Boeing 737-800
Service difficulty reports · 843
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 = '737800' 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 = '737800' 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 CA141215011Connector · damaged(CAN) DURING CRUISE FLIGHT, CREW REPORTED THAT RIGHT HAND ELEVATOR HAD UN-COMMENDED PITCH CHANGES ON AUTOPILOT A/B AND MANUAL +/- 300 FT WHEN LEVEL. THE DECISION WAS MADE TO RETURN THE AIRCRAFT, WHERE THE AIRCRAFT LANDED SAFELY. TROUBLE SHOUTING CARRIED OUT FOSDR CA141211004Oven · smoke(CAN) ABOUT 45 MINUTES AFTER TAKEOFF, SMOKE COMING OUT OF THE AFT GALLEY OVEN #2 WAS REPORTED BY THE CABIN CREW TO FLIGHT CREW WHO HAD COMPLETED THE Ï¿½SMOKE, FIRE OR FUMESÏ¿½ CHECKLIST , QRH 8.8. IN ABOUT FIVE MINUTES AFTER QRH 8.8 HAS BEEN APPLIED, THE SMOKESDR ASMF201501014Warning System · false activationDURING TRANSIT CHECK, THE ANTI-SKID LIGHT TURNED ON WAS DETECTED ON CABIN CREW. PERFORMED FIM 32-42 TASK 829 PROCEDURE, CONFIRMING THE FAILURE, SO THE ANTI-SKID SYS WAS DEFERRED IAW MEL 32-2-2 CAT C. ACFT PERFORMED AN UNSCHEDULED LANDING DUE TO RAIN IN THE DSDR ASMF2015010500002Brake Assy · damagedAIRCRAFT REJECTED TAKEOFF AT 120 KNOTS, DUE TO AN ABNORMAL VIBRATION IN THE LT MLG. PERFORMED HIGH ENERGY STOP INSPECTION & AIRFRAME VIBRATION CONDITION INSPECTION IAW AMM 05-51-07 & AMM 05-51-67, DETECTED LT MLG BRAKES & WHEELS NRS 1 & 2 DAMAGED, LT MLG AXLESDR CA140716011Bolt · loose(CAN) NR 2 MAIN WHEEL FOUND WITH FLAT TIRE AFTER FIVE FLIGHT CYCLES FROM INSTALLATION SINCE LAST SOP VISIT (O/H). INSPECTION REVEALED THAT THE BOLTS NR 9 AND 15 WERE FOUND WITH 2-3 THREADS VISIBLE ABOVE THE TOP OF THE NUT - BOLT NR 3 SHARED (IRREGULAR) STARSDR CA140623006Control Cable · stretched(CAN) UN-ABLE TO OBTAIN PROPER HORIZONTAL STAB TRIM CABLE TENSIONS. NEW HORIZONTAL STAB TRIM CABLES INSTALLED AND RIGGED IAW BOEING 737-800 MM 27-41-000-802 AND 27-41-82-000-802.SDR CA140623005Floorbeam · corroded(CAN) LEVEL 3 CORROSION FWD PASSENGER WET AREA AT BS 270 UPPER SURFACE OF FLOOR BEAM. REPAIRED IAW SERVICE REQUEST 4-2537007535 INSTRUCTIONS AND ENGINEERING REPAIR ORDER 11566.SDR CA140625008Floorbeam · corroded(CAN) CORROSION, FWD PASSENGER WET AREA AT BS 294, UPPER SURFACE OF FLOORBEAM REPAIRED IAW SR 4-2533437668, AND EO.SDR CA140625002Floorbeam · corroded(CAN) CORROSION AFT WET AREA BS 947.5, RBL 7 TO LBL 52 TOP SURFACE OF FLOORBEAM REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5, REV 50 AND SERVICE REQUEST 3-2869338901, INSTRUCTIONS AND EO 11587, PART 1 AND 2.SDR CA140623021Floorbeam · corroded(CAN) CORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION FLOORBEAM WEB AT BS 616 - 639, LBL 65 - 71. REPAIRED IAW SERVICE REQUEST 4-2555431155 AND ERO 11575.SDR CA140623020Web · corroded(CAN) CORROSION IN PASSENGER COMPARTMENT CENTER SECTION ON WEB AT BS 639 - 663.75, LBL 65 - 71. REPAIRED IAW SR 4-2555431155.SDR CA140623019Web · corrodedCORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION ON WEB AT BS 601 TO 616 RBL 65 TO 71. REPAIRED IAW SERVICE REQUEST NR 4-2555431155 AND CASCADE ENGINEERING REPAIR ORDER 11575.SDR CA140623015Floorbeam · corrodedCORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT SPLICE BS 773 BETWEEN RBL 13.5 TO LBL 8.5. REPAIRED IAW SERVICE REQUEST 4-2570223763 INSTRUCTIONS AND CASCADE ENGINEERING REPAIR ORDER 11579.SDR CA140623014Web · corrodedPASSENGER COMPARTMENT CENTER SECTION ON WEB AT BS 616 TO 639, LBL 65 TO 71 CORRODED. REPAIRED IAW SERVICE REQUEST NR 4-2555431155 AND ENGINEERING REPAIR ORDER 11575.SDR CA140623013Floor Support · corroded(CAN) CORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION FLOORBEAM WEB AT BS 639 - 663.75, LBL 65 - 71. REPAIRED IAW SERVICE REQUEST 4-2555431155 AND ERO 11575.SDR CA140623012Floor Support · corroded(CAN) CORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION FLOORBEAM WEB BS BS 540 - 559, RBL 65 - 71. REPAIRED IAW SERVICE REQUEST 4-2555431155 AND ERO 11575.SDR CA140623011Floor Support · corroded(CAN) CORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION FLOORBEAM WEB AT BS 578 - 601, RBL 65 - 71. REPAIRED IAW SERVICE REQUEST 4-2555431155 AND ERO 11575.SDR CA140623010Floorbeam · corroded(CAN) CORROSION FOUND ON PASSENGER COMPARTMENT CENTER SECTION FLOORBEAM WEB BS 601 - 616, RBL 65 - 71. REPAIRED IAW SERVICE REQUEST 4-2555431155 AND ERO 11575.SDR CA140623009Floorbeam · corroded(CAN) CORROSION FOUND ON FWD PASSENGER WET AREA AT BS 328, BETWEEN RBL 14 TO 58 UPPER AND LOWER SURFACE OF FLOORBEAM. REPAIRED IAW SERVICE REQUEST 4-2539667301.SDR CA140623008Floorbeam · corroded(CAN) CORROSION FOUND ON FWD PASSENGER WET AREA AT BS 328, BETWEEN RBL 14 TO 58 UPPER AND LOWER SURFACE OF FLOORBEAM. REPAIRED IAW SERVICE REQUEST 4-2539667301.SDR CA140623007Floorbeam · corroded(CAN) FWD PASSENGER WET AREA AT BS 360 BETWEEN LBL 8 AND RBL 41 UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED. REPAIRED IAW SERVICE REQUEST 4-2536511871.SDR SAJF2014042703013Warning System · false activationCREW ACARS MSG FLAP ASYMMETRY, TPE-LJG DIVER TO KMG.SDR SAJF2014041403011Unknown · smokeDURING CRUISE, CABIN CREW CHECK FND 1L OVERHEAD BIN HAS SMOKE EVIDENCE & CREW APPLIED HELON EXTINGUISHER. THE CREW DECIDED DIVERT TO BKK. MECHANIC CHECK FND 1L OVERHEAD BIN HAS SMOKE EVIDENCE & REMOVED CEILING PANEL, CHECKED BEHIND BIN HAS SMOKE EVIDENCE TOOSDR CA140428005Ground Wire · broken(CAN) DURING THE 2013-2014 SEASONAL OPERATION, WE HAVE EXPERIENCED SEVERAL REPEATED "FDR OFF" INTERMITTENT ILLUMINATIONS. THE EXTENSIVE TROUBLESHOOTING CARRIED OUT DID NOT ISOLATE THE FAULT AS IT WAS IT VERY HARD TO REPLICATE THE DEFECT, THE ACFT WAS OPERATEDSDR Z6WR20140331003Web · crackedAFT WEB HAS A VISIBLE CRACK IN THE OUTER FLANGE BELOW THE PLUNGER FIRESEAL MEASURING APPROX 3.0 LONG. VISUAL CRACK CONDITION VERIFIED PER ULTRASONIC INSPECTION PER NDT MANUAL PART 6.SDR ASMF201403016Warning Light · false indicationAIRCRAFT REJECTED TAKEOFF AT 50 KNOTS, DUE TO AFT CARGO DOOR LIGHT TURNED ON. PERFORMED REVISION TO THE AFT CARGO DOOR, NO FAILURE WAS DETECTED.SDR Z6WR201403110001Web · crackedAFT WEB HAS A VISIBLE CRACK MEASURING 2.4 INCHES LONG IN THE RADIUS OF THE OUTER FLANGE BELOW THE PLUNGER FIRESEAL. VISUAL CRACK CONDITION VERIFIED IAW ULTRASONIC INSPECTION IAW NDT MANUAL PART 6, VERIFIED. ALTHOUGH NOT EFFECTIVE ON THIS THRUST REVERSER ASSY,SDR ASMF201403001Adiru · inoperativeAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO DURING CRUISE THE RT ADIRU WAS INOPERATIVE. AT HMO, MX PERFORMED THE LT ADIRU OPERATIONAL TEST IAW AMM 34-21-01, TESTED CORRECT. THE RT ADIRU REPORT WAS DEFERRED IAW MEL 34-35 CAT B. AT GDL, MX REPLACSDR ASAA2014012512487Battery Pack · no testEMERGENCY LIGHT SWITCH OPS CHECKED & BATTERY PACKS FUNCTIONAL CHECK BATTERY PACKS M1672 & M1673 FAILED. ACFT GROUNDED. R & R BATTERY PACKS. OPS NORMAL, IAW 33-51-06 AND WDG 33-51-14.SDR ASMF201402002Regulator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG. MX PERSONNEL DETECTED THE RT ENG BLEED AIR REGULATOR DRAIN WITH FUEL LEAK WITHIN OPERATIONAL IAW MM 71-00-00, DISPATCHING THE AIRCRAFT IN SUCH CONDITION. AT GDL, MX PERSONNEL REPLACED RT ENG BLSDR ASMF201312012Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO RIGHT FWD OVERWING LIGHT TURNED ON. PERFORMED THE QRH 1.14 PROCEDURE, NO CONFIRMING THE FAILURE & INITIATING AGAIN SEQUENCE OF TAKEOFF. AT MEX, AS PRECAUTIONARY ACTION, PERFORMED BITE TO OVERWING EXIT DOOR FLIGHSDR CA131216017Window · cracked(CAN) DURING PREFLIGHT CHECK, CAPTAIN`S NR 2 WINDOW CRACKED. NR 2 WINDOW REPLACED IAW AMM 56-12-11. WINDOW ELECTRICAL RESISTANCE CHECK CARRIED OUT IAW AMM 30-41-21. WHCU REPLACED IAW AMM 30-41-11. WINDOW HEAT SYSTEM CHECK SERVICEABLE.SDR ASMF2013110800008Receiver · failedACFT RETURNED OF FLIGHT DUE TO EICAS MESSAGE FRM’S 342 - 440-00, 345 - 030-02, 345 - 050-02 AND 345 - 060-02. MAINTENANCE PERFORMED THE FIM 34-51 TASK’S 801, 802, 805 AND 806 PROCEDURE. VOR/MARKER AND FMC WERE REPLACED IAW AMM 34-51-01 AND AMM 34-61-02, TESTSDR P7UR20130920001Cable Assy · damagedLANDING GEAR CONTROL CABLE LOCATED AT BS 500E, LBL 45 WL 205 WAS NOT RESTING ON PULLEY BUT RESTING IN BETWEEN THE PULLEY AND PULLEY BRACKET. CABLE APPEARS TO HAVE "SLIGHT FLAT SPOT" WEAR AND PULLEY BRACKET APPEARS TO HAVE SLIGHT WEAR FROM WHERE THE CABLE WAS SDR ASAA2013071695621Power Supply · inoperativeOVERWING ESC GROUND ILLUMINATION LIGHT INOPERATIVE. ACFT GROUNDED. R & R POWER SUPPLY REF MM 33-51-06-960-806. OPS NORMAL.SDR ASMF201308007Unknown · odorACFT RETURNED TO PLATFORM AFTER ENGINES START. A RUBBER BURNING ODOR WITH NO EVIDENCE TO SMOKE. MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56 AND FIM 21-00 TASK 806 PROCEDURE, NO ODOR OR SMOKE EVIDENCES WERE FOUND. THSDR ASMF20130531013Skin · damagedCAPTAIN REPORTED A LIGHTNING STRIKE DURING APPROACH IN THE FUSELAGE SKIN. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING A PERFORATION OUT OF LIMITS OF .1250" DIAMETER AT BS 480. FUSELAGE SKIN AT BS 480 WAS REPAIRED IAW SRM 53SDR ASAA2013042794630Terminal Block · corrodedWHILE ACCOMPLISHING CENTER LIGHTS CHECK, FOUND FWD ENTRY EXIT SIGN ADJACENT TO F/A SEAT INOPERATIVE. ACFT GROUNDED. R & R FWD ENTRY EMERGENCY EXIT SIGN. REPLACED ASSY TWICE, NO GOOD. REF AMM 33-51-01-960-802. REF WDM 33-51-21 FOUND BAD GROUND APPROX 500 OHMS SDR CA130325001Bolt · sheared(CAN) NR 2 MAIN WHEEL FOUND WITH 1 TIE BOLT SHEARED.SDR ASAA2013030894134Guide Arm · out of adjustL1 DOOR IS STIFF TO CLOSE, DIFFICULT TO LOCK. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT IAW AMM 52-11-00-820-801. REMOVED L-1 DOOR GUIDE ARM DUE TO FROZEN ADJUSTER REF AMM 52-11-21-000-802. INSTALLED NEW GUIDE ARM REF MM TASK 52-11-21-400-802 STEPS A THRU FSDR ASMF201303020Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED. MAINTENANCE PERSONNEL DETECTED THE FUEL PUMP SEAL DAMAGED ON RT ENGINE, FUEL PUMP WAS REPLACED IAW AMM 73-11-01 AND TESTED IAW AMM 71-00-00, ALL CORRECT.SDR O4HR2013022201Wheel · failedWHEEL HUB FAILURE.SDR CA130218001Wire · shorted(CAN) RT AFT MAINTANK FUEL PUMP LOW PRESSURE ANNUNCIATOR ILLUMINATED. FOUND SHORTED WIRES ON FUEL PUMP WIRING HARNESS. W1134-3601R-18, 360IY-18, W1134-360IB-18.SDR ASMF201303007Snubber · crackedDURING TRANSIT CHECK, IT WAS DETECTED A CRACK AT THE EXTERNAL SKIN LOWER HINGE. MX PERSONNEL PERFORMED REVISION DETECTING THE EXTERNAL SKIN LOWER HINGE OUT OF LIMITS IAW SRM 52-10-01 PARA B (1)(A). THE ACFT WAS INSPECTED AND FOUND SAFE FOR THE INTENDED SPECISDR ASMF201303006Connector · out of positionCAPTAIN REPORTED THAT DURING CLIMB AN ELECTRICAL CABLE BURNED ODOR WITH NO EVIDENCE OF SMOKE, DISAPPEARING DURING CLIMB. MX PERSONNEL PERFORMED FIM 21-00, TASK 806 PROCEDURE AND SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING A FORWASDR CA130114001Rod End · broken(CAN) APU FAILED TO START ON GROUND. PILOT REPORTED IT, MAINTENANCE HAVE PUT SYS ON MEL 49-01. DURING NIGHT TURN-OVER MAINTENANCE TROUBLESHOT FAULTY APU START AND FOUND APU INLET DOOR ROD END, X2, BROKEN, ACTUATOR STILL WORKING GOOD.SDR SCNA20121031049Battery Pack · failedROW 11 RIGHT SIDE EMERGENCY BATTERY PACK FAILED CAPACITY CHECK.SDR CALA2012100900660Sign · missingMID CABIN OVERHEAD EXIT SIGN MISSING. AT ROW 25. REINSTALLED SIGN ON FWD SIDE, SIGN TESTED OK.SDR ASAA2012070592523Housing · gougedAFT CARGO DOOR HANDLE HOUSING IS GOUGED BEYOND LIMITS. REMOVED DAMAGED HANDLE HOUSING. BEYOND LIMITS IAW MM 52-31-15. CLEANED UP ADJACENT AREA FOR NEW HOUSING INSTALLATION. ACCOMPLISHED HFEC INSPECTION OF HANDLE CAVITY AFT CARGO DOOR IAW NDT MANUAL PART SESDR ASMF201207002Line · leakingDURING PUSH BACK, DETECTED A HYD LEAK IN THE RT MLG. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED FLEXIBLE BRAKE LINE NR 4 IAW MM 32-41-00, TESTED CORRECT.
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