Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA960733Stringer · corrosionROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27 L, BS 947 TO 1006. REMOVED CORRODED STRINGER AND SPLICED IN NEW SECTION, REPAIRED PER SRM 53-10-3 DETAIL 6. (M)SDR USAA960732Skin · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN (STRINGER 17L BS 950). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M)SDR USAASB96221Outflow Valve · intermittentMCO - FLT 1176 - CREW REPORTED A PRESSURIZATION PROBLEM OVER JAX. NEITHER AUTO STANDBY OR MANUAL WOULD STOP CABIN FROM CLIMBING. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE FORWARD OUTFLOSDR USAASB96220Overheat Module · defectiveMCO - FLT 1176 - DURING CLIMB-OUT, THE LT WING BODY O/H LIGHT ILLUMINATED AT FL 020. CREW ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. FLIGHT RETURNED TO FIELD AT MCO AS PRECAUTIONARY. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR USAASB96214Fuel Control · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW SDR 96ZZZM1487Fuel Pump · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW SDR USAA960666Skin · crackedROA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK FORWARD ENTRY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN, BONDED DOUBLER AND BEAR STRAP. INSTALLED STRAPS, REPAIRED PER EA 41616 INTERIM REPAIR. (M)SDR USAASB96211Battery Pack · dischargedIAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT SIGN OVER THE RIGHT FORWARD SERVICE DOOR INOP. MAINTENANCE REPLACED THE BATTERIES IN THE LIGHT ASSEMBLY OVER THE RIGHT FORWARD SERVICE DOOR. OPS CHECK GOOD. (M)SDR USAASB96197Fuel Heat Vlv · stuck openCMH - FL 1183 - DURING CLIMB AT FL 280, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE. THE OIL TEMPERATURE WAS IN THE YELLOW BAND FOR APPROX 15 MINS PRIOR TO SHUTDOWN. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH WHERE THE FLIGHT LANDED WITSDR USAA960918Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM RBL 24.5 BS 674. INSTALLED STIFFENER AND NEW CHANNEL, REPAIRED PER EO 5791G632. (M)SDR USAA960622Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA OF HEAVY SURFACE CORROSION FLOOR BEAM STATION 360, RBL 12 TO RBL 56. INSTALLED REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. (SDR USAA960621Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKED WEBS RBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M)SDR USAA960620Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEBS LBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 FIG 1. (M)SDR USAA960619Web · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKED WEBS BL 0 BS 707. INSTALLED WEB REPAIR AND FILLERS. REPAIRED PER SRM 51-40-2. (M)SDR USAA960617Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AND 1.5 INCH BY 6 INCH CORRODED AREAS FLOOR BEAM BS 328 LBL 10 AND LBL 24-30. REPAIR ANGLES AND T-CAP. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. (M)SDR USAA960616Floor Beam · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 1 INCH BY 68 INCH FLOOR BEAM BS 986 LBL 18 INCH TO RBL 50 INCH. INSTALLED T-CAP REPAIR AND REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960615Door Frame · corrsionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 1 INCH CORROSION DOOR FRAME LONGERONO STATINO 317 STRINGER 27R. REMOVED CORROSION AND INSTALLED STRAP DOUBLER PER EA 41489. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960614Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 55 INCH CORRODED AREA FLOOR BEAM BS 947 BL 30 INCH - RBL 25 INCH. INSTALLED T-CAP REPAIR, REPAIRED TR 53-10-05 C AND SPM. CORROSION TASK NR C53-107-02, CORROSION LEVLE 1. (M)SDR USAA960613Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM BS 674 LBL 24.5. INSTALLED STIFFENER AND NEW CHANNEL. REPAIRED PER EO 5791G632. (M)SDR USAASB96187Seal · leakingBWI - FL 1930 - DURING CLIMB, THE NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED. THE OIL QTY GAUGE BEGAN DECREASING TO ZERO. CREW SHUT DOWN THE NR 2 ENG. OIL PRESS AT SHUTDOWN WAS 16 PSI. AFTER SHUTDOWN, WINDMILLING OIL PRESS WAS APPROX 15-16 PSI. ENG WAS OPERSDR USAASB96177Battery Pack · dischargedPIT - FL 560 - ON PREFLIGHT COCKPIT CHECK, CREW REPORTED LOW LEVEL TRACK LIGHTING AND EMERGENCY LIGHTS INOP THROUGHOUT CABIN. MAINTENANCE REPLACED THREE BATTERY PACKS IN THE FORWARD AND AFT SECTIONS OF THE CABIN. OPS CHECK GOOD. (M)SDR 96ZZZM1378Battery Pack · dischargedPIT - FL 560 - ON PREFLIGHT COCKPIT CHECK, CREW REPORTED LOW LEVEL TRACK LIGHTING AND EMERGENCY LIGHTS INOP THROUGHOUT CABIN. MAINTENANCE REPLACED THREE BATTERY PACKS IN THE FORWARD AND AFT SECTIONS OF THE CABIN. OPS CHECK GOOD. REFERENCE USAASB96177.SDR USAASB96191Battery Pack · dischargedCLT - MX FOUND THE EXTERIOR LEFT WING EMERGENCY EVACUATION LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK FOR THE LEFT WING EMERGENCY EVACUATION LIGHTS. OPS CHECK GOOD. (M)SDR USAASB96172Light · failedPIT - FL 902 - CREW REPORTED, THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD SERVICE DOOR IS INOP. MAINTENANCE REPLACED THE LIGHT ASSEMBLY ABOVE THE FORWARD SERVICE DOOR. OPS CHECK GOOD. (M)SDR USAA960603Chord · crackedCLT - INSPECTION FOUND, BY ULTRASONIC, CRACKS .5 INCH LONG FROM FASTENER HOLE TO EDGE OF CHORD AT STATION 727 STRINGER 18A OUTER CHORD LEFT SIDE. REPLACED CHORD PER EO NR 5394GD68, EA NR 58752 AND EA NR 58778. (M)SDR USAASB96169Tr Unit · failedPIT - FL 2165 - AIRCRAFT WAS AT CRUISE ALTITUDE APPROXIMATELY 20 MINUTES OUT OF BWI WHEN RADAR BECAME INTERMITTENT. CAPTAIN CYCLED BREAKERS AND WEATHER RADAR WENT COMPLETELY OUT BUT STILL HAD TCAS. CAPTAIN RADIOED INTO OPERATIONS CONTROL AND AFTER FAILED ATTSDR USAASB96164Battery Pack · dischargedCLT - MAINTENANCE FOUND THE CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REPLACED THE CENTER AISLE OVERHEAD EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M)SDR USAA960575Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS CORROSION AT SCREW HOLES BS 947 LBL 15, 17, 18, 21, 30, 36 AND 49 TOP OF FLOOR BEAM T-CAP. INSTALLED T-CAP REPAIR LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TP 53-10-05C. CORROSION TASK NRSDR USAA960574Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CORROSION ON T-CAP ON FLOOR BEAM STATION 312, AT BL 0. CUT OFF T-CAP, FABRICATED AND INSTALLED NEW PIECE FROM LBL 18 TO RBL 39, REPAIRED PER TR 53-107-02, CORROSION LEVEL 1. (M)SDR USAA960573T-Cap · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION BS 328 FROM RBL 12 TO RBL 49 T-CAP. REMOVED CORRODED T-CAP, FABRICATED AND INSTALLED NEW ONE. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960572Angle · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH SPOT OF CORROSION ON Z-ANGLE BS 270 LBL 10 TO LBL 5. INSTALLED ANGLE REPAIR/SPLICE, REPAIRED PER TR 53-20-04. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960571Keel Beam · chaffingINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CHAFFING AT 5 FASTENER HOLES 17 INCH LEFT STATION 727 TO STATION 710 KEEL BEAM LOWER CHORD ANGLE. SPOT FACED HOLES, FABRICATED FILLERS, STRAP DOUBLER AND INSTALLED PER EA 41405. (M)SDR USAA960570Keel Beam · frettingINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FRETTING AT BOLT HOLES RIGHT HAND BOTTOM FLANGE OF KEEL BEAM STATION 710-727. SPOT FACED HOLES, FABRICATED FILLERS, STRAP DOUBLER AND INSTALLED PER EA 41405. (M)SDR USAA960569T-Cap · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH SURFACE CORROSION AT BS 360 RBL 12 T-CAP. CUT OUT DAMAGE, FABRICATED FILLER, REPAIR ANGLES AND INSTALLED PER SRM 53-10-9, 51-10-1. (M)SDR USAA960566Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH, 2 INCH BY 6 INCH AND SMALLER SPOTS OF CORROSION BS 987 LBL 16 TO RBL 45 TOP FLOOR BEAM T-CAP. REMOVED T-CAP, FABRICATED AND INSTALLED NEW T-CAP, REPAIRED PER TR 53-10-5C. CORROSION TASK NR C53SDR USAASB96156Light · inoperativeBWI - MAINTENANCE FOUND MULTIPLE INTERIOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. MAINTENANCE RESEATED CANNON PLUG ON POWER SUPPLY. OPS CHECK GOOD. (M)SDR USAASB96149Pressurization · malfunctionedPIT - FLT 1217 - DUE TO HEAVY LOAD, TAKEOFF WAS ACCOMPLISHED WITH APU BLEED USED FOR PRESSURIZATION. IN CLIMB, CREW SWITCHED RIGHT PACK ON AND HEARD A BANGING NOISE FOLLOWED BY A LOUD HISS. PRESSURIZATION WENT TO AUTO FAIL AND THE CABIN BEGAN TO CLIMB WITH TSDR USAASB96190Battery Pack · dischargedSYR - MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT INOP IN THE FORWARD CABIN. MAINTENANCE REPLACED THE BATTERY PACK AT THE FORWARD OVERHEAD CABIN. OPS CHECK GOOD. (M)SDR USAASB96146Engine · failedSEA - FLT 100 - FLIGHT CREW OBSERVED THAT THE NR 2 ENGINE WAS CONSUMING MORE OIL THAN NORMAL AFTER DEPARTURE FROM SEA. CHECKING THE EN ROUTE TIME LEFT TO CLT, THEY FELT THEY WOULD NOT HAVE ENOUGH OIL TO MAKE CLT. THEY WERE NOT SURE IF IT WAS A LEAK AND/OR A HSDR USAASB96137Wire · shortedLGA - MAINTENANCE FOUND THE FORWARD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. ALSO, FOUND INOP WERE THE MAIN ENTRY DOOR AND SERVICE DOOR EXIT IDENTIFIERS. MAINTENANCE FOUND THE MAIN ENTRY DOOR EXIT IDENTIFIER LIGHT WIRING SHORTED OUT. REWIRED EXIT IDENTIFIERSDR USAA960532Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 3INCH CORRODED AREAS AT NUT PLATE HOLES T-CAP, BS 312 FLOOR BEAM BBL 0, RBL8. INSTALLED T-CAP REPAIR AND REPAIRED PER SRM 53-10-9. CORROSION TASK NRC53-107-02, CORROSION LEVEL 1. (M)SDR USAA960531Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 3INCHES AT FLOOR BEAM STATION 1006 LBL 8. CUT OFF T-CAP THAT WAS OUT OFLIMITS, FABRICATED REPLACEMENT AND INSTALLED PER SRM 53-10-9 FIG 2.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960530Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .33 INCH CORRODEDAREA FLOOR BEAM BS 947.5 RBL 10 TO LBL 36. INSTALLED REPLACEMENT T-CAP,REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960529Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SPOTS OFCORROSION ALONG SIDES OF STRINGER BS 947-995 S-27L. REMOVED STRINGERSECTION, FABRICATED NEW SECTION AND INSTALLED, REPAIRED PER SRM 53-10-3.CORROSION TASK NR C53-202-01 CORROSION LEVEL 1. (M)SDR USAA960528Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODEDAREAS FLOOR BEAM BS 967. INSTALLED DOUBLER REPAIRED PER SRM 53-10-9.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1 (M)SDR USAA960527Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY1 INCH CORRODED AREAS ON FLOOR BEAM BS 328 RBL 12 INCH TO RBL 45 INCH.INSTALLED NEW T-CAP WITH REPAIR ANGLES, REPAIRED PER TR 53-10-13. CORROSIONTASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA960526Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHCORRODED AREA FLOOR BEAM BS 360 RBL 54. INSTALLED REPAIR ANGLE, REPAIREDPER TR 53-10-05 C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1.(M)SDR USAA960525Skin · gougedINT - DURING Q-6 CHECK VISUAL INSPECTION FOUND TWO GOUGES .75INCH AND .625 INCH SKIN STABILIZER STATION 92.7 APPROXIMATELY 17 INCHES FROMAFT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)SDR USAA960524Skin · gougesINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO GOUGES 1 INCHAND .625 INCH SKIN STABILIZER STATION 226 15 INCHES AND 20 INCHES AFT OFFRONT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)SDR USAA960523Bulkhead Skin · scratchINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH SCRATCHAFT PRESSURE BULKHEAD SKIN 5 O'CLOCK POSITION. INSTALLED DOUBLER, REPAIREDPER SRM 53-10-4 FIG 3. (M)
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