Boeing 737-4B7
Service difficulty reports · 5,757
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 = '7374B7' 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 = '7374B7' 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 USAA2009012290128Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME IS CRACKED AT BS 500A, BETWEEN S8R & S9R. REPAIRED FUSELAGE FRAME AT BS 500A, BETWEEN S8R & S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.SDR USAA2009012290127Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME IS CRACKED AT BS 827, BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 827, BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.SDR USAA2009012290126Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME HAS A .250 INCH CRACK AT BS 747, BETWEEN S8L & S9L, ALSO A .062 INCH CRACK AT BS 747, BETWEEN S8R & S9R. REPAIRED FUSELAGE FRAME AT BS 727 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-2SDR USAA2009012390148Angle · corrodedCLT - Q5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON AFT ENTRY DOOR ZEE ANGLE BETWEEN BS 975 TO BS 986, LBL 55. REPAIRED AFT ENTRY DOOR ZEE ANGLE BETWEEN BS 975 TO BS 986, LBL 55 IAW B737 SRM 51-70-11.SDR USAA2009020990307Door Frame · crackedCLT - Q5 MAJOR REPAIR - CRACK ON DOOR FRAME AT NR 6 STOP PIN ACCESS HOLE ON AFT SIDE AT MAIN ENTRY DOOR. REPAIRED DOOR FRAME AT NR 6 STOP PIN ACCESS HOLE ON AFT SIDE AT MAIN ENTRY DOOR IAW EA 100829.SDR USAA2009012290125Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME IS CRACKED AT BS 727D, BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 727D, BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.SDR USAA2009012390147Channel · corrodedCLT - Q5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON ZEE CHANNEL AT BS 991, RBL 50. REPLACED ZEE CHANNEL AT BS 991, RBL 50 IAW B737 SRM 53-60-51.SDR USAA2009012290124Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME HAS A .125 INCH CRACK AT BS 440, BETWEEN S8R & S9R. ALSO BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 440, BETWEEN S8R & S9R, ALSO BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.SDR USAA2009012290121Floorbeam · corrodedCLT - Q5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 328, LBL 28. REPAIRED FLOORBEAM T-CAP AT BS 328, LBL 28 IAW B737 SRM 53-10-51 REPAIR 5.SDR USAA2009012290120Floorbeam · corrodedCLT - Q5 - MAJOR REPAIRS - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 344, BL 0. REPAIRED FLOORBEAM T-CAP AT BS 344, BL 0 IAW B737 SRM 53-10-51 REPAIR 6.SDR USAASB09012Bottle · low pressureCLT MX REPORTED THE R1 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MX R&R THE R1 DOOR EMERGENCY ESCAPE SLIDE PER JOB CARD 03T10025002.SDR USAA2009011490075Skin · crackedCLT - RON - MAJOR REPAIR - LOG NR 4434973 & 03-0553-8-0361 - 3.5 INCH CRACK ON FUSELAGE SKIN AT BS727F, S26L. REPAIRED FUSELAGE SKIN AT BS727F, S26L IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA2009011290066Tee Fitting · crackedNR 03C21952009/001 AND 5031292 - CRACKED UPPER T CHORD INSIDE AFT CARGO DOOR, SECOND FROM TOP. REPLACED AFT CARGO DOOR IAW JOB CARD 03C2195008.SDR USAASB09009Battery · dischargedPILOT REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. MX REMOVED AND REPLACED THE BATTERY. OPS CHECK GOOD.SDR USAA2009010890050Skin · debondedCLT - C6 - MAJOR REPAIR - NR 03C40057003/022 - NR 8 SPOILER DELAMINATED ON UPPER SURFACE. REPLACED NR 8 SPOILER IAW B737 / AMM 27-62-91/501.SDR USAA2009010890049Flap · delaminatedCLT - C6 - MAJOR REPAIR - NR 03C30057003/024 - AREA OF DELAMINATION ON LT OTBD AFT FLAP AT INBD CORNER. REPAIRED LT OTBD AFT FLAP AT INBD CORNER IAW B737 SRM 51-70-10.SDR USAA2009010890053Wedge · delaminatedCLT - Q5 - MAJOR REPAIR - NR 03C30257009/002 - NR 2 SLAT DELAMINATED AT OTBD UPPER EDGE OF WEDGE. REPAIRED NR 2 SLAT IAW US AIRWAYS TYPICAL REPAIR NR 57-42-02.SDR USAASB09004Power Supply · dischargedORD MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR USAA2009010290002Skin · crackedCLT RON MAJOR REPAIR LOG NR 4434952. 2 1/4" CRACK IN FUSELAGE SKIN BETWEEN STA 727D & 727E AT STR 24R. VERIFIED CRACK AND MARKED ENDS USING HFEC INSP. REPAIRED FUSELAGE SKIN BETWEEN STA 727D & 727E AT STR 24R IAW B737 SRM 53-00-01 REPAIR 31.SDR USAASB08129Splice · defectiveORD MAINTENANCE REPORTED THE EMERGENCY EXIT PATH LIGHT AT ROW 19, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BAD SPLICE AT ROW 19, LEFT-HAND SIDE, PER SWPM 20-30-12. OPERATIONAL CHECK GOOD PER MM 33-51-12.SDR USAA2009010590025Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/009 & 03C20853011/010 CRACK ON FUSELAGE FRAME AT BS500E BETWEEN S20R & S21R, ALSO BETWEEN S20L & S21L. REPAIRED FUSELAGE FRAME AT BS500E BETWEEN S20R & S21R, ALSO BETWEEN S20L & S21L IAW B737 SRM 53-00-07 & US AIRWAY EA NR 1SDR USAA2009010590024Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/002 & 03C20853011/003 CRACK ON FUSELAGE FRAME AT BS500D BELOW S20L & S20R. REPAIRED FUSELAGE FRAME AT BS500D BELOW S20L & S20R IAW B737 SRM 53-00-07, US AIRWAYS EA NR 100790, & EA NR 100792.SDR USAA2009010590023Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/001 CRACK ON FUSELAGE FRAME AT BS500B BELOW S20L. REPAIRED FUSELAGE FRAME AT BS500B BELOW S20L IAW B737 SRM 53-00-07 & US AIRWAYS EA NR 100790.SDR USAA2009010290005Skin · delaminatedCLT Q5 MAJOR REPAIR NR 03C70827010/001 DELAMINATION ON RUDDER 3 INCHES ABOVE NR 4 HINGE ON RT SIDE. REPAIRED RUDDER ABOVE NR 4 HINGE ON RT SIDE IAW US AIRWAYS EA NR 100793.SDR USAA2009010290007Skin · crackedCLT Q5 MAJOR REPAIR NR 03C30257005/001 CRACKS IN NR 3 SLAT LOWER SKIN AT OTBD AUXILIARY TRACK. REPAIRED NR 3 SLAT LOWER SKIN IAW B737 SRM 57-43-01.SDR USAA2009012190105Wedge · delaminatedCLT - Q5 - MAJOR REPAIR - NR 2 SLAT DELAMINATED AT THE INBOARD END OF THE TRAILING EDGE WEDGE UPPER SURFACE. REPAIRED NR 2 SLAT AT THE INBOARD END OF THE TRAILING EDGE WEDGE UPPER SURFACE IAW B737 SRM 51-70-10.SDR USAA2009012190104Seal · crackedCLT - Q5 - MAJOR REPAIR - CRACK AT FORWARD SERVICE DOOR RAMP SEAL AT UPPER FORWARD CORNER. REPAIRED FORWARD SERVICE DOOR RAMP SEAL AT UPPER FORWARD CORNER IAW B737 SRM 53-10-15.SDR USAA2009010290008Stringer Splice · crackedCLT Q5 MAJOR REPAIR NR 03C10725040/001 STRINGER SPLICE CRACKED AT BS907, S4R. REPLACED STRINGER SPLICE AT BS907, S4R IAW B737 SRM 51-10-2.SDR USAA2008123192362Stringer Splice · crackedCLT Q5 MAJOR REPAIR NR 03C10725042/001 2 CRACKS IN STRINGER SPLICE AT BS907, S4L. REPLACED STRINGER SPLICE AT BS907, S4L IAW B737 SRM 51-10-2.SDR USAA2009010590027Bear Strap · crackedCLT - Q5 - MAJOR REPAIR - NR 03-0553-8-0550/002 & 5031233 - 3 CRACKS ON FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT IN SECOND LAYER AT BS303, WL236.68, .125, .250, & .400 INCHES LENGTH. REPAIRED FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT AT BS303, WL236.68 ISDR USAA2009010590022Intercostal · corrodedINTERGRANULAR CORROSION ON INTERCOSTAL BETWEEN BS 947 TO BS 967, S21R. REPAIRED INTERCOSTAL BETWEEN BS 947 TO BS 967, S21R IAW DRAWING 65-458562. UPON FURTHER REVIEW BY ENGINEERING, IT HAS BEEN DETERMINED THAT THIS IS NOT CLASSIFIED AS STRUCTURE REQUIRING CPSDR USAA2009010590029Angle · corrodedCLT - Q5 - MAJOR REPAIR - NR 03C10853029/004 - LEVEL 2 EXFOLIATION CORROSION ON Z ANGLE UPPER FLANGE AT L2 DOOR FROM BS967 TO BS987, LBL50. REPLACED Z ANGLE UPPER FLANGE AT L2 DOOR FROM BS967 TO BS987, LBL50 IAW B737 SRM 51-40-02.SDR USAA2009010590026Skin · crackedCLT Q5 MAJOR REPAIR NR 03-0553-8-0550/001 & 5031231 CRACK ON FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT IN SECOND LAYER AT BS312, BETWEEN S8L & S12L. REPAIRED L1 DOOR UPPER HINGE CUTOUT SKIN IAW B737 US AIRWAYS EA NR100772.SDR USAA2009010590021Floorbeam · corrodedCLT Q5 MAJOR REPAIR NR 03C10853057/002 LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS986.5, LBL11.5 TO LBL26.5. REPLACED FLOORBEAM AT BS986.5, LBL11.5 TO LBL26.5 IAW B737 SRM 51-40-02, 53-60-01 REV A & US AIRWAYS TYPICAL REPAIR NR 53-60-01.SDR USAA2009010590030Floor Support · corrodedEXFOLIATION CORROSION ON FLOOR SUPPORT ANGLE BETWEEN BS 967 TO BS 987, RBL 18. REPLACED FLOOR SUPPORT ANGLE BETWEEN BS 967 TO BS 987, RBL 18 IAW SRM 51-40-02. UPON FURTHER REVIEW BY ENGINEERING, IT HAS BEEN DETERMINED THAT THIS IS NOT CLASSIFIED AS STRUCTURESDR USAASB08124Transmitter · faultyON APPROACH TO CLT, FROM BDL, CREW REPORTED AN ASYMMETRICAL FLAP CONDITION BETWEEN 10 - 15 UNITS. NO ROLL DIFFICULTY OR CONTROL ISSUES NOTED. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED A GO-AROUND TO RESOLVE PROBLEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT SDR USAA2009010290009Skin · debondedCLT Q5 MAJOR REPAIR NR 03C30257009/005 NR 1 SLAT DISBONDED ON UPPER SURFACE AT WEDGE AREA. REPAIRED NR 1 SLAT IAW B737 SRM 57-43-02 & 51-70-10.SDR USAA2009010590031Angle · crackedCLT - Q5 - MAJOR REPAIR - NR 03C20353004/002 - CRACK ON ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R. REPAIRED ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R IAW B737 SRM 51-10-02.SDR USAA2009010590034Frame · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/004 - FUSELAGE FRAME CRACKED AT BS277, S16L. REPAIRED FUSELAGE FRAME AT BS277, S16L IAW B737 SRM 53-00-07.SDR USAA2009010590033Angle · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/002 - ANGLE CRACKED FORWARD OF R1 DOOR AT BS294.5, S17L. REPLACED ANGLE FORWARD OF R1 DOOR AT BS294.5, S17L IAW B737 SRM 51-40-02.SDR USAA2009010590032Stringer Clip · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/001 - STRINGER TIE CLIP CRACKED AT BS344, S11R. REPLACED STRINGER TIE CLIP AT BS344, S11R IAW B737 SRM 51-40-02.SDR USAA2009010290006Tab · delaminatedCLT Q5 MAJOR REPAIR NR 03C40627011/002 RT AILERON TAB SEPARATED AT OTBD END. REPLACED RT AILERON TAB & INSTALLED ON US AIRWAYS TASK CARD NR 03C40627010.SDR USAA2009010590036Strap · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/007 - CRACK ON L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L. REPLACED L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L IAW B737 SRM 51-10-02.SDR USAA2009010590035Door Frame · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/006 - CRACK IN R1 DOOR FRAME AT BS294.5, BETWEEN S6R & S7R. REPAIRED R1 DOOR FRAME AT BS294.5, BETWEEN S6R & S7R IAW B737 SRM 51-70-11.SDR USAA2009010590028Floorbeam · corrodedCLT - Q5 - MAJOR REPAIR - NR 03C10753060/011 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS312, RBL13 & RBL30. REPAIRED FLOORBEAM AT BS312, RBL13 & RBL30 IAW B737 SRM 53-10-51.SDR USAA2008121992278Angle · crackedCLT - Q5 - MAJOR REPAIR - ANGLE CRACKED AT BS 294, BETWEEN S11R & S12R FORWARD OF R2 DOOR. REPLACED ANGLE AT BS 294, BETWEEN S11R & S12R FORWARD OF R2 DOOR IAW B737 SRM 51-10-02.SDR USAA2008121992277Frame · crackedCLT - Q5 - MAJOR REPAIR - FRAME WEB CRACKED AT BS 328, LBL 50. REPLACED FRAME WEB AT BS 328, LBL 50 IAW SRM 51-40-02.SDR USAA2008121992276Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 747, BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 747, BETWEEN S8L & S9L TYPICAL REPAIR 53-10-20E.SDR USAA2008121992275Skin · crackedCLT - Q5 - MAJOR REPAIR - NR 1 SLAT SKIN CRACKED AT RIVET HOLES AT INBOARD AUXILIARY TRACK. REPAIRED NR 1 SLAT SKIN IAW SRM 57-43-01.SDR USAA2008121992274Strap · crackedCLT - Q5 - MAJOR REPAIR - LOWER STABILIZER STRAP CRACKED AT BS 344, LBL 44. REPLACED LOWER STABILIZER STRAP AT BS 344, LBL 44 IAW SRM 51-10-02 & DRAWING 65-45834.
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