Boeing 737-222
Service difficulty reports · 657
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 = '737222' 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 = '737222' 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 CALA9700680Angle · corrodedINSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 270 TO 360, RBL 52. THE CORRODED AREA WAS REMOVED, A SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-40-3.SDR CALA9700677Frame · corrodedINSPECTION FOUND FRAME CORRODED AT FS 480, STRINGER 25L TO 22L. THE CORRODED SECTION OF FRAME WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-10-4.SDR 97UAL900290Air Distrbution · odorBURNING LIKE ODOR IN COCKPIT, POSSIBLY COMING FROM UNDER GLARESHIELD. ACCOMPLISHED INSPECTION OF ENTIRE COCKPIT AREA, FOUND ALL TO BE NORMAL. FOUND NO CIRCUIT BREAKERS POPPED AND ALL LIGHTING AND INSTRUMENTS NORMAL. RAN PACKS OFF OF APU. ALL OPERATION FOUNSDR CALA9700688Channel · corrodedINSPECTION FOUND AFT CABIN CLOSET TO FLOOR ATTACH CHANNEL CORRODED AT STA 1016 TO AFT PRESSURE BULKHEAD, RBL 2. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR CALA9700678Floor · corrodedINSPECTION FOUND AFT LAV FLOOR WEB CORRODED AT STA 994 TO 1016, LBL 37 TO LBL 46. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-01 AND 51-30-2.SDR CALA9700703Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 24 TO RBL 24. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-9.SDR CALA9700699Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD FRAME OF R-1 DOOR AT STA 294, STRINGER 17R. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-6.SDR 97UAL900282Skin · bird strikeBIRD STRIKE REPORTED DURING TAKEOFF, AND CREW RETURNED TO FIELD. ACCOMPLISHED BIRD STRIKE INSPECTION FOR THREE STRIKES ON THE LEFT SIDE OF THE NOSE AND ONE STRIKE ON THE RIGHT SIDE. THERE WAS NO DAMAGE TO THE AIRCRAFT OR EITHER ENGINE.SDR CALA9700687Angle · corrodedINSPECTION FOUND SUPPORT ANGLES ATTACHED TO FLOORBEAM AT STA 994, LBL 17 TO LBL 44 AND RBL 17 TO RBL 44 CORRODED. THE SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-30-2 AND 53-10-2.SDR CALA9700686Angle · corrodedINSPECTION FOUND TIE ANGLE CORRODED AT STA 360, STRINGER 28R. THE TIE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-6, AND 51-30-2.SDR CALA9700685Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL IN FORWARD CARGO PIT AT STA 500A TO 500B, STRINGER 26R. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-00, FIGURE 23, 51-40-2, AND 51-30-2.SDR P2EA97027Coalescer Bag · dirtyFLT 123 - MCI - TAKEOFF PLUS 30 MINUTES, ODOR DETECTED IN COCKPIT. NO FUMES, NO SMOKE NOR ANY ODOR IN CABIN. LEFT PACK TURNED OFF, ODOR SEEMED TO IMPROVE SLIGHTLY INC COCKPIT. CHANGED LT AND RT WATER SEPARATOR SOCKS AS PER MM 21-51-41. PERFORMED DETAILED INSDR CALA9700695Angle · corrodedINSPECTION FOUND L-ANGLE CORRODED AT STA 267 TO 277, LBL 12 TO RBL 12. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9700683Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM CHANNEL AT STA 807. THE CRACKED AREA WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-10-2, AND 51-30-2.SDR CALA9700684Support · crackedINSPECTION FOUND A .5 INCH CRACK IN SUPPORT AT FS 770 LT. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 7.SDR 97UAL900263Switch · failedAIRCRAFT DIVERTED TO SAGINAW, MICHIGAN, WITH A NR 2 ENGINE FUEL FILTER ICING LIGHT ON. FUEL HEAT, NO HELP. REPLACED DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD.SDR CALA9700696Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN SUPPORT CHANNEL AT BASE OF VERTICAL FIN. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9700694Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 312, LBL 20 TO RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-01.SDR CALA9700692Frame · crackedINSPECTION FOUND A .125 INCH CRACK IN FRAME UPPER FLANGE IN FORWARD CARGO PIT AT FS 500A, STRINGER 23L. THE CRACKED AREA WAS REMOVED IAW SRM 53-10-4. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 53-10-2.SDR CALA9700690Floor · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOOR WEB AT STA 986 TO 995, RBL 43. THE CRACKED AREA WAS REMOVED IAW SRM 51-40-2, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-3, AND 51-10-3.SDR CALA9700682Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT LOWER FORWARD CORNER OF R-2 DOOR SKIN. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 52-00-3.SDR CALA9700681Intercostal · corrodedINSPECTION FOUND FLOOR INTERCOSTAL CORRODED AT STA 1006 TO 1016. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9700675Skin · crackedINSPECTION FOUND A 0.4 CRACK IN NR 2 ENGINE FORWARD PYLON FAIRING SKIN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-10-2 AND 51-30-2.SDR CALA9700674Panel · crackedINSPECTION FOUND A 1 CRACK IN NR 2 ENGINE TO PYLON UPPER AFT PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-10-2, 51-40-2, AND 51-30-2.SDR CALA9700704Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN BELTFRAME AT STA 767, STRINGER 13 AND 14R. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.SDR CALA9700700Floorbeam · corrodedINSPECTION FOUND UPPER CAP CORRODED AT STA 344, LBL 40 TO RBL 17. THE FLOORBEAM UPPER CAP WAS REMOVED IAW SRM 53-10-9, FIGURE 5. REPAIR ANGLES, SHIM, AND CHORD WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-10-2.SDR CALA9700698Tee · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORMED TEE AT BS 342, LBL 12. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9700697Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM SUPPORT TEE AT STA 328, LBL 48. THE TEE WAS REMOVED AND A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-10-2.SDR 97UAL900250Connector · failedEEL LIGHTING INOPERABLE FROM ROWS 12 TO 14 AS IS OVER-WING EEL EXIT MARKER. REPAIRED WIRING AT SIDEWALL CONNECTOR. OPS CHECK GOOD.SDR P2EA97024Connector · not connectedFLT 631 - MCI - FL 240, CABIN ALTITUDE SLOWLY CLIMBED ABOVE 10M'. MASKS DID NOT DROP. REF CI M208754, AMENDED DEFERRAL. PLACED FORWARD OUTFLOW VALVE IN CLOSED POSITION. CANNON PLUG PREVIOUSLY REMOVED. (M)SDR 97UAL900243Egt Indication · erraticCREW REPORTS, NR 1 ENGINE EGT IS ERRATIC. *S/D* REPAIRED BROKEN SOLDER JOINT AT THE EGT BALANCE RESISTOR. NO EGT SYSTEM PROBLEMS HAVE BEEN NOTED SINCE THE REPAIR WAS COMPLETED 3/31/97.SDR 97ZZZM663Skin · crackedDURING COMPLIANCE OF BOEING SB INSPECTION, FOUND AFT LOWER L1 DOOR CUTOUT CRACKED VERTICALLY 1.5 INCH LONG AT FUSELAGE STATION 340. REMOVED SCUFF PLATE AND INSTALLED INTERMI REPAIR PER BOEING SB 737-53-1083 REVISION 3 FIG 3. INTERIM REPAIR WILL BE MADE A PERSDR 97UAL900236Light Plate · failed bulbCREW REPORTS, SMOKE IN COCKPIT FROM THE AUTOPILOT CONTROL PANEL. PANEL WAS HOT. *S/D* AUTOPILOT MODE CONTROL PANEL LIGHT PLATE 5VDC LIGHT BULB BURNED LIGHT PLATE ASSEMBLY. MODE CONTROL PANEL LIGHT PLATE ASSEMBLY REPAIRED AND NEW BULB INSTALLED.SDR P2EA97023Pressurization · failedFLT 703 - MSP - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. AUTO PRESSURIZATION FAILURE, UNABLE TO CATCH CABIN PRESSURE MASKS DROPPED. STANDBY MANUAL OPERATES NORMAL. DEFERRED AUTO PRESSURIZATION IAW MEL 21-14. CONTROL ITEM NR M208725. CABIN O2 MASKS RE-PACSDR 97ZZZX1625Motor · leakingDURING FUNCTIONAL CHECK FLIGHT, A-SYSTEM HYDRAULICS WAS LOST. UPON LANDING, FOUND THE FLAP DRIVE MOTOR LEAKING AT MOUNT SURFACE. UPON REMOVAL OF FLAP DRIVE MOTOR, FOUND THE SEAL PLATE P/N 176002 S/N 569341 SHEARED AWAY FROM MOTOR DUE TO CORROSION OF INTERNALSDR 97UAL900221Actuator · failedAFTER LANDING AT MSP, LOST THE A-HYDRAULIC SYSTEM. AIRCRAFT WAS TOWED TO GATE. REPLACED LEAKING NR 8 SPOILER ACTUATOR. SERVICED HYDRAULIC SYSTEM. OPS CHECK GOOD.SDR 97UAL900201Battery · dischargedAFT GALLEY EMERGENCY LIGHT IS INOP. REPLACED BATTERY AND CHARGER, OPS CHECK OK.SDR 97UAL900306Skin · corrodedFOUND EVIDENCE OF CORROSION IN FUSELAGE SKIN UNDER AFT CARGO DOOR OPENING. UPON REMOVAL OF DAMAGED OUTER SKIN SECTION, FOUND THAT CORROSION CONTINUED BETWEEN SKIN AND INNER DOUBLER (REF: SRM 53-30-2, ITEMS 1 AND 15) UNDER DOOR OPENING AS WELL AS CIRCUMFERENTSDR 97UAL900184Compressor · stalledCREW REPORTED, POSSIBLE COMPRESSOR STALL FROM NR 2 ENGINE. *S/D* THIS POSSIBLE COMPRESSOR STALL COULD NOT BE CONFIRMED. THE INCIDENT HAS NOT BEEN REPEATED.SDR 97UAL900167Gasper Fan · failedACRID SMELL IN THE COCKPIT AND MAIN CABIN. AFTER INSPECTION OF CABIN AND WATER SEPARATORS, FOUND GASPER FAN BURNED UP AND CIRCUIT BREAKER TRIPPED. GASPER FAN WAS REPLACED. OPS CHECK GOOD.SDR 97UAL900174Lights · inoperativeBOTH OVERWING EXIT LIGHTS IN CABIN AND DOOR 1L EMERGENCY EXIT LIGHTS INOPERABLE. RESEATED RT OVERWING INTERIOR EMERGENCY EXIT LIGHT, LT OVERWING LIGHT. OPS CHECK GOOD.SDR 97UAL900162Light · inoperativeBOTH OVERWING EXIT LIGHTS IN CABIN AND DOOR 1 LEFT EMERGENCY EXIT LIGHTS ARE INOPERATIVE. *S/D* THE RT OVERWING INTERIOR EMERGENCY EXIT LIGHT AND LT OVERWING LIGHT WERE RESEATED, OPS CHECK GOOD.SDR 97UAL900154Latch Plate · bentAIRCRAFT DIVERTED TO SYR DUE TO CABIN PRESSURE PROBLEMS. *S/D* FOUND DOOR FRAME LATCH PLATE BENT (NOT FLUSH) CAUSING SEAL NOT TO SEAT ON THE FRAME. REPAIRED COVER PLATE.SDR 97UAL900153Valve · failedCREW REPORTED THAT THEY WERE UNABLE TO GET 'A' SYSTEM HYDRAULICS TO FLIGHT CONTROLS. FOUND A SYSTEM FLIGHT CONTROL SHUT-OFF VALVE FAILED CLOSED. REPLACED SHUTOFF VALVE. OPS CHECK GOOD.SDR P2EA97006Oil Temp Bulb · failedFLT 631 - MDW - A/C DIVERTED TO DSM, EMERGENCY DECLARED, LANDING UNEVENTFUL. NR 2 ENGINE OIL TEMPERATURE PEGGED FULL SCALE DID NOT SHUT ENGINE DOWN DUE TO NR 1 ENGINE GENERATOR PROBLEM. REPLACED OIL FILTER AND OIL TEMPERATURE BULB. OPS CHECK NORMAL IAW MM 7SDR 97UAL900141Trash Can · fireSMOKE REPORTED IN TRASH CAN OR SHELF AREA OF AFT GALLEY. *S/D* OPERATIONALLY CHECKED ALL GALLEY EQUIPMENT AND ELECTRICAL CONNECTORS, NO FAULT FOUND.SDR 97UAL900139Control Lever · lack of lubeON GEAR RETRACTION, HAD TO USE OVERRIDE TO GET HANDLE TO UP POSITION. TROUBLESHOT AND CHECKED LEVER LATCH OPERATION. NO DEFECTS NOTED. LUBED CONTROL LEVER MECHANISM. LATCH OPERATES NORMALLY.SDR 97UAL900128Tr Access Unit · looseNR 1 ENGINE THRUST REVERSER UNLOCKED LIGHT CAME ON INTERMITTENTLY IN-FLIGHT. FOUND LOOSE ENGINE ACCESSORY UNIT. SECURED UNIT.SDR 97UAL90013113th Stage Duct · rupturedAT 500 FEET ON TAKEOFF, AIRCRAFT EXPERIENCED THRUST LOSS OF NR 2 ENGINE FOLLOWED BY AN OVERHEAT INDICATION. OVERHEAT LIGHT EXTINGUISHED WITH THROTTLE AT IDLE. LANDED WITHIN 10 MINUTES. THE 13TH STAGE SADDLE DUCT RUPTURED AROUND THE DOUBLER WELD. THE SADDLSDR 97UAL900118Slide Bottle · low pressureDOOR 2L SLIDE PRESSURE APPROXIMATELY 2700 PSI. SLIDE PRESSURE BOTTLE APPEARED TO BE COLD SOAKED. PRESSURE READ NORMAL AT ROOM TEMPERATURE.
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