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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA201232231Actuator · failedOUTBOARD FLAP WOULD NOT COME UP AFTER TAKEOFF. (FLT 7790) REPLACED LEFT INBOARD FLAP ACTUATOR AND WIRE W602-0014-22 IAW AMM AND WDM.SDR CA121213008Coupling · twisted(CAN) RUBBER FLAP ACTUATOR COUPLING FOUND EXCESSIVELY TWISTED DURING FLAP ACTUATOR INSPECTION. RUBBER COUPLING REPLACED AND ACFT RETURNED TO SERVICE.SDR CA121120007Actuator · failed(CAN) FLAPS FAIL C/M POSTED ON EICAS DURING FLAP SELECTION ON APPROACH. FLAPS DID NOT MOVE FROM THE ZERO POSITION. QRH ACTIONED. GO AROUND FOR ZERO FLAP LANDING WAS C/O. FLAP FAIL FORM SENT TO TECH OPS. NO HISTORY. FLAP FAIL EVENT, OPERATING UNDER CREW SDR SWAA2012111509482Control Unit · faultyDECLARED EMERGENCY -- FLAPS WOULD NOT EXTEND HYDRAULICALLY (ON APPROACH). EXTEND FLAPS ELECTRICALLY (ALTERNATE FLAP EXTENSION). VIA QRH PROCEDURE - FLAPS EXTENDED TO POS 15 FOR APPROACH AND LANDING. REMOVED AND REPLACED FLAP MOTOR HYD UNIT. SYS CHECKS NORMSDR SIMA20121112004Actuator · leakingON FLIGHT 4009 THE CREW REPORTED THEY WERE CLEARED FOR AN ILS 27L INTO ORD AND RECEIVED A FLAP FAIL MESSAGE WHEN TRYING TO DEPLOY FLAPS 9, FLAPS STAYED AT 0. THE CREW PERFROMED THE AOM CHECKLIST AND ASKED FOR VECTORS OFF THE APPROACH AND DECLARED AN EMERGENCYSDR UALA2012111206509Motor · failedDURING PRIMARY ELECTRIC MODE CHECK OUTBOARD TRAILING EDGES FAILED TO DRIVE TO 5 UNITS. CORRELATED MAINTENANCE MESSAGE 27773. REPLACED OUTBOARD FLAP ALTER DRIVE MOTOR PER MM, CHECKED GOOD.SDR CA121107003Actuator · failed(CAN) PRELIMINARY REPORT FLAP FAIL ON APPROACH. FLAP FAIL EVENT, OPERATING UNDER CREW RESET. ACTION PLAN ASSIGNED 182-06, NOV 12-01 NO RESOLULTION YET MORE TO FOLLOW.SDR SIMA20121101001Pdu · failedON FLIGHT 4350 THE CREW REPORTED THAT ON APPORACH THE FLAPS FAILED IN THE ZERO POSITION. THE CREW COULD NOT OBTAIN ANY FLAPS ON LANDING. THE CREW DECLARED AN EMERGENCY AND RAN THE APPROPRIATE CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WASDR SIMA20121028002Actuator · lack of lubeON FLIGHT 4018 THE CREW REPORTED THAT THE FLAP FAILED WHEN SELECTING FLAP 9 ON APPROACH INTO ORD. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP SCREW JACK ACTUATOR GEAR - LUBRICATION IAW FISDR CA121024006Actuator · failed(CAN) ON APPROACH, THE FLAPS REMAINED AT 0 DEG WHEN SELECTED. THE CREW DID A MISS APPROACH AND CAME AROUND AND LANDED SAFELY WITH FLAP 0. NO EMERGENCY WAS DECLARED. REF DEFECT- 1081476, RESOLVED ON WO: 358098, TASKCARD: NR-00001, REPLACED FLAP ACTUATORS- LSDR SWIA201231838Flex Drive · corrodedMOST OUTBOARD FLEX SHAFT RUSTED INTO THE OUTBOARD FLAP OUTBOARD ACTUATOR. (C-CHECK) REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR AND NR 5 FLEX DRIVE IN REFERENCE TO CRJ200 AMM.SDR UALA2012092005323Actuator · faultyFLIGHT CONTROL SYSTEM EICAS MESSAGE. NEEDS RIGHT INBOARD FLAPERON ACTUATOR REPLACED. REPLACED RIGHT FLAPERON INBOARD ACTUATOR AS PER AMM. ALL REQUIRED MAT TEST PASSED OPS AND LEAK CHECK ACCOMPLISHED. NO LEAKS NOTED, ALL INDICATIONS NORMAL NOW.SDR A6WA20120920022Actuator · chafedRIGHT I/B FLAP VANE ACTUATOR TUBE ARE CHAFED FROM ROLLERS. REPAIRED DAMAGE IAW REO 601R-57-52-1962.SDR A6WA20124M515Actuator · chafedLEFT I/B FLAP VANE ACTUATOR TUBES ARE CHAFED FROM ROLLERS. REPAIRED DAMAGE IAW REO 601R-57-52-1961.SDR 6RXA20120911001Pdu · failedDURING GO AROUND FLAPS WOULD NOT RETRACT AND FLAP CAWS WARNING ILLUMINATED. SYSTEM WAS TROUBLESHOT TO A FAULTY FLAP CONTROL AND WARNING UNIT. REPLACED UNIT AND PERFORMED FUNCTIONAL TESTS. FLAP SYSTEM FAILED ON THE GROUND AFTER SEVERAL EXTENSIONS AND RETRACTSDR UALA2012081404508Actuator · malfunctionedFCTL FLAPS SYS FAULT. FLIGHT DIVERTED. WHILE PERFORMING VISUAL INSPECTION, FOUND NR 1 LT FLAP ROTARY ACTUATOR WITH ACTIVATED TORQUE LIMITER. INSTALLED NR 1 LT ROTARY ACTUATOR PER AMM. REPLACED LT NR 1 FLAP TRACK ACTUATOR. COMPLETED INSTALLATION FROM ITEM SDR CA120816003Adapter · broken(CAN) FLAP MOTOR ACTUATOR ADAPTER PLATE STUD FOUND TO HAVE BROKEN OFF.SDR CA120803002Actuator · defective(CAN) ON APPROACH EICAS, FLAP FAIL, MESSAGE WHEN FLAPS SELECTED FROM 1 TO 2. TOUCHDOWN SPEED 175 KTS RATE OF DESCENT APPROXIMATELY 300 FPM AT TOUCHDOWN. LT NR 3 FLAP ACTUATOR REPLACED IAW AMM 27-51-01.SDR UALA2012072003952Actuator · leakingSMALL HYDRAULIC LEAK FROM RT OTBD FLAPERON ACTUATOR ROD END. FOUND RT FLAPERON OTBD ACTUATOR ROD END LEAKING 2 DROPS PER MINUTE WITHIN LIMITS. REPAIR WITHIN 75 FLIGHT HOURS. SERVICE HYDRAULICS TO FULL.SDR CA120503002Actuator · failed(CAN) ON APPROACH HAD A FLAP FAILURE, THE CREW CONDUCTED A MISSED APPROACH AND WENT THROUGH THE CHECKLIST. NO EMERGENCY WAS DECLARED. NO FURTHER ISSUES. FOUND NR 3 R FLAP ACTUATOR TRIPPED. REMOVED AND INSTALLED NR 3 RT FLAP TRANSMISSION IAW AMM 27-51-01.SDR CA120430003Gimbal Joint · misinstalled(CAN) DURING WALK-AROUND, IT WAS NOTED THAT THE LT INBD FLAP SEGMENT EXHIBITED AN EXCESSIVE AMOUNT OF FORE AND AFT PLAY. INVESTIGATION REVEALED THAT THE FLAP ACTUATOR GIMBAL ASSY THAT PROVIDES THE ACTUATOR TO AIRFRAME MOUNTING INTERFACE WAS LOOSE ON THE FLAP SDR CA120424003Actuator · failed(CAN) DURING FLAPS ZERO DEGREE RIGGING PROCESS FLAPS SEENED TO BLOCK, AFTER INVESTIGATION LARGE PIECES OF NON FERRUS MATERIAL WAS SEEN THROUGH OIL SERVICING PORT. LEFT OTBD NR 4 FLAP TRANSMISSION .SDR CA120417005Pin · sheared(CAN) AFTER LANDING, THE FLAPS WOULD NOT RETRACT. THE FLAP ACTUATOR WAS REPLACED AND THE FLAPS FUNCTION CHECKED. UPON DISASSEMBLY OF THE FLAP ACTUATOR THE PIN THAT SECURES THE PISTON TO THE SHAFT WAS FOUND SHEARED.SDR UALA2012032301848Pcu · leakingFLUID COMING OUT 1ST FLAP FAIRING OUTBOARD OF RT ENGINE. MAINT TEXT: CHECKED & FOUND LEAK I/B OF RT ENGINE AT RT FLAPERON I/B ACTUATOR ROD END. LEAK RATE IS 2 DPM STATIC & 9 DPM IN OPERATION. NEEDS FLAPERON ACTUATOR 646-9013. NEEDS REPLACEMENT WITHIN 75 HOSDR CA120321004Actuator · failed(CAN) AFTER TAKE OFF THE FLAP FAIL AT 20 DEGREES DOWN, THE AIPLANE FLEW TO DESTINATION WITH THE FLAPS AT 20 DEGREES AND LANDED WITHOUT INCIDENT.SDR 9JLA2012032104403Actuator · defectiveTHE CREW REPORTED THAT THE TE FLAPS FAILED TO RETRACT FROM THE 12 DEGREE POSITION AFTER TAKEOFF. TROUBLESHOOTING IDENTIFIED THE RT NR 3 FLAP ACTUATOR AS DEFECTIVE. INSTALLED AN O/H UNIT. OPS CHECKED SATISFACTORY.SDR CA120402006Actuator · malfunctioned(CAN) FLAP DRIVE CAUTION LIGHT ILLUMINATED DURING FLAP RETRACTION. FLAPS STALLED AT 10 DEGREES. MAINTENANCE REPLACED 1 WORN FLAP ROLLER, RT INBD FLAP, INBD AFT ROLLER. MAINTENANCE ALSO REPLACED ALL 4 INBD FLAP ACTUATORS DUE TO SUSPECT WEAR. ALL 4 UNITS HAVSDR SWAA2012030802010Motor · faultyDECLARED EMERGENCY, FLAPS FAILED TO EXTEND ON APPROACH EMERGENCY WAS DECLARED NON NORMAL CHECKLISTS RUN ALTERNATE FLAPS. DID NOT EXTEND CHECK LIST FOR L/E. FLAPS ONLY WERE EXTENDED. REMOVED AND REPLACED FLAP HYD POWER MOTOR PER MM.SDR REXA2012030700344Actuator · failedFLAPS FAIL AT 17 WITH HANDLE AT 20. FLAPS EXTENDED AT 8000FT AND 190KTS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009, TR # 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REFSDR REXA2012022600276Actuator · malfunctionedFLAPS FAIL MESSAGE - EICAS MESSAGE (FLAPS FAIL) OCCURED IN FLIGHT DURING CLIMBOUT. OCCURED DURING FLAP RETRACTION. EICAS POSITION WAS AT ZERO WHICH MATCHED FLAP LEVER, AIRSPEED APPROX 170 IAS, TEM - 24 ABOUT 2 MIN INTO FLIGHT. PERFORMED TROUBLESHOOTING PER BSDR UALA2012020700736Actuator · leakingRT WING INBD FLAP CANOE FAIRING LEAKING HYDRAULIC FLUID OUT OF THE DRAIN HOLES. CHECKED AND FOUND DROPS PER MINUTE UNDER 10 AND WITHIN LIMITS PER AMM. CARRIED FORWARD 150 FLIGHT HOURS. CURRENT PTT 58864. WHILE TROUBLESHOOTING HYD LEAK FOUND TO BE OUT OF LISDR MASA2012020894402Actuator · failedFLAPS FAIL. R2 LT NR 1 FLAP ACTUATOR AND RIGGED FLAPS.SDR CA120131002Actuator · failed(CAN) FLAP FAIL MESSAGE C APPEARED JUST AFTER THE FLAP LEVER WAS SET FROM 0 TO 20 DEGREE DURING APPROACH, IAS 190KT, OAT -15C. FLIGHT HR IS APPROXIMATERY 1 HR FROM DEPATURE. FLAP POSITION INDICATION WAS 0 DEGREE THROUGH THE ENTIRE EVENT. THE CREW ATTEMPT FLSDR SWIA201229417Actuator · out of rigRIGHT ROLLING FORCE UPON EXTENSION OF FLAPS. (FLT 4658) RE-RIGGED FLAP ACTUATOR R-4.SDR CA120221004Actuator · failed(CAN) FLAPS FAIL C ON APPROACH - FLAPLESS LANDING. MAINTENANCE APPLIED TC AD CF2007-10R1, PART V. ALL FLEXSHAFT WERE INSPECTED, CLEANED AND LUBRICATED. RT OTBD FLAP ACTUATORS WERE REPLACED.SDR USAA2012011700033Actuator · malfunctionedON APPROACH AT 4000 FEET, UNABLE TO GET FLAPS IN PROPER LANDING CONFIGURATION, FLIGHT CONTROL FLAP FAULT - NO TRAILING EDGE FLAPS. DECLARED EMERGENCY. FOUND TRIPPED TORQUE LIMITER ON LEFT FLAP TRACK 1 ACTUATOR 6205CM. REMOVED AND REPLACED ACTUATOR ASSEMBLY SDR REXA201200124Flex Drive · damagedFLAP FAIL CAUTION MSG AT 0 DEG ON APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) AMOC DATED MARCH 27, 2009, TR #27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD 27-052G. FOUND LT NR 3 FLEX SHAFT AND RT SDR REXA201200109Actuator · failedFLAPS FAIL AT 16 DEGREES ON DEPARTURE. T/S PER FIM 27-50-00. FOUND NR 2, 3, 4, 1 ACTUATORS ON RT WING BAD. REMOVED AND REPLACED ACTUATORS IAW AMM 27-53-01, AMM 27-53-05. OK FOR SVC. XFER TO AML PAGE 2230543 C/W PA AD 27-052G.SDR REXA201200102Actuator · failedAIR RETURN FOR FLAPS FAIL IN FLT AT 16 DEGREES. REMOVED AND REPLACED ACTUATOR, OPS CHECK GOOD.SDR REXA201200031Flex Drive · dirtyON APPROACH INTO DTW FLAPS FAIL HAPPENED AT 0 DEGREES WHEN TRYING TO SELECT TO 20 DEGREES. JAM CODES HAVE BEEN DOCUMENTED AND SENT TO MOTOR GROUP AIRSPEED 190 KTS. PERFORMED FLAP FLEX SHAFT CLEAN & LUBE IAW FLAP LUBE CHECKLIST. OK FOR SERVICE, OP CHECK GOODSDR REXA201200028Flex Drive · dirtyEMERGENCY DECLARED FOR FLAPS FAIL CAUTION MSG IN FLIGHT, PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARA (N)(6)(I), AMOC DATED MARCH 27, 2009 TR#27-012 PER AMOC DATED DEC18,2009 AND PA AD 27-052G, WITH NEWEST FIM REV 42 AS T/S AID. SEE DISC NR 2SDR REXA201200025Flex Drive · damagedAIR RETURN FOR FLAP FAIL CAUTION MESSAGE FLAPS 13 INDICATION QRH FLAPS FAIL COMPLETE. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) AMOC DATED MARCH 27, 2009, TR#27-012 PER AMOC DATED DECEMBE 18, 2009 AND PA AD 27SDR UALA2011122107041Rotary Actuator · failedFCTL FLAPS FAULT WITH FLP1 SYSTEM JAM CHECK FLP MECH DRIVE AND FLP2 SYSTEM JAM CHECK FLP MECH DRIVE FAILURE MESSAGES. REFERENCE TSM 27-51-00-810-810. RECORD PPU ANGLES PRIOR TO RESETTING ANY CB'S OR MOVING FLAP-SLAT HANDLE. REPLACED NR 2 LT FLAP ROTARY ACTSDR CA111206014Actuator · worn(CAN) DURING HEAVY MAINTENACE, INSPECTION OF THE LT INBD FLAP ACTUATOR, NR 1 POSITION, REVEALED EXCESSIVE PLAY IN THE INPUT SHAFT. THE ACTUATOR HAS BEEN SENT TO THE VENDOR FOR INSPECTION/REPAIR. A SERVICEABLE ACTUATOR WAS INSTALLED IAW THE AMM. THIS SDR WILLSDR R61A20110417Actuator · malfunctionedCREW REPORTED FLAP FAIL MSG DURING CLIMB AFTER TAKE-OFF FROM MCI. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT MCI, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED 2L FLAP ACTUATOR PER EMB AMM, OPS CHECK GOOD.SDR SWIA201128779Actuator · corrodedRUST COMING FROM THE INBOARD SHAFT OF THE L-3 FLAP ACTUATOR. (SERVICE) REPLACED FLAP ACTUATOR L-3. / P/N OFF: 766365B S/N OFF: 0360SDR REXA201100887Pdu · defectiveFLAPS FAILED AT 43 UPON FINAL APPROACH. OAT 3C. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009, TR#27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-05AG. FECU CODES 11 2A, 11 2B, 15 2A, 1SDR SIMA201133401Motor · inoperativeON FLIGHT 4074 THE CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE DURING DESCENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB 145 AMM 27-53-03. THE OPESDR CA111123005Actuator · failed(CAN) EN-ROUTE, FLIGHT CREW FELT LIKE IF THE FLAPS WERE EXTENDED. THE SPEED WAS REDUCED, THE FLAP SELECTOR CYCLED FROM 0 TO 5 DEGREES & BACK TO 0 DEGREES. HOWEVER THERE WAS NO FLAP MOVEMENT DETECTED. FLAPS POSITION WERE VISUALLY CONFIRMED & FOUND EXTENDED. SDR ASOA2011TY003Control Unit · bindingFLAP FAIL MESSAGE AT 45 DEGREES AND WILL NOT COME UP. R & R FECU IAW AMM 27-53-02. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK OF BOTH FLAP TRANSMISSION BRAKES OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
Back to JASC 2752