Boeing 737-300
Service difficulty reports · 184
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 = '737300' 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 = '737300' 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 DU4R0507172Skin · dentedDENT IN LT SIDE FUSELAGE SKIN IN AREA OF S-20L BS 465.SDR AWXA200500737Wire · brokenFOUND EMERGENCY EXIT LIGHTS AT ROWS 11 THROUGH ROW 15 ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SEATS OPERATIONAL CHECKS GOOD.SDR 20050622ASkin · dentedDENT IN THE LT FUSELAGE SKIN IN AREA OF S20L AT BS 465.SDR 78Skin · dentedDENTS AND GOUGES STA 770 - 827 STR 26 - 27 RT BELOW AFT PIT DOOR.SDR F3L2005F00000Engine · leakingAPPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR 2 ENG ALSO GOING TO ZERO. NR 1 ENG OIL PRESS THEN DROPPED TO ZERO, NR 2 ENG OIL PRESS DROPPED TO MSDR AWXA200500051Hinge Pin · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER OUTER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED RT HORIZONTAL STABILIZER OUTER HINGE PIN IAW AWA T/C E6C55101.SDR AWXA200500050Hinge Pin · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER INNER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER INNER HINGE PIN IAW AWA T/C E6C55102.SDR AWXA200500049Hinge Pin · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER OUTER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER OUTER HINGE PIN IAW AWA T/C E6C55102.SDR AWXA200500048Skin · chafedMCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED IN 3 PLACES BELOW DORSAL FIN AT BS 860, STR 1. MAINTENANCE TRIMMED DAMAGED AREAS ON FUSELAGE SKIN AT BS 860, STR 1; FABRICATED -1, -8, -9, AND -10 FILLERS, AND 3 EACH WEAR STRIPS AND REPAISDR AWXA200401245Tab · debondedDURING C-15 CHECK AN AREA OF DISBOND WAS FOUND ON RT AILERON TAB AT OUTBOARD AFT CORNER BETWEEN WBL 479.75 AND WBL 480 RT. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-06, FIG 13.SDR AWXA200401188Wire · brokenDURING TAXI OUT, THE "APU DET INOP" ANNUNCIATOR LIGHT ILLUMINATED INTERMITTENTLY, SWITCHED APU TO OFF AND APPROXIMATELY 2 MINUTES LATER RECEIVED AN APU FIRE INDICATION. PULLED APU FIRE HANDLE AND DISCHARGED THE APU FIRE BOTTLE. MAINTENANCE TROUBLESHOT AND FOSDR QEM2004F00000Turbine Blades · crackedTHE HPT DISC WAS FOUND WITH 5 CRACKED FIR TREES. MFG WAS INFORMED AND HAVE REQUESTED THE HPT DISC AND HPT BLADES BE RETURNED FOR INVESTIGATION. HPT AND LPT NOZZLE WERE INSPECTED AND NO DEFECTS THAT COULD HAVE AFFECTED THE DISC NOTED. FUEL NOZZLES FLOW, WERESDR 2004FA0000411Fuse · brokenINSIDE THE HYDRAULIC FUSE P/N 2-8041-1 IS A MATCHED SET OF PARTS P/N 7-2500-6 SEPARATED BY A FORMED WASHER. UPON DISASSEMBLY OF THESE PART THE FORMED WASHER HAS BEEN FOUND TO BE BROKEN. THESE UNITS ARE SUPPLIED TO US FROM AN AIRLINE TO INSPECT, MANY OF THESSDR F3LA200400057Wire · shortedWHILE PERFORMING OPERATIONAL TEST OF LT OTBD LANDING LIGHT, FOUND SHORT IN LT WING WIRE BUNDLE, AFT SPAR INBD OF NR 1 ENGINE PYLON, AFT. RESPLICED W802-001-16 WIRE SECTION AT RSS 283 AND RSS 230 ON LT WING T/E PER WPM 20-10-13 AND 20-30-12. PERFORMED OPERATISDR F3LA200400033Spindle · corrodedINSPECTION REPORTED RT OTBD FLAP CARRIAGE SPINDLE SHOWED CRACK INDICATION ON ULTRASOUND INSPECTION (REF. AD 2003-24-08, FRONTIER WORK CARD 9-5702). REMOVED SPINDLE AND FOUND NO CRACK, BUT FOUND HEAVY CORROSION AT SADDLE. REPLACED CARRIAGE SPINDLE.SDR COOSDR030032Attach Fitting · corrodedLT HORIZONTAL STABILIZER FRONT SPAR, LOWER ATTACH LUG SURFACE CORRODED.SDR COOSDR030029Frame · crackedBS 178, RBL 28 AND LBL 28, SIDE CHORDS CRACKED.SDR 2004FA0000006Spar · crackedCRACKED AT OB AFT FLAP TRACK LOWER ATTACH HOLES.SDR AWXA200300548Light · inoperativePHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300442Light · inoperativeLAS - EEL - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 20 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 20 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300093Skin · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 3/4 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 867, BETWEEN STR 18-19 RT. MAINTENANCE CUTOUT DAMAGED SECTION OF FUSELAGE SKIN AT BS 867, BETWEEN STR 18-19 RT AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKSDR AWXA200300092Stiffener · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 1 INCH CRACK WAS FOUND ON LT WING INBOARD CANOE FITTING WS 191. MAINTENANCE CUTOUT CRACKED AREA OF LT WING INBOARD CANOE FITTING; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02,SDR AWXA200300091Reveal · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 1/4 INCH CRACK WAS FOUND ON R-1 DOOR FORWARD UPPER REVEAL BS 305, STR 16 R/H. MAINTENANCE REMOVED R-1 DOOR FORWARD UPPER REVEAL; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. SDR AWXA200300080Sill · crackedDURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND CABIN FLOORBOARD SILL ANGLE BS 639, LBL 56. MAINTENANCE FABRICATED REPAIR PLATES FOR CRACKED CABIN FLOORBOARD SILL ANGLE BS 639, LBL 56; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, PG. 1-3, 6-7, FIG. 1.SDR AWXA200300102Frame · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 1 1/4 INCH CRACK WAS FOUND ON LOWER INBOARD ANGLE AT BS 616 RT, RBL 60. MAINTENANCE CUTOUT CRACK ON ANGLE AT BS 616 RT, RBL 60; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENING ANSDR AWXA200300064Bulkhead · crackedDURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, RBL 4.7, WL 198.5, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALSDR AWXA200300063Web · crackedDURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, LBL 4.7, WL 201, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLESDR AWXA200300090Doubler · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 5/8 INCHES CRACKS WERE FOUND ON NR 1 PYLON SKIN AND DOUBLER AT THE AFT LOWER CORNER OF PANEL 5724L, NAC STA 254. MAINTENANCE REMOVED EXISTING EXTERNAL DOUBLER AND PERFORMED HFEC INSPECTION VERIFYING CRACK LENGTH; SSDR AWXA200300079Bulkhead · crackedDURING C-14 CHECK A 1 INCH CRACK WAS FOUND BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5. MAINTENANCE REMOVED STIFFENER AND "L" ANGLE TO ACCESS DAMAGE; CUTOUT CRACKED AREA OF BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5; PERFORMED A HFEC INSPECTION OF CUOUT TO VERIFY NO CRSDR AWXA200300060Web · corrodedDURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB IN VICINITY OF LT AFT LAVATORY POTABLE WATER AND SINK DRAIN LINES, BS 996, LBL 55, WL 208. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS PER B737-300 SRM 53-6SDR AWXA200300103Reveal · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON THE AFT CARGO COMPARTMENT DOOR OPENING AFT TORQUE BOX WEB COVER. MAINTENANCE REMOVED CRACKED AFT CARGO COMPARTMENT DOOR OPENING AFT TORQUE BOX WEB; FABRICATED A NEW REPLACEMENT TORQUE BOX WEBSDR AWXA200300068Skin · delaminatedDURING C-14 CHECK THE NR 2 SLAT INBOARD AND OUTBOARD WEDGES WERE FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 SLAT IAW BMM 27-81-21, PG. 401-419; OPERATIONAL TEST AND ADJUSTMENT COMPLIED WITH BMM 27-81-00, PG. 513-530.SDR AWXA200300065Structure · delaminatedDURING C-14 CHECK THE NR 5 SLAT OUTBOARD WEDGE WAS FOUND DELAMINATED. MAINTENANCE REPAIRED DAMAGE TO HONEYCOMB OF NR 5 SLAT OUTBOARD WEDGE IAW B737-300 SRM 51-70-10, REP. 22, FIG. 31, PG. 88F-88H.SDR AWXA200300066Skin · delaminatedDURING C-14 CHECK THE LT INBOARD FOREFLAP UPPER OUTBOARD END WAS FOUND DELAMINATED. MAINTENANCE REPAIRED DAMAGE TO HONEYCOMB OF LT INBOARD FOREFLAP UPPER OUTBOARD END IAW B737-300 SRM 51-70-10, REP. 9, FIG. 18, PG. 73-77.SDR AWXA200300061Skin · crackedDURING C-14 CHECK A 7/8 INCH CRACK WAS FOUND ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE. MAINTENANCE STOP DRILLED CRACK ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE; PERFORMED HFEC INSPESDR AWXA200201183Wire · brokenDURING INSPECTION A BROKEN WIRE WAS FOUND AT THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT, OPERATIONAL CHECK GOOD.SDR AWXA200201065Indicator · malfunctionedFLT 0491 - ON TAKEOFF AT PHX EN ROUTE FOR DEN AT 80 KTS THE FIRST OFFICERS AIRSPEED INDICATOR WAS INDICATING ZERO, ABORTED TAKEOFF AT 90 KTS. AFTER TURNING OFF RUNWAY FIRST OFFICERS AIRSPEED FLAG CAME INTO VIEW. MAINTENANCE PERFORMED POWER UP TEST OF AIR SPEEDSDR F3LA200200370Intercostal · corrodedDURING C 2 CHECK, CORROSION WAS FOUND ON THE AFT CARGO PIT INTERCOSTAL SURFACE AND AROUND NUT PLATES BETWEEN STA 767 TO STA 794 AND RBL 21. NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02 AND SOPM 20-41-02.SDR F3LA200200363Floor Support · corrodedDURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND CORRODED AT STA 727D AT RBL 13.8 THE CORRODED SECTION OF TRACK WAS REPLACED BETWEEN STA 727 AND STA 767 IAW SRM 51-40-02SDR F3LA200200372Floor Support · corrodedDURING C 2 CHECK, CORROSION WAS FOUND OF THE AFT CARGO COMPARTMENT FLOOR TRACK AT STA 791, LBL 11.5. REMOVED AND REPLACED THE FLOOR TRACK IAW SRM 51-10-02 AND SRM 51-40-02, BETWEEN STA 727 AND STA 947 AT LBL 11.5.SDR F3LA200200369Floor Support · corrodedDURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, RBL 2. FLOOR TRACK WAS REPLACED BETWEEN STA 727 AND STA 947, RBL 2.5 IAW SRM 51-40-05 AND SRM 51-40-02.SDR F3LA200200368Skin · puncturedDURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IAW SRM 51-70-10 AND REINSTALLED IAW BOEING 737 MM 27-51-07.SDR F3LA200200366Floor Support · corrodedDURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, LBL 3.0 FLOOR TRACK REPLACED BETWEEN STA 791 TO STA 860. LBL 3.0, IAW SRM 51-40-02SDR F3LA200200371Floor Panel · corrodedDURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS FOUND CORRODED BETWEEN STA 787 AND STA 807. AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS REMOVED AND REPLACED BETWEEN STA 727 AND 947, LBL 20 IAW SRM 53-60-53 AND SRM 51-40-02.SDR F3LA200200365Tail Cone · dentedDURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-300 MM 51-21-99 AND SRM 51-70-06.SDR F3LA200200367Skin · bird strikeDURING C 2 CHECK, A BIRD STRIKE WAS FOUND ON THE RT LEADING EDGE OF THE STABILIZER BETWEEN STA 184.7 AND STA 189.2. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-10-01.SDR SWA2002F00000Spar · crackedCRACK WAS FOUND DURING D CHECK VISUAL INSPECTION IN THE BACK SHOP. DISCOVERED THE MAIN SPAR CRACKED IN THE LOWER CHORD/WEB RADIUS COMMON TO THE OUTBOARD AFT FLAP TRACK ATTACH POINT. THE CIRCUMSTANCES UNDER WHICH IT OCCURED IS UNKNOWN. COULD BE FATIGUE OR ANSDR F3LA200200347Shear Tie · corrodedCORROSION FOUND ON FRAME AND SHEAR TIE FORWARD AND AFT SIDES AT BS 500D, LBL 9 TO 22SDR AWXA200200588Flashlight · inoperativeFLIGHT CREW REPORTED THE FOWARD BULKHEAD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FOWARD BULKHEAD EMERGENCY FLASHLIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR RIVA020308MDoor Frame · crackedMQY - NR 3 CARGO DOOR STATION1090 FRAME HAS CRACK BETWEEN STRINGERS 26R AND 27R. ROUTED OUT CRACK. FABRICATED REPAIR ANGLES AND FILLERS. TREATED AND PRIMED AND INSTALLED REPAIR ANGLES AND FILLERS PER BOEING REPAIR SKETCH TEK MQY 02-0001F WITH 8110-3, DATED
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