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 F3LA97049Seat Track · corrodedPAE - WHILE WORKING INTERIOR 00171, FOUND CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360. REMOVED CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360, WL 208, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 344-BS 360, FABRICATED SEAT TRSDR F3LA97053Stringer · crackedPAE - AT STATION 500B PLUS 2.5, STRINGER 16L IS CRACKED, LENGTH OF CRACK .25 INCH. CUTOUT DAMAGED AREA AND REPAIRED PER TRAMCO EWO NR 97-0115 AND BOEING SB 737-53-1145. WORK ACCOMPLISHED ON TRAMCO WORK ORDER NR INTERIOR 262. (M)SDR F3LA97046Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD, BS 360, RBL 1 TO LBL 11, WL 208.1. FOUND CORROSION BEYOND LIMITS. REMOVED BS 360, WL 208.1 CHORD FROM LBL 13 TO RBL 15. FABRICATED AND INSTALLED REPAIR. ALL WORK DONE IAW SRM 53-10-1, 53-10-9, 5SDR F3LA97037Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 344, RBL 9 TO LBL 65. FOUND CORROSION BEYOND LIMITS PER SRM 52-10-1. REMOVED CHORD FROM LBL 65 TO RBL 65. FABRICATED AND INSTALLED NEW CHORD. ALL WORK PERFORMED IAW SRM 51-10-6, 53-10-2, 53-10SDR F3LA97036Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 328, RBL 60 - LBL 30, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 328. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED UPPER CHORD AND REPAIR ANGLES FROM 7075-T6 .090 T-ANGLESDR F3LA97035Skin · gougedPAE - AFT CARGO DOOR EXTERNAL SKIN GOUGED 28 INCH FROM FWD EDGE. BLENDED GOUGED AREA IN EXTERNAL SKIN OF AFT CARGO DOOR 28 INCH IN FROM FORWARD EDGE AND 21 INCH DOWN FROM EDGE. DAMAGED AREA FOUND TO BE OUT LIMITS IAW SRM 52-00-2. REMOVED, FABRICATED DOUBLERSDR F3LA97034Seat Track · corrodedFOUND CORROSION (C53-107-01), ON SEAT TRACK BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208 IN AN AREA 6 INCH BY 1 INCH BY .020 INCH. ORIGINAL THICKNESS . 270 INCH OF SEAT SDR F3LA97033Floor Beam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1 IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED UPPER CHORD FSDR F3LA97032Access Door · crackedAPU ACCESS DOOR MOST AFT RIB RIGHT CORNER CRACKED. STOP DRILLED CRACK END USING .125 INCH DRILL, CRACK WAS FOUND TO BE 2 INCHES IN LENGTH. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS FROM STOCK MATERIAL OF 2024-T3 .050 IAW SRM 51-10-1, 52-40-1SDR F3LA97031Skin · dentedPAE - FORWARD CARGO DOOR EXTERNAL SKIN DENTED 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. DENT IN FORWARD CARGO DOOR EXTERNAL SKIN 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-SDR F3LA97094Skin · crackedCLT - FOUND CRACK IN THE NR 2 ENGINE PYLON SCREW HOLE. INSTALLED NEW ANGLE, DOUBLERS AND FILLERS PER EA 57446, EA 57462, SRM 51-40-01 AND SRM 54-10-3. (M)SDR USAASB97042Battery · failedSYR - MAINTENANCE FOUND THE FORWARD RIGHT CABIN EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. (M)SDR USAA970049Longeron · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED LONGERON AT BS 520 RBBL 17. FABRICATED AND REPAIRED PER SRM 53-10-5. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA970047Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT FUSELAGE FRAME BS 767 BL 0. INSTALLED WEB TYPE REPAIR, REPAIRED PER SRM 51-40-2. (M)SDR USAA970045Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SKIN AT STATION 378, STRINGER 28 LBL 3. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)SDR USAASB97034T-Fitting · leakingPHL - FL 319 - AT 1,000 FT, MASTER CAUTION LIGHT AND THE 'A' SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED. THE 'A' SYSTEM HYDRAULIC QTY INDICATED ZERO. FLIGHT RETURNED TO FIELD AT PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER SDR F3LA97030Skin · dentedPAE - DENT ON SKIN AT BS 388.5, 4 INCH ABOVE STRINGER 19L. REMOVED DAMAGED SKIN ON BS 388.5, 4 INCHES ABOVE STRINGER 19L. FABRICATED THE DOUBLER FROM 2024-T3 .050 MATERIAL. SEALED AND INSTALLED WITH RIVETS PER SRM 53-30-3. (M)SDR F3LA97029Skin · dentedPAE - DENT IN SKIN AT BS 875-879, BETWEEN STRINGER 17R-18R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-30-01. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SHEET STOCK. DOUBLER INSTALLED WET SEALANT. ALL WORK DONE IAW SRM 53-30-3 FIG SDR USAASB97036Coalescer Bag · dirtyCLT - FL 832 - IMMEDIATELY AFTER TAKEOFF, CREW HEARD A FLAPPING NOISE ON THE RIGHT SIDE OF AIRCRAFT AND NOTICED A BURNING OIL TYPE ODOR. CREW SUSPECTED RIGHT PACK AND TURNED PACK OFF. NOISE AND ODOR WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACKSDR F3LA97027Slide · low pressureDEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSRUE LOW. REPLACED ESCAPE SLIDE. (M)SDR F3LA97045Seat Track · corrodedCLT - FOUND SURFACE CORROSION AT SEAT TRACK MOUNT AT STATION 294, RBL 45.5. REMOVED SURFACE CORROSION ALODINED AND PRIMED. (M)SDR USAA970040Splice · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA STRINGER SPLICE STATION 360, STRINGER 27L. REMOVED CORROSION AND INSTALLED NEW STRINGER SPLICE, C/C 1127803. REPAIRED PER SRM 51-10-6/51-30-2. (M)SDR F3LA97026Skin · delaminatedPAE - RIGHT WING OUTBOARD FOREFLAP HAS AREA OF DELAMINATION ON UPPER SURFACE MID-SECTION. REPAIRED RIGHT WING FOREFLAP UPPER SURFACE MID-SECTION PER SRM 51-40-6. FABRICATED AND INSTALLED DOUBLERS, USING 2024-T3 .016 MATERIAL. (M)SDR F3LA97025Skin · disbondedPAE - RIGHT WING OUTBOARD FORE FLAP HAS AREA OF DISBOND ON UPPER INBOARD END. REPAIRED RIGHT WING OUTBOARD FORE FLAP UPPER INBOARD END IAW SRM 51-40-6. FABRICATED AND INSTALLED DOUBLERS, USING 2024-T3 .010 MATERIAL. (M)SDR USAASB97033Escape Slide · failedINT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD MAIN ENTRY DOOR ESCAPE SLIDE, INSPECTION REPORTED THAT THE ESCAPE SLIDE WAS TANGLED AND DID NOT FULLY INFLATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD MAIN ENTRY DOOR ESDR F3LA97044Floor Beam · corrodedCLT - FOUND CORROSION AROUND SCREW HOLE BS 947, RBL 40. REMOVED SURFACE CORROSION ON FLOOR BEAM PER SRM 51-10-06. (M)SDR F3LA97043Floor Beam · corrodedCLT - FOUND CORROSION AROUND SCREW HOLES AND ADJACENT AREAS, BS 947, RBL 3 THROUGH RBL 22 ON FLOOR BEAM. REMOVED SURFACE CORROSION BY BURNISHING THE TOP SURFACE. (M)SDR F3LA97042Floor Beam · corrodedCLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 987, LBL 5. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-0. (M)SDR F3LA97041Floor Beam · corrodedCLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 967, RBL 42. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-6. (M)SDR F3LA97040Seat Track · corrodedCLT - FOUND CORROSION (C53-107-02) ON AFT GALLEY SEAT TRACK AT STATION 986-1016, RBL 20. REMOVED CORROSION PER SRM 51-10-6 AND ALODINED AND PRIMED THE AREA. (M)SDR F3LA97039Support · corrodedCLT - FOUND CORROSION (C53-107-02) ON AFT LAV FLOOR SUPPORT, STATION 1006-966, LBL 10-10. REMOVED NUT PLATES ON THE FLOOR BEAM SUPPORT, REMOVED LIGHT CORROSION BY BURNISHING PER SRM 51-10-6. (M)SDR F3LA97038Floor Beam · corrodedCLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 986, RBL 50 THROUGH LBL 21. REMOVED SURFACE CORROSION PER SRM 51-10-6. ALODINED AND PRIMED THE AREA. (M)SDR F3LA97024Frame · gougedPAE - BS 328 STRINGER 28L FRAME IS GOUGED GREATER THAN 50 PERCENT AT FASTENER COMMON TO FRAME AND STRINGER. REMOVED DAMAGED SECTION OF FRAME AT BS 328 STRINGER 28L. FABRICATED REPAIR ANGLE AND FILLER, TREATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-03. (MSDR F3LA97019Doubler · corrodedUPON REMOVAL OF NR 2 DME ANTENNA FOR BS 520 FRAME REMOVAL FOUND CORROSION ON NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0 WL 148.5. REMOVED CORROSION FROM AROUND NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0, WL 148.5 AREA FOUND TO BE OUT OF LIMITS. (SDR 97ZZZM203Doubler · corrodedPAE - UPON REMOVAL OF NR 1 ADF ANTENNA FOR BS 520 FRAME REMOVAL, FOUND CORROSION ON NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. REMOVED CORROSION FROM AROUND NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. AREA FOUND TO BE OUT OF SDR F3LA97017Nose Chord · corrodedFOUND CORROSION ON RIGHT LOWER NOSE CHORD HORIZONTAL FLANGE BS 237 TO 250 RBL 18, WL 164. REMOVED RT LOWER NOSE CHORD DUE TO CORROSION WAS BEYOND LIMITS IN A ONE INCH AREA IAW SRM 53-10-1. INSTALLED NEW NOSE CHORD WITH A SPLICE IAW SRM 51-40-3, 53-10-2, 51-3SDR USAASB97020Battery Pack · dischargedROA - MAINTENANCE FOUND THE AFT ENTRY DOOR INTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)SDR 97ZZZM214Power Supply · inoperativeROA - MAINTENANCE FOUND THE AFT ENTRY DOOR INTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB97019Bypass Switch · failedPIT - FL 1261 - ON CLIMB-OUT OF PIT, THE OIL FILTER BYPASS LIGHT FOR THE NR 1 ENGINE ILLUMINATED AT APPROX 11,000 FEET. THE CAPT SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT PIT. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR USAASB97017Heat Manifold · failedTPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTTLE AND THE LIGHT ILLUMINATED AGAIN. CAPT DECIDED TO RETURN TO FIELD AT TPA. NO EMERGENCY WAS DECLSDR USAASB97014Battery Pack · dischargedCLE - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M)SDR USAA970016Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK AT STATON 332.10 LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED DOUBLER PER EA, GENERATED OM-7 NR 13021 FOR FINAL REPAIR DUE IN 18 MONTHS OR 4500 CYCLES. REPAIRED PER EA 59266 ASDR USAA970015Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCHES OF STRINGER 27L CORRODED AT STATION 947.5. INSTALLED STRINGER REPAIR PER SRM 53-10-3.(M)SDR USAA970014Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 22 INCH OF STRINGER 27 L CORRODED AT STATION 966. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR USAA970013Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 16 INCHES OF STRINGER 27L CORRODED AT STATION 986.5. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR F3LA97015Delta Beam · crackedPAE - FOUND CRACK ON PREVIOUS REPAIR BEHIND RAM AIR DUCT RIGHT SIDE AT BS 574-579, RBL 40, WL 152 ON DELTA BEAM. REMOVED 2 INCH CRACK BY REMOVING DAMAGE AREA, REPAIRED LOWER DELTA BEAM WEB, RT SIDE BS 574-579, RBL 40, WL 152 IAW SRM 53-10-6 FIG 1 WITH PART FASDR F3LA97014Skin · gougedPAE - WHILE WORKING ENGINE NR 195 FOUND RT LOWER RAM AIR INTAKE SKIN GOUGED AT BS 500B PLUS 7 STRINGER 24 RT. REMOVED DAMAGED WEB AT BS 500B PLUS7, STRINGER 24 RT FABRICATED WEB FROM MATERIAL 2024-T3, .040 INCH PER SRM 51-20-01. ALODINED, PRIMED AND INSTALLESDR F3LA97013Frame · damagedFOUND CORROSION ON THE FORWARD SIDE OF THE 520 FRAME IN THE FORWARD CARGO BAY BS 520 LBL 18 TO RBL 14, WL 149. REMOVED DAMAGED FRAME, STRINGER CLIPS, STRINGER 26 LT (30 INCH) AND DAMAGED INTERCOSTALS AS WELL AS FLOOR TO SIDEWALL SUPPORT PLATES. FABRICATED NESDR 97ZZZX877Actuator Sleeve · wornTHE ELONGATED HOLE WHERE THE CAM SEGMENT IS INSERTED INTO THE YAW DAMPER PISTON IS BEING RUBBED AND WORN BY THE CAM SEGMENT.SDR 97ZZZX875Cam Segment · wornTHE SHAFT JUST ABOVE THE BALL IS RUBBING/WEARING ON THE YAW DAMPER SLEEVE. WHEN THE UNIT WAS EXTENDED AND THE YAW DAMPER WAS ENERGIZED IN THE EXTEND POSITION, THE UNIT BOUND AND WOULD NOT RETRACT PER PARA 12, G, 889. THE AREA OF WEAR HAS A RIDGE THAT WILL CA
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