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 MT9A00000010Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)SDR DL76G080619Limiter · malfunctionedTE FLAP DISAGREE ON GO AROUND. A/C DECLARED EMERGENCY LANDING. TE FLAP SHUTDOWN EICAS MSG WITH FLAPS LOCKED AT 24 DEG. ON ARRIVAL AT GATE, MTC PERFORMED, BITE OF FSPM CARDSALL TEST OK, PSEU BITE IS GO. FLAP TORQUE LIMITERS WERE NOT TRIPPED. ALL T/DONE PERSDR SWAA082076Torque Tube · corrodedDURING SCHEDULED 16Y CHECK, FOUND LEFT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED AT TOGGLE SUPPORTS. REMOVED AND REPLACED FLAP PER MM.SDR DALA1121490624Gear · defectiveTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME02, ME04.SDR DALA1210380121Link · unknownLINK REPLACEMENT IAW 01-076248-12. ME07 OUTBOARD LINK REPL-OUTBOARD FLAP-LEFT P/N 113T1321-XX ME08 INBOARD LINK REPL-OUTBOARD FLAP-LEFT P/N 113T1322-XX ME09 OUTBOARD LINK REPL-INBOARD FLAP-LEFT OUTER PINS ME10 INBOARD LINK REPL-OUTBOARD FLAP RIGHT P/N 113SDR MASA200800323Flap · malfunctionedASH 7167 ORD-GSO - FLAP FAIL WHILE IN CRUISE AT FLAPS ZERO. DECLARED AN EMERGENCY AND LANDED IN GSO WITHOUT INCIDENT. MX COMPLIED WITH THE FLAP FAIL INSPECTIONS AND COMPLIED WITH PART A.SDR AALA200800964Fseu · inoperativeLAX INFLIGHT T263/15APR - CREW REPORTED FLAPS STUCK AT 17 DEGREES. LANDED LAX WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ANCF200800008Warning Light · illuminatedFLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO THE RIGHT TO CENTER COLUMN. FIM PROCEDURE 27-81-00 FIG 105 WAS ACCOMPLISHED. IN ACCORDANCE AMM 27-51-01/201 FLAP SLAT ELECTRONIC UNIT NR 1 ASDR REXA200800008Flap System · malfunctionedON APPROACH, FLAPS FAILED AT ZERO WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL ZERO FLAP LANDING. SYSTEM RESET PER FIM 27-50 AND PLACED ON SEVENTY TWO HOUR WATCH.SDR VNAA0804013Fcu · failedCREW REPORTED A FLAPS FAIL CAS MESSAGE DURING APPROACH/LANDING. THE ARFF RESPONDED AND THE ACFT TAXIED TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE FECU PER MEL 27-51-01-2. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE ACFT MAINTENSDR A6WA200840323Flap System · malfunctionedABORTED TAKEOFF DUE TO CONFIG FLAP WARNING. FLAP INDICATION SHOWED 3 DEGREES WHEN SELECTED TO 8 DEGREES. TAKEOFF ABORTED AT 60 KNOTS. BTMS INDICATED 3-3-5-3. INTERROGATED FECU PER AMM 27-50-00. NO DEFECTS NOTED. RESET FLAP SYSTEM IAW FIM PROCEDURES. OPSDR MT9A00000009Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)SDR MT9A00000008Bearing · frozenTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K)SDR MT9A00000006Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)SDR CA080415004Control Cable · frayedFLAP CENTER CABLE WAS FOUND FRAYED DURING REGULARLY SCHEDULED MAINTENANCE.SDR CA080410005Bpsu · unserviceableON DESCENT, CREW SELECTED AND RECEIVED FLAPS 8 DEGREES, WHEN THEY ATTEMPTED TO PROCEED TO FLAPS 20 CREW RECEIVED A FLAP FAIL MESSAGE. FLIGHT LANDED WITHOUT INCIDENT. FECU MESSAGE POINTED TO THE RT BPSU AS THE FAULT. THE RT BPSU WAS REPLACED, FLAP SYSTEM RIGSDR ANCF200800007Flap System · malfunctionedPILOT REPORT: EICAS MSG TE FLAP DISAGREE DISPLAYED TRAILING EDGE LIGHT ILLUMINATE WHEN ANY TE FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION. IAW FIM 27-51-00 FIG 105. FLAPS OPERATED CORRECTLY TO SELECTED POSITIONS FSEU SHOWS NO FAULTS. MESSASDR DXTA20082984Flap System · malfunctionedFLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION.SDR COMA0860210Controller · faultyFLIGHT 5163 - EN ROUTE CVG-FSD PRIOR TO APPROACH RECEIVED A FLAPS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP ELECTRONIC UNIT.SDR MT9A00000004Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)SDR DALA1140800138Link · damagedTRAILING EDGE FLAP 3-10 LINKS. REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.SDR 08FDEA01272Flap System · malfunctionedWHEN SELECTED FLAPS 15 ON APPROACH SFPI SHOWED FLAPS LIGHT AND FLAPS WOULD NOT EXTEND, RE-CYCLED FLAPS AND ON SECOND ATTEMPT FLAPS EXTENDS NORMALLY. PERFORMED WIRING CHECK HIGH SPEED SOL V/V, ENABLE V/V AND RETRACT SOL V/V ALL RESISTANCE VALUE WITHIN LIMIT. SDR CA080403002Bpsu · malfunctionedTHE POST MAINTENANCE TEST FLIGHT WAS UNSUCCESSFUL. THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE ON APPROACH WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES. THE FLAP ELECTRONIC CONTROL UNIT (FECU) CODES WERE RETRIEVED. THE RT BRAKE AND POSITION SENSOR UNIT SDR A6WA200840280Flap System · inoperativeFLAPS FAILED AT 20 DEGREES, COMPLIED WITH QRH, LANDED DCA. LANDED NORMAL, MAX BTMS READING 4 FOR ALL BRAKES. RESET PER AWAC SUPPLEMENT 98-018B. (M)SDR COMA0860200Ecu · faultyFLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED FECU. ALSO, COMPLIED WITHSDR CA080408002Control Unit · failedPRIOR TO DEPARTURE FLIGHT CREW COMPLETED A STAB TRIM RESET. SHORTLY AFTER FLAP RETRACTION ON TAKEOFF, FLIGHT CREW RECEIVED AN AP TRIM IS ND ASSOCIATED WITH AN AP PITCH TRIM ‘CAUTION MESSAGE. SUBSEQUENTLY CREW RECEIVED A ELEVATOR SPLIT’ CAUTION MESSAGE. CREWSDR COMA0860201Flap · failedFLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAISDR CA080331006Flap System · failed(CAN) FLAP FAILED ON APPROACH , LT FLAP INDICATING 3 DEG , RT INDICATING 4 DEG PARTIAL FLAP LANDING CARRIED OUT. MAINT ACTIONS : ALL 8 FLAP ACTUATORS REPLACED IAW COMPANY FLAP FAIL POLICY. (TC NR 20080331006)SDR DXTA200802968Pdu · inoperativeUPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00.SDR CALA0800272Torque Tube · corrodedNR 3 MID FLAP I/B AND O/B TORQUE TUBES CORRODED AND PITTED. REMOVED AND REPLACED WITH SERVICEABLE TORQUE TUBES I/B AND O/B REF CMM 57-53-17.SDR DXTA20082968Pdu · malfunctionedUPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00.SDR CA080328010Flap System · failed(CAN) ON APPROACH WHEN MAKING INITIAL FLAP SELECTION CREW RECEIVED FLAP FAULT MESSAGE, FLAPS FAILED TO OPERATE. CREW PERFORMED FLAP (0) LANDING. CREW ADVISE OAT WAS -57 TO -59 FOR ABOUT AN HOUR AT FLIGHT LEVEL 260 PRIOR TO COMMENCING DESCENT. ON GROUND FLAPS PSDR DXTA200802966Fseu · inoperativeLEAVING, AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 AND 27-SDR 2008UALA01726Flap System · stuckFLAP HANDLE AT 5, FLAPS LOCKED UP AT 1 EICAS, T/E FLAP DISAGREE.SDR DXTA20082966Control Unit · inoperativeLEAVING TQPF AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 ANDSDR TRAX200800472Flap · failedREPEAT FLAP SYSTEM FAILURE, FLAPS FAILED AT ZERO ON APPROACH INTO ROC ON 3/23/08, FERRIED TO ATL 3/24/08; REFER TO DEFECT 373059-3.SDR TRAX200800467Flap · failedFLAPS FAIL EICAS APPEARED WHEN SELECTING FLAPS 8 DEGREES ON APPROACH. LANDED FLAPS 0 DEGREES. EMERGENCY DECLARED.SDR TRAX200800466Flap · failedFLAP FAIL AT ZERO WHEN SELECTING 8 AT 200 KTS. EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLT4656 DEL 171 MINS.SDR TSAA0827018Flap · malfunctionedETOPS FLIGHT 483 SNA -OGG - ON APPROACH, THE CREW EXTENDED THE TRAILING EDGE FLAPS BUT THE FLAPS STOPPED AT FLAPS 1. THE CREW EXTENDED THE FLAPS USING THE ALTERNATE EXTENSION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AIRCRAFT FIM 27-51-00-81SDR DALA1202911501Link · unknownO/B I/B FLAP LINK REPLACED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.SDR COMA0860192Flap · malfunctionedFLIGHT 5108 - RECEIVED FLAP FAIL MESSAGE ON FLAP SELECTION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.SDR DXTA20082959Flap System · failed(FLAPS FAIL) AT APPROX 3 DEGREES WITH SLATS EXTENDED. PERFORMED FLAP SYSTEM OPERATION TEST IAW MM 27-50-00 4 A, B, C, D & F. RAN FLAPS THROUGH 10 TIMES. OPS CHECK GOOD AT THIS TIMESDR MASA200800254Ecu · malfunctionedASH FLT 2934 PHX- MEM, FLAP HALF SPEED MESSAGE, SPOILER STAB FAULT MESSAGE, FLAP AURAL WARNING WITH FLAP AT ZERO DEGREES, AND ALT 100-200 FT HIGH AT FL 330. REMOVED AND REPLACED NR 1 SFECU.SDR A6WA200840230Flap System · failedFLAPS FAILED OCCURRED ON APPROACH TO PHL, FLAPS FAILED AT 20 DEGREES, QRH PROCEDURE COMPLIED WITH OPS CHECK GOOD. COMPLIED WITH RESET PER SUPP 98-018B, OPS CHECK GOOD. (M)SDR MASA200800243Flap · failedASH FLT MFR-LAS, CREW REPORTED FLAPS FAIL CAUTION OCCURRED ON APPROACH AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. MX COMPLIED WITH THE FLAPS FAIL PART A PROCEDURE AND FECU INTERROGATION.SDR A6WA200840206Flap System · malfunctionedFLAP FAILED MESSAGE, FLAP FAILED AT ZERO. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET. OK. (M)SDR A6WA200840211Flap System · malfunctionedFLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO POSITION, FLAPS READ 45 DEGREES LT, 45 DEGREES RT. (M)SDR A6WA200840225Flap System · malfunctionedFLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO FLAPS READ ZERO ON FLIGHT CONTROL PAGE. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAPS RESET AIRCRAFT RELEASED FOR SERVICE. (M)SDR A6WA200840200Flap System · malfunctionedFLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 0 DURING EXTENSION. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET, OK. (M)SDR TRAX200800426Flap · failedFLAP FAIL AT 200 KTS AT ZERO DEGREES WHEN SELECTING 8. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. EMERGENCY DECLARED. FLT 4568 DEL 279 MINS. (SKEW DETECTION SYSTEM) LUBED, RESHIMED AND RIGGED FLAP ACTU
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