Airbus A320-232

Service difficulty reports · 32,652

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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 CALA2025051404664Bottle · no discrepancyDOOR 2L SLIDE PRESSURE LOW IN THE RED. LET TEMPERATURE BECOME STABLE REF AMM 25-62-00, OK FOR SERVICEMay 11, 2025 · N489UA · Airbus A320232 · Escape SlideSDR YENA2025051300489Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – PERMANENT REPAIR (PENDING DTA); REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS DMay 11, 2025 · N633JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025051300488Skin · gougedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – TEMPORARY REPAIR; REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS DOSSIER 8158766May 11, 2025 · N633JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025051300487Support · damagedDURING HEAVY MAINTENANCE: EXISTING REPAIR ON LOWER SILL LOCATED AT FR 68 AND AT LEVEL STR 23R AF T GALLEY AREA (FOR AGING AIRCRAFT PROGRAM FCBS); (RESOLVED ON W/O: 1353728 TASKCARD: NR-00019) REMOVED EXISTING REPAIR ON LOWER SILL LOCATED AT FR 68 AND AT LEVEL May 11, 2025 · N775JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025051300485Door Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON BOTH FRAME SEGMENTS 1 OF THE FWD LH SIDE OVERWING EMERGENCY EXIT HATCH DOOR 833. MAXIMUM CRACK LENGTH: 0.600 INCHES; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00029) OVERWING EMERGENCY EXIT HATCH (FWD LMay 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025051300486Door Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON BOTH FRAME SEGMENTS 1 OF THE AFT LH SIDE OVERWING EMERGENCY EXIT HATCH DOOR 834. MAXIMUM CRACK LENGTH: 0.300 INCHES; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00030) ACCOMPLISHED DOORS / EMERGENCY EXIMay 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025051300484Door Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON BOTH FRAME SEGMENTS 1 OF THE FWD RH SIDE OVERWING EMERGENCY EXIT HATCHDOOR 843. MAXIMUM CRACK LENGTH: 0. 300 INCHES; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00035) EMERGENCY EXIT / OVERWING EMERGENCY May 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025051300483Door Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON BOTH FRAME SEGMENTS 1 OF THE AFT RH SIDE OVERWING EMERGENCY EXIT HATCH DOOR 844. MAXIMUM CRACK LENGTH: 0. 400 INCHES; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00036) / EMERGENCY EXIT / OVERWING EMERGMay 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025051300482Coupling · corrodedDURING HEAVY MAINTENANCE: CORROSION ON COUPLING LOC BTW FR 64 TO FR 65 AND STR 43L AFT CARGO COM PARTMENT; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00039) MOVED AND REPLACED COUPLING LOC BTW FR 64 TO FR 65 AND STR 43L AFT CARGO COMPARTMENT I.A.W. A320 SRM 51-42-May 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025051300481Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 44 AT LEVEL FR 65 IN AFT CARGO COMPARTMENT (CPCP F INDING); (RESOLVED ON W/O: 1353728 TASKCARD: NR-00043) PERFORMED PERMANENT REPAIR ON STRINGER 44 AT LEVEL FR 65 IN AFT CARGO COMPARTMENT I.A.W A320 SRM 53-41-13-300May 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025051300480Frame · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE FR 64 AND BTW STR 42L TO STR 43R IN AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1353728 TASKCARD: NR-00046) REF AEROMAN NR 2025-245373 WO 2025 178/1 PERFORMED REPAIR INTERNAL STRUCTURE FR 64 AND BTW STR 42L TMay 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025051300479Access Panel · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE FUEL TANK ACCESS CUT OUT BOTTOM SKIN BTW RIB 18 AND RIB 19 ON LH WING; WORK ACCOMPLISHED ON AEROMAN W/O:2025 178/1 2025 - 245360 TECH: N. CARCAMO INSP: J. MORALES. PERFORMED REPAIR ON FUEL TANK ACCESS CUT OUT BOTTOM SKIMay 11, 2025 · N775JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2025051300478Frame · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE FR 64 AND BTW STR 42L TO STR 43R IN AFT CARGO COMPARTMENT; REF AEROMAN NR 2025-245373 WO 2025 178/1 PERFORMED REPAIR INTERNAL STRUCTURE FR 64 AND BTW STR 42L TO STR 43R IN AFT CARGO COMPARTMENT I.A.W EA# 5May 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025051300477Buttstrap · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / BUTTSTRAP / @ LEVEL OF FR64 BTWN STR 42L-43R / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0024-25 REV. 0 (COVER + PART 1) /2/ AIRBUS RDAF 81575884/003/2025 ISSUE A /3/ AIRBUS DOSSIER 8157588May 11, 2025 · N775JB · Airbus A320232 · Fuselage Main, StructureSDR CALA2025051604724Shear Plate · corrodedMAIN CABIN AFT WET AREA FR69-70 LH SHEAR PLATE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED LH FR 69-70 SHEAR PLATE IAW A320 SRM 51-42- 11/001.May 10, 2025 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2025051238914Proximity Sensor · inoperativeF/CTL ANTI ICE STBY PITOT, LG SHOCK ABSORBER FAULT, AUTO FLT AP OFF, AUTO FLT A/THR OFF-ACCOMPLISHED INSPECTION OF NLG PROX SENSOR 25GA , NO DEFECTS NOTED.AND BITE OF LGCIU IAW AMM 32-31-73-200-002-A AND 32-69-00. . R/R NLG PROX SENSOR IAW 32-31-73. FAULT CMay 10, 2025 · N625NK · Airbus A320232 · Landing Gear Position and WarningSDR GTIA2025051238913Unknown · odorFUME EVENT PLANE SMELLS BAD CLIMB AND DESCENT. DESCRIPTION OF ODOR/FUMES: PERSISTENT, DIRTY SOCKS SMELL. APPARENT CABIN SOURCE: UNKNOWN. FLIGHT DECK AND FWD CABIN. NO VISIBLE SMOKE/HAZE. NO MEDICAL ATTENTION REQUIRED.-AS PER TSM 05-50-00-810-831-A PERFOMED DECMay 10, 2025 · N608NK · Airbus A320232 · Air Distribution SystemSDR GTIA2025051238910Blower · inoperativeBOTH PILOTS COULD DETECT AN ELECTRICAL SMELL INTERMITTENTLY IN THE COCKPIT. HEARD LOUD HUMMING AND SHORT SOUND OF FAN STRIKING SHROUD-FOUND RUMBLING NOISE IN THE COCPIT.PERFORMED TSM 21-26-00-810-837-A.R/R FAN BLEWER 20HQ OPS CHECK GOOD NO DEFECT NOTED A.A/C May 10, 2025 · N652NK · Airbus A320232 · Air Distribution FanSDR CALA2025051504700Frame · crackedCRACKS OF 1.062" AND 0.218" OF LENGTH AT RH SIDE AFT PASSENGER/C REW DOOR CUTOUT UPPER CORNER RADIUS ABOVE STR 8 AND FR 68 WEB JO INT TO DOOR FRAME. GEN BY V947494 ON HAECO LCQ NR 9292561 / 3456 1 ACCOMPLISHED INTERIM RPR AT RH FR68 STRG 8R FR WEB STIFFNER ANDMay 9, 2025 · N462UA · Airbus A320232 · Fuselage Main, FrameSDR YENA2025051300476Lap Joint · dentedDURING HEAVY MAINTENANCE: FUSELAGGE/REAR FUSELAGE/EXTERNAL SKIN NEAR LAP JOINT @ FR65-66 AND STGR 32L-33L DENT WITH GOUGE; PERFORMED JB TASKCARD A25-455-01 WITH NO DEVIATIONS. REF: CAS W/O 703-1410376 N/R 2.May 9, 2025 · N703JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025050900468Unknown · odorFLT#436, STI-JFK. 'AT 10,000FEET ON DECENT AA STRONG DIRTY SOCKS SMELL WAS REPORTED BT THE FLIGHT ATTENDANTS IN THE FORWARD AND MID CABIN. THE ODOR WAS ALSO OBSERVED IN THE FLIGHT DECK. THE ODOR WAS FAINT IN THE FLIGHT DECK, APU WAS NOT ON; PERFORMED DETAILED May 9, 2025 · N665JB · Airbus A320232 · Air Distribution SystemSDR CALA2025050904584Service Door · damagedAFT LAV SERVICE DOOR HAS OVER SIZED HOLE ON LATCH ATTACH HOLES. REMOVED AND REPLACED AFT LAV SERVICE DOOR IAW A320 AMM 52-42-11- 400-001.May 8, 2025 · N462UA · Airbus A320232 · Fluid Service DoorsSDR GTIA2025050938909Skin · damagedGOUGE DAMAGE FOUND ON CROWN SKIN AT FRAME 52 STRINGERS 2R-3R. RAF-01 3292829-01.-ACCOMPLISHED REPAIR OF GOUGE ON WO 346167 RAF 01-3292829-01May 7, 2025 · N693NK · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2025050538904Bottle · low pressureAFT LEFT DOOR ASSIST BOTTLE LOW PRESSURE-SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A NO LEAKS NOTED MOC 111830May 7, 2025 · N690NK · Airbus A320232 · Passenger/Crew DoorsSDR YENA2025050700466Battery · no testFLT#591, BOS-TPA. 'EPSU 10WL BATTERY FAILS OPERATIONAL TEST; REMOVED AND REPLACED EPSU 10WL BATTERY IAW AMM 33-51-38 OPS CHECKS GOOD.'May 7, 2025 · N621JB · Airbus A320232 · Emergency LightingSDR CALA2025052704981Window Frame · crackedFLIGHTDECK WINDSHIELD CTR POST LOWER NODE, LH SIDE I/B MOST HOLE HAS CRACK INDICATION @ 6 OCLOCK AFT DIRECTION, 90% SH APPROX .0 80 LONG LOWER SURFACE ONLY. INTERIM REPAIR HAS BEEN ACCOMPLISHED PER PART 1 OF ECRA 5311-03362 WITHOUT DEVIATIONS. ORIGINAL DISCREMay 6, 2025 · N464UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025050804560Cover · unsecureTEST FLIGHT DISCREPANCY. R1 DOOR RATTLING NOISE DURING FLIGHT. RESECURE R-1 DOOR SLIDE COVER AND VERIFIED DOOR COVER INSULATION AND VISUAL INDICATOR AND ARMED INDICATOR IAW A320 MM 25-62-44-4 00-802-A STEPS 10,11, AND 12.May 6, 2025 · N460UA · Airbus A320232 · Escape SlideSDR CALA2025050704534Fmc · faultedAP1 WAS NOT RELIABLE IN REGARDS TO SPEED OR ALTITUDE. ATTEMPTED TWICE. PERFORMED POST FLIGHT REPORT, NO FAULTS LOGGED. PERFORMED AFS TEST, FMGC 1 FAILED TEST. RESET FMGC1 SYS & PERFORMED AFS TEST A SECOND TIME, ALL TEST PASSED. PERFORMED LAND TEST, TEST FAILEDMay 5, 2025 · N495UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR CALA2025050704519Bottle · no discrepancySLIDE 2L SERVICE PRESSURE IN RED ZONE EVALUATE GAUGE AND CONTACT TOMC WITH FINDINGS NEEDLE IS ON THE SPLIT BETWEEN GREEN AND RED, REF AMM25-62-00-810-803-A -GAUGE MODEL A IS INSTALLED AND PRESSURE IS WITHIN LIMITS (ACCEPTABLE UP TO A NEEDLE WIDTH INTO THE RMay 5, 2025 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025050604489Cover · detachedECAM LEFT AFT OVER WING EXIT OPEN NOTED MESSAGE ON DOOR PAGE ECAM DISPLAY. FOUND COVER FOR OVER WING EXIT LYING ON FLOOR IN FRONT OF DOOR. UNABLE TO DETERMINE WHY THIS PANEL FELL OFF OR WAS REMOVED. REPLACED PANEL AND DETERMINED THAT IT IS SECURELY INSTALLED. May 5, 2025 · N461UA · Airbus A320232 · Emergency ExitsSDR CALA2025050804561Computer · faultedVENT SKIN VALVE FAULT. PERFORMED TEST OF AEVC, NO FAULTS FOUND. PERFORMED OP CHECK OF AIR INLET CHECK VALVE PER AMM 21-26-56-280-002-A, OP CHECK OKAY. DUE TO PRIOR WRITE UP FOR AEVC SYSTEM FAULT REPLACED AEVC. DURING SYSTEM TEST, RECEIVED SKIN AIR OUTLET VALVMay 4, 2025 · N456UA · Airbus A320232 · Cabin Pressure Control SystemSDR GTIA2025050538900Flashlight · inoperativeFLIGHT DECK F/O FLASHLIGHT INOP-R/R FO FLASHLIGHT PER A320 DETAILED DRAWING OK FOR SVC.May 4, 2025 · N624NK · Airbus A320232 · Emergency EquipmentSDR CALA2025050504457Stringer · damagedSTRINGER 25L FR 21-24 HAS A PREVIOUS MISDRILLED HOLE. ACCOMPLISH REPAIR INSTRUCTIONS PER HAECO REO L25446 REV IR WITH NO DEVIATIONS/ECRA 5311-03356.May 4, 2025 · N460UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202505067182Display · deterioratedAIRCRAFT WAS NOT GROUNDED: WX RADAR NOT ADEQUATELY PAINTING WEATHER TO AVOID CELLS.. AIRCRAFT DIVERTED TO PNS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FO NAV DATA DISPLAY UNIT IAW AMM 31-63-22,.May 3, 2025 · N660AW · Airbus A320232 · Weather Radar SystemSDR YENA2025050500464Hose · leakingFLT#592, TPA-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO TPA). 'HYD G RSVR LO LVL COMPLETE LOSS OF HYD G SYSTEM IN FLIGHT. EMERGENCY GEAR EXTENSION POR GRH; REF L/P 4168061-2 (FOUND RH OUTBOARD LOCKSTAY ACTUATOR HOSE BROKEN REMOVED AND REPLACED LOCKSTAY ACTUMay 3, 2025 · N634JB · Airbus A320232 · Hydraulic System, MainSDR CALA2025050504461Window Frame · crackedRH COCKPIT, SLIDING WINDOW , FWD LATCH AREA , MILLED RISER, UNDE R LATCH CRACKED. ACCOMPLISHED REPAIR PER HAECO REO-L25450 REV 1R WITH NO DEVIATIONS. INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03359 TO RH FR4 VERTICAL STIFFENER.May 3, 2025 · N460UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025050504452Cover · corrodedFWD PIT TORSION BOX COVER REQUIRES REPLACEMENT. REPLACED FWD PIT TORSION BOX COVER. REMOVED AND REPLACED FWD IT TORSION BOX COVER IAW A320 SRM 51-42 -11.May 3, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025050504450Scuff Plate · gougedAFT CARGO DOOR CUTOUT THRESHOLD UNDER SCUFF PLATE HAS GOUGES/T OOLING MARKS 2 EA LOCATIONS. REMOVED AND REPLACED TORSION BOX COVER ON AFT CARGO DOOR CUTOUT IAW A320 SR, 51-72-11-911-001.May 2, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025050504449Stringer · corrodedAFT CARGO LH STRINGER 43 AT FR 56 HAS CORROSION. REMOVED AFT CARGO LH STRINGER 43 CORROSION IAW A320 SRM 51-74-00 . PERFORMED NDT INSPECTION IAW NTM51-10-4 AND 51-50-00 STRINGER FOUND OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 1, ORIGINA L THICKNESS 0.108" RMay 2, 2025 · N464UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2025050504440Chiller · faultedGALLEY FOUR CHILLER GETTING HOT SMELL SMOKE WHEN TURNED ON REQUEST NEF 2522AG FOR GALLEY FOUR CHILLER INOP.OKAY TO DEFER CHILLER PER MEL 2522AG PLACED GALLEY FOUR CHILLER ON NEF 2522AG FOR INOP FOUND CHILLER G41 SN 568 EXHAUST OUTLET COVERPLATE INSTALLED IN THMay 2, 2025 · N459UA · Airbus A320232 · Buffet/GalleysSDR CALA2025052704980Door · crackedCRACK OF 0.625" APPROX AT LH AFT PASSENGER/CREW DOOR CUTOUT UPPE R RADIUS AT STR 8 AFT FACE INTERIM REPAIR HAS BEEN ACCOMPLISHED PER PART 1 OF ECRA 5341-01489 WITHOUT DEVIATIONS. ORIGINAL DISCREPANCY FOUND ON LCQ 9290288. INSPECTIONS AT INTERVALS NOT TO EXMay 1, 2025 · N464UA · Airbus A320232 · Passenger/Crew DoorsSDR YENA2025050500465Valve · faultedFLT#1091, BOS-TPA. 'HIGH SPEED REJECTED TAKEOFF AT APPROXIMATELY 95-115 KNOTS. AIRCRAFT LOST DIRECTIONAL CONTROL AND PULLED LEFT DEVIATED 20 FEET LEFT WHEN DECISION TO REJECT WAS MADE. FOLLOWED REJECTED TAKEOFF PROCEDURE AND CAME TO FULL STOP. AFTER EXITING RUMay 1, 2025 · N809JB · Airbus A320232 · Landing Gear Steering SystemSDR YENA2025050500463Cooling Fan · leakingFLT#525, PVD-SJU. 'NOTICE OILY/FUEL SMELL AT FL200 ON DECENT WITH PWR AT IDLE SMELL CONTINUE UNTIL 10,000 WHEN APU WAS STARTED AND APU BLEED USED. DIDN'T SEEM ASSOCIATED WITH APU; COMPLIED WITH INFORMATION NOTICE 2017-T015K SECTION B2, IDENTIFIED TYPE 1 LEVEL May 1, 2025 · N524JB · Airbus A320232 · APU Oil SystemSDR CALA2025050504463Fuel Cap · missingFUEL CAP MISSING. REQUEST CDL, NEEDS CAP ASSY 31-2825-9-0001. UNABLE TO FIND CAP AT DFW. INSTALLED REFUEL / DEFUEL COUPLING CAP AND CHAIN ASSEMBLY PER AMM 28-25-41.May 1, 2025 · N494UA · Airbus A320232 · Fuel StorageSDR CALA2025050204416Skin · crackedL/H HOLE #2 AT FR 35 HAS BEEN PREVIOUSLY WORKED. ACCOMPLISHED REPAIR PER HAECO RCO-L25396 WITH NO DEVIATIONS. ACCOMPLISHED A PERMANENT REPAIR AT LH FR35 STA R30LH HOLE #2 PER PART 3 OF THE LATEST REVISION OF ECRA 5320-07500 ON OR BEFORE 22OCT2025. INTERIM REMay 1, 2025 · N460UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025050204414Rib · corrodedLH WING T/E LOWER SURFACE PANEL LANDS AT RIB 23-27 HAVE EVIDENCE OF CORROSION. ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO-L25457 REV IR WIT H NO DEVIATIONS IAW A320 ECRA 5751-01560.May 1, 2025 · N460UA · Airbus A320232 · Wing, Rib/BulkheadSDR CALA2025050204412Frame · crackedFRAME 68 RH AT STR 8 HAS CRACK INDICATION ON AFT FACE AT RADIUS OF FLANGE JUST ABOVE UPPERMOST FASTENER IN WEB, APPROX .50 INCH LONG. PREFORMED FRAME FITTING REPAIR AT FR68 RH STR8R IAW A320SRN53-41-12. W/P/B PERFORMED FRAME FITTING REPAIR AT FR68 RH STR8R May 1, 2025 · N460UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2025050504434Proximity Sensor · out of adjust[LEVEL 0 CHRONIC]-FWD CARGO DOOR IND-DUE TO HISTORY, PLEASE CHECK THE 28WV AND 30WV PROX SW INDUCTANCE READINGS PER AMM 32-31-73- 820-008-A AND ADJUST PER AMM 52-71-00-820-003-A AND 52-71-00-820 -004-A AS NEEDED TO GET THE TARGET NEAR INDUCTANCE TO 5.8 MH. PApr 30, 2025 · N482UA · Airbus A320232 · Door Warning SystemSDR GTIA2025050138893Diaphragm · damagedR2 DOOR ASSIST BOTTLE REQUIRES DIAPHRAGM R&R DUE TO SLIDE DEPLOYMENT-R&R R2 DOOR ASSIST BOTTLE DIAPHRAGM IAW AMM 52-10-00-610-001-AApr 30, 2025 · N5210 · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025050104386Door Sill · corrodedAFT CARGO ENTRY DOOR SILL HAS CORROSION. MARKED. BLENDED OUT AND SMOOTHED 03 EACH CORRODED AREA, AT AFT CARGO ENTRY DOOR SILL SKIN, WERE FOUND WITHIN LIMIT LIMITS IAW A320 SRM 53-41-49. REMOVED AND PLACED INTERNAL INTERCOSTAL AT FR 53 AND BTW STR 39R/ 41 R IAApr 30, 2025 · N464UA · Airbus A320232 · Fuselage Main, Structure
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