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 FDEA202609281443Fitting · damagedCOMPLY WITH EO 6-5230-E0378588 C P5. DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOSep 28, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202609281442Solenoid Valve · malfunctionedDURING TAKEOFF, PF NOTICED AN UNUSUAL AMOUNT OF FORCE TO ROTATE ACFT. DURING CLIMB, HAND FLYING, APPROX 3X AMOUNT OF USUAL FORCE REQUIRED TO MOVE ACFT IN PITCH AXIS. WHEN AP1 IN USE, AP FUNCTIONED NORMAL. ATTEMPT MADE TO SWITCH TO AP2, AP2 WAS NOT AVAIL. Sep 28, 2026 · N591FE · Doug MD11F · Autopilot SystemSDR FDEA202609281441Floor Panel · puncturedPUNCTURE (2EA) ON FLOOR PANEL 242 TFA AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242 TFA AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR 4-B FIG. 201 SHEET 2 REV 96 AUG 15/2026Sep 28, 2026 · N255FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202609281440Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231 PFF AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 PFF AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG.201 SHEET 2 REV 96 AUG 15/2026Sep 28, 2026 · N255FE · Boeing 7673S2F · Fuselage Floor PanelSDR EE4Y2026280925043Window Frame · no discrepancyDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK CARD #A32X-53-212-022, THE RHS LATERAL WINDOW FRAME WAS PREVENTIVELY REWORKED. THIS REWORK WAS PERFORMED IN ACCORDANCE WITH ALLEGIANT EO 5311-0006 R02, AD2023-09-11 PARAGRAPH (G), AND SBA320-53-1337 R02. THIS CONSep 28, 2026 · N258NV · Airbus A320214 · Standard Practices/StructuresSDR EE4Y2026280925042Window Frame · not reportedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK CARD #A32X-53-211-022, THE LHS LATERAL WINDOW FRAME WAS PREVENTIVELY REWORKED. THIS REWORK WAS PERFORMED IN ACCORDANCE WITH ALLEGIANT EO 5311-0005 R02, AD2023-09-11 PARAGRAPH (G), AND SBA320-53-1338 R02. THIS CONSep 28, 2026 · N258NV · Airbus A320214 · Fuselage Main, StructureSDR SCNA20260928414Oxygen Mask · damagedFOUND AFT SUPERNUMERARY SEAT PORTABLE O2 BOTTLE FACE MASK DAMAGED ( SUPERNUMERARY SEATS ) FOUND PORTABLE O2 MASK CRACKED THIS CLEARS MEL 25-31 MDDR # 141727 APPLIED MEL 35-4-2 WITH THE SAME DATE OF DISCOVERY.Sep 28, 2026 · N5479A · Boeing 73783N · Portable Oxygen SystemSDR CALA2026092819853Light · inoperativeROW 12ABC RED EMERGENCY ISLE LIGHT INOPERATIVE. REMOVED AND REPLACED RED SEAT MOUNTED EMERGENCY LIGHT AT ROW 12ABC REF AMM 33-51-18. OPS CHECK GOOD. GOOD FOR SERVICE.Sep 28, 2026 · N437UA · Airbus A320232 · Emergency LightingSDR CALA2026092819846Engine · bird ingestionBIRD STRIKE. INJESTED IN NR 2 ENGINE. PERFORMED VISUAL INGESTION INSPECTION OF E2 IAW AMM TASK 05-51-19-200-001-A. FOUND BLOOD ON SINGLE BLADE. CLEANED FAN BLADE AS REQUIRED. NO DAMAGE TO FRONT OR BACK OF FAN BLADE NOTED. NO OTHER FLUIDS OR FEATHERS NOTED.BIRSep 28, 2026 · N890UA · Airbus A319132 · Engine (Turbine/Turboprop)SDR REXA2026110402036Floor Support · damagedSECONDARY NRC FROM NRC 168: AFTER ANGLES REMOVAL, ELONGATED HOLES ON LONGITUDINAL BEAM LBL12 BTW FS280 TO FS275 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. LONGITUDINAL BEAM LBL12 BTW FS280 TO FS275 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW Sep 27, 2026 · N299PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR AALA202611023653Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER. MAINTENNCE REPLACED HINGE ARM END FITTING NUMBER 1LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR SWAA2026102976583Rail · corrodedFWD CARGO BAY, FOUND CORROSION AT MULTIPLE LOCATIONS ON THE AFT BULKHEAD LOWER RAIL, BS 500I, LBL 19 & RBL 23. REMOVED AND REPLACED THE BULKHEAD LOWER RAIL IAW SRM 51-40-02, AND DWG 143A9481, REV -.Sep 27, 2026 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102981593Stringer Clip · crackedCRACKED STRINGER CLIP 3R, BS 706. THE STRINGER CLIP WAS REPAIRED BY REPLACEMENT IAW SRM 51-10-02, STEP 9.C.Sep 27, 2026 · N8655D · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026102930701Stringer Clip · crackedFWD CARGO BAY, FOUND A STRINGER CLIP CRACKED AT BS 500I, STRINGER 26L. R & R THE STRINGER CLIP IAW SRM 51-40-02, DWG 143A1234- 0014, REV A.Sep 27, 2026 · N8655D · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026102942675Threshold Web · corrodedFWD CARGO BAY, FOUND CORROSION ON THE THRESHOLD WEB, BS 440+31 - 440+45, WL 156 (MULTIPLE LOCATIONS) THE FWD CARGO THRESHOLD WEB WAS REMOVED AND REPLACED BTWN BS 440 - 492.4 IAW SRM 51-40-02-0G-0, AND DWG 143A8330, REV -.Sep 27, 2026 · N8655D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102708475Tie Clip · crackedCRACKED TIE CLIP, BS 559, STRINGER 3L. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 144A1101, SHEET 19, REV-.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026102776552Web · crackedCRACKED WEB, BTWN BS 500D - 520, STR 28R. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026102733869Tie Clip · crackedCRACKED TIE CLIP, BS 277, STRINGER 10R. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 141A1110, SHEET 17, REV-.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026102774961Access Panel · crackedCRACKED ACCESS PANEL 211B, CONTROL STAND AT CONTROL CABIN. MEASURED DAMAGE AREA AND REPAIRED THE ACCESS PANEL WAS FOUND WITHIN LIMITS TO REPAIR THE LONGEST CRACK IN (4 IN2) IAW AMM 25-00-00-340-801, PROCEDURE 8E, METHOD 1.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026102725470Tie Clip · crackedCRACKED TIE CLIP, BS 597, STRINGER 3L. REPLACED TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 144A1103, SHEET 5, REV A.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026102779679Angle · crackedCRACKED ANGLE, BS 294.5, STRINGER 13L, FWD GALLEY AREA. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 141A1311, SHEET 1, REV C.Sep 27, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202610278465Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 2 LH HORIZONTAL STABILIZERI.A.W A320FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610271890Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 3 LHHORIZONTAL STABILIZER IAW A320FAM AMM 55-16-42-000-001-A ANDA320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610273401Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 6 OH HORIZONTAL STABILIZERI.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610270798Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 6 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610276820Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 3 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610271755Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 2 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610275811Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 4 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610272035Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 5 LH HORIZONTAL STABILIZER IAW A320FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610271726Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 5 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR AALA202610270223Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING NUMBER 1 RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.Sep 27, 2026 · N652AW · Airbus A320232 · Elevator StructureSDR SWAA2026102656126Web · crackedCRACKED WEB TRAILING EDGE AREA AT LEVEL ORSS 272, RT WING. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 16, REV -.Sep 27, 2026 · N8306H · Boeing 7378H4 · Wing Miscellaneous StructureSDR AALA202610265307Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L - MAINTENANCE REPLACED SHEAR PLATE PER SRM 51-72-11Sep 27, 2026 · N913US · Airbus A321231 · Fuselage Miscellaneous StructureSDR SWAA2026102395868Plate · crackedCRACKED CORRUGATED PLATE, TRAILING EDGE AREA AT LEVEL IRSS 220 AT RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2001, SHEET 67, REV-. DRILLED NEW CORRUGATED PLATE IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENTSep 27, 2026 · N8306H · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026102395893Plate · crackedCRACKED CORRUGATED PLATE, TRAILING EDGE AREA AT LEVEL ORSS 297, RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AREA AT LEVEL ORSS 297 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A3700, SHEET 61, REV-. DRILLED NEW CORRUGATED PLATE IAW SRM Sep 27, 2026 · N8306H · Boeing 7378H4 · Wing Miscellaneous StructureSDR AALA202610232005Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L - REPLACED SHEAR PLATE PER SRM 51-72-11Sep 27, 2026 · N913US · Airbus A321231 · Fuselage Miscellaneous StructureSDR ASAA2026092769385Trunnion · corrodedRIGHT MAIN GEAR FWD TRUNNION MOUNT FITTING, UPPER OUTBOARD BUSHING BORE HAS CORROSION ON OUTBOARD FACE & IN THE BORE. GROUNDED - YES. REPAIRED RH GEAR FWD TRUNNION MOUNT SUPPORT FITTING UPPER O/B BUSHING BORE & OUTER BORE FACE SURFACE IAW BOEING 737-800 SRM 57Sep 27, 2026 · N564AS · Boeing 737890 · Wing, Landing Gear Attach FittingsSDR ASAA2026092769384Trunnion · corrodedLEFT MAIN GEAR FWD TRUNNION MOUNT FITTING, LOWER OUTBOARD BUSHING BORE HAS CORROSION ON OUTBOARD FACE & IN THE BORE. GROUNDED - YES. REPAIRED LG GEAR FWD TRUNNION MOUNT SUPPORT FITTING LOWER O/B BUSHING BORE & BORE OUTER FACE SURFACE IAW BOEING 737-800 SRM 57-Sep 27, 2026 · N564AS · Boeing 737890 · Wing, Landing Gear Attach FittingsSDR ASAA2026092769383Trunnion · corrodedLEFT MAIN LANDING GEAR FWD TRUNNION MOUNT FITTING, LOWER INBOARD BUSHING BORE HAS CORROSION ON INBOARD FACE & IN THE BORE. GROUNDED - YES. REPAIRED LH GEAR FWD TRUNNION MOUNT SUPPORT FITTING LOWER I/B BUSHING BORE & BORE OUTER FACE SURFACE IAW BOEING 737-800 SSep 27, 2026 · N564AS · Boeing 737890 · Wing, Landing Gear Attach FittingsSDR HNAA2026101901011Firewall · crackedAPU FIREWALL WAS CRACKED ABOVE UPPER LEFT APU MOUNT ATTACH BRACKET. PERFORMED DOUBLER AND FILLER REPAIR ON APU FIREWALL IAW ETD2026-145-017372, REV A AND EO1-53-26-0511.Sep 27, 2026 · N656AE · Emb EMB145LR · APU Cowling/ContainmentSDR SCNA20261014429Skin · crackedWO 98046 NR00014 INITIAL / CRACK WAS FOUND OF: L=0.688IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.70 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-11150-RH, THE HORIZONTAL STAB WAS REPAIRED IAW SRM 55-10-01-2R-11, REPASep 27, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/SkinSDR SCNA20261014428Skin · crackedCRACK WAS FOUND OF: L=0.625IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 184.70 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-11150-RH,Sep 27, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/SkinSDR CALA2026101320340Feeder Cable · damagedDURING ALI VISIT, FOUND RT PYLON IDG FEEDER CABLE WIRE 2422-4519 INSULATION DAMAGED UNDER PANEL 521BT BETWEEN RIB 5A & PS 6480/RIB09 STA MLB. PERFORMED DAMAGE ASSESSMENT OF RT PYLON WIRE 2422-4519 IAW ESPM 20-53-21-02. REPAIRED WIRE WITH A GRADE 3 TEMP REPAIRSep 27, 2026 · N827UA · Airbus A319131 · Electrical Power System WiringSDR IPXA2026100252112Fairing · puncturedPUNCTURED SKIN, LT WING NR 4 FLAP TRACK AFT FAIRING EXTERNAL SKIN. REMOVE THE PUNCTURED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 240 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRSep 27, 2026 · N634UP · Boeing 7478F · Trailing Edge FlapsSDR CALA2026101220293Skin · damagedRAMP REPORT FWD CARGO LOWER AFT CORNER SKIN CUT OUT JUST ABOVE STRINGER 24 APROX BS 495. CUT OUT DAMAGE A REMOVED FASTERNERS COMMON TO THE REPAIR IAW SRM 53-00-01-2R-23, REPAIR 23 PGH 4 A-C 1,2,3. VERIFIED ACCOMPLISHMENT OF SRM 53-00-01-2R-23 STEPS 4 A THRU C(Sep 27, 2026 · N16701 · Boeing 737724 · Fuselage Main, Plate/SkinSDR IPXA2026100853404Collar · obstructedMAJOR REPAIR, DEVIATION DURING PERFORM SB EO-97169-REQ 1, HAD ONE COLLAR THAT CAN NOT BE INSTALLED. ACCOMPLISH IAW EO-97169-REQ4, REV 1, & EI F2026A53M-2113, REV 0, & REV 1.Sep 27, 2026 · N634UP · Boeing 7478F · Fuselage Main, StructureSDR AALA202610084684Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON EXPOSED INNER SKIN IN THE AFT CARGO AT RBL09 BETWEEN ST 767 AND 787. EXTERNAL DOUBLER, WITH CUTOUTS AND FILLERS IN 2 LOCATIONS IAW EA 379610.Sep 27, 2026 · N810NN · Boeing 737823 · Fuselage Main, Plate/SkinSDR IPXA2026100352096Seal · brokenBROKEN-MOLDING SEAL, LT WING NR 1,FLAP EXTERNAL SKIN MOLDING SEAL AREA. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70F FOR 20 HOURS IAW SRM 57-43-02-2R-4 REV.49 REFER TO SOPM 20-50-12 REV. 160.Sep 27, 2026 · N634UP · Boeing 7478F · Trailing Edge FlapsSDR CALA2026100520117Wire Harness · faultedEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - SEAT MOUNTED FLOOR PROXIMITY LIGHT AT 34ABC INOP REQUESTING MEL RELIEF, ALL MONUMENT MOUNTED LIGHTS OPERATIONAL, ALL FLOODLIGHTS AND EXIT IDENTIFIER LIGHTS OPERATIONAL, ALL OTHER SEAT MOSep 27, 2026 · N24224 · Boeing 737824 · Light System WiringSDR DALA2026100405477Oxygen Mask · leakingSUSPECTED CREW 02 LEAK. CA MASK AND BOX REPLACED. C/A: REFER TO LOG 6797929 FOR CORRECTIVE ACTION, OK TO CLOSE LOG. (LP: 1835948, AIRCRAFT WAS GROUNDED)Sep 27, 2026 · N345NB · Airbus A319114 · Crew Oxygen System