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 USAA2011081900036Skin · crackedQ3 CHECK - CRACK IN FUSELAGE SKIN AT MAIN ENTRY DOOR SKIN AT LOWER HINGE CUTOUT BS303.9 BETWEEN S13L TO S14L. REPAIRED FUSELAGE SKIN AT MAIN ENTRY DOOR SKIN AT LOWER HINGE CUTOUT IAW B737 SRM 53-10-01, REPAIR 14.SDR USAA2011071500016Skin · damagedQ4 CHECK - PREVIOUSLY BLENDED AREA OF FUSELAGE SKIN IS OUT OF LIMITS AT BS312, S24R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01 REP 31, FIG 201 DETAIL XII.SDR USAA2011071500029Trim Tab · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT ELEVATOR TRIM TAB MAST FITTING. REPLACED RIGHT ELEVATOR TRIM TAB IAW JOB CARD 03C71227004.SDR USAA2011071500013Trim Tab · crackedQ4 CHECK - 4 CRACKS ON LEFT ELEVATOR TRIM TAB 3 & 4 HINGE CUTOUTS. REPLACED LEFT ELEVATOR TRIM TAB IAW JOB CARD 03C71127007.SDR USAA2011071500015Skin · delaminatedQ4 CHECK - DELAMINATION ON LEFT ELEVATOR LOWER SKIN AT TAB CONTROL ROD CUTOUT. REPLACED LEFT ELEVATOR IAW JOB CARD 03C71127007.SDR USAA2011070700010Skin · crackedC1 CHECK - CRACK ON FUSELAGE SKIN AT BS767 + 6", STR24L. REPAIRED FUSELAGE SKIN AT BS 767 + 6", STR 24L IAW 737-400 SRM 53-00-01 REP 31 DETAIL XI.SDR USAA2011071200018Torque Shaft · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT INBOARD MID FLAP INBOARD TORQUE SHAFT. REPLACED RIGHT INBOARD MID FLAP IAW JOB CARD 03C40927012 & 03C40927009.SDR USAA2011070700009Skin · crackedC1 CHECK - CRACK ON FUSELAGE SKIN AT BS 747 + 6", STR 24L. REPAIRED FUSELAGE SKIN AT BS 747 + 6", STR 24L IAW B737-400 SRM 53-00-01 REP 31 FIG 201 DETAIL XIX.SDR USAA2011071200019Stiffener · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON VERTICAL STIFFENER AT BS 1124 BETWEEN S13L TO S17L AT APU INLET CUTOUT (INSIDE TORQUE BOX). REPLACED VERTICAL STIFFENER IAW B737 SRM 51-40-02, 51-10-02 & BOEING DRAWING 65-46579.SDR USAA2011071200015Skin · crackedQ4 CHECK - CRACK ON SKIN DOUBLER AT AIR CONDITIONING HOOK-UP CUTOUT AT BS 520 BETWEEN S28L TO S28R, BL 0. REPAIRED SKIN DOUBLER AT AIR CONDITIONING HOOK-UP CUT-OUT IAW EA 103155.SDR USAA2011071200014Frame · crackedQ4 CHECK - CRACK ON STUB FRAME INNER CHORD AT BS 616 BETWEEN S17R TO S18R. REPAIRED STUB FRAME INNER CHORD AT BS 616 BETWEEN S17R TO S18R IAW EA 103107 & TYPICAL REPAIR 737-5362-10-0023.SDR USAA2011070600019Flap · wornQ6 - LOOSE BUSHINGS INBOARD END ON CARRIAGE ATTACH POINT TRAILING EDGE OF LEFT OUTBOARD FOREFLAP. REPLACED LEFT OUTBOARD FOREFLAP IAW JOB CARD 03C30727030.SDR USAA2011063000007Sign · detachedFLT 739 - PHL-TPA - EEL - CREW REPORTED THE EMERGENCY EXIT SIGN HAS DETACHED FROM AIRCRAFT RIGHT BETWEEN THE TWO WINDOW EXITS. MAINTENANCE INSTALLED EXIT SIGN PROPERLY PER AMM 25-60-10.SDR USAA2011071200022Frame · crackedQ4 CHECK - CRACKS ON FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S23L. REPAIRED FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S23L IAW EA 103130.SDR USAA2011071200017Beam · crackedQ4 CHECK - CRACK IN FORWARD ENTRY DOOR AT AFT TRACE BEAM AT NR 11 & NR 12 STOP FITTING ACCESS HOLES. REPAIRED FORWARD ENTRY DOOR AT AFT TRACE BEAM AT NR 11 & NR 12 STOP FITTING ACCESS HOLES IAW EA 103142A.SDR USAA2011071200016Skin · crackedQ4 CHECK - CRACK IN FORWARD ENTRY DOOR SKIN AT AFT TRACE BEAM UNDER NR 6 STOP FITTING. REPAIRED FORWARD ENTRY DOOR SKIN AT AFT TRACE BEAM UNDER NR 6 STOP FITTING IAW EA 103142A.SDR USAA2011071200008Skin Panel · wornQ4 CHECK - WORN SKIN PANEL AT RIGHT STABILIZER HINGE JOINT AT BS 1142, STR 12R+ 6 INCHES. REPLACED SKIN PANEL AT RIGHT STABILIZER HINGE JOINT AT BS 1142, STR 12R+ 6 INCHES IAW B737 SRM 51-40-05, B737 SRM 51-40-08, BOEING DRAWING 65-48240.SDR USAA2011071200010Fastener · looseQ4 CHECK - APPROX 50 LOOSE & WORKING FASTENERS IN LEADING EDGE OF RIGHT OUTBOARD FORE FLAP SKIN. REPLACED RIGHT OUTBOARD FORE FLAP IAW JOB CARDS 03C40727020 & 03C40727016.SDR USAA2011071200011Skin · corrodedQ4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM COVER AT STAB STA 200. REPAIRED LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM COVER AT STAB STA 200 IAW B737 SRM 55-10-13 REPAIR 3.SDR USAA2011062400009Skin Panel · delaminatedCLT - C6 - 18 INCHES OE DELAMINATION ON UPPER & LOWER SURFACE OF RIGHT WING NR 5 SPOILER APPROX 5 INCHES FROM OUTBOARD END. REPLACED RIGHT WING NR 5 SPOILER IAW B737 AMM 27-62-12.SDR USAA2011062400008Skin · crackedCLT - C6 - 26 INCH LONG AREA OF LOOSE RIVETS & A CRACK ON LEFT WING OUTBOARD FOREFLAP SKIN ALONG LEADING EDGE. REPLACED LEFT WING OUTBOARD FORE FLAP IAW B737 AMM 27-51-37-404.SDR USAA2011070100032Support Tube · corrodedCLT - Q6 CHECK - CORROSION ON RIGHT WING INBOARD FLAP OUTBOARD CARRIAGE SUPPORT TUBE. REPLACED RIGHT WING INBOARD FLAP OUTBOARD CARRIAGE SUPPORT TUBE IAW TASK CARD 03C40927004.SDR USAA2011062300001Slide · unserviceableBFM - C3 - AFT ENTRY DOOR EVACUATION SLIDE NEEDS REPLACED DUE TO INFLATION TUBE KINKED. REPLACED AFT ENTRY DOOR EVACUATION SLIDE IAW JOB CARD 03C11052007.SDR USAA2011071200013Strap · crackedQ4 CHECK - CRACK ON STRAP BELOW LEFT HORIZONTAL STABILIZER AT BS 1183.6, RBBL 40. REPAIRED STRAP BELOW LEFT HORIZONTAL STABILIZER AT BS 1183.6, RBBL 40 IAW B737 SRM 53-00-01 FIG 201 REPAIR 22.SDR USAA2011070600017Skin · crackedQ6 CHECK - CRACK ON NR 2 PYLON SKIN AT PANEL 5828R, BETWEEN NAC STA 220 TO NAC STA 226, RBL 12. REPAIRED NR 2 PYLON SKIN AT PANEL 5828R, BETWEEN NAC STA 220 TO NAC STA 226, RBL 12 IAW TR 737-5430-10-0054.SDR USAA2011062300024Skin · crackedCLT - C6 - FUSELAGE SKIN CRACKED AT BS 727E + 3 INCHES, S24L. REPAIRED FUSELAGE SKIN AT BS 727E + 3 INCHES, S24L IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA2011062300023Skin · crackedCLT - C6 - FUSELAGE SKIN CRACKED AT BS 727D + 10 INCHES, S23R. REPAIRED FUSELAGE SKIN AT BS 727D + 10 INCHES, S23R IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA2011071200007Door Frame · crackedQ4 CHECK - CRACK IN FORWARD LEFT ENTRY DOOR FRAME WEB DOUBLER AT LOWER DOOR STOP FITTING AT BS 303.9, S16L. REPLACED FORWARD LEFT ENTRY DOOR FRAME WEB IAW EO 5311-01025.SDR USAA2011070100028Skin · crackedCLT - Q6 CHECK - TWO CRACKS IN UPPER HINGE CUTOUT OF FORWARD ENTRY DOOR SKIN AT BS 312, STR 15L. REPAIRED UPPER HINGE CUTOUT OF FORWARD ENTRY DOOR SKIN BS 312, STR 15L IAW EA 103104.SDR USAA20110622SB107Engine · bird ingestionMCO - CREW REPORTED A STRONG SMELL AFTER ROTATION. THE NR 1 ENGINE EGT MAXED OUT WITH RED LIGHT ILLUMINATING. PULLED THROTTLES BACK AND LIGHT WENT OUT. NO EGT INDICATION, LIGHT ON 4 TO 5 SECONDS. COMPLETED CHECKLIST AND SHUT DOWN THE NR 1 ENGINE. FLIGHT RESDR USAA2011071100005Skin · delaminatedQ4 CHECK - DELAMINATION ON NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END. REPAIRED NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END IAW EA 103090.SDR USAA2011071100006Fastener · looseQ4 CHECK - LOOSE FASTENERS ON LEFT OUTBOARD FOREFLAP BETWEEN WBL 202.60 TO WBL 414.40. REPLACED LEFT OUTBOARD FOREFLAP BETWEEN WBL 202.60 TO WBL 414.40 IAW JOB CARDS 03C30727030 AND 03C30727026.SDR USAA2011071100008Frame · crackedQ4 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME AT BS 500E, BETWEEN STR 20R TO STR 21R IAW B737 SRM 53-00-07 REPAIR 13.SDR USAA2011070600021Skin · crackedQ6 - CRACK ON FUSELAGE SKIN AT BS 303.9, WL 259.88. REPAIRED FUSELAGE SKIN AT BS 303.9, WL 259.88 IAW EA EA 1030022.SDR USAA2011070100031Frame · crackedCLT - Q6 - 3/16 INCH CRACK ON FRAME AT WIRE PENETRATION HOLE, BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME AT WIRE PENETRATION HOLE, BS 500B, BETWEEN STR 20L TO STR 21L IAW EA 103096, B737-300 SRM 53-00-07, REP 13.SDR USAA2011071100011Frame · crackedQ3 CHECK - CRACKS ON FRAME AT BS 500B, STR 20L. REPAIRED FRAME AT BS 500B, STR 20L IAW B737 SRM 53-00-07R13.SDR USAA2011062900015Frame · crackedCLT - Q6 CHECK - CRACK ON FRAME WEB AT BS 303.9, STR 16L. REPLACED FRAME WEB AT BS 303.9, STR 16L IAW EO 5311-01025.SDR USAA2011062900017Tie Clip · crackedCLT - Q6 CHECK - CRACK ON TIE CLIP AT BS 727E, STR 23R. REPLACED TIE CLIP AT BS 727E, STR 23R IAW B737-400 SRM 51-40-02.SDR USAA2011062900016Door Frame · crackedCLT - Q6 CHECK - CRACK ON FORWARD ENTRY DOOR AFT FRAME AT NR 6 STOP PIN. REPAIRED FORWARD ENTRY DOOR AFT FRAME AT NR 6 STOP PIN IAW EA 103086.SDR USAA20110616SB102Unknown · odorCLT - EN ROUTE FROM TPA TO CLT, AT FL290, FLIGHT ATTENDANT REPORTED A SMELL AND HAZE IN THE CABIN. BEGAN DESCENT TO FL270, SMELL AND HAZE STOPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED CABIN ODOR JOB CARD 03L00021001. DURING GROUSDR USAA2011071100003Angle · corrodedQ4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON Z-ANGLE AT BS 970, RBL 50. REPLACED Z-ANGLE AT BS 970, RBL 50 IAW B737 SRM 51-10-02.SDR USAA2011070600020Skin · crackedQ6 - CRACK ON FORWARD UPPER CORNER OF PYLON ACCESS (5724L) CUTOUT. REPAIRED FORWARD UPPER CORNER OF PYLON ACCESS (5724L) CUTOUT IAW EA 103051.SDR USAA2011062900014Frame · crackedCLT - Q6 CHECK - CRACK ON FRAME AT BS 360 BETWEEN STR 13R TO S14R. REPAIRED FRAME AT BS 360 BETWEEN STR 13R TO S14R IAW TYPICAL REPAIR 737-5310-10-0327.SDR USAA2011061400026Skin · crackedCLT - Q4 CHECK, CRACK ON AFT PRESSURE BULKHEAD SKIN AT BS 1016, STR 6R. REPAIRED AFT PRESSURE BULKHEAD SKIN AT BS 1016, STR 6R IAW B737-400 SRM 53-80-08 REPAIR 7.SDR USAA2011061400035Rivet · looseRIVETS WORKING LEADING EDGE CLT - Q6 - RIVETS WORKING AT LEADING EDGE OF RIGHT INBOARD FOREFLAP APPROX 12 INCHES FROM OUTBOARD EDGE.SDR USAA2011070100034Keelbeam · corrodedCLT - Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON KEEL BEAM AT BS 727G, RBL 7. REPAIRED KEEL BEAM AT BS 727G, RBL 7 IAW B737 SRM 51-20-01, 51-00-07, FIGURE 202, REPAIR 3.SDR USAA2011070100033Shear Tie · corrodedCLT - Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 747, RBL 7. REPAIRED SHEAR TIE AT BS 747, RBL 7 IAW B737 SRM 53-00-07, REPAIR 4.SDR USAA2011070100027Keelbeam · corrodedCLT - Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON KEEL BEAM AT BS 727F, RBL 7. REPAIRED KEEL BEAM AT BS 727F, RBL 7 IAW B737 SRM 53-00-07, REP 3.SDR USAA2011070100026Shear Tie · corrodedCLT - Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FRAME SHEAR TIE AT BS 727, RBL 7. REPAIRED FRAME SHEAR TIE AT BS 727, RBL 7 IAW B737-300 SRM 53-00-07, REP 3-10.SDR USAA2011061400032Stiffener · crackedCLT - Q6 - CRACK ON VERTICAL STIFFENER AT BS 328, RBL 32. REPLACED VERTICAL STIFFENER AT BS 328, RBL 32 IAW BOEING DRAWING 65-45812.
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