JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap Control System, 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 = '2750' 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 = '2750' 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 SWIA200312566Lever · malfunctionedFLAPS FAIL MESSAGE CAME ON AFTER TAKEOFF WHEN SELECTING FLAPS 0 TO FLAPS 8. RETURNED TO SLC. REPLACED FLAP CONTROL HANDLE IAW 27-51-01. OPS CHECK GOOD.SDR ASOA03553Control Unit · malfunctionedDURING CLIMB-OUT, WHEN FLAPS WERE SELECTED TO ZERO DEGREES, THEY STAYED AT EIGHT DEGREES AND THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW LEVELED OFF THE AIRCRAFT AND MAINTAINED A SPEED OF 200 KNOTS WHILE COMPLYING WITH THE QRH. UPON NOTIFYING THSDR SWIA200312571Actuator · malfunctionedAFTER LANDING, BOTH NACELLE FLAPS WERE SLOW TO RETRACT, CAUSING DISAGREEMENT. NACELLE FLAPS EVENTUALLY RETRACTED ON THEIR OWN. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECKS GOOD. PN: 343100-1001, SN ON: 0228,SDR SIMA200330202Fcu · failedDURING FLIGHT CREW REPORTED A FLAPS FAIL MESSAGE ON EICAS AND FLAPS STUCK IN THE FIVE DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SWIA200312586Control Unit · malfunctionedAFTER LANDING NAC FLAPS CONTROL FAULTED AND WOULD NOT RESET. REMOVED FLAP COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. P/N: 307500-1007, S/N OFF: 169.SDR ASOA03536Pdu · failedFLT 4600 - DURING APPROACH INTO YOW FROM ATL, THE CREW SELECTED THE FLAPS TO TWENTY DEGREES AND AT ELEVEN DEGREES RECEIVED A FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT ELEVEN DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. SDR AALA20031168Control Unit · inoperativeON APPROACH TO DFW FLAPS FAILED TO DEPLOY HYDRAULICALLY. CREW ACCOMPLISHED NO FLAP LANDING WITHOUT INCIDENT. REPLACED FLAP/SLAT ELECTRIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR CA031030004Torque Tube · grooved(CAN) DURING MAINTENANCE IT WAS DISCOVERED THAT THE R/H WING FLAP PRIMARY TORQUE TUBE AT APPROX. WING STN YW 325.00 WAS DEEPLY GROOVED. GROOVE WAS AT ABOUT THE MIDLENGTH OF THE TUBE AROUND ITS CIRCUMFERENCE. TUBE HAD BEEN WEARING ON A NEARBY ELECTRICAL BUNDLE SDR 03FDEA01792Flap · out of rigUPON TAKEOFF WHILE RETRACTING THE FLAPS FROM 5 DEGREES TO 2, BOTH FLAP INDICATIONS STUCK BETWEEN 5 AND 2 AND INTRANSIT LIGHT SHOWED AMBER, THE S/O'S VERIFICATION PANEL SHOWED ALL LED'S DOWN. AFTER APPROX 5 MIN THE LED'S RANDOMLY SEQUENCED TO 2, 3, 6, 7 AND SDR SWIA200312535Bpsu · malfunctionedFLAPS FAIL MESSAGE ON CLIMBOUT. CONTINUED TO SLC. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. OPS CHECK GOOD.SDR A6WA200340148Flap · misriggedFLAP FAIL CAS MESSAGE AT ZERO FLAPS ON CLIMB, DECLARED EMERGENCY. RE-RIGGED, FLAPS. (M)SDR 2003F00601Control Unit · malfunctionedDURING APPROACH SELECTED FLAPS 20 DEGREES. STOPPED AT 15 DEGREES. PERFORMED ABNORMAL/EMERGENCY CHECKLIST WITH A NORMAL LANDING. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM 3 TIMES AND ALL CHECKS GOOD IAW B757 MM 27-51-00. (M)SDR AUS20031143Control Cable · frayed(AUS) LT AND RT FLAP DOWN CABLES PN 1460100-7 AND PN 1460100-8 FRAYED WITH BROKEN STRANDS AROUND BELLCRANK ACTUATOR.SDR COMA0360462Flap · malfunctionedFLIGHT 5248 FLAPS FAIL WARNING WHEN SELECTED TO 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR SWIA200312522Pdu · malfunctionedFLAPS HALFSPEED MESSAGE. REMOVED AND REPLACED THE PDU IAW MM 27-52-05. OPS CHECK GOOD.SDR ARWA20031001Link · brokenON APPROACH, WHEN SELECTING FLAPS 23 DEGREES AIRCRAFT ROLLED TO THE LEFT WITH SPLIT FLAP INDICATION, ON POST FLIGHT FOUND RT INBOARD FLAP BRACKET BROKEN. RECORD FOR 27-268. REMOVED AND REPLACED RT INBOARD FLAP IAW MM 27-51-4. OPERATIONAL CHECK NORMAL IAW 27SDR SWIA200312519Brake · malfunctionedAFTER TAKEOFF WHEN THE FLAPS WERE SELECTED UP, GOT THE FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED RIGHT MOTOR BRAKE UNIT ON FLAP PDU. SYSTEM OPS CHECKS GOOD IAW 27-52-05.SDR 55177AMWAControl Unit · failedAFTER TAKE OFF CREW TRIED TO RETRACT THE FLAPS. THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS.SDR SWIA200312491Pdu · malfunctionedFLAPS HALF SPEED STATUS MESSAGE ILLUMINATED. REPLACED FLAP PDU WITH SERVICEABLE UNIT IAW CRJ MM 27-52-01. OPS CHECK NORMAL. S/N OFF: 109.SDR SWIA200312498Selector · malfunctionedFLAP CONTROL FAULT AND ADVANCED SWS DURING TAXI OUT. RESET ONCE, REPEATED FAULT WHEN SELECTED TO 15 DEGREES. REPLACED FLAP SELECTOR SWITCH. OPS CK GOOD.SDR SWIA200312494Selector · malfunctionedDURING DESCENT INTO IAH THERE WERE NUMEROUS CONTROL FAULT ON OVERHEAD WITH FLAP AND ADVANCED SWS ON MAP THAT APPEARED FOR A COUPLE SECONDS THEN CLEARED ITSELF. REMOVED AND REPLACED FLAP CONTROL LEVER PER MM 27-00-00. OPS CHECKS GOOD.SDR CA031006002Control Cable · frayed(CAN) RT FLAP CABLE FRAYED AT WING ROOT PULLEY AT FLAP FULL DOWN POSITION.SDR BAQA089805Motor · intermittentUNIT ONLY LASTED 2.6 HOURS. MOTOR IS INTERMITTENT. WILL RUN IF AND WHEN IT WANTS TO. WE DO NOT NEED ANOTHER UNIT.SDR COMA0360445Controller · failedFLIGHT 5821 FLAPS FAILED AT 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR BAQA089500Motor · overheatedMOTOR OVERHEATED. REPLACED WITH SERVICEABLE UNIT.SDR BAQA089501Gearbox · malfunctionedGEARBOX BINDING. REPLACED WITH SERVICEABLE UNIT.SDR ASOA03476Control Unit · inoperativeDURING APPROACH INTO DFW FROM HSV, TEH CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WHEN SELECTING THE FLAPS TO 30 DEGREES FOR LANDING. QRH PROCEDURES WERE COMPLIED WITH AND A NORMAL LANDING ACHIEVED WITH FLAPS SELECTED AT 20 DEGREES. EMERGENCY VEHICLES WERE RSDR CA031014005Control Rod · cracked(CAN) DURING ROUTINE INSPECTION THE FLAP CONTROL ROD (TUNING FORK) WAS FOUND TO HAVE A .70 INCH CRACK RUNNING LENGTHWISE FROM THE THREADED END OF THE ROD.SDR CA040127003Control Arm · cracked(CAN) THIS LT FLAP COANTROL ARM WAS FOUND CRACKED DURING AN INSPECTION. THE CRACK WAS 188 MM/0.7 INCH RUNNING LENGTHWISE FROM THE THREADED END OF THE ROD ENDING AT THE INSPECTION HOLE. THIS PART WAS REPLACED WITH A NEW UNIT.SDR AUS20031045Torque Tube · worn(AUS) FLAP TORQUE TUBE WORN BEYOND LIMITS. FOUND DURING INSPECTION IAWAD/PA23/89.SDR AUS20031044Bellcrank · corroded(AUS) FLAP BELLCRANK CORRODED. FOUND DURING INSPECTION IAW AD/PA23/50.SDR SWIA200312470Bpsu · out of rigFLAP CAUTION MESSAGE ENROUTE. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. OPS CHECK GOOD.SDR SWIA200312467Selector · malfunctionedON SHORT FINAL FLAP ASYMMETRY LEFT OUTBOARD 25 DEGREES, RIGHT OUTBOARD 15 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER AND FLAP CONTROL UNIT. OPS CHECK GOOD ON GROUND. S/N OFF: 120197SDR COMA0360434Warning Light · illuminatedFLT 5275 FLAPS FAIL CAUTION MESSAGE WHEN SELECTED TO 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR COMA0360436Control Unit · unreliableFLAPS FAIL MESSAGE WHEN TRANSFERRING POWER TO NR 2 GENERATOR. REPLACED THE FECU.SDR COMA0360430Warning Light · illuminatedFLIGHT 5836 DURING DECENT INTO YUL RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3,(A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.SDR CA031001010Control Cable · damaged(CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE PN 14601007 AND 14601008 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT SERVISDR CA031001009Control Cable · damaged(CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE P/N 1460 100-7 AND 1460100-8 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT. SDR CA030925003Control Rod · cracked(CAN) WHILE CARRYING OUT A PHASE INSPECTION, THE CONTROL COLUMN CONNECTING TUBE WAS FOUND CRACKED. THE CRACK WAS LOCATED AT ONE OF THE ATTACHMENT BOLT HOLES TO THE KNUCKLE FITTING. THE CRACK EMANATED FROM THE BOLT HOLE CLOSEST TO THE END OF THE TUBE, TO THE SDR SWIA200312436Fcu · malfunctionedFLAP CONTROL FAULT INDICATION OCCURED WHEN GOING FROM 25 TO 45 DEGREE FLAP COULD NOT RESET. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR COMA0360420Warning Light · illuminatedDURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES.SDR SWIA200312448Pdu · malfunctionedAFTER FLAPS REACHED 45 DEGREES WE RECEIVED A FLAPS FAIL MESSAGE.REMOVED AND REPLACED FLAP PDU OPS CHECK GOOD IAW CRJ MM 27-52-01.P/N 865D100-7 S/N OFF 0831 S/N ON 0706.SDR SWIA200312446Ecu · malfunctioned''FLAPS FAIL'' CAUTION DURING CRUISE FLIGHT. NO FLAP LANDING IAW QRH. REMOVED AND REPLACED FECU IAW CL 600 MM 27-51-05. OPS CHECKS GOOD.SDR SWIA200312439Fcu · malfunctionedUPON FLAP RETRACTION AFTER TAKEOFF, FLAPS HAD DISAGREEMENT. IB WOULD NOT RETRACT INITIALLY. AFTER APPROXIMATELY 1 MIN, IB FLAPS RETRACTED. AFTER LANDING, FLAPS WOULD NOT RETRACT BEYOND 5-10 DEGREES WITH DISAGREEMENT ALL FLAPS. REMOVED AND REPLACED FCU IASDR C1HA200395070Power Unit · failedDURING FLAP RETRACTION INBOARD TRAILING EDGE FLAPS STAYED AT 5 DEG OUTBOARDS WENT TO 2 DEG RAN SPLIT FLAP PROCEDURE AND FLAPS WOULD RETRACT FROM 5 DEG WITH ALTERNATE FLAPS. AS PER CHECK LIST. RETURNED TO HRL. FOUND ROLLER ON LT IB FLAP CARRIAGE OB TRUCK IB DEASDR SWIA200312428Annunciator · malfunctionedFLAP'S FAULT COULD NOT BE CLEARED (IT WOULDN'T GO TO ''M'' MODE). REPLACED FLAP ANNUNICIATOR. OPS CHECK GOOD.SDR MD001Drive System · damagedUPON APPROACH TO SUA A SPLIT FLAP CONDITION WAS REPORTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. SUBSEQUENT INVESTIGATION REVEALED A SEPARATION OF THE SWAGED END FITTING TO THE FLAP ACTUATOR CAUSING A BIND IN THE LEFT FLAP SYSTEM. P/N 12325Y116 FLAP DRIVE CABSDR C1HA200395068Jackscrew · lack of lubeDURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD FLAPS RETRACTED TO 2 DEGREE POSITION WHILE INBOARDS REMAINED AT 5 DEGREE POSITION. RAN SPLIT FLAP EMERGENCY PROCEDURE INBOARDS REMAINED AT 5 WITH ALTERNATE FLAPS. RETURNED TO ELP, VERIFIED INBOARD FLAPS LOCKED OUSDR SWIA200312425Control Unit · malfunctionedAFTER TAKEOFF PHX, FLAPS FAIL CAUTION MSG. 0 DEGREES FLAP LANDING SLC IAW QRH. REMOVED AND REPLACED FECU IAW MM 27-50-00. OPS CHECK GOOD.SDR COMA0360411Warning Light · illuminatedFLIGHT 5530 FLAPS FAIL MESSAGE DURING TAXI. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
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