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.

SDR COMA0860285Flap System · malfunctionedRECEIVED FLAP FAIL MESSAGE AT CRUISE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I0001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. (S)Jun 12, 2008 · N927CA · Cndair CL6002B19SDR A6WA200840458Flap System · malfunctionedFLAPS FAILED AT ZERO IN FLIGHT. BRAKE TEMPS WERE IN NORMAL RANGE AT LANDING. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEM RESET OK. AIRCRAFT RELEASED FOR SERVICE. (A)Jun 9, 2008 · N425AW · Cndair CL6002B19SDR 2008UALA03115Flap · malfunctionedFLAP RETRACT PROBLEM CAUSED DIVERSION. UNABLE TO DUPLICATE. ADJUSTED CABLE TENSION AND SERVICED NR 7 FLAP TRANSMISSION.Jun 2, 2008 · N318UA · Boeing 737322SDR 2008UALA03148Solenoid Valve · faultyFLAPS PRIMARY FAIL PRIMARY (HYDRAULIC) FLAPS DRIVE FAILURE. FLAPS OPERATING IN SECONDARY (ELECTRIC) MODE. CAUTION MSG-2720372 LATCHD DC MODE. FAILED HIGH LIFT CONTROLS TEST. FOUND FLAPS PRIMARY LOW SPEED SOLENOID VALVE AT FAULT AND REPLACED REF MM 27-51-05May 31, 2008 · N799UA · Boeing 777222SDR MALA080113Control Valve · failedFLAPS WOULD NOT EXTEND, PERFORMED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL VALVE.May 31, 2008 · N434XJ · Saab 340BSDR TRAX200800695Flap System · failedFLAP FAIL AT 8 DEGREES (EN ROUTE TO ATL ACFT DIVERTED TO MDT DUE TO MTC, EMERGENCY DECLARED). PERFORMED EXTERNAL VISUAL CHECK OF FLAPS IN ALL SETTINGS. NO TWISTING OR SKEWING DETECTED. CYCLED FLAPS MULTIPLE TIMES WITH NO FURTHER FAULTS NOTED. INTERROGATED May 27, 2008 · N844AS · Cndair CL6002B19SDR BB08097Transmission · malfunctionedCLT FLT 1075 EN-ROUTE PHL TO CLT. ON APPROACH, A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WAS INDICATED. ALSO, THE TRAILING EDGE FLAPS STAYED AT 20 DEGREES WITH THE FLAPS SELECTED TO 25 DEGREES. THE CREW PERFORMED A GO-AROUND, AND THEN COMPLETED THE QRH May 25, 2008 · N917UW · Boeing 757225SDR TRAX200800677Bpsu · malfunctionedFLAPS FAIL AT ZERO WHEN SELECTING 8 DEGREES. FLT 4349 CX EMERGENCY DECLARED. REMOVED AND REPLACED BPSU LT SIDE IAW CRJ200 AMM 27-50-01. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME. [SDR CLOSED](B)May 21, 2008 · N680BR · Cndair CL6002B19SDR 2008FA0000361Fcu · failedAC HAS BEEN EXPERIENCING INTERMITTENT FLAP SYSTEM FAILURES IN DIFFERENT MODES OF FLIGHT, PRIMARILY DURING APPROACH. TROUBLESHOOTING IAW MM RECOMMENDED REPLACEMENT OF FLAP CONTROL UNIT DUE TO IMMEDIATE ( INTERMITTENT) FAILURES AFTER FLAP MOVEMENT SELECTION. AFTMay 21, 2008 · N779AZ · Cndair CL6002B16SDR 2008FA0000359Control Handle · damagedAIRCRAFT HAD BEEN EXPERIENCING MULTIPLE INFLIGHT FLAP FAILURES WHICH WERE NOT DUPLICATED ON THE GROUND. DURING TROUBLESHOOTING OF THE FLAP SYSTEM, FLAPS WOULD NOT MOVE FROM 45 DEGREES TO 30 DEGREES WHEN SELECTED. NO FAILURE WAS DISPLAYED BY THE AIRCRAFT. FLAP May 21, 2008 · N779AZ · Cndair CL6002B16SDR 08FDEA01942Check Valve · failedAFTER TAKEOFF, FLAPS UP GOT LEVEL 2 "FLAP DISAG". FLAPS INDICATED 8/7 (LEFT) AND 5/4 RIGHT WING. FLAP HANDLE BACK TO LAST POSITION AND FLAPS WOULD NOT MOVE. HANDLE BACK TO UP NO CHANGE, WHILE MANEUVERING TO LAND FLAPS INDICATED 3/1 AND UP. RETURNED TO MEM.May 21, 2008 · N68052 · Doug MD1010FSDR R61A200800008Flap · malfunctionedCREW REPORTED FLAP FAIL MESSAGE ON EICAS DURING DESCENT. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT. RESET THE SF. ACE AND CLEARED INHIBITS. SYSTEM OPERATIONAL CHECK GOOD AND AIRCRAFTMay 21, 2008 · N125HQ · Emb ERJ170200LRSDR 2008UALA02957Electronic Unit · activatedPRIMARY CHANNEL MESSAGE ON MAINTENANCE PAGE WHEN LOWERING FLAPS AND FLAPS ARE SLOW. SUSPECT FAULTY FSEU. REPLACED NR 2 FSEU REF. MM 21-51-01. OP CHECKS GOOD. AC OK FOR SERVICE.May 20, 2008 · N787UA · Boeing 777222SDR TRAX200800661Bpsu · inoperativeFLAPS FAIL MSG WHEN SELECTING FLAPS FROM 20 DEG TO 30 DEG FLAPS FAILED AND 20 DEG. REMOVED AND REPLACED RT FLAPS BPSU ASSY AND FECU ASSY IAW AMM 21-51-10 AND 21-51-05. OPS CHECK GOOD. (B)May 19, 2008 · N824AS · Cndair CL6002B19SDR 2008FA0000358Control Box · failedCREW REPORTED FLAP FAILURE DURING APPROACH APPROXIMATELY 8 HOURS AFTER INSTALLATION. RESET SYSTEM AND FLAPS WORKED FINE. FLEW AIRCRAFT HOME AND NO DISCREPANCIES. UNABLE TO DUPLICATE PROBLEM UNTIL SEVERAL WEEKS LATER DURING MAINTENANCE RUN. FLAPS WOULD IMMEDIATMay 19, 2008 · N779AZ · Cndair CL6002B16SDR SB08030Circuit Breaker · trippedFLL - FLT 1723 ON APPROACH TO FLL, WHEN FLAP HANDLE WAS SELECTED TO FLAPS 10 POSITION, THE FLAP INDICATOR SHOWED ONLY FLAPS 5 WITH L/E FLAPS EXTEND LIGHT. SELECTING FLAPS 15 POSITION, INDICATOR REMAINED AT FLAPS 5. CREW ACCOMPLISHED A GO-AROUND AND ACCOMPLIMay 18, 2008 · N440US · Boeing 7374B7SDR CA080707010Worm Gear · worn(CAN) WHILE INSP, IT WAS NOTICED THAT BOTH FLAP TRANSMISSION WERE WORN OUT OF LIMITS. OVERHAULED FLAP TRANMISSIONS WERE INSTALLED. THEY WERE BOTH WITHIN LIMITS AT THE LAST INSP. ONCE THEY START TO WEAR THEY REALLY WEAR FAST.May 16, 2008 · Piper PA31SDR TRAX200800653Bpsu · inoperativeFLAPS FAILED AT 20 DEGREES DURING APPROACH INTO FSM. REMOVED AND REPLACED RT BPSU IAW AMM 27-51-10 COMPLIED WITH PER SP 607 AND AMM 27-51-10 WORK SATISFACTORY. PERFORMED RIGGING OF SYSTEM. OPS CHECK GOOD ON FLAP SYSTEM AT THIS TIME. (B)May 16, 2008 · N844AS · Cndair CL6002B19SDR TRAX200800649Pdu · out of rigFLAPS FAILED IN FLIGHT AT 20. BOTH FLAPS INDICATED 20 ON THE SYNOPTIC PAGE, BOTH FLAPS OUTLINED IN YELLOW ON SYNOPTIC PAGE. FLAPS WERE LOWERED AT AIRSPEED OF 180KNOTS. COMPLIED WITH QRH, NO UNUSUAL CONTROL FEEL---[EMERGENCY DECLARED] REMOVED & REPLACED PDU ANDMay 16, 2008 · N844AS · Cndair CL6002B19SDR A6WA200840423Flap · failedFLAPS FAILED AFTER TAKEOFF AT 12 DEGREES, PERFORMED QRH, RETURNED TO CMH. OPEN (A)May 15, 2008 · N437AW · Cndair CL6002B19SDR VNAA0805020Flap · malfunctionedCREW REPORTED A FLAPS FAIL AT 8 DEGREES DURING DESCENT INTO DCA. CREW ELECTED TO DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU, BITE CHECK AND SKEW DETECTOR. MAINTENANCE RESET THE FLAP CHANNELS IN ACCORDANCE WITH THE AIMay 15, 2008 · N254PS · Cndair CL6002B19SDR MT9A00000035Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO THE BEARING WAS CORRODED TO THE BOLT. (K)May 15, 2008 · N9623B · Cessna 208BSDR MT9A00000036Bearing · corrodedTHE SEALED BEARING WERE CORRODED. (K)May 15, 2008 · N9623B · Cessna 208BSDR COMA0860245Flap · failedFLIGHT 4988 - EN ROUTE FROM JAX TO LGA RECEIVED FLAPS FAIL CAUTION MESSAGE. EMERGENCY DECLARED, AIRCRAFT DIVERTED TO JFK AND LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION.May 15, 2008 · N811CA · Cndair CL6002B19SDR A6WA200840422Flap · malfunctionedFLAP FAILURE AFTER TAKEOFF DURING RETRACTION FROM 20 DEGREES. FAILED AT 16 DEGREES. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. (S)May 14, 2008 · N437AW · Cndair CL6002B19SDR MT9A00000029Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1041L · Cessna 208BSDR MT9A00000030Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1041L · Cessna 208BSDR MT9A00000031Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1037N · Cessna 208BSDR MT9A00000032Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN, ALSO THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1037N · Cessna 208BSDR MT9A00000007Bellcrank · frozenTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K)May 9, 2008 · N9505B · Cessna 208BSDR VNAA0805011Flap System · malfunctionedCREW REPORTED A FLAPS FAIL AT 0 DEGREES DURING FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. SYSTEM OPS CHEMay 8, 2008 · N259PS · Cndair CL6002B19SDR MT9A00000018Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. ALSO, THE SLEEVE CORRODED TO THE BELLCRANK. (K)May 8, 2008 · N9760B · Cessna 208BSDR MT9A00000005Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 8, 2008 · N9331B · Cessna 208BSDR MT9A00000017Bellcrank · corrodedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET, ALSO, THE SLEEVE HAD CORRODED TO THE BELLCRANK. (K)May 8, 2008 · N9760B · Cessna 208BSDR MASA200800380Bpsu · out of rigASH FLT 1908 HNL- OVERNIGHT - FLAPS FAIL CAUTION OCCURRED ON EXTENSION BETWEEN 20 AND 30 DEGREES WITH THE HANDLE SELECTED TO 30 DEGREES. MX COMPLIED WITH THE FLAPS FAIL PARTS A AND B PROCEDURES AND RIGGED THE BPSU UNITS.May 7, 2008 · N693BR · Cndair CL6002B19SDR VNAA0805009Flap System · malfunctionedCREW REPORTED A FLAPS FAIL AT 20 DEGREES WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL TEST OF THE FECU BIT TEST SKEW DETECTION. SYSTEM OPS CHECKED GOOD AND MESSAGEMay 6, 2008 · N207PS · Cndair CL6002B19SDR BB08083Transmission · bindingPHX FLT 31 OGG TO PHX - DURING APPROACH, RECEIVED A TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW EMPLOYED THE ALTERNATE EXTENSION METHOD TO EXTEND THE TRAILING EDGE FLAPS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE NR 1 OVERLOAD INDMay 6, 2008 · N904AW · Boeing 7572S7SDR MT9A00000015Bellcrank · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 5, 2008 · N4602B · Cessna 208BSDR MT9A00000014Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 5, 2008 · N4602B · Cessna 208BSDR MT9A00000016Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)May 5, 2008 · N9760B · Cessna 208BSDR MT9A00000028Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 5, 2008 · N1041L · Cessna 208BSDR VNAA0805006Fcu · failedCREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEMay 5, 2008 · N259PS · Cndair CL6002B19SDR MASA200800359Bpsu · jammedASH FLT 2986 SLC-LAS. FLAPS FAIL CAUTION AT ZERO DEGREES IN CLIMBOUT. FLAP HANDLE AT ZERO AND NOT MOVED. REPLACED THE RT BPSU.May 1, 2008 · N17337 · Cndair CL6002B19SDR RAIA00804034Flap · malfunctionedFLT 5530 - STL - CREW REPORTED RECEIVING A SPS ADVANCED AND FLAP FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. FLAP INDICATION SHOWED AMBER DASHES. MAINTENANCE RESET THE FLAP SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED.Apr 30, 2008 · N825HK · Emb EMB145LRSDR REXA200800010Flap System · failedFLAPS FAILED WHEN SELECTED FROM 20 TO 30 ON APPROACH. SYSTEM RESET AND PLACED ON SEVENTY TWO HOUR WATCH PER AD 2006-12-21.Apr 30, 2008 · N834AY · Cndair CL6002B19SDR MASA200800351Pdu · malfunctionedASH FLT 2721- PHX-SBA - FLAPS FAIL CAUTION AT 2 DEGREES, WOULD NOT RESET. DECLARED AN EMERGENCY AND DIVERTED TO LAX. C/W PART A/B, REPLACED LT/RT BPSU AND PDU.Apr 28, 2008 · N17337 · Cndair CL6002B19SDR 2008UALA02458Computer · failedSLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND FAILURE OF SFCC-2. 22CV. REPLACED SFCC-2. 22CV, OPS TESTED NORMAL.Apr 25, 2008 · N824UA · Airbus A319131SDR MT9A00000013Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)Apr 23, 2008 · N9653F · Cessna 208SDR MT9A00000012Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)Apr 23, 2008 · N9653F · Cessna 208SDR MT9A00000011Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)Apr 23, 2008 · N9653F · Cessna 208
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