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 CA000719025Actuator · cracked(CAN) PART NUMBER FOR TIME X CONDITION. CENTRE SHAFT LONGITUDINAL CRACKED. CRACK DISCOVERED AFTER REMOVAL.SDR RRXA002788Actuator · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING FLAP ACTUATOR CRANK (KNUCKLE) AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW MM 27-51-9.SDR CA000726004Drive Shaft · worn(CAN) INITY MAINT NOTIFIED THAT WHEN SELECTING FLAPS TO UP POS (ON GROUND) THAT FLAP IND. SHOWING 20 DEGS&THAT FLAPS WERE NOT ABLE TO RETRACT ANY FURTHER. MAINT FOUND L/H INBOARD FLAP IN APPROX. 25DEGS DOWN POS,&THAT FLAP SPLIT SYS PREVENTING FURTHER FLAP-MOTSDR 20000720SH021Actuator · shearedSTANDBY FLAP MOTOR INOPERATIVE. ACTUATOR SHAFT ROLL PIN SHEARED. JACKSCREW CONTAMINATED WITH METAL PARTICLES, MOTOR INOPERATIVE. UPON REPLACEMENT OF TRANSMISSION ASSY, ALSO DISCOVERED ELECTRICAL PIN IN PRIMARY FLAP MOTOR POWER CONNECTOR PARTIALLY DISENGAGED SDR SCNA00056Motor · leakingDURING CRUISE FLIGHT THE A-SYSTEM LOST ALL FLUID, THE FLIGHT CREW EXECUTED EMERGENCY CHECK LIST PROCEDURES. PERFORMED MANUAL FLAP AND GEAR EXTENSION AND LANDED. REMOVED AND REPLACED THE FLAP POWER UNIT HYDRAULIC MOTOR IAW B727 MM CH 275162, OPERATIONAL AND LSDR CA000606027Actuator · worn(CAN) ON INSPECTION OF BACKLASH CHECK UNITS WORN BEYOND LIMITS ON THREE OUT OF FOUR ACTUATORS. THEY ALL HAVE THE SAME CYCLES AND HOURS ON THE UNITS.SDR AU000436Bracket · failed(AUS) STANDBY FLAP MOTOR SUPPORT BRACKETS PN 2611144-6 AND PN 2611144-7 FAILED.SDR ASOA00061Actuator · inoperativeFLT 4639 - CREW SELECTED FLAPS TO 8 DEGREES AND FLAPS FAIL MESSAGE APPEARED ON EICAS. CREW FOLLOWED PROCEDURES AS LAID OUT IN ABNORMAL SECTION OF QRH PAGE 8-8. CREW INFORMED ATC OF SITUATION, DECLARED AN EMERGENCY, AND REQUESTED EMERGENCY VEHICLES BE STANDINSDR DHL200080502Actuator · failedAIRCRAFT OSCILATING AROUND VERT AXIS DURING FLT, BEGAN DURING ACCELERATION ACCOMPANIED BY LOUD NOISE (WIND). FOUND RIGHT I/B FLAP ACTUATOR BROKEN. REMOVED AND REPLACED FLAP ACTUATOR PER DC-8 M/M 27-51-10. LEAK CHECK AND OPS CHECK OK PER M/M 27-51-10.SDR AU000454Fitting · cracked(AUS) OUTBOARD RT AFT TRAILING EDGE FLAP DRIVE MECHANISM OUTBOARD FITTING CRACKED AND BOLT BADLY CORRODED. BOLT HEAD MISSING ANDBOLT PROTRUDING.SDR CA000516010Actuator · worn(CAN) DURING SCHEDULED INSPECTION OF THE FLAP ACTUATORS, THREE OUT OF FOUR ACTUATORS WERE FOUND WORN BEYOND SERVICE LIMITS.SDR COMA0060410Actuator · wornFOUND LEFT OUTBOARD FLAP, INBOARD ACTUATOR HAD PLAY AT FORWARD BUSHING MOUNT. REMOVED AND REPLACED ACTUATOR WITH A SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE.SDR COMA0060409Actuator · wornFOUND RIGHT OUTBOARD FLAP, INBOARD ACTUATOR HAS EXCESSIVE PLAY AT AFT END. REMOVED AND REPLACED ACTUATOR WITH A SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE.SDR CA000511033Actuator · failed(CAN) FLAPS FAIL AT 17 DEG. FLAP ACTUATOR REPLACEDSDR CA000530068Actuator · failed(CAN) FLAP FAIL MESSAGE ON EICAS WHEN FLAP SELECTED TO 45 DEG AT 155 KNOTS. VISUAL CHECK CARRIED OUT AND FLAPS RESET. FLAPS CYCLED. REPLACED LT BPSU AND NR 3 ACTUATOR. COMPLETE RIGGING AND FUNCTIONAL CHECK CARRIED OUT.SDR CA000505028Actuator · failed(CAN) DURING FINAL APPROACH A/C HAD FLAP FAIL AT 17 DEGREES. RT O/B FLAP FOUND TWISTED. FLAP PANEL AND BOTH ACTUATORS REPLACED.SDR COMA0060396Actuator · seizedFLAPS FAILED AT 17 DEGREES ON APPROACH. FERRIED AIRCRAFT TO CVG WHERE RIGHT OUTBOARD FLAP AND ACTUATORS WERE REPLACED.SDR C2XA00IA108Actuator · gougedIAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD FLAP OUTBOARD ACTUATOR WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ACTUATOR IAW EMB145 MM 27-51-00, AND THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR AU000386Gear · stripped(AUS) TRAILING EDGE FLAP DRIVE GEARBOX INPUT GEAR STRIPPED.SDR COMA0060346Actuator · jammedFLAPS FAIL MESSAGE. REPLACED THE NR 3 FLAP ACTUATOR.SDR CA000516008Gear · worn(CAN) DURING SCHEDULED INSPECTION, THE FLAP ACTUATOR WAS FOUND WORN BEYOND SERVICE LIMITS.SDR CA000414015Actuator · seized(CAN) ON APPROACH, THE FLAP MOTOR CIRCUIT BREAKER TRIPPED WHEN THE FLAPS WERE SELECTED DOWN, THE CIRCUIT BREAKER WAS RESET AND THE WHEN THE FLAPS WERE SELECTED UP IT TRIPPED AGAIN. THE AIRCRAFT RETURNED TO BASE WITH THE FLAPS IN A PARTIAL DOWN POSITION. MAINTESDR CA000414001Actuator · unapproved part(CAN) WHILE PERFORMING ROUTINE MAINTENANCE AND CERTIFICATION OF TWO FLAP ACTUATORS AT THE REQUEST OF A CLIENT, THE AMO DISCOVERED THAT THE PARTS SUPPLIED FOR REPAIR HAD BEEN INVOLVED IN AN AIRCRAFT ACCIDENT. THIS DISCOVERY WAS DISCOVERED AFTER THE PARTS HAD BESDR SWIA971761Connector · failedCONTROL FAULT INFLIGHT WOULD NOT RESET. RETURNED TO SLC RAN FLAPS ON GROUND FAILED ON RIGHT OUTBOARD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG PER MM 27-51-00 AND 50-50-00, OPS CHECKS GOOD. (P/N MS3476612201) ON.SDR AU001260Jackscrew · faulty(AUS) RT OUTBOARD FLAP JACKSCREW SUSPECT FAULTY. INVESTIGATION COULD NOT CONFIRM THE DEFECT ALTHOUGH THE JACKSCREW WAS NOTCHY IN OPERATION.SDR RAIA0004005Actuator · failed7092-STL- WITH FLAPS SELECTED TO 10 DEGREES, FLAPS DROOP TO 15 DEGREES THEN CYCLE BETWEEN 10 AND 15 DEGREES. MAINTENANCE REPLACED FLAP ACTUATOR.SDR COMA0060296Actuator · seizedFLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND FLAP OUTBOARD ACTUATOR.SDR COMA0010042Actuator · failedFLAP ANNUNCIATOR CONTROL FAULT APPEARED ON TAKEOFF ROLL. REMOVED LEFT INBOARD FLAP ACTUATOR AND INSTALLED A SERVICEABLE ONE.SDR COMA0010041Actuator · leakingFOUND RIGHT INBOARD FLAP ACTUATOR LEAKING. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE.SDR COMA0010046Actuator · malfunctionedFLAP CONTROL FAULT DURING T/O. REPLACED THE LEFT HAND INBOARD FLAP ACTUATOR.SDR COMA0060285Actuator · defectiveFLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND INBOARD FLAP ACTUATOR.SDR SWIA971734Actuator · failedLEFT OUTBOARD FLAP WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09 AND RII 27307, OPS AND LEAK CHECK GOOD. (P/N 3430001003) ON, (S/N 0790) (S/N 0330) OFF.SDR MYWA2000ADB00Transmission · wornFLAPS WILL NOT RETRACT FULLY DUE TO RT. MID FLAP FAIRING BEARING WORN(I/B).SDR CA000306026Actuator · failed(CAN) ON APPROACH WHEN EXTENDING THE FLAPS,THE LEFT OUTBOARD FLAP TWISTED. INBOARD END OF THE FLAP STOPPED, OUTBOARD END CONTINUED TO EXTEND. FOUND THE INBOARD ACTUATOR HAD FAILED.SDR SWIA971725Connector · dirtyFLAP DISAGREEMENT WHEN RETRACTING FLAPS FROM 15 TO 0. RETURNED TO YVR. FOUND DEICE FLUID IN OUTBOARD FLAP ACTUATOR CANNON PLUGS. CLEANED CANNON PLUGS, OPERATED FLAPS SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED.SDR 20000412SH005Valve · looseFLAP ACTUATION SLUGGISH WITH ENGINE RUNNING. WOULD NOT OPERATE USING AUXILIARY SYSTEM. FOUND FLAP SELECTOR VALVE INTERNAL SPOOL ACCESS CAP HAD NEVER BEEN SAFETIED (NO SAFETY WIRE MARKS ON UNIT) AND HAD BACKED OUT 3 TURNS. REPLACED SELECTOR VALVE (REPLACEMENSDR CA000209018Actuator · damaged(CAN) WHILE PERFORMING A SCHEDULED CHECK OF THE ACTUATOR, IT WAS FOUND TO BE BEYOND SERVICE LIMITS.SDR CA000128034Limit Switch · frozen(CAN) FROZEN FLAP LIMIT SWITCH FOUND FROZEN WHICH CAUSED THE FLAPS TO FAULT. SWITCH CLEANED AND FREED UP.SDR COMA0060084Actuator · bindingFLAPS FAILED MESSAGE. REPLACED THE LEFT WING NR 3 AND NR 4 FLAP ACTUATORS.SDR CA000128061Drive Shaft · corroded(CAN) THE PILOT FOUND THE FLAP DOWN TO 17 DEGREES BUT THEY JAMMED AT 8 DEGREES. WE FOUND THE LT INBOARD FLAP FLEX DRIVE BROKEN APPROXIMATELY 4 FROM THE END. SHAFT REPLACED.SDR AU000019Actuator · damaged(AUS) LEFT OUTBOARD FLAP ACTUATOR FAULTY DUE TO EXCESSIVE BACKLASH.SDR COMA0060016Actuator · malfunctionedFLAPS FAILED AT 37 DEGREES DURING LANDING APPROACH. REPLACED LEFT WING NR 3 FLAP ACTUATOR.SDR 2000ZZZM67Motor · leakingFLL-IND - FLT 476 - DURING CRUISE, THE 'A' HYDRAULIC SYSTEM QTY SLOWLY DECREASED, RAN AOM PROCEDURE, WAS UNABLE TO ISOLATE LEAK. LANDING GEAR WAS EXTENDED USING MANUAL PROCEDURES, LANDED AT IND WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LEFT FLAP POWER USDR COMA9960774Actuator · bindingFLAPS FAIL MESSAGE DURING APPROACH. REPLACED LEFT I/B FLAP ACTUATORS.SDR CA000128062Drive Shaft · broken(CAN) AFTER LANDING THE PILOT SELECTED THE FLAP UP AND THEY JAMMED AT 17 DEGREES. INVESTIGATION FOUND THE RT OUTBOARD FLAP FLEX DRIVE WAS BROKEN APPROXIMATELY 24 INCHES FROM THE END.DAMAGED PARTS REPLACED.SDR 99T64R491EWABellcrank · crackedFOUND DURING D-CHECK, MID WING FLAP CRANK HAS CRACK APPROX .1875 INCH IN LENGTH AT STATION 219 LEFT. REPLACED MIDWING FLAP CRANK IAW DC-8 O/H/M 27-28-8. (M)SDR 99T64R476EWABellcrank · crackedFOUND DURING D-CHECK, INBOARD FLAP ACTUATOR ASSY CRANK HAS TWO CRACKS, ONE IS .5 INCH IN LENGTH AND THE OTHER IS .375 INCH LENGTH. REPLACED CRANK IAW DC-8 O/H/M 27-28-9. (M)SDR 2000ZZZX233Switch · brokenCAM, PN 5115253-1, SLIPPED MISSING ARM ON SWITCH. COCKPIT SWITCH BROKE AND THIS WAS THE BACK-UP CAUSING FAILURE OF FLAP SYSTEM.SDR UPS99831192Actuator · leakingINSPECTION TYPE:N/A, AFTER LANDING WHEN PULLING INTO PARKING RES PRESSURE LIGHT ILLUMINATED AND THEN FLIGHT CONTROL MANUAL LIGHTS. ONLY HAD ACCUMULATOR PRESSURE TO STOP AIRCRAFT. FLAPS DID NOT RETRACT. REMOVED AND REPLACED INBOARD LT FLAP ACTUATOR, OPS CK ASDR CA991229019Bolt · broken(CAN) DURING INSP FLAPS AND AILERONS REMOVED FOR INSP. PORT INBD FLAP ACTUATOR-TO-FLAP ATTACH BOLT FOUND BROKEN, NO DAMAGE TO SURROUNDING AREA. BOLT REPLACED.
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