Service difficulty reports

1,770,704 reports of malfunctions and defects, newest first. Air carriers must report; 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'
  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 YENA2026091000783Floorbeam · not reportedDURING HEAVY MAINTEANCE, (CPCP) "REF AEROMAN N/R 2026-432642, REMOVED AND REPLACED FLOOR BEAM (Y1292) LOC.BTW FR 12 TO FR 24 AT AFT GALLEY AREA I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11-911-001, DWG D53112813 AND DWG D53110876.Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000782Floorbeam · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ2 FRAME 36. CRACK L= 0.320 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346060 ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CSep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000781Floorbeam · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ3 FRAME 36. CRACK L= 0.405 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346061, ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000780Floorbeam · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ4 FRAME 36. CRACK L= 0.316 INCH.; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00078 ) REF AEROMAN WO 2026-280/1, NR 2026 - 346062: ACCSep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000779Floorbeam · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ5 FRAME 36. CRACK L= 0.450 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346063ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CESep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000778Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE MIDD LE LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0 .105 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00065 ) RESep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000777Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE AFT LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.12 0 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00066 ) REF ASep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000776Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE LOWE R OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION IS 3 OCLOCK, CRA CK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000775Stringer · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON STR 5 LH FR 74 PLUS 1 INCH .CRACK DIRECTION PARALEL TO RADIUS OF STRINGER.CRACK LENGTH 0.250INCH; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00069 ) REF AEROMAN W/O 2026 280/1 NR 346167. ACCOMPLISHED THE REPAIR OSep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026091000774Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE FWD MIDDLE COMMON TO SKIN,CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS0.085INCH,IN FWD CARGO COMPARTMENT (1EA) ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00070 ) REF AEROMSep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000773Door · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON OPEN HOLE LOC FR38RH STR19. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00071 ) REF AEROMAN WO 2026-280/1, NR 2026 - 346115, ACCOMPLISHED REPAIR OF LH/RH ESep 5, 2026 · N521JB · Airbus A320232 · Emergency ExitsSDR YENA2026091000772Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR39RH STR14 PLUS 4 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00072 ) REF AEROMAN WO 2026-280/1,Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000771Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR41LH STR14 PLUS 3 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH )PAX CABIN ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00073 ) REF AEROMAN WO 2026-280/1, Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000770Door Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR41LH STR14 PLUS 4. CRACK DIRECTION 3 OCLOCK AND DEPT H =0.100 INCH )PAX CABIN ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00074 ) REF AEROMAN WO 2026-280/1, NR Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091000769Door Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR39LH STR14 PLUS 3 INCH. CRACK DIRECTION 9 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00075 ) REF AEROMAN WO 2026-280/1,Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091000768Frame · crackedDURING HEAVY MAINTEANCE,DURING HEAVY MAINTEANCE,CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND ON OPENHOLE LOC FR39LH STR14 PLUS 4 INCH. CRACK DIRECTION 9 OCLOCK AND DEPTH =0.100 INCH )PAXCABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00076 ) REF AEROSep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000767Power Supply · no testDURING HEAVY MAINTEANCE,EPSU 10WL DOES NOT PASS EMERGENCY LIGHT TEST; REF AEROMAN NR 2026-346269 W/O:2026 280/1: REMOVED AND REPLACED EPSU 10WL IAW AMM 33-51-38-400-001-A AND AMM 33-51-38-000-001-A. PERFORMED OPERATIONAL TEST, TEST IS OK.Sep 5, 2026 · N521JB · Airbus A320232 · Emergency LightingSDR YENA2026091000766Floorbeam · crackedDURING HEAVY MAINTEANCE,FRONT SPAR STRINGERS & HORIZONTAL FLOORBEAMS FR36 CRACKED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091000765Stringer · crackedDURING HEAVY MAINTEANCE, REAR FUSELAGE, TAILCONE STGR 5LH AT LEVEL OF FR74, CRACK DAMAGE. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026091000764Attach Angle · crackedDURING HEAVY MAINTEANCE,FUSELAGE. CENTER FUSELAGE FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT AT LEVEL OF STGR 30LH, FASTENER HOLES, CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR A26-646-01)Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2026091000763Skin · crackedDURING HEAVY MAINTENANCE, (CPCP) ""REF AEROMAN 2026-252/1, NR 354594, ACCOMPLISH REPAIR OF CORROSION DAMAGES AFFECTING THE LH WING TOP SKIN PANEL 2, LOWER SURFACE ALONG THE FALSE REAR SPAR AND TRAILING EDGE OVERHANG BETWEEN WX3494.5 - WX4490.52 IN ACCORDANCE Sep 5, 2026 · N784JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091000754Support Angle · corrodedDURING HEAVY MAINTENANCE, CORROSION SUPPORT ANGLE LOC AT LEVEL FR 71 ACCESS DOOR CUTOUT 312AR IN TERNAL AREA THS COMPARTMENT; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00021 ) REFERENCE AEROMAN W.O. 2026 252/1 NR 2026 - 354832, REMOVED & REPLACED SUPPORT ANGLE Sep 5, 2026 · N784JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026091000753Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT +Y254 FR16 TO FR20 IN PASSENGER CABIN (CPCP FINDING); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00022 ) REF AEROMAN N/R 2026-355123, REMOVED AND REPLACED FLOOR SUPPORT Y254 AND FASTENERS LOC. FR12 TO FR24 IN PASSESep 5, 2026 · N784JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026091000752Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 20 LH SIDE IN OPEN FASTENER HOLE H26 AT CROSSBEAM SPLICING AREA, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.0 85 INCH, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00025 ) REF: ARM WSep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091000751Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION RAIL DUMMY Y503.2 LOCATED FR12 TO FR16 FWD GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00026 ) REF: W/O 2026-252/1 N/R 2026-355101 REMOVED AND REPLACED RAIL DUMMY Y503.2 AND FASTENERS LOC ON FR 12 TO FSep 5, 2026 · N784JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2026091000750Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT Y940 AND FR14 TO FR16 AT FWD GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00027 ) REF: ARM W/O 2026-252/1 N/R 2026-355125 REMOVED AND REPLACED FLOOR SUPPORT Y 940 AND FASTENERS LOC ON FR Sep 5, 2026 · N784JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026091000749Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOORBEAM +Y765 AND FR14 TO FR20 FWD GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00028 ) REF: ARM W/O 2026-252/1 N/R 2026-355124 REMOVED AND REPLACED FLOOR BEAM Y 765 AND FASTENERS LOC ON FR 12 TO FR Sep 5, 2026 · N784JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026091000748Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 38L LOC BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00031 ) REF: ARM W/O 2026-252/1 N/R 2026-354761 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT STGR 38LH BETWEENSep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026091000747Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 37L LOC. BTW FR 58 TO FR59 IN AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00033 ) ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT STGR 37 LH BETWEEN FR56 TO FR59 IN ACCORDANCE WITH AEROMAN AE 53-0072Sep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026091000746Skin · not reportedDURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE - SRM REPAIR SURVEY, DEFECTS 153 6503, 7265500087; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00037 ) PERFORMED PERMANENT REPAIR LOCATED ON LOWER FUSELAGE AT FR68 PLUS 14 INCH AND BTW STR42L TO STR43L, THIS REPAIRSep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026091000745Access Panel · damagedDURING HEAVY MAINTENANCE, SECONDARY FINDING ELONGATED HOLE CUT OUT FUEL TANK ACCESS PANEL 640KB ON RT WING ; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00042 ) REF AEROMAN PERFORMED PERMANENT REPAIR ON (HOLE #1) LOCATED ON BOTTOM SKIN PANEL #2 BTW RIB 15 TO RIB 1Sep 5, 2026 · N784JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091000744Skin · corrodedDURING HEAVY MAINTENANCE, SECONDARY FINDING ELONGATED HOLE CUT OUT FUEL TANK ACCESS PANEL 640KB ON RT WING (HOLE 2) FOR TRACKING PURPOSE ONLY; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00044 ) REF AEROMAN WO 2026-252/1 NR 2026-355336 PERFORMED PERMANENT REPAIR OSep 5, 2026 · N784JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091000743Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE AREA LOCATED OVERHANG BTW RIB 8 TO RIB 9 ON LT WING; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00048 ) REF AEROMAN 2026-252/1, NR 354594, ACCOMPLISH REPAIR OF CORROSION DAMAGES AFFECTING THE LT WING TOP SKIN PANESep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026091000742Skin · corrodedDURING HEAVY MAINTENANCE, REF AEROMAN WO 2026-252/1, CORROSION TRAILING EDGE AREA LOCATED OVERHANG AT LEVEL RIB 7 ON LT WING; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00049 ) ACCOMPLISH REPAIR OF CORROSION DAMAGES AFFECTING THE LT WING TOP SKIN PANEL 2, LOWER SSep 5, 2026 · N784JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091000741Skin · corrodedDURING HEAVY MAINTENANCE, AFT FUSELAGE, FR56-61 & STGR 37L-38L CORRODED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR A26-610-01)Sep 5, 2026 · N784JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026091000740Skin · corrodedDURING HEAVY MAINTENANCE, LT WING TOP SKIN PANEL 2, LOWER SURFACE, FALSE REAR SPAR, BTWN WX3494.5-WX4490.52, CORROSION – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR A26-766-01)Sep 5, 2026 · N784JB · Airbus A320232 · Wing, Plate/SkinSDR SWAA2026091063368Assist Handle · looseL1 DOOR ENTRY DOOR AFT ASSIST HANDLE IS LOOSE. INSTALLED CORRECTLY L1 DOOR ENTRY DOOR AFT ASSIST HANDLE IAW AMM 52-11-31-400-802 STEP 3.G(2).Sep 5, 2026 · N8652B · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026091089337Slide · out of adjustL1 DOOR SLIDE IS COMING OUT OF THE COVER. INSTALLED CORRECTLY L1 DOOR SLIDE PACK ON COVER IAW MT 725-61-06 COMPLETED TASK.Sep 5, 2026 · N8652B · Boeing 7378H4 · Escape SlideSDR ASAA2026090566778Smoke Detector · false activationCARGO SMOKE AFT . REQUEST VIA RESET. GROUNDED - YES. PERFORMED FIM 26-22 TASK 805. PERFORMED VIA RESET IN REF TO AMM 31-43-00. NO FAULTS NOTED. OK FOR SVC.Sep 5, 2026 · N477HA · Boeing 717200 · Smoke DetectionSDR SWAA2026090914475Lens · unsecureAFT SERVICE DOOR R2 EMERGENCY EXIT SIGN COVER WILL NOT STAY ON SECURED. AFT RT SERVICE OVER DOOR EXIT LIGHT LENS WITH CLEAR MYLAR TAPE PER MT-21-133-00720STEP 9. OPS CHECK GOOD IAW AMM 33-51-00. OK TO CONTINUE PER TDL.Sep 5, 2026 · N940WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026090956952Bulb · inoperativeCEILING LIGHTS OUT ABOVE ROWS 2 3 4 5 D SIDE. 2 BULBS BURNED OUT.Sep 5, 2026 · N7724A · Boeing 7377BD · Emergency LightingSDR SWAA2026090941486Battery · inoperativeF/O SIDE AFT F/A OTBD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW S.I.P.Sep 5, 2026 · N8765Q · Boeing 7378 · Emergency EquipmentSDR SWAA2026090902957Light · faultedSIDEWALL LIGHT AFT EMERGENCY EXIT ROW 15 DEF FLICKERING. R & R SIDEWALL LIGHT AT ROW 15 DEF IAW AMM 33-21-00. OPS CHKD GOOD.Sep 5, 2026 · N8728Q · Boeing 7378 · Emergency LightingSDR JIKA2026090901Hydraulic Line · brokenDURING DEPARTURE FROM KBUR, THE FLIGHT CREW REPORTED THAT THE NR 1 & 2 HYDRAULIC LOW-PRESSURE ANNUNCIATORS ILLUMINATED AS WELL AS A LOW-PRESSURE INDICATION ON THE PRESSURE GAUGE. A MANUAL LANDING GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT RETURNED TO KBUR SSep 5, 2026 · N801AF · Swrngn SA227AC · Hydraulic System, MainSDR UIEA2026090500853Shutoff Valve · faultedBLEED 3 EICAS DURING CLIMB. REMOVED AND REPLACED ENG 3 PRV, OPS CHECK NORMAL AND ENG RUN OK IAW AMM 36-11-19, AMM 71-00-00 AND IPC 36-11-05-02A.Sep 5, 2026 · N451PA · Boeing 74746NF · Pneumatic Distribution SystemSDR CVGA20260909001Flap System · failedFLAP FAILURE WITH THE FOLLOWING CAS MSGS. SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND SPOILER FAULT ADVISORY. THE FLAP INDICATOR HAD YELLOW XS AND PITCH TRIM HAD YELLOW XS. ( EMERGENCY DECLARED ) PERFORMED FLAPS FAIL ABNORMAL PROCEDURE CHECKLIST IAW AMF-2066 4-1Sep 5, 2026 · N653UP · Emb EMB505 · Trailing Edge Flap Control SystemSDR R61A2026090500256Power Supply · no testFWD LEFT EMERGENCY LIGHTS WENT OUT DURING EMERGENCY LIGHT FUNCTION TEST. R & R ELPU 1.Sep 5, 2026 · N106HQ · Emb ERJ170200LR · Emergency LightingSDR CALA2026090719288Battery · inoperativeDURING ACCOMPLISHMENT TO CONFORMITY CHECK, FOUND AFT FLIGHT ATTENDANT SEAT, FOUND FLASHLIGHT BATTERY DISCHARGED. THE FLASHLIGHT BATTERY WAS REPLACED IAW DWG 2560DD15305.Sep 5, 2026 · N673UA · Boeing 767322 · Emergency EquipmentSDR CALA2026090719286Battery Pack · no testR1 DOOR EMERGENCY POWER ASSIST SYSTEM (EPAS) BATTERY OPS TEST DID NOT WORK.Sep 5, 2026 · N799UA · Boeing 777222 · Passenger/Crew DoorsSDR CALA2026090719283Doubler · crackedFOUNDED LOWER STRUCTURE DOUBLER WHERE EXTERNAL POWER RECEPTACLE DOOR CLOSES, CRACKED. PERFORMED PERMANENT REPAIR ON LOWER EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE DOUBLER IAW SRM 53-10-15-2R-4, 51-40-02-0G-0, AMM 20-60-07-913-801, NDTM PART 6, 51-00-00 PSep 5, 2026 · N14704 · Boeing 737724 · Fuselage Main, Plate/Skin