Boeing 737-401
Service difficulty reports · 2,961
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 = '737401' 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 = '737401' 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 USAA2011071100012Hinge Fitting · wornQ4 CHECK - WORN HINGE FITTING ON ELEVATOR HINGE LINE AT STABILIZER STATION 258. REPLACED HINGE FITTING ON ELEVATOR HINGE LINE AT STABILIZER STATION 258 IAW B737 SRM 51-40-02, BAC DRAWING 65C25144.SDR USAA2011061400031Frame · crackedCLT - Q6 - CRACK ON FRAME AT VERTICAL SHELF AT BS 1112 FROM INSIDE HORIZONTAL STAB TORQUE BOX AREA. REPAIRED FRAME AT VERTICAL SHELF AT BS 1112 IAW B737 SRM 51-70-11.SDR USAA2011070600018Skin · crackedQ6 CHECK - CRACK ON NR 2 PYLON SKIN AT RIGHT ACCESS PANEL, NAC STA 240. REPAIRED NR 2 PYLON SKIN AT RIGHT ACCESS PANEL, NAC STA 240 IAW EA 103063.SDR USAA2011061400024Frame · crackedCLT - Q4 CHECK - CRACK ON FRAME AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME AT BS 500B, BETWEEN STR 19R TO STR 22R IAW B737-400 SRM 53-00-07, REPAIR 13.SDR USAA2011061500016Frame · crackedQ6 - CRACK ON FRAME AT VERTICAL SHELF AT BS 1112 FROM INSIDE HORIZONTAL STAB TORQUE BOX AREA. REPAIRED FRAME AT VERTICAL SHELF AT BS 1112 IAW B737 SRM 51-70-11.SDR USAA2011061400030Frame · crackedCLT - Q6 - CRACK IN FUSELAGE FRAME AT BS 500E BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500E BETWEEN S20R TO S21R IAW B737 SRM 53-00-07.SDR USAA2011062900018Frame · crackedCLT - Q6 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN STR 20L AND S21L. REPAIRED FRAME AT BS 500E, BETWEEN STR 20L AND S21L IAW B737-400 SRM 53-00-07 REPAIR 13.SDR USAA2011061400029Frame · crackedCLT - Q6 - 3/16" CRACK IN FWD SIDE OF FRAME IN PENETRATION HOLE AND 3/16" HOLE IN FRAME ANGLE AT BS 500C BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM SRM 53-00-07.SDR USAA2011071500028Angle · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON APU INLET TORQUE BOX ANGLE BETWEEN BS 1114 TO BS 1120. REPAIRED APU INLET TORQUE BOX ANGLE BETWEEN BS 1114 TO BS 1120 IAW EA 103102.SDR USAA2011071200012Threshold · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO LOWER SILL THRESHOLD WEB BETWEEN BS 807 TO BS 827+10 INCHES, RBL 27.5. REPLACED AFT CARGO LOWER SILL THRESHOLD WEB IAW B737 SRM 53-60-15 FIG 101 DETAIL L VIIL.SDR USAA2011070600022Shear Tie · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 847, BETWEEN STR 26R TO 27R. REPAIRED SHEAR TIE AT BS 847, BETWEEN STR 26R TO 27R IAW EA 103071.SDR USAA2011071800021Angle · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON ZEE ANGLE BETWEEN BS 767 TO BS 794, RBL 22. REPLACED ZEE ANGLE BETWEEN BS 767 TO BS 794, RBL 22 IAW B737 SRM 51-10-02.SDR USAA2011071500014Seat Track · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOOR TRACK BEAM AT BS 727F, RBL 13.8. REPLACED AFT CARGO FLOOR TRACK BEAM AT BS 727F, RBL 13.8 IAW B737 SRM 53-00-53 REPAIR 2.SDR USAA2011071200021Doubler · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON IFPC ANTENNA DOUBLER AT BS 754, BL 0. REPLACED IFPC ANTENNA DOUBLER AT BS 754, BL 0 IAW EA 103188.SDR USAA2011070100030Frame · crackedCLT - Q6 - CRACK ON FRAME AT BS500F BETWEEN STR 8R TO STR 9R. REPAIRED FRAME AT BS 500F BETWEEN STR 8R TO STR 9R IAW EA103054.SDR USAA2011061400023Tie Clip · corrodedCLT - Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER TIE CLIP AT BS 323, STR 28R. REPAIRED STRINGER TIE CLIP AT BS 323, STR 28R IAW B737-400 SRM 53-00-03 REPAIR 1.SDR USAA2011071100007Angle · corrodedQ4 CHECK - WIDESPREAD EXFOLIATION CORROSION ON Z ANGLE BETWEEN BS 294.5 TO BS 390, LBL 56. REPLACED Z ANGLE BETWEEN BS 294.5 TO BS 390, LBL 56.SDR USAA2011071100004Structure · corrodedQ4 CHECK - EXFOLIATION CORROSION ON PREVIOUSLY BLENDED UPPER CHORD TCAP AT BS 334, WL 208, BETWEEN LBL 33 TO RBL 68. REPLACED UPPER CHORD TCAP AT BS 334, WL 208, BETWEEN LBL 33 TO RBL 68 IAW B737 SRM 53-10-51, FIG 201, REPAIR 5.SDR USAA2011071200009Bracket · corrodedQ4 CHECK - EXFOLIATION CORROSION ON AFT FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56. REPLACED AFT FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56 IAW B737 SRM 51-10-02.SDR USAA2011071100009Bracket · corrodedQ4 CHECK - EXFOLIATION CORROSION ON FORWARD FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56. REPLACED FORWARD FLOOR GIRT BAR BRACKETS BETWEEN BS 312 TO BS 340, LBL 56 IAW B737 SRM 51-10-02.SDR USAA2011061500013Shear Tie · corrodedCLT - Q6 - CORROSION ON SHEAR TIE FLANGE AT BS 807, LBL 5. REPAIRED SHEAR TIE FLANGE AT BS 807, LBL 5 IAW EA 103083.SDR USAA20110601SB083Connector · disconnectedFLL - THE EMERGENCY LOW LEVEL LIGHTS WERE INOPERATIVE AT SEAT 12-13. MAINTENANCE RESECURED CONNECTIONS TO THE EMERGENCY LIGHTS FOR SEATS 12-13. OPERATIONALLY CHECKS OK.SDR USAA2011071200020Shear Tie · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE ATTACH ANGLE AT BS947 BETWEEN S26L TO S27L. REPAIRED SHEAR TIE ATTACH ANGLE IAW B737 SRM 53-00-07 REPAIR 5 & BOEING DRAWING 65-46560.SDR USAA2011071100002Shear Tie · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 947, BETWEEN STR 19L TO STR 20L. REPLACED SHEAR TIE AT BS 947, BETWEEN STR 19L TO STR 20L IAW B737 SRM 51-10-02 AND BOEING DRAWING 65-46560.SDR USAA2011071800022Shear Tie · corrodedQ4 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR TIE BETWEEN BS 1026 TO BS 1031, RBL 7. REPAIRED SHEAR TIE BETWEEN BS 1026 TO BS 1031, RBL 7 IAW SRM 51-70-13-04.SDR USAA2011071100010Floorbeam · corrodedQ4 CHECK - EXFOLIATION CORROSION ON PREVIOUSLY BLENDED FLOORBEAM T-CAP AT BS 986, BL-9. REPLACED FLOORBEAM T-CAP AT BS 986, BL-9 IAW B737 SRM 51-10-02, BOEING DRAWING 69C5346117.SDR USAA2011061400025Floorbeam · corrodedCLT - Q4 CHECK - CORROSION ON FLOORBEAM AT BS 967, RBL 18. REPAIRED FLOORBEAM AT BS 967, RBL 18 IAW B737-400 SRM 53-60-51 FIG 201.SDR USAA2011061500012Skin · crackedCLT - Q6 - CRACK IN FUSELAGE SKIN AT BS 984, S25R. REPAIRED FUSELAGE SKIN AT BS 984, S25R IAW B737 SRM 53-00-01, REP 31.SDR USAA2011061500011Stringer · crackedCLT - Q6 - CRACK IN STRINGER CHANNEL AT BS 360, S15L. REPLACED STRINGER CHANNEL AT BS 360, S15L IAW B737 SRM 51-10-02.SDR USAA2011061500008Skin · delaminatedCLT - Q6 - DELAMINATION ON NR 2 SLAT TRAILING EDGE WEDGE UPPER SURFACE 2 INCHES INBOARD OF OUTBOARD END. REPLACED NR 2 SLAT IAW JOB CARD 03C40227004.SDR USAA2011061500010Skin · debondedCLT - Q6 - DISBOND ON RIGHT WING NR 5 SLAT TRAILING EDGE LOWER SURFACE APPROX 1.5 INCHES FROM INBOARD END OF SLAT. REPLACED RIGHT WING NR 5 SLAT IAW B737 AMM 57-54-00.SDR USAA2011061500009Skin · crackedCLT - Q6 - CRACK IN FUSELAGE SKIN AT 727F +8 INCHES, S22L. REPAIRED FUSELAGE SKIN AT 727F +8 INCHES, S22L IAW B737 SRM 53-00-01, REP 31.SDR USAA2011061400028Angle · corrodedCLT - Q6 - LEVEL 2 WIDE SPREAD EXFOLIATION CORROSION ON AFT ENTRY ZEE ANGLE BETWEEN BS 887 TO 1016, S17L. REPLACED AFT ENTRY ZEE ANGLE BETWEEN BS 887 TO 1016, S17L IAW B737 SRM 53-60-15.SDR USAA2011061500007Skin · debondedCLT - Q6 - DISBOND ON NR 4 SLAT TRAILING EDGE WEDGE UPPER & LOWER SURFACES APPROX 1.5 INCHES FROM OUTBOARD END. REPAIRED NR 4 SLAT TRAILING EDGE WEDGE IAW B737 NR 4 SRM 57-70-10.SDR USAA20110523SB080Rod End · brokenTPA - CREW REPORTED THE FORWARD MAIN ENTRY DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR GUIDE ARM ROD END. OPERATIONAL CHECK NORMAL PER MM 52-11-21.SDR USAA2011070100029Web · corrodedCLT - Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON THRESHOLD SUPPORT WEB AT BS 807, STR 25R. REPLACED THRESHOLD SUPPORT WEB AT BS 807, STR 25R IAW B737 SRM 51-40-02, 51-10-02, BOEING DRAWING 65-47957.SDR USAA2011070600023Floorbeam · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 312, RBL 20.5. REPAIRED FLOORBEAM AT BS 312, RBL 20.5 IAW B737 SRM 53-10-51.SDR USAA2011052400003Hinge Pin · corroded.LEVEL 2 EXFOLIATION CORROSION ON LEFT HORIZONTAL STAB INNER HINGE PIN AT BS1138. REPLACED LEFT HORIZONTAL STAB INNER HINGE PIN IAW JOB CARD 03T70927002.SDR USAA2011052400002Hinge Pin · corrodedLEVEL 2 EXFOLIATION CORROSION ON RIGHT HORIZONTAL STABILIZER INNER HINGE PIN AT BS 1138. REPLACED RIGHT HORIZONTAL STABILIZER INNER PIN IAW JOB CARD 03T71027003.SDR USAA20110518SB078Door · lack of lubeCLT - FLIGHT ATTENDANT REPORTED THE FORWARD MAIN ENTRY DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE FORWARD MAIN ENTRY DOOR, INCLUDING THE GUIDE ARM. DOOR OPERATES GOOD IN ASSOCIATION WITH MM 52-11 AND 52-11-21-4.SDR USAA2011052400005Fitting · crackedCRACK ON EAR OF RIGHT ELEVATOR TAB MAST FITTING AT ELEV STA 32. REPLACED RIGHT ELEVATOR TAB IAW JOB CARD 03C71227004 & AMM 27-31-31.SDR USAA2011052400001Door Frame · crackedA .5 INCH CRACK ON FORWARD SERVICE DOOR FRAME AT BS 318, S15L. REPAIRED FORWARD SERVICE DOOR FRAME AT BS 318, S15L IAW EA 102887.SDR USAA2011051791873Slat · crackedCLT - Q2 - CRACK IN NR 1 SLAT AT RIVET AT INBOARD AUXILLARY ARM AT SS 283.80. REPLACED NR 1 SLAT IAW JOB CARD 03C30227005.SDR USAA2011051891891Torque Box · corrodedCLT - Q2 - LEVEL 2 FRETTING CORROSION ON APU TORQUE BOX INLET AT BS 1121 RIGHT SIDE. REPAIRED APU TORQUE BOX INLET AT BS 1121 RIGHT SIDE IAW EA 102942.SDR USAA2011051791878Bulkhead · crackedCLT - Q2 - CRACKS IN BS 178 FORWARD PRESSURE BULKHEAD AT WL 219, LBL 7. REPLACED BS 178 FORWARD PRESSURE BULKHEAD CENTER WEB SECTION IAW EA 102936.SDR USAA2011051791874Support Fitting · crackedCLT - Q2 - CRACK IN LEFT MAIN LANDING GEAR AFT SUPPORT FITTING AT WS 135.5. REPAIRED LEFT MAIN LANDING GEAR AFT SUPPORT FITTING AT WS 135.5 IAW TYPICAL REPAIR 737-5715-10-0313.SDR USAA2011052400004Tube · crackedANTI-ICE SPRAY TUBE IS CRACKED INSIDE OF NR 4 SLAT LEADING EDGE AT INBOARD CUTOUT. REPLACED NR 4 SLAT IAW B737 AMM 27-81-21-4.SDR USAA2011051791867Skin · crackedCLT - Q2 - CRACK IN FUSELAGE SKIN AT BS 444 APPROX 9 INCHES ABOVE S25R. REPAIRED FUSELAGE SKIN AT BS 444 APPROX 9 INCHES ABOVE S25R IAW B737 SRM 53-00-01 REPAIR 32 & EA 102913.SDR USAA20110510SB074Csd · leakingCLT - CREW REPORTED A STRANGE ODOR (DIRTY SOCK SMELL) IN COCKPIT AND CABIN DURING LAST 30 MINUTES OF FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED BOROSCOPE OF BOTH ENGINES AND TROUBLESHOOTING TASK CARD 03L00021001 CABIN ODOR CHECKSDR USAA2011051891890Angle · corrodedCLT - Q2 - LEVEL 2 INTERGRANULAR CORROSION ON Z-ANGLE BETWEEN BS 344 TO BS 380, S17L. REPLACED Z-ANGLE BETWEEN BS 344 TO BS 380, S17L IAW B737 SRM 51-10-02.
Back to Boeing 737-401