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 A6WA201542868Flap System · malfunctionedFLIGHT 3815, RECEIVED A FLAP FAIL CAUTION MESSAGE DURING APPROACH. FLAPS FAILED AT 30 DEG. COMPLIED WITH QRH. BTMS 3, 5, 3 & 3 DECLARED AN EMERGENCY AND PERFORMED FLAP RESET PROCEDURE IAW 98-018G BOX 12. FLAPS RESET.Jun 26, 2015 · N428AW · Cndair CL6002B19SDR CA150626009Control Cable · frayed(CAN) FLAP CENTER CABLE FOUND FRAYED.Jun 25, 2015 · Moravn Z242LSDR A6WA201542870Control Unit · failedFLIGHT 3939, FLAPS CAUTION MESSAGE AT ZERO DEGREES, PERFORMED FLAP RESET PROCEDURE IAW 98-18G BOX 12. FLAPS RESET. R & R BTSU.Jun 25, 2015 · N456ZW · Cndair CL6002B19SDR CA150624005Drive Shaft · damaged(CAN) DURING MX TASK 000-27-690-104, MX NOTED THE NR 5 DRIVE SHAFT HAD A BROKEN STRAND WHICH HAD UNRAVELED FROM THE CORE. SHAFT REQUIRES REPLACEMENT.Jun 24, 2015 · Cndair CL6002B19SDR CA150624004Flex Drive · damaged(CAN) WHILE PERFORMING TASK 000-27-690-104, DETAILED INSPECTION OF THE RT FLAP FLEXIBLE DRIVE, MX OBSERVED THAT THE NR 4 RT FLAP FLEX DRIVE CASING WAS FOUND TO HAVE INNER COIL SEPARATED FROM END. THIS CONDITION ALLOWS FOR THE POSSIBILITY OF MOISTURE & FINE DEJun 24, 2015 · Cndair CL6002B19SDR AALA201506249008Flap · out of rigEMERGENCY LANDING, DURING APPROACH, A LOCKED FLAPS 1 & SLAT 1 MSG OCCURRED WHEN MOVING FLAP LEVER TO POSITION 2. THE FLIGHT CREW DECLARED AN EMER & EMER EQUIP WERE STANDING BY. THE ACFT LANDED WITHOUT INCIDENT. PERFORMED FLAP ALIGNMENTS IAW TSM 27-51-00-810Jun 23, 2015 · N918US · Airbus A321231SDR CA150619003Cable · frayed(CAN) FLAP CABLE FOUND FRAYED.Jun 18, 2015 · Moravn Z242LSDR RU3A20150618014Flap · lack of lubeFLAPS FAIL ON INITIAL TAKE OFF. FAILED AT 18^. AIRSPEED REACHED 240 KIAS WITH NO OVER SPEED WARNING. COMPLIED WITH OVER SPEED INSPECTION. LUBED FLAPS.Jun 18, 2015 · N86 · Cndair CL6002B16SDR RU3A20150616013Handle · looseFLAPS WOULD NOT EXTEND. TIGHTENED LOOSE FLAP SWITCH HANDLE, CLEANED & RESEATED 2 CONNECTORS.Jun 16, 2015 · N57 · Lear 60LEARSDR RAIA201506150001Drive Unit · inoperativeFLAP FAIL EICAS MSG WITH FLAP STUCK AT 9 DEGREES ON APPROACH. MAINTENANCE RESET FLAPS, OPS CHECK GOOD, SAFE FOR 1 TIME FERRY FLIGHT. MAINTENANCE REPLACED FLAP DRIVE UNIT, OPS CHECK GOOD AND RELEASE FOR REVENUE SERVICE.Jun 15, 2015 · N14153 · Emb EMB145XRSDR VNAA2015061500010Control Unit · failedCREW REPORTED FLAPS FAIL AMBER MESSAGE ON APPROACH. FLAPS FAILED AT ZERO DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW ACFT FAULT ISOLATION MANUAL, FIM, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PERFORMED CHECKS IJun 15, 2015 · N230PS · Cndair CL6002B19SDR ANCF2015061501Strut · out of adjustDURING APPROACH, WHEN FLAPS WAS SELECTED, FLIGHT CONTROL FLAPS LOCKED APPEAR ON ECAM. IAW AMM 27-54-00-200-001 A VISUAL INSPECTION OF THE TRANSMISSION ASSEMBLY, AMM 27-51-44-820-001-A ADJUSTMENT OF THE INTERCONNECTING STRUT LT FLAPS WAS ACCOMPLISHED. OPERATJun 14, 2015 · N451AV · Airbus A320214SDR CALA2015060800494Control Valve · unserviceablePRIMARY FLAP CONTROL FAILURE, EMER DECLARED WITH ATC. TROUBLESHOOTING IAW FIM 27-51-00-810-801. FOUND LOW SPEED SOLENOID OUT OF LIMITS. R & R FLAP PRIMARY CONTROL VLV IAW AMM 27-52-00-810-801. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD.Jun 8, 2015 · N69020 · Boeing 777224SDR Q2SA20150529226Warning Light · illuminatedFLAP DISAGREE INFLIGHT. QRH PROCEDURE PERFORMED. REMOVED FLAP POSITION INDICATOR CONNECTOR PLUG, CLEANED & RE-INSTALLED. PERFORMED T/E OPS TEST IAW AMM 27-51-00, PG 501. SYSTEM CHECKS SERVICEABLE. INDICATION SYS RET FOR CONTINUED SERVICE.May 29, 2015 · N494SA · Boeing 7374H6SDR AALA20150527010Fseu · inoperativeAFTER TAKEOFF, SELECTED FLAPS UP. FLAPS INDICATOR SHOWED A SPLIT & REMAINED AT FLAPS 1 DEGREE. LANDED WITH FLAPS AT 1B DEGREE. REPLACED THE FSEU.May 27, 2015 · N938AN · Boeing 737823SDR IPXA2015052789463Flap System · malfunctionedEMERGENCY DECLARED, RECEIVED EICAS FLAP DISAGREE AND DISCREET LIGHT. STATUS PAGE MSG T/E FLAP DRIVE OFF. CANCELLED EMERGENCY AFTER FLAPS CORRECTED, REF FIM 27-51-00-815-839, PFM FSEU AND FSPM BITE TEST NORMAL. NO FAULT FOUND IAW AMM 27-51-00-201 OPERATED FLMay 25, 2015 · N308UP · Boeing 76734AFSDR ASMF201507004Flap System · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH, TE FLAP DISAGREE WITH FLAPS INDICATOR STAYING IN 2 UNITS & DECLARED AN EMERGENCY. ACCOMPLISHED WITH THE PROCEDURE TO EXTEND FLAPS TO 30 UNITS USING ALTERNATE FLAP EXTENSION. PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 830May 20, 2015 · N520AM · Boeing 73781QSDR FDEA201505201570Brake · lack of lubeRECEIVED TE FLAP DISAGREE EICAS MSG ON APPROACH WHEN MOVING FLAPS FROM 20' TO 25'. RETRACTED FLAP HANDLE TO 20' IAW GO AROUND PROCEDURES, RAN QRH & LANDED FLAPS 20' TROUBLE SHOT FLAP DISAGREE IAW FIM 27-51 FAULT TREE 808. FOUND LT OTBD FLAP TRANSMISSION OVERMay 20, 2015 · N961FD · Boeing 7572Y0SDR REXA2015051900518Bpsu · malfunctionedFLAPS FAIL CAUTION MSGS CAME ON WHILE SELECTING FLAPS 0 TO 20 DEG AT EXTENSION 3000 FT MSL. OUTSIDE TEMP, TAT 07 DEG, CLEAR SKY. CURRENT SPEED AT SELECTION 185 KTS, TIME WAS APPROX 1 HR INTO FLIGHT, 6:52 LOCAL, FOLLOW QRH LANDING WEIGHT 43000. PERFORMED TROMay 19, 2015 · N8913A · Cndair CL6002B19SDR ASAA2015051811971Fitting · corrodedRT INBD FLAP, EB RIB TORQUE TUBE FITTING HAS PITTING , DISCOVERED AFTER REMOVING TORQUE TUBE. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW SAS EA 400, 57EA, 15179, REV. NEW DATED 04JUN15. THIS IS A CATEGORY B REPAIR STAGEMay 18, 2015 · N763AS · Boeing 7374Q8SDR CA150526002Bpsu · failed(CAN) FLAPS FAIL MSG ON APPROACH WITH FLAPS AT ZERO. ACFT WAS AT 195 KTS & 2500` NO EMER DECLARED. RIGGED LT & RT FLAP BPSUS IAW AMM 27-51-10-830-801. BOTH BPSUS READ 0.00 WITH FLAPS SET TO ZERO. ACCOMPLISHED OPERATIONAL TEST OF FLAP SYS IAW AMM 27-54-00. May 17, 2015 · Cndair CL6002B19SDR REXA2015051700509Ecu · malfunctionedFLAPS FAIL, FLAPS 0 LANDING, LIGHT CAME ON 195 KTS, 2500 FEET. FLAPS FAILED TRYING TO SET 20 DEG. REF FLAP FAIL EVENT ON AML 3222764. LT & RT FLAP BPSUS REQUIRED RIGGING IAW AMM 27-51-10. PERFORM OPERATIONAL TEST OF FLAPS IAW TASK 27-54-00-710-801. IAW FIMay 17, 2015 · N8913A · Cndair CL6002B19SDR CALA2015051593790Control Unit · malfunctionedAIR RETURN DUE TO FLAP SLAT LOCK MSG STUCK BETWEEN 1 & 0. REPLACED FLAP SLAT CONTROL UNIT SFCC1. OPERATIONS NORMAL.May 13, 2015 · N439UA · Airbus A320232SDR J7SA2015051152116Pdu · leakingSHORTLY AFTER TAKEOFF, CREW EXPERIENCED, MAIN HYD QTY LO, CAS MSG. DURING APPROACH, AFTER SELECTING FLAPS 8 FOR LANDING, CREW RECEIVED MAIN HYD PRESS CAS. DECLARED EMER & LANDED WITHOUT INCIDENT. CREW HAD BRAKE AUTHORITY DURING LANDING. ON POST FLIGHT CREWMay 6, 2015 · N625FX · Lear 45LEARSDR DALA2015050803146Shaft · corrodedNR 2 AFT FLAP DRIVE BALLSCREW SHAFT IS CORRODED. REPLACED NR 2 AFT FLAP BALLSCREW IAW AMM 27-51-21.May 6, 2015 · N547US · Boeing 757251SDR DALA2015050803147Ball Screw · corrodedLT INBD FLAP, OTBD FLAP SCREW HAS PITTING AT ATTACH AREA. NR 3 SCREW. REPLACED NR 3 FLAP BALLSCREW. INSTALLED ON AMDS CARD 2751-2538. LP1937564.May 3, 2015 · N547US · Boeing 757251SDR CA150430004Drive Shaft · worn(CAN) LT & RT OTBD FLAP DRIVE SHAFTS ARE CONTACTING WING T/E STRUCTURE DURING FLAP OPERATION. NOTED DURING FLAP OPS CHECKS. FURTHER INSPECTION OF BOTH DRIVE SHAFTS REQUIRED.Apr 30, 2015 · Gulstm GIVSDR JJBA20150430001Solenoid Valve · trippedFLAPS WOULD NOT EXTEND ON LANDING. FLAP CONT L7 POPPED & WOULD NOT RESET. R & R FLAP POWER UNIT SOLENOID VALVE.Apr 30, 2015 · N857CA · Dhav DHC8202SDR CA150501005Drive Shaft · broken(CAN) THE END OF ITS LIFE DRIVE SHAFT HEAD BROKE OFF AT THE ACTUATOR.Apr 29, 2015 · Beech 1900CSDR AALA20150429016Fseu · failedWHILE CONFIGURING TO FLAPS 5 DEGREES DURING APPROACH RECEIVED, FLAPS PRIMARY FAIL, EICAS MSG. FLAPS LOWERED BY ALTERNATE PROCEDURE & LANDED FLAPS 20 WITHOUT INCIDENT. EMERGENCY DECLARED, LANDING UNEVENTFUL. ACCOMPLISHED FIM 27-52-00-810-801. R & R NR 2 FSEApr 29, 2015 · N758AN · Boeing 777223SDR CALA2015042800330Flap · malfunctionedON FINAL APPROACH, WIND GUST EXCEEDED FLAPS 30 SPD & THEY RETRACTED TO 25, ON MISSED APPROACH THEY WERE LOCKED OUT AT ABOUT 27 COULD NOT RETRACT, FLAP STAYED AT 27 UNTIL LANDING & RETURNED TO 25 AFTER TOUCHDOWN. MAX SPEED ON MISS WAS 195 WITH GUSTS & FLAP AT Apr 24, 2015 · N36280 · Boeing 737824SDR CA150505007Cable · broken(CAN) BOTH MID FLAP EXTENSION CABLES,, WERE FOUND BROKEN DURING A DAILY INSPECTION WHEN THE FLAPS WOULD NOT RETRACT. BOTH CABLES WERE REPLACED AND FLAPS WERE CYCLED REPEATEDLY WITH NO FURTHER PROBLEM . ACFT WAS RETURNED TO SERVICE.Apr 22, 2015 · Boeing 727223SDR FDEA201504221287Transmission · lowWHEN PUTTING FLAPS FROM 20 TO 25, TE FLAP DISAGREE EICAS WARNING CAME ON. FLAPS STAYED AT 20. WENT AROUND & FOLLOWED QRH. RETURNED TO AIRPORT FOR UNEVENTFUL 20 FLAP LANDING. TROUBLE SHOT SYS IAW FIM 27-51 FT 808. FOUND NO FLAP OVERLOAD INDICATORS TRIPPED.Apr 22, 2015 · N915FD · Boeing 757236SDR AALA201504249010Warning Message · false activationFLIGHT 2041 EN-ROUTE. WHILE ON APPROACH, CREW RECEIVED ECAM MESSAGE, FLIGHT CONTROL FLAP SYS 2 FAULT, WHEN FLAPS 3 WAS SELECTED. DECLARED AN EMERGENCY & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. PERFORMED SFCC 2 BITE TEST. THE SFCC 2 TESTED NORMAL. NO FApr 21, 2015 · N737US · Airbus A319112SDR FDEA201504171267Seal · brokenON CONFIGURING FOR LANDING, WHEN SELECTING FLAP 30 FROM TE DISPLAY, EICAS MSG APPEARED. RAN QRH PROCEDURE & LANDED FLAP 20 DEGREE. RAN THE FLAP HYD FROM 0 TO 30 DEGREES 2 TIMES, RAN THE FLAPS ELEC 0 TO 30, 2 TIMES WITH NO FAULTS. CHECKED ALL 3 FSEU'S NO FAUApr 17, 2015 · N991FD · Boeing 757232SDR CA150416004Control Rod · bent(CAN) ANNUAL INSPECTION, LT WING, FOUND THE ACTUATING CONTROL ROD FOR FLAP SYSTEM, PN C3CF105-7 WAS BENT, DEFLECT .5", INSIDE WING, NEAR FUSELAGE, JUST BEHIND THE FIBER ROLLER APPROXIMATE 2", IN NORMAL OPERATION THIS SECTION DOESN`T TOUCH THE FIBER ROLLER, NO Apr 16, 2015 · Dhav DHC3SDR CA150417008Control Unit · failed(CAN) AIR TURNBACK DUE TO FLAPS FAIL AFTER TAKEOFF. NO EMERGENCY DECLARED. MX REPLACED FECU.Apr 15, 2015 · Cndair CL6002B19SDR REXA2015041500411Control Unit · failedFLAP FAILED AT TAKEOFF 170KT AT 20 DEGREES AT 1.5 MIN. RETURNED TO FIELD. PERFORMED RESET & MESSAGE CLEARED. TROUBLESHOT IAW 27-50-00. R & R FECU IAW AMM 27-51-05. ALL CHECKED GOOD.Apr 15, 2015 · N8980A · Cndair CL6002B19SDR REXA2015041400409Detector · faultyFLAPS FAIL MSG. DURING AFTER START PROCEDURE WHEN FLAPS WERE SELECTED TO 20 DEGREES. PERFORMED R & R OF SKEW DETECTION UNIT IAW AMM 27-51-15. OPERATIONS TESTED GOOD IAW AMM 27-51-15. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD 1009 - 0Apr 14, 2015 · N834AY · Cndair CL6002B19SDR FDEA201504141230Nut · lack of lubeON APPROACH, WHEN CONFIG FROM SLATS 15 TO FLAPS 15, RECEIVED FLAPS SYS 1 & SYS 2 FAULT. RECYCLED HANDLE TO SLATS 15 IAW PHASE ONES THEN RE-ATTEMPTED FLAPS 15, SAME RESULT FLAPS SYS 1 & SYS 2 FAULT. REVIEWED QRH, ELECTED TO DIVERT, ON APPROACH, CONFIGURED WHEApr 14, 2015 · N427FE · Airbus A310203SDR CA150414002Flap System · failed(CAN) ON APPROACH WHEN SELECTING FLAP TO FULL, LEVER DISAGREE FOLLOWED BY SLAT LOW RATE MESSAGE APPEARED. FULL FLAP EVENTUALLY ACHIEVED AND NORMAL LANDING PERFORMED. RESET FLAP/SLAT SYSTEM IAW QRRG. OPS CHK NORMAL. NO FURTHER DEFECTS.Apr 13, 2015 · Emb ERJ190100IGWSDR AALA20150408025Flap System · malfunctionedDURING DESCENT FLIGHT CREW RECEIVED A FLAP ASYMMETRY SPLIT OF ONE DEGREE ON THE INDICATOR. FLAPS WORKED IN ALTERNATE MODE. EMERGENCY DECLARED, LANDING UNEVENTFUL. INSPECTED TE TRIP INDICATORS & NONE FOUND TRIPPED. PERFORMED TE OPERATIONAL CHECK IAW AMM 27-Apr 8, 2015 · N925AN · Boeing 737823SDR CA150410017Motor · unserviceable(CAN) SMOKE IN COCKPIT, FLAP CB POPPED, DEFECT DESCRIPTION IN LOGBOOK. FLAP MOTOR WAS FOUND BURNT FROM BEING OVERHEATED. FLAPS FOUND TO BE IN THE UP POSITION , TIGHT UP AGAINST THE WING. THOUGHT IS, THAT THE FLAPS RIGGING SLOWLY WENT OUT OF RIG & TIGHTER UApr 7, 2015 · Beech 200BEECHSDR DXTA201504086002Control Unit · failedSWPS FAULT & SPOILER FAULT EICAS IN FLIGHT. ASSOCIATED NO FLAP INDICATION YELLOW X'S & NO PITCH INDICATION YELLOW X'S. FOLLOWED QRH PROCEDURE & EXECUTED FLAPLESS APPROACH. REMOVED & INSTALLED NR 1 FCE. OPS CHECKED GOOD IAW AMM 27-03-01.Apr 7, 2015 · N330QS · Emb EMB505SDR AALA20150406023Transmitter · faultyDURING APPROACH FLAPS WOULD NOT GO BEYOND 15 DEGREES. FSEU BITE RETURNED, TE FLAP SENSOR DISAGREE, WITH CODE 27-52261. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R, RIGGED NR 2 FLAP POSITION TRANSMITTER IAW AMM 27-58-01. SYS CHECKED NORMAL. SEE ALSO AALAApr 6, 2015 · N859NN · Boeing 737823SDR F3LA2015040601127Unknown · malfunctionedFLAP JAM AT SLAT ONLY, FLAPS LOCKED. PERFORMED BITE TEST OF SFCC IAW AMM 27-51-00-740-002-A. PERFORMED 2 FULL FLAPS & SLATS CYCLES, NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF THE FLAPS & SLATS, NO DEFECTS NOTED LP 893710.Apr 2, 2015 · N935FR · Airbus A319111SDR HNAA2015040100114Switch · failedAFTER TAKEOFF AND CREW SELECTED FLAPS O ZERO, FLAP INDICATOR REMAINED AT 5 DEGREES. NO ASSOCIATED CAUTION LIGHTS ON THE GROUND. FLAPS APPEAR TO BE 5 DEGREES. TROUBLE SHOOT AND FOUND FLAP SELECTED ARMING SWITCH 2752-S1 AT FLAP HANDLE BAD. REPLACED MICROSWITCApr 1, 2015 · N935HA · Dhav DHC8102SDR CALA2015040293502Pin · migratedTRAILING EDGE FLAPS WILL NOT MOVE ELEC OR WITH HYD. FOUND PIN MIGRATING OUT OF VLV INDICATOR LEVER PROHIBITING FULL VLV MOVEMENT. REPLACED FLAP PDU BYPASS VLV & ROTARY ACTUATOR.Mar 31, 2015 · N649UA · Boeing 767322SDR QXEA2015032800169Power Unit · malfunctionedON DESCENT AT 270 KNOTS AT 14,000 FT, FLAP POWER CAUTION ILLUMINATED, NO TURBULENCE. RAN CHECKLIST, CYCLED L7 FLAP CONT CB, NO HELP, CAUTION REMAINED ILLUMINATED. LANDING UNEVENTFUL. R & R FLAP POWER UNIT, FUNCTIONAL CHECKS GOOD. FLAP POWER CAUTION DOES NOT ILMar 28, 2015 · N426QX · Bombdr DHC8402SDR R61A201503260190Sensor · failedCREW RECEIVED A FLAP FAIL MESSAGE. CREW RAN QRH WITH NO SUCCESS. CREW DECLARED AN EMERGENCY, DIVERTED AND WITH VEHICLES ROLLING, LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND FLAP SKEW SENSOR VOLTAGE OUT OF LIMITS. MAINTENANCEMar 26, 2015 · N829MD · Emb ERJ170100SU
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