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 FDEA201008032801Actuator · malfunctionedDURING FLAP RETRACTION AMBER L/E FLAP REMAINED ILLUMINATED AT FLAPS 2DEG POSITION. S/O PANEL VERIFIED NR 5 SLAT REMAINED EXTENDED ROLLING MOMENT FELT IN YOKE. RAN QRH NO HELP. LANDED NORMAL MEM NO DUMP REQUIRED. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP PSDR CA100812014Retaining Nut · mismanufactured(CAN) NOTICED THE LT INBD FLAP TO BE TIGHT, LOWERED FLAPS TO INVESTIGATE IF ANY FAULTS WERE PRESENT, THEN NOTICED THAT THE LT INBD FLAP ACTUATOR RETAINING NUT WAS RETREATED BEYOND ACCEPTABLE TOLERANCE.SDR C2XA10CL121Brake · faultyCLE FLT 2243 - THE CREW REPORTED A FLAP FAILURE AFTER TAKEOFF UPON FLAP RETRACTING. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECKS WERE GOOD.SDR RAIA201007250002Actuator · malfunctionedON APPROACH FLIGHT CREW GOT A "FLAP FAIL" MESSAGE AND FLAPS WERE STUCK AT 0 DEGREES. AIRCRAFT MADE AN EMERGENCY LANDING. MAINTENANCE INSPECTED AND LUBRICATED ALL FLAP SCREW ACTUATOR GEARS. FLAP SYSTEM OPS CHECKED GOOD.SDR CHQA201000140Flex Drive · damagedWHILE ON APPROACH TO CID, WHEN THE CREW SELECTED THE FLAPS TO 9 DEGREES, THE FLAPS STAYED AT ZERO AND FLAP FAIL WAS DISPLAYED ON EICAS. THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO SDSDR UALA2010070602412Motor · faultyON EXTENSION FLAP HANDLE MAKES A NOISE & VIBRATION AS IT APPROACHES EACH SELECTED FLAP SETTING. FLAPS HAS A VIBRATION PRIOR TO REACHING A SELECTED POSITION, NO NOISE IN ALTERNATE. PROBLEM ISOLATED TO HYD MOTOR. REPLACED HYDR MOTOR. OPS CKS NORMAL.SDR CA100528010Actuator · malfunctioned(CAN) ON A WALKAROUND, IT WAS DISCOVERED THAT THE WING FLAPS WERE EXTENDING VERY SLOWLY WITH AN AUDIBLE GRINDING NOISE. UPON INSP, IT WAS FOUND THAT THE FLAP ACTUATOR HAD A WORN INPUT SHAFT AND FAILED COUPLER TO THE ELECTRIC MOTOR. THE ACFT WAS SNAGGED AND ASDR UALA2010051101594Motor · faultyALT FLAP SYS FAILED INBOARD CHECK. IND STOPPED HALFWAY BETWEEN 0 AND 1, LEADING EDGE AND TRAILING EDGE DISAGREE. REMOVED AND REPLACED INBOARD SLAT ELECTRIC MOTOR AND TRAILING EDGE FLAP ALTERNATE ELECTRIC MOTOR PER MM. ALT SLAT OPS CHECK GOOD PER MM AND TRAISDR UHLA2010042100042Actuator · malfunctionedFLAP FAIL MESSAGE ON FINAL APPROACH INTO YHZ WHEN FLAPS WERE SELECTED 3. CANCELLED APPROACH AND RAN QRH. MESSAGE DISAPPEARED WHEN FLAPS RETRACTED. ON NEXT APPROACH MESSAGE RETURNED WHEN FLAPS BROUGHT FROM 1 TO 2. RAN QRH AND WHEN LEVER BROUGHT BACK TO 1 MESDR NSVA201065Actuator · faultyTHE HYDRAULIC SYSTEM MALFUNCTIONED. CREW DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY. AIRCRAFT TUG TO THE GATE (DUTY OFFICER HAS NOTIFIED THE FAA). ACFT TROUBLESHOT TO BACK FLAP ACTUATOR.SDR UALA2010032200934Actuator · faultedFLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER EC AM SCREEN, - F-CTL. REMOVED RT WING NR 1 FLAP ACTUATOR, INSTALLED NR 1 RT WING FLAP ACTUATOR (PN 791C0000-02, SN (N985). NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. INSTALLED CORRECT LENGTH BOLTS. INSTALLED NSDR UALA2010032200929Actuator · faultyREPLACE RIGHT WING NR 3 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. INSTALLED NR 3 RT WING FLAP ACTUATOR PER MM. NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. TEMPORARILY INSTALLED WITH SHORTER BOLTS, WILL NEED CORRECT LENGTH BOLTS. ON AOG T1408 & S1381. ISDR UALA2010032200926Actuator · faultyREPLACE RIGHT WING NR 4 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. REPLACED RIGHT WING NR 4 FLAP TRACK ACTUATOR.SDR UALA2010031900923Actuator · malfunctionedREPLACE RIGHT WING NR 3 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS PER CH8644. INSTALLED NR 3 RT WING FLAP ACTUATOR PER MM. INSTALLED BOLTS AND COMPLETED INSTALLATION AND ADJUSTMENT OF NR 3 RT FLAP ACTUATOR.SDR UALA2010031900914Bolt · wrong partREPLACE RIGHT WING NR 1 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. REMOVED RIGHT WING NR 1 FLAP ACTUATOR. INSTALLED 1 RT WING FLAP ACTUATOR. INSTALLED CORRECT LENGTH BOLTS.SDR SWAA101640Motor · faultyON APPROACH TRAILING EDGE FLAPS FAILED TO EXTEND. L/E EXTENDED USING ALT FLAPS SWITCH. ALT FLAP DRIVE TRAILING EDGE AC/C CB TRIPPED LANDED WITH L/E FLAPS ONLY. REMOVED AND REPLACED FLAP HYDRAULIC MOTOR PER MM.SDR FDEA201003090707Actuator · failedAFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 2, DEG TO FLAPS 0 AMBER LE FLAP LIGHT REMAINED ILLUMINATED. COMPLIED WITH STABILIZER AND IDENTIFIED NR3 SLAT STILL DEPLOYED. EXECUTED RED TABS BUT UNABLE TO ATTAIN CLEAN ACFT CONFIG NR 3 SLAT. REMAINED DEPLOYESDR C2XA10CL014Pdu · faultyCLE FLT 5737 - THE CREW REPORTED A FLAP FAIL AT 9 DEGREES MESSAGE ON THE EICAS. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLAP POWER DRIVE UNIT. OPERATIONAL CHECKS WERE GOOD.SDR CA100122006Sleeve · cracked(CAN) DURING THE COMPLETION OF SB45-27-40 IT WAS DETERMINED THAT NR 3 (RT INBD) FLAP ACTUATOR BALLSCREW SLEEVE WAS CRACKED APPROX 0.250 INCHES LONG, CTR OF THE SLEEVE. REMAINING FLAP ACTUATORS (POSITIONS 1, 2, AND 4) WERE FOUND TO BE SERVICEABLE AT TIME OF INSDR AALA20100112LAX01Actuator · malfunctionedLAX - CAPTAIN REPORTED ON APPROACH TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INBOARD AND OUTBOARD ACTUATORS THAT HAD TRIPPED. SYSTEM GROUND CHECKED NORSDR FDEA200912244513Actuator · failedON FLAP RETRACTION FROM 5 TO 2 DEGREE THE NR 5 SLAT WOULD NOT RETRACT. THE OTBD AND INBD FLAP NEEDLES TRAVEL FURTHER INTO THE WHITE BAND WHEN OPS TESTED ON THE GROUND. AIRPLANE FLEW WITH NO SIGNIFICANT ROLL. REPLACED NR 5 SLAT ACTUATOR REF AMM 27-81-032-4. SDR MASA2009122200358Pdu · malfunctionedASH 2916 PHX-COS. CAPT DECLARED AN EMERGENCY AND DIVERTED TO DEN WHEN THE FLAPS FAILED AT 0 DEGREES WITH DETENT SELECTED AT 8 DEGREES ON APPROACH. RESET FLAP SYSTEM AND MX REMOVED AND REPLACED PDU.SDR CHQA200900263ATransmission · failedAFTER TAKEOFF THE CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. RAN THROUGH THE APPROPRIATE CHECK LISTS AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR MESSAGES AND FOUND A RT TRANSMISSION FAIL CMC. THE RIGHT FLAP TRANSMISSIONSDR REXA200900140Pdu · failedFLAPS FAIL AT O DEGREES IN FLIGHT. NORMAL TOUCH DOWN ON LANDING. REMOVED AND REPLACED FLAP PDU IAW AMM 27-52-01, FLAPS OP CHECK GOOD IAW AMM 27-51-00.SDR REXA200900132Shaft · out of limitsFLAP FAIL CAUTION MSG ON APPROACH, EXTENSION AT 0, 200KTS 2430, -13C. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARA, (H) (6) (I), PER AMOC DATED MAR 27, 09 AND PA AD27-052F. FOUND LT WING FLAP FLEX SHAFT TO BE OUT OF TORQUE LIMISDR TRBA2009123Actuator · failedFLAP UNLOCK ON FINAL APPROACH AT 1200 FT EMERGENCY DECLARED. REMOVED AND REPLACED LT AND RT OTBD FLAP ACTUATORS IAW JIC NR 27-54-72-RAI-10000. ALSO REMOVED AND REPLACED FLAP VALVE BLOCK IAW JIC NR 27-54-71-RAI-1000. PERFORMED OPT CHECK, FOUND GOOD AND NO LEAKSDR CA091214006Actuator · malfunctioned(CAN) ON APPROACH TO MSP, THE FLAP FAIL CAUTION MESSAGE WAS DISPLAYED ON EICAS WHEN THE FLAPS WERE SELECTED FROM ZERO TO 8 DEGREES. THE FLAPS FAILED AT ZERO DEGREES AND AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. THE LT AND RT FLAP FLEX DRIVES WERE CLEANSDR DL76L091957Actuator · malfunctionedDURING TAXI OUT MX IN PROGRESS, T/S PERFORMED - RAIL LOCKOUT ACT/ FSEU FAULT ON SAM. PSEU SHOW TARGET 294. FSEU SHOW FLAP POS TRANSMITTER 8 MSG 27-51014. F/S ELEC INTERMITTENT. RESET FAULTS. RETRACT AND EXTEND FLAP/SLAT SEVERAL TIMES. NO FAULTS NOTED. OPS NOSDR UHLA2009120600116Actuator · failedFLAPS FAILED IN POSITION 2 AFTER TAKEOFF. DECLARED AN EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FLAP ACTUATOR IAW EMB 170 MM 27-51-01. OPS CHECK GOOD.SDR UALA2009120703756Actuator · faultyAFTER A FLAPS 5 TAKEOFF, THE FLAPS AND L-E DEVICES RETRACTED NORMALLY TO THE 1 DEGREE POSITION, BUT WHEN 0 FLAPS SELECTED, T-E FLAPS AND L-E DEVICES LOCKED OUT WITH NEEDLE STUCK AT A POSITION HALFWAY BETWEEN 1 AND O. ALSO GOT LE SLAT DISAGREE EICAS MESSAGE. ALSDR TRBA2009116Actuator · failedDURING APPROACH TO NAS FLAP EXT FLAG APPEARED INTERMITTENTLY, WENT AWAY AND BEFORE LANDING ON APPROACH, RECEIVED FLAP UNLK WARNING ON APPROACH. DECLARED EMERGENCY, WENT AROUND, PERFOMED AOM VOL 1 PROCEDURES AND MADE "0" FLAP LANDING. REMOVED AND INSTALLED LT SDR CA091126003Actuator · malfunctioned(CAN) DURING THE APPROACH, THE FLIGHT HAD A FLAPS FAILED MESSAGE. THE CREW EXECUTED A GO-AROUND, DECLARED AN EMERGENCY AND LANDED NORMALLY WITH THE FLAPS IN POSITION 1 (TC NR 20091126003)SDR YENA20091121161Actuator · failedFLT JB350 - DECLARED AN EMERGENCY FOR FLIGHT CONTROL FLAPS FAILURE FAULT. LANDED WITHOUT INCIDENT. MX TROUBLESHOT PER TSM 27-51-00-810-810 OPERATIONAL TEST OF FLAP SYSTEM AND FOUND NO FAULTS NOTED. FOUND LEFT WING FLAP ACTUATOR ASSY NR 1 TORQUE LIMITER TRIPSDR C8GA20090296Motor · leakingDURING CLIMB OPERATION PASSING THROUGH 9000 FT A COMPLETE "A" HYD SYS FLUID LOSS WAS ENCOUNTER. AN EMERGENCY WAS DECLARED, APPROPRIATE CHECKLIST PERFORMED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, NOSDR CA091116005Actuator · failed(CAN) FLT CREW REPORTED FLAP SLAT FAILURE INBOUND. FLAPS 2, SLATS 0 NO EMERGENCY DECLARED. MX RT SLAT ACTUATOR REPLACED.SDR CA091113009Actuator · failed(CAN) EICAS FLAP FAIL CAUTION MESSAGE APPEARED ON APPROACH INTO WHEN FLAPS SELECTED FROM 0 TO 8 DEGREES. AIRSPEED WAS 200 KNOTS AND OAT WAS 3 DEGREES C.MDC FAULT CODES WERE RETRIEVED AND INDICATED JAM,RIGHT BPSU, AND WIRING. JAZZ TECH OPS DEPARTMENT INITIATE SDR FDEA200911093915Actuator · damagedDURING WALK AROUND, FOUND LT OTBD FLAP INBD ACT BROKEN. INSPECTED FLAP FOR ANY PULLED RIVETS AND NONE FOUND. INSPECTED OTBD FLAP ACT"S ATTACKING POINTS TO MAKE SURE NO OTHER DAMAGE TO FLAPS, NONE FOUND. INSPECTED ALL OTHER FLAPS AND NO DAMAGE FOUND IAW AMM-SDR USAA2009111093073Actuator · malfunctionedFLT 938 CLT - LGA - DIVERSION - ON APPROACH TO LGA, CREW RECEIVED A FLAPS LOCKED FLAPS 0 / SLAT 2 ALIGNMENT FAULT ON ECAM. COMPLIED WITH ECAM AND QRH - DIVERTED TO EWR. MAINTENANCE DRAINED AND FILLED FLAP ACTUATOR ASSEMBLIES AND BITE TESTED SFCC 1 & 2 WITH NSDR GN0A11072009Actuator · failedFLIGHT NUMBER 1070 LEG 3 KAFW-KJQF. AFTER TAKEOFF WHEN FLAPS WERE SELECTED UP, THE INBOARD FLAPS REMAINED AT 15 DEGREE WHILE THE NACELLE AND OUTBOARD FLAPS RETRACTED TO 0 DEGREES. CREW RECEIVED A FLAP "DISAGREEMENT" WARNING. ATC WAS NOTIFIED AND AIRCRAFT TUSDR CA091206001Actuator · jammed(CAN) ONE FLAP ACTUATOR WAS JAMMED DURING APPROACH, ACFT WAS LANDED SAFELY. ACTUATOR REPLACED IAW AMM.SDR CHQA200900225Drive Unit · failedWHILE ON APPROACH TO IAH THE CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS WITH THE FLAPS STUCK AT 7 DEGREES. THE APPROACH WAS ABORTED AND THE CREW RAN THE APPROPRIATE CHECKLISTS AND PERFORMED ANOTHER APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TSDR WRLA20091023258Bushing · wornFOUND LT WING OUTBOARD FLAP INBOARD AFT HINGE LWR BUSHING WORN. REMOVED LT OUTBOARD FLAP INBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED LT OUTBOARD FLAP OUTBOARD AFT HINGE REF EGAT NRC U01042 JOB CARD ATTACHING SHEET 074962 & 070606. INSTALLED SDR WRLA20091023257Bushing · wornFOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR CONNECTION BUSHING WORN. REMOVED RT OUTBOARD FLAP OUTBOARD AFT HINGE IAW AMM 20-50-02-900-801 REV 65. REPAIRED OUTBOARD FLAP OUTBOARD AFT HINGE REF EGAT NRC U01038 JOB CARD ATTACHING SHEET 074960 & 07496SDR UALA2009102003265Gearbox · wornRIGHT T/E FLAP ANGLE TEE GEARBOX RATTLES AND CHATTERS THROUGHOUT RIGHT SIDE, UNABLE TO LOCATE SOURCE OF PROBLEM, LEFT SIDE IS SMOOTH AND QUIET, HYD POWER OR ELECTRIC MAKES NO DIFFERENCE, BUT SOUND IS MUCH LOUDER WITH ELECTRIC MOTOR. SUSPECT WORN OUTPUT GEAR OSDR CA091019007Actuator · failed(CAN) FLAPS FAILED AT ZERO DEGREES (WHEN SELECTED TO 8 DEGREES) ON APPROACH. AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. ALL FLAP ACTUATORS WERE REPLACED AND THE SYS FUNCTION CHECKED. PN OF THE REMOVED ACTUATORS ARE: LT1, 852D100-23, LT 2, 852D100-25, LSDR UALA2009101203211Pdu · malfunctionedUNABLE TO DROP TRAILING EDGE FLAP ELEC. REMOVED TRAILING EDGE POWER DRIVE UNIT. INSTALLED NEW ALT FLAP DRIVE MOTOR. ACCOMPLISHED FUNCTIONAL TEST WITH NO PROBLEMS.SDR UHLA2009101100068Actuator · failedDURING APPROACH SELECTED FLAPS 1 AND RECEIVED `FLAP FAIL` EICAS MESSAGE. RAN QRH FOR NO FLAPS AND SLATS 3. DECLARED EMERGENCY. LANDED WITH 0 FLAPS. MAINTENANCE RELEASED ELECTRONIC BRAKE, CLEARED INHIBITS, AND OPS CHECKED GOOD. SI275042 WAS COMPLIED WITH 10SDR AALA20090929ORD01Actuator · leakingSHORTLY AFTER TAKEOFF, LOST RIGHT HYDRAULIC SYSTEM QUANTITY. RETURNED ORD, LANDED UNEVENTFULLY AND TAXIED TO GATE UNDER OWN POWER. UNDER INITIAL EXAMINATION BY GATE MECHANICS, FOUND FLUID LEAK IN AREA OF LEFT FLAPERON. FOUND LEFT OUTBOARD FLAPERON ACTUATOR SDR SIMA200925301Drive Unit · malfunctionedON FLIGHT 3962 DURING CRUISE A FLAP FAIL MESSAGE APPEARED AND REMAINED ON EICAS. THE FLAPS FAILED AT 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. THE AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSARY FOSDR CHQA200900168Flex Drive · shearedFLIGHT 5512, SDF TO CLE. ON FINAL APPROACH INTO CLE THE CREW CONFIGURED THE FLAPS FROM 20 DEGREES TO 30 DEGREES. UPON SELECTION THE CREW RECEIVED A FLAP FAIL MSG. THE FLIGHT CONTROL STATUS PAGE INDICATED 28 DEGREES ON THE LEFT FLAP AND 27 DEGREES ON THE RIG
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