Boeing 737-375
Service difficulty reports · 174
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 = '737375' 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 = '737375' 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 K11A20200105309Cusp Web · crackedCUSP WEB CRACKED AFT OF BS 616 LBL 64 & LBL 70SDR K11A2020010308Cusp Web · crackedCUSP WEB CRACKED FWD OF BS 639 LBL 70SDR K11A2020010307Floorbeam · crackedBS 639 LBL 45.5 WL 204 FLOORBEAM WEB CRACKED @ 1 LOWER FASTENERSDR K11A2020010306Floorbeam · crackedBS 639 RBL 45.5 WL 204 FLLORBEAM WEB CRACKED @ 2 LOWER FASTER HOLESSDR K11A2020010305Spar · gougedR/H I/B AFT UPPER SIDE OF FRONT SPAR CHORD LUG HAS GOUGED AREAS AROUND WASHERSDR K11A2020010304Spar · gougedL/H I/B UPPER SIDE OF FRONT SPAR CHORD LUG HAS GUAGED AREAS AROUND WASHER (HORIZONTAL STAB)SDR K11A2020010303Frame · crackedR/H FRAME @ STA 500B HAS A CRACK IN THE INBD SIDE OF POWER CABLE HOLE BETWEEN S-20 & S-21SDR K11A2020010302Skin · corrodedLEFT WING UPPER SURFACE WBL 72 APPROX S-19C HAS CORROSIONSDR K11A2020010333201Skin · crackedFWD GALLEY SERVICE DOOR FWD UPPER CORNER HAS CRACKS COMING FROM FASTENER HOLE WITH ENDS OF CRACKS MARKEDSDR AWXA200601003Structure · delaminatedPHX - MAJOR REPAIR - LOG 7260237 - DURING POST FLIGHT INSPECTION CREW REPORTED FINDING THE RT TRAILING EDGE FLAP DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD TRAILING EDGE AFT FLAP IAW AMERICA WEST AIRLINES TASKCARD R3M27007. FLAP WAS REPAIRESDR AWXA200600530Switch · faultyPHX - AIR TURN BACK - FLT 0551 - CREW REPORTED THAT DURING CLIMB-OUT THE RT PACK TRIPPED OFF TWICE, RESET PER QRH AND PACK FAILED AGAIN. THE LT PACK WAS CURRENTLY DEFERRED SO CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED TROUBLSDR AWXA200600425Window Post · crackedREPORTED THAT THE CAPTAIN'S WINDOW POST WAS CRACKED. MAINTENANCE CUT OUT DAMAGED AREA OF GUSSET IAW SRM 53-10-01-2R. AFTER REMOVAL OF INITIAL DAMAGE, FOUND INNER SKIN TO BE CRACKED APPROX. .400 IN. CUTOUT DAMAGED AREA OF INNER SKIN. DRILLED AND LOCATED NEWSDR GAIA06001Slide · deployedR1 ESCAPE SLIDE ACCIDENTALLY DEPLOYED BY MAINTENANCE. DIFFERED R1 DOOR SLIDE IAW MEL. UPON ARRIVAL AT THE NEXT STATION, REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. OPERATIONAL CHECK OK. (DMI CLEARED). AIRCRAFT RETURNED TO SERVICE. (K)SDR AWXA200600043Line · brokenYVR - EMERGENCY EQUIPMENT, CREW REPORTED THAT THE AIR LINE TO THE F/O'S O2 MASK BROKE OFF. CREW O2 VALVE WAS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE F/O'S O2 MASK IAW AMERICA WEST AIRLINES TASK CARD R1B35001.SDR AWXA200501569Valve · failedCREW REPORTED THAT THE NR 2 ENGINE COWL ICE VALVE WOULD NOT OPEN ONCE AIRBORNE BUT WORKED ON GROUND IN SEA. CREW CYCLED SWITCH SEVERAL TIMES PER MX CONTROL AND WAS NO HELP. ICING CONDITIONS WERE EXPECTED EN ROUTE. CREW RETURNED TO SEA AND LANDED WITHOUT FURSDR AWXA200501222Handle · malfunctionedAFTER T/O AND UPON RETRACTION OF GEAR, GEAR HANDLE WOULD NOT PHYSICALLY MOVE PAST CENTER FOR GEAR RETRACTION. A/C RETURNED TO STL AND LANDED W/O FURTHER INCIDENT. MX TROUBLESHOT AND REPLACED THE LOCKING SOLENOID IN THE GEAR HANDLE. ACFT THEN WENT ON MX FERRSDR AWXA200500901Rib · crackedPHX - DISCOVERED SERVERAL CRACKS ON THE LT LEADING EDGE BETWEEN STATION 208-219. REMOVED CRACKS ON LT LEADING EDGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5741-05214-RC2. FABRICATED FILLER IAW AWA ER 03-5741-05214-RC2. INSTALLED FABRICATED REPAIR PASDR AWXA200500442Battery Pack · dischargedMCN - EEL - DURING C-05 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE LT FORWARD ENTRYWAY EMERGENCY LIGHT BATTERY PACK WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD ENTRYWAY EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOSDR AWXA200500439Clip · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON UPPER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED UPPER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT; ORDERED & RECEIVED A NEW REPLACEMENT CLIP;SDR AWXA200500438Clip · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER ATTACH CLIP AT BS 1105, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED ATTACH CLIP AT BS 1105, BETWEEN STR 15 RT AND STR 16 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-465SDR AWXA200500437Clip · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED LOWER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT; ORDERED & RECEIVED A NEW REPLACEMENT CLIP;SDR AWXA200500430Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON U-CHANNEL (STIFFENER) AT BS 1113 ON RT SIDE 3.5 INCH FROM BOTTOM, STR 17 RT. MAINTENANCE REMOVED CORRODED STIFFENER AT BS 1113, STR 17 RT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46579; ISDR AWXA200500443Connector · brokenMCN - EEL - DURING C-05 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT HOOK-UPS DAMAGED THROUGHOUT CABIN ON BOTH THE HARNESS AND AIRCRAFT SIDE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HOOK-UPS, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500409Gusset · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON RT STRINGER GUSSET AT BS 1088, STR 20 RT. MAINTENANCE REMOVED CORRODED RT STRINGER GUSSET AT BS 1088, STR 20 RT; FABRICATED A NEW REPLACEMENT GUSSET PER DWG 69-40234; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02.SDR AWXA200500485Fitting · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR STABILIZER BEAM FORWARD ATTACH FITTING AT LOWER WING AT RS 197. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR STABILIZER BEAM FORWARD ATTACH FITTING IAW SOPM 20-50-01.SDR AWXA200500435Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON VERTICAL STIFFENER AT FORWARD FACE OF BULKHEAD AT BS 1088, RBL 23, BETWEEN WL 210-220. MAINTENANCE REMOVED CORRODED VERTICAL STIFFENER AT FORWARD FACE OF BULKHEAD BS 1088, RBL 23, FROM WL 210 TO WLSDR AWXA200500425Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON HORIZONTAL STIFFENER ANGLE AT FORWARD FACE OF BULKHEAD AT BS 1088, BETWEEN RBL 23 AND RBL 33. MAINTENANCE REMOVED CORRODED HORIZONTAL STIFFENER ANGLE AT FORWARD FACE OF BULKHEAD AT BS 1088, FROM RBSDR AWXA200500423Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STIFFENER AT BS 1106, STR 17 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STIFFENER AT BS 1106, STR 17 RT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46579; INSTALLED REPAIR SDR AWXA200500419Stiffener · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON VERTICAL STIFFENER ON FORWARD FACE OF BULKHEAD BS 1088, RBL 33, BETWEEN WL 210 AND WL 220. MAINTENANCE REMOVED CORRODED VERTICAL STIFFENER AT BS 1088, RBL 33, FROM WL 210 TO WL 220; FABRICATED A NEW REPLACEMENT STIFFENSDR AWXA200500418Stringer · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STRINGER BETWEEN BS 1105 AND 1117, STR 16 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STRINGER FROM BS 1105 TO 1117, STR 16 RT; INSTALLED NEW REPLACEMENT STRINGER IAW B737-300 SRM 51-40-02, FIG 3 AND 8SDR AWXA200500417Stiffener · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STIFFENER AT BS 1116, STR 15 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STIFFENER AT BS 1116, STR 15 RT; INSTALLED NEW REPLACEMENT STIFFENER IAW B737-300 SRM 51-40-02, FIG 3 & 8.SDR AWXA200500416Stringer · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STRINGER BETWEEN BS 1105 AND BS 1117, STR 13 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STRINGER FROM BS 1105 TO BS 1117, STR 13 RT; INSTALLED NEW REPLACEMENT STRINGER IAW B737-300 SRM 51-40-02, FIG 3SDR AWXA200500415Stiffener · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX ANGLE AT BS 1104, STR 14 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX ANGLE AT BS 1104, STR 14 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-40355; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02.SDR AWXA200500406Fitting · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR STABILIZER BEAM AFT ATTACH FITTING WHERE IT CONNECTS TO LOWER WING AT RS 197. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR STABILIZER BEAM AFT ATTACH FITTING IAW SOPM 20-50-01.SDR AWXA200500446Frame · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT LOWER FUSELAGE FRAME AT BS 986.5, STR 25 RT. MAINTENANCE CUT OUT CORRODED AREA OF AFT LOWER FUSELAGE FRAME AT BS 986.5, STR 25 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR SDR AWXA200500436Strap · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT TAIL COMPARTMENT LOWER STRAP AT BS 1088, BETWEEN STR 19 RT AND STR 20 RT. MAINTENANCE REMOVED CORRODED STRAP AT BS 1088, FROM STR 19 RT TO STR 20 RT; FABRICATED A NEW REPLACEMENT STSDR AWXA200500362Web · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR SILL AFT WEB AT RBL 44, BETWEEN BS 988 AND BS 993, WL 208. MAINTENANCE CUT OUT DAMAGED R-2 DOOR SILL AFT WEB AT RBL 44, FROM BS 988 TO BS 993; FABRICATED A NEW REPLACEMENTSDR AWXA200500441Sill · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FORWARD CARGO DOOR LOWER SILL WEB BETWEEN BS 447 AND BS 488, AT RBL 28. MAINTENANCE REMOVED CORRODED FORWARD CARGO DOOR LOWER SILL WEB FROM BS 447 TO BS 488, AT RBL 28; FABRICATED SDR AWXA200500440Shear Tie · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LOWER FUSELAGE FRAME SHEAR TIE AT BS 986.5, STR 25 RT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 986.5, STR 25 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-46564; INSTALSDR AWXA200500431Attach Angle · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD UPPER ATTACH ANGLE FOR INTERCOSTAL AT BS 474, STR 25 RT. MAINTENANCE REMOVED CORRODED ATTACH ANGLE AT BS 474, STR 25 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DSDR AWXA200500429Attach Angle · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO DOOR LOWER SILL, LOWER AFT ATTACH ANGLE AT BS 491, RBL 23. MAINTENANCE REMOVED CORRODED LOWER AFT ATTACH ANGLE AT BS 491, RBL 23; FABRICATED A NEW REPLACEMENT ANGLE PER DWSDR AWXA200500413Intercostal · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD INTERCOSTAL WEB AT BS 474, STR 25 RT. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB AT BS 474, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 69-16783; INSTALLED REPAIR PART IAW SDR AWXA200500410Web · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD INBOARD WEB SILL BETWEEN BS 440 AND BS 492, STR 25 RT. MAINTENANCE REMOVED CORRODED WEB FROM BS 440 TO BS 492, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-20726; INSTALLEDSDR AWXA200500408Intercostal · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT INTERCOSTAL AT FORWARD SIDE OF BS 500D, STR 26 LT. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 500D, STR 26 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41757; INSTALSDR AWXA200500405Attach Angle · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON UPPER ATTACH ANGLE FOR INTERCOSTAL AT FORWARD CARGO COMPARTMENT THRESHOLD BS 460, STR 25 RT. MAINTENANCE REMOVED CORRODED ATTACH ANGLE AT BS 460, STR 25 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-20726; INSTALLESDR AWXA200500448Skin · delaminatedMCN - MAJOR REPAIR - DURING C-05 CHECK FOUND THE UPPER SURFACE OF THE NR 7 SPOILER DELAMINATED BETWEEN WS 366 AND WS 368 RT. MAINTENANCE REMOVED DELAMINATED AREA OF NR 7 SPOILER UPPER SURFACE SKIN; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILSDR AWXA200500424Attach Angle · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE AFT CARGO DOOR CUTOUT SILL WEB TO FRAME ATTACH ANGLE AT BS 794, BETWEEN STR 26 RT & STR 27 RT. MAINTENANCE REMOVED CORRODED SILL WEB TO FRAME ATTACH ANGLE AT BS SDR AWXA200500421Channel · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB CLOSE OUT "U" CHANNEL BETWEEN BS 794 AND BS 847, AT RBL 28. MAINTENANCE REMOVED CORRODED "U" CHANNEL FROM BS 794 TO BS 847, AT RBL 28; FABRICATED A NEW REPLACEMENTSDR AWXA200500383Panel · delaminatedMCN - MAJOR REPAIR - DURING C-05 CHECK FOUND THE UPPER SURFACE OF THE NR 8 SPOILER DELAMINATED BETWEEN WS 432 AND WS 434.5. MAINTENANCE REMOVED DELAMINATED AREA OF NR 8 UPPER SURFACE SPOILER SKIN; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILESDR AWXA200500449Door Frame · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK FOUND CORROSION ON R-2 DOOR INNER CHORD BETWEEN BS 964 AND BS 995, RBL 44 AND RBL 49. MAINTENANCE REMOVED CORRODED R-2 DOOR INNER CHORD FROM BS 964 TO BS 995, RBL 44 TO RBL 49; FABRICATED A NEW REPLACEMENT INNER CHORD; I
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