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.

SDR VNAA0507014Flap · unknownON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. MAINTENANCE CLEARED THE CAUTION MESSAGE IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Jul 20, 2005 · N209PS · Cndair CL6002C10SDR A6WA200540260Bpsu · inoperativeFLAPS FAIL CAS APPROACH, MYR FLAPS SELECTED NOT MOVE QAR C/W FLAPS ZERO LANDING. ACCOMPLISHED -30 DEGREES. REMOVED AND REPLACED LT BPSU IAW AMM. OPS CHECK GOOD. (K)Jul 19, 2005 · N426AW · Cndair CL6002B19SDR SWIA200515305Sensor · malfunctionedFLAPS FAIL .17 DEGREES ON APPROACH INTO SLC. REMOVED AND REPLACED NR 1 BPSU AND RIGGED LEFT AND RIGHT BPSU IAW CRJ 27-51-10. OPERATIONAL CHECK GOOD.Jul 19, 2005 · N416SW · Cndair CL6002B19SDR DXTA200500846Flap System · malfunctionedSLATS AND FLAPS INTERMITTANT AFTER TAKEOFF, SELECTED FLAPS, SLATS & KRUEGERS UP. FLAPS STAYED AT 20 DEGREES, SLATS STAYED DOWN AND KRUEGER'S RETRACTED. ALSO HAD THE FOLLOWING ICAS MSG SLAT/FLAP MAINTEN. ITEM IS UNDER INVESTIGATION.Jul 19, 2005 · N721QS · Gulstm 200SDR MASA200500561Fcu · warning lightASH 2687 CLT, FLAP FAIL MESSAGE IN FLIGHT. R2 FECU.Jul 18, 2005 · N843MJ · Emb EMB145LRSDR P9RA20050095Flap System · out of adjustDURING DESCENT BACK INTO SFB, CREW NOTED VIBRATION IN AIRCRAFT ABOVE 270KIAS. LOW FREQUENCY VIBRATION. SUSPECT RIGHT FLAP AREA. MAINTENANCE ADJUSTED RIGHT INBD. FLAP IAW M/M. OPS CHECKED GOOD. NOTE. NO FURTHER VIBRATION NOTED AS OF 7/28/2005.Jul 18, 2005 · N54344 · Boeing 727231SDR SWIA200515306Control Unit · out of rig"FLAPS FAIL" CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU AND FOUND BOTH LEFT AND RIGHT BPSU'S OUT OF TOLERANCE. RE-RIGGED BOTH LEFT AND RIGHT BPSU'S IAW CRJ 200 MM 27-51-10. OPERATIONAL CHECK GOOD.Jul 18, 2005 · N906SW · Cndair CL6002B19SDR SWIA200515296Control Unit · malfunctionedDURING CLEAN UP ON OUR CLIMB OUT, WE RECEIVED "FLAPS FAIL" MESSAGE ON ED 1. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW 27-50-01. OPERATIONAL CHECK OK.Jul 17, 2005 · N919SW · Cndair CL6002B19SDR REX2005F00016Control System · failed(REF NR: 05-087) FLAPS FAILED ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jul 15, 2005 · N801AY · Cndair CL6002B19SDR VNAA0507012Flap · unknownON FINAL APPROACH WITH FLAPS 20° THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH THE FLAP FAIL RESET PROCEDURES IAW CRJ200 RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECK GOOD. THE AIJul 15, 2005 · N221PS · Cndair CL6002B19SDR MALA050583Computer · failedAFTER TAKEOFF FLAP STUCK AT 18 WITH FLAP INOP AND FLAP FAULT. REMOVED AND REPLACED COMPUTER PN 676801007 SN OFF UEL/DRG/1435-92, SN ON UEL/DEG/1121-85 IAW AMM 2750-17. OPS CHECK GOOD.Jul 15, 2005 · N520XJ · Bac AVRO146RJ85ASDR DL76L050370Flap System · malfunctionedCREW REPORTS T/E FLAP DISAGREE WITH FLAPS AT 15 EMERGENCY DECLARED INTO CDG. PERFORMED SEVERAL RETRACTION/EXTENSION WITH HYDRAULIC AND ELECTRIC POWER ALTERNATE. NO FAULT DUPLICATED. PERFORMED FSEU BITE TEST, TEST PASSED.Jul 15, 2005 · N179DN · Boeing 767332SDR SWIA200515286Control Unit · malfunctionedCONTROL FAULT FLAPS EXTEND TO 7 DEGREES. REPLACED FLAP COMPUTER IAW 27-50-06. OPERATIONAL CHECK GOOD.Jul 15, 2005 · N295SW · Emb EMB120ERSDR ERYR682DCable · brokenFLAP FOLLOW-UP CABLE WAS DISCOVERED CORRODED AND BROKEN IN HALF DURING AN INSPECTION.Jul 15, 2005 · N746TA · Beech 400ASDR 2005FA0000960Cable · brokenFLAP FOLLOW-UP CABLE WAS DISCOVERED CORRODED AND BROKEN IN HALF DURING AN INSPECTION.Jul 15, 2005 · N746TA · Beech 400ASDR SWIA200515299Control Unit · malfunctionedFLAPS AND SWS LIGHT ON MAP. REPLACED FLAP CONTROL UNIT IAW 27-50-06. OPERATIONAL CHECK GOOD. PN: 347200-1001, SNOFF: 211Jul 14, 2005 · N578SW · Emb EMB120ERSDR COMA0560392Flap System · malfunctionedFLIGHT 5321 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 14, 2005 · N937CA · Cndair CL6002B19SDR SWIA200515282Pdu · malfunctionedFLAPS FAIL CAUTION MESSAGE ON GROUND. REPLACED FLAP PDU IAW MM 27-52-37. OPERATIONAL CHECK GOOD, PN 766359B, SNOFF 0543.Jul 14, 2005 · N719SK · Cndair CL6002C10SDR COMA0560391Flap System · malfunctionedFLIGHT 5384 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 13, 2005 · N814CA · Cndair CL6002B19SDR 71722Switch · out of rigAFTER TAKEOFF, CREW WAS NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE FLAP LIMIT CAM SWITCH S-4 WAS RIGGED. THEREFORE NO PARTS WERE USED.Jul 11, 2005 · N155YV · Beech 1900DSDR 71222Flap System · malfunctionedAFTER TAKEOFF, CREW NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. STILL AWAITING MORE INFORMATION.Jul 11, 2005 · N155YV · Beech 1900DSDR SWIA200515271Control Unit · malfunctionedFLAP CONTROL FAULT AT ALTITUDE. REPLACED FLAP CONTROL COMPUTER IAW EMB 120 MM 27-50-06. OPERATIONAL CHECK GOOD.Jul 9, 2005 · N215SW · Emb EMB120ERSDR SWIA200515260Motor-Brake Unit · malfunctionedON TAXI IN, FLAPS 45 TO 30 FOR FLAPS HALFSPEED STATUS MSG. REPLACED RT FLAP BRAKE/MOTOR. OPERATIONAL CHECK GOOD IAW MM 27-24-02.Jul 8, 2005 · N959SW · Cndair CL6002B19SDR DXTA200500824Connector · corrodedON APPROACH INTO ASE FLAPS LOCKED UP AT 10 DEGREES. DIVERTED TO GJT FOR LANDING AT FLAPS 10. TROUBLESHOT FAULT BY OPENING THROTTLE QUAD AND CLEANED, LUBED. INSPECTION FLAP LEVER AND FOUND NO FAULT. INSPECTED 10 DEG FLAP SWITCH AND ACTUATOR SWITCH. BOTH CHJul 8, 2005 · N117QS · Beech 400ASDR 05FDEA01866Flap · jammedASYMETRICAL INBOARD TRAILING EDGE FLAPS AT 2 DEGREES UPON FLAP RETRACTION. RAN APPROPRIATE QRH PROCEDURES, FOUND LT INBD FLAP COCKED AND JAMMED INTO INBD AILERON. UPON FURTHER TROUBLESHOOTING FOUND BEARING WALKED OUT OF SCREWSHAFT END OF LT INBD TRANSMISSION.Jul 8, 2005 · N204FE · Boeing 7272S2FSDR SWIA200515267Control Unit · malfunctionedFLAP DISAGREEMENT WHEN FLAPS WERE SELECTED TO 45 DEGREES. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00.Jul 7, 2005 · N268UE · Emb EMB120ERSDR SWIA200515256Control Unit · malfunctionedFLAPS HALFSPEED STATUS MESSAGE. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW MM 27-51-05. OPERATIONAL CHECK GOOD.Jul 7, 2005 · N443SW · Cndair CL6002B19SDR SWIA200515245Pdu · malfunctionedDURING TAXI, AFTER SELECTING FLAPS TO 8 DEGREES FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. REPLACED PDU IAW 27-52-00 AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD PN 865D100-7, SN/OFF 162 PN 860D100-18 SN/OFF 768.Jul 7, 2005 · N409SW · Cndair CL6002B19SDR REX2005F00018Control System · failed(REF NR: 05-085) FLAP FAILED ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jul 6, 2005 · N8554A · Cndair CL6002B19SDR CA050706005Control Cable · frayedRT FLAP CABLE FRAYED AT WING ROOT PULLEY. THIS CABLE WAS A GALVANIZED CABLE.Jul 6, 2005 · Bbavia 8GCBCSDR QXEA200501101Control Unit · malfunctionedFLAP POWER CAUTION IN FLIGHT. RAN CHECKLIST. CAUTION STILL ILLUMINATED. GPWS CAUTION ALSO ILLUMINATED 15 MINUTES LATER WHILE CHANGING TO LOWER ALTITUDE. REPLACED FLAP CONTROL UNIT AS A PRECAUTIONARY MEASURE. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.Jul 6, 2005 · N404QX · Bombdr DHC8402SDR QXEA200501096Control Unit · malfunctionedFLAP POWER CAUTION IN FLIGHT. RAN CHECKLIST. CAUTION STILL ILLUMINATED. GPWS CAUTION ALSO ILLUMINATED 15 MINUTES LATER WHILE CHANGING TO LOWER ALTITUDE. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.Jul 6, 2005 · N404QX · Bombdr DHC8402SDR SWIA200515265Control Unit · malfunctionedON APPROACH FLAPS SELECTED 30 DEGREES, OVERSPEED FLAP CLACKER SOUNDED. REPLACED FECU. OPERATIONAL CHECK GOOD IAW 27-50-00.Jul 5, 2005 · N947SW · Cndair CL6002B19SDR SWIA200515259Detector · malfunctionedFLAPS HALFSPEED STATUS MESSAGE ON TAXI OUT. REPLACED LT INBOARD FLAP SKEW DETECTOR AND RIGGED IAW MM 27-52-45. OPERATIONAL CHECK GOOD.Jul 5, 2005 · N701SK · Cndair CL6002C10SDR F3LA200500030Flap System · malfunctionedDURING ARRIVAL IN ANC, FLIGHT CREW REPORTED FLT CONTROL FLAPS FAULT ON ECAM. SLATS TRAVELED TO THE 2 POSITION, FLAPS DID NOT MOVE FROM THE ZERO POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED BITE TEST OF SFCC 1 AND SFCC 2. NO FAULTS NOTED. OPERATEDJul 5, 2005 · N915FR · Airbus A319112SDR SWIA200515239Bpsu · malfunctionedFLAPS FAIL MSG CAME ON DURING CLIMB-OUT WHEN SELECTED FROM 20 TO 8 DEG. REPLACED LT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.Jul 4, 2005 · N407SW · Cndair CL6002B19SDR COMA0560378Bpsu · malfunctionedFLAPS FAIL CAUTION. REPLACED LT BPSU.Jul 4, 2005 · N981CA · Cndair CL6002B19SDR SWIA200515246Control Lever · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED CONTROL LEVER IAW 27-51-01. OPERATIONAL CHECK GOOD.Jul 3, 2005 · N403SW · Cndair CL6002B19SDR 2005FA0001009Bellcrank · bindingBINDING IN FLAP DR SYS AT BELLCRANKS WHERE ROD ENDS ATTACH. FLAP DR RODENDS WERE FOUND DIGGING INTO BELLCRANK ARMS AS THEY OPERATED, NML TRAVEL AS SHOWN BY RUB MARKS ON RODENDS. BELLCRANK ARMS, EXCESS CLAMPED BY RODEND ATTACH BOLTS, SOME BOLTS NOT TIGHTENED Jul 1, 2005 · N239LF · Cessna 206HSDR 20050605BTorque Tube · cutIN PERFORMING AD 2003-09-13, FOUND TORQUE TUBE WORE/CUT BY LEFT RUDDER CABLE. 2 INCH LOG AND THRU TUBE WALL. TUBE HAS BEEN INSTALLED SINCE 1996 1100 HRS AGO.Jul 1, 2005 · Piper PA23250SDR 2005FA0000944Torque Tube · cutPERFORMING AD 2003-09-13, FOUND TORQUE TUBE WORE/CUT BY LEFT RUDDER CABLE, 2 INCHES LONG AND THRU TUBE WALL. TUBE HAS BEEN INSTALLED SINCE 1996 1100 HRS AGO.Jul 1, 2005 · Piper PA23250SDR 2005FA0000943Torque Tube · cutPERFORMING AD 2003-09-13, FOUND TORQUE TUBE WORE/CUT BY LEFT RUDDER CABLE, 2 INCHES LONG AND THRU TUBE WALL. TUBE HAS BEEN INSTALLED SINCE 1996 1100 HRS AGO.Jul 1, 2005 · Piper PA23250SDR 386506171Torque Tube · cutPERFORMING AD 2003-09-13, FOUND TORQUE TUBE WORE/CUT BY LEFT RUDDER CABLE, 2 INCH LONG AND THRU TUBE WALL. TUBE HAS BEEN INSTALLED SINCE 1996 1100 HRS AGO.Jul 1, 2005 · Piper PA23250SDR SWIA200515226Control Unit · malfunctionedDURING APPROACH RECEIVED FLAPS HALFSPEED STATUS MSG WITH FLAPS SELECTED. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW 27-51-05. OPERATIONAL CHECK GOOD, SN OFF 753.Jun 30, 2005 · N407SW · Cndair CL6002B19SDR COMA0560370Warning System · activatedFLAPS FAIL CAUTION. RESET FLAPS AND DEFERRED MAINTENANCE PER AD 98-20-01.Jun 30, 2005 · N779CA · Cndair CL6002B19SDR COMA0560367Warning System · activatedFLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jun 29, 2005 · N917CA · Cndair CL6002B19SDR SWIA200515204Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE AFTER FLAPS RETRACTED. REPLACED LT BPSU AND RE-RIGGED FLAP SYSTEM IAW MM 27-51-10. OPERATIONAL CHECK GOOD.Jun 29, 2005 · N407SW · Cndair CL6002B19SDR SWIA200515203Bpsu · malfunctionedAFTER T/O RECEIVED A FLAPS FAIL CAUTION MESSAGE. REPLACED RT BPSU IAW CRJ MM 27-51-10.Jun 29, 2005 · N588SW · Cndair CL6002B19SDR REX2005F00019Control System · failed(REF NR: 05-084) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 28, 2005 · N8914A · Cndair CL6002B19SDR DHL2005802503Drive Link · crackedRT OUTBD FLAP DRIVE LINK ASSY CRACKED 0.500 INCH LENGTH AT POINT J STA XF 219.498. REMOVED AND REPLACED RH OUTBD FLAP DRIVE LINK ASSY AT STA XF 219.498 IAW MM 27-51-4 PG. 201-204. REFER TO NR 030703 FOR OPS CHECK.Jun 28, 2005 · N802DH · Doug DC873
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