JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap Control System, newest first.
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 jasc_code = '2750' 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 jasc_code = '2750' 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 COMA0060233Bpsu · malfunctionedFLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BPSU.SDR 2000UALA00097Relay · failedT/E FLAP DISAGREE LIGHT ON SHORT FINAL. FLAPS STOPPED AND REMAINED AT 23 DEGREES. AMBER ALERT. *S/D* A FAULTY T/E FLAP SHUTOFF VALVE RELAY (K351) CAUSED THE T/E FLAP SHUTOFF VALVE TO CLOSE WHICH INHIBITED FLAP MOVEMENT. WITH FLAP MOVEMENT INHIBITED AT 23 SDR USAASB00052Flap · failedCUN - FLT 1515 - ON APPROACH, CAPTAIN COULD NOT EXTEND FLAPS BEYOND 10 DEGREES. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND CIRCUIT BREAKERS CHECKED OK. PUMPS AND PRESSURE WERE ALSO OK. CREW ATTEMPTED ALTERNATE FLAP EXTENSION PROCEDURE BUT THISDR AU000173Valve · faulty(AUS) FLAP SOLENOID VALVE SUSPECT FAULTY.SDR CA000320032Fcu · failed(CAN) THE CREW RECEIVED A FLAPS FAIL WARNING. MAINTENANCE REPLACED THE FECU AND THE BPSU P/N 855D100-9.SDR COMA0010029Control Unit · malfunctionedFLAP CONTROL FAULT. REPLACED THE FLAP CONTROL UNIT.SDR CA000222012Flap · twisted(CAN) FLAP FAIL MESSAGE AFTER SELECTED AND REACHED APPROXIMATELY 20 DEGREES. LEFT FLAP TWISTED. INBOARD END AT APPROXIMATELY ZERO DEGREES AND OUTBOARD END AT APPROXIMATELY 8 DEGREES. (X)SDR CA000306029Switch · stuck(CAN) DURING UNSCHED MAINT ON FLAP RIGGING, LT INBOARD FLAP ACTUATOR DRIVE WAS DISCONNECTED AT FLAP ATTACH. FLAPS WERE FULLY DOWN (35 DEGREES). FLAP SELECTED FROM DOWN TO 17 DEGREES AND FLAPS TRAVELLED TO 17 DEGREES. THE LT SPLIT FLAP SWITCH ACTUATOR HAD MOSDR CA000320019Fcu · failed(CAN) DURING APPROACH, THE FLAPS WERE SET TO 45 DEGREES AND THE CREW GOT A FLAPS FAIL WARNING. THE FLAPS STOPPED AT 34 DEGREES. A RESET WAS ATTEMPTED WITHOUT SUCCESS. MAINTENANCE TRACED THE PROBLEM TO A FAILED FLAP ELECTRONIC CONTROL UNIT AND REPLACED IT.SDR MALA000207Jackscrew · lack of lubeON APPROACH SELECTED FLAPS 18 DEGREES, FLAP INOP CAUTION ILLUMINATED WITH FLAP FAULT. MAINTENANCE PERFORMED TORQUE LIMITER RESET & FLAP FAULT RESET LUBED BALL NUTS ON SCREW JACKS IAW RJ 85 MM 27-50-00. PERFORMED FUNCTIONAL TEST OF FLAPS IAW 27-50-00. ALSO, SDR EISA2000018Warning Light · illuminatedON TAKEOFF, NR 1 LEADING EDGE FLAP UNSAFE LIGHT ILLUMINATED. AIR TURN BACK TO (OVL). (M)SDR 2000ZZZX841Control Cable · frayedDURING AN ANNUAL INSPECTION, THE OUTBOARD END OF THE RIGHT FLAP CABLE WAS FOUND FRAYED .50 INCH AFT OF THE CLEVIS END. THIS MAY HAVE BEEN CAUSED BY WIND ON THE FLAP FLEXING THE CABLE AT THAT POINT. SUBMITTER SUGGESTED AGE OF THE CABLE WAS POSSIBLY A FACTOR ASDR F3LA00015Bearing · damagedDURING C-5 CHECK, INSPECTION FOUND EXCESSIVE PLAY IN LT WING OUTBOARD MIDFLAP NR 1 SPINDLE BEARINGS. MAINTENANCE REPLACED SPINDLE BEARINGS PER OHM 57-53-35. (M)SDR F3LA00014Bearing · damagedDEN - DURING C-5 CHECK, INSPECTION FOUND EXCESSIVE PLAY IN LT WING NR 2 INBOARD FLAP SPINDLE BEARINGS. MAINTENANCE REPLACED SPINDLE BEARINGS AND TORQUED NR 2 INBOARD FLAP CARRIAGE PER MM 27-51-34. (M)SDR 0000372769Power Unit · leakingON APPROACH TO LGA, AIRCRAFT LOST BOTH PRESSURE AND QUANTITY IN THE 'A' HYDRAULIC SYSTEM. CREW DECIDED TO DIVERT TO JFK DUE TO LONGER RUNWAYS. FLIGHT 522 MADE AN UNEVENTFUL LANDING IN JFK. NWA MAINTENANCE REPLACED THE RIGHT OUTBOARD FLAP HYDRAULIC POWER UNISDR 20000329SH003Jackscrew · wrong partDURING REPLACEMENT OF FLAP ACTUATORS, LEFT INBOARD FLAP MOVED IN THE OPPOSITE DIRECTION OF FLAP SELECTOR POSITION. REMOVED FLAP ACTUATOR AND DETERMINED THAT DRIVE ASSEMBLY WAS INCORRECT FOR INBOARD ACTUATOR. (X)SDR COMA0060134Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU.SDR CA000203017Control Cable · worn(CAN) DURING ROUTINE 100 HR INSPECTION WE FOUND A CABLE THAT WAS SHOWING SIGNS OF WEAR. CABLE WAS REMOVED AND INSPECTED. SEVERAL BROKEN STRANDS WERE FOUND. IT SHOULD BE NOTED THAT THE WEAR CAN ONLY BE SEEN WITH THE FLAPS IN THE FULL DOWN POSITION. WHEN FLAPSSDR 2000UALA00053Flap · out of rigON APPROACH INTO LAX, FLAPS LOCKED UP AT POSITION 1. MADE A NO FLAP LANDING. *S/D* LEFT HAND FLAP SYSTEM REQUIRED RIGGING. SYSTEM WAS RIGGED AND HAS BEEN FUNCTIONAL SINCE.SDR AU000203017Control Cable · worn(AU) DURING ROUTINE 100 HOUR INSPECTION, FOUND A CABLE THAT WAS SHOWING SIGNS OF WEAR. CABLE WAS REMOVED AND INSPECTED. SEVERAL BROKEN STRANDS WERE FOUND. IT SHOULD BE NOTED THE WEAR CAN ONLY BE SEEN WITH THE FLAPS IN THE FULL DOWN POSITION. WHEN FLAPS WERSDR MALA000132Indicator · failedDTW - FLT 2808 - LOW FLAPS WARNING AT 300 FT WITH FLAPS IN 20 DEGREE POSITION AND INDICATING 20 DEGREES. MAINTENANCE REPLACED INDICATOR, RE-RIGGED R POT, ALL WORK DONE IAW SF340 MM2, ALL CHECKS GOOD AT THIS TIME. (M)SDR 20000328SH003Control Cable · failedCABLE WITH A TWIST TEST OF THE CABLE END SIMILAR TO THE DUKES CABLES ON THE PIPER PA31 FLAP SYSTEMS. (X)SDR COMA0060123Te Flap · failedFLAPS FAILED AT 45 DEGREES RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060120Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE RIGHT BPSU.SDR GAIA0045Flap · malfunctionedFLT 1760 - FWA-MEM - THE CREW RAISED THE FLAPS AND HAD THE OUTBOARD FLAPS STICK AT 4 DEGREES. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. MAINTENANCE USED THE ALTERNATE METHOD TO RAISE THE FLAPS TO ZERO DEGSDR EIA2000007Flap · malfunctionedKLCK - ON TAXI OUT, PLACED FLAP HANDLE TO 5 DEGREE POSITION. SLATS EXTENDED AND FLAPS STAYED 0 DEGREES. SELECTED FLAPS 40 DEGREES; FLAPS WENT TO 40 DEGREES. RETRACTED FLAPS TO 25 DEGREES POSITION; FLAPS RETRACTED AND THEN EXTENDED TO 25 DEGREES. PLACED FLASDR UPS00231510Gimbal · crackedINSPECTION TYPE:C, RIGHT I/B TRAILING EDGE FLAP, GIMBAL ELECTRIC ASSY, CRACKED AT NR 5 FLAP TRANSMISSION ATTACH POINT. GIMBAL REPLACED IAW MM 27-51-251, ADJUST/TEST CARRIED OUT IAW MM 27-51-22.SDR 20000428AP003Actuator · failedON APPROACH INTO JVY, THE FIRST NOTCH OF FLAPS EXTENDED NORMALLY, BUT THEN THE RIGHT FLAP ACTUATOR FAILED AND ALLOWED THE RIGHT FLAP TO RETRACT. THE PILOT CONTROLLED THE AIRCAFT WITH DIFFERENTIAL AILERON AND POWER AND LANDED WITHOUT INCIDENT AT JVY. MAINTENASDR COMA0010013Warning System · activatedFLAP DISAGREE WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. OPERATON OF FLAPS NORMAL.SDR ASOA00007Fecu · inoperativeCREW GOT FLAP FAIL MESSAGE WHEN SELECTING FLAPS FROM EIGHT TO ZERO DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FECU. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)SDR AU000096Connector · contaminated(AUS) NACELLE FLAP ACTUATOR ELECTRICAL CONNECTORS PNO P1758 AND PNO P1759 CONTAMINATED WITH MOISTURE.SDR COMA0060070Warning Light · illuminatedFLAPS FAIL MESSAGE RESET AND DEFERRED FLAP MAINTENANCE PER AD 98-20-01.SDR COMA0060069Bpsu · malfFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU.SDR CA000209057Control Unit · failed(CAN) FLAPS FAIL AT 0 DEG. RT BPSU AND FCU REPLACED.SDR CA000209056Controller · failed(CAN) ON FINAL APPROACH, SELECTED FLAPS TO 30 DEGREES AND HAD FLAP FAIL MESSAGE. RESET FLAP CONTROL 1&2, CYCLED FLAPS SEVERAL TIMES. NO FAULT FOUND.SDR CA000201025Switch · frozen(CAN) ON APPROACH THE CREW SELECTED LANDING FLAPS. THE FLAPS EXTENDED TO LANDING POSITION (35 DEGREES), BUT THE RIGHT INBOARD FLAP PANEL STAYED RETRACTED. MAINTENANCE FOUND THE RIGHT INBOARD FLEX DRIVE CABLE SWAGED END HAD SLIPPED ON THE CABLE END, ALLOWING THSDR DHL200071773DBracket · brokenAT D-CK, LEFT WING MID FLAP O/B CARRIAGE LEAF SPRING ATTACH BRACKET BROKEN. REMOVED AND REPLACED BRACKET AT LT MID FLAP OUTBOARD CARRIAGE SPRING PER 727 MM 27-51-13. REF: N/R 1679.SDR COMA0060058Warning Sys · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR CA000209055Lever · failed(CAN) ON APPROACH FLAP FAIL MESSAGE APPEARED WITH NO MOVEMENT OF FLAP LEVER. FLAPS INSPECTED AS PER AD CF98-14R1, NO FAULT FOUND.SDR CA000209053Flap · out of rig(CAN) ON APPROACH, FLAPS FAIL MESSAGE.FLAPS FAILED AT 0 DEG.FLAPS INSPECTED AND BREAK AWAY TORQUE WITHIN LIMITS. FOUND LT FLAP OUT OF RIG. SYSTEM RE-RIGGED.SDR AU000128061Flex Drive · broken(AU) THE PILOT FOUND THE FLAP DOWN TO 17 DEGREES, BUT THEY JAMMED AT 8 DEGREES. FOUND THE LT INBOARD FLAP FLEX DRIVE BROKEN APPROXIMATELY 4 INCHES FROM THE END. SHAFT REPLACED.SDR COMA0060046Te Flaps · stuckFLAPS FAILED MESSAGE, FLAPS STUCK AT 0 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060038Bpsu · failedFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT BPSU.SDR COMA0060052Bpsu · malfuctionedFLAPS FAILED. REPLACED THE LEFT HAND BPSU.SDR COMA0060040Fecu · malfunctionedFLAPS FAILED AT 3 DEGREES. REPLACED THE FECU.SDR SWIA971646Control Unit · malfunctionedON CLIMB-OUT, CONTROL FAULT APPEARED WITH FLAP HANDLE UP, OVERHEAD FLAP CONTROL PANEL INDICATED NAC WAS FULLY EXTENDED. CONTROL FAULT INITIALLY WOULD NOT RESET, RESET SUCCESSFUL PER QRH 3RD TRY. RETURNED TO PDX. REPLACED FLAP CONTROL UNIT IAW 270000 AND CLESDR 2000UALA00011Control Cable · out of adjLEADING AND TRAILING FLAPS STOPPED BETWEEN 3 AND 5. *S/D* INSPECTED SYSTEM AND FOUND 3-32ND CABLES WFA AND WFB AT 25 LBS. HANDLE WAS SLUGGISH IN EITHER DIRECTION. ADJUSTED CABLES TO 58 LBSAT 60 DEG. HANDLE OPERATION SMOOTH AND FLAPS OPERATING WITHINNORMASDR SWIA971643Controller · malfunctionedCONTROL FAULT ILLUMINATED IN FLIGHT AND WOULD NOT CANCEL. FAULT CORRECTED ITSELF AFTER 5 MINUTES. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST PER MM 275000. FUNCTIONAL TEST GOOD, NO DISCREPENCIES NOTED. UNABLE TO DUPLICATE PROBLEM.SDR COMA0010002Flap · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. COULD NOT DUPLICATE, NO FAULTS FOUND IN FLAP SYSTEM.SDR COMA0060013Bpsu · malfunctionedFLAPS FAILED AFTER TAKE OFF. REPLACED THE RIGHT HAND BPSU.
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