Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAA050991Stringer Splice · crackedCLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K)SDR USAA050992Frame · crackedCLT, Q6 FRAME, 1.4 INCH CRACK, BS 616 RT BOTTOM OF FRAME INNER CHORD BS 616 RT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW TR 53-62-01. (K)SDR USAA050993Frame · crackedCLT, Q6, FRAME .125 INCH CRACK, STRINGER 9 LT STA 500A. REPAIRED IAW TR 53-10-20B. (K)SDR AWXA200500919Battery · lowPHX - EEL - DURING 4 DAY CHECK, THE EXTERIOR EMERGENCY ESCAPE LIGHT AT L2 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY ABOVE AFT GALLEY IAW BOEING 737-300 AMM 33-51-51-201. POWER SUPPLY; RADIANT ILLUM; PN 100865, SN UNK; INSDR SB05088Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE FORWARDED EMERGENCY LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA050984Beam · crackedCLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K)SDR USAA050973Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 8R AT STATION 500. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-03. (M)SDR USAA050972Crease Beam · crackedCLT - FOUND CREASE BEAM CRACKED .75 INCH, BS 576, S17R. REPLACED WITH FACTORY NEW PART IAW SRM 51-10-02. (M)SDR USAA050968Clevis · corrodedCLT - FOUND ATTACH CLEVIS CORRODED 2 INCHES DIAMETER BY .015 TYPICAL, RIGHT HORIZ STAB FORWARD SPAR ATTACH CLEVIS AFT FACE. REMOVED CORROSION AND BUSHED IAW 55-10-10. (M)SDR USAA050969Attach Fitting · corrodedCLT - FOUND STAB LUG CORRODED, R1 LUG AFT FACE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10. (M)SDR USAA050967Attach Angle · wornCLT - FOUND ATTACH ANGLE CRACKED 1 INCH DIAMETER, WORN AREAS, RT WHEEL WELL STATION 727 RBL 14 BOTTOM OF BULKHEAD. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DWG 65-48689 AND SRM 51-10-02 AND 51-40-02. (M)SDR USAA050966Web · crackedCLT - FOUND WEB CRACKED 2 INCHES, AFT CARGO DOOR CUTOUT FRAME, LOWER WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-20723 AND SRM 51-10-02. (M)SDR USAA050965Angle · corrodedCLT - FOUND C-ANGLE CORRODED 2 INCHES, UPPER SURFACE OF FORWARD ENTRY DOOR THRESHOLD C-ANGLE. REMOVED DAMAGED ANGLE AND REINSTALLED NEW ANGLE IAW SRM 53-10-15. (M)SDR USAA050964Floorbeam · corrodedCLT - FOUND BEAM CORRODED 28 INCHES, T-CAP OF FLOORBEAM STATION 312, LBL 2, RBL 26. REMOVED PREVIOUS T-CAP AND REPLACED WITH NEW CAP EXTENDING SPLICES PER SRM IAW SRM 53-10-51. (M)SDR USAA050963Stringer Clip · crackedCLT - FOUND STRINGER TIE CRACKED .25 INCH, BS 847, STRINGER 4R. REMOVED CRACKED TIE, BS 847, STRINGER 4R. REMOVED CRACKED TIE CLIP AND INSTALLED NEW CLIP IAW SRM 51-10-02 AND 51-40-02. (M)SDR USAA050962Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 327, BL 0, CABIN FLOOR STRUCTURE. REMOVED CRACKED STRAP AND REPLACE WITH NEW FROM STOCK IAW SRM 51-10-02 AND 51-40-02. (M)SDR USAA050948Bushing · corrodedCLT - Q6 - LUG/BUSHING, CORROSION, L6 LUG, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR USAA050947Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L3, AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)SDR USAA050941Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK. L5, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR USAA050961Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 326, LBL 11. DEF PART REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 AND 51-40-02. (M)SDR USAA050960Floorbeam · corrodedCLT - FOUND BEAM T-CAP CORRODED 6 INCHES, STATION 360, RBL 55 - RBL 61. REMOVED DAMAGED METAL, INSTALLED NEW T-CAP FROM RBL 35 - RBL 72 IAW SRM 53-00-51. (M)SDR USAA050959Stiffener · corrodedCLT - FOUND STIFFENER CORRODED .5 INCHES BY 6 INCHES, STRINGER 26R BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION ATTACH FITTING AND STIFFENER IAW SRM 53-60-03 AND 51-10-02. (M)SDR USAA050958Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCH BY .015 INCH, FORWARD SPAR ATTACH LUG AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM 55-10-10. (M)SDR USAA050957Skin · crackedCLT - FOUND PYLON SKIN CRACKED 2 INCHES, RT ENGINE PYLON UNDER PANEL 5858. REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER IAW TR 57-41-02. (M)SDR USAA050943Lug · corrodedCLT - Q6 - LUGS, CORROSION; NO LEVEL OR TASK, L2/L5 BORES, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHINGS IAW SRM. (K)SDR USAA050942Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L5, AFT FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR USAA050956Floorbeam · corrodedCLT - FOUND FLOORBEAM UPPER CHORD CORRODED 1 INCH BY 1 INCH, BS 344 BETWEEN LBL 55 - RBL 13. REMOVED UPPER CHORD OF FLOORBEAM. INSTALLED NEW CHORD AND ASSOCIATED REPAIR SPLICES IAW SRM 53-10-51. (M)SDR USAA0540944Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L2, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR USAA050955Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 3 INCHES, STATION 312 AND 394.5 ATL LBL 12. REMOVED PART, FABRICATED NEW AND INSTALLED IAW SRM 51-10-02. (M)SDR USAA050954Beam · corrodedCLT - FOUND BEAM CORRODED 6 INCHES, STATION 986, EXTREME RT END. REPLACED T-CAP IAW TR 53-60-05B. (M)SDR USAA050945Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, LT,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR USAA050946Bushing · corrodedCLT - Q6 -LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L1,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)SDR USAA050953Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCHES BY .015 TYPICAL, LT STAB CENTER SECTION FORWARD LOWER LUG. REMOVED CORROSION, FABRICATED NEW BUSHING. (M)SDR USAA050952Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCH DIAMETER BY .015 TYPICAL, L3, FORWRD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)SDR USAA050951Bushing · corrodedCLT - BUSHING CORRODED, L1, FORWARD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)SDR USAA050950Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCHES IN DIAMETER BY .015 TYPICAL, L6, AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)SDR USAA050949Bushing · corrodedCLT - FOUND CORROSION ON LUG/BUSHING 2 INCHES BY .015, LEFT STAB, FORWARD LOWER LUG LEFT HORIZ STABILIZER. OVERSIZED LUG, FABRICATED NEW BUSHING IAW SRM 55-10-10. (M)SDR USAA050971Skin · crackedCLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K)SDR USAA200508001Skin · cracked1/2" CRACK AT AFT CARGO DOOR LOWER FWD CORNER OF OUTER SKIN, REPAIR: INSTALLED FILLER, DOUBLER, TRIPLER PER EA 96770.SDR USAA200507005Skin · delaminated3 INCH BY 4 INCH AREA OF DELAMINATION ON TRAILING EDGE OF TAB, 18 INCH FROM OUTBOARD END. WET COMPOSITE LAYUP PER SRM 51-70-16.SDR USAA050906Stiffener · corrodedCLT - Q6 - STIFFENER, .5 INCH X 6 INCH CORROSION; NO LEVEL OR TASK. STR 26R, BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION, ATTACH FITTING AND STIFFENER IAW SRM. (K)SDR SB05083Battery Pack · dischargedPVD MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA050884Skin · crackedCLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)SDR USAA050880Flange · wornCLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)SDR USAA200507004Skin · cracked5 IN CRACK FOUND BETWEEN FRAME 727D AND 727E STR 24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229.SDR USAA200507003Frame · cracked1.5 IN CRACK FOUND AT FRAME 767, STR 24L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229.SDR USAA200507001Skin · crackedCRACK AT BS 767 BETWEEN STRINGERS 21 RT AND 22 RT ON FUSELAGE SKIN. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229, DETAIL X.SDR USAA050852Skin · crackedCLT - FOUND SKIN CRACKED 1.75 INCH, FS 745 AT STRINGER 24L. INSTALLED REPAIRED DOUBLER IAW SRM 53-00-01 DETAIL XI. (M)SDR USAA050848Skin · crackedCLT - FOUND SKIN CRACKED 1.3 INCH, MAIN ENTRY LOWER HINGE CUTOUT AT LOWER RADIUS. INSTALLED DOUBLER IAW TYPICAL REPAIR NR 52-10-12. (M)SDR USAA050849Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT ON THE SKIN. INSTALLED DOUBLER IAW EA 96719. (M)
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