Boeing 737-201
Service difficulty reports · 2,471
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 = '737201' 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 = '737201' 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 USAA960561Angle · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCH STATION 277 TO 340 'Z' ANGLE RIGHT SIDE. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960560Beam · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 420 TO BS 500, STRINGER 26R BEAM. FABRICATED AND REPLACED WITH NEW BEAM. SPLICED AT 420 AND 500. REPAIRED PER SRM 53-00-53 AND SRM 53-10-5. CORROSION TAKS NR 53-208-SDR USAA960559Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS AT FASTENER HOLES STATION 532, STRINGER 15R. REMOVED DAMAGED SECTION OF STRINGER AND PERFORMED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. (M)SDR USAASB96154Actuator · internal leakageROA - FLT 2520 - THE NR 5 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO FIELD AT ROA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDGE SLAT ACTUATOR TO HAVE INTERNAL LEAKAGE. REPLACED ACTUATOR PER MM 27-81-SDR USAASB96153Retract Mech · malfunctionedGOO - FLT 8028 - AFTER TAKEOFF FROM GSO, CAPTAIN WAS UNABLE TO RAISE LANDING GEAR LEVER. TWO OTHER ATTEMPTS WERE MADE BUT WERE UNSUCCESSFUL. CIRCUIT BREAKERS WERE ALL IN AND GEAR PINS WERE ONBOARD. CAPTAIN ELECTED TO RETURN TO FIELD AT GSO. NO EMERGENCY WASDR USAASB96148Snubber · misinstalledPHL - FL 351 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED AN EXCESSIVE NOISE COMING FROM THE FORWARD MAIN ENTRANCE DOOR. THE CAPTAIN INDICATED THE CABIN WAS PRESSURIZING TOO SLOWLY AND DECIDED TO RETURN TO THE FIELD AT PHL. THE FLIGHT LANDED WITH NO FURTHERSDR USAASB96145Battery Pack · dischargedROC - MAINTENANCE FOUND EMERGENCY AISLE LOW LEVEL LIGHTING INOP AT ROWS 7, 9, 11, 12, AND 13 LEFT SIDE. MAINTENANCE REPLACED BATTERY PACK AT ROW 12. OPS CHECK GOOD. (M)SDR USAASB96141Hyd Hose · loosePVD - FL 381 - SHORTLY AFTER TAKEOFF FROM BOS, A STRONG UNIDENTIFIABLE SMELL OCCURRED IN THE CABIN. THE SMELL TAPERED OFF DURING CLIMB-OUT, BUT CAME BACK VERY STRONG WHEN LEVELING AT FL 310. FLIGHT DIVERTED TO PVD. NO EMERGENCY WAS DECLARED AND THE FLIGHT LSDR 96ZZZX3744Escape Slide · low pressureDEN - FLT 601 - UPON ARRIVAL, FLIGHT CREW REPORTED THE FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE AT ZERO. MAINTENANCE REPLACED ESCAPE SLIDE.SDR USAA960536Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCHCRACK IN 178 BULKHEAD 2 PLACES RIGHT SIDE AT LOWER RIGHT MOUNT FOR RADAR.INSTALLED DOUBLER AND FILLERS, REPAIRED PER TR 53-10-11.(M)SDR USAA960535Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1INCH CRACK IN 178 BULKHEAD TWO PLACES LEFT SIDE AT LOWER LEFT MOUNT FORRADAR. INSTALLED DOUBLERS, REPAIRED PER TR 53-10-11.(M)SDR USAA960534Keelbeam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETERCORRODED AREA PLUS 4 KEEL BEAM RBL 6.4 FS 727 TO FS 710. SPOT FACED HOLESINSTALLED, INSTALLED REPAIR STRAP. REPAIRED PER EA 41303. (M)SDR USAA960533Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCHCORROSION FLOOR BEAM F/S 1016 BL 0 TO RBL 12. SPLICED IN FLOOR BEAM T-CAPAND DOUBLERS REPAIRED PER SRM 53-10-9 EA 41313. (M)SDR USAA960514Shear Beam · crackedROA - DURING BX-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACKSTRINGER 18 A RIGHT SHEAR BEAM AT BS 706. INSTALLED REPAIR KIT, REPAIREDPER EO 5393G256 PART 3 STEP 4. (M)SDR USAA960515Skin · crackedROA - DURING 'BX CHECK' VISUAL, CONFIRMED WITH HFEC INSPECTIONFOUND 1 INCH FUSELAGE SKIN CRACK BS 747 STRINGER 18R. REMOVED CRACK ANDINSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAASB96124Flow Control Vlv · failedMSP - FLT 824 - ON CLIMB-OUT ABOVE 15,000 FEET, A LOUD RUMBLING NOISE BEGAN. CREW DECIDED TO RETURN TO FIELD AT MSP. ALL AIRCRAFT INDICATORS WERE NORMAL. CREW SWITCHED EQUIPMENT COOLING FAN TO ALTERNATE, THEN GASPER FAN TO OFF, NO HELP. NOSE EVENTUALLY DIMSDR USAA960506Skin · crackedROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND .4375 INCH CRACK AT AFT ENTRY DOOR CUT OUT FORWARD LOWER HINGE CUT OUT FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 34. (X)SDR USAA960505Skin · crackedROA - DURING 'BX' CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC, FOUND .75 INCH FUSELAGE SKIN CRACK S19L, BS 760. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 3. (X)SDR USAASB96118Oil Filter Studs · pulled outCLE - FLT 273 - FLYING AT 27,000 FEET, THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN NR 2 ENGINE AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO CLE AND LANDED WITH NO FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCSDR USAASB96115Retract Mech · malfunctionedORF - FLT 1177 - AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR. LANDING GEAR INDICATIONS WERE BLANK. CREW ACCOMPLISHED CHECK LIST AND FOUND LIGHTS AND LEVER LATCH CIRCUIT BREAKERS TRIPPED. RESET SAME AND GOT NORMAL INDICATIONS. CAPTAIN DECIDED TO RESDR USAASB96114Strap · out of positionPIT - FLT 1279 - WHILE CLIMBING THROUGH 8,000/9,000 FEET, FLIGHT ATTENDANT ADVISED CAPTAIN OF A NOISE FROM THE REAR OF THE AIRCRAFT. AFTER LEVELLING OFF AT 11,000 FEET, DISCOVERED THE SAFETY RESTRAINING STRAP WAS CAUGHT IN THE 2L DOOR. THERE WAS NO DOOR WARNSDR F3LA96017Power Supply · inoperativeDEN - DURING AN A-6 CHECK, MX REPORTED THE RIGHT EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED THE RIGHT BATTERY POWER SUPPLY AND CHECKED OK. (M)SDR F3LA96016Battery Pack · dischargedDEN - DURING AN A-6 CHECK, MAINTENANCE REPORTED THE RIGHT WING EMERGENCY EXIT LIGHT ABOVE INBOARD FLAPS INOPERATIVE. REPLACED THE RIGHT BATTERY PACK AND CHECKED OK. (M)SDR USAA960482Stiffener · crackedINT - DURING 'Q-6' CHECK EDDY CURRENT, FOUND .50 INCH LONG CRACK AT STIFFENER STA 178, LBL 5.7 INCH, WL 184. INSTALLED REPAIR ANGLES AND REPAIRED PER TR 53-10-17. (X)SDR USAA960481Skin · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 1.6250 INCH CRACK IN OUTER SKIN S18R, BS 727A PLUS 7 INCHES. DOUBLER INSTALLED, REPAIRED PER SRM 53-30-3. (X)SDR USAA960480Stringer · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STR 18A SHELF, 1 INCH FORWARD OF STA 727 BULKHEAD AT INBOARD VERTICAL FASTENER. STOP DRILL CRACK AND INSTALLED REPAIR KIT. REPAIRED PER EO 5393G256. (X)SDR USAA960479Floor Beam · corrosionINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION FLOOR BEAM, STA 328, LBL 27. FABRICATED TEE-CAP REPAIR, REPAIRED PER TR 53-10-13. (X)SDR USAA960478Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 1156, WL 380 RT OUTBOARD CHORD OF BULKHEAD. STOP DRILLED AND INSTALLED REPAIR. REPAIRED PER EO 5391G569. (X)SDR USAA960477Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK, 178 BULKHEAD. STOP DRILLED CRACK, FABRICATED DOUBLER, FILLERS, AND INSTALLED. REPAIRED PER SRM 51-01-1, TR 53-10-11. (X)SDR USAA960476Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION FOUND 3 CRACKS, 1 INCH, 1 INCH, AND .50 INCH, 178 BULKHEAD. STOP DRILL CRACKS, FABRICATED DOUBLER, FILLERS, AND INSTALLED. REPAIRED PER SRM 51-10-1, TR 53-10-11. (X)SDR USAASB96109Oil Press Ind · failedBWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT BWI. THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY EQUIPMENT WAS CALLED OUT. THE FLIGHT LANDESDR USAASB96107Battery Pack · dischargedSYR - MAINTENANCE FOUND THE AFT SET OF AISLE EMERGENCY SEAT LIGHTS BLINKING ON AND OFF. MAINTENANCE REPLACED THE BATTERY PACK. (M)SDR USAA960470Skin · lightning strikeROA - DURING BX CHECK, FOUND LIGHTNING STRIKE DAMAGE 2 INCHES BY 8 INCHES ON FUSELAGE CROWN SKIN. BURNISHED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6. (X)SDR USAA960469Skin · crackedROA - DURING VISUAL INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-30-03. (X)SDR USAASB96099Elect Trim · activatedLGA - FLT 2221 - ON APPROACH TO LGA, CREW REPORTED WHILE FLYING WITH AUTOPILOT DISENGAGED, THE ELECTRIC STABILIZER TRIM ACTIVATED FOR 3-5 SECONDS. CREW OVERRODE TRIM AND PERFORMED A GO-AROUND. FLIGHT THEN LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMSDR USAA960468Stringer · corrosionROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5. INSTALLED DOUBLER AND STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR USAA960467Skin · crackedROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION VERIFIED WITH HFEC, FOUND TWO .75 INCH CRACK IN FUSELAGE SKIN JUST ABOVE STRINGER 18L, FORWARD OF BS 787. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAASB96093Power Supply · inoperativeROC - MAINTENANCE FOUND THE AFT AISLE BULLNOSE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY. (M)SDR 96ZZZX3266Valve · failedDEN - FLT 546 - AFTER TOUCHDOWN, FLIGHT CREW REPORTED A-SYSTEM HYDRAULIC PRESSURE FLUCTUATING AND LOSS OF NOSE WHEEL STEERING. TOWED AIRCRAFT TO GATE. REPLACED LEFT HYDRAULIC SHUT OFF VALVE, CASE DRAIN FILTER AND PRESSURE FILTER AND SYSTEM CHECKED OKAY. TOTSDR USAA960465Skin · crackedROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 2 CRACKS .875 INCH AND .125 INCH IN LENGTH AT FUSELAGE SKIN AT STRINGER 16L BS 727A. CONTAINED CRACKS AND INSTALLED DOUBLER, REPARIED PER SRM 53-30-3 FIG 1. (M)SDR USAASB96092Engine · failedPHL - FL 945 - DESCENDING FROM 20,000 FEET, NR 1 ENGINE BEGAN BANGING SEVERELY. CREW REDUCED POWER, PARAMETERS LOOKED GOOD. CREW THEN ADVANCED POWER, BANGING RETURNED. AS POWER WAS REDUCED TO IDLE, EGT CLIMBED TO RED. NR 1 ENGINE WAS SHUT DOWN IN FLT. TOTSDR USAA960439Chord · crackedCLT - INSPECTION FOUND TWO APPROXIMATELY .375 INCH CRACK BY ULTRASONIC AND EDDY CURRENT LOCATED AT STATION 727 AT STRINGER 18A RIGHT CHORD. INSTALLED CHORD SECTION, AUX CHORD AND LOWER SPLICE PER EO NR 9394G068. (M)SDR F3LA96013Connector · dirtyMSP - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED LIGHT ASSEMBLY CONTACTS AND CHECKED OK. (M)SDR USAASB96083Oil Cooler · failedFLT NR 2316 - RIC - NR 1 ENGINE OIL TEMP REMAINED IN YELLOW ARC FOR MAX 15 MIN RESTRICTION. PRECAUTIONARY ENGINE SHUTDOWN COMPLETED. MAINTENANCE REPLACED LEFT ENGINE FUEL/OIL EXCHANGER. OPS AND LEAK CHECK OK. (M)SDR USAASB96087Light Emergency · failedFLT 916 - PHL - COCKPIT EMERGENCY LIGHT INOP. MX REPLACED COCKPIT EMERGENCY LIGHT ASSY. OPS CHECK SATISFACTORY. (M)SDR USAA960427Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FUSELAGE SKIN AT BS 727 A BETWEEN STRINGER 15 AND 16 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 01. (M)SDR USAA960418Skin · dentedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 12/32 INCH BY .065 DENT RIGHT FUSELAGE SKIN AT STRINGER 20 BS 390. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER. REPAIRED PER EA 58327. (M)SDR USAASB96075Smoke Detector · failedFLT NR 2359 - LGA - MX FOUND THAT THE AFT LAV SMOKE DETECTOR WAS INOP. MX REPLACED THE SMOKE DETECTOR IN THE AFT LAV. OPS CHECKS SATISFACTORY. (M)SDR USAASB96074Power Pack · failedFLT 510 - ROC - MAINTENANCE FOUND THAT THE AFT ENTRY AND SERVICE DOOR EMERGENCY SLIDE LIGHTING SYSTEM WAS INOP. MX REPLACED THE BATTERY AND THE CHARGER. SYSTEM CHECKED SAT. (M)SDR USAASB96073Engine · bird strikePHL - FLT 819 - AIRCRAFT RETURNED TO FIELD DUE TO INGESTION OF BIRD IN NR 1 ENGINE. MAINTENANCE FOUND DAMAGE FROM BIRD INGESTION THAT WAS CAUSE FOR NR 1 ENGINE REPLACEMENT. (X)
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