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 COMA0760220Control Handle · faultyFLIGHT 5686 - FLAP FAIL MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE AS INDICATED BY FECU INTERROGATION. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS.SDR RAIA00702051Flap · malfunctionedFLT NR 5464 - STL - FLAPS WOULD NOT RETRACT AFTER T/O. MAINTENANCE RESET POWER TO SYSTEM. OPS CHECK GOOD OF FLAP EXTENSION AND RETRACTION, NO DEFECTS NOTED.SDR TRAX200700301Flap · failedFLAP FAIL AT 0 DEGREE ON APPROACH. EMERGENCY DECLARED.SDR RAIA00702045Flap · malfunctionedFLT NR 5518 - AUS - FLAPS STUCK AT 9 DEGREES AFTER TAKEOFF. MAINTENANCE RESET FLAP SYSTEM. OPS CHECKS GOOD AT THIS TIME.SDR NSVA20070052Control Valve · malfunctionedFLAPS DEPLOY BETWEEN 0 - 7 DEGREES IN FLIGHT. REMOVED AND REPLACED FLAP CONTROL VALUE IAW CHAPTER 27-51-15-04 THE SAAB 340 AMM PN OFF HP1416100-5 PN ON HP1416100-5 SN OFF 1327 SN ON 1435. PERFORMED OPS CHECK AND LEAK CHECK IAW 27-51-00, OPS AND LEAK CHECK GOSDR CA070320008Control Cable · frayed(CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN RT WING GAP AREA. (TC NR 20070320008)SDR CA070320006Control Cable · frayed(CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN LT WING GAP AREA. (TC NR 20070320006)SDR 2007FA0000189Control Cable · frayedPILOT REPORTED EXCESSIVE MOVEMENT IN LT FLAP DURING PRE-FLIGHT WALK AROUND OF AIRCRAFT. INITIAL INVESTIGATION BY MAINTENANCE PERSONNEL CONFIRMED FINDINGS. MAINTENANCE PERSONNEL DISCOVERED THAT CABLE P/N 0510105-93 HAD MULTIPLE BROKEN STRANDS/FRAYING NEAR THESDR COMA0760211Flap · obstructedFLIGHT 5174 - EN ROUTE CID-CVG RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REMOVED ICE BETWEEN THE LEFT AND RIGHT INBOARD FLAP LEADING EDGE AND THE MOVEABLE VANE.SDR DU4R2007072Torque Tube · corrodedFOUND CORROSION INSIDE LT I/B T/E FLAP TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE WITH P/N 117N2105-1 NSN, CARRIAGE ASSY WITH P/N 113N2100-13 S/N 248, FAIL SAFE AND P/N 113N2108-1 NSN IAW DELTA EA 06-097981-14 REV A.SDR 2007UALA00584Unknown · unknownAFTER TAKEOFF, FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS FINALLY RETRACTED NORMALLY. FLAP TRANSMITTERS OUT OF TOLERANCE. ADJUSTED TRANSMITTERS. OPERATIONAL CHECKS GOOD.SDR DU4R2007073Torque Tube · corrodedFOUND CORROSION INSIDE LT I/B T/E FLAP TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE WITH P/N 117N2105-1 NSN, CARRIAGE ASSY WITH P/N 113N2100-13 S/N 248, FAIL SAFE AND P/N 113N2108-1 NSN IAW DELTA EA 06-097981-14 REV A.SDR VNAA0702013Flap System · inoperativeCREW REPORTED A FLAP FAIL MESSAGE DISPLAYED AFTER TAKEOFF. CREW ELECTED TO CONTINUE FLIGHT AND LAND IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE AIRCRAFT SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.SDR A6WA200740083Potentiometer · out of adjustFLAPS FAIL CAS MSG AT ZERO DEGREES, LANDING WEIGHT 40,000 LBS, TOUCHDOWN SPEED 160 KNOTS, MAX BRAKE TEMP = 6.0 FLAP LANDING PERFORMED RIG CHECK OF BPSU`S, IAW AMM 27-51-10, FOUND NR 6 AND NR 7 POTENTIOMETERS OUT OF ADJUSTMENT. ADJUSTED POTENTIOMETERS AND PERSDR 2007UALA00579Unknown · unknownON FLAP EXTENSION FLAPS DID NOT EXTEND TO SELECTED SETTING, 10 DEG SELECTED ON HANDLE. INDICATOR SPLIT WITH LEFT INDICATING BETWEEN 0 AND 1, RIGHT INDICATING 1, RIGHT INDICATING. CAUSED BY A FAULTY LEFT HAND FLAP TRANSMITTER. REPLACED LEFT HAND FLAP TRANSMITSDR COMA0760207Flap · malfunctionedFLIGHT 5294 - DURING PIT APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.SDR COMA0760206Flap · malfunctionedFLIGHT 5446 - FLAPS FAIL AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.SDR SB07016Flap · out of rigCLT FLT750 ON DESCENT INTO CLT FROM GCM, WHEN FLAPS WERE SELECTED TO 30 UNITS, THE AIRCRAFT ROLLS TO THE LEFT. WINGS CAN BE KEPT LEVEL WITH 3 DEGREES OF RIGHT AILERON. FUEL WAS BALANCED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE CABLE DSDR COMA0760203Flap · malfunctionedFLIGHT 5689 - FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 27-046 AD INCLUDING FLAP FLEX SHAFT REJUVE TASK. NO FURTHER DEFECTS.SDR DA62007F00002Motor · damagedFLAPS FAILED IN DOWN POSITION ON LANDING. DURING TROUBLESHOOTING AND INSPECTION FOUND FLAP MOTOR AND WIRING TO BE SUBMERGED IN WATER APPROXIMATELY 1.5 INCHES TO 2 INCHES DEEP. AFTER WATER WAS CLEANED UP AND MOTOR WAS ALLOWED TO DRY FLAPS FUNCTIONED PROPERLY.SDR TRAX200700271Warning System · activatedDURING APPROACH AT APPROX 400 W/FLAPS 30 DEG, RECEIVED "FLAP UNLOCK". EXECUTED MISSED APPROACH. RAN QRH. EXECUTED NO FLAP LANDING, EMERGENCY DECLARED.SDR ABXA070049Fseu · defectiveA 27 51 12 00 STATUS MSG; FLAP/SLAT ELEC FLAP INDICATOR INDICATES 1 WITH FLAP LEVER IN UP POSITION. REPLACED FSEU IAW B767 MM 27-51-01.SDR COMA0760199Flap · malfunctionedFLIGHT 5138 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.SDR CA070219003Flap System · jammed(CAN) ON APPROACH, CREW RECEIVED SLATS FAIL MESSAGE, ALSO, FLAPS STOPPED AT 8 DEGREES. FLIGHT LANDED WITHOUT INCIDENT. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE. (TC NR 20070219003)SDR TRAX200700245Flap · malfunctionedFLAPS FAIL WHEN SELECTING FLAPS 20 DEGREES ON APPROACH. LEFT AT 8 DEGREES, RIGHT AT 10 DEGREES. EMERGENCY DECLARED.SDR SWAA070994Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA070993Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR CA070219009Flap System · failed(CAN) DURING APPROACH WHEN FLAP SELECTED TO 8 DEG, CREW RECEIVED (FLAP FAIL) CAUTION MESSAGE ON EICAS, CONTROL POSITION DISPLAY SHOWED 2DEG ON LT FLAP AND 0 DEG ON RT FLAP. ZERO DEG FLAP LANDING CARRIED OUT. AFTER LANDING CREW PERFORMED VISUAL INSPECTION OF TSDR AMW082683Link · wornAFTER TAKEOFF, FLAPS STUCK AT 17 DEGREES. THE CAPTAIN RETURNED TO FIELD AND DECLARED AN EMERGENCY. ACFT LANDED AND FLAPS RETRACTED TO ZERO WITH NO FURTHER INCIDENT. REMOVED AND REPLACED RT FLAP SAFETY SWITCH LINKS AND BUSHINGS. OPS CK NORMAL.SDR DXTA200701952Flap System · unknownFLAPS FAIL DURING APPROACH AND DID NOT RESET. FLAPS FAILED AT 0* INDICATION (UP). PERFORMED VISUAL INSPECTION OF FLAP SYSTEM. CHECKED BITE CODES, CLEARED BITE CODES. CYCLED FLAPS AND RECHECKED BITE CODES - NO DEFECTS AT THIS TIME. OPS CHECKS - GOOD - ALL ISDR SWAA070920Torque Tube · wornDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING AFT FLAP OUTBOARD TORQUE TUBE FAILED CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR 2007FA0000225Bracket · crackedTHIS BRACKET IS RIVETED IN THE CENTER TUNNEL AND ACCEPTS (2) BOLTS AT THE FORWARD SIDE OF THE FLAP HANDLE SUPPORT MOUNT. THIS IS A DIFFICULT AREA TO SEE, EVEN WITH A MIRROR. WE HAVE FOUND (6) CRACKED BRACKETS SO FAR TO DATE. SUSPECT FATIGUE AND AIR LOADS CASDR DXTA200701949Flap System · malfunctionedAFTER TAKEOFF WE GOT A FLAPS FAIL AMBER CAS MESSAGE & INDICATIONS WHEN WE RETRACTED THE FLAPS THEY WERE FULLY UP. RESET DIDN'T WORK, UPON APPROACH TO LANDING SLATS ONLY CAME OUT. UPON INSPECTION FOUND FAULT "2" DISPLAYED ON FLAP CONTROLLER IN TAILCONE. PUSHEDSDR COMA0760194Flap · malfunctionedFLIGHT 5137 - DURING YYZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.SDR COMA0760193Flap · obstructedFLIGHT 5363 - DURING CLIMBOUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. REMOVED ICE AND SAND FROM FLAP AREA THAT INTERFERED WITH PROPER OPERATION OF THE FLAP SYSTEM.SDR CA070216002Motor · failed(CAN) ON FINAL APPROACH, THE PILOT SELECTED FLAPS DOWN, WHEN THE FLAPS REACHED 5 DEGREES, THE ASSOCIATED CIRCUIT BREAKER POPPED. THE PILOT OVERSHOT TO EVALUATE THE SITUATION AND THEN CARRIED OUT AN UNEVENTFUL LANDING WITH 5 DEGREE OF FLAP. UPON INVESTIGATION BSDR CA070214001Flap System · jammed(CAN) ON APPROACH, WHEN THE CREW SELECTED FLAP 8, THE FLAPS DID NOT MOVE AND THEY STAYED AT 0. CREW LANDED FLAPLESS WITHOUT INCIDENT. NO MORE DETAILS. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE. (TC NR 20070214001)SDR NSVA20070038Control Valve · malfunctionedFLAPS WOULD NOT EXTEND ON APPROACH. NO WARNINGS AURAL OR VISUAL. FLAPS TAKE 10 SECONDS TO EXTEND WHEN ACTUATED WITH HANDLE. TESTED IAW AMM 27-51-00-05 AND OPERATIONAL CHECK GOOD. PERFORMED ADJUSTMENT AND TEST OF FLAP CONTROL IAW 27-51-00-05 PROCEDURE 3 ELSDR DXTA200701946Flap System · malfunctionedON FINAL APPROACH AMBER CAS MESSAGE FLAP FAIL WHEN FLAPS/SLATS SELECTED TO 5'. ABNORMAL PROCEDURES COMPLETED AND FLAPS FAILED TO EXTEND BEYOND ABOUT 2' WITH SLATS EXTENDED. OPERATED FLAP SYSTEM THROUGH NUMEROUS CYCLES PERFORMED CONTINUITY CHECKS & GROUND CHECSDR FDKA200702069Shaft · unknownFDM 6109 MCO (1523 PHX LCL). CREW REPORTED FLAP FAIL MESSAGE. MX REMOVED AND REPLACED HARNESS W170, RIGHT BRACKET FLEX SHAFT.SDR 68DA2Motor · faultyON APPROACH, NO PAX, PILOT NOTICED A SMELL OF ELECTRICAL SMOKE, CONCURRENTLY WITH A POPPED FLAP MOTOR CIRCUIT BREAKER POPPING. ON INSPECTION, MAINTENANCE FOUND AN INOP FLAP MOTOR.SDR CA070213001Fcu · malfunctioned(CAN) FLAP FAIL MESSAGE RECEIVED IN-FLIGHT. AIRCRAFT LANDED UNEVENTFUL WITH FLAPS ZERO (FLAPS WOULD NOT MOVE). (TC NR 20070213001)SDR COMA0760181Flap · malfunctionedFLIGHT 5448 - DURING BGR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.SDR FDKA200702065Control Unit · malfunctionedFDM 6018 BNA-MCO (0616 PHX LCL). FLAPS FAIL MESSAGE AT 0 DEGREES. MX REMOVED AND REPLACED FECU, PERFORMED RIGGING, OPS CHECKED GOOD.SDR AMW082600Switch · dirtyAFTER T/O, FLAPS STUCK AT 17 DEGREES. CREW CALLED IT IN AND TOWER DECLARED EMERGENCY. EMERGENCY WAS THEN IMMEDIATELY TERMINATED A/C FLEW ITS ROUTE, ARRIVED ON TIME, NO FURTHER INCIDENT. (DIRECTED BY FAA TO ENTER AS AN SDR, INITIALLY ENTERED AS AN MIS) CLEASDR COMA0760178Flap · malfunctionedFLIGHT 5052 - RECEIVED FLAPS FAIL MESSAGE ON APPROACH. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.SDR TRAX200700212Flap · malfunctionedFLAPS FAIL ON APPROACH. EMERGENCY DECLARED.SDR TRAX200700211Flap · malfunctionedFLAPS FAILED AT 0 DEGREES ON APP INTO GRR. EMERGENCY DECLARED.SDR QXEA200700159Flap System · unknownSEA FLIGHT NR 2328: FLAP POWER CAUTION LIGHT ILLUMINATED DURING PUSH BACK. RESET C/B PER EA CHECKLIST. LIGHT WAS STILL ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED Q400 FIM TASK 27-50-00-810-802 AND OPS TEST OF THE WING FLAPS IAW Q400 AMMSDR CA070209022Flap System · frozen(CAN) THE COLD WEATHER HAS AFFECTED SEVERAL AIRCRAFT IN THE FLEET OF 9. IN -25 C OR COLDER TEMPERATURES, THE CIRCUIT BREAKERS POP AFTER LANDING WHEN THE FLAPS ARE SELECTED (TC NR 20070209022)
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