Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAASB01284Landing Gear · lack of lubeCLT - FLT 237 - AFTER TAKEOFF FROM ORF, EN ROUTE TO CLT, CREW RECEIVED MAIN LANDING GEAR RED UNSAFE LIGHTS WITH GEAR HANDLE SELECTED TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND LIGHTS EXTINGUISHED. FLIGHT CONTINUED ONTO CLT. OSDR AWXA200100537Pressure Panel · crackedMCN - C16 CK - C - CRACK FOUND ON PRESSURE WEB IN LT MAIN LANDING GEAR WELL, CONFIRMED WITH HFEC, BS 664, LBL 32, 1.25 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 03-5702-01286-GF1.SDR USAASB01279Battery Pack · dischargedTPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS, FROM ROW 4 THROUGH EMERGENCY EXIT ROW, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID-CABIN BATTERY PACK, RIGHT SIDE. OPS CHECK GOOD. (M)SDR USAASB01276Charger · inoperativeTPA - MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR AND AFT RIGHT SERVICE DOOR EXTERIOR EGRESS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK OF ALL EMERGENCY LIGHTS GOOD. (M)SDR USAA011274Bulkhead · dentedCLT - FOUND WEB DENTED 4 INCHES BY 4 INCHES, BS 178 WL 181.5 BL 0. INSTALLED DOUBLER. (M)SDR USAA011277Stiffener · crackedCLT - FOUND CHORD VERTICAL CRACKED .25 INCH, BS 178 WL 184 LBL 505. INSTALLED ANGLE AND STRAP. (M)SDR USAASB01273Seal · out of positionJAX - FLT 1505 - DURING DESCENT, FLIGHT ATTENDANTS AND PAX NOTICED AN ELEC BURNING SMELL IN THE AFT CABIN WITH A LOUD SQUEALING NOISE. PAX WERE HOLDING THEIR EARS AND COMPLAINING OF THE NOISE. FLIGHT LANDED WITHOUT INCIDENT. MX INSPECTED OF ALL CABIN LIGHTSSDR USAA011273Strap · bentCLT - FOUND STRAP BENT AND GOUGED, BS 178 BL 0 WL 181.5. FABRICATED REPLACEMENT STRAP AND INSTALLED. (M)SDR SWAA012656Flap · delaminatedDURING WALKAROUND INSPECTION FOUND LH INBD T/E FLAP DELAMINATED. R&R FLAP PER MM.SDR USAA011270Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 207 LBL 1. REMOVED CRACK AND INSTALLED DOUBLER. (M)SDR USAA011271Bulkhead · damagedCLT - FOUND WEB WITH OLD REPAIR REMOVED, STATION 178 WL 187 BL 0. MADE NEW REPAIR AND INSTALLED SAME. (M)SDR USAA011294Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 178 SIDE CHORD RADIUS AT WL 207 LBL 26. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO 5300V157. (M)SDR USAASB01259Charger · inoperativeGSO - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS, IN THE AFT CABIN, THAT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA011245Skin · damagedTPA - FOUND SKIN WITH 6 INCH CREASE, STATION 807 STRINGER 28 LEFT AND 28 RIGHT. REPAIRED BY INSTALLING DOUBLER, ONE DOUBLER INSTALLED FOR 2 DAMAGES PER SRM 53-00-01 FIG 201. (M)SDR USAASB01253Battery Pack · dischargedDCA - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHTS AND THE L1 DOOR EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA011266Frame · crackedCLT - FOUND CHORD CRACKED .250 INCH, BS 178, WL 184, LBL 55. SPLICED IN NEW CHORD SECTION. (M)SDR AWXA200100483Stringer · gougedMCN - C16 CK - "C" - GOUGE IN STR 27R AT BS 480, FOUND TO BE BEYOND SRM LIMITS AFTER BLEND OUT. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED STRINGER SECTION AND FILLERS, AND INSTALLED REPAIR PARTS IAW B737 SRM 53-00-03, PG 201 - 206.SDR USAA011296Frame · crackedCLT - FOUND CHORD CRACKED .25 INCH, BS 178 WL 207 LBL 26 AND RBL 26. DAMAGE AREAS WERE CUTOUT, SIDE CHORD SPLICE REPAIRS INSTALLED PER EO 5300V157. (M)SDR USAA011297Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 213 RBL 6 AND WL 207 LBL 1. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M)SDR USAA011244Skin · gougedTPA - FOUND SKIN WITH 6 INCH GOUGE, STATION 807 STRINGER 27R AND 28R. REPAIRED USING SAME DOUBLER PER SRM 53-00-01 FIG 201. (M)SDR SWAA012479Light · brokenOVERHEAD EMERGENCY LIGHT BROKEN AT ROW 22 R&R LIGHT ASSY PER MM.SDR USAA011177Skin · crackedTPA - FOUND SKIN CRACKED 1.3 INCHES, STATION 947.5 LOWER FORWARD CORNER OF HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 208. (M)SDR AWXA200100484Skin · damagedMCN - C16 CK - NON STANDARD REPAIR INSTALLED AT BS 440 TO 490, STR 26R TO 28R BELOW FWD CARGO DOOR. MAINTENANCE REMOVED NON STANDARD REPAIR, TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5300-01264-BA1.SDR USAA011181Skin · crackedTPA - FOUND SKIN CRACKED .125 INCH FROM FASTENERS THREE PLACES, STATION 787 AT STRINGER 7R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 201. (M)SDR AWXA200100482Frame · crackedMCN - C16 CK - "C" - FRAME FOUND CRACKED AT BS 663, STR 2L. MAINTENANCE REPAIRED FRAME IAW B737 SRM 53-00-07, PG 226, FIG 209.SDR AWXA200100481Frame · crackedMCN - C16 CK - "C" - FRAME CRACKED AT BS 663, STR 2R. MAINTENANCE PERFORMED REPAIR TO FRAME IAW B737 SRM 53-00-07 PG 226, FIG 209.SDR AWXA200100488Frame · crackedMCN - C16 CK - "C" - .625" CRACK IN FRAME AT BS 727, STR 14L. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE & DOUBLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5300-01271-TB1.SDR USAA011183Mount · scoredPIT - FOUND MOUNT BEARING BORE SCORED, FORWARD ENGINE MOUNT. MACHINED BORE PER TYPICAL REPAIR 54-50-08 REV A. (M)SDR F3LA200100103Intercostal · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK IN INTERCOSTAL AT BS 178, WL 195, RBL 24. MAINTENANCE REPAIRED INTERCOSTAL PER SRM 737-300 MM 53-10-08.SDR F3LA200100102Intercostal · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK IN INTERCOSTAL AT BS 178, WL 195, LBL 24. MAINTENANCE REPAIRED INTERCOSTAL PER SRM 737-300 MM 53-10-08.SDR AWXA200100487Skin · dentedMCN - C16 CK - DENT IN FUSELAGE SKIN BS 1017, BETWEEN STR 15R & 16R, .5 INCH LONG X .5 INCH WIDE X .060 DEEP, BEYOND SRM LIMITS. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 03-5331-01269-DL1.SDR AWXA200100486Skin · dentedMCN - C16 CK - PERMANENT REPAIR TO DENT IN RT HORIZONTAL STABILIZER LOWER SKIN, STA 111.10, THAT HAD PREVIOUSLY BEEN PLACED ON A DEFERRED MAINTENANCE ITEM UNTIL C CHECK. MAINTENANCE REMOVED DAMAGED SKIN SECTION (STA 89 TO 116), FABRICATED NEW SKIN SECTION, INTSDR AWXA200100480Skin · dentedMCN - C16 CK - DENT IN RT HORIZONTAL STABILIZER SKIN 2.5 INCH WIDE X .065 DEEP, STA 239 INTER SPAR AREA, BEYOND SRM LIMITS. MAINTENANCE CUT OUT DAMAGED AREA, FORMED DOUBLER, FILLERS, AND ANGLES AND INSTALLED REPAIR PARTS IAW B737 SRM 55-10-01, PG 225, 228.SDR USAA011136Keelbeam · corrodedCLT - FOUND 2 INCHES OF CORROSION, LEFT KEEL BEAM, VERTICAL LEG, INBOARD SURFACE BS 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTORED FINISH, PER EA 85288 SRM 53-60-12. (M)SDR USAA011186Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .25 INCH, BELTFRAME AT STATION 747 BELOW STRINGER 8R. ROUTED OUT CRACK, INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-14. (M)SDR USAASB01234Bolt · wornDCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMESDR USAA011180Keelbeam · crackedTPA - FOUND KEELBEAM CRACKED 2 INCHES, LEFT KEEL BEAM VERTICAL LEG INBOARD SURFACE STATION 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTORED FINISH PER EA 85288, SRM 53-60-12. (M)SDR USAA011178Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, STATION 947.5 UPPER FORWARD CORNER HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 205. (M)SDR USAA011265Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 178, WL 207, LBL 28. SPLICED IN NWE CHORD SECTION PER EO 85479. (M)SDR USAA011272Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .250 INCH, BS 178 WL 207 RBL 28. REMOVED AND REPLACED PER EO 5300V157. (M)SDR USAA011275Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 WL 213 RBL 5.9 AND LBL 5.9 AND LBL 5.5. CUT OUT DAMAGE AND INSTALLED DOUBLER. (M)SDR USAA011278Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 WL 213 RBL 6. CRACK CUT OUT AND DOUBLER INSTALLED. (M)SDR USAA011295Frame · crackedCLT - FOUND CHORD CRACKED 1 INCH, BS 178 WL 207 RBL 28. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO5300V157. (M)SDR USAASB01230Controller · failedPBI - FLT 431 - EN ROUTE FROM DCA TO PBI, AT FL350 AND 100 TO 120 MILES OUT FROM PBI, THE AIRCRAFT DEPRESSURIZED, CABIN ALTITUDE WENT TO 15,000 FEET AND THE OXYGEN MASKS AUTO DEPLOYED. CREW DECLARED AN EMERGENCY, DESCENDED AIRCRAFT TO 10,000 FEET AND SWITCHEDSDR USAA011070Floorbeam · corrodedPIT - FOUND BEAM CORRODED LBL 60 - RBL 18, STATION 344 CABIN FLOOR LBL 60 RBL 18. REPLACED UPPER CHORD PER SRM 53-10-51, FIG 205 AND EA 71720. (M)SDR USAA011071Beam · corrodedPIT - FOUND BEAM CORRODED, LBL 48 INCHES-RBL 48 INCHES, STATION 986.5 CABIN FLOOR LBL 48 INCHES RBL 48 INCHES. REPLACED UPPER CHORD PER TYPICAL REPAIR 53-10-05. (M)SDR USAA011072Beam · corrodedPIT - FOUND BEAM CORRODED LBL 60 INCHES - RBL 60 INCHES, STATION 328 CABIN FLOOR LBL 60 INCHES, RBL 60 INCHES. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-51. (M)SDR USAA011084Gate · corrodedPIT - FOUND GATE CORRODED .125 INCH BY 4 INCH, BOTTOM GATE OF AFT SERVICE DOOR. (M)SDR USAA011052SkinCLT - FOUND SKIN DAMAGED 1 INCH, BETWEEN BS 28L AND BS 28R BS 380. INSTALLED .100 INCH THICK 2024 T3 DOUBLER PER TR 53-30-07, SB 737-53-1117 REV 1. (M)SDR SWAA012237Retainer · out of positionAIR TURNBACK, AFTER TAKEOFF A/C CABIN WOULD NOT PRESSURIZE. F/A REPORTED NOISE FROM AFT SVC DOOR. REPOSITIONED AFT SVC DOOR PRESS SEAL RETAINER PER MM.
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