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 COMA9860255Bpsu · failedFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU.Sep 4, 1998 · N964CA · Cndair CL6002B19SDR AU981113Control Cable · worn(AUS) RIGHT OUTBOARD FLAP DRIVE CABLE WORN AT THE MOTOR END. PART TC: 9,693.Sep 4, 1998 · Beech B200CSDR ARWA980903Flaps · malfunctionedMIA - FLT 501 - FLAPS WILL NOT GO DOWN, NO INDICATION. UNLOCKED FLAPS AT FLAP BRAKE, OPS CHECK GOOD IAW MM 27-51-00. (M)Sep 4, 1998 · N306GB · Lkheed 1011385115SDR VNAA9809005Control Unit · malfunctionedWHILE AWAITING CLEARANCE FOR TAKEOFF, A FLAP CONTROL FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE PERFORMED A RE-RACK OF THE FLAP CONTROL UNIT AND COMPLIED WITH OPERATIONAL CHECKS, IN ACCORDANCE WITH DORNIER MAISep 3, 1998 · N424JS · Dorner DO328100SDR SWIA971268Retract Mech · malfunctionedWHILE DESCENDING INTO TUC FLAPS FAIL MESSAGE CAME ON. COMPLIED WITH CHECKLIST AND LANDED IN TUC WITH 0 FLAPS. POWERED DOWN AIRCRAFT FLAPS SYSTEM AND RESET SYSTEM. CHECKS NORMAL.Sep 3, 1998 · N403SW · Cndair CL6002B19SDR F3LA98162Control Cable · failedDEN - DURING DESCENT, FLIGHT CREW REPORTED TRAILING EDGE FLAPS STUCK. LEFT FLAP UP, RIGHT FLAP AT 1 DEGREE. LEADING EDGE DEVICES FULL EXTEND. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP ASYMMETRY FAC-4 CABLE. ADAug 30, 1998 · N212US · Boeing 737201SDR ABXA9800856Fitting · gougedWHILE COMPLYING WITH C-INSPECTION, FOUND A RIGHT FLAP MOVEABLE VANE PULLEY BRACKET ATTACH FITTING GOUGED AND RIVETS SHEARED. REPLACED RIGHT FLAP PULLEY BRACKET ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.Aug 28, 1998 · N903AX · Doug DC932SDR COMA9860243Fecu · failedFLAPS FAILED WHEN SELECTED FOR LANDING. REPLACED THE FECU.Aug 27, 1998 · N969CA · Cndair CL6002B19SDR 98ZZZX3336Flexshaft · brokenFLAPS FAILED DURING EXTENSION. SLATS EXTENDED. FLAPS MOVED ABOUT .50 INCH, BOTH FLAPS FAIL CAS MESSAGE. FOUND BROKEN RIGHT HAND INBOARD FLEXSHAFT.Aug 26, 1998 · N934QS · Cessna 750SDR VTZA98271Bpsu · failedIAD/RSW - FLT 6745 - ON 8-25-98 AT 1900 HOURS, EXPERIENCED A FLAP FAIL MESSAGE ON MASTER CAUTION PANEL. ACFT CONTACTED MAINT CONTROL AND DISPATCHED, DECISION TO RETURN TO IAD WAS MADE. UPON ARRIVAL AT IAD, ACFT DECLARED AN EMERGENCY AND LANDED AT IAD WITH NOAug 25, 1998 · N627BR · Cndair CL6002B19SDR VTZA98270Fecu · failedIND/IAD - FLT 6723 - DURING LANDING ON 8-25-98 AT 1150 HOURS, EXPERIENCED A FLAP FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT IAD WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT WAS TAXIED TO Aug 25, 1998 · N627BR · Cndair CL6002B19SDR CA980909017Bpsu · failed(CAN) FLAPS FAILED AT 33 DEGRESS WHEN SELECTED TO 45 DEGREES. REPLACED LEFT HAND BRAKE AND POSITION UNIT.. PART TC: 3,567.Aug 18, 1998 · Cndair CL6002B19SDR CA980827018Flaps · failed(CAN) DURING FLAP EXTENSION BETWEEN 35 TO 45 DEGREES, FLAPS STOPPED AT 33 DEGREES AND A FLAP FAIL MESSAGE CAME ON EICAS. SYSTEM RESET.Aug 15, 1998 · Cndair CL6002B19SDR 99ZZZX167Pin · fracturedWHILE ON BASE LEG FOR LANDING WITH 2ND NOTCH OF FLAPS APPLIED THERE WAS A LOUD BANG AND ACFT PITCHED DOWN SUDDENLY. FLAP HANDLE HAD RETRACTED TO ZERO DEGREE FLAP POSITION. A SAFE ZERO DEGREE FLAP LANDING WAS MADE. DISASSY OF FLAP HANDLE AREA REVEALED THE LAAug 15, 1998 · N7624J · Piper PA28R180SDR VTZA98258Bspu · failedFLT 6633 - CRW-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS AMBER FLAP FAIL MESSAGE ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT BSPU AND RT OUTBOARAug 12, 1998 · N622BR · Cndair CL6002B19SDR 98ZZZM802Control Cable · failedFLT 6633 - CRW-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS AMBER FLAP FAIL MESSAGE ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT BSPU AND RT OUTBOARAug 12, 1998 · N622BR · Cndair CL6002B19SDR VTZA98257Fecu · failedFLT 6760 - BNA-IAD - DURING LANDING, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP WARNING LIGHT ILLUMINATED, FLAPS STUCK AT 0 DEGREES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACEAug 11, 1998 · N622BR · Cndair CL6002B19SDR CA980825009Bellcrank · cracked(CAN) DEFLECTION CRANK FOUND CRACKED USING NDT TECHNIQUE. PART TC: 19,718.Aug 10, 1998 · Gulstm G159SDR COMA9860227Flexshaft · wornDURING C-CHECK, FOUND RIGHT OUTBOARD FLAP FLEX SHAFT TO BE WORN. REPLACED FLEX SHAFT.Aug 8, 1998 · N937CA · Cndair CL6002B19SDR CA980909012Te Flap · failed(CAN) FLAPS FAIL MESSAGE ON FLAP SELECTION FROM 30 TO 45 DEGREES. RESET CIRCUIT BREAKERS ON BOTH CHANNELS, TWIST CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE.Aug 8, 1998 · Cndair CL6002B19SDR QXEA9801116Cables · rustedFOUR SEGMENTS OF FLAP DRIVE CABLES IN HYDRAULIC TUNNEL HAVE RED RUST CORROSION FROM FRONT BULKHEAD TO SWITCH UNIT. REPAIRED IAW FOKKER SRM 20-30-09 AND SRM 27-51-00, PARAGRAPH B, STEPS 1 THRU 54.Aug 6, 1998 · N498US · Fokker F28MK4000SDR 98ZZZX4440Impeller · crackedINDICATIONS FOUND DURING DYE PENETRANT INSPECTION DUE TO CASTING FLAWS. SUBMITTER SUGGESTED CLEANING UP DURING MANUFACTURING.Aug 5, 1998 · Boeing 737*SDR 98ZZZX4439Impeller · crackedINDICATIONS FOUND DURING DYE PENETRANT INSPECTION DUE TO CASTING FLAWS. SUBMITTER SUGGESTED CLEANING UP DURING MANUFACTURING.Aug 5, 1998 · Boeing 737*SDR CA980909015Fecu · failed(CAN) ON FLAP SELECTION FROM 8 DEGREES TO ZERO, FLAP FAIL MESSAGE ON EICAS. QUICK REF. CARRIED OUT. LEFT HAND FLAP ELECTRONIC CONTROL UNIT FAILED. LEFT HAND BPSU WIRING CHANGED AND FECU ADJUSTED.. PART TC: 4,726.Aug 3, 1998 · Cndair CL6002B19SDR SWIA971240Fcu · failedOUTBOARD FLAPS CONTROL FAULT AND WILL NOT RESET. RETURNED TO PDX. REPLACED FLAP CONTROL UNIT IAW MM 27.Aug 2, 1998 · N128AM · Emb EMB120RTSDR 98ZZZX3431Pin · shearedTHE PIN WHICH HOLDS THE FLAP HANDLE IN SELECTED POSITIONS WAS FOUND MISSING. IT APPEARS THE PIN FRACTURED IN HALF AT THE ROLL PIN HOLE AND FELL OUT OF THE PLUG, PIPER P/N 62734-00. THE PIN COULD NOT BE LOCATED IN THE AIRCRAFT OR AT THE ACCIDENT SITE. THERE Aug 1, 1998 · N1793J · Piper PA28140SDR RRXA98398Fitting · gougedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP, EXHAUST GATE ACTUATING FITTING GOUGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05157.Jul 31, 1998 · N8076U · Doug DC871FSDR AU980917Control Unit · malfunctioned(AUS) FLAP CONTROL UNIT FAULTY.Jul 30, 1998 · Emb EMB120SDR ARWA9807132Comparator · failedMIA - FLT 617 - SLAT ASYMMETRY DETECTION FAULT, LIGHT ON AFTER EXTENDING FLAPS. PERFORMED ABNORMAL PROCEDURES. LIGHT REMAINED ON. RETURNED TO BLOCK. REMOVED AND REPLACED SLAT ASYMMETRY COMPARATOR. OPS CHECK NORMAL IAW MM 27-81-01. (X)Jul 30, 1998 · N308GB · Lkheed 1011385115SDR CA980814015Lever · failed(CAN) EN ROUTE FLAPS FAIL CAUTION MESSAGE AFTER SELECTING FLAPS TO 8 DEGREES ON APPROACH. FLAPS INDICATED EXTENDED. REPLACED FLAP CONTROL POSITION LEVER.. PART TC: 5,470.Jul 29, 1998 · Cndair CL6002B19SDR UPS98227249Cable · brokenFOL UNEVENTFUL 340 KT CLIMB, .80M/330 IAS SET. AFTER APROX 10 MIN, MOD VIBS STARTED AND WERE AIRSPEED. A/S REDUCED 263 KTS BEFORE VIBS ABATED. FLR COMPLIED BELOW 260 KTS. FOUND CABLE BROKEN IN MID FLAP TO AFT FLAP ASSY RT INBD T/E FLAP SEE LOG PAGE 267071 IJul 28, 1998 · N948UP · Boeing 72725CSDR COMA9860205Flexshaft · strippedDURING C CHECK, FOUND RIGHT INBOARD FLAP FLEXSHAFT TO HAVE STRIPPED CASING THREADS. REPLACED FLEXSHAFT.Jul 25, 1998 · N978CA · Cndair CL6002B19SDR COMA9860204Flexshaft · separatedDURING C-CHECK, FOUND RIGHT OUTBOARD FLAP FLEXSHAFT TO BE UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEXSHAFT.Jul 25, 1998 · N978CA · Cndair CL6002B19SDR 98ZZZM613Lever · out of adjustFLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LEVER GUARD. OPERATIONAL CHECKS SATISFACTORY. (M)Jul 25, 1998 · N188GA · Beech 1900SDR 98UAL900353Mechanism · out of adjustAT 20,000 FEET AND 350 KNOTS GOT RIGHT FLAP FLUTTER. PASSENGER SAW RIGHT HAND OUTBOARD AFT FLAP FLUTTER 4 INCHES WITH FLAPS UP. RETURNED TO DEN. *S/D* ADJUSTED OUTBOARD TRAILING EDGE FLAP ECCENTRICS. SYSTEM CHECKS OK.Jul 25, 1998 · N7460U · Boeing 727222SDR UPS98527245Beam · brokenINSPECTION TYPE-N/A ON WALKAROUND, FOUND RT I/B AFT FLAP JAMMED AND RT I/B BELLCRANK SPROCKET BEAM ASSY BROKEN. FOUND LEFT I/B FLAP BELLCRANK SPROCKET BEAM ASSY BROKEN. REMOVED AND REPLACED LEFT I/B BELLCRANK BEAM ASSY PER M/M 27-51-13, (P/N 113N2363-1) FLAPJul 24, 1998 · N411UP · Boeing 75724APFSDR COMA9860193Flex Shaft · brokenFLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE LEFT HAND WING NR 5 FLAP FLEX DRIVE CABLE. CABLE WAS CORRODED AND BROKEN.Jul 22, 1998 · N965CA · Cndair CL6002B19SDR AU981029Flap · malfunctioned(AUS) FLAP SYSTEM FAULTY.Jul 19, 1998 · Bac AVRO146RJ70ASDR SCNA98089Torque Tube · disconnectedAFTER DEPARTURE THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. AIR RETURNED TO LTO. INSPECTED THE AIRCRAFT AND FOUND THE OUTBOARD FLAP TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED THE FLAPS WJul 18, 1998 · N282SC · Boeing 727225SDR SCNA98071Torque Tube · disconnectedAFTER DEPARTURE, THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. RETURNED TO LTO. FOUND THE OUTBOARD FLAP TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED FLAPS WITH NO DEFECTS NOTED IN ACCORDANCEJul 18, 1998 · N282SC · Boeing 727225SDR QXEA9801033Line · failedEN ROUTE, NR 1 HYD FLUID QUANTITY DEPLETED. CREW PERFORMED ALTERNATE GEAR EXTENSION. LANDED WITH DOORS DOWN. MAINTENANCE INSPECTED AND FOUND A HYDRAULIC RETURN LINE ON THE FLAP DRIVE GEARBOX BROKEN. INSTALLED A FLEX LINE, SERVICED HYDRAULIC SYSTEM, LEAK CHJul 18, 1998 · N488US · Fokker F28MK4000SDR COMA9860188Flex Shaft · separatedDURING C-CHECK, FOUND CT NR 1 FLAP FLEX SHAFT UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEX SHAFT.Jul 18, 1998 · N914CA · Cndair CL6002B19SDR CA980814017Shaft · sheared(CAN) ON APPROACH AFTER SELECTING FLAPS 45 DEGREES, A FLAP FAIL AMBER CAUTION MESSAGE AND FLAPS STOPPED AT 39 DEGREES. QUICK REF. PROCEDURE CARRIED OUT. RIGHT HAND OUTBOARD FLAP CENTER SHAFT HAD SHEARED.. PART TC: 6,520.Jul 17, 1998 · Cndair CL6002B19SDR TAOA079808Bearing · missingFLT 6480 DCA-LGA - INBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF FROM DCA, DIVERTED TO BALTIMORE WASHINGTON INTERNATIONAL AIRPORT. REPLACED RIGHT INBOARD FLAP JACKSCREW CARRIAGE BEARING FOR ELEPHANT EAR, REPLACED INBOARD JACKSCREW END CAP, OPERATIONAL CHECK NJul 13, 1998 · N927TS · Boeing 727227SDR EISA98176Gearbox · contaminatedAFTER TAKEOFF FROM IND WHILE RETRACTING FLAPS, OUTBOARD FLAPS DID NOT RETRACT FROM 2 DEGREES TO UP. PERFORMED PROCEDURE AND PROBLEM REMAINED. RETURNED TO IND. GENERATED FROM PILOT REPORT. CYCLED FLAPS, FLUSHING ANY POSSIBILITY OF AIR, INSPECTED FLAPS, FLAPJul 11, 1998 · N310NE · Boeing 7272A7SDR AU980834Control Unit · failed(AUS) FLAP CONTROL UNIT INTERNAL POWER SUPPLY FAILED.Jul 11, 1998 · Pilats PC12SDR C2XA98IA252Fitting · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD FLAP, INBOARD AFT HINGE FITTING AT RIB NR 5, ATTACHMENT FASTENER HOLE ELONGATED. MAINTENANCE REPAIRED THE HINGE FITTING BY INSTALLING A REPAIR BUSHING IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHOJul 10, 1998 · N11835 · Aerosp ATR42320SDR CA980908025Bearing · seized(CAN) INBOARD FLAP WOULD NOT EXTEND. FOUND RIGHT INBOARD SCREW JACK FAIRING FORWARD BEARING SEIZED. REPAIRED. PART TC: 931.Jul 9, 1998 · Boeing 727260SDR ABXA9800615Link · brokenWITH FLAPS SET AT 35 DEGREES THE INDICATOR SHOWED 5 DEGREES OF SPLIT, REQUIRING 2 DEGREES OF LEFT AILERON TRIM. REPLACED BROKEN RIGHT FLAP DRIVER LINK IAW DC8 MM 27-51-04. RIGGED FLAP SYSTEM IAW DC8 MM 27-50-00.Jul 8, 1998 · N821AX · Doug DC863SDR S2YA98019Cam · malfunctionedCMH/MKE - FLT 1829 - DURING TAKEOFF ROLL, CREW DETECTED SMELL OF SMOKE AND SAW SMOKE IN CABIN. ABORTED T/O, RETURNED TO GATE. MAINT INSPECTED ACFT, FOUND THE FLAP MOTOR DAMAGED FROM OVERHEATING. FLAP SYSTEM WAS PLACED ON MEL AND ACFT RETURNED TO SERVICE. MJul 5, 1998 · N891SK · Beech 1900D
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