Service difficulty reports
1,771,708 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA202603183632Sign · peelingAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND EMERGENCY EXIT PLACARD AFT OF ROW 16ABC OVERWING EXIT DOOR PEELING. REMOVE AND REPLACED EMERGENCY EXIT LIGHT LENS. PER AMM 33-51-01.SDR AALA202603182074Sign · peelingAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND EMERGENCY EXIT PLACARD AFT OF ROW 16DEF OVERWING EXIT PEELING. REMOVE AND REPLACED EMERGENCY EXIT LIGHT LENS. PER AMM 33-51-01.SDR AALA202603184221Battery · depletedAIRCRAFT WAS NOT GROUNDED: FOUND FORWARD L1 DOOR EMERGENCY BATTERY DEPLETED. REMOVED AND REPLACED BATTERY PACK ON L1 DOOR. PER AMM 33-51-06. OPS CHECK GOOD.SDR QR9R2026031800001Display · failedVEMD LANE 2 FAILURE DURING HOVER TAXI. VEMD HAS AN INTERNAL FAILURE. LANE 2 WOULD NOT PASS SELF TEST/INITIALIZATION PAGE. REMOVED AND REPLACED VEMD IAW AMM 31-60-00, 4-2.SDR DALA2026031801874Skin · corrodedCRACK ON STRUCTURE ARROUND OF THE CABLE CRAFT HANDLE RH /LH TOILET INTO AFT LAVATORY SERVICE DOOR PANEL AT LOWER FUSELAGE (ZONE 100). AFT LAVATORY SERVICE DOOR PANEL AT LOWER FUSELAGE WAS REPAIRED PER PRI 632905-14 REV. 0 TO REV 1 AND ER/A 632905-14 REV. ORSDR DALA2026031801873Intercostal · corrodedCORROSION ON INTERCOSTAL FROM STA. 1520 TO STA 1540 AND STR 29R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. INTERCOSTAL FROM STA. 1520 TO STA 1540 AND STR 29R AT AFT CARGO COMPARTMENT.WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR. 7. D. (1499827)SDR IXXA2026031801Angle · crackedFUSELAGE INTERCOSTAL ANGLE AT STA 1351 S17R IS CRACKEDSDR JR2R20260318119Seat Track · corrodedSEAT TRACK BEAM LBL11 FR17 CORRODED. REPAIREDSDR JR2R20260318118Seat Track · corrodedSEAT TRACK BEAM LBL11 FR18 CORRODED. REPAIREDSDR ABXA20260318116Fire Warning · false activationDURING CRUISE, R ENG FIRE LP 1 STATUS MSG ILLUMINATED. MAINTENANCE PERFORMED OPS CHECK IAW B767 AMM 26-11-00. OPS CHECK GOOD. AIRCRAFT REMAINS NO ETOPS DEFERRED IAW MEL 26-11-1-1. PLACARDS INSTALLED. NO DEACTIVATION PROCEDURES REQUIRED. REF LP 39307-90/1. AISDR JR2R20260318120Floorbeam · corrodedEXISTING FLOOR BEAM REPAIR AT FR16 LBL11 CORRODED. REPLACE REPAIRSDR ABXA20260318115Warning Message · illuminatedDURING CRUISE, EICAS MESSAGE INFLIGHT FIRE/OVHT SYS. EICAS MESSAGE INFLIGHT FIRE/OVHT SYS PREVIOUSLY DEFERRED; DI 71505 REF LOG PG 39439-75/2 DEFERRED ON 15 MAR 26. AIRCRAFT RETURNED TO SERIVCE.SDR JR2R20260318107Floorbeam · corrodedEXISTING FLOOR BEAM REPAIR AT FR19 LBL11 CORRODED. REPLACE REPAIRSDR ABXA20260318114Warning Message · false activationDURING TAXI OUT, AFTER BLOCK OUT THE RAT UNLOCKED MESAGE ON EICAS. A/C RETURNED TO BLOCKS (BTB). DEPLOYED AND RESTOWED RAT IAW B767 AMM 29-21-00. MESSAGE CLEARED. NO FAULTS PRESENT AT THIS TIME. RAT GUARD RESECURED. A/C RETURNED TO SERVICE.SDR ABXA20260318113Starter · defectiveDURING ENGINE START, L ENG STARTER EICAS MESSAGE, UNABLE TO START NO. 1 ENGINE, NO N2. AIRCRAFT RETURNED TO BLOCKS (BTB). T/S #1 ENG STARTER IAW B767 FIM 80-11 FT 805. REMOVED AND REPLACED #1 ENG STARTER IAW B767 AMM 80-11-02. OPS CHECK #1 ENG IAW B767 AMM 7SDR AALA202603185329Wire · brokenAIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS AT 17ABC AND 18ABC INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE ON HARNESS AT SEAT 17 ABC, RE-PINNED WIRE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-50-00SDR JR2R20260318122Floor Support · corrodedLH FLOOR SILL AFT OF THE L1 DOOR BETWEEN FR19 - FR20 CORRODED.SDR JR2R20260318049Frame · chafedLH PYLON AFT FAIRING FRAME 3 I/B ATTACH POINT CHAFED.SDR JR2R20260318050Frame · chafedLH PYLON AFT FAIRING FRAME 5 I/B ATTACH POINT CHAFED.SDR SCNA20260318128Holder · looseGIRT BAR HOLDER ON L1 DOOR LOOSE. ACOMPLISHED REPAIR OF THE DOOR 1L GRIT BAR HOOK PER SCA EA 25-0138 THIS CLEARS MEL 52-16-1.SDR AALA202611067618Hydraulic Line · leakingAIRCRAFT WAS GROUNDED: HYD Y RSVR LO LEVEL. THE RESERVOIR IS INDICATING EMPTY. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE SUPPLY LINE LEAKING FOR THE T/R ISOLATION VALVE ON RT ENG. R/R PRESSURE SUPPLY LINE IAW AMM 29-13SDR SWIA2026031777458Angle · corrodedGALLEY SERVICE DOOR SURROUND STRUCTURE LOWER SILL ANGLE, MOUNTING HAS CORROSION ON BOTH SIDES. REMOVED AND REPLACED LOWER SILL ANGLE MOUNTING REF SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y.SDR SWIA2026031777402Floorbeam · crackedCOCKPIT FLOORBEAM AT APPROX FS 28000 LBL12 HAS CRACK TRANS 31900501 C-CHECK RO 09302026REPARED COCKPIT FLOORBEAM AT LBL1200 REF CRJ700 SRM 53-11-43-201-003-A01 AND COMPLIED WITH FORM M337 AND TASK CARD 51-900-1002-SKY,SEE CONTINUE CARD FORE MORE DETAILSSDR SWIA2026031777387Floorbeam · crackedCOCKPIT FLOORBEAM AT APPROX FS 28000 RBL12 HAS CRACK. INSTALLED REPAIR PARTS FOR COCKPIT FLOORBEAM AT RBL1200 REF SRM 53-11-43-201-003-A01SDR SWIA2026031777357Attach Angle · crackedATTACH ANGLE AT BS 280, RBL12 HAS CRACK. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21-001-001-A1 AND DWG CC670-34010 REV -K ,SDR SWIA2026031777080Pressure Web · crackedINSIDE THE AIRCRAFT CABIN AT APPROX FS. 461.00 PRESSURE BOX SKIN SURFACE BETWEEN RBL9 AND LBL 9 SHOWS SIGNS OF CRACKS (2 CRACKS) (C-CHECK RO 08/31/2026)REPAIRED TO PRESSURE FLOOR WEB AT FS 461.00 BETWEEN LBL 9 AND RBL 9 IAW CRJ200 MHIRJ REO 601R-53-41-3419 RSDR CALA2026082718966Skin · fomLEFT HORIZONTAL STAB LOWER SKIN AT BS 92.70 BETWEEN NR 2 & 3 VERTICAL STIFFENER REQUIRES CUTOUT TO FOM. COMPLIED WITH CUTOUT LOWER SKIN AT STA 92.70 BETWEEN NR 2 & 3 VERTICAL STIFFENERS IAW SRM 55-10-01-2R-11. ACCOMPLISHED SURFACE HFEC IN SP OF CUTOUT & AREASDR REXA2026050700502Support Bracket · crackedBROKEN SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM. SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & EA CRJ957-22035 REV. IR.SDR REXA2026050500490Hinge · corrodedSECONDARY NRC IN REF TO RC 900-27-900-910: CORROSION ON LUG BORES L5 AND L6 IN CENTER FITTING AT LEFT AILERON. LUG BORES L5, L6 AND L1 IN CENTER FITTING AT LEFT AILERON WERE REPAIRED PER REO 670-57-61-237 REV -- & REO 690-57-61-511 REV - ASDR VNAA20260501012Seat Track · corrodedCORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM SDR VNAA20260501011Seat Track · corrodedCORROSION ON SEVERAL POINTS SEAT RAIL BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. SEAT TRACK BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-ASDR VNAA20260501010Seat Track · corrodedCORROSION ON SEVERAL POINTS SEAT RAIL BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. SEAT TRACK BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 AND REPLACED IAW AMM 53-00-49 (CONFIG A12).SDR VNAA20260501009Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL (1EA) BTW STA FS 661+16 TO STA FS 669.40. CORROSION ON RH SIDE SEAT RAIL (1EA) BTW BS 661+16 TO BS 669.40 WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER AMM 53-00-49-400-801-A12.SDR VNAA20260501008Seat Track · corrodedWEAR ON LH SIDE SEAT RAIL (1EA) ,BTW STA FS 379 TO STA FS 469.00,AND WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 469.00 TO STA FS 581,ALSO WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 581 TO STA FS 661+16. AND CORROSION ON WEAR LH SIDE SEAT RAIL (2EA) BTW STA FS 661+16SDR 3EJA2026050100726Actuator · looseLANDING GEAR WILL NOT RETRACT AFTER TAKEOFF ( RED GEAR UNLOCK LIGHT REMAIN ON) FOLLOWED WITH QRH PROBLEM REMAINED. RETURNED BACK TO RBD AIRPORT SAFELY.//////DISCOVERED LH MAIN LANDING GEAR ACTUATOR JAM NUT TO BE LOOSE PERFORMED ROD ENG ADJUSTMENT AND SECURED JSDR SWAA2026042880786Scuff Plate · crackedCRACKED FWD SCUFF PLATE IN THE AFT CARGO COMPARTMENT CUTOUT. REPAIRED THE FWD SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026042280779Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221BF IN THE FWD GALLEY. REPAIRED FLOOR PANEL 221BF AT FWD GALLEY IAW SRM 53-00-50-2R-7, REPAIR 7.SDR SWAA2026042280770Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221GF IN THE FWD GALLEY. REPAIRED THE FLOOR PANEL 221GF IAW SRM 53-00-50-2R-7, REPAIR 7.SDR SWAA2026042280597Floorbeam · crackedCRACKED FLOORBEAM BS 967, LBL 50. PERFORMED REPAIR AT FLOORBEAM IAW EA 26-153-00821, AND 26-153-00821, WIP 1, & WIP 2.SDR SWAA2026042280766Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 434CL AT LT PYLON. REPLACED ACCESS PANEL 434CL LOC. LT PYLON IAW B737-700 AMM 05-41-04-210-814 STEP 14. E(5) THE INSTALLATION IS DOCUMENTED TTG8Q01ACG7W.SDR SWAA2026042280783Access Panel · crackedCRACK ON ACCESS PANEL 551GB AT TRAILING EDGE LT WING. REPAIRED ACCESS PANEL 551GB AT TRAILING EDGE LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202604179502Channel · corrodedAIRCRAFT IN BASE MAINTENANCE: LEVEL 2 CORROSION ON AFT CARGO BAY ZEE CHANNEL AT BS 727 PLUS 3 INCHES, AT LBL 35. REPLACED ZEE CHANNEL IAW SRM 53-00-53-2R-5.SDR SWAA2026041480751Angle · crackedCRACK ANGLE LOCATED STA500I AND RBL 7 AT FWD CARGO COMPARTMENT. REPLACED ANGLE IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A7902, SHEET 320, REV -, & SRM 53-00-53-1A-2.SDR SWAA2026041380738Cartridge · crackedCRACK FOUND ON RH O/B AFT FLAP CATRIDGE INNER SURFACE; L: 0.380. REMOVED AND REPLACED RT OTBD AFT FLAP CARTRIDGE IAW SRM 51-40-02 AND GWN# 113A3700 REV: F.SDR SWAA2026040980584Baffle · crackedFCB BAFFLE IS CRACKED AT BS440-BS460 LBL25; WL156<[01] REMOVED AND INSTALLED FCB BAFFLE AT BS440 TO BS460; LBL25 PER SRM 51-10-02 AND DWG 143A7505 REV:-;[02] VERIFIED CORRECTIVE ACTION 1SDR IPXA2026040115702Floor Support · corrodedAFTER REMOVAL OF FLOOR TAPE FOUND AFT CARGO COMP FLOOR CENTER STRINGER STA 1475 RBL 2 EXFOLIATED INSTALLED 10 EA NUT PLATES ON NEW FLOOR SUPPORT STRINGER AND INSTALLED FLOOR SUPPORT STRINGER AT AFT CARGO STA 1443.6 TO 1495 RBL 2 IAW B757-200 SRM51-40-02-0G-SDR AALA202604018233Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER TEE CAP AT BS 947 AND RBL 51. REPLACED UPPER TEE PER SRM 53-70-51-2R-5.SDR AALA202604015064Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER TEE CAP AT BS 947 AND RBL 24.75. REPLACED UPPER TEE CAP PER SRM 53-70-51-2R-5.SDR AALA202604015821Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER TEE CAP AT BS 947 AND LBL 26. REPLACED UPPER CHORD PER SRM 53-70-51-2R-5.SDR AALA202603317074Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.