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 USAA920080814Angle · corrodedCLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON ANGLE AT BS 300 - 328, RBL 59. INSTALLED REPAIR IAW SRM 53-10-15 FIG 101, 51-10-02.SDR USAA920080827Door Frame · crackedCLT- MAJOR REPAIR - Q6 CHECK - .25 INCH CRACK ON L1 DOOR FRAME AT NR 7 STOP. INSTALLED REPAIR IAW EA100332.SDR USAA920080826Door Frame · crackedCLT- MAJOR REPAIR - Q6 CHECK - .25 INCH CRACK ON L1 DOOR FRAME AT NR 6 STOP. INSTALLED REPAIR IAW EA100332.SDR USAA920080828Angle · crackedCLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON ANGLE AT BS 500C, STR 22L. REPLACED ANGLE IAW SRM 51-70-11.SDR USAA920080812Floorbeam · corrodedCLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS 328, RBL 9. INSTALLED REPAIR IAW SRM 53-10-51 AND DWG 65-45812.SDR USAA920080824Door Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .1875" CRACK ON FUSELAGE DOOR FRAME AT BS 294.5, STR 17R. INSTALLED DOUBLER REPAIR IAW SRM 51-70-11 FIG 1.SDR USAA920080815Attach Angle · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON FLOORBEAM ATTACH ANGLE AT BS 328, RBL 32. INSTALLED REPAIR IAW SRM 51-10-02 AND DWG 65-45839.SDR USAA920080811Angle · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .25" CRACK ON FLOORBEAM ANGLE AT BS 328, LBL 26. INSTALLED REPAIR IAW SRM 53-10-51 FIG 201.SDR SB08019Altimeter · faultyPHL - FLT 1833 - ON CLIMBOUT FROM PHL, EN ROUTE TO NAS, THE NR 2 ALTIMETER FAILED IN FLIGHT WITH FLAG IN VIEW. STANDBY ALTIMETER INDICATED 300 FEET LOW AT 30,000 FEET AND 200 FEET LOW AT 20,000 FEET. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHERSDR USAA920080818Fitting · crackedCLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON CLIP AT BS 344, LBL 12. INSTALLED REPAIR IAW SRM 53-10-51.SDR USAA920080825Seat Track · corrodedCLT- MAJOR REPAIR - Q6 CHECK - 3 INCH LENGTH CORROSION ON SEAT TRACK AT BS 943, LBL17.2. INSTALLED SPLICE REPAIR IAW SRM 53-00-53 FIG 201.SDR USAA920080819Skin · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - NR 1 SLAT HAS 4" AREA OF DELAMINATION ON O/B END UPPER SURFACE. REPLACED SLAT IAW JOB CARD O3C30227005.SDR USAA920080817Angle · corrodedCLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON CHORD ANGLE AT BS 294 - 312, RBL 16. REPLACED ANGLE IAW SRM 51-40-02.SDR USAA920080816Floorbeam · corrodedCLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS 312, RBL 21 - 45. INSTALLED REPAIR IAW SRM 53-10-51.SDR SB08018Windshield · crackedPHL FLT 954 EN ROUTE FROM FLL TO PHL, CREW REPORTED THE FIRST OFFICER'S NR 1 WINDSHIELD OUTER PANE ARCED AND THEN CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S NR 1 WINDSHIELD PER JOB CARD. OPERATIONALSDR USAA920080820Skin · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON NR 6 SLAT SKIN JUST I/B OF AUX TRACK. INSTALLED DOUBLER REPAIR IAW SRM 57-43-01 REPAIR 6.SDR USAA920080823Floor Panel · crackedCLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON COCKPIT FLOOR AT BS 257, LBL 3. INSTALLED DOUBLER REPAIR IAW SRM 53-10-51.SDR USAA920080813Floorbeam · corrodedCLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM AT BS 344, RBL 12 - LBL 12. INSTALLED REPAIR IAW SRM 53-10-51.SDR USAA920080810Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .5" CRACK ON FRAME AT BS 907 BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20E.SDR USAA920080867Skin · crackedA .3125 INCH CRACK IN FUSELAGE SKIN AT CORNER OF LWR AFT SERVICE DOOR. REPAIRED IAW EA 100368.SDR USAA920080866Web · crackedPRESSURE DECK WEB HAS 1.5" CRACK AT BS 663.75, WL 208.1, LBL 30. INSTALLED DOUBLER REPAIR IAW SRM 56-60-51.SDR USAA920080809Aileron · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - A 1" AREA OF DELAMINATION ON LEFT AILERON AT MIDDLE HINGE AREA. REPLACED AILERON IAW JOB CARD O3L30627001.SDR USAA920080808Support · crackedCLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON FRAME SUPPORT AT BS 947, STR 22L. INSTALLED REPAIR IAW SRM 51-10-02.SDR USAA920080807Support · crackedCLT - MAJOR REPAIR - Q6 CHECK - A 2" CRACK ON FRAME SUPPORT AT BS 927 - 947, BL 0. INSTALLED REPAIR IAW SRM 51-40-02.SDR USAA920080757Frame · crackedPIT - MAJOR REPAIR - FPBH INSPECTION, FRAME CRACKED, BS 440, S24R. REPAIRED FRAME, BS 440, S24R, IAW US AIRWAYS EA 110807.SDR USAA920080721Frame · crackedPIT - MAJOR REPAIR - FPBH INSPECTION, CRACKED FRAME, BS 440, S24R. REPAIRED FRAME, BS 440, S24R IAW USAIRWAYS EA 110807.SDR USAA920080713Rib · crackedMIA - MAJOR REPAIR - PAINT LINE - VERTICAL STABILIZER HINGE RIB CRACKED. REPAIRED VERTICAL STABILIZER HINGE RIB IAW USAIRWAYS EA 100364.SDR USAA920080804Wedge · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - A 5" X 2.5" DISBOND ON NR 5 SLAT TRAILING EDGE WEDGE. INSTALLED REPAIR IAW SRM 57-43-02, 51-70-00, 57-70-10 R4 AND AMM 51-21-99.SDR USAA920080803Wedge · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - A 5" X 7" DISBOND AREA ON NR 4 SLAT TRAILING EDGE WEDGE. INSTALLED REPAIR IAW SRM 51-70-10.SDR USAA920080802Wedge · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - A 14.5" X 6.5" DISBONDED AREA ON NR 5 SLAT T/E WEDGE. INSTALLED REPAIR IAW SRM 57-43-02, TR 57-42-02, 51-70-10 AND AMM 51-21-99.SDR USAA920080800Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON FRAME AT BS 727B, STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20.SDR USAA920080759Beam · crackedPIT - MAJOR REPAIR - CRACKED BULKHEAD RIGHT VERTICAL BEAM WEB, BS 178, RBL 17, WL 185. REPAIRED BULKHEAD RIGHT VERTICAL BEAM WEB, BS 178, RBL 17, WL 185 IAW B737 SRM 53-10-08.SDR USAA920080758Beam · crackedPIT - MAJOR REPAIR - CRACKED BULKHEAD LEFT VERTICAL BEAM WEB, BS 178, LBL 17, WL 225. REPAIRED BULKHEAD LEFT VERTICAL BEAM WEB, BS 178, LBL 17, WL 225 IAW B737 SRM 53-10-08.SDR USAA920080806Shear Web · corrodedCLT - MAJOR REPAIR - Q6 CHECK - A 5" X 7" AREA OF CORROSION ON SHEAR WEB AT BS 988 - 989, LBL 30 - 31. INSTALLED REPAIR IAW SRM 51-70-13 PG 1-3.SDR SB08016Battery Pack · dischargedPHL - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN THE MID CABIN WILL NOT STAY ILLUMINATED DURING TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACK M1479. OPERATIONAL CHECK GOOD.SDR USAA920080701Skin · crackedCLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727D, S23L. REPAIRED FUSELAGE SKIN, BS 727D, S23L IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA920080805Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .7" CRACK ON FRAME AT BS 727F BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20.SDR SB08015Circuit Card · faultyFLL - FLT919 - ON APPROACH TO FLL, UPON LOWERING LANDING GEAR, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT WITH NO MAIN GEAR INDICATION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RESET A CIRCUIT BREAKER. CREW THEN RECEIVED A NORMAL GEASDR USAA920080679Skin · crackedCLT - MAJOR REPAIR - AFT CARGO DOOR SKIN IS CRACKED AT THE HANDLE CUT OUT. REPLACED AFT CARGO COMPARTMENT DOOR IAW USAIRWAYS TASK CARD 03L21952008.SDR USAA920080675Angle · corrodedCLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON AFT ENTRY DOOR "Z" ANGLE, BS 947 - BS 991, LBL 53. REPAIRED AFT ENTRY DOOR "Z" ANGLE, BS 947 - BS 991, LBL 53 IAW B737 SRM 51-70-11.SDR USAA920080674Support Angle · corrodedCLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON GALLEY "Z" SUPPORT ANGLE, BS 969, RBL 33 - RBL 45. REPLACED GALLEY "Z" SUPPORT ANGLE, BS 969, RBL 33 - RBL 45 IAW B737 53-60-51.SDR USAA920080649Skin · crackedCLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727E - BS 727F, S24R - S26R. REPAIRED FUSELAGE SKIN, BS 727E - BS 727F, S24R - S26R IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA920080801Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .5" CRACK ON FRAME AT BS 727D BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20E.SDR SB08014Hydraulic Line · blownMCO - FLT1926 - ON LIFTOFF AND GEAR RETRACTION OUT OF MCO, CREW LOST A SYSTEM HYDRAULICS AS LOW PRESSURE LIGHTS ILLUMINATED. PUMPS WERE LEFT ON ABOUT FIVE MINUTES AFTER THE LOW PRESSURE LIGHTS ILLUMINATED. FLUID WAS DEPLETED. CREW DECLARED AN EMERGENCY AND SDR USAA920080829Angle · crackedCLT- MAJOR REPAIR - Q6 CHECK - 1 INCH CRACK ON ANGLE AT BS 500F, STR 21L. REPLACED ANGLE IAW DWG 65C32055.SDR USAA920080799Frame · crackedCLT - MAJOR REPAIR - Q6 CHECK - A .25" CRACK ON FRAME AT BS 500F BETWEEN STR 8L AND STR 9L. INSTALLED REPAIR IAW SRM TR 53-10-20E.SDR USAA920080822Gate · corrodedCLT- MAJOR REPAIR - Q6 CHECK - 4 INCH AREA OF CORROSION ON THE R2 DOOR LOWER GATE. REPLACED LOWER GATE IAW SRM 51-10-02.SDR USAA920080821Door Frame · crackedCLT- MAJOR REPAIR - Q6 CHECK - .1875 INCH CRACK ON R2 DOOR AFT FRAME, 3RD FROM BOTTOM DOOR STOP. INSTALLED REPAIR IAW SRM 52-10-11.SDR USAA920080615Skin · crackedCLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727F, S25R. REPAIRED FUSELAGE SKIN, BS 727F, S25R IAW USAIRWAYS EA 100306.SDR SB08013Battery Pack · dischargedMIA - MAINTENANCE REPORTED THE EMERGENCY EXIT SLIDE LIGHTS AT RIGHT-HAND SIDE (FORWARD, AFT AND OVERWING LIGHTS-EXTERIOR) ALONG WITH THE LEFT AND RIGHT OVERWING ESCAPE HATCH AND SEAT MOUNTED EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE B
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