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 SWIA200110456Connector · dirtyFLAP DISAGREEMENT ON AFTER TAKEOFF FLAP RETRACTION. REQUIRED QRH PROCEDURE TO CORRECT. INSPECTED FLAP. CLEANED CONNECTORS FROM ACTUATOR CANNON PLUGS. RAN FLAPS SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.Dec 15, 2001 · N215SW · Emb EMB120ERSDR SWIA200110454Actuator · failedFLAP DISAGREEMENT UPON SELECTION OF FLAPS TO 45 DEGREES. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-00. OPS CHECK, LEAK CHECK GOOD.Dec 13, 2001 · N213SW · Emb EMB120ERSDR SWIA200110431Actuator · failedAFTER TAKEOFF A FLAP DISAGREEMENT OCCURRED. TWO SEGMENTS OF THE INBOARD PAIR WERE ILLUMINATED AND 1 BAR OF THE NACELLE AND OUTBOARD PAIR FLASHED. DISAGREEMENT CLEARED AFTER SELECTING 15 DEGREES UP, BUT THEN AN INVALID ANALOG IND WAS DISPLAYED. REMOVED AND RDec 11, 2001 · N207SW · Emb EMB120ERSDR SWIA200110404Actuator · failedFLAP ASYMMETRY INDICATION FOR RIGHT INBOARD FLAPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPS CHECK IAW 27-50-00.Nov 30, 2001 · N198SW · Emb EMB120ERSDR SWIA200110385Actuator · failedRIGHT NACELLE FLAP WOULD NOT RETRACT AFTER LANDING. REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECK GOOD.Nov 27, 2001 · N298SW · Emb EMB120ERSDR DL72S011926Attach Fitting · cracked1/4 INCH CRACK NR 5 L/E FLAP ACTUATOR ATTACH BOX O/B RIB. REPAIRED PER MM 57-20-021-8Nov 26, 2001 · N8890Z · Boeing 727225ASDR AUS20011308Connector · corroded(AUS) BOTH OUTBOARD TRAILING EDGE FLAP ACTUATOR CONNECTORS CORRODED.Nov 25, 2001 · Emb EMB120SDR SWIA200110381Wire · brokenON TAXI OUT FLAP CONTROL FAULT INDICATION OCCURRED UPON FLAP DEPLOYMENT TO 15 DEGREES. LEFT LVDT FLR ON ANNUNCIATOR OUTBOARD PAIR. FOUND BROKEN WIRE AND REPAIRED ON LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG. OPS CHECK GOOD ON FLAP EXTENSION AND RETRACTION.Nov 19, 2001 · N220SW · Emb EMB120ERSDR CA011116013Actuator · seized(CAN) ON APPROACH FLAPS SELECTED FROM 10 TO 20 AS FLAPS TRAVELLED THROUGH APPROXIMATELY 15 DEGREES THE FORWARD FLAP MOTOR FAILED AND BROKE FREE OF THE TRANSMISSION/JACKSCREW ASSY. THIS CAUSED THE FLAP ACTUATOR ASSEMBLY TO BRAKE FREE OF THE ATTACHING STRUCTURENov 5, 2001 · Cessna 208BSDR AUS20011261Brush Holder · cracked(AUS) TRAILING EDGE FLAP ACTUATOR MOTOR BRUSH HOLDER ASSEMBLIES CRACKED. EXCESSIVE HEAT THROUGH FIELD WINDINGS. INSUFFICIENT GREASE OF INCORRECT TYPE IN GEARBOX ASSEMBLY. UNAPPROVED PART.Nov 5, 2001 · Beech 58SDR AUS20011260Attach Fitting · corroded(AUS) TRAILING EDGE FLAP ACTUATOR INTERNALLY CORRODED. ATTACHMENT LUG ALSO CORRODED.Nov 5, 2001 · Beech 58SDR CA011105004Actuator · stuck(CAN) PILOT REPORTED IN FLIGHT FAILURE OF FLAP SYSTEM LOCKED IN ONE POSITION. RETURNED TO MAINTENANCE BASE AND REPLACED FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE.Nov 4, 2001 · Cessna 208BSDR AUS20011205Pdu · failed(AUS) FLAP POWER DRIVE UNIT (PDU) FAILED. INTERNAL THERMAL SWITCH TRIPPED.Nov 2, 2001 · Pilats PC12SDR SWIA200110315Actuator · failedWHEN FLAPS 45 IS SELECTED OUTBOARDS DO NOT COME DOWN UNTIL TOUCHDOWN CAUSING DISAGREEMENT. REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. S/N OFF: 0400.Nov 2, 2001 · N268UE · Emb EMB120ERSDR AUS20011257Actuator · misinstalled(AUS) RT WING FLAP ACTUATOR INCORRECTLY INSTALLED.Oct 30, 2001 · Beech 58SDR SWIA200110305Actuator · failedCONTROL FAULT WOULD NOT RESET PER QRH. INBOARD FLAPS SHOWED 10 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR PER MM 27-50-00. OPS CHECK, LEAK CHECKS GOOD.Oct 29, 2001 · N190SW · Emb EMB120ERSDR IXXA0100066OActuator · leakingDURING DESCENT FROM DXB TO BRU, THE FLIGHT CREW NOTICED A DECLINE IN THE THE HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BRU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOCATED A DEFECTIVE FLAOct 22, 2001 · N822BX · Doug DC871FSDR SWIA200110257Actuator · failedUPON INITIAL POWER-UP, INBOARD FLAPS SHOWED 1 LIGHT BAR W/DISAGREEMENT ALARM. AFTER FOLLOWING MX PROCEDURES, INBOARD FLAPS SHOW ONLY 2 BARS W/45 DEGREES FLAPS SELECTED AND DISAGREEMENT. RESET OF FLAPS THEN GO TO 45 DEGREES, INBOARD FLAPS DON'T EXTEND AT ALL.Oct 19, 2001 · N250YV · Emb EMB120ERSDR SWIA200110255Connector · dirtyWHEN FLAPS 45 SELECTED DISAGREEMENT ON OUTBOARD FLAPS, 2 BARS DIFFERENCE. CLEANED OUTBOARD FLAP ACTUATOR CANNON PLUGS. CLEANED FLAP TRACKS AND ROLLERS. CYCLED FLAPS 2 DOZEN TIMES. CLEARED COMPUTER FAULTS. OPS CHECK GOOD.Oct 16, 2001 · N223SW · Emb EMB120ERSDR SWIA200110251Actuator · failedLOST BLUE HYDRAULIC SYSTEM ON FINAL APPROACH INTO SAN. REPLACED LT NACELLE FLAP ACTUATOR IAW EMB120 MM CHAPTER 27-50-00. OPS AND LEAK CHECK GOOD.Oct 14, 2001 · N560SW · Emb EMB120ERSDR CA011101005Actuator · inoperative(CAN) ON APPROACH, WHEN EXTENDING THE FLAPS, THE FLAP FAIL MESSAGE APPEARED AT 23 DEGREES. THE RIGHT OUTBOARD FLAP TWISTED, (OUTBOARD ACTUATOR STOPPED TRAVELLING). FOUND THE RT OUTBOARD FLAP TWISTED AND ACTUATOR NR 4 NOT OPERATIONAL.Oct 12, 2001 · Cndair CL6002B19SDR SWIA200110236Actuator · failedCONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD.Oct 9, 2001 · N190SW · Emb EMB120ERSDR SWIA200110224Actuator · failedFLAP DISAGREEMENT DURING FLAP RETRACTION AFTER LANDING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. NO LEAKS NOTED. NO FLAP DISAGREEMENTS NOTED. FLAPS FUNCTIONAL CHECK GOOD.Oct 5, 2001 · N250YV · Emb EMB120ERSDR SWIA200110295Rod End · wornRIGHT NACELLE FLAP ACTUATOR ROD END WORN. REPLACED RIGHT NACELLE FLAP ACTUATOR ROD END IAW 27-50-08.Oct 4, 2001 · N218SW · Emb EMB120ERSDR SWIA200110294Link · wornRIGHT OUTBOARD FLAP ACTUATOR ATTACHMENT LINK WORN. REPLACED ATTACHMENT LINK IAW 27-50-00.Oct 4, 2001 · N218SW · Emb EMB120ERSDR 2001FA0000323Piston · crackedRIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBSep 18, 2001 · N988ME · Beech B300SDR N988MEPiston · crackedRIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBSep 18, 2001 · N988ME · Beech B300SDR DL764011504Pin · out of adjON DEPARTURE, RECEIVED T/E FLAP DISAGREE UPON RETRACTION, RETURNED TO HNL FOR AN OVERWEIGHT LANDING 376,000 LBS. T/S PER FIM 27-51-00. RESET NR 1 ROTARY ACTUATOR PIN. RAN FLAPS SEVERAL TIMES WITH NO DISCREPANCIES. RETURNED A/C TO SERVICE.Sep 7, 2001 · N835MH · Boeing 767432ERSDR SWIA200110144Solenoid · brokenDURING APPROACH AFTER NORMAL GEAR EXTENSION FLAPS WERE SELECTED TO 15 DEGREES. A FLAP DISAGREEMENT WITH WARNINGS WAS OBSERVED FOLLOWED BY A HYDRAULIC WARNING AND COMPLETE LOSS OF BLUE SYSTEM HYDRAULICS. APPROXIMATE 10 MINUTES AFTER INITIAL FAILURE A LEFT ANSep 2, 2001 · N297SW · Emb EMB120ERSDR ASOA01149Actuator · failedFLT 4112 - DURING TAKEOFF FROM ATL, CREW RECEIVED A FLAP ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO ATL FOR A ZERO FLAP LANDING. MAINTENANCE TESTED FLAP ACTUATORS WITH BRAKE OUT BOX CHECK. BOTH LEFT AND RIGHT ACTUATORS FAILED.Aug 27, 2001 · N237AS · Emb EMB120SDR SWIA200110109Actuator · malfunctionedON DEPARTURE DURING FLAP RETRACTION, FLAP DISAGREEMENT INBOARD PAIR.FOUND LEFT INBOARD FLAP ACTUATOR WITH BAD WIPER. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. OPS GOOD.Aug 20, 2001 · N196SW · Emb EMB120ERSDR DHL2001727518Bellcrank · gougedINBOARD FLAP, O/B AFT FLAP ACTUATOR BELL CRANK, HAS SPRING GOUGING. CLEANED AND PAINTED RIGHT O/B FLAP AFT FLAP ACTUATOR DRUM PER M/M 12-10-00. REPLACED BOLT AND 2 SPACERS AND CONICAL WASHER AT AFT END OF FOLLOW UP DRUM. RESHIMMED FWD END OF FOLLOW UP DRUM Aug 19, 2001 · N727DH · Boeing 727228SDR SWIA200110106Actuator · erraticRT NACELLE FLAP POT IS ERRATIC.REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD IAW MM 27-50-08.Aug 18, 2001 · N1110J · Emb EMB120RTSDR SWIA200110096Actuator · malfunctionedAFTER SELECTING FLAPS TO 15 DEGREES ON DOWNWIND, RECEIVED ''FLAP ASYMMETRY'' WARNING. RIGHT INBOARD FLAP INDICATED 2 SEGMENTS BEYOND 15 DEGREES. INITIATED GO-AROUND. COMPLETED QRH PROCEDURE. SUBSEQUENT LANDING UNEVENTFUL. REMOVED AIRCRAFT FCU AND BENCH CHEAug 15, 2001 · N268UE · Emb EMB120ERSDR 2001FA0000213Bearing · brokenFLAP ACTUATOR ROD END BEARING, BROKEN ON SHORT FINAL. REPLACED BEARING PN 452860.Aug 10, 2001 · N54828 · Piper PA23250SDR UG82001F00002Power Unit · failedPROBLEM ENCOUNTERED: FLAPS FAILED. FLAP SYSTEM COMPONENT FAILURE. REPLACED FLAP POWER DRIVE UNIT, OPS CHECKED NORMAL.Aug 9, 2001 · N5115 · Cessna 750SDR 01FDEA00636Motor · leakingINBOARD FLAP DRIVE HYD MOTOR LEAKING IN LT WHEEL WELL. REMOVED AND REPLACED MOTOR PER 727 200 MM 27-51-062-4. LEAK CHECK GOOD.Aug 3, 2001 · N219FE · Boeing 727233SDR 2001FA0000340Actuator · crackedNORMAL FLIGHT OPERATION THE CENTER SHAFT OF THE ACTUATOR CRACKED THE ENTIRE LENGTH CAUSING FLAP BOUNCING SIMILAR TO BAD ROLLERS. RECOMMEND INSPECTING TOP AND BOTTOM OF ACTUATOR CENTER SHAFT DURING REGULAR PHASE INSPECTIONS.Aug 1, 2001 · N711HA · Beech B200SDR SWIA200110070Connector · contaminatedFLAP DISAGREEMENT WARNING AFTER SELECTION OF FLAPS 45. OUTBOARD FLAP PAIR INDICATES 2 BAR DISAGREEMENT. COMPUTER FAULT CODES SHOWING RIGHT OUTBOARD FLAP NOT RESPONDING. FOUND MOISTURE IN RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG, CLEANED MOISTURE. OPS CHECKEDJul 26, 2001 · N284YV · Emb EMB120ERSDR AUS20010791Connector · contaminated(AUS) RT OUTBOARD FLAP ACTUATOR ELECTRICAL CONNECTOR CONTAMINATED WITH MOISTURE.Jul 24, 2001 · Emb EMB120SDR 2001UALA01422Screw · missingLOSS OF HYDRAULIC FLUID IN THE 'A' SYSTEM. FOUND FLAP DRIVE MOTOR SHAFT SEAL PLATE MISSING SCREWS AND O-RING POPPED OUT. REPLACED FLAP DRIVE MOTOR AND SERVICED HYD SYS. OPERATIONS AND LEAK CHECK NORMAL.Jul 20, 2001 · N7261U · Boeing 727222SDR SWIA200110059Actuator · malfunctionedON DEPARTURE, FLAP DISAGREEMENT - INBOARD. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-02. LEAK AND OPS CHECK SATISFACTORY.Jul 20, 2001 · N215SW · Emb EMB120ERSDR ABXA010405Actuator · brokenSPLIT FLAP INDICATION FROM 15 DEGREES TO ZERO DEGREES. MECHANICS FOUND THE LEFT OUTBOARD FLAP ACTUATOR WITH BROKEN MOUNTING EAR. REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW DC-9 AMM 27-52-02-2-0001. NO LEAKS NOTED.Jul 19, 2001 · N984AX · Doug DC932SDR SWAA012022Motor · leaking(AIR TURNBACK) AFTER GEAR RETRACTION AT 400 FT BOTH A-HYD PUMP LOW PRESS LIGHTS ILLUMINATED, HYD SYSTEM QTY INDICATED 0. FOUND T/E FLAP HYD MOTOR LEAKING. REMOVED AND REPLACED FLAP MOTOR AND CASE FILTERS PER MM.Jul 16, 2001 · Boeing 7372H4SDR 2001UALA01406Motor · leakingINBOARD FLAPS INDICATION LIGHT ILLUMINATED WHILE RAISING FLAPS. AIRCRAFT RETURNED TO DEN. FOUND INBD FLAP HYD MOTOR LEAKING. REMOVED AND FOUND BEARINGS ROUGH, REPLACED WITH NEW REF MM27-53-19. CYCLED FLAPS SEVERAL TIMES, SYSTEM OPERATION NORMAL.Jul 14, 2001 · N7445U · Boeing 727222SDR CA010725013Drive Gear · failed(CAN) PILOTS REPORTED FLAP SYSTEM 1 AMP CIRCUIT BREAKER ON BATTERY BUS TRIPPED WHEN FLAP SELECTED DOWN. THE SYSTEM WOULD FUNCTION NORMAL IF THEY KEPT THE AIR SPEED BELOW 140 KNOTS. THE FAILURE COULD NOT BE DUPLICATED ON THE GROUND. THE FLAP POWER DRIVE UNIT WAJul 10, 2001 · Pilats PC1245SDR SWIA200110013Actuator · weakMULTIPLE FLAP DISAGREEMENT WHEN SET TO 45 DEGREES. NORMAL LANDING FLAPS 25 DEGREES. INSPECTED FLAP TRACKS FOR BROKEN/LOOSE HARDWARE, ALL OK. OPERATED ON GROUND, CHECK OK. LUBED ROLLERS CLEANED TRACKS, GROUND OPS GOOD. FOUND LEFT OUTBOARD FLAP ACTUATOR TO Jul 2, 2001 · N218SW · Emb EMB120ERSDR SWIA972656Actuator · failedOUTBOARD FLAPS DO NOT EXTEND FOR LANDING. PERFORMED TEST WITH BREAKOUT BOX AND LEFT OUTBOARD ACTUATOR FAILED WIPER TEST. INSTALLED SERVICEABLE UNIT IAW MM 27-50-09 AND CYCLED WITH BREAKOUT BOX AND WITH AIRCRAFT SYSTEM. ALL OPS AND LEAK CHECKS GOOD. PN ON 32Jun 25, 2001 · N194SW · Emb EMB120ERSDR SWIA972655Actuator · failedCONTROL FAULT OCCURS IN FLIGHT, WILL NOT RESET. OUTBOARD FLAPS FLASHING. REMOVED AND REPLACED BOTH OUTBOARD FLAP ACTUATORS IAW 27-50-04. RAN FLAPS NUMEROUS TIMES, OPS AND LEAK CHECK GOOD ON BOTH SIDES. PN ON 320300-1007 SN ON RT 1148, LT 0026A SN OFF RT Jun 24, 2001 · N194SW · Emb EMB120ERSDR DHL2001806002Mount · crackedASYMMETRICAL FLAP CONDITION ON APPROACH OUTER NEEDLE FAILED TO EXTEND, PASSED 23. ROLL TENDENCY FELT. EMERGENCY DECLARED. FOUND RT INBOARD ACT MOUNT LUG CRACKED. INSPECTED AREA, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED ACT ASSY IAW 27-59-9. SERVICED AJun 21, 2001 · N806DH · Doug DC873F
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