Boeing 737-3Y0
Service difficulty reports · 3,007
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 = '7373Y0' 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 = '7373Y0' 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 SWAA2012042003290Skin · crackedFUSELAGE SKIN CRACKED AT STA 500C+5 ABOVE STR 15R. REPAIRED PER EA.SDR SWAA2012040202783Skin · crackedFUSELAGE SKIN CRACKED AT BS 500C + 5, STR 15R. REPAIRED SKIN PER SRM.SDR SWAA2012040202746Skin · crackedCHEM MILL FUSELAGE SKIN CRACKED BS 396, STR 15L. REPAIRED SKIN IAW ATS ER AND EA.SDR SWAA2012032602555Lens · missingRIGHT OVERWING EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED SIGN ASSY PER MM.SDR SWAA2012031602259Controller · faultyDECLARED EMERGENCY - CABIN ALT HORN SOUNDED. AUTO CONTROL INOP. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM.SDR SWAA2012030902065Shutoff Valve · leakingAIR TURNBACK - ON INITIAL CLIMBOUT LOSS OF ALL OF A SYSTEM HYD FLUID FIRST INDICATION WAS THE STBY RUDDER LIGHT FOLLOWED BY THE A SYSTEM ENGINE PUMP LOW PRESS LIGHT AND THE A SYSTEM ELEC PUMP LOW PRESS LIGHT. NORMAL LANDING NORMAL BRAKING. LANDING WT 113,500SDR SWAA2012022401739Flap · delaminatedRT WING O/B FORE FLAP I/B END DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA2012022401738Lens · looseRT BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 12. SECURED LENS PER M/M.SDR SWAA2012022401737Lens · looseLT BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 13. SECURED LENS PER M/M.SDR SWAA2012021501478Frame · crackedFRAME CRACKED AT 500C, STR 21R. REPAIRED FRAME PER SRM.SDR SWAA2012021501481Frame · crackedFRAME CRACKED AT BS 500C ON I/B RIGHT SIDE. REPAIRED FRAME PER SRM.SDR SWAA201201249Shear Tie · corrodedAFT CARGO COMPARTMENT STATION 727E RBL 7 SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM.SDR SWAA201201215Shear Tie · corrodedAFT CARGO COMPARTMENT STATION 787 RBL 9 SHEAR TIE HAS CORROSION ON AFT SIDE. REMOVED AND REPLACED SHEAR TIE IAW SRM AND AMM.SDR SWAA1201184Channel · corrodedFORWARD PIT STA, 500B+11 TO 500D, LBL 24, Z-CHANNEL LOWER SURFACE, CORROSION AROUND 6 EACH FASTENER HOLES. REMOVED AND REPLACED Z-CHANNEL IAW SRM.SDR SWAA1201183Angle · corrodedAFT CARGO COMPARTMENT STATION 727C-767 RT Z-ANGLE HAS CORROSION ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG AND AMM.SDR SWAA120678Compressor · damagedAIR TURNBACK/DECLARED EMERGENCY. ON DEPARTURE FROM LAS NR 1 ENGINE COMPRESS STALL RIGHT AFTER LIFT OFF. FOUND 9TH STAGE BLADES HAVE OUT OF LIMITS DAMAGE. REMOVED AND REPLACED NR 1 ENGINE PER MT.SDR USAA2012012400002Sign · damagedC21 CHECK - AFT CLOSET LOWER EXIT SIGN DAMAGED. REPLACED AFT CLOSET LOWER EXIT SIGN AS NEEDED.SDR USAA2012013000005Skin · crackedC21 CHECK - 1.7 INCH CRACK IN FUSELAGE SKIN AT BS 874, S25R. REPAIRED FUSELAGE SKIN AT BS 874, S25R IAW B737 SRM 53-00-01-2R-31 FIG 201.SDR USAA2012013000007Door Frame · crackedC21 CHECK - .250 INCH LONG CRACK IN L1 DOOR AFT DOOR FRAME AT NR 6 STOP FITTING AT BS 344, WL 255. REPAIRED L1 DOOR AFT DOOR FRAME AT NR 6 STOP FITTING AT BS 344, WL 255 IAW EA 130781.SDR USAA2012011800014Stringer · crackedC21 CHECK - CRACK ON STRINGER AT BS 440, S28R. REPAIRED STRINGER AT BS 440, S28R IAW B737-300 SRM 53-00-03-2R-1 FIG 201.SDR USAA2012010900020Support · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB SUPPORT BETWEEN BS 1001 TO BS 1005, WL 208, BETWEEN LBL 41 TO LBL 42. REPLACED WEB SUPPORT BETWEEN BS 1001 TO BS 1005, WL 208, BETWEEN LBL 41 TO LBL 42 IAW B737-300 SRM 51-40-02-0G FIGURE 11 AND 16.SDR USAA2012012500003Angle · corrodedC21 CHECK - CORROSION ON SPLICE ANGLE AT BS 317, WL 208, LBL 54. REPLACED SPLICE ANGLE AT BS 317, WL 208, LBL 54 IAW B737 SRM 51-40-02-0G FIG 12.SDR USAA2011122700010Lens · crazedEXTERNAL FUSELAGE RT OVER WING EMERGENCY EXIT LIGHT LENS COVER IS CRAZED AFT OF EXIT DOOR. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT LENS COVER EXTERNAL FUSELAGE AFT EXIT DOOR IAW B737 AMM.SDR USAA2012012300006Strap · crackedC21 CHECK - CRACKS ON FORWARD CARGO DOOR LOWER SEAL STRAP BETWEEN BS 478.5 TO BS 484.5, WL 150, S26R. REPLACED FORWARD CARGO DOOR LOWER SEAL STRAP BETWEEN BS 478.5 TO BS 484.5, WL 150, S26R IAW B737-300 SRM 51-40-05-0G.SDR SWAA118387Skin · crackedDURING SCHDULED CV CHECK, FOUND SKIN CRACKED AT BS 500B+12, STR 19R. REPAIRED SKIN IAW SRM.SDR USAA2012013000008Frame · crackedC21 CHECK - 2 CRACKS IN FUSELAGE FRAME AT BS 440, S22R. REPLACED FUSELAGE FRAME AT BS 440, S22R IAW B737-300 SRM 51.40.02.0G FIG 8, 12.SDR USAA2012012500006Floorbeam · corrodedC21 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208, RBL 36. REPLACED FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208, RBL 36 IAW B737 SRM 51-40-02-0G FIG 3 & 8.SDR USAA2012012500005Floor Support · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 994, WL 208 BETWEEN LBL 14 TO LBL 44. REPLACED FLOOR SUPPORT AT BS 994, WL 208 BETWEEN LBL14 TO LBL 44 IAW B737 SRM 51-40-02-0G FIG 3 & 8.SDR USAA2012012500004Shear Web · corrodedC21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB BETWEEN BS 996 TO BS 1016, WL 208 & BETWEEN RBL 37 TO RBL 45. REPLACED SHEAR WEB BETWEEN BS 996 TO BS 1016, WL 208 & BETWEEN RBL 37 TO RBL 45 IAW B737 SRM 51-40-02-0G FIG 3 & 8.SDR USAA2012012300007Shear Web · corrodedC21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB BETWEEN BS 986 TO BS 1016, WL 208, BETWEEN LBL 41 TO LBL 42. REPLACED SHEAR WEB BETWEEN BS 986 TO BS 1016, WL 208, BETWEEN LBL 41 TO LBL 42 IAW B737-300 SRM 51-40-02-0G FIGURE 3 & 8.SDR USAA2012011700011Channel · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL AT BS 996, WL 208 BETWEEN RBL 13 TO RBL 44. REPLACED HAT CHANNEL AT BS 996, WL 208 BETWEEN RBL 13 TO RBL 44 IAW B737 SRM 51-40-02-0G FIG 12.SDR USAA2012011000011Floorbeam · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 1006 TO BS 1016, WL 208 & BETWEEN RBL 4 TO RBL 11. REPLACED FLOORBEAM BETWEEN BS 1006 TO BS 1016, WL 208 & BETWEEN RBL 4 TO RBL 11 IAW B737 SRM 51-40-02-0G FIG 12.SDR USAA2012011000010Floorbeam · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208 & BETWEEN RBL 9 TO RBL 17. REPLACED FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208 & BETWEEN RBL 9 TO RBL 17 IAW B737 SRM 51-40-02-0G FIG 12.SDR USAA2012010900022Strap · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB UPPER STRAP AT BS 1027, WL 208, LBL 3. REPLACED WEB UPPER STRAP AT BS 1027, WL 208, LBL 3 IAW B737-300 SRM 51-40-02-0G FIGURE 9 AND 10.SDR USAA2012010900019Floor Support · corrodedC21 CHECK - FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN BS 1006 TO BS 1016, WL 208, LBL 38. REPLACED FLOOR SUPPORT BETWEEN BS 1006 TO BS 1016, WL 208, LBL 38 IAW B737-300 SRM 51-40-02-0G FIGURE 12.SDR USAA2011122800024Floorbeam · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT LAV FLOORBEAM BETWEEN BS 1006 TO BS 1016 & BETWEEN LBL 6 TO LBL 11. REPLACED LEFT AFT LAV FLOORBEAM BETWEEN BS 1006 TO BS 1016 & BETWEEN LBL 6 TO LBL 11 IAW B737 SRM 51-10-02-0G, 53-60-51-1A-1 & 51-40-02-0SDR USAA2011122800023Floor Support · corrodedC21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT LAV FLOOR SUPPORT BEAM BETWEEN BS 986 TO BS 1016, LBL 12. REPLACED LEFT AFT LAV FLOOR SUPPORT BEAM BETWEEN BS 986 TO BS 1016, LBL 12 IAW B737 SRM 51-40-02-0G FIG 2.SDR USAA2012013000010Attach Angle · corrodedC21 CHECK - CORROSION ON DOOR THRESHOLD ATTACH ANGLE BETWEEN BS 312 TO BS 344, WL 208, LBL 53. REPLACED DOOR THRESHOLD ATTACH ANGLE BETWEEN BS 312 TO BS 344, WL 208, LBL 53 IAW B737-300 SRM 51-40-02-0G FIG 8 & 12.SDR USAA2012013000009Skin · corrodedC21 CHECK - CORROSION ON LOWER MARKER BEACON ANTENNA PANEL AT BS 585, BL 0. REPAIRED LOWER MARKER BEACON ANTENNA PANEL AT BS 585, BL 0 IAW B737-300 SRM 51-40-02-0G FIG 3 & 8.SDR USAA2012013000006Door Frame · crackedC21 CHECK - 250 INCH LONG CRACK IN R1 DOOR FRAME AT NR 4 STOP (30.5" FROM BOTTOM OF DOOR) AT BS 328, WL 238.5. REPAIRED R1 DOOR FRAME AT NR 4 STOP (30.5" FROM BOTTOM OF DOOR) AT BS 328, WL 238.5 IAW EA 130764.SDR USAA2012010900021Attach Angle · crackedC21 CHECK - CRACKS ON ATTACH ANGLE BETWEEN BS 500D TO BS 520, BL 0. REPLACED ATTACH ANGLE BETWEEN BS 500D TO BS 520, BL 0 IAW B737-300 SRM 51-40-02-0G FIGURE 2.SDR SWAA118329Rod End · faultyON APPROACH FLAPS L/E TRANSIT LIGHT ON NR 2 SLAT. REMOVED AND REPLACED NR 2 SLAT ROD END IAW MM.SDR USAA2012012000008Wedge · debondedC21 CHECK - RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE DISBONDED BETWEEN SS116 TO SS124, 6 INCHES INBOARD OF OUTBOARD END 2.5 INCHES FROM TRAILING EDGE. REPAIRED NR 4 SLAT IAW B737-300 SRM 51-70-10-2R-4, REPAIR 4 FIGURE 202.SDR SWAA118214Sign · looseDURING SCHEDULED CV CHECK, FOUND FWD GALLEY CENTER UPPER EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.SDR SWAA117865Crease Beam · crackedDURING SCHEDULED SPV CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 618, LBL 63.5. REPAIRED CHORD IAW SRM.SDR SWAA117864Crease Beam · crackedDURING SCHEDULED SPV CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 617.5, RBL 63.5. REPAIRED CHORD IAW SRM.SDR SWAA117863Skin · crackedDURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 934 TO BS 935.5, STR 24R. REPAIRED SKIN IAW SRM.SDR SWAA117862Skin · crackedDURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 911 TO BS 912, STR 23R. REPAIRED SKIN IAW SRM.SDR SWAA117861Skin · crackedDURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 940 TO BS 941, STR 23R. REPAIRED SKIN IAW SRM.SDR SWAA117860Skin · crackedDURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 940 TO BS 945, STR 25R. REPAIRED SKIN IAW SRM.
Back to Boeing 737-3Y0