Boeing 737-33A
Service difficulty reports · 1,809
Newest first. 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' WHERE aircraft_model_key = '73733A' 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' WHERE aircraft_model_key = '73733A' 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 AWXA200200446Cable · frayedPHX - EMERGENCY EVACUATION - DURING INSPECTION FOUND FRAYED R-2 DOOR ESCAPE SLIDE RELEASE CABLE. MAINTENANCE REMOVED AND REPLACED FRAYED RELEASE CABLE AT R2 DOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200442Wire · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H WAS FOUND INOPERATIVE. MAINTENANCE SPLICED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H PER CHAP. 20 WIRING PRACTICES, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200438Switch · stickingSMF - ABORTED TAKEOFF - FLT 0259 - DURING TAKEOFF ROLL AT SMF THE TAKEOFF WARNING HORN SOUNDED, TAKEOFF WAS ABORTED. RESET THE FLAPS, TRIM, AND SPEEDBRAKES; REATTEMPTED TAKEOFF BUT HORN SOUNDED AGAIN. MAINTENANCE CLEANED THROTTLE SWITCHES AT OVERHEAD IN E/E BASDR AWXA200200475Frame · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK CRACKS WERE FOUND ON 3 EACH INTERCOASTAL TO SKIN ATTACH ANGLES AT BS 294.5, BELOW STR 12 R/H, AND BELOW & ABOVE STR 11. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED 3 EACH INTERCOASTAL TO SKIN ATTACH ANGLES AT BS 294.5 SDR AWXA200200468Floorbeam · corrodedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM AT BS 312, BL 0, RBL 8, AND RBL 11. MAINTENANCE CUT OUT DAMAGED AREA OF FLOORBEAM T-CHORD AT BS 312, BL 0, RBL 8, AND RBL 11; FABRICATED REPAIR ANGLES, AND STIFSDR AWXA200200478Web · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND IN THE L/H STRINGER 18A SHEAR BEAM (WEB) AT ATTACHMENT TO STA 727 BULKHEAD. MAINTENANCE REMOVED CRACKED WEB AT BS 727, STR 18A L/H; FABRICATED A NEW WEB AND INSTALLED REPAIR IAW B737-300 SRM 51-10-02, PGSDR AWXA200200477Web · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND IN THE R/H STRINGER 18A SHEAR BEAM (WEB) AT ATTACHMENT TO STA 727 BULKHEAD. MAINTENANCE REMOVED CRACKED WEB AT BS 727, STR 18A R/H; FABRICATED A NEW WEB AND INSTALLED REPAIR IAW B737-300 SRM 51-10-02, PGSDR AWXA200200470Beltframe · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON METAL ANGLE ATTACHED TO FUSELAGE WEB BETWEEN STR 13 & 14 RT, BS 400. MAINTENANCE CUT OUT CRACKED PORTION OF FRAME AT BS 400, BETWEEN STR 13 & 14; FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR IAW B73SDR AWXA200200469Bracket · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON METAL BRACKET ATTACHED TO L/H FUSELAGE SKIN UNDER L1 DOOR BS 332. MAINTENANCE REMOVED DAMAGED GUSSET BRACKET AT BS 332, FABRICATED A NEW BRACKET AND INSTALLED REPAIR IAW B737-300 SRM 51-10-02, P.12, ASDR AWXA200200467Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON 2 EACH STRINGER TIE CLIPS AT BS 380, STR 1 & 2 RT. MAINTENANCE REMOVED STRINGER TIE CLIPS AT BS 380, STR 1 & 2 RT. FABRICATED A NEW STRINGER TIE CLIPS, AND INSTALLED REPAIR PARTS IAW B737-300 SDR AWXA200200466Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 663, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG SDR AWXA200200464Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 LT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 663, STR 10 LT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG SDR AWXA200200463Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 2 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 639, STR 2 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG 12SDR AWXA200200462Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 4 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 639, STR 4 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG 12SDR AWXA200200465Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 767, STR 10 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 767, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG SDR AWXA200200461Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 867, STR 14 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 867, STR 14 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG SDR AWXA200200460Stringer Clip · crackedYVR - MAJOR REPAIR - DURING C-16 INSPECTION A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727D, STR 10 RT. MAINTENANCE REMOVED STRINGER TIE CLIP AT BS 727D, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PGSDR AWXA200200476Door Frame · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON THE FORWARD CARGO DOOR LOWER AFT FRAME AT THE OUTER RADIUS. MAINTENANCE REPAIRED THE FORWARD CARGO DOOR LOWER AFT FRAME AT OUTER RADUIS IAW EO 52-31-04.SDR AWXA200200327Connector · brokenMCN - EEL - DURING C-16 CHECK THE R/H OVERWING HATCH LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R/H OVERWING HATCH LOWER EMERGENCY EXIT LIGHT CONNECTOR IAW BOEING SWPM 20-42-01, PG. 1-6, OPERATIONAL CHECK WAS GOOD IASDR AWXA200200330Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON THE CABIN FLOORBEAM UPPER TEE CHORD AND WEB AT BS 660, LBL 0.07. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 03-5717-02098-KB1.SDR AWXA200200329Web · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON THE CABIN FLOOR BEAM UPPER TEE CHORD AND WEB AT BS 660, LBL 0.07. MAINTENANCE REMOVED DAMAGED AREA OF WEB AT BS 660, LBL 0.07, FABRICATED 2 EACH REPAIR ANGLES, 3 EACH STRAPS, 2 EACH SPLICE PLATES, SDR AUS20020316Beam · corroded(AUS) LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED IN AREA OF ELEVATOR STA 111.SDR AWXA200200302Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER CHORD AT NUT PLATE HOLES OF UPPER AND LOWER SURFACE FROM BS 306 TO BS 328, ON LOWER SURFACE CORROSION WAS FOUND TO BE ON THE INNER CHORD STIFFENER (ANGLE). MAINTENANCE REMOVED CORSDR AWXA200200314Sill · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER CHORD AT THE L1 DOOR THRESHOLD BETWEEN BS 328 AND BS 340 AT THE DOME NUT LOCATION. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE, SPLICE PLATE AND STIFFENER IAW B737-300 SRM 5SDR AWXA200200304Tee Chord · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK 2 CRACKS WERE FOUND ON THE AFT CARGO DOOR LOWER BEAM (TEE CHORD) FORWARD END AT 2ND AND 3RD FASTENER HOLES ON VERTICAL LEG, CRACKS 1/8" AND 1/4" RESPECTIVELY. MAINTENANCE TRIMMED OUT FORWARD END OF TEE CHORD, FABRICATED SDR AWXA200200290Frame · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON R/H INBOARD ANGLE AT THE LOWER FASTENER HOLE ON THE FRAME AT BS 616, WL 199. MAINTENANCE REMOVED CRACKED AREA OF INNER CHORD AND PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED. FABRICATED REPASDR AWXA200200315Skin · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 3/16" CRACK WAS FOUND ON THE EXTERNAL FUSELAGE SKIN AT THE LOWER AFT CUTOUT OF THE L1 DOOR, BS 338, CONFIRMED BY HFEC. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION, CRACK CONTAINED. FABRICATED A -26 REPASDR AWXA200200303Skin · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND EMANATING FROM EXTERNAL SKIN COUNTERSUNK FASTENER HOLE AT THE UPPER AFT CUTOUT OF THE L2 DOOR. MAINTENANCE STOP DRILLED CRACKS ON FIRST AND SECOND LAYER OF SKIN AND PERFORMED HFEC INSPECTION VERIFYING THSDR AWXA200200260Skin · buckledMCN - MAJOR REPAIR - DURING C-16 CHECK THE CENTER KEEL PANEL BETWEEN L/H AND R/H LANDING GEAR WHEEL WELL CUTOUTS ARE BUCKLED IN SEVERAL PLACES AND ALL FASTENERS ARE WORKING. MAINTENANCE REMOVED CENTER KEEL PANEL, FABRICATED A NEW PANEL, AND DOUBLERS FOR BS 690SDR AUS20020187Segment · missing(AUS) ENGINE THRUST REVERSER NR 12 CASCADE SEGMENT MISSING. FORWARD ANDAFT FLANGES CRACKED.SDR AWXA200200192Light · missingLCQ - EEL - C - DURING C-16 CHECK AT LCQ SEAT ROW 3 LT WAS FOUND TO HAVE 2 MISSING SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES. MAINTENANCE INSTALLED 2 EACH EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES ON SEAT ROW 3 LT PER EO 33-50-34, REV A, OPERATIONAL CHSDR AWXA200200152Warning System · malfunctionedPHX - ABORTED TAKEOFF -C- WHEN PREPARING TO TAKEOFF FROM PHX EN ROUTE TO LGB THE CONFIGURATION WARNING HORN SOUNDED. TAKEOFF WAS ABORTED AND AIRCRAFT TAXIED OFF RUNWAY. FLIGHT CREW RESET FLIGHT CONTROLS; AIRCRAFT TAXIED BACK ON RUNWAY AND TOOK OFF WITHOUT INSDR AWAX200200134Battery · dischargedLCQ - EEL - C - DURING C-16 CHECK CABIN EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 13-14 LT, 17 LT, AND 19 RT, WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT BS 973, OPERATIONAL CHECK WAS GOOD IAW T/C A1C33005.SDR AWXA200200173Stringer Clip · crackedLCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 663.75, STR 11L. MAINTENANCE REMOVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2 PG 1-4 & 64.SDR AWXA200200111Skin · dentedLCQ - MAJOR REPAIR - "C" - DURING C-16 CHECK A DENT WAS FOUND IN FUSELAGE SKIN AT FS 365, WL 209 L/H. MAINTENANCE CUTOUT DENTED AREA OF FUSELAGE SKIN AT FS 365, WL 209 L/H; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS FROM CUTOUT; FABRICATED A REPAIR DOUBLESDR AWXA200200105Skin · dentedLCQ - MAJOR REPAIR - "C" - DURING C-16 CHECK A 2" X 10" DENT WAS FOUND AT BS 907 R/H BETWEEN STR 21R AND 22R. MAINTENANCE CUTOUT DENTED AREA OF FUSELAGE SKIN AT BS 907 STR 21R & 22R; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS AT CUTOUT; FABRICATED FILLER ANSDR AWXA200200172Stringer Clip · crackedLCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 639, STR 4R. MAINTENANCE REMOVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2, PG 64 AND 51-40-5 PG 1-8.SDR AWXA200200171Stringer Clip · crackedLCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 639, STR 2R. MAINTENANCE REMOVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2 PG 64 AND 51-40-5 PG 1-8.SDR AWXA200200081Wire · chafedDURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 19 ALL THE WAY AFT ON LT SIDE OF CABIN. MAINTENANCE TROUBLESHOT AND FOUND A CHAFED WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT ROW 19 LT. REMOVED AND REPLACED LIGHT ASSDR AWXA200200077Battery · dischargedWHILE AT GATE GROUND POWER WAS DISCONNECTED FROM AIRCRAFT AND EMERGENCY LIGHTS ILLUMINATED FOR 10 MINUTES. (NOTED BY FLIGHT ATTENDANT) FLIGHT ATTENDANT ATTEMPTED TO TURN LIGHTS OFF BY TURNING ON THE GROUND POWER SERVICE BUS, BUT EMERGENCY LIGHTS WOULD NOT EXTISDR AWXA200200031Rib · damagedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK MAINTENANCE DISCOVERD A HOLE DRILLED THROUGH INBOARD L/H MIDFLAP LOWER SURFACE INTO THE FLAP TRACK SUPPORT RIB AT APPROXIMATELY WBL 116. DAMAGE APPEARED TO BE FROM A DRILLED OUT GREASE FITTING. MAINTENANCE REMOVED ISDR AWXA200200045Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 1/4" CRACK WAS FOUND AT 12 OCLOCK POSITION AT HILOC FASTENER HOLE LOWER AFT CORNER OF L1 DOOR CUTOUT BS 340. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRSDR AWXA200200030Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 1.3" CRACK WAS FOUND ON SKIN AT CAPTAINS WINDSHIELD ON THE AFT POST UPPER CORNER BS 200, STR 8L. MAINTENANCE CUTOUT AND REMOVED DAMAGED AREA OF SKIN AT AFT POST UPPER CORNER AND FOUND GUSSET CRACKED APPROXIMATELY 1"SDR AWXA200200028Web · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 2 CRACKS WERE FOUND ON WEB BELOW SEAT TRACKS AT BS 709-710, LBL 24. MAINTENANCE REMOVED DAMAGED AREA OF WEB, FABRICATED REINFORCEMENT DOUBLER AND NEW WEB AND INSTALLED REPAIRS IAW AWA ER 03-5715-02011-ES3.SDR AWXA200200027Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A CRACK WAS FOUND ON THE F/O'S SLIDING WINDOW FWD POST LOWER CORNER BS 210. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO CONFIRM CRACK WAS CONTAINED. FABRICATED DOUBLER AND INSTALLED REPAIR AT BS SDR AWXA200200026Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A CRACK WAS FOUND ON THE F/O'S SLIDING WINDOW FWD POST UPPER CORNER BS 220. MAINTENANCE CUTOUT THE DAMAGED AREA OF CRACKED SKIN AT THE F/O'S SLIDING WINDOW AND PERFORMED HFEC INSPECTION TO CONFIRM CRACK WAS CONTAINESDR AWXA200200025Skin · crackedMCN - MAJOR REPAIR - C - DURING C-17 CHECK L1 DOOR LOWER FUSELAGE HINGE CUTOUT WAS FOUND CRACKED APPROXIMATELY .25 INCH FORWARD BS 305. MAINTENANCE REMOVED DAMAGED AREA OF CUTOUT SKIN AT DOOR HINGE BS 305, FABRICATED A REPAIR PLATE AND INSTALLED REPAIR IAW 53SDR AWXA200200046Tee Chord · corrodedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR BEAM UPPER FLANGE AT BS 947, LBL 10 TO RBL 10. MAINTENANCE REMOVED 6 EACH FLOOR SUPPORT, 1 EACH INTERCOASTAL BRACKET ASSEMBLY, AND TEE CHORD FROM LBL 32 TO RBL 33. FABRICATED AND INSTALLSDR AWXA200200029Floorbeam · corrodedMCN - MAJOR REPAIR - C - DURING C-17 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER FLANGE AT BS 986, RBL 3 TO LBL 18. REMOVED DAMAGED AREA OF FLOORBEAM UPPER T-CHORD AT BS 986, RBL 3 TO LBL 50. FABRICATED 2 SPLICE STRAPS AND REPAIR ANGLES AND NEW UPPER T-CHORSDR AWXA200200059Doubler · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A 1/4" CRACK WAS FOUND ON DOUBLER FOR PYLON ACCESS PANEL 5727L AT NAC 216. MAINTENANCE PERFORMED HFEC INSPECTION TO IDENTIFY END OF CRACK THEN STOP DRILLED CRACK; FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW A
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