Service difficulty reports

1,769,551 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 IXXA20261016001Skin · crackedPERFORM REPLACEMENT OF THE FOLLOWING DAMAGE SECTION 43 FUSELAGE STRUCTURE FROM STA. 654 TO STA 785.9Oct 16, 2026 · N443AZ · Boeing 767323 · Fuselage Main, Plate/SkinSDR AALA202610294499Fitting · out of adjustAIRCRAFT IN BASE MAINTENANCE: L1 DOOR GIRT BAR FITTING REQUIRES ADJUSTMENT - MAINTENANCE ADJUSTED L1 DOOR GIRT BAR FITTINGS PER JOB CARD 26C83152006Oct 15, 2026 · N423AN · Airbus A321253NX · Emergency EquipmentSDR AALA202610294643Fitting · out of adjustAIRCRAFT IN BASE MAINTENANCE: R1 DOOR GIRT BAR FITTING REQUIRES ADJUSTMENT - MAINTENANCE ADJUSTED R1 DOOR GIRT BAR FITTINGS PER JOB CARD 26C83152006Oct 15, 2026 · N423AN · Airbus A321253NX · Emergency EquipmentSDR IPXA2026102159794Crossbeam · corrodedMDC COMPARTMENT SURFACE CORROSIONS (3 SPOTS) ON CROSSBEAM AT STA.324 BTWN RBL 45.5 BL 0. REMOVED CORROSION AT MDC COMPARTMENT SURFACE ON CROSSBEAM AT STA 324 BTW RBL 45.5 BL 0 IAW B757-200 SRM 51-10-02-0G-0. RESTORED SURFACE PROTECTION AT CROSSBEAM STA 324 BTOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026102460680Shear Web · corrodedMAIN CARGO COMPARTMENT, FLOOR STRUCTURE BTWN STA 333.45-345 LBL 45.5-54.9 HAS CORROSION UNDER DRAIN PLATE. AFTER REMOVED SURFACE PROTECTION ON REPORTED MARK IN SHEAR WEB FOUND 03 SPOT OF CORROSION LOCATED BTW STA 333.45-345 LBL 45.5-54.9. REMOVED CORROSION IAWOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102460794Shear Web · corrodedMAIN CARGO COMPARTMENT, FLOOR STRUCTURE BTWN STA 333.45-440 UNDER PANEL 221XCF HAS BARE METAL AND CORROSION. RESTORED SURFACE PROTECTION ONLY ON BAREMETAL AREAS. IAW B757-200 SRM 51-20-01 AND AMM 51-21-15-370-801. PERFORMED CHECK SURFACE SMOOTH, FOUND 63 MICROct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102460884Shear Web · corrodedMAIN CARGO COMPARTMENT, FLOOR STRUCTURE BTWN STA 333.45-418 UNDER PANEL 221XBF HAS BARE METAL AND CORROSION. RESTORED SURFACE PROTECTION ONLY ON BAREMETAL AREAS. IAW B757-200 SRM 51-20-01 AND AMM 51-21-15-370-801. PERFORMED CHECK SURFACE SMOOTH, FOUND 63 MICROOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102460967Shear Web · corrodedMAIN CARGO COMPARTMENT, FLOOR STRUCTURE BTWN STA 333.45-337.7 UNDER PANEL 221XAF HAS CORROSION . AFTER REMOVED SURFACE PROTECTION ON REPORTED MARK IN SHEAR WEB FOUND 05 SPOT OF CORROSION LOCATED BTW STA 324 TO STA 377.70 AND BTW BL0 TO LBL24.75. AFTER REMOVED Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102470613Shear Web · corrodedEVIDENCE OF CORR0SION IN MULTIPLE AREAS BELOW PANEL 231XCF. AFTER REMOVED SURFACE PROTECTION ON REPORTED MARK IN SHEAR WEB FOUND 06 SPOT OF CORROSION LOCATED BTW STA 440 TO STA 480 AND BTW LBL45.5 TO LBL62.75. PERFORMED CHECK SURFACE SMOOTH, FOUND 63 MICROINCHOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102473440Web · crackedFLOOR SUPPORT WEB CRACKED BETWEEN STA 480 & 500, RDL 45.5 & 55. REMOVED FLOOR SUPPORT WEB CRACKED BETWEEN STA 480 & 500, RDL 45.5 & 55 IAW B757-200 SRM 51-40-02. INSTALLED NEW FLOOR SUPPORT WEB BETWEEN STA 480 & 500, RDL 45.5 & 55.Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102173472Seat Track · corrodedCORROSION OVER SUPPORT FLOOR STA 520/RBL 45.5. REMOVED CORROSION ON BOTTON SURFACE OF SEAT TRACK, STA 520 AND RBL 45.5. MATERIAL LOSS: 0.025'' IAW B757 SRM 53-00-52-1A-1 AD1 DETAIL I. RESTORED SURFACE PROTECTION IAW B757 SRM 51-20-01 AND AMM 51-21-15-370-80Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101973887Deck Plate · corrodedMAIN DECK, FLOOR DECK HAS SEVERAL SPOTS WITH CORROSION BETWEEN BL0 & RBL65 AND STA 1680 & AFT PRESSURE BULKHEAD. REWORKED AREAS.MAIN DECK, FLOOR DECK, BETWEEN BL0 & RBL65 AND STA 1680 & AFT PRESSURE BULKHEAD. IAW B757-200PF 51-10-02-0G-0, PARAGRAPH 15 A (5)(A)Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026101873907Seat Track · corrodedMAIN DECK, FLOOR STRUCTURE SEAT TRACK (BASE) HAS CORROSION AT BL0 BETWEEN STA 1640 & STA 1540 (UPPER AND LOWER SIDE). REMOVED CORROSION (3 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. B757-200PF SRM 51-10-02 AND EVALUATED I.A.W. B757-200PF SRM 53-00-52-1A-1. ROct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101873914Seat Track · corrodedMAIN DECK, FLOOR STRUCTURE SEAT TRACK (BASE) HAS CORROSION AT RBL25 BETWEEN STA 1640 & STA 1540 (UPPER AND LOWER SIDE). REMOVED CORROSION (1 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. B757-200PF SRM 51-10-02 AND EVALUATED I.A.W. B757-200PF SRM 53-00-52-1A-1.Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101873875Seat Track · corrodedFAULT - STR - 200 - MAIN DECK, FLOOR STRUCTURE SEAT TRACK (BASE) HAS CORROSION AT RBL45 BETWEEN STA 1620 & STA 1540 (UPPER AND LOWER SIDE) (MARKED IN RED) (DOT 64-011). REMOVED CORROSION (5 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. B757-200PF SRM 51-10-02 AOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102473951Web · corrodedMAIN DECK, FLOOR STRUCTURE WEB HAS CORROSION AT RBL45 BETWEEN STA 1600 & STA 1580 (DOT 64-013). LIGHT SANDING BY HAND SURFACE, LIGHT CORROSION AT MAIN DECK, FLOOR STRUCTURE WEB, RBL45 BETWEEN STA 1600 & STA 1580 FOUND TO BE WITHIN LIMITS IAW SRM 51-10-02-0G-0Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026101973945Floorbeam · corrodedMAIN DECK, FLOOR STRUCTURE, FLOOR BEAM AT STA 1600 HAS CORROSION BETWEEN RBL45 & RBL65 (UPPER AND LOWER SIDE). REMOVED CORROSION ON MAIN DECK, FLOOR STRUCTURE, FLOOR BEAM AT STA 1600 BETWEEN RBL45 & RBL65 IAW SRM 51-10-02. APPLIED SURFACE PROTECTION ON AREAS ROct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026101973990Floorbeam · corrodedMAIN DECK FLOOR STRUCTURE, FLOOR BEAM AT STA 1540 HAS CORROSION BETWEEN BL0 & RBL25 (UPPER AND LOWER SIDE). REMOVED CORROSION ON MAIN DECK FLOOR STRUCTURE, FLOOR BEAM AT STA 1540 BETWEEN BL0 & RBL25 IAW , SRM 51-10-0. APPLIED SURFACE PROTECTION ON AREAS REWORKOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026101874023Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK (BASE) HAS CORROSION AT RBL65 BETWEEN STA 1500 & STA 1480 (UPPER AND LOWER SIDE). REMOVED CORROSION (3 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. SRM 51-10-02 AND EVALUATED I.A.W. SRM 53-00-52-1A-1. RESTORED SURFACE PROTOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101974063Floorbeam · corrodedMAIN DECK FLOOR STRUCTURE, FLOOR BEAM HAS CORROSION AT STA 1540 BETWEEN RBL 25 & RBL 45. REMOVED CORROSION MAIN DECK FLOOR STRUCTURE, FLOOR BEAM AT STA 1540 BETWEEN RBL 25 & RBL 45 IAW SRM 51-10-02, WITHIN LIMITS IAW SRM 53-00-51-1A-1. APPLIED SURFACE PROTECOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026101874066Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK (BASE) HAS CORROSION AT RBL45 BETWEEN STA 1540 & STA 1520. REMOVED CORROSION (3 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. SRM 51-10-02 AND EVALUATED I.A.W. SRM 53-00-52-1A-1. RESTORED SURFACE PROTECTIVE I.A.W. SRM 53-0Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101874088Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK (BASE) HAS CORROSION AT BL0 BETWEEN STA 1520 & STA 1420 (UPPER AND LOWER SIDE). REMOVED CORROSION (1 POINTS) FROM SEAT TRACK FLANGE (BASE) I.A.W. SRM 51-10-02 AND EVALUATED I.A.W. SRM 53-00-52-1A-1. RESTORED SURFACE PROTOct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101974102Floorbeam · corrodedMAIN DECK FLOOR STRUCTURE, FLOOR BEAM HAS CORROSION AT STA 1320 BETWEEN RBL25 & RBL45. REMOVED CORRORION ON MAIN DECK FLOOR STRUCTURE, FLOOR BEAM, AT STA 1320 BETWEEN RBL25 & RBL45 IAW B757-200PF, SRM 51-10-02. APPLIED SURFACE PROTECTION ON AREAS REWORKED IAW Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR SWAA2026102791019Chute Assy · crackedCRACKED CHUTE ASSY IN THE FWD CARGO BAY. REPLACED THE CHUTE ASSY BTWN BS 500B TO 500C RT SIDE IAW SRM 51-40-02.Oct 15, 2026 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026101974382Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK BASE (BOTH SIDES) HAS CORROSION AT RBL 25 BETWEEN STA 1200 & 1180. REMOVED DAMAGE FROM SEAT TRACK BASE AT RBL 25 BETWEEN STA 1200 & 1180 IAW B757-200PF SRM 51-10-02. TREATED AND PRIMED AREA IAW B757-200PF SRM 51-20-01.Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101974455Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK BASE (BOTH SIDES) HAS CORROSION AT BL 0 BETWEEN STA 1200 & 1180. REMOVED DAMAGE FROM SEAT TRACK BASE AT BL 0 BETWEEN STA 1200 & 1180 IAW B757-200PF SRM 51-10-02. TREATED AND PRIMED AREA IAW SRM 51-20-01.Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102766538Skin · dentedMAJOR REPAIR. AGING ACFT INSPECTION- RIGHT WING #10 SLAT HAS A DENT ON UPPER SURFACE OUTBD END. NO DOT. OK TO INSTALL REPAIR PARTS "INSP ONLY" (PER GMM 04-02 ATA 51 #2(C) RII MAJOR REPAIR)Oct 15, 2026 · N462UP · Boeing 75724APF · Leading Edge DevicesSDR N6WA2026102311Fms · failedFMS FAILED, NOT AVAILABLE. RERACKED IAPS FMC MODULE IAW AMM-34-61-07. OP CHKD GOOD.Oct 15, 2026 · N524GJ · Cndair CL6002C11 · Flight Management Computing Hardware SystemSDR N6WA2026102310Relay · faultedLOW OIL PRESSURE WARNING -RFF (ACARS MSG 0651HRS). R & R RELAYS K61 AND K62 IAW CRJ-ESPM-20-39-00. OP CHECK/ENGINE RUN OKAY ATT THIS TIME.Oct 15, 2026 · N526GJ · Cndair CL6002C11 · Engine Oil Indicating SystemSDR N6WA2026102309Door · no discrepancyPAX DOOR WILL NOT OPEN. PERFORMED A DETAILED INSPECTION AND OPS TEST OF THE PAX DOOR AND MECHANISM IAW AMM 52-11-00-710-801, & AMM 52-11-02-710-801. DOOR OPS NORMAL. ACFT OK FOR SERVICE.Oct 15, 2026 · N543GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR HYIA20261023002Elbow · crackedDURING ROUTINE INSPECTION THE LEFT ENGINE OUTBOARD EXHAUST ELBOW WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE ELBOW WITH NO FURTHER DEFECTS NOTED.Oct 15, 2026 · N722CA · Tecnam P2012 · Engine Collector/Tailpipe/NozzleSDR AALA202610237245Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202610239538Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202610235242Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202610237010Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202610230099Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202610230246Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Oct 15, 2026 · N912UY · Airbus A321231 · Horizontal Stabilizer StructureSDR SWAA2026102207678Battery · inoperativeALL EMERGENCY LIGHTS COMMON TO BATTERY M1676 INOP. BATTERY REPLACED AND PERFORMED GOOD OPS CHECK OF EMERGENCY BATTERY AND POWER SUPPLY M1676 PER AMM 33-51-06-960-803 AND AMM 33-51-06-960-802.Oct 15, 2026 · N8736J · Boeing 7378 · Emergency LightingSDR SWAA2026102267953Power Supply · inoperativeALL EMERGENCY LIGHTS COMMON TO BATTERY M1676 INOP ALL EMERGENCY LIGHTS COMMON TO BATTER M1676 INOP REPLACED AND PERFORMED GOOD OPS CHECK OF EMERGENCY BATTERY AND POWER SUPPLY M1676 PER AMM 33-51-06-960-803 AND AMM 33-51-06-960-802.Oct 15, 2026 · N8736J · Boeing 7378 · Emergency LightingSDR MASA20261022240Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII FR84 RBL5 FOUND CORRODED CROSSBEAM UPPER FLANGE AND I BEAM UPPEER FLANGE. REMOVED AND REPLACED I BEAM AT CFIII FR 84 RBL25-29.5 IAW EMBRAER 175 SRM51-43-03 REV OCT 20-23 AND CARRIED OUT PERMANENT REPAIR ON CROSSBEAM UPPEOct 15, 2026 · N83329 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR MASA20261022239Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII FR84 RBL5 FOUND CORRODED CROSSBEAM UPPER FLANGE CARRIED OUT PERMANENT REPAIR ON CROSSBEAM UPPER FLANGE IAW ETD 2026-170-016565 SEE AWS AND NOT REPORT# TW048418-16 FOR DETAILS, NOT FINDINGS NO CRACK FOUND. NRC # 4502703-2Oct 15, 2026 · N83329 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR IPXA2026101973542Floorbeam · corrodedLIGHT CORROSION UNDER NUT PLATE BS 700 BTWN RBL 45.5 & 25.5. REMOVED NUT PLATE AND INSTALLED NEW NUT PLATE IAW SRM 51-40-02-0G-0.Oct 15, 2026 · N462UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR 4EZF20261015362AGStarter Gen · overtempR GEN OVER TEMP LGT ILLUMINATING WITH GEN ONLINE. REMOVED AND REPLACED THE RH STARTER GENERATOR IAW SAAB 340B AMM 24-31-05-04. OPERATIONAL TEST SATISFACTORY.Oct 15, 2026 · N326AG · Saab 340B · DC Generating SystemSDR CALA2026102220516Warning Light · false activationREJECTED T/O DUE TO RT FWD OVERWING LIGHT & T/O CONFIG WARNING. TAKE OFF WAS REJECTED AT AROUND 60 KTS. CREW REPORTED THERE WERE NO SIGNS OF DOOR MOVEMENT. MAINT LIGHT WAS ILLUMINATED & RT FWD OVERWING DOOR LIGHT FOUND ILLUMINATED. PERFORMED PSEU TEST. Oct 15, 2026 · N17456 · Boeing 7379 · Door Warning SystemSDR DALA2026102105802Fuse · blownDURING SVC CHECK, FOUND EXTERIOR EMERGENCY LT @ LEFT FUSELAGE BEHIND WTB AREA INOP. R/R FUSE #9 ON BATT PACK M738 (9373303) (AIRCRAFT GROUNDED)Oct 15, 2026 · N172DZ · Boeing 767332 · Emergency LightingSDR DALA2026102105798Stringer · corrodedREPAIR ON STRINGER 34L LOCATED BTW STA 522 PLUS 10 IN AND STA 566 PLUS 10 IN AT FWD CARGO COMPARTMENT AS PER B767-400 SRM 53-00-03. SECONDARY FINDING CORROSION STRINGER 34L LOCATED STA 544 AT FWD CARGO COMPARTMENT. (1867597)(AIRCARFT GROUNDED)Oct 15, 2026 · N843MH · Boeing 767432ER · Fuselage Main, Longeron/StringerSDR AALA202610217203Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO SEVERAL SPOTS OF EXFOLIATION CORROSION ON RIGHT-HAND TRANSITION PANEL BETWEEN STATIONS 767 AND 787, RIGHT BUTT LINE 24 JUST FORWARD OF DOOR CUTOUT. MAINTENANCE REMOVED AFT CARGO FORWARD SHIELD BETWEEN STATIONS 767 AND 78Oct 15, 2026 · N961NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR DALA2026102105767Floor Support · corrodedAFT GALLEY WET AREA FWD L2 DOOR FLOOR INTERCOSTAL CORROSION BETWEEN STA 967 TO 947 L/H SIDE CENTER. CORROSION ON INTERCOSTAL LOCATED BETWEEN STA 967 TO 947 L/H SIDE CENTER. FOUND TO BE OUT OF LIMITS. LOCATED DRILLED, TREATED, AND PRIMED NEW INTERCOSTAL. INSTOct 15, 2026 · N891DN · Boeing 737932ER · Fuselage Miscellaneous StructureSDR AALA202610208372Bottle · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 831 DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTIONAL TEST - REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14Oct 15, 2026 · N120EE · Airbus A321231 · Passenger/Crew DoorsSDR SWAA2026101970438Seat · looseSEAT ROW LOOSE AT 15FED REMOVED AND REINSTALLED SEAT ROW 15FED IAW AMM 25-22-00-401-NG T.W:K01112 CAL:17DEC2025 DUE:31DEC2026 VERIFIED REMOVED AND REINSTALLED SEAT ROW 15FED IAW AMM 25-22-00-401-NG T.W:K01112 CAL:17DEC2025 DUE:31DEC2026Oct 15, 2026 · N7887A · Boeing 737752 · Passenger Compartment Equipment