R1 SAFETY BELTS AND RESTRAINT SYSTEMS TYPE 343. SICMA AERO SEAT. SPI NO SB SB / 4829:12/ 5454 CHECK. SUPERSEDES AD BLA (RLD) CAA AIR CARGO PALLETS & AIR CARGO NETS. NOT APPLICABLE DUE TO TYPE & MANUF MPR / ROCKWELL COLLINS TDR-94 MODEL TRANSPONDERS. NOT APPLICABLE DUE TO ADC INPUT IMP(B) TRANSPONDER MODE C621A (B) CARGO NET ASSEMBLY. NOT APPLICABLE AS PER THE PART (B) FLT CONTROLS - PITCH CONTROL INTERFERENCE SB ATR SB ATR EO T / 9559:49/ COMPLIED DURING 3C CHECK WO: COMPLIED ON LH AND RH (B) (AB) SICMA AERO SEATS - PASSENGER SEAT, CENTRAL SPREADS. SB (AB) (AB) SICMA AERO SEATS - PASSENGER SEATS 9801 AND 9802 SERIES. NOT APPLICABLE DUE TO P/N AND TYPE (B) FORWARD ATTENDANT SEATS (ATA 25) SB ATR SICMA SB EO T / 10052:15/ CHECK WO: Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 5 of 18

6 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) IMP(AB) / AFD-3010 FLIGHT DISPLAY UNITS EMERGENCY EVACUATION SLIDE/RAFTS (AIR CRUISERS CO.) HONEYWELL INTEGRATED NAVIGATION UNIT P/N (INU) NOT APPLICABLE DUE TO P/N AND TYPE ANJOU AERO SAFETY BELTS & RESTRAINT SYSTEM INSP. Anjou SB / EO T C NOT APPLICABLE TO A4O-AL NAVIGATION - TRANSPONDER - /. / NOT APPLICABLE DUE TO VENDOR AND P/N (AB) MODE 'S' INTERROGATION INC. NOT APPLICABLE AS PER P/N & VENDOR. F MP AIRCRUISER COMPANY EMERGENCY EVALUATION SLIDE. MODEL (B)R1 FLT CONTROLS- STAND-BY PITCH TRIM SWITCH (ATA92) SB ATR R01 EO T R / 9147:04/ CHECK WO: IMP R1 A/C EQPD WITH HONEYWELL INTEGRATED NAV UNIT MODEL (B) MAIN LANDING GEAR - SWINGING LEVER (ATA32) NOT APPLICABLE DUE TO AIRCRAFT MODEL. F EQPT/FURNISHING - THERMAL/ACOUSTICAL MATERIALS AD SUPERSEDED BY F SHIFTING OF UNRESTRAINED CARGO WHICH COULD CHANGE OF C OF G AND CAUSE POSSIBLE LOSS OF CONTROLLABILITY OF THE A/C. TO UPDATE AFM. UPDATE COMPLIED AS PER FLT. OPS. NOTIFICATION FORM FOTR/006/05. F TA/RA VSI-TCAS INDICATOR. CANCELLED AD IS CANCELLED BY ITS REV.1 F / TCAS INDICATOR EO T R00 SB ATR R00 SB R04 F/O SIDE CAPTAIN SIDE / 15818:36/ / 15818:36/ CHECK WO: CHECK WO: Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 6 of 18

7 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) F LANDING GEAR - SECONDARY SIDE BRACE. NOT APPLICABLE DUE TO AIRCRAFT MODEL. F B LANDING GEAR - MAIN LANDING GEAR SIDE BRAKE. AIRCRAFT TYPE. F OPERATIONAL ORDER ON INSTRUCTION FOR CONTINUED AIRWORTHINESS. FOR INFORMATION ONLY (B) (B) R / VERTICAL STABILIZERS - INSP ON FIN TIP CLOSURE RIB SB ATR R / 15702:44/ COMPLIED AS PER AIR DECCAN REF. DGCA MOD ATR42/133. REPEAT REQUIREMENT OF 550FH TERMINATED DUE TO OF EO T COMPLIED DURING COMPLIED DURING AIR DECCAN EO REF. ATR42/1331. AD SUPERSEDED BY AD GODORICH PROP DE-ICERS NOT APPLICABLE TO OMAN AIR FLEET TO PREVENT DISCREPANCIES BETWEEN ELEVATOR TRIM TAB CONTROL ROD AND FWD EDGE OF LOWER SKIN OF THE ELEVATOR SB ATR SB ATR EO T R00 ACCOMPLISHMENT THROUGH AD (B) AVIO INTERIOR BOXMOUNTED SEATS. VENDOR & PART NUMBER TO PREVENT FATIGUE CRACKS OF THE CARGO DOOR SKIN NOT APPLICABLE DUE TO AIRCRAFT SERIES AIR DATA COMPUTER F LANDING GEAR - MLG - SIDE BRACE ASSY. F R1 LANDING GEAR - MLG - SIDE BRACE ASSY. CANCELLED INSTALLED. MODEL NUMBERS. NOT APPLICABLE - THIS CANCELS AD F F EQPT/FURNISHING OF READING LIGHTS/ ELECT POWER SUPPLIES OF SICMA SEATS. SERIES. UF FUEL QUANTITY INDICATOR SWI T RECORDING / 12258:13/ COMPLIED DURING AIRDECCAN 2A/1K FH+1A/500FH CHECK REF. DGCA/ATR42/ Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 7 of 18

8 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) OF SMOKE DETECTOR AMENDMENT MLG SIDE BRACE ASSY PART PART NUMBERS PROTECTIVE GUARD OF STANDBY PUTCH TRIM SWITCH SB ATR R01 EO T R01 ACCOMPLISHMENT THROUGH AD (B)R F WINGS OUTER WING BOXES UPPER SKIN AND RIBS. SB ATR EO T / 10780:44/ COMPLIED DURING YRLY+OUT-OF- PHASE CHECK WO: SICMA SEAT NOT APPLICABLE TO WY FLEET DELAMINATED BLADE FIBREFLASS REPAIR F SANDAL AVIONICS EQUIPMENT. MODEL. MODEL TREAD SEPARATIONS AND TREAD AREA BULGES. PART INCORRECTLY SECURED BUSHINGS MODEL E / MLG SHOCK ABSORBER CROSS LOCKING BOLT OF ATTACHMENT PIN. SB R / 14981:49/ COMPLIED DURING AIR DECCAN OPERATION R FUEL TANK SAFETY - AIRWORTHINESS LIMINATIONS / 20957:45/ EVERY 12.5 YEARS OPEN/REPETITIVE COMPLIED DURING 1C+1/2/4/12 YRLY+6K+24K FC+400FH+C3/P9 CHECK WO: / & COMPLIED ON LH AND RH POS. SUPERSEDED BY AD EMERGENCY LOCATOR TRANSMITTER PART NAV SYSTEMS - MOD 'S & 'C' TRANSPONDER CHK. VENDOR NAVIGATION SYSTEMS - NOT APPLICABLE DIFFERENT VENDOR. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 8 of 18

9 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) ELECTRICAL POWER-120VU ELECT HARNESS INSP. SB ATR R / 15702:44/ COMPLIED AS PER AIRDECCAN REF. ADN/PL/169. SUPERSEDED BY AD E R1 OXYGEN RESERVE CYLINDERS - REMOVAL/EMPTYING REMOVAL PART F / VERTICAL STABILIZER - FIN TIP UPPER CLOSURE RIB INSP. ATR R / 15702:44/ COMPLIED AS PER AIRDECCAN REF. ADN/PL/171. SUPERSEDES AD EQPT/FURNISHING - PAX SEATS BRACKETS NOT APPLICABLE TO PART FITTED FLT CONTROLS - AILERON TAB BELLCRANK ASSY - INSP. NOT APPLICABLE DUE EMBODIED AT PRODUCTION BONDING LEAD ON 120VU EO T R01 SB ATR ACCOMPLISHMENT THROUGH AD SUPERSEDES AD E THERMAL ACOUSTICAL INSULATION BLANKETS SB ATR REMOVAL INSTALLATION ACCOMPLISHED THROUGH AD AS PER AIR DECCAN OPERATION MLG - SIDE BRACE ASSY COMM UNITS & TRANSPONDERS SERIES. VENDORS F F R1 / EQPT/FURNISHING - THERMAL/ACOUSTICAL MATERIALS SB ATR R02 REMOVAL INSTALLATION / 16225:17/ CARRIED OUT DURING OUT-OF-PHASE CHECK WO: CARRIED OUT WORKPACKAGE 1 AND 2. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 9 of 18

10 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) (B) / ICE&RAIN PROTECTION EO T R02 SB ATR R01 EO T R02 SB ATR R / 18350:32/ / 18498:17/ COMPLIED DURING WEEKLY CHECK WO: COMPLIED DURING 1C+2C+2YRLY+6K+O/P CHECK WO: / FUEL TANK SYSTEM WIRING & SENSORS. SB ATR R05 EO T R / 18498:17/ COMPLIED DURING 1C+2C+2YRLY+6K+O/P CHECK WO: SEAT RESTRAINT SYSTEM ROTARY BUCKLE - TYPE MLG - SIDE BRACE ASSY SERIES F DGAC OF THE ZIPPER ON THE LIFE VEST S AVAILABILITY ELECTRICAL/ ELECTRONIC- REAR PRESSURE BULKHEAD AREA AND WIRE CHAFING AND EO T R02 SB ATR R00 EO T R03 SB ATR R / 17806:56/ / 17806:56/ CHECK WO: CHECK WO: EQUIPMENT AND FURNISHING- PASSENGER SEAT SB REPAIR NOT APPLICABLE TO PART FITTED. AD SUPERSEDED BY AD EQUIPMENT AND FURNISHING- PASSENGER SEAT SB REPAIR NOT APPLICABLE TO PART FITTED. AD SUPERSEDES AD DGAC FLAPS-USE OF THE 45 DEGREE CONFIGURATION PROHIBITION NOT APPLICABLE TO AIRCRAFT TYPE EU AB DGAC EQUIPMENT AND FURNISHING- PASSENGER SEAT BACKREST NOT APPLICABLE TO PART FITTED. EU NAVIGATION SYSTEMS- MODE S TRANSPONDERS LIMITATION NOT APPLICABLE TO AIRCRAFT AND PART FITTED. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 10 of 18

11 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) EU NAVIGATION SYSTEMS- MODE S TRANSPONDERS NOT APPLICABLE TO AIRCRAFT AND PART FITTED. EU NAVIGATION-MODE S TRANSPONDER S USED. N A GARMIN INTERNATION INC. GSM 85 SERVO GEARBOX UNITS NOT APPLICABLE TO AIRCRAFT AND PART FITTED. EU DGAC WIRE BUNDLES IN THE REAR BAGGAGE ZONE SB ATR PROTECTION CLAMPING NOT APPLICABLE DUE TO MSN NO. N PFD DISPLAYING INCORRECT FLIGHT DATA NOT APPLICABLE TO PART FITTED AILERON TAB BELLCRANK ASSEMBLIES SB ATR SB ATR SB ATR SB ATR SB ATR NOT APPLICABLE AS ATR MOD WAS ALREADY CARRIED OUT DURING THE PRODUCTION ICE&RAIN PROTECTION SB ATR R01 SB ATR R00 ACCOMPLISHMENT THROUGH AD LANDING GEAR- FOR CRACKING OF THE MLG SIDE BRACE SB NOT APPLICABLE TO AIRCRAFT TYPE SOFTWARE UPDATE TO VERSION 241J SB 8140-XXX UPDATE NOT APPLICABLE DUE TO WY EQUIPPED WITH HONEYWELL NAVIGATION NAVIGATION - MODE S TRANSPONDER - CHECK/ EO T R00 SB ATR R00 CHECK/ / 19260:49/ COMPLIED DURING WEEKLY CHECK WO: SUPERSEDED BY AD Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 11 of 18

12 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) EU DGAC INDICATING/RECORDING SYSTEM- MULTI- PURPOSE COMPUTER (MPC) WITH AIRCRAFT PERFORMANCE MONITORING (APM) FUNCTION INSTALLATION EO T R05 SB ATR R / 24542:08/ COMPLIED DURING 1/2/4C+1/2 YRLY CHECK WO: ,3880,81, NAVIGATION - MODE S TRANSPONDER - / SB TDR-94/94D SB TDR-94/94D OMAN AIR ATR FLEET FALLS UNDER EXEMPTION PARA. 4 OF THIS AD. INITIAL NO.2/ RH / 19190:01/ INITIAL OF 2000 FC AFTER. CHECK WO: E WINDOWS-COCKPIT FORWARD SIDE WINDOWS- AND SB NP R00 EO T R00 REPEAT NO.2 LH AND RH / 20706:18/ EVERY 550FH OR 750FC WHICHEVER COMES 1ST REPEAT OF EVERY 550FH OR 750FC WHICHEVER COMES FIRST IS TERMINATED DUE NO.2/RH SIDE HAS BEEN REPLACED AS PER NRDC NO DTD WO: / & PART / 20957:45/ COMPLIED DURING 1C+1/2/4/12 YRLY+6K+24K FC+400FH+C3/P9 CHECK WO: / & CARRIED OUT ON LH NRDC NO AND RH NRDC NO US OXYGEN- OXYGEN CYLINDER ASSEMBLIES SB SB A1126 NOT APPLICABLE TO NOT APPLICABLE DUE AFFECTED SN's ARE NOT FOUND IN EITHER OMAN AIR STOCKS OR ON INSTALLED ON AIRCRAFT NAVIGATION MODE S TRANSPONDER CHECK/ INSTALLED FUEL SAFETY TANK - FUEL AIRWORTHINESS LIMITATIONS SUPERSEDES AD R E FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERS - IDENTIFICATION/ IDENTIFICATION NOT APPLICABLE DUE TO P/N, OMAN AIR P/N IS Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 12 of 18

13 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) R FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/ FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/ IDENTIFICATION IDENTIFICATION NOT APPLICABLE DUE AFFECTED SN's ARE NOT FOUND IN EITHER OMAN AIR STOCKS OR ON INSTALLED ON AIRCRAFT NOT APPLICABLE DUE AFFECTED SN's ARE NOT FOUND IN EITHER OMAN AIR STOCKS OR ON INSTALLED ON AIRCRAFT. SUPERSEDED BY AD IDENTIFICATION OF OIT SUBJECT ATA SICLI PORTABLE FIRE EXTINGUISHER IDENTIFICATION IDENTIFICATION NOT APPLICABLE DUE TO PN INSTALLED AND AVAILABLE IN INVENTORY NAVIGATION- MODE S TRANSPONDER A/C TYPE MODE STRAPPING - CHECK/ CHECK NOT APPLICABLE DUE TO P/N, OMAN AIR FLEET ARE FITTED WITH MODE S XPONDER P/N / EQUIPMENT/ FURNISHINGS- EMERGENCY PARACHUTES REWORK NOT APPLICABLE DUE PART NOT INSTALLED ON WY FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/ IDENTIFICATION/ NOT APPLICABLE DUE AFFECTED SN's ARE NOT FOUND IN EITHER OMAN AIR STOCKS OR ON O/B AIRCRAFT. SUPERSEDES AD FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/ IDENTIFICATION/ NOT APPLICABLE DUE AFFECTED SN's ARE NOT FOUND IN EITHER OMAN AIR STOCKS OR ON O/B AIRCRAFT SICMA AERO SEAT - CENTRAL SPREADER NOT APPLICABLE DUE TO P/N, OMAN AIR FLEET ARE FITTED WITH PAX SEAT FROM DIFFERENT MANUFACTURER OF SICLI PORTABLE FIRE EXTINGUISHER H1-10 AIR FILLED WITH CONTAMINATED HALON 1211 NOT APPLICABLE DUE TO PN INSTALLED AND AVAILABLE IN INVENTORY US HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/ INU's - AIRCRAFT FLIGHT MANUAL REVISION/ ASB ISSUE A IDENTIFICATION NOT APPLICABLE DUE OMAN AIR DUE AFFECTED SN's LISTED IN APPDX 1 OF FFE ASB ARE NOT FOUND IN OMAN AIR INVENTORY. NOT APPLICABLE DUE OMAN AIR ATR FLEET IS FITTED W/ HONEYWELL IRS(AHRU) P/N , WHICH IS DIFFERENT FROM THOSE LISTED IN THE AD. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 13 of 18

14 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) NAVIGATION- ATC- MOFICATION WEIGHT ON WHEEL INPUTS ON ATC/ MODE S TRANSPONDERS EO T R00 SB ATR R00 COMPLIED THRU AD SUPERSEDES AD US NAV - PRIMUS EPIC & APEX FMS - A/P FLIGHT MANUAL REV NOT APPLICABLE TO OMA ATR AS THEY ARE FITTED WITH HONEYWELL GNSS S/W P/N H. US INSP OF AVOX SYSTEMS & B/E AEROSPACE 114/115 CF OXYGEN CYLINDERS NOT APPLICABLE TO OMA FLEET, INVESTIGATION C/OUT FOUND NIL OF THE AFFECTED P/N's AND S/N's EITHER INSTALLED ONBOARD AIRCRAFT OR HELD IN STORES STABILIZERS - ELEVATOR INBOARD HINGE FITTING LOWER STOP ANGLES - / ATR R01 EO T R / 20957:45/ COMPLIED DURING 1C+1/2/4/12 YRLY+6K+24K FC+400FH+C3/P9 CHECK WO: / & COMMUNICATION- VHF/AM TRANSCEIVER NOT APPLICABLE DUE TO WY FITTED WITH ROCKWELL COLLINS MODE S TRANSPONDER - / NOT APPLICABLE DUE OMAN AIR ATR FLEET ARE EQUIPPED WITH MODE S TRANSPONDER BUT INSTALLED WITH HONEYWELL ADC US B/E AEROSPACE PBE P/N INSTALLED ON VARIOUS TRANSPORT AIRPLANES B/E ASB /-6 NOT APPLICABLE TO OMAN AIR ATR FLEET DUE TO DIFF. S/N's PREVENT FLIGHT SAFETY HAZARDS CAUSED BY CURRENT DESIGN OF OXYGEN GENERATORS NOT APPLICABLE DUE OMAN AIR IS NOT OPERATING UNDER 14 CFR PART 121 OR 129, BUT UNDER DGSAS CAR. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 14 of 18

15 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) RESTORATION FIRST OFFICER / 25535:28/ CHECK WO: SN: SE OXYGEN MASK REGULATOR INFLATABLE HARNESS - IDENTIFICATION/ EO T C SB MXH R07 RESTORATION CAPTAIN / 24515:57/24771 SN: SE RESTORATION OBSERVER / 28300:01/ SN: B US PAX OXYGEN MASK SYSTEM MASK IN-LINE FLOW INDICATOR SB R00 EO T R / 25283:23/ CHECK WO: SICMA AERO SEAT EO T C SB SWI ST R00 ACCOMPLISHED THROUGH AD PAX SEAT ASSEMBLIES - 94XX SERIES - LATERAL AND CENTRAL SPREADERS CHECKING PROCEDURES SB R03 BOTH AD's ARE NOT APPLICABLE DUE OMA ATR FLEET ARE FITTED W/9619- SERIES SEATS. SUPERSEDED BY AD STABILIZERS - LH & RH ELEVATORS - INBOARD HINGE FITTINGS - INSP OF LOWER STOP FITTING ANGLES ATR R01 EO T R02 ACCOMPLISHMENT THROUGH AD NAVIGATION - REPORTS OF ANOMALIES W/TCAS UNITS DURING A FLIGHT TEST OVER HIGH DENSITY AIRPORT NOT APPLICABLE DUE OMA ATR FLEET ARE FITTED W/TCAS P/N PAX SEAT ASSEMBLIES - 94XX SERIES - LATERAL AND CENTRAL SPREADERS CHECKING PROCEDURES AD SB R03/ -012R01/-013R4 BOTH AD's ARE NOT APPLICABLE DUE OMA ATR FLEET ARE FITTED W/9619- SERIES SEATS. SUPERSEDES AD FIRE PROTECTION- HAND OPERATED FIRE EXTIGUISHER SB A NOT APPLICABLE DUE TO PN INSTALLEED FLIGHT CONTROLS - RUDDER TAB, RUDDER PEDAL AND ELEVATOR CONTROL RODS - / AD E NOT APPLICABLE TO OMAN AIR ATR FLEET DUE TO MSN PREVENT FLIGHT SAFETY HAZARDS CAUSED BY CURRENT DESIGN OF OXYGEN GENERATORS NOT APPLICABLE DUE OMAN AIR IS NOT OPERATING UNDER 14 CFR PART 121 OR 129, BUT UNDER DGSAS CAR. SUPERSEDES AD Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 15 of 18

16 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) NACELLES/PYLONS - ENGINE NACELLE LOWER FAIRING JUNCTION WITH UNDERWING BOX - SB ATR R00 EO T R / 27929:20/ EVERY 4000FC OPEN/REPETITIVE COMPLIED DURING 8YRLY + LOWER CHECKS WO: CARRIED OUT ON LH AND RH. FR 26 FLOOR BEAM - DETAILED VISUAL OF THE FLOOR BEAM AT FRAME 26, ON BOTH LEFT HAND (LH) AND RIGHT HAND (RH) SIDES. IAW ATR42 AMM JIC DVI TASK REF DVI DETAILED VISUAL / 27929:20/ REPEAT EVERY 12,000 CYC OPEN/REPETITIVE COMPLIED DURING 8YRLY + LOWER CHECKS WO: FUSELAGE CENTER SECTION - DETAILED VISUAL OF FLOOR BEAM FRO CRACK DETECTION OF FLOOR BEAM AT FRAME 26 FOR CRACK DETECTION AROUND CUT-OUTS FOR ELECTRICAL/ELECTRONICS COOLING DUCTS AND HYDRAULIC PIPES INSTALLATION. TASK REF DVI DETAILED VISUAL / 27929:20/ REPEAT EVERY 12,000 CYC OPEN/REPETITIVE COMPLIED DURING 8YRLY + LOWER CHECKS WO: OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION / OPERATIONAL PROCEDURE / SB MCF-SBU IDENTIFICATION NOT APPLICABLE DUE TO OMA FLEET BY SERIAL NUMBER EQUIPMENT/FURNISHINGS - SAFETY BELTS/TORSO RESTRAINT SYSTEM - / EO T C R / 25859:44/ CHECK WO: CARRIED OUT PART I,II,III ICE AND RAIN PROTECTION - PNEUMATIC ICE PROTECTION DUAL DISTRIBUTOR VALVES - / SB ATR SB ATR NOT APPLICABLE DUE TO OMA FLEET BY MSN WINDOWS-COCKPIT FORWARD SIDE WINDOWS- AND SB NP R00 EO T R00 / ACCOMPLISHMENT THROUGH AD E. SUPERSEDES AD E CF AIR TRASNPORT ASSOCIATION (ATA) OF AMERICA CODE 23 COMMUNICATION SB A22 EO A C NOT APPLICABLE DUE TO ATR FLEET EQUIPPED WITH SOCATA ELT EQUIPMENT/FURNISHINGS - TYPE III EMERGENCY EXIT DOOR - / SB ATR R0 / NOT APPLICABLE DUE TO OA ATR FLEET ARE NOT EMBODIED WITH MOD 6518 DURING PRODUCTION. MOREOVER, SB ATR R0 IS NOT AAPLICABLE TO OA ATR FLEET R01 ELECTRICAL ROUTING - ELECTRONICS RACK 90VU SHELF / ELECTRICAL HARNESS - SB ATR R00 EO T R / 26411:21/ ACCOMPLISHMENT THROUGH SB ATR CARRIED OUT DURING OUT-OF-PHASE CHECKS WO: Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 16 of 18

17 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) ELECTRICAL ROUTING - ELECTRONICS RACK 120VU SHELF / ELECTRICAL HARNESS - / SB ATR / NOT APPLICABLE BY MSN NAVIGATION- MODE S TRANSPONDER TEST/ CALIBRATION DETAILED OF COCKPIT FWD SIDE WINDOWS TO DETECT FOR DAMAGE PPG SB NP EO T R00 SUPERSEDES AD LANDING GEAR - MAIN LANDING GEAR HINGE PIN - / SB SB / NOT APPLICABLE DUE TO PIN P/N FITTED ON OA FLEET ARE NOT AFFECTED BY THE REF. SB's R01 FUEL PROBES - / SB ATR SB ATR TN / NOT APPLICABLE DUE TO OA FLEET ARE EMBODIED W/MOD DURING PRODUCTION EQUIPMENT/FURNISHINGS- CRASH POSITION INDICATOR SYSTEM-, AIRCRAFT FLIGHT MANUAL- AMENDMENT NOT APPLICABLE DUE TO WY NOT EQUIPPED WITH CRASH POSITION INDICATOR SYSTEM EQUIPMENT/FURNISHINGS- CRASH POSITION INDICATOR SYSTEM-, AIRCRAFT FLIGHT MANUAL- AMENDMENT NOT APPLICABLE DUE TO WY NOT EQUIPPED WITH CRASH POSITION INDICATOR SYSTEM OXYGEN- OXYGEN MASK REGULATOR INFLATABLE HARNESS/ INFLATION HOSE IDENTIFICATION/ NOT APPLICATION BY PN FIRE PROTECTION - ENGINE FIRE EXTINGUISHING PIPE - SB ATR NOT APPLICABLE BY MSN AIR TRASNPORT ASSOCIATION (ATA) OF AMERICA CODE 23 COMMUNICATION NAVIGATION- MODE TRANSPONDER AIRCRAFT TYPE MODES STRAPPING- CHECK/ AD SB A22 EO A C CHECK/ NOT APPLICABLE DUE TO ATR FLEET EQUIPPED WITH SOCATA ELT. NOT APPLICATION DUE TO PARTS INSTALLED EQUIPMENT/ FURNISHING- SAFETY BELT ATTACHMENT BOLTS- / NOT APPLICATION DUE TO PARTS INSTALLED EQUIPMENT/ FURNISHING- RESTRAINT SYSTEM ROTARY BUCKLE SUB-ASSEMBLY SB 358SB IDENTIFICATION/ NOT APPLICATION DUE TO PART MODEL TYPE FIRE PROTECTION- ENGINE FIRE EXTINGUISHING PIPE SB ATR NOT APPLICATION DUE TO MSN. - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 17 of 18

18 A4O-AT AIRWORTHINESS (AIRFRAME AND APPLIANCE) AIRFRAME EQUIPMENT/ FURNISHING- TYPE III EMERGENCY EXIT DOOR ZODIAC AEROTECHNICS FLT. CREW OXYGEN MASK SB MXH R07 EO T C NOT APPLICABLE DUE TO WY NOT EMBODIED WITH SUPERSEDES AD NO FURTHER ACTION REQUIRED. EQUIVALENT TO AD HAS BEEN ACTIONED. Certified by: SM - Quality Assurance - Not Applicable - Rqmnt is fully complied with CANCELLED - AD has been cancelled Page 18 of 18