Airbus A320-232

Service difficulty reports · 32,652

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320232'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2025032000285Tail Cone · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SB-53-1500 TAIL CONE / LH/RH FIREWALL / BTWN FR81-83 / DEVIATION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0008-25 (COVER + PART 1) REV 0 /2/ AIRBUS RDAF 81545334/003/2025#A /3/ AIRBUS TD/81545334/007/20Mar 19, 2025 · N766JB · Airbus A320232 · Aerodynamic FairingsSDR YENA2025032000284Stringer · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / BTWN FR54-61 AT STGR 38L / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0008-25 (COVER + PART 1) REV 0 /2/ AIRBUS RDAF 81545334/003/2025#A /3/ AIRBUS TD/81545334/007/2025#A. DESCRIPTION: DURING THMar 19, 2025 · N766JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025032000283Skin · crackedDURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / RH LOWER SKIN TRAILING EDGE AT RIB 10 / CRACK - PERMANENT REPAIR; REFERENCES: /1/ ETD2025-190-903379 REV / /2/ SRM II 57-10-010 REPAIR 54P. DESCRIPTION: ON 3/5/2025, DURING THE LEASE RETURN CHECK FOR Mar 19, 2025 · N766JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2025032000282Skin · corrodedDURING HEAVY MAINTENANCE: WING / LH WING / SLAT # 3 / TOP SKIN TE OUTBD END / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0010-25 (COVER & PART 1 REV 0) /2/ AIRBUS DOSSIER REFERENCE: 81544590 /3/ RDAF 81544590/003/2025#A. DESCRIPTION: DURING CMar 19, 2025 · N766JB · Airbus A320232 · Leading Edge DevicesSDR YENA2025032000281Skin · crackedDURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / RH LOWER SKIN TRAILING EDGE AT RIB 10 / CRACK - PERMANENT REPAIR; REFERENCES: /1/ ETD2025-190-903379 REV / /2/ SRM II 57-10-010 REPAIR 54P DESCRIPTION: ON 3/5/2025, DURING THE LEASE RETURN CHECK FOR NMar 19, 2025 · N766JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2025032000280Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE LOC. BTW FR64 TO FR 65 AND BTW STR 30R T O STR 31R IN AFT CARGO COMPARTMENT. (SKIN); REF AEROMAN W/O:2025 84/1 NR 2025 -125815; PERFORMED PERMANENT REPAIR LOC. BTW FR64 TO FR 65 AND BTW STR 30R TO STR 31R Mar 19, 2025 · N766JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025032003016Skin · contaminatedR.H ELEVATOR HAS LIQUID INGRESS AT 180.5IN FROM I/B END, 10IN FR OM TRAILING EDGE. 1IN DIAMETER. REPAIRED RH ELEVATOR 180.5 IN FROM I/B 10IN FROM T/E 1.5IN DIAME TER ZONE A IAW A320 SRM 55-21-11-300-005 CATEGORY A REPAIRMar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025032003013Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS TOP SIDE AT 131.5 IN FROM I/B EN D, 6.5 IN FROM TRAILING EDGE 3IN IN DIAMETER. REPAIRED LH ELEVATOR 131.5 IN FROM IB AND 6.5 IN FROM TE IAW SRM 55-21-11-300-005.Mar 19, 2025 · N460UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025032003012Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS TOP SIDE AT 159 IN FROM I/B END, 12IN FROM TRAILING EDGE , 1 IN IN DIAMETER. REPAIRED L/H ELEVATOR TOP SIDE OF 159IN FROM INBOARD END, 12IN FROM TRAILING EDGE. 1INCH IN DIAMETER AS REQUIRED IN ZONE A IAW A320 SRM 55-21-11-300-Mar 19, 2025 · N460UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025032003008Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS AT 168.5IN FROM I/B END, 4.5IN F ROM TRAILING EDGE, 1IN DIAMETER.Mar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025032002995Skin · dentedR/H ELEVATOR HAS LIQUID INGRESS AT 74.5 FROM I/B END, 8IN FROM T RAILING EDGE, 1IN DIAMETER. GENERATED BY V061632 ON HAECO LCQ NR 9292782/34782 ESFR COMPLETE REPAIRED RH ELEVATOR 74.5 IN FROM I/B 8 IN FROMT/E 1.5IN DIAMETE R IAW A320 SRM 55-21-11-300-005 CATEGMar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/SkinSDR YENA2025032000279Bearing · damagedDURING HEAVY MAINTENANCE: RUDDER HINGE #4 FORK-END BEARING ASSEMBLY REQUIRES REPLACEMENT; (RESOLVED ON W/O: 1396851 TASKCARD: NR-00004) REF STS WO# W003815. N/R# N0020. REMOVED AND REPLACED RUDDER HINGE #4 FORK-END BEARING ASSEMBLY PER A320 AMM 27-21-41-400-00Mar 18, 2025 · N636JB · Airbus A320232 · Rudder StructureSDR YENA2025031900274Pump · faultedFLT#2096, CUN-FLL. (AIRCRAFT DECLARED AN EMERGENCY INTO FLL) 'HYD G RSVR LO LVL ECAM MSG. EMG 1 PUMP AND PTU OFF ACCORDING TO ECAM.' (SUPPLEMENTAL INFORMATION TO FOLLOW)Mar 18, 2025 · N613JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR YENA2025031900273Unknown · odorFLT#2904, RSW-BDL. 'ODOR/ FUME EVENT. DURING DESCENT FA'S IN AFT GALLEY REPORTED A FUEL SMELL IN THE FLIGHT DECK WE SMELLED A DIRTY SOCK SMELL. ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)Mar 18, 2025 · N715JB · Airbus A320232 · Air Distribution SystemSDR CALA2025031902942Skin · damaged#1 ENG PYLON AFT FIXED FAIRING LOWER SKIN PANEL HAS 1EA CHAFED RIVIT HEAD WITH MATERIAL LOSS. ESFR COMPLETE RMVD AND RPLD 1EA RIVET AT #1 ENG AFT FIXED FAIRING LOWER SKIN PNL IAW A320 SRM 51-42-11.Mar 18, 2025 · N459UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR CALA2025031902941Skin · damaged#1 ENG PYLON AFT FIXED FAIRING INBD SIDE SKIN IS CRACKED AND HAS BROKEN/MISSING RIVETS. ESFR COMPLETE RMVD AND RPLD SKIN AT #1 ENG PYLON AFT FIXED FAIRING I/B IAW A320 SRM 54-54-11Mar 18, 2025 · N459UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR CALA2025031902957Skin · contaminatedLH ELEVATOR HAS LIQUID INGRESS AT 138 IN FROM INBOARD EDGE, 5.5I NIN FROM TRAILING EDGE, 1IN DIAMETER REPAIRED LH ELEVATOR IAW A320 SRM 55-21-11-300-005Mar 17, 2025 · N462UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025031802903Switch · malfunctionedFLIGHT CREW REPORTS EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN OFF POSITION UNDER GUIDANCE OF TOMC CREW CYCLED EMERGENCY LIGHT SWITCH ON AAP PANEL NEAR L2 DOOR, LIGHTS ARE NOW OFF. NO FURTHER ACTION REQUIRED. VARGAS TOMCMar 17, 2025 · N418UA · Airbus A320232 · Emergency LightingSDR CALA2025031702900Skin · contaminatedLH ELEVATOR HAS LIQUID INGRESS AT 52 IN FROM INBOARD EDGE, 5 IN FROM TRAILING EDGE, 2 IN DIAMETER.Mar 17, 2025 · N462UA · Airbus A320232 · Elevator, Plate/SkinSDR AALA202503170622Power Supply · no testAIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND SEAT 26C FLOOR POXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM INOP. MAINTENANCE REPLACED EPSU 11WL AND BATTERY ASSY IAW AMM 33-51-38.Mar 16, 2025 · N657AW · Airbus A320232 · Emergency LightingSDR YENA2025031900267Battery · no testFLT#591, BOS-TPA.'DURING OPS CHK OF EPSU SYS, BATT 11WL FAILED OPS CHECK; REMOVED AND REPLACED L/H OVERWING EPSU EMERG LIGHT BATT (11WL) IAW AMM 33-51-38. OPS CHECK GOOD. TEST PASSED. SYS OK FOR CONT SVC.'Mar 15, 2025 · N784JB · Airbus A320232 · Emergency LightingSDR CALA2025031802912Bottle · no discrepancySLIDE PRESSURE ON DOOR2L IS IN THE RED. REF AMM 25-62-00-210-001-A. INSPECTED SLIDE PRESSURE AND NEEDLE IS RIGHT BETWEEN GREEN AND RED BAND. ACCEPTABLE PER AMM INSPECTION REQUIREMENTS FOR MODEL A GUAGE.Mar 14, 2025 · N429UA · Airbus A320232 · Escape SlideSDR GTIA2025031838800Unknown · odorF/A INDICATED THE PRESENCE OF A BURMIMG PLASTIC SMELL COMING FROM LAV F -PERFORMED INSPECTION OF LAV F FOR ODOR/BURNING SMELL, NO DEFECTS NOTED REF TSM 05-50-00-810-831-A. A/C OK FOR SERVICE. REF DEFECT 3587851-2 FOR LAV F DEFERRAL.Mar 14, 2025 · N607NK · Airbus A320232 · Air Distribution SystemSDR CALA2025031702864Bracket · out of adjustDOOR R AFT EMER EXIT AT ALT IN LGT CHOP.CAB ALT AND V/S CAB PRESS NORM. REPEAT W/U LOCKING FOR POSITIVE FIX. FOUND ON COVER FLAP ASSY ON RT AFT EMERGENCY EXIT DOOR, BRACKET ASSY ON BACK OUT OF ADJUSTMENT. ADJUSTED BRACKET AS REQUIRED, COVER FLAP ASSY TIGHT Mar 14, 2025 · N453UA · Airbus A320232 · Emergency ExitsSDR CALA2025031702853Angle · crackedRH AFT TI-ANGLE IS CRACKED. ESFR COMPLETED REMOVED SECTION-CONNECTING (TI-ANGLE) ON RH AFT FR41-42 KEEL BEA M IAW A320 SRM 51-42-11/001 REV 152 REPLACED SECTION CONNECTING (TI-ANGLE) IAW A320 SRM 51-42-11/001 REV 152.Mar 14, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025031402829Slide · unknownA/C LEFT DOOR 2L SLIDE PRESSURE INDICATOR IS RED WITHIN LIMITS IN REF MM 25-62-00-210-001-AMar 14, 2025 · N489UA · Airbus A320232 · Escape SlideSDR CALA2025031402820Warning Message · false activationDOOR R FWD EMER EXITAND R AFT EMER EXITECAM NO AB CAB PSI DUPLICATE L/P, REF L/P 4138158 AND L/P 4137214, RH AFT AND AND RH FWD EMERGENCY OVERWING EMERGENCY DOOR WARNING INDICATION ARE CURRENTLY ON MEL.Mar 14, 2025 · N453UA · Airbus A320232 · Door Warning SystemSDR YENA2025031800266Servo Valve · failedFLT#1349, MHT-RSW. (AIRCRAFT DIVERTED TO JFK) ' LEFT ELEVATOR INTERMITTENT DEFLECTION RODUCED UNWANTED FLIGHT PATH (CHOPPY SENSATION) AFTER LANDING F/CTRL ELEVATOR SERVO FAULT PRESENTED WITH AMBER BRACKETS AROUND BLUE SYSTEM MESSAGE DISAPPEARED AFTER SHUTDOWN;Mar 13, 2025 · N651JB · Airbus A320232 · Elevator Control SystemSDR CALA2025031802908Slide · faultyR1 DOOR SLIDE PN- D30664-705 S/N- A5823 AND GIRT BAR REMOVED PER WORKCARD. PLACED UNDER FWD GALLEY. SAFETY PIN IS INSTALLED. STARTED INSTALLING R1 DOOR SLIDE REF TASK CARD 31-25-62-1-3810 UP TO BLOCK 16 COMPLETED R1 DOOR SLIDE INSTALLATION PER WORK CARD 31-2Mar 13, 2025 · N471UA · Airbus A320232 · Escape SlideSDR YENA2025031700259Unknown · odorFLT#1603, JFK-SJU. 'DURING FINAL DESCENT, SLIGHT ODOR OF OIL IN VENTS IN CLEAR AIR. PACK 1 SET TO OFF, XBLEED SHUT AND ODOR CEASED; C/W INFO NOTICE 2017-T015K SECTION A.ISOLATED FAULT TO TYPE 10 AMBIENT AIR. PERFORMED DECONTAMINATION OF THE ECS LEVEL A PER AMMMar 13, 2025 · N606JB · Airbus A320232 · Air Distribution SystemSDR CALA2025031702873Hydraulic Line · leakingHYD Y RSVR LO LVL FOUND MAJOR LEAK UNDER PYLON ,YELLOW RESERVOIR AT 0,UNABLE TO REPLENISH HYDRAULIC, ,RESERVOIR NOT RETAINING HYDRAULIC PIC UPDATE FOUND HYD LEAK COMING FROM HYD LINE IN PYLON PART # D2901010201200. PARTS ORDER WAITING ON CLAMPS REF AIPC 29-13-Mar 13, 2025 · N473UA · Airbus A320232 · Hydraulic System, MainSDR CALA2025031702852Angle · corrodedL2 PAX DOOR LOWER FWD ANGLE FITTING CORRODED. ESFR COMPLETE R & R CORNER FITTING AT L2 PAX DOOR LWR FWD IAW A320 SRM 51 -42-11 + SRM 51-72-11Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025031702851Floor Support · corrodedAFT WET AREA FLOOR SUPPORT Y160.5 FASTENER HOLES CORRODED APPROX. 5 " FWD OF FRM 70. ESFR COMPLETE RMVD CORROSION ON FLOOR SUPPORT Y160.5 FOUND OUT OF LIMITS RMVD DMG FLOOR SUPPORT Y160.5 RECEIVED NEW FLOOR SUPPORT RPLCD COMPONENTS TRANSFERRED DRILL HOLES + Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025031702850Angle · corrodedR2 DOOR LOWER AFT CORNER ANGLE FITTING CORRODED. ESFR COMPLETE RMVD + RPLCD CORNER FITTING AT RE PAX DOOR LWR AFT IAW A320 SRM 51-42-11 + SRM 51-72-11.Mar 13, 2025 · N462UA · Airbus A320232 · Service DoorsSDR CALA2025031402804Angle · crackedLH AFT TI-ANGLE IS CRACKED. RMVD TI-ANGLE IAW A320 SRM 51-42-11/001 REV.152 RPLCD TI-ANGLE O N LH AFT FRM 41-42 KEEL BEAM IAW A320 SRM 51-42-11/001 REV.152Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025031700258Tachometer · failedFLT#2834, RSW-ORH. (AIRCRAFT DIVERTED TO BOS) 'BRAKES AUTO BRK FAULT BRAKE RELEASED; REMOVED AND REPLACED #4 TACHOMETER IAW AMM 32-42-57-04. OPS CHECK GOOD.'Mar 12, 2025 · N506JB · Airbus A320232 · Landing Gear Brake SystemSDR CALA2025031302792Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK EPSU BATTERY 1L WAS UNSATISFACTORY EPSU BATTERY REPLACED AS PER AMM 33-51-38-000-002-A AND INSTALLATION OF THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) A SPER AMM TASK 33-51-38-400-002-A0 TEMar 12, 2025 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2025031302764Skin · damaged4634 FR35 STGR30RH PREVIOUS REPAIR MULTIPLE FASTENER HOLE DISCREPANCIES FOUND DURING RE-INSPECTION OUTLINED IN ECRA 5330-06963. REF LOG PAGE 8992357. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5330-07480 WITH NO DEVIATION. ACCOMPLISH A PERMANENT REPAIR ON THE FR35 SMar 11, 2025 · N434UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025031302763Crossbeam · crackedFRAME 16 RH CROSSBEAM HOLE #H3 HAS CRACK INDICATIONS IN BOTH LAY ERS AT 9 AND 5 OCLOCK 100% S.H. (AD 2024-04-04) PER NON ROUTINE 9296355/44355. ORIGINAL ACCOMPLISHED INTERIM REPAIR PART 1 TO FRAME 16 RH CROSSBEAM HOLE #H3 PER ECRA5311-03343 WITH NO DEVIATIONMar 11, 2025 · N434UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2025031400257Fairing · looseFLT#2110, SDQ-JFK. (AIRCRAFT DIVERTED TO SJU.) 'CLIMBING THROUGH 20000 AT PROFILE SPEED SMOOTH AIR AIRCRAFT STARTED VIBRATING ON A SCALE FROM 1-10 IT WAS 8. VIBRATION WAS FLUCTUATING AND INCREASED AS AIRSPEED INCREASE. THE VIBRATION SEVERITY INCREASED ABOVE 0.Mar 10, 2025 · N588JB · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2025031302788Cover · detachedFA REPORTS - AFT LIGHT P ANEL/EMERGENCY LIGHT SWI TCH CLEAR COVE R DETACHED INSTALLED AFT PANEL EMERGENCY LIGHT PB CLEAR COVER OK TO CONTINUE.Mar 10, 2025 · N482UA · Airbus A320232 · Emergency LightingSDR YENA2025031200254Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120245. CRACK INDICATION ON OPEN HOLE 6 FR20LH JOGGLE AREA. CRACK DEPTH 0.100 INCH, CRACK DIRECTION 3 OCLOCK, (RESOLVED ON W/O: 1353259 TASKCARD: NR-00013) FUR-A320-53-02078. REF AEROMAN WO# 2025 17/Mar 10, 2025 · N607JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025031200253Lug · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120296. CRACK ON LUG O/B ACTUATOR ON RH HORIZONTAL STABILIZER, (RESOLVED ON W/O: 1353259 TASKCARD: NR-00014) REF AEROMAN WO# 2025 17/1 NR# 2025-120296. PERFORMED PERMANENT REPAIR ON LOCKING LUG LOCATMar 10, 2025 · N607JB · Airbus A320232 · Fuselage, Stabilizer Attach FittingsSDR YENA2025031200252Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120246. CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION ON OPEN HOLE 8 FR20LH JOGGLE AREA. CRACK DEPTH 0.100 INCH, CRACK DIRECTION 9 OCLOCK ), (RESOLVED ON W/O: 1353259 TASKCARD: NR-00015) FUR-A32Mar 10, 2025 · N607JB · Airbus A320232 · Fuselage Main, FrameSDR AALA202503112595Bottle · low pressureAIRCRAFT WAS GROUNDED: CIDS CAUTION MESSAGE FOR OVERWING BOTTLE PRESSURE. MAINTENANCE SERVICED R1 DOOR ASSIST BOTTLE TO NORMAL PRESSURE ,CIDS CAUTIONRESET AND SYS.OK.FOR CONT.FLT.IAW AMM.52-10-00-614-001-A.Mar 10, 2025 · N654AW · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025031102700Battery · inoperativeOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L MSG REPLACEMENT OF THE AFT L EPSU BATTERY WAS PERFORMED IAW AMM 33-51-38/401. OK FOR SERVICE PARTS USED: 18-3351-3-0001,QTY :1Mar 10, 2025 · N473UA · Airbus A320232 · Emergency LightingSDR CALA2025031302766Crossbeam · crackedFRAME 16 RH CROSSBEAM HOLE #H4 HAS CRACK INDICATION IN BOTH LAYE RS AT 6 OCLOCK 100% S.H. (AD 2024-04-04) PER HAECO LCQ NON ROUTI NE 9296351/44351 ACCOMPLISHED INTERIM REPAIR PART 1 TO FRAME 16 RH CROSSBEAM HOLE #H4 PER ECRA5311-03343 WITH NO DEVIATIONS. ACCMar 9, 2025 · N434UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025031302765Crossbeam · crackedFRAME 16 RH CROSSBEAM HOLE #H2 HAS CRACK INDICATION IN BOTH LAYE RS AT 4 OCLOCK 100% S.H. (AD 2024-04-04) PER HAECO LCQ NON ROUTI NE 9296353/44353 GENERATED BY V892444 ACCOMPLISHED INTERIM REPAIR AT FRAME 16 RH CROSSBEAM HOLE #H2 PER PART 1 OF ECRA5311-03343 WMar 9, 2025 · N434UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025031102705Skin · crackedSECONDARY FINDING. L1 DOOR EXTERIOR SKIN UPPER AFT CORNER CRACKED. ESFR ENTRY GENERATED REMOVED AND REPLACED L1 DOOR UPPER EXTERNAL SKIN IAW A320 SRM 51 -72-11-911-001.Mar 9, 2025 · N434UA · Airbus A320232 · Passenger/Crew DoorsSDR GTIA2025031038792Megaphone · inoperativeDURING SERVICE CHECK FOUND FWD MEGAPHONE INOP -R/R FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.Mar 9, 2025 · N628NK · Airbus A320232 · Emergency Equipment
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