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 SWIA2026050176636Bulkhead Web · corrodedUPON REMOVAL OF THE BS 280 CROSSBEAM LT THE COCKPIT BULKHEAD LOWER WEB HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE CROSSBEAM, THE COCKPIT BULKHEAD LOWER WEB IAW SRM 53-00-00, 51-42-06, 51-42-13, 53-11-10, 51-21-11, 51-25-06, 51-42-21, 51-25-16,, AMM 25SDR QREA202607070001Pressure Switch · stuckRIGHT ENGINE OIL PRESSURE LOW WARNING- OIL PRESSURE SWITCH STUCK IN THE OIL PRESSURE ZERO POSITIONSDR REXA2026070301060Floorbeam · corrodedSECONDARY NRC FROM NRC 00088': AFTER REMOVAL SUPPORT ANGLE, CORROSION ON FS 280 CROSS BEAM LH SIDE WAS FOUND. DUE TO EXCESSIVE CORROSION ON FS 280 CROSS BEAM LH SIDE WAS REPLACED PER CRJ/900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-10-001-SDR REXA2026070301019Floorbeam · damagedSEVERAL ELONGATE HOLES WERE FOUND ON CROSSBEAM AND ANGLE ATTACHED TO CROSSBEAM. ELONGATE HOLES ON LH SIDE WERE ATTENDED WITH THE REPLACE OF CROSSBEAM UNDER NRC 00097 AND ELONGATE HOLES RH SIDE WERE REPAIRED PER REO 690-53-11-2188 REV. A.SDR REXA2026070301018Rib · crackedCRACK ON LEADING EDGE RIB SS57.16 AT RH WING. CRACKED ON LEADING EDGE RIB SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-604 REV. --SDR REXA2026070301017Floorbeam · corrodedCORROSION ON ANGLE FLOOR SUPPORT AT FS 280.00 AND BRW LBL 9.00 TO RBL 9.00 CORROSION ON ANGLE FLOOR SUPPORT AT FS 280.00 AND BRW LBL 9.00 TO RBL 9.00 WAS EVALUATED OUT OF LIMITS CRJ/900 SRM 51-10-06-001-001-A01 AND ANGLE WAS REPLACED PER CRJ 900 SRM 51-42-06-0SDR VNAA202606120006Web · crackedCRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.SDR VNAA202606120005Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01SDR SIMA20260501002Seal Rest · corrodedREMOVE AND REPLACE FWD CARGO AFT DOOR SEAL REST CORRODED. (MAJOR REPAIR/LVL 2 CORROSION) RAR FWD CARGO AFT DOOR SEAL REST IAW ERJ 170 SRM 51-40-08, SRM 51-21-02, SRM 51-21-01, AND AMM 20-10-01SDR AALA202606055414Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD AT STA 847 AND S25R. REPLACED SHIELD PER AARD 51-00-05-1.SDR SWAA2026060394602Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.500 IN. APPROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GASDR SWAA2026060394724Lug · corrodedCORROSION ON REAR LOWER LUG AFT SIDE AT LT HORIZONTAL STABILIZER. REPAIRED REAR LOWER LUG LOCATED AFT SIDE AT LT HORIZONTAL STABILIZER IAW EA# 26-155-01244-WIP1; EA# 26-155-01244-WIP2 AND EA# 26-155-01244.SDR IPXA2026051469624Stringer · crackedMAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 2598 S-6L. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60316 STEP 11 (SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR IAW EO-97410-REQ0028 REV.1 AND EGAT EI F2026ASDR IPXA2026051469637Stringer · crackedMAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 2598 S-8L. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60312 STEP 11 (SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0030 REV.1 AND EGAT EI F20SDR IPXA2026051469626Stringer · crackedMAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 2598 S-6R. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60315 STEP 11 (SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0032 REV.1 AND EGAT EI NO.SDR IPXA2026051469664Stringer · crackedMAJOR REPAIR. STRINGER CRACKED, FWD SIDE OF BS 2598, S-8R. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60311 STEP 11 (SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0034 REV.1 AND EGAT EI SDR IPXA2026051469611Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2598 S-4R. ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0036 REV.1 AND EGAT EI NO.F2026A53M-1029 REV.0 AND EGAT WORK SHEET 60320 AND SRM 53-80-03-2R-2 REV.48.SDR AALA202606020528Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN STA 727 AND STA 793 AT RBL 50. REPLACED SHIELD PER AARD 51-00-05-1.SDR AALA202606027229Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 727D AND 727E AT RBL 34. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR SWAA2026060194686Angle · crackedCRACK ANGLE LOCATED BETWEEN STA380 TO STA400 AND LBL13 WL 208.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BETWEEN STA380 TO STA400 AND LBL13 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 140 RESDR SWAA2026060194688Angle · crackedCRACK ANGLE LOCATED BETWEEN BS 380 TO 400 AND LBL52 WL 208.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO 400 AND LBL52 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET: 140 REV:-.SDR AALA202606011321Web · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON AFT CARGO COMPARTMENT DOOR THRESHOLD WEB BETWEEN STA 807 AND STA 847 AT RBL 24. REPLACED WEB PER AARD 51-00-05-05.SDR SWAA2026052894474Tray · brokenBROKEN FOOD TRAY, SEAT ROWS 1B; 5B; 3B; 7A; 7B; 15A; 19C AND 24C IN THE PASSENGER CABIN. REPLACED FOOD TRAYS IAW CMM-25-21-45-3860, REV 7, FIG 4, PAGE 10102, ITEM 60, & 60A PAGE 10104, STEP 3.AB.(1) PAGE.7018.SDR SWAA2026052894470Table · brokenBROKEN TABLE ON SEAT ROW POSITION 2D; 3D; 4D; 5D; 8D; 15F; 16DEF; 17D; 18DE; 19E; 24E. REPLACED TABLE ON SEAT ROW POSITION 2D; 3D; 4D; 5D; 8D; 15F; 16DEF; 17D; 18DE; 19E; 24E IAW CMM-25-21-45-3860, REV -. FIGURE 4, ITEM 60A, PAGE 10104, STEP 3. AB.(1). PAGE SDR SWAA2026052894738Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN IAW AMM-33-51-15-400-802.SDR SWAA2026052894748Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, RBL 40, BS 663 IN THE PAX CABIN. CRACK LENGTH APPROX. 0.375 INCH. PERFORMED PERMANENT REPAIR ON THE HORIZONTAL PRESSURE DECK WEB BTW RBL 30 - RBL 60, BTW BS 663 - 675 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026052894730Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026052894739Scuff Plate · crackedCRACK CENTER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026052794700Skin · delaminatedDELAMINATED ON UPPER AREA NEAR OF HINGE ELEVATOR 5 OF LT ELEVATOR. REPAIRED UPPER AREA NEAR OF HINGE ELEVATOR 5 OF LT ELEVATOR IAW SRM 55-20-01-2R-1 REPAIR 1 AND SRM 51-70-05-2R-1 REPAIR 1.SDR AALA202605229367Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE WEB BETWEEN STA 986 AND STA 992, BETWEEN RBL 50 AND RBL 54. REPLACED WEB PER AARD 51-00-05-1.SDR SWAA2026052294705Access Panel · damagedELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026052294704Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS867 LBL19 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS867 LBL19 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0; DWG 149A8102 SHEET 19 REV A AND DWG 149A8104 SHEET 1 REV B. MEASUREMENT OF CRACK IS L= 1.435? INCH.SDR SWIA2026050176020Seal Rest · chafedAFT PAX DOOR UPPER FWD CORNER SEAL REST HAS CHAFING DAMAGE ON INTERIOR SIDE. REMOVED AND REPLACED AFT PAX DOOR UPPER FWD CORNER SEAL REST, REF SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED.REPLACED WITH FACTORY PART.SDR AALA202605195602Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND VACUUM WASTE VENT AT STA 917 AND S21L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR IPXA2026050679318Profile · crackedMCD FR75 RH CRACK FOUND IN THE Z-PROFILE. INSTALLED NEW Z- PROFILE. MCD FR75 RH: I.A.W. A300-600 SRM 51-40-21-001SDR MASA20260512115Support Plate · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE AT CFIII, CORROSION FOUND SUPPORT PLATE, FR 85 TO FR 86 UH, LBL 11, HAS BEEN REPLACED IAW ERJ 175 SRM 51-41-01, AND SRM 51-43-01. REV 45.SDR MASA20260512108Web · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE CORROSION FOUND ON UH 1/B SEAT TRACK AT REPAIR ON FR 19, LBL 10. REPAIRED DOUBLER REPAIRED IAW SRM 53-10-10, REPAIR 01P, REPAIR 01.REV 46.SDR MASA20260512107Seat Track · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE CORROSION FOUND ON UH 1/B SEAT TRACK AT REPAIR ON FR 19, LBL 10. REPAIRED DOUBLER REPAIRED IAW SRM 53-10-10, REPAIR 01P, REPAIR 01.REV 46.SDR IPXA2026051269582Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2598 S-5L. ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0035 REV.1 AND EGAT EI NO.F2026A53M-1028 REV.0 AND EGAT WORK SHEET NO.60319AND SRM 53-80-03-2R-2 REV.48. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2026051269605Stringer · crackedSTRINGER CRACKED, FWD SIDE OF BS 2598 S-5L. ACCOMPLISH THE REPAIR IAW UPS EO-97410-REQ0027 REV.1 AND SRM 53-80-03-2R-2 REV.48 AND EGAT WORK SHEET NO.60318 AND EGAT EI F2026A53M-1020 REV.0.SDR IPXA2026051269622Stringer · crackedSTRINGER CRACKED, FWD SIDE OF STA 2598 S-5R. ACCOMPLISH THE REPAIR I.A.W UPS EO-97410-REQ0031 REV.1 AND SRM 53-80-03-2R-2 REV.48 AND EGAT WORK SHEET NO.60317 AND EGAT EI NO.F2026A53M-1026 REV.0.SDR IPXA2026051269635Stringer · crackedMAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 2598 S-7R. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60313 STEP 11(SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0033 REV.1 AND EGAT EI NO.F2SDR IPXA2026051269628Stringer · crackedMAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 2598 S-7L. FABRICATED REPAIR STRINGER AND U-SECTION SPLICE AND L-SECTION SPLICE I.A.W. EGAT WORK SHEET NO.60314 STEP 11(SRM 53-80-03-2R-2 REV.48). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0029 REV.1 AND EGAT EI NO.F2SDR IPXA2026050666083Former · cracked***SUPPLEMENTAL SDR*** FAULT-CRACK-FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 441.6 (REPLACE) INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2241 SH 4 REV. - AND UPS EO NO: SREO-54290-REQ1 REV2.SDR IPXA2026050779287Tee Angle · crackedMCD FR80/82 RT CRACK IN THE TEE PROFILE AT THE CORNER. REMOVED TEE PROFILE CRACKED IAW0 SRM 51-40-21-001. INSTALLED NEW TEE PROFILE IAW SRM 51-40-21-001.SDR AALA202605115834Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y1162. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR IPXA2026050779288Seat Track · damagedMCD FR80/82 Y450 SEAT TRACK BARE METAL. UF-03. INSTALLED NEW SEAT TRACK AT Z200 - MCD FR80/82 Y450, I.A.W. A300-600 SRM 53-10-16-201 (FIG 201) AND SRM 51-40-21-001.SDR AALA202605088056Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL PLATE AT FR 68 AND S23R JUST AFT OF THE AFT GIRTBAR FITTING. REPAIRED SILL PLATE PER SRM 53-41-14-300-001.SDR AALA202605086490Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR DALA2026050602860Skin · crackedFOUND ONE CRACK AT NR 4 HOLE, THE CRACK AT THE SKIN OF FUSELAGE, CRACKED AT 9 O'CLOCK, AS MARKED. REPAIRED IAW PRI:633657-14AD (1572340) (AIRCRAFT GROUNDED)