JASC 2752

Service difficulty reports · 1,979

Reports filed under 2752 · Trailing Edge Flap Actuator, 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 = '2752'
  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 GLBA2003040Actuator · failedLEFT I/B FLAP FAILED TO RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ACTUATOR , OPS CHECK GOOD.Mar 30, 2003 · N100UX · Beech 1900DSDR XNOA01109Flap · malfunctionedAFTER T/O FROM DAY, OUTBOARD FLAPS WOULD NOT RETRACT PAST 5 DEGREES. ALL APPLICABLE ENA EMERG/ABNORMAL PROCEDURES COMPLETED. AIRCRAFT RETURNED TO DAY. INSPECTED FLAP SYSTEM. NO DEFECTS NOTED. RESET SYSTEM. OPS CHECK SYSTEM SEVERAL TIMES. OPS CHECK GOOD IAW 72Mar 25, 2003 · N793A · Boeing 727227SDR IXXA0300027OFitting · damagedON APPROACH TO BFI CREW RECEIVED A FLAP SPLIT INDICATION ALONG WITH A AIRCRAFT ROLL TO THE LT. CREW RAISED FLAPS AND DIVERTED TO PDX. MAINTENANCE INSPECTION AND REPAIR IS IN PROGRESS. ADDITIONAL INFORMATION WILL BE PROVIDED AS IT BECOMES AVAILABLE. MAINTENMar 19, 2003 · N830BX · Doug DC871FSDR UQR2003F00000Actuator · failedON APPROACH TO LANDING, THE FLAPS WERE MOVED FROM THE 12 DEGREE POSITION TO THE 20 DEGREE POSITION. AT THIS TIME THE AIRCRAFT BEGAN TO ROLL TO THE LEFT AND HAD TO BE CORRECTED BY FULL AILERON DEFLECTION TO THE RIGHT. THE CREW LANDED THE AIRCRAFT WITH FULL AMar 17, 2003 · N140DR · Israel 1124SDR ASOA03100Actuator · inoperativeFLT 4810 - DURING APPROACH INTO SYR FROM ATL, THE CREW RECEIVED A FLAP FAILURE MESSAGE. WHEN SELECTING THE FLAPS TO EIGHT DEGREES THEY DID NOT MOVE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN SYR. THE LOCAL MECHANIC COMPILED WITH ADMar 10, 2003 · N847AS · Cndair CL6002B19SDR AUS20030236Actuator · worn(AUS) LT AND RT FLAP ACTUATOR BRUSHES AND BEARINGS WORN. FLAP CONTROLAND FOLLOW UP POTENTIOMETERS FAULTY.Feb 24, 2003 · Swrngn SA227*SDR A20203Seal · leakingFUEL BEGAN LEAKING FROM LEFT WING UPON REMOVAL OF LEFT OUTBOARD FLAP LINEAR ACTUATOR FROM THE WING REAR SPAR. INVESTIGATION REVEALED FLAP ACTUATOR BOX, SEAL PACKING HAD BEGUN LEAKING DUE TO (4 EACH) IMPROPERLY SECURED FASTENERS. THESE FASTENERS ATTACH THE BOFeb 7, 2003 · N253PC · Pilats PC1245SDR SWIA200311764Actuator · malfunctionedFLAPS FAIL MESSAGE. FLAPS WOULD NOT MOVE FROM 5 DEGREES POSITION. REMOVED AND REPLACED RIGHT OUTBOARD FLAP INBOARD ACTUATOR IAW CRJ MM 27-53-05. RIGGED FLAPS AND OPS CHECK GOOD.Feb 1, 2003 · N413SW · Cndair CL6002B19SDR SWIA200311743Actuator · leakingON SHORT FINAL RECEIVED A FLAP DISAGREE MESSAGE ON THE NACELLE FLAPS AFTER SELECTING FLAPS 45 (ABOUT 125 KTS). THEN LOST RT HYD PRESSURE. REMOVED AND REPLACED LEAKING RIGHT NACELLE FLAP ACTUATOR PER EMB MM 27-50-08. GROUND OPS CHECK AND LEAK CHECK COMPLIED Jan 28, 2003 · N292SW · Emb EMB120ERSDR 2003FA0000115Clip · backed outLEFT FLAP OUTBOARD LOWER ACTUATOR COVER PLATE FOUND DISTORTED AND BENT. UPON INVESTIGATION FOUND CIR-CLIP FOR LOWER GIMBLE PIN MISSING. THIS MISSING CLIP ALLOWED GIMBLE PIN TO DROP DOWN. WHILE PIN WAS BACKING OUT AND DURING FLAP OPERATION DAMAGED OCCURRED TO TJan 27, 2003 · N720CC · Lear 45LEARSDR CA030205003Pdu · failed(CAN) FLAPS FAILED TO EXTEND ON APPROACH INTO PE. A/C LANDED AND FLAP SYSTEM INSPECTED, FLAP POWER DRIVE UNIT FOUND FAULTY PN 952D1005. UNIT REPLACED AND FLAP O SET CARRIED OUT.Jan 26, 2003 · Pilats PC1245SDR CA030130004Actuator · failed(CAN) ON DEPARTURE FLAPS FAILED AT 20 DEGREES. DURING TROUBLE SHOOTING IT WAS DISCOVERED THAT THE FOLLOWING ACTUATORS FAILED THE ACTUATOR TORQUE CHECK AS PER MM 27-53-00-750-002, AND WERE REPLACED.Jan 21, 2003 · Cndair CL6002B19SDR CA030205005Actuator · frozen(CAN) ON APPROACH, FLAPS WERE SELECTED AND C/B FOR FLAPS POPPED. A/C LANDED AND SYSTEM WAS RESET AND TRIED AGAIN, C/B POPPED AGAIN. UPON INVESTIGATION IT WAS FOUND THAT SEVERAL OF THE FLAP ACTUATORS WERE FROZEN. WHEN SYSTEM WAS WARMED EVERYTHING WORKED PROPEJan 21, 2003 · Pilats PC1245SDR ENHA200300001Support · crackedFLAP ACTUATOR STRUCTURE SUPPORT ASSY FAILURE. PILOT REPORTED FLAPS SELECTED TO 10 DEGREE, FLAPS DEPLOYED TO 10 DEGREE. AT THE NEXT FLAP SELECTION, FLAP C/B TRIPPED, C/B WOULD NOT RESET. STANDBY FLAP SWITCH WAS NOT USED AND BREAKAWAY WIRE INTACT. INSPECTION Jan 21, 2003 · N1276P · Cessna 208BSDR 208000103Structure · crackedSUPPORT ASSEMBLY-FLAP ACTUATOR FAILURE. PILOT REPORTED FLAPS SELECTED 10 DEG FLAPS WENT TO 10 DEGREE STOPPED AT THE NEXT FLAP SELECTION CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE INTACT. FURTHEJan 20, 2003 · N1276P · Cessna 208BSDR SWIA200311738Actuator · malfunctionedUNCOMMANDED, THE RIGHT INBOARD FLAP WENT DOWN PARTIALLY WHILE AIRCRAFT WAS PARKED. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AS PER MM 27-50-00. NO LEAKS. OPS CHECK GOOD.Jan 19, 2003 · N270YV · Emb EMB120ERSDR SWIA200311697Actuator · malfunctionedFLAP LIGHT ON MAP PANEL ASSOCIATED WITH ADVANCED SWS AND CONTROL FAULT ON OVERHEAD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00. CYCLED FLAPS SEVERAL TIMES. ALL CHECKS GOOD.Jan 8, 2003 · N269UE · Emb EMB120RTSDR 03FDEA00006Motor · failedCOMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID JUST PRIOR TO FLAP EXTENSION. SPOILERS HAD BEEN USED JUST PRIOR TO LOSS. REPLACED RIGHT OUTBOARD FLAP MOTOR IAW MM, SERVICED HYDRAULIC SYSTEM TO FULL LEVEL. OPERATED FLAPS UP AND DOWN SEVERAL TIMES, ALL INDICATIONS Jan 8, 2003 · N244FE · Boeing 727200SDR SWIA200311681Actuator · malfunctionedRIGHT AFTER STARTING BOTH ENGINES, THE LEFT INBOARD FLAP EXTENDED ALL THE WAY DOWN. THE FLAP LIGHT ON MAP AND FLAP ASYMMETRY LIGHT ILLUMINATED. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS CHECK GOOD AT THIS TIME.Jan 7, 2003 · N270YV · Emb EMB120ERSDR SWIA200211577Actuator · leakingON TAXI OUT, AFTER SELECTING FLAPS 15 DEGREES, THE HYDRAULIC QUANTITY ON THE BLUE SIDE WENT TO ZERO WITH ASSOCIATED LIGHTS. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW RII 27-307 AND 27-50-08. LEAK CHECKS GOOD. NO LEAKS NOTED AT THIS TIME.Dec 15, 2002 · N288SW · Emb EMB120ERSDR SWIA200211627Actuator · malfunctionedDISAGREEMENT MESSAGE WHEN FLAPS ARE RETRACTED FROM 45 DEGREE FLAPS, DISAGREEMENT FIX THEMSELVES ON TAXI. INSTALLED SERVICEABLE NACELLE FLAP ACTUATOR ON LEFT SIDE. OPS CHECKS GOOD. PERFORMED IAW MM 27-50-00.Dec 9, 2002 · N227SW · Emb EMB120ERSDR SWIA200211500Actuator · malfunctionedFLAP DISAGREEMENT ON NACELLE FLAPS ON RETRACTION FROM 45 DEGREES. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. LEAK CHECK GOOD.Nov 24, 2002 · N199SW · Emb EMB120ERSDR MWEA020707Bushing · wornRIGHT OUTBOARD FLAP HINGE BRACKET HAS WORN HINGE POINT BUSHINGS. -- FABRICATED AND INSTALLED REPAIR BUSHINGS.Nov 19, 2002 · N813ME · Doug DC981SDR MWE020703Bushing · corrodedLEFT OUTBOARD FLAP, INBOARD AFT HINGE BRACKET HINGE POINT AND ACUTATOR MOUNT HAT BUSHINGS ARE WORN. -- REMOVED CORROSION AND INSTALLED NEW HINGE.Nov 19, 2002 · N813ME · Doug DC981SDR SWIA200211501Connector · contaminatedAFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT WITH 2 BARS ON OUTBOARD FLAPS, AND ALL LIGHTS ON THE 10 DEGREE LINE FLASHING. RESET AS PER QRH. RESET NOT SUCCESSFUL. RETURNED TO LAX. FOUND LT OUTBOARD FLAP ACTUATOR CONNECTOR PLUG CONTAMINATED WITH MOISTURE. CNov 18, 2002 · N214SW · Emb EMB120ERSDR CA021115013Actuator · failed(CAN) DURING SCHEDULED MAINTENANCE OF THE AIRCRAFT. THE FLAPS WERE SELECTED DOWN TO THE 40 DEGREE POSITION. DURING MOVEMENT OF THE FLAPS A 'GRINDING' NOISE WAS HEARD COMING FROM THE L/H INBOARD FLAP ACTUATOR. THE ACTUATOR BECAME VERY HOT AND WOULD CAUSE THE FLNov 12, 2002 · Pilats PC1245SDR ABXA020305Actuator · brokenHYD QTY LOSS ON LANDING. MAINTENACE FOUND THE RT INBOARD FLAP ACTUATOR CRANK ASSEMBLY BROKEN ALONG WITH A BROKEN HYD LINE TO THE ACTUATOR AND ASSOCIATED ATTACHING HARDWARE BROKEN. OPEN: CORRECTIVE ACTION IS NOT COMPLETE.Nov 12, 2002 · N811AX · Doug DC863FSDR DL764021312Actuator · trippedT/E FLAP DISAGREE DURING RETRACTION AFTER T/O FROM LAX. DUE TO FLAPS 20 QRH PROCEDURE REQD AND SHORT OGG RUNWAY DIVERTED TO HNL. HNL MTC DISCOVERED NR 6 AND NR 7 T/E FLAP ROTARY ACT TRIP. NO HISTORY. RESET AND CHECKED OK PER FIM.Nov 11, 2002 · N828MH · Boeing 767432ERSDR SWIA200211411Actuator · malfunctionedAFTER FLAP RETRACTION ON LANDING, THE INBOARD PAIR OF FLAPS REMAINED AT 25 DEGREES. THERE WERE NO CONTROL FAULTS OR DISAGREEMENT WARNINGS. AFTER RESETTING THE SYSTEM, THE FLAPS RETRACTED. REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-5Oct 29, 2002 · N269UE · Emb EMB120RTSDR SWIA200211380Actuator · malfunctionedFLAPS FAIL CAUTION MESSAGE RECEIVED ON APPROACH. FLAPS FAILED AT 4 DEGREES. NR 3 FLAP ACTUATOR ON LT SIDE CHATTERS ON EXTENSION. REMOVED FLAP PDU AND REPLACED IT WITH A SERVICEABLE UNIT IAW CL600 27-52-05. INFLIGHT FUNCTION TEST REQUIRED - FAILED. REMOVEOct 24, 2002 · N438SW · Cndair CL6002B19SDR SWIA200211361Pdu · failedFLAPS FAILED MESSAGE IN FLIGHT. REMOVED AND REPLACED PDU FOR FLAPS. OPS CHECKS GOOD IAW 27-52-01.Oct 24, 2002 · N441SW · Cndair CL6002B19SDR CA021101005Actuator · failed(CAN) THE PILOT SELECTED FLAPS IN PREPARATION FOR LANDING.THE AURAL WARNING AND FLAP CAUTION LIGHT ON THE CAWS PANEL WERE THEN OBSERVED BY THE PILOT. THE AIRCRAFT LANDED AND THE FLAPS WERE RESET ON THE GROUND.THIS SNAG OCCURRED AN ADDITIONAL TWO (2) TIMES THROct 19, 2002 · Pilats PC1245SDR AUS20021218Stud · sheared(AUS) FLAP MOTOR MOUNT STUD BROKEN. MOTOR SEPARATED FROM ACTUATOR.Oct 15, 2002 · Cessna 210NSDR MASA200200022Actuator · malfunctionedAIRSHUTTLE 6412 FROM PHX TO COS DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO THE FLAPS SYSTEM FAILING AT DEGREES. MAINTENANCE HAD REPLACED THE LT IB FLAP ACTUATOR THE NIGHT BEFORE FOR A PREVIOUS FAILURE. MAINTENANCE IS STILL TROUBLESHOOTING.Oct 14, 2002 · N47239 · Cndair CL6002B19SDR SWIA200211309Actuator · leakingRIGHT HYDRAULIC RESERVOIR EMPTIED EN ROUTE. FOUND LEFT NACELLE FLAP ACTUATOR TO BE LEAKING FROM A POSITION TRANSDUCER. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPS CHECKED GOOD.Oct 6, 2002 · N290SW · Emb EMB120ERSDR CA021008004Pin · out of position(CAN) THE FLAP DRIVE CAUTION LIGHT ILLUMINATED DURING PUSHBACK. FLAPS DRIVE OK FROM 5 DEGREES, TO 35, EXTENDING.FLAP DRIVE LIGHT ILLUMINATED AGAIN, WHEN FLAPS WE RERAISED FROM 35 TO 5 DEGREES. FCU WAS RESET AND THE A/C FERRIED TO HOME BASE. MECHANICS FOUND ACCSep 30, 2002 · Bombdr DHC8400SDR CA020925001Pdu · failed(CAN) FLAP FAIL MESSAGE FOUND ON EICAS INTEROGATION CHECK ( FOUND ON ACCOMPLISHMENT OF SERVICE CHECK.)DURING TEST FOUND PDU2 C/B POPPING AND FLAPS HALF SPEED . PDU REPLACED AS PER AMMSep 22, 2002 · Cndair CL6002B19SDR 2002FA0001197Shaft · crackedDURING A ROUTINE PHASE 1 AND 2 INSPECTION ON THIS AIRCRAFT, LUBRICANT WAS FOUND ACCUMULATING AT ACTUATOR HOUSING. FURTHER INSPECTION REVEALED A CRACK IN THE CHROMED SHAFT RUNNING PARALLEL WITH THE SHAFT STARTING AT THE ROD-END. THIS CRACK WAS APPROXIMATELY Sep 13, 2002 · N394B · Beech C90ASDR DL764021070Actuator · trippedT/E FLAP DISAGREE AFTER T/O RAISED WITH ALT SYSTEM. DUE TO SHORT RUNWAY IN OGG DIVERTED TO HNL. T/S PER FIM, FOUND NR 6 T/E FLAP ROTARY ACT TRIPPED. RESET SAME. CYCLED FLAPS NO OTHER FAULTS.Sep 12, 2002 · N839MH · Boeing 767432ERSDR SWIA200211219Actuator · leakingON SHORT FINAL, LOST GREEN HYD FLUID & PSI AFTER EXTENDING THE FLAPS TO 25 DEGREES. REMOVED THE RT FLAP ACTUATOR AND INSTALLED A SERVICEABLE ACTUATOR. SERVICED THE HYD SYSTEM AS NEEDED. OPS CHECK GOOD, LEAK CHECK GOOD.Sep 12, 2002 · N224SW · Emb EMB120ERSDR SWIA200211221Actuator · failedINBOARD FLAPS CONTROL FAULT FROM 15 DEGREES TO 0 DEGREES WHEN RETRACTING THEM. REPAIRED ENVIRONMENTAL SPLICE AT LEFT I/B FLAP ACTUATOR CANNON PLUG. INSPECTED WIRING AT CANNON PLUGS AND FCU. FOUND LEFT INBOARD FLAP ACTUATOR BAD. REPLACED LEFT FLAP ACTUATOR Sep 11, 2002 · N1105G · Emb EMB120RTSDR C2XA02IA189Motor · failedIAH- THE CREW NOTED THAT THE FLAPS FAIL IN FLIGHT. NO POSITION INDICATION OF FLAPS ON EICAS. THE CREW RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP DRIVE MOTOR UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. Sep 10, 2002 · N26549 · Emb EMB145LRSDR DL764021084Actuator · trippedIRREG: TRAILING EDGE FLAP DISAGREE AFTER TO WHEN RETRACTING FROM FLAPS 5 TO 1. RAISED FLAPS ELECTRICALLY WITH THE STANDBY SYSTEM. TROUBLESHOT PER FIM 27-51-00 PERFORMED BITE ON FSEU WITH FAULT 27-51104 INSPECTED ROTARY ACTUATORS FOUND LT WING FLAP ACTUATORS Sep 5, 2002 · N833MH · Boeing 767432ERSDR C2XA02CL178Drive Unit · failedCLE FLT 3187 CREW REPORTED THAT THE FLAPS EXTENDED NORMALLY TO 45 DEGREES. AFTER EXTENSION FLAP FAIL ON EICAS APPEARED AND FLAP INDICATOR DISPLAYED AMBER DASH. FLAPS WOULD NOT RETRACT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE FLAP POWER DRSep 3, 2002 · N14516 · Emb EMB135LRSDR SWIA200211141Actuator · malfunctionedON DESCENT INTO ELKO, RIGHT NACELLE WOULD NOT EXTEND PAST 15 DEGREES WITH CONTROL FAULTS. AFTER LANDING, ALL FLAPS RETRACTED. THEREAFTER, RIGHT NACELLE FLAP WOULD NOT WORK, CAUSING FLAP ASYMMETRY. REMOVED AND REPLACED NACELLE FLAP ACTUATOR. REMOVED AND REPAug 19, 2002 · N199SW · Emb EMB120ERSDR SWAA021901Motor · failedAFTER LANDING, T/E FLAPS WOULD NOT RETRACT. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM.Aug 15, 2002 · N679AA · Boeing 7373A4SDR SWIA200211126Actuator · failedNACELLE FLAPS WOULD NOT GO PAST 4 ROWS OF LIGHTS WHEN 25 DEGREES OF FLAPS SELECTED. FLAP DISAGREEMENT WARNING. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-09. LEAK CHECK GOOD. OPS CHECK GOOD AT THIS TIME.Aug 15, 2002 · N199SW · Emb EMB120ERSDR SWAA021820Motor · failedAIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT RETRACT HYDRAULICALLY. REMOVED AND REPLACED T/E FLAP HYDRAULIC MOTOR PER MM.Aug 12, 2002 · N693SW · Boeing 737317SDR QXEA0201229Attach Fitting · damagedPDX- LEFT HAND INBOARD FLAP OUTBOARD ACTUATOR ATTACH BRACKET BEARING SURFACE DAMAGED BY ACTUATOR ATTACH PIN. REPAIRED IAW HORIZON AIR EA 6-57-51.Aug 9, 2002 · N408QX · Bombdr DHC8401SDR CA020812001Arm · cracked(CAN) DURING TAXI, AIRCRAFT CREW RECEIVED A FLAP WARNING FAULT. THE COMPUTER AUTOMATICALLY DISABLES THE SYSTEM WHEN A WARNING OCCURS SO NO FLAP SELECTION WAS AVAILABLE. ON INSPECTION THE RT INBOARD FLAP DRIVE ARM WAS FOUND CRACKED AT THE WING ATTACHMENT.Aug 6, 2002 · Pilats PC1245
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