Airbus A320-232

Service difficulty reports · 32,652

Newest first. General aviation reporting is voluntary.

Query with SQL
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 CALA2025081307688Cap · missingPDA 2 PDA CREATED FOR FUEL CAP MISSING LP#5856941 REFERENCE LP# 5856941 FOR CLEARING OF LOGPGE.Aug 9, 2025 · N496UA · Airbus A320232 · Fuel StorageSDR YENA2025081200829Fitting · not reportedDURING HEAVY MAINTENANCE: REPLACE THE CONTINUITY FITTINGS IAW EA #53-0053-25 PART# 3 AND 4 ; REF AEROMAN WO# 2025-190/1 WCC# 2025-416752 FOR WORK PERFORMED. REMOVED AND REPLACED CONTINUITY FITTINGS I.A.W. EA# 53-0035-25,(COVER PLUS REV 0), PART #3 AND PART #Aug 9, 2025 · N608JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025081200828Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER LOWER POST ON UPPER TENSION BOLT AREA ON LH SIDE CRACK LENGTH = 0.250 INCH APPROX; AEROMAN WO#2025-190/1 WCC# 2025-416536 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR ON FUSELAGE WINDSHIELAug 9, 2025 · N608JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025081200827Window Frame · crackedDURING HEAVY MAINTENANCE: WINDSHIELD FRAME CENTER POST LOWER NODE AREA CRACKED. POST REPAIR INSPECTIONS OF THE MIRROR FITTINGS (TBD) AEROMAN EA 53-0371-22 REV. 0. AIRBUS RDAF 81098121/004/2022#A. AIRBUS DOSSIER 81098121. AIRBUS TD/81039011/009/2022#A. Aug 9, 2025 · N608JB · Airbus A320232 · Fuselage Main, StructureSDR CALA2025081107583Indicator · faultedSTDBY ATTITUDE INDICATOR HAS FAILED REPLACED STANDBY ATTITUDE INDICATOR, OPS CHECK GOOD MM 34-22-24.APARTS USED: 31-4170-9-0001,QTY :1 ROTABLE PARTS CHG:TT # 1449521 SN OFF 2440 PN OFF 31-4170-9-0001 INDICATOR, STAN OFF 31-4170-9-0001 2440 ON 31-4170-9-0001 Aug 9, 2025 · N469UA · Airbus A320232 · Attitude and Direction Data SystemSDR CALA2025081107573Battery Pack · inoperativeDURING TEST FOUND ERROR MSG "EPSU BATTERY EMER L" ATA 33-51-38 SEE PIC REMOVED AND REPLACED LEFT OVERWING EMERGECNY EXIT LIGHT POWER SUPPLY BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, BITE TEST PASSES WITH A GREEN SYS OK LIGHT AND NO FAULTS.Aug 9, 2025 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2025081107572Battery Pack · inoperativeWHILE PERFORMING BITE OF EPSU SYSTEM REF AMM 33-51-00-710-001-A RECIEVED AN EPSU BATTERY AFT L MESSAGE REMOVED AND REPLACED THE AFT LEFT EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, FAULT IS NO LONGER PRESENT AND THE BITE TEST PASSES.Aug 9, 2025 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2025081107537Light · no testDURING FUNCTION TEST, RECEIVED ERROR MSG "EPSU INT LOAD EMER L" ATA 33-51-38 C/W TEST OF THE EMERGENCY LIGHTS REF AMM: 33-51-00-710-096-A. TEST OK AND NO OTHER FAULTS NOTED AT THIS TIME.Aug 9, 2025 · N480UA · Airbus A320232 · Emergency LightingSDR AALA202509118736Support Angle · out of toleranceAIRCRAFT IN BASE MAINTENANCE: OUT OF ROUND HOLE AT FRAME 59 LH STRINGER 37. MAINTENANCE FABRICATED AND REPLACED ANGLE FROM 2024T3.01 PER DRW #53470322 AND EA #362953.Aug 8, 2025 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202509106621Fitting · wornAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE UPPER FITTING LOCATED AT LEVEL FR20 NOSE LANDING GEAR BAY INTERNAL STRUCTURE IN LATERAL AVIONIC COMP LH HOLE WIDTH =0.560 INCH. MAINTENANCE REPLACED UPPER FITTING AT LEVEL FR20 NOSE LANDING GEAR BAY INTERNAL STRUCAug 8, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510146811Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23R AT AFT GALLEY AREA, MEASURE OF CRACK IS L= 1.021 IN. MAINTENANCE REPLACED SHEAR SHEAR PLATE STR 23R BETWEEN FR69 AND FR70 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801, A320 SRM 51-72-11-911-001 AND DWG D5Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202509294444Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 42L BTW FR58 AND FR 59 IN AFT CARGO COMPARTMENT MEASURE CORROSION ARE L=6.823 INCH W=0.878 INCH D=0.025 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON STRINGER 42L BTW FR58 AND FR 59 IN AFT CARGO COMPARTMENT IAAug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202509290845Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT L=5.748 INCH W=0.878 INCH D=0.023 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON STRINGER LOC ON STRG 43L BTW FR57 AND FR59 IN AFT CARGO COMPARTMENT IAW A320 SAug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202509028347Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 FR 66 AT AFT GALLEY AREA, MEASURE OF CORROSION ARE: L= 1.613 INCH W= 1.060 INCH D= 0.040 INCH. MAINTENANCE REPLACED FLOOR BEAM Y1292 BETWEEN FR64 TO FR66 AFT GALLEY AREA LH SIDE IAW A320 SRM 51-72-11-91Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202509020656Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. CRACK L= 1.465 IN. MAINTENANCE REPLACED SHEAR PLATE LOC. ON STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202508269906Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING PASSENGER CREW DOOR BETWEEN FR16 AND FR20 AT LEVEL STR23R FWD GALLEY AREA MEASURE CORROSION ARE L=0.456 INCH W=0.388 INCH D=0.014 INCH.Aug 7, 2025 · N664AW · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025081107522Lavatory · odorAFT LAV D GIVING VERYROUGH SMELL. NO WASTE VISIBLE. STARTED SMELLING AFTER TAKEOFF, NOTIFY LAV SERVICE TO DUMP AND RESERVICE LAV SYS, NO WATER OR WASTE LEAKS NOTED, NO FOUL ODORS NOTED AT AFT LAV D.Aug 7, 2025 · N438UA · Airbus A320232 · LavatoriesSDR YENA2025080800820A/C Pack · odorFLT#2251, BOS-MCO. AFT FA'S REPORTING A STRONG DIRTY SOCK SMELL ON LANDING APU NOT RUNNING. IN COCKPIT A PAINT SMELL WAS NOTICED ON DESENT LANDING; COMPLIED WITH INFO NOTICE 2017-T015. IDENTIFIED ODOR AT PACK 1. INSPECTED APU & APU BLEED DUCT FOR OIL CONTAMINAAug 7, 2025 · N712JB · Airbus A320232 · Cabin Cooling SystemSDR AALA202508207140Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR AALA202508205069Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR AALA202508205551Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 FITTING ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR AALA202508203061Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR AALA202508202380Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR AALA202508206708Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. MSINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Aug 6, 2025 · N664AW · Airbus A320232 · Elevator StructureSDR YENA2025080800818Oil System · leakingFLT#257, BOS-BZN. APU OILY ODOR / DIRTY SOCKS AFTER GATE ARRIVAL MILD ODOR IN FLIGHT DECK STRONG ODOR IN AFT CABIN IN GALLEY; COMPLIED WITH INFO NOTICE 2017-T015L SECTION B ISOLATED FAULT TO TYEP 1 EVIDENCE OF OIL LEAK IN APU INLET AREA PER TSM 05-50-00-810-0Aug 6, 2025 · N828JB · Airbus A320232 · APU Oil SystemSDR YENA2025080700808Unknown · odorFLT#2924, STI-BOS. (AIRCRAFT PERFORMED AN AIR RETURN TO STI) DIRTY COCK ODOR EVENT SHORTLY AFTER TAKE OFF. STRONG IN BOTH CABIN AND COCKPIT. RAN ODOR ISOLATION PROCEDURE. DID NOT HELP, BOTH PACKS APPEAR TO BE CONTAMINATED. SUSPECT APU BLEED AS SOURCE. AIRCRAFAug 6, 2025 · N561JB · Airbus A320232 · Air Distribution SystemSDR CALA2025080707436Battery Pack · no testEPSU BATTERY AFT LT FAILED CAP CHECK. REMOVED AND REPLACED EPSU BATTERY PER AMM 33-51-38-000-002-A. OP CHECK OKAug 6, 2025 · N459UA · Airbus A320232 · Emergency LightingSDR YENA2025080600806A/C Pack · odorFLT#1146, FLL-RIC. "AFTER FL350 FAS CALLED TO REPORT STRONG SOCK SMELL IN ROWS 15 TO AFT A/C ROW CABIN ODOR RECOGNITION AND ISOLATION CHECK LIST . TURNED OFF PACK#2 AFTER 5 MINUTES, THE ODOR HAD DISSIPATED , CROSSBLEED VALVE SHUT AND PACK2 #2 REMAINED OFF FORAug 6, 2025 · N633JB · Airbus A320232 · Cabin Cooling SystemSDR AALA202510140621Structure · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN HOLE LOCATED ON FUSELAGE AT FR35 AND STGR 30 LH. (CRACK: 0.125 INCH). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON HOLE 2 LOC FR 35 AT LEVEL STGR 30LH IAW EA 367091.Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510146795Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 5 OPEN HOLE ZONE 1, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.094 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 5 (-Y765), CENTER BOX FRONT SPAR VERTICAL STR FR36 IAW EA 3673Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510148145Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 4 OPEN HOLE ZONE 1, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH IS: 0.157 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 4 (-Y254), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EAAug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510141712Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 3 OPEN HOLE ZONE 2, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.155 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 3 (Y254), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EA 3673Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510147088Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 2 OPEN HOLE ZONE 2, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.155 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 2 (+Y765), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EA 367Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025080807516Fuel Cap · missingDURING WALK AROUMD NOTICE CAP,COUPLING REFUELING UNDERWING MISSING .Aug 5, 2025 · N436UA · Airbus A320232 · Fuel StorageSDR YENA2025080700811Smoke Detector · failedFLT#1685, JFK-TPA. "LAV F SMOKE DETECTOR ALARM GOES OFF; ACCOMPLISHED TSM 26-17-00-810-807-A, FOUND LAV B (2WQ) TO BE AT FAULT. R&R LAV B SMOKE DETECTOR IAW AMM 26-17-15. OPS CHECK OK."Aug 5, 2025 · N561JB · Airbus A320232 · Smoke DetectionSDR YENA2025080700809Fan · failedFLT#1152, MCO-BOS. "DURING DESCENT FROM FL 370 TO APPROX FL 270, MODERATE ELECTRIC OR BURNING PLASTIC SMELL, ANTI ICE WAS ON BUT LATER USED AGAIN WITH NO SMELL SO I DO NOT SUSPECT A CONNECTION TO ANTI-ICE. ; UPON ARRIVAL ON A/C FOUND C/B X18 TO BE TRIPPED. REMAug 5, 2025 · N554JB · Airbus A320232 · Air Distribution FanSDR CALA2025080607387Battery · no testEMERGENCY EPSU BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED RT EMERGENCY EPSU BATTERY IAW AMM 33-51-38-000-002-A. OPS CHECKED GOODAug 5, 2025 · N433UA · Airbus A320232 · Emergency LightingSDR AALA202510082347Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510080186Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 843 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510080481Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510087242Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 844 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510089637Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510088979Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, StructureSDR CALA2025080707407Slide · not reportedR1 ESCAPE SLIDE ASSEMBLY REPLACED REF AMM 25-62-44. REPLACED R1 ESCAPE SLIDE ASSEMBLY REF AMM 25-62-44. ACP RII INSP REF GMM 09-25-05.Aug 4, 2025 · N480UA · Airbus A320232 · Escape SlideSDR CALA2025081207628Shear Tie · damagedFORWARD CARGO AT FR 32 SHEAR-TIE BETWEEN STR 39L-40L HAS ELONGAT ED FASTENER HOLES REQUIRES REPLACEMENT. REMOVED AND REPLACED SHEAR TIE AT FWD CARGO FR32 BTW STR 39L-40L IAW A320 SRM 51-42-11 AND 51-72-11.Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2025081207627Shear Tie · damagedHAS ELONGATED FASTENER HOLES REQUIRES REPLACEMENT. REMOVED AND REPLACED CLEAT AT FWD CARGO FR32 BTW STR 40L-41L IAW A320 SRM 51-42-11 51-72-11.Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2025081207626Shear Tie · damagedFORWARD CARGO COMPARTMENT AT FR 32 SHEAR TIE BETWEEN STR 41L-42L HAS ELONGATED FASTENER HOLES REQUIRES REPLACEMENT. GENERATED BY V077960 PER HAECO LCQ NR 9296915/30915. ESFR COMPLETED REMOVED AND REPLACED SHEAR TIE AT FWD CARGO FR 32 BTW STR 41L-ST R42L IAW A3Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2025080607376Indicator · detachedPIECE OF METAL DETACHED FROM DOOR 2L ESCAPE SLIDE BUSTLE COVER. REINSTALLED ARMING INDICATOR ON DOOR 2L. OP CHECK GOOD.Aug 3, 2025 · N436UA · Airbus A320232 · Escape SlideSDR CALA2025080507327Skin · corrodedFWD CARGO COMP CORRODED FASTENERS FWD OF FR 32 BETWEEN STR 40L A ND SRT 42L. ACCOMPLISED REPAIR INSTRUCTIONS PER HAECO REO L25555 WITH NO DEV IATIONS AT FWD CARGO COMP FR32 BETWEEN 39L-42L STRG IAW SRM 53-2 1-11-300-063 AND ECRA 5321-02165Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2025080439032Megaphone · no testDURING WALKAROUND, FOUND FWD F/A STATION MEGAPHONE NOT TESTING AND LEAKING WATER. R & R FWD F/A MEGAPHONE IAW SPIRIT NKS DRAWINGS A320 EMER EQUIP REV 7. PERFORMED OPS TEST IAW AMM 25-65-51-710-002-A. OPS TEST GOOD AT THIS TIME.Aug 3, 2025 · N631NK · Airbus A320232 · Emergency Equipment
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