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 SWIA972173Connector · contaminatedCONTROL FAULT IN OUTBOARD PAIR OF FLAPS DURING APPROACH WITH ASSOCIATED ''FLAP'' AND ''ADVANCED SWS'' ON MAP. ATTEMPTED TO RESET AS PER QRH WHICH WAS UNSUCCESSFUL. CLEANED MOISTURE FROM RIGHT OUTBOARD ACTUATOR CANNON PLUG. FLAP SYSTEM OPS CHECK GOOD.Dec 9, 2000 · N200CD · Emb EMB120RTSDR SCNA00127Jackscrew · brokenDURING CLIMB OUT FROM MSP THE INBOARD FLAPS WOULD NOT RETRACT PAST THE TWO DEGREE POSITION. THE FLIGHT CREW RETURNED TO MSP. THE LEFT INBOARD JACKSCREW END TIP WAS FOUND BROKEN OFF, ALSO FORWARD ELEPHANT EAR BEARING DAMAGE WAS FOUND. REMOVED AND REPLACED JADec 2, 2000 · N275AF · Boeing 727227SDR SWIA972141Connector · contaminatedON DESCENT FLAP, ADVANCED SWS, CONTROL FAULT, OUTBOARD PAIR FLASHING. QRH WAS FOLLOWED BUT SYSTEM DID NOT RESET. FOUND MOISTURE IN CANNON PLUGS, CLEANED. USING PARKER FLAP TROUBLESHOOTING GUIDE, FOUND LEFT INBOARD FLAP SLOW TO EXTEND. REPLACED LEFT INBOARD Nov 30, 2000 · N200CD · Emb EMB120RTSDR CA010111003Actuator · frozen(CAN) AS COLD WEATHER ARRIVED LATE SEPTEMBER THE FLAP SYSTEM DEVELOPED MORE FREQUENT FLAP FAILURE INDICATIONS. WHEN TROUBLESHOOTING THE SYSTEM IT WOULD ALWAYS OPERATE NORMALLY IN THE HANGAR. AS A LAST RESORT TO CLARIFY THE PROBLEM THE FLAP ACTUATORS WERE FROZENov 29, 2000 · Pilats PC1245SDR CA001206013Support Bracket · cracked(CAN) PILOT REPORTED CIRCUIT BREAKER TRIPPED DURING FLAP SELECTION. MAINTENANCE FOUND FLAP MOTOR AND ACTUATOR MOUNTING STRUCTURE BENT AND CRACKED. REPLACED SUPPORT ASSEMBLY 2611144-1 AND FLAP MOTOR/ACTUATOR ASSY 9910586-3. NEW PARTS RIGGED, FLAPS AND TESTEDNov 24, 2000 · Cessna 208BSDR JBXA000221Actuator · bindingFLAPS FAIL MESSAGE ON EICAS ON APPROACH FLAPS AT 4 DEGREES. REMOVED AND REPLACED RIGHT OUTBOARD FLAP, OUTBOARD ACTUATOR IAW CRJ AMM 27-53-05. ALSO REMOVED AND REPLACED RIGHT BPSU IAW CRJ AMM 27-51-10. OPERATIONAL TEST OF FLAP SYSTEM GOOD AT THIS TIME IAW CRNov 23, 2000 · N571ML · Cndair CL6002B19SDR CA001211016Actuator · inoperative(CAN) THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AT 14 DEGREES DURING APPROACH.THE MAINTENANCE CREW REPLACED THE RT NR 3 ACTUATOR.Nov 22, 2000 · Cndair CL6002B19SDR SWIA972136Actuator · failedFLAPS DISAGREEMENT ON RETRACTION AFTER LANDING. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00 AND RII 27-307. FLAP ACTUATOR AND FLAP SYSTEM OPS CHECK GOOD. P/N ON 320300-1007, /SN ON 452, S/N OFF 0946.Nov 21, 2000 · N268UE · Emb EMB120ERSDR CA001212010Actuator · failed(CAN) FLAPS FAIL MESSAGE WHEN FLAPS SELECTED TO 8 DEGREES. FLAPS WENT TO 2 DEGREES. FOUND LEFT HAND INBOARD ACTUATOR WITH A HIGH RUNNING TORQUE.LEFT HAND INBOARD ACTUATOR REPLACED, OPERATION CHECK CARRIED OUT.Nov 18, 2000 · Cndair CL6002B19SDR SWIA972117Actuator · malfunctionedMOMENTARY FLAP LIGHT ON MAP ASSOCIATED WITH FLAP RETRACTION IN AIR/GROUND. REPLACED INLINE HYDRAULIC FILTER FOR INBOARD FLAPS AS REQUIRED. OPS CHECK FAILED. REPLACED LEFT AND RIGHT INBOARD FLAP ACTUATORS IAW MM 27-50-07, EMB 120 MM RII 27-307. OPERATIONS CNov 18, 2000 · N197SW · Emb EMB120ERSDR SWIA972115Connector · contaminatedFLAP DISAGREEMENT WHEN SELECTING FLAPS 45 DEGREES, OUTBOARD PAIR. CYCLED FLAPS SEVERAL TIMES. INSPECTED FLAP TRACKS. CLEANED MOISTURE FROM OUTBOARD LEFT AND RIGHT FLAP ACTUATOR AND CONNECTORS, OPS CHECK GOOD.Nov 18, 2000 · N196SW · Emb EMB120ERSDR CA001212008Actuator · failed(CAN) FLAPS FAILED AT ZERO. REPLACED RIGHT HAND WING NR4 FLAP ACTUATOR, ADJUSTMENT AND TEST CARRIED OUT NIL FAULT.Nov 17, 2000 · Cndair CL6002B19SDR SWIA972126Connector · contaminatedON CLIMBOUT, DIFFICULTY BRINGING UP FLAPS. CLEANED GLYCOL FROM ACTUATOR CANNON PLUGS. FOUND SYSTEM TO OPERATE NORMAL.Nov 16, 2000 · N215SW · Emb EMB120ERSDR SWIA972113Connector · contaminatedWHEN RETRACTING FLAPS FROM 15 DEGREES TO UP ON DEPARTURE CONTROL FAULT PERIODICALLY AND THEN EXTINGUISHES. CLEANED DEICE FLUID FROM O/B FLAP ACTUATOR CANNON PLUGS. OPS CHECK GOOD.Nov 15, 2000 · N194SW · Emb EMB120ERSDR CA001129025Actuator · failed(CAN) FLAPS FAILED ON APPROACH AT ZERO. FLAPLESS LANDING CARRIED OUT NORMALLY.SYSTEM RESET IN CHICAGO. CHANGED NR 4 FLEX SHAFT AND NR 1 FLAP ACTUATOR, FLAPS SYSTEM RIGGED OPERATION CHECKED NORMAL. WINTERIZATION TASK COMPLETED.Nov 14, 2000 · Cndair CL6002B19SDR JBXA000219Bpsu · inoperativeFLT 44 RDU/BDL EN ROUTE FLAP OVERSPEED CLACKER SOUNDED WHILE CLIMBING THROUGH FL 265 FOLLOWED BY A FLAPS FAIL CAUTION MESSAGE. RETURNED TO RDU. REMOVED AND REPLACED LT AND RT BPSU. RIGGED AND OPS CHECK IAW CRJ MM 27-51-10.Nov 12, 2000 · N592ML · Cndair CL6002B19SDR UPS00234433Actuator · inoperativeINSPECTION TYPE:N/A ON T/O RFD, FLAPS HUNG AT GREATER THAN 2 DEG (IN BLACK BAND) L/E FLAP LIGHT RED CHRISTMAS TREE INDICATES LEP 5, 6 FAILED TO RETRACT, AMBER LIGHTS. RECYCLED, NO HELP. AIR TURNBACK RFD, GROUND TEST IN RFD INBOARD FLAPS LAGGING BEHIND OUTBOANov 10, 2000 · N207UP · Boeing 727247SDR AU001077Actuator · cracked(AUS) RT FLAP ACTUATOR BODY CRACKED AND LEAKING. CRACK LENGTH 40MM(1.57IN). MANUFACTURER STATES THAT THIS ITEM IS ONE OF A BATCH OF ACTUATORS WITH SUSPECT INCORRECT MACHINING OF THE ACTUATOR BODY BORE.Nov 7, 2000 · Frchld SA227DCSDR 20001102SH030Actuator · crackedNOTED DURING REMOVAL OF ACTUATOR FOR ROUTINE 1,200-HOUR LUBE THAT ACTUATOR PISTON WAS CRACKED FOR ENTIRE LENGTH IN AN APPROXIMATELY STRAIGHT LINE. A NEW P/N''D ACTUATOR AND ACTUATOR SHAFT WAS INCORPORATED ON AIRCRAFT, SN R-129, AND UP. REPLACED ACTUATOR WITNov 2, 2000 · Beech B300SDR AU001043Actuator · cracked(AUS) FLAP ACTUATOR HOUSING CRACKED. LOSS OF HYDRAULIC FLUID.Oct 30, 2000 · Frchld SA227DCSDR RRXA001072Actuator · failedHYDRAULIC SYSTEM QUANTITY LOSS ON TAXI IN. COMPLETED EMERGENCY ACTION ITEMS TOWED AIRCRAFT TO RAMP. REMOVED AND REPLACED LT INBOARD FLAP ACTUATOR ASSY IAW DC-8 MM 27-51-9. LEAK AND OPS CHECK GOOD AT THIS TIME.Oct 19, 2000 · N795FT · Doug DC873FSDR CA001024040Actuator · failed(CAN) FLAPS FAILED AT 38 DEGREES. PERFORMED ACTUATOR TORQUE CHECKS PER AMM, FOOUND NR 1 ACTUATOR RT WITH SLIGHTLY HIGHER TORQUE THAN THE OTHER ONES. REPLACED NR1 ACTUATOR RT.Oct 17, 2000 · Cndair CL6002B19SDR 20001030SH015Motor · failedFLAP MOTOR BURNED OUT. SUBMITTER STATED THEY PUT 2 NEW UNITS IN FROM CESSNA, CHECK OF ACTUATOR AND GEARBOX FOUND NO DEFECTS. TURNS FREELY. CHECKED WIRES, NO DEFECTS. UNKNOWN CAUSE OF FAILURES. DATE OF MANUFACTURE OF MOTOR NR 2 IS 7/99. (X)Oct 13, 2000 · N737XM · Cessna 172NSDR 20001030SH014Motor · failedFLAP MOTOR BURNED OUT. SUBMITTER STATED THEY PUT 2 NEW UNITS IN FROM CESSNA, CHECK OF ACTUATOR AND GEARBOX FOUND NO DEFECTS. TURNS FREELY. CHECKED WIRES, NO DEFECTS. UNKNOWN CAUSE OF FAILURES. DATE OF MANUFACTURE OF MOTOR NR 2 IS 7/99. (X)Oct 13, 2000 · N737XM · Cessna 172NSDR COMA0060807Actuator · failedFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT INBOARD FLAP ACTUATOR.Oct 6, 2000 · N969CA · Cndair CL6002B19SDR CA001024009Actuator · failed(CAN) CREW REPORTED FLAP FAIL MESSAGE AND FLAPS MOVEMENT STOPPED AFTER SELECTION FROM 0 TO 8 DEGREES DURING APPROACH. (NOTE: SB 601R-27-111 WAS CARRIED OUT 3 WEEKS AGO.) THE MAINTENANCE FOUND THE FLEXSHAFT BETWEEN NR 3 & NR 4 ACTUATORS TWISTED/KINKED. CABLES RSep 23, 2000 · Cndair CL6002B19SDR 31270922528Actuator · failedFLAP CONTROL UNIT AND FLAP ASYM INDICATIONS ON EICAS SCREEN. RIGHT FLAP INDICATED 27 DEGREES AND LEFT FLAP INDICATED 0 DEGREES. BOTH FLAPS ACTUALLY AT 0 DEGREES. REMOVED AND REPLACED RIGHT FLAP ACTUATOR. OPS CHECK GOOD ON GROUND.Sep 22, 2000 · N430Z · Dorner DO328300SDR RRXA003098Link · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE SUPPORT AFT LINK ON THE LEFT I/B FLAP SUPPORT AT STA 98 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 22, 2000 · N957R · Doug DC863FSDR RRXA003093Link · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE LEFT I/B FLAP SUPPORT AFT LINK AT STA 98 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 22, 2000 · N957R · Doug DC863FSDR USAASB00268Actuator · detachedBDL - FLT 1738 - WHEN FLAPS WERE EXTENDED FOR LANDING AT BDL, FROM PHL, THE AIRCRAFT ROLLED RIGHT. IT REQUIRED OPPOSING AILERON FORCE OF 2 TO 3 DEGREES LEFT AILERON TO STOP ROLL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT INBOARD AFSep 21, 2000 · N395US · Boeing 7373B7SDR SWIA971989Actuator · failedSETTING FLAPS FROM 0 DEGREES TO 8 DEGREES FLAPS FAILED AT 0 DEGREES WITH ATTENDING FLAP FAIL CAUTION MESSAGE. PERFORMED A ''''NO FLAP'''' LANDING. FOUND RIGHT HAND FLAP NUMBER 4 FLEX SHAFT SHEARED AND NUMBER 4 FLAP ACTUATOR BAD ON THE RIGHT SIDE. REPLACED DSep 20, 2000 · N410SW · Cndair CL6002B19SDR 20001031SH010Actuator · wornTWO SHAFT SUPPORT BEARINGS WERE NOT INSTALLED AT THE TIME OF ORIGINAL ASSEMBLY. THE OMISSION OF THESE BEARINGS SA13589-1 AND SA13588-1 CAUSED PREMATURE WEAR OF THE WORN SHAFT RESULTING IN EXCESSIVE GEAR BACKLASH. (X)Sep 14, 2000 · Pilats PC12SDR COMA0060756Actuator · failedFLAP FAIL CAUTION MESSAGE AT ZERO DEGREES WHILE ON GROUND. REPLACED THE LEFT OUTBOARD FLAP ACTUATOR.Sep 14, 2000 · N917CA · Cndair CL6002B19SDR P2EA00251Fitting · crackedSJO - DURING C-CHECK, LEFT WING INBOARD FLAP BOOM FORWARD ATTACH FITTING CRACKED. REPAIRED BY MODIFICATION IAW SB 737-27-1110 SECTION III FIGURES 2, 3 AND 4. (M)Sep 12, 2000 · N124NJ · Boeing 737230SDR DL76K001779Actuator · failedHIGH FREQUENCY POPPING SOUND COMING FROM RT ENG ON TAXI OUT. FOUND RT I/B FLAP ROLLERS TRANSMITTING SOUND. REPLACED RT O/B ROTARY ACTUATOR AND PDU CNTRL VLV.Sep 12, 2000 · N171DZ · Boeing 767332SDR AU001318Actuator · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF SYSTEM 1 HYDRAULIC FLUID.Sep 10, 2000 · Fokker F28MK4000SDR CA000926006Actuator · worn(CAN) ON INSPECTION, THE BACKLASH WAS FOUND EXCESSIVE. (X)Sep 10, 2000 · Pilats PC1245SDR AU001320Actuator · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF UTILITY HYDRAULIC SYSTEM FLUID (SYSTEM 1).Sep 9, 2000 · Fokker F28MK4000SDR SWIA971959Actuator · failedOUTBOARD FLAP DISAGREEMENT. COULD NOT FIX PER QRH. RETURNED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPS CHECKS AND LEAK CHECKS GOOD. RII 27-307. P/N ON: 343000-1003, S/N: 0330, S/N OFF: 0554.Sep 6, 2000 · N308SW · Emb EMB120ERSDR SWIA971975Actuator · malfunctionedFLAP ASYMMETRY AFTER TAKEOFF. RETURNED TO MRY. MX COMPUTER SHOWED (LT LVDT IMP FLR ), PERFORMED CONTINUITY CHECK FROM FCU TO LEFT OUTBOARD ACTUATOR IAW MM 27-51-00, OPS CHECKS GOOD. REPLACED OUTBOARD FLAP ACTUATOR IAW 27-50-09, OPS CHECKS GOOD. (P/N 34300Sep 6, 2000 · N292UX · Emb EMB120ERSDR AU000825Actuator · cracked(AUS) RT FLAP ACTUATOR BODY CRACKED. LOSS OF HYDRAULIC FLUID.Sep 4, 2000 · Frchld SA227DCSDR AU000706Jackscrew · faulty(AUS) FLAPS UNABLE TO BE MOVED FROM THE UP' POSITION. SUSPECT FAULTY RT OUTBOARD SCREWJACK.Sep 1, 2000 · Bac 146200ASDR CA000925008Bracket · broken(CAN) WHILE COMPLETING THE ROUTNE A INSPECTION THE OUTBOARD FLAP ACTUATOR ATTACHMENT ARMS WERE FOUND BROKEN. THE AIRCRAFT WAS GROUNDED UNTIL THE FLAP WAS REPLACED. PARTS ARE BEING SHIPPED BACK TO CONAIR FOR INSPECTION.ALL ACTIVE AIRCRAFT INSPECTED AND FOUND SEAug 26, 2000 · Doug DC6ASDR 20001030SH034Transmission · separatedON TAXIING AFTER LANDING, PILOT SELECTED FLAPS UP. HE THEN HEARD A LOUD POPPING SOUND, THE FLAPS STOPPED RETRACTING, AND THE FLAP FAULT LIGHT ILLUMINATED. MAINTENANCE FOUND THE RIGHT FLAP HANGING LOOSE, FULLY DOWN. THE FLAP JACKSCREW HAD BECOME SEPARATED FRAug 24, 2000 · N509F · Sud CM170SDR 2000UALA00501Bypass Valve · malfunctionedFLAP HANDLE WOULD NOT OPERATE. *S/D* REPLACED TRAILING EDGE SLAT ACTUATOR BYPASS VALVE (P/N: S256T005-8).Aug 22, 2000 · N650UA · Boeing 767322SDR 00FDEA00540Actuator · leakingNR 1 A SYS LOW PRESSURE LIGHT CAME ON. NR 2 A SYS LIGHT OUT. RAN HYD LEAK OR LOSS CKLIST, SHUTOFF A SYS PUMP AND FLUID. *S/D* REMOVED AND REPLACED NR 1 & 2 A SYS HYD PUMPS, CASE DRAIN AND PRESSURE FILTERS AND I/B FLAP DRIVE MOTOR PER MM 29-11-0, 29-11-41, Aug 11, 2000 · N216FE · Boeing 7272S2FSDR AU000763Bearing · failed(AUS) TRAILING EDGE HYDRAULIC FLAP DRIVE MOTOR DRIVE SHAFT BEARING FAILED.Jul 25, 2000 · Boeing 737377SDR FWT2001F00003Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROL VALVE IAW Jul 12, 2000 · N872SJ · Doug DC871FSDR FWT2001F00002Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP, WHEN FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROLJul 12, 2000 · N872SJ · Doug DC871FSDR 20000803SH006Control Cable · brokenASG/LIT - WHILE EN ROUTE AND ON APPROACH AT ABOUT 500 AGL, PILOT EXPERIENCED A FLAP SYSTEM FAILURE UPON DEPLOYMENT OF THE FLAPS, ONLY THE LT SIDE CAME DOWN. THIS CAUSED THE AIRPLANE TO ROLL VIOLENTLY. THE FLAPS WERE RETRACTED, CONTROL OF THE AIRCRAFT WAS REGJul 12, 2000 · N402BF · Cessna 402B
Back to JASC 2752