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 USAA991085Skin · crackedPIT - DURING RON VISIT, FOUND 4 CRACKS TOTAL .5 INCH LONG, 1 INCH LONG, 1.25 INCH LONG AND 1.5 INCH LONG IN LOWER WEB SKIN PANEL AT KEEL BEAM BETWEEN STATION 690 AND 727. EXTERNAL DOUBLER INSTALLED WITH TEMPORARY FASTENERS PER SRM 53-60-12 FIG 202. (M)SDR SWAA991647Wire · brokenDURING SCHEDULED 1/2D CHECK, FOUND EEPLS HAS BROKEN WIRE AT BATTERY PACK, BS 975. REMOVED AND REPLACED WIRING SECTION PER MM.SDR USAASB99238Fairing · missingBOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDOW AT SEAT ROW 9ABC. VIBRATION AND HUMMING NOISE DECREASED UNDER 10,000 FT AND 220 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENASDR USAA991019Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION RT SERVICE DOOR Z-ANGLE BETWEEN STATION 947.5 AND 986.5. CORROSION LEVEL 1. INSTALLED NEW Z-ANGLE PER SRM 53-60-51, LIMITS AND SRM 51-10-02. (M)SDR USAA991018Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREAS OF CORROSION AT ANCHOR NUT HOLES BS 312 TO BS 370 FORWARD ENTRY SILL Z-ANGLE. CORROSION LEVEL 2. REPAIRED AND REPLACED PER SRM 51-10-02. (M)SDR USAA991017Splice · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT RIVETS BS 907, STRINGER SPLICE 4R. INSTALLED NEW SPLICE PER SRM 51-10-02. (M)SDR USAA991016Frame · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORROSION SPOT AT FRAME BS 500 RBL 25 FORWARD CARGO. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER EA 65486 REV A AND SRM 53-00-07 FIG 202. (M)SDR USAA991001Stringer · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4.5 INCH CRACK BS 1138 TO STATION 1143 STRINGER 5R. INSTALLED REPAIR ANGLE PER EA 65627A. (M)SDR USAA990999Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 24 INCH AREA OF CORROSION AT STATION 1016 FLOORBEAM AND INTERCOSTAL. CORROSION LEVEL 2. REPLACED INTERCOSTAL. INSTALLED REPAIR DOUBLERS AND STRAPS PER EA 65584. (M)SDR USAA990993Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 3 INCHES AT STATION 986.5, 44 RBL FLOORBEAM. CORROSION LEVEL 2. INSTALLED BEAM CAP REPAIR PER TR 53-10-05. (M)SDR USAA990983Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AND .500 INCH CRACK AFT CARGO AT BS 727D BL 3L AND 3R CLIP. INSTALLED REPAIR ANGLES PER SRM 51-10-02 AND BOEING DRAWING 65-65710. (M)SDR USAA990982Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2.75 INCH CRACKS IN UPPER PRESS DECK OF LEFT MLG W/W BS 664, LBL 30, WL 203 SKIN. INSTALLED DOUBLER PER EA 65333. (M)SDR USAA990981Bracket · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .2 5INCH CRACK INBOARD COAT CLOSET BRACKET AT BS 1016. REPLACED BRACKET PER REPAIR DOCUMENT 51-10-02. (M)SDR USAA990980Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, F OUND 2 CRACKS .750 LEFT AND .500 RIGHT AFT CARGO BS 727D, LBL 3 AND RBL 3 FRAME. INSTALLED DOUBLER PER EA 65325. (M)SDR USAA990979Beam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION RUNNING ALONG TOP AND SECONDARY CAPS OF BEAM APPROX 1 INCH BEAM 986.5, LBL 04, CORROSION LEVEL 1. INSTALLED UPPER BEAM CAP REPAIR PER SRM 53-10-05. (M)SDR USAA990966Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178, BL 5 LEFT 10.5 INCH FROM BOTTOM BULKHEAD WEB ATTACH ANGLE. INSTALLED REPAIR FILLER, ANGLES, RADIUS STRAPS PER SRM 53-10-08 FIG 205. (M)SDR USAA990962Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 379, LBL 2.5 AFT SIDE OF EQUIP COOLING EXHAUST OUTLET FUSELAGE SKIN. INSTALLED SKIN DOUBLER PER TR 53-30-07 AND BOEING DWG 65C33930. (M)SDR USAA990961Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 327 FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER EXTERIOR SKIN. INSTALLED TRIPLER PER SRM 53-10-01. (M)SDR USAA990960Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKS AT FAST HOLES ALONG WEB SKIN AT BS 709-712, WL 203, BBL 0. INSTALLED WEB REPAIR PER EA 65480 AND SB 737-57-1210. (M)SDR USAA990959Intercostal · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, RBL 24, WL 195 INTERCOSTAL. INSTALLED NEW INTERCOSTAL PER TR 53-10-15/SRM 51-40-03 FIG 1/SRM 53-10-08. (M)SDR USAA990938Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 1040, STRINGER 2R TO 3R SHEAR TIE CLIP. INSTALLED FABRICATED SHEAR TIE CLIP PER DWG 65-46369. (M)SDR USAA990937Bulkhead Web · corrodedCLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION LEFT FACE OF BS 1016 PRESSURE BULKHEAD CTR BL 0 STIFFENER. CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 53-80-08 AND EA 65447. (M)SDR USAA990936Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203. INSTALLED DOUBLER AND FILLER PER EA 65336A AND TR 53-10-23. (M)SDR USAA990935Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203 LEFT SIDE. INSTALLED DOUBLER AND FILLER PR EA 65336A AND TR 53-10-23. (M)SDR USAA990934T-Cap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLE BS 344, LBL 49 FORWARD FLANGE AND LBL 31 SPLICE T-CAP. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51 FIG 1 AND TR 53-10-13 AND EA 65489. (M)SDR USAA990933Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN RADIUS BS 1040 BETWEEN STRINGER 6R AND STRINGER 7R SHEAR TIE CLIP. FABRICATED NEW SHEAR TIE PER SRM 51-10-02 AND DRAWING 65-46569. (M)SDR USAA990924Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 344, LBL 49 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-30-51. (M)SDR USAA990923Splice · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK, 2 RIVETS WORKING AND CRACKED AT BS 907, STRINGER SPLICE 4L. INSTALLED NEW SPLICE PER SRM 51-10-02. (M)SDR USAA990919Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY .300 INCH CRACK AT STATION 178, BULKHEAD LBL 7, 32 INCHES FROM BOTTOM OF BULKHEAD. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR USAA990917Beam · corrodedCLT - DURING RON CHECK VISUAL INSPECTION, FOUND 7 EACH 1 INCH BY .50 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES AT BS 360 - BS 380, LT CREASE BEAM INBOARD ANGLE CORROSION LEVEL 1. REMOVED CORROSION WITHIN LIMITS PER SRM 53-10-51. (X)SDR USAA990916Floorbeam · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT BS 520, RBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)SDR USAA990915Floorbeam · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)SDR USAA990914Floorbeam · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 24 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)SDR USAA990913Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 520 AND STR 16L FRAME TIE CLIP. REMOVED AND REPLACED TIE CLIP PER BOEING DWG 65-46534 SHEET 3 AND SRM 51-10-02. (X)SDR USAA990885Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 328, LBL 20, TO RBL 50 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51. (M)SDR AWXA9900328Spar · delaminatedLOWER FLANGE OF LT AILERON FWD SPAR DELAMINATED IN 7 SPOTS FWD SPAR WBL 322.536 TO WBL 417.230. REPAIRED PER AWA ER 57-51-17B, PAINTED PER SRM 51-21-00.SDR USAASB99234Duct · failedPIT - FLT 1840 - AFTER PASSING 7,000 FT, A VERY LOUD BANG OCCURRED FROM BEHIND THE INSTRUMENT PANEL. HIGH PRESSURE AIR RUSHED OUT AND BLEW INSULATION THROUGH OUT THE COCKPIT. COCKPIT WAS VERY LOUD. AUTOPILOT OPERATION WAS AFFECTED AND HAD TO BE TAKEN OFF LSDR USAA990920Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 EACH, .50 INCH CRACKS, NR 1 SLAT INBOARD EDGE OF LOWER SKIN AFT FASTENER ROW. INSTALLED DOUBLER PER BOEING DWG 65C30133 AND TR 57-50-01 REV H. (X)SDR AWXA9900322Window · crackedL2 WINDOW OUTER PANE CRACKED AT ALTITUDE THEN STARTED ARCING, NO PRESS LOSS. REMOVED AND REPLACED CAPT'S SLIDING WINDOW. ALSO, REPLACED WINDOW HEAT CONTROL.SDR AWXA9900321Hyd Module · failedON FINAL, LOWERED LANDING GEAR, DID NOT GET GREEN LIGHTS BUT RED. CYCLED GEAR WITH SAME RESULTS. MANUALLY EXTENDED RT GEAR AND GOT GREEN LIGHT, LANDED NORMALLY. REMOVED AND REPLACED RT MLG HYDRAULIC MODULE, LK AND OPS CHECK GOOD.SDR USAASB99227Indicator · failedCLT - FLT 2250 - AFTER TAKEOFF WHEN FLAPS WERE RETRACTED FROM 5 DEGREES TO 1 DEGREE, FLAP TRAVEL STOPPED AT APPROXIMATELY 1-3/4 DEGREE POSITION WHILE LEADING EDGE REMAINED EXTENDED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENSDR AWXA9900311Skin · crackedC-CHECK, R1 DOOR AFT LOWER CORNER HAS 3 INCH LONG CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 FIG 202.SDR AWXA9900310Rib · gougedC-CHECK, LT HORIZONTAL STAB STA 295.10 O/B EDGE HAS GOUGE ON FRAME. REMOVED, FABRICATED, TREATED AND INSTALLED FRAME AND PLATE IAW 55-10-9, 51-40-02, AND 51-20-01.SDR AWXA9900309Chord · corrodedC-CHECK, CORROSION AFT CABIN AT CREASE BEAM BTWN BS 847 AND BS 867. REMOVED AND FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-60-13, SRM 51-70-12, AND SRM 51-40-2.SDR AWXA9900308Sill · corrodedC-CHECK, CORROSION FROM STA 947.5 TO 1006 BL 65R MOPSILL R2 DOOR CUTOUT. REMOVED, FABRICATED, HEAT TREATED AND INSTALLED SILL AND REPAIR ANGLE IAW SRM 51-40-02 AND 53-60-15 FIG 1.SDR AWXA9900307Floorbeam · corrodedC-CHECK, TOP OF FLOORBEAM STA 986.5 FROM RBL 55 TO LBL 55 CORROSION BEYOND LIMITS AT TWO PLACES. CUT OUT DAMAGED SECTION, REMOVED INTERCOSTALS, FABRICATED T FROM BAC1505-100617-7075-T-7, INSTALLED T AND INTERCOSTALS IAW SRM 53-00-51SDR AWXA9900303Spar · brokenCONDITION: C-CHECK SLAT DAMAGEDISCREPANCY: #3 SLAT LOWER AFT SPAR BROKEN OUT SECTION AT ACTUATORCORRECTIVE ACTION: REPAIRED PER AWA ER 3-57-55-38ARECOMMENDATION: CLOSESDR SWAA991502Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 767, STRINGER 19L. REPAIRED SKIN PER SRM.SDR USAA990926Angle · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH FORWARD OF STATION 251 FRAME, RBL 16, WL 157 ALONG INBOARD ROW OF FASTENERS RIGHT LOWER CHORD ANGLE. CORROSION LEVEL 2. REPLACED RIGHT LOWER CHORD ANGLE IN NLG WHEEL WELL PER SRM 51-70-12 FIG 1SDR USAA990910Chord · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 270, RBL 2.5 - LBL 2.5 Z-CHORD. CORROSION LEVEL 1. REPAIRED REPLACEMENT 'Z' CHORD PER EA 65414 AND TR 53-20-04. (M)
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