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.
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 SWAA2026092862752Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE, BS 986.5, LBL 43, WL 208. REPAIRED THE FLOORBEAM FWD UPPER FLANGE IAW SRM 51-40-02-0G-0 AND SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026092835493Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 947+2 LBL51. WL208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A5650, REV A.SDR SWAA2026092838693Support · corrodedCORROSION ON LH SHEAR WEB ZEE SUPPORT ANGLE BS986.5+6 LBL33, WL208. REMOVED AND REPLACED ON LH SHEAR WEB ZEE SUPPORT AT BS1000 BS1016 LBL 33 IAW B737-800 SRM 51-40-02-0G-0 AND DWG:147A5700 ID:0121 REV:A VERIFIED CORRECTIVE ACTION STEP 1.SDR CALA2026092819858Skin · crackedLH HORIZONTAL STAB, LOWER SKIN, ONE CRACK INDICATION AT HSS 157.10, 9.5 INCHES IN FRONT OF REAR SPAR. PERFORMED REPAIR ON LH HORIZONTAL STAB, LOWER SKIN AT HSS 157.10 AND 9.5" IN FRONT OF REAR SPAR IAW SRM 55-10-01-2R-11, 51-40-02-0G-0, 51-40-05-0G-0, & 51-40SDR SWAA2026092491559Support Angle · crackedCRACKED SUPPORT ANGLE, FWD FACE, BS 695, LBL 1, WL 208.1. REPLACED THE SUPPORT ANGLE LOCATED FWD FACE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 273A9111, SHEET 9, REV -.SDR SWAA2026092429167Seat Track · corrodedCORRODED SEAT TRACK, BOTTOM SURFACE, BS 727F + 13 INCHES, RBL 24.75, WL 208.1. REMOVED THE DAMAGE & EVALUATED REWORK ON SEAT TRACK IAW SRM 53-00-52-1A-1, STEP 4.A (2)(A), FIGURE 103, DETAIL A.SDR SWAA2026092411677Floor Panel · delaminatedDELAMINATION ON TOP SKIN OF FLOOR PANEL 231KF. REPAIRED THE FLOOR PANEL 231KF IAW SRM 53-00-50-2R-7, REPAIR 7.SDR SWAA2026092472284Crossbeam · crackedCRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 - LBL 24.75, WL 208.1. REPLACED THE BRAKE PANEL IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV- .SDR SWAA2026092407246Seat Track · corrodedCORROSION SEAT TRACK LOCATED BTW BS 540 - 727B, WL 208, LBL 45.5, CROWN AREA BOTTOM SURFACE (4 E/A). REMOVED DAMAGE AND EVALUATED REWORK AREA IAW SRM 53-00-52-1A-1 STEP 4.A (2)(A), FIGURE 103, DETAIL A.SDR SWAA2026092476359Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE FLOORBEAM, IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026092455644Seat Track · corrodedCORRODED SEAT TRACK, BOTTOM SURFACE, BS 727 + 13 INCHES, RBL 24.75, WL 208.1. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SURFACE LOCATED BS 727 + 13 INCHES, RBL 24.75, WL 208.1 IAW SRM 53-00-52-1A-1, STEP 4.A (2)(A), FIGURE 103, DETAIL A.SDR SWAA2026092415985Seat Track · corrodedCORRODED SEAT TRACK BTW BS 727B - 887, WL 208, RBL45.5 CROWN AREA BOTTOM SURFACE, (5 EA). REMOVED DAMAGE AND EVALUATED SEAT TRACK LOCATED BTW BS 727B - 887, WL 208, RBL45.5 , FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, PARAGRAPH 4.A.(2(A), FIGURE 103, DETAILSDR SWAA2026092416069Seat Track · corrodedCORROSION ON SEAT TRACK BOTTOM SURFACE LOCATED BS 500F PLUS 10 INCHES RBL 24.75 WL 208.1 AT PASSENGER CABIN. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SURFACE LOCATED BS 500F PLUS 10 INCHES RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM 53-00-52-1A-1 STESDR SWAA2026092352715Bullnose · crackedLEFT WING, NR 2 KRUEGER FLAP, BULL NOSE CRACKED AT CENTER RIB. REMOVED AND REPLACED THE LT WING MID BULL NOSE KRUEGER FLAP NR 2 IAW CMM 57-56-44-NG.SDR SWAA2026092374461Bracket · crackedCRACKED BRACKET ANGLE BTW BS 188 - 203, RBL 3, LOWER NOSE COMPARTMENT. REPLACED THE BRACKET ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 141A9194, SHEET 4, REV D.SDR SIMA20260820004Shear Tie · corrodedSHEAR TIE AT FR 78 BETWEEN STGR 29L-29R IS CORRODED. R & R SHEAR TIE AT FR 78 BTW STGR 29L-29R IAW SRM 51-40-08.SDR SIMA20260820003Shear Tie · corrodedSHEAR TIE AT FR75 BETWEEN STGR 28R-29R IS CORRODED. R & R SHEAR TIE AT FR 75 BTW STGR 28R-29R IAW ERJ 170 SRM 51-40-08.SDR SIMA20260820005Shear Tie · corrodedSSI: 53-23-003 SHEAR CLIP AT FR75 BETWEEN STGR 27L-28L IS CORRODED. (LEVEL 2 CORROSION) RAR SHEAR CLIP AT FR 75 BTW STGR 27L-28L IAW ERJ 170 SRM 51-40-08.SDR SIMA20260820002Support · corrodedSSI: 53-23-003 SHEAR CLIP AT FR77 BETWEEN STGR 29L-29R IS CORRODED. (LEVEL 2 CORROSION) RAR SHEAR CLIP AT FR 77 BTW STGR 29L-29R IAW ERJ 170 SRM 51-40-08SDR SWAA2026092190056Fastener · pulledRIGHT WING LEADING EDGE, JUST INBD OF NR 2 ENGINE HAD THREE FASTENERS PULLING THROUGH SKIN. REMOVED THE THREE PULLING FASTENERS AND OVERSIZED HOLES TO .214 IAW SRM 57-41-01-2R-7. ACCOMPLISHED HFEC HOLE PROBE AND COUNTERSINK INSPECTION IAW NDT PART 6 51-00-00,SDR SWAA2026092143268Shield · corrodedCORROSION SHIELD WEB LOCATED BS 492.5 TO BS500A RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BS 492.5 TO BS500A RBL21 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG:143A0080 SHEET:33 REV:- RII.SDR SWAA2026092143257Cowling · pulledNR 2 ENGINE INLET COWLING OUTER LIP SKIN FASTENERS AT 2 OCLOCK AND 10 OCLOCK ARE PULLED THROUGH SKIN . REMOVED AND REPLACED #2 ENGINE INLET FAN COWL IAW AMM 71-11-01 AND COMPLIED WITH ACOUSTIC PANEL BLOCKAGE SURVEY IAW SRM 54-00-01. REMOVED AND REPLACED #2 ENSDR SWAA2026092148806Support · corrodedCORRODED SUPPORT ZEE, BTWN BS 500 - 500A, LBL 21, WL 156 IN THE FWD CARGO BAY. REPAIRED THE SUPPORT ZEE BTWN BS 500 - 500D IAW SRM-53-00-53-2R-5, REPAIR 5, SRM 51-40-02, & DWG 143A7500, SHEET 58, REV -.SDR SWAA2026092148509Frame · crackedCRACKED FRAME, BS 259.5 BTWN STRINGERS 8 - 9R. REPAIRED THE FRAME BS 259.5, STR 6 - 11R IAW EA 26-153-02323-WIP1, AND EA 26-153-02323.SDR SWAA2026092192325Rub Strip · gougedGOUGED RUB STRIP ON THE BODY FAIRING LOWER ANGLE, BS 540 + 10 INCHES AND RBL 41. REPAIRED THE RUB STRIP IAW SRM 57-10-13-2R-3.SDR SWIA2026082077211Seat Track · corrodedRIGHT SEAT TRACK AT FRAME 1625 AND Y 1075 HAS MULTIPLE AREAS OF CORROSION REMOVED AND REPLACED RT SEAT TRACK AT FRAME 16 25 AND Y 1075 PER SRM 51-40-08.SDR SWAA2026091682161Seat Track · corrodedCORROSION SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND WL 208 ON TOP SURFACE AT LBL 45.5 AT PASSENGER CABIN REPAIRED SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND WL 208 ON TOP SURFACE AT LBL 45.5 AT PASSENGER CABIN IAW EA 26-153-02367 AND EA 26-153-02367-WIP1.SDR IPXA2026091681129Panel · wornWORN - HOLE, RT WING NR 8 SLAT INBD SIDE LWR CLOSURE DOOR. (REPAIR). IAW SRM 57-43-01-2R-3 REFER TO SRM 51-70-08-0G-0 REV. 132 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE SIZE AND LOCATION ( L : 0.3", W : 0.2"SDR MASA202609142039Gusset · corrodedDURING HEAVY CHECK OF AFT WET AREA, CORRODED FLOOR SUPPORT GUSSET AT FR 90 UH, LBL 18, REPLACED WITH NEW IAW ERJ 175 SRM 51-41-02. NRC # 4502706-2000-0278. REV 45.SDR MASA202609142038Gusset · corrodedDURING HEAVY CHECK OF AFT WET AREA, CORROSSION ON FLOOR SUPPORT GUSSET, FR90, RBL 24 REMOVED AND REPLACED IAW ERJ 15 SRM 51-41-02 NRC# 4502706-2000-027, REV 45.SDR MASA202609142037Floor Support · corrodedDURING HEAVY CHECK OF AFT WET AREA, CORROSION ON FLOOR SUPPORT ANGLE, REMOVED AND REPLACED IAW SRM 51-41-01, SRM 51-42-01 AND SRM 51-43-01. NRC 4502706-2000-0276, REV 45, REV 46SDR MASA202609142036Floor Support · corrodedDURING HEAVY CHECK OF AFT WET AREA, CORRODED FLOOR SUPPORT ANGLE HAS BEEN REPLACED WITH NEW \AW SRM 51-42-01. NRC # 4502706-2000-02751REV 45.SDR MASA202609142031Floor Support · corrodedDURING HEAVY CHECK OF AFT AREA, CORRODED FLOOR SUPPORT, CF ILL FR 86 RT, RBL 28, REPLACED WITH NEW IAW SRM 51-41-01.SDR SWAA2026091433998Frame · crackedCRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED TRIM OUT OF FRAME UPPER ANGLE IAW EA M-22-153-01244, REV B.SDR MASA202609142029Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII, FLOOR STRUCTURE, CFIII FR 84, RBL 46 FLOOR SUPPORT. REMOVED AND REPLACED IAW SRM 51-41-02.SDR AALA202609094676Support Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL SUPPORT BRACKET AT FS 312 AT RBL 12 WAS FOUND CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW AARD 51-00-05-1 AND BOEING DWG 141A5710.SDR SWIA2026082077109Flap Track · wornRH WING FLAP TRACK 2A OUTBOARD HAS WIDTH REDUCTION WEAR OF 1.13MM MAX ALONG ENTIRE LENGTH. REMOVED AND REPLACED RH WING FLAP TRACK 2A OUTBOARD.REF. EMB AMM. 57-54-25.ASSET. TC2-50254 DUE. 9-24-26SDR REXA2026090801780Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN FS310 AND FS319. ON FURTHER INVESTIGATION FOUND TO BE HEAVILY CORRODED TO THE POINT WHERE THERE IS CHUNKS OF MATERIAL MISSING AT BS 319. REMOVED & REPLACED THE FLOOR SUPPORT BETWEEN FS280 - FS319 IAW SRM 51- 42-21-001-0SDR SWAA2026090796097Stiffener · crackedLEFT HORIZONTAL STAB RIB NR 4, 4TH STIFFENER FWD CRACKED. STIFFENER REPAIRED IAW SRM 55-10-09-2R-4.SDR SWAA2026090712921Stiffener · crackedLEFT HORIZONTAL STAB RIB NR 4 3RD STIFFENER FROM THE FWD, CRACKED. REPAIRED THE RIB IAW SRM 55-10-09-2R-4.SDR R61A2026090700253Skin · crackedDURING HEAVY CHECK L/H WING L/E SKIN AT SLAT #2 OB SLAT TRACK CUTOUT FOUND CRACKED. REPAIRED CRACK IAW EMB 170/175 SRM 57-49-01SDR R61A2026090700252Bracket · crackedDURING HEAVY CHECK FWD FUSELAGE INTERNAL LOWER STRUCTURE, SUPPORT, WATER SYSTEM AT FR 15 BETWEEN STGR 22L-23L FOUND CRACKED. REMOVED AND REPLACED SUPPORT IAW EMB 170/175 SRM 51-41-01SDR R61A2026090700250Shear Tie · crackedDURING HEAVY CHECK FWD FUSELAGE SHEAR CLIP AT FR 22 BETWEEN STGR 23R-22R FOUND WITH CORROSION. REMOVED AND REPLACED SHEAR CLIP IAW EBM 170/175 SRM 51-41-01 AND 51-41-02SDR U5QA202608200177Pump · leakingLEFT HYD AMBER HIGH TEMP CAS FOLLOWED BY LT SOV CLOSED. LOSS OF ALL LT HYD (B3-303036 CODE), MANUAL GEAR EXTENSION DUE TO LOSS OF LT SIDE HYD. INSTALLED A REPAIRED LT ED HYD PUMP. FLUSHED THE LT HYD SYS. INSTALLED A NEW LT OTBD CASE DRAIN FILTER. A NEW LSDR AALA202609045612Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF INTERCOSTAL, FOUND STRINGER WITH INTERGRANULAR CORROSION AT S20L, BETWEEN FS 787 AND 807. REPAIRED STRINGER IAW SRM 53-00-03-2R-1 AND EA 377509.SDR REXA2026090401774Bushing · abnormalRIGHT AILERON CENTER HINGE FITTING BUSHING LUG MARKED C FOUND TO BE O/S UPON BUSHING REMOVAL. REPAIRED RT AILERON SIDE LUG LABELED C IAW STEP F.(1) - F.(4) OF GREO 670-57-61-237 REV --. LPI PERFORMED ON REAMED BORE IAW STEP F.(5) OF GREO 670-57-61-237 REV --.SDR IPXA2026090377741Skin · debondedDEBONDED SKIN, INBD EDGE UPPER FACE OF LT WING T/E OTBD FLAP T/E SKIN , WBL 355. IAW SREO-70175-REQ001, REV 1, REMOVED THE CRACK AND CLEANED. MEASURE THE DAMAGE AREA L : 0.5", W : 0.01", 7" FROM TRAILING EDGE, AT INBD EDGE. BONDED THE REPAIR PLIES WITH RESDR 2026FA0000676Motor · burned outCAPTAIN WAS PILOT FLYING. N301PT DEPARTED ANC FOR IGG. WHILE IN THE CLIMB AT ABOUT 7,000FT, SMOKE COULD BE SMELLED INSIDE THE AIRCRAFT. PILOT LEVELED OFF AND NOTIFIED ANC OF THE SMELL AND REQUESTED TO RETURN TO ANC. AT THIS POINT THERE WAS NO SMOKE. AIRCRAFT WSDR CALA2026090119125Angle · crackedANGLE RT AFT CRACKED AT LWR INBD RIVET LINE. REPAIRED IAW EA 5331-01718, OP 08.SDR CALA2026090119124Structure · corrodedMAIN CABIN R1 DOOR CUTOUT CORRODED AT FWD GIRT BAR FITTING AREA. REMOVED THE CORROSION & FOUND TO BE WITHIN LIMITS IAW SRM 53-11-14-283-005,