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 USAA2011051791882Skin · delaminatedCLT - Q2 - DELAMINATION ON LEFT ELEVATOR TAB UPPER SKIN AT OUTBOARD HINGE CUTOUT AT ELEVATOR STA 121.79. REPLACED LEFT ELEVATOR TAB IAW JOB CARD 03C71127007.SDR USAA2011051791868Frame · crackedCLT - Q2 - 4 CRACKS IN FUSELAGE FRAME AT BS 380, S20L. REPAIRED FUSELAGE FRAME AT BS 380, S20L IAW EA 102958.SDR USAA2011051791875Skin · crackedCLT - Q2 - CRACK IN LEFT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF REAR SPAR AT ELEV STA 98. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF REAR SPAR AT ELEV STA 98 IAW EA 102935.SDR USAA2011051791872Tie Clip · crackedCLT - Q2 - CRACK IN STRINGER TIE CLIP AT BS 887, S8R. REPLACED STRINGER TIE CLIP AT BS 887, S8R IAW ENGINEERING JOB CARD E1C53005.SDR USAA2011051791879Tie Clip · crackedCLT - Q2 - CRACK IN STRINGER TIE CLIP AT BS 887, S3R. REPLACED STRINGER TIE CLIP AT BS 887, S3R IAW EA 102953.SDR USAA2011051791877Skin · crackedCLT - Q2 - CRACK IN FUSELAGE SKIN AT L1 LOWER DOOR SKIN HINGE CUTOUT AT BS 303.93 BETWEEN WL 238 TO WL 234. REPAIRED FUSELAGE SKIN AT L1 LOWER DOOR SKIN HINGE CUTOUT AT BS 303.93 BETWEEN WL 238 TO WL 234 IAW EA 102888.SDR USAA2011051791876Skin · crackedCLT - Q2 - CRACKS IN FUSELAGE SKIN AT L-1 UPPER DOOR HINGE CUTOUTS BS 303.93 BETWEEN WL 257 TO WL 261. REPAIRED FUSELAGE SKIN AT L-1 UPPER DOOR HINGE CUTOUTS BS 303.93 BETWEEN WL 257 TO WL 261 IAW EA 102888.SDR USAA2011051791870Attach Angle · crackedCLT - Q2 - CRACK IN INTERCOSTAL WEB ATTACH ANGLE AT BS 300 ABOVE S10L. REPLACED INTERCOSTAL WEB ATTACH ANGLE AT BS 300 ABOVE S10L IAW B737 SRM 51-10-02.SDR USAA2011051891892Frame · crackedCLT - Q2 - CRACK ON FRAME WEB DOUBLER AT BS 303.9, S16L. REPAIRED FRAME WEB DOUBLER AT BS 303.9, S16L IAW BOEING DRAWING 65-17684.SDR USAA2011051791871Frame · crackedCLT - Q2 - CRACK IN FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13.SDR USAA2011051791884Plate · corrodedCLT - Q2 - LEVEL 2 EXFOLIATION CORROSION ON FRAME SILL PLATE BETWEEN BS 807 TO BS 830, S25R. REPLACED FRAME SILL PLATE BETWEEN BS 807 TO BS 830, S25R IAW B737 SRM 51-40-02.SDR USAA2011051791880Frame Splice · crackedCLT - Q2 - CRACK IN FUSELAGE FRAME SPLICE AT BS 500 BETWEEN S13R TO S14R. REPAIRED FUSELAGE FRAME SPLICE AT BS 500 BETWEEN S13R TO S14R IAW EA 102918.SDR USAA2011051791881Frame · crackedCLT - Q2 - CRACK IN FUSELAGE FRAME AT BS 500B BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500B BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13.SDR USAA2011050291713Door Frame · crackedCLT - Q2 CHECK - CRACK ON THE AFT FRAME OF THE FORWARD SERVICE DOOR CUTOUT BETWEEN WL 240 TO WL 250. REPAIRED THE AFT FRAME OF THE FORWARD SERVICE DOOR CUTOUT BETWEEN WL 240 TO WL 250 IAW EA 102887.SDR USAA20110425SB061Tru · malfunctionedPBI - DURING FLIGHT, CREW REPORTED THE NR 1 TR CIRCUIT BREAKER POPPED (27 VOLTS/0 AMPS). MULTIPLE FAILURES OCCURRED INCLUDING AFT MAIN FUEL PUMP AND CAPTAIN'S STATIC 1 AUX PITOT STATIC. ON RETURN TO FIELD TO PBI, ALL FAILURES CLEARED. CIRCUIT BREAKER FOR NRSDR USAA2011050291714Frame · crackedCLT - Q2 CHECK - CRACK ON FRAME AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME AT BS 500B, BETWEEN STR 20R TO STR 21R IAW B737-400 SRM 53-00-07 AND BOEING SB 737-53A1279.SDR USAA2011051791885Flap Track · corrodedCLT - Q2 - LEVEL 2 INTERGRANULAR CORROSION ON RIGHT WING NR 6 FLAP TRACK UPPER & LOWER SURFACES. REPLACED RIGHT WING NR 6 FLAP TRACK IAW B737 AMM 54-51-01.SDR USAA2011050291717Tie Clip · crackedCLT - Q2 CHECK - CRACK ON STRINGER TIE CLIP AT BS 887, STR 2R. REPLACED STRINGER TIE CLIP AT BS 887, STR 2R IAW EO 5310-01047 AND TC E1C53005.SDR USAA2011050291716Tie Clip · crackedCLT - Q2 CHECK - CRACK ON STRINGER TIE CLIP AT BS 887, STR 1, BL 0. REPLACED STRINGER TIE CLIP AT BS 887, STR 1, BL 0 IAW EO 5310-01047, TC E1C53005.SDR USAA2011050291715Tie Clip · crackedCLT - Q2 CHECK - CRACK ON STRINGER TIE CLIP AT BS 807, STR 4R. REPLACED STRINGER TIE CLIP AT BS 807, STR 4R IAW EO 5310-01047.SDR USAA2011050291720Angle · corrodedCLT - Q2 CHECK - CORROSION ON Z-ANGLE AT BS 967, LBL 40. REPLACED Z-ANGLE AT BS 967, LBL 40 IAW B737-400 SRM 51-10-02.SDR USAA2011050291719Skin · crackedCLT - Q2 CHECK - CRACK ON FUSELAGE SKIN AT BS 727F PLUS 4 INCHES, STR 22R. REPAIRED FUSELAGE SKIN AT BS 727F PLUS 4 INCHES, STR 22R IAW B737-400 SRM 53-00-01, REPAIR 31.SDR USAA2011050291718Tie Clip · crackedCLT - Q2 CHECK - CRACK ON STRINGER TIE CLIP AT BS 727B, STR 9R. REPLACED STRINGER TIE CLIP AT BS 727B, STR 9R IAW EO 5310-01047 AND TC E1C53005.SDR USAA2011050291726Flap · corrodedCLT - Q2 CHECK - CORROSION ON RIGHT WING INBOARD FLAP ASSEMBLY AT WBL 235. REPLACED RIGHT WING INBOARD FLAP ASSEMBLY AT WBL 235 IAW B737-400 AMM 57-52-00.SDR USAA2011050291725Reveal · crackedCLT - Q2 CHECK - CRACK ON REVEAL AT BS 328, UPPER AFT CORNER OF FSD CUTOUT BETWEEN STR 7R AND 8R. REPLACED REVEAL AT BS 328, UPPER AFT CORNER OF FSD CUTOUT BETWEEN STR 7R AND 8R IAW B737-400 SRM 51-40-01.SDR USAA2011041991555Bulkhead · crackedCLT - Q2 CHECK - CRACKED BULKHEAD SKIN AT BS 178, WL 234, RBL 10.5. REPAIRED BULKHEAD SKIN AT BS 178, WL 234, RBL 10.5 IAW B737-400 SRM 53-10-08-2R-9.SDR USAA2011050291727Frame · crackedCLT - Q2 CHECK - CRACK ON FRAME AT BS 907, BETWEEN STR 8L TO 9L. REPAIRED FRAME AT BS 907, BETWEEN STR 8L TO 9L IAW EA 102739.SDR USAA2011041991548Tie Clip · crackedCLT - Q2 CHECK - CRACKED TIE CLIP AT BS 887, STR 6L. REPLACED TIE CLIP AT BS 887, STR 6L IAW EO 5310-01047.SDR USAA2011051791869Frame · crackedCLT - Q2 - CRACK IN FUSELAGE FRAME STUB BEAM AT BS 706, LBL 46. REPAIRED FUSELAGE FRAME STUB BEAM AT BS 706, LBL 46 IAW EA 102886.SDR USAA2011051791866Frame · crackedCLT - Q2 - CRACK ON FUSELAGE FRAME AT BS 787 BETWEEN S8R TO S9R. REPAIRED FUSELAGE FRAME AT BS 787 BETWEEN S8R TO S9R IAW EA 102903.SDR USAA2011041991549Tie Clip · crackedCLT - Q2 CHECK - CRACKED TIE CLIP AT BS 727D STR 5R. REPLACED TIE CLIP AT BS 887, STR 6L IAW EO EIC 53005.SDR USAA2011041991547Tie Clip · crackedCLT - Q2 CHECK - CRACKED TIE CLIP AT BS 706, STR 4R. REPLACED TIE CLIP AT BS 706, STR 4R IAW EO 5310-01047.SDR USAA2011041991546Web · crackedCLT - Q2 CHECK - CRACKED FLOOR WEB AT BS 178, STR 17L. REPAIRED CRACKED FLOOR WEB AT BS 178, STR 17L IAW B737-400 SRM 53-10-51.SDR USAA2011051791886Support · corrodedCLT - Q2 - LEVEL 2 EXFOLIATION CORROSION ON LEFT WING TRAILING EDGE INBOARD FLAP CARRIAGE SUPPORT ARM AT WS 250. REPLACED LEFT WING TRAILING EDGE INBOARD FLAP CARRIAGE SUPPORT ARM AT WS 250 IAW JOB CARD 03C30927012.SDR USAA2011041991550Frame · crackedCLT - Q2 CHECK - CRACKED FRAME INNER CHORD AT BS 616, STR 18L. REPAIRED FRAME INNER CHORD AT BS 616, STR 18L IAW TYPICAL REPAIR 737-5362-10-0023.SDR USAA2011041991551Skin · crackedCLT - Q2 CHECK - CRACKED SKIN AT BS 750, STR 21L. REPAIRED SKIN AT BS 750, STR 21L IAW B737-400 SRM 53-00-01 REPAIR 31.SDR USAA2011041991545Wedge · debondedCLT - Q2 CHECK - DISBONDED AREA ON LOWER SURFACE OF NR 5 SLAT TRAILING EDGE WEDGE. REPAIRED AREA ON LOWER SURFACE OF NR 5 SLAT TRAILING EDGE WEDGE IAW B737-400 SRM 57-43-02, 51-70-10.SDR USAA2011041991552Skin · crackedCLT - Q2 CHECK - CRACKED SKIN AT BS 727E + 14 INCHES, STR 23R. REPAIRED SKIN AT BS 727E + 14 INCHES, STR 23R IAW B737-400 SRM 53-00-01 REPAIR 31.SDR USAA2011050291728Intercostal · corrodedCLT - Q2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS 947, LBL 47. REPLACED INTERCOSTAL AT BS 947, LBL 47 IAW SRM 51-40-02.SDR USAA2011041991553Floor Support · corrodedCLT - Q2 CHECK - CORROSION ON FLOOR SUPPORT AT BS 306, RBL 12. REPLACED FLOOR SUPPORT AT BS 306, RBL 12 IAW B737-400 SRM 51-10-02.SDR USAA2011041291484Skin · crackedCLT - Q2 CHECK - LEFT WING NR 2 SLAT LOWER SKIN HAS 2 CRACKS, 31 INCHES TO 42 INCHES FROM THE INBOARD END AND 36 INCHES TO 41 INCHES FROM THE OUTBOARD END. REPAIRED LEFT WING NR 2 SLAT LOWER SKIN, 31 INCHES TO 42 INCHES FROM THE INBOARD END AND 36 INCHES TO 4SDR USAA2011041291483Tie Clip · crackedCLT - Q2 CHECK - CRACKED TIE CLIP AT BS 578, S4R. REPLACED TIE CLIP AT BS 578, S4R IAW 737 SRM 51-10-02.SDR USAA2011041291482Tie Clip · crackedCLT - Q2 CHECK - CRACKED TIE CLIP AT BS 578, S4R. REPLACED TIE CLIP AT BS 578, S4R IAW 737 SRM 51-10-02.SDR USAA2011051791883Shear Tie · corrodedCLT - Q2 - LEVEL 2 EXFOLIATION CORROSION ON FRAME SHEAR TIE AT BS 747 BETWEEN LBL 10 TO LBL 18. REPAIRED FRAME SHEAR TIE AT BS 747 BETWEEN LBL 10 TO LBL 18 IAW B737 SRM 53-00-07 REPAIR 4.SDR USAA2011041991554Angle · corrodedCLT - Q2 CHECK - CORROSION ON Z-ANGLE AT BS 967, ST 17R. REPLACED Z-ANGLE AT BS 967, ST 17R IAW B737-400 SRM 51-10-02.SDR USAA20110405SB049Seal · leakingCLT - DURING MAINTENANCE TEST FLIGHT FOR Q5 CHECK, STRONG FUMES FORWARD OF FIRST CLASS WERE REPORTED AS TAKEOFF THRUST WAS SET. FUMES WERE THAT OF A MUSTY SMELL. TURNED LEFT PACK OFF AND RETURNED TO CLT. FUMES CONTINUED UNTIL TOUCHDOWN. OPENED WINDOWS ONCESDR USAA2011040191316Rib · corrodedCLT - Q2 - CRACK ON RUDDER CLOSE OUT RIB AT STA 1127. REPLACED RUDDER CLOSE OUT RIB AT STA 1127 IAW B737 SRM 51-40-02 & EA 102809.SDR USAA2011033191299Frame · crackedCLT - Q5/QX6 - CRACK ON FRAME WEB AT BS 291, S10L. REPAIRED FRAME WEB AT BS 291, S10L IAW EA 102738.SDR USAA2011040191312Threshold · corrodedCLT - Q5 - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO THRESHOLD WEB AT BS 828, S26R. REPLACED AFT CARGO THRESHOLD WEB AT BS 828, S26R IAW B737 SRM 51-10-02 & BOEING DRAWING 65-47957.SDR USAA2011033191304Skin · delaminatedCLT - Q5/QX6 - DELAMINATION ON LEFT SIDE OF RUDDER 3 INCHES BELOW STA 174 & 7.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT SIDE OF RUDDER IAW EA 102811.
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