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 UALA2013052003472Computer · faultedECAM FLAP FAULT. POST FLIGHT REPORT SHOWS SFCC-1. REPLACE COMPUTER, SLAT FLAP CONTROL IAW AMM.SDR AALA20130518008Fseu · inoperativeINFLIGHT, CREW REPORTED FLAPS WOULD NOT DEPLOY FURTHER THAN 1 DEGREE. EMERGENCY DECLARED, FLIGHT DIVERTED, AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYS GROUND CHECK NORMAL OPERATION.SDR AALA20130521001Sensor · inoperativeINFLIGHT CREW REPORTED WHEN SELECTING FLAPS 1 ON APPROACH THE FLAPS DID NOT EXTEND. EXTENDED FLAPS WITH THE ALTERNATE FLAPS SWITCH TO FLAPS 15 IAW QRH. EMERGENCY DECLARED, FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 2 SKSDR AALA20130518001Transmitter · failedCREW REPORTED FLAPS WOULD NOT EXTEND AND HAD TO EXTEND ELECTRICALLY. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT FLAP POSITION TRANSMITTER T428. SYS GROUND CHECK NORMAL OPERATION.SDR IPXA3678341Flap System · inoperativeAT APPROXIMATELY 5000 FT WHEN CONFIGURED FOR LANDING, LEFT FLAP STAYED AT 5 AND RT FLAP WENT TO 20. RAN EMERGENCY NON NORMAL CHECKLIST AND LANDED WITH FLAPS 20. EMERGENCY DECLARED. FLAPS CHECKS IAW FIM 27-58-00-815-803. R & R INDICATOR FLAP POSITION ISDR R61A201305130473Torque Tube · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING FLAP TORQUE TUBE SPLINE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT WING FLAP TORQUE TUBE IAW EMB 170 AMM 27-51-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR USAA2013051600016Torque Tube · corrodedQ4 CHECK - LEVEL 2 PITTING CORROSION ON RIGHT INBOARD MIDFLAP TORQUE TUBE UNDER OUTBOARD FLAP CARRAGE ARM AT WBL 183. REPLACED MIDFLAP ASSEMBLY IAW JOB CARD.SDR UHLA2013051300137Unknown · malfunctionedWHEN FLAPS 1 CALLED FOR VISUAL APPROACH, FLAP FAIL EICAS MESSAGE APPEARED. FOLLOWED QRH, EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. MAINTENANCE RETRACTED FLAPS TO 0 AND PERFORMED ELECTRICAL RIG ON FLAPS IAW AMM 27-50-00. OPS CHECKED FLAPS MULTIPLE TIMES OSDR UALA2013051503367Valve · failedTESTED FSEU, FLAPS FAIL WITH CMC MESSAGE 27-25241. REPLACED PRIMARY RETRACT SOLENOID ON FLAP PRIMARY CONTROL VALVE PER MM, OPS CHECKED OK PER MM. FLAP PRIMARY CONTROL VALVE TEST. EICAS MESSAGE CLEARED.SDR A6WA201305124021Control Lever · malfunctionedAFTER LANDING, FLAPS FAILED AT 30 DEG DURING RETRACTION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18F BOX 12. FLAPS RESET. REMOVED AND REPLACED FLAP CONTROL LEVER REF AMM 27-51-01. OPS CHECKED GOOD.SDR UHLA2013051100215Torque Tube · corrodedCORROSION ON RT WING, NR 6 FLAP TORQUE TUBE MALE END SPLINES. R & R JOINT UNIVERSAL.SDR AALA20130512005Fseu · inoperativeSEA - CREW REPORTED UNABLE TO FULLY DEPLOY FLAPS DURING LANDING. EMERGENCY DECLARED FLIGHT LANDED SEA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP/SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CA130510001Arm · cracked(CAN) DURING A SCHEDULED INSPECTION, THE CENTER FORWARD FLAP BRACKET ON THE RT FLAP ASSY WAS FOUND CRACKED IN THE ARM RADIUS ON THE INBD SIDE. THE FLAP ROLLER ARM ASSY PN 100-330-5003-02 WAS REPLACED WITH A NEW FLAP ROLLER ARM ASSY SUPPLIED BY QUEST ACFT COMPSDR AALA20130510001Transmitter · inoperativeBOS - CREW REPORTED FLAP LEVER SELECTED TO 1 DEGREE AND NOTHING HAPPENED. FOLLOWED QRH AND EXTENDED SLATS WITH ALTERNATE FLAP SWITCH. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP LEVER POSITION TRANSMITTER AND FLAP SKEW SENSOR. SYSTEM GROUND CHECK NORMAL OSDR DBCA201305050006Switch · failedON APPROACH TO ORD THE FLAPS WOULD NOT EXTEND. CREW RETURNED TO MKE, THE LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT TO FAILED FLAP RESET SWITCH WHICH CAUSED THE SYSTEM TO STICK IN SELF-TEST MODE. REPLACED FLAP RESET SWITCH. OPS CHECKED GOOD.SDR REXA2013050400869Flap · malfunctionedFLAPS FAIL AT 45 UPON RETRACTION AFTER LANDING, FLAP LEVER POSTION AT 45 AT FAILURE. AIRSPEED=0KTS OAT= 22. PERFORMED OPERATIONS CHECK OF FECU IAW AMM 27-51-05 & SKEW DETECTION SYS IAW AMM 27-51-15. OPERATIONS CHECK GOOD. CYCLED FLAPS MESSAGE CLEARED. OPESDR SIMA20130504004Ecu · malfunctionedON FLIGHT 2977 THE CREW REPORTED THAT DURING LANDING WHEN SELECTED FLAPS TO 9%. THE CREW RECEIVED A CAUTION MESSAGE FLAP FAIL AND EICAS INDICATION 0%. COMPLIED WITH AOM VO L 1 AND DECLARED AN EMERGENCY. THE CREW CALLED FOR CFR AS A PRECAUTIONARY MEASURE. TSDR PCSA2013050602Bypass Valve · faultyUPON RETRACTION, INBOARD FLAPS REMAINED AT 20°. AFTER LANDING FLAPS RETRACTED NORMALLY. MAINTENANCE REPLACED THE FLAP BYPASS VALVE, THE INBD FLAP ASYMMETRIC RELAY R187 AND THE INBD FLAP INDICATOR PER THE AMM, ACCOMPLISHED THE FLAP OPERATIONAL CHECK PER THE ASDR UALA2013050303120Fseu · failedPRIMARY FLAPS FAILED. FAULT CODE 27-20371, REF 27-51 TASK 801. REPLACED NR 1 FSEU PER MM 27-51-01. PERFORMED TRAILING EDGE FLAP SYSTEM OPS TESTED AND RAN FLAPS TO FULL. MESSAGE DID NOT RETURN.SDR REXA2013050200865Flap · failedFLAP FAIL UPON LANDING. CREW REPORTED FLAPS FAIL AT 4S DEGREES UPON RETRACTION AFTER LANDING FLAP LEVER POSITION AT 45 AT FAILURE AIRSPEED=0KTS OAT=22 DEGREES C. CREW DID NOT DECLARE EMERGENCY.
"SDR SAJF20130502015Flap System · stuck(B-18717) FLAP LT OTBD T/E FLAP STUCK AT 8.82 UNIT, RT OTBD T/E FLAP AT 7.01 UNIT, MSG FLAP DRIVE & ASYM COME ATB. FOLLOWING TROUBLESHOOTING, RVDT HAS BEEN REPLACED.SDR CA130430020Roller · worn(CAN) IT WAS DETERMINED THIS WEAR WAS THE RESULT OF THE FLAP ROLLERS P/N C6CWM1072-29, ALLOWING TOO MUCH FORE AND AFT MOVEMENT WHEN FLAPS WERE FULLY EXTENDED. NEW FLAP RODS P/N C6CW1083-1 INSTALLED AND ROLLERS ADJUSTED ACCORDINGLY. THERE WAS AN MRO FINDING RESDR FDEA201304300890Computer · failedFLAP RETRACTED PASSING 205KTS ECAM VMO WARNING O'SPD 205 KTS. ECAM CANCELED WARNING AND SLOWED TO 200 KTS. AFT T/O ECAM WRNG T/O CONF WRNG TOO LOW FLAPS ONLY MOMENTARYILY. PDIS 741 27-01 5155 AFT LANDING ECAM WARNING FWS AMBER FAULT MONITOR SYSTEM. AFTER TSDR UALA2013043003021Solenoid · faultyFLAP TIP BRAKE FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND SFCC-1 FAULTING LEFT WTB BLUE SOLENOID 33CV. REPLACED 33CV SOLENOID REF MM.SDR CA130429001Flap System · malfunctioned(CAN) UPON FLAPS RETRACTION FROM 5" FLIGHT CREW RECEIVED A "FLAP POWER" CAUTION MESSAGE AND FLAPS REMAINED AT 5". WEATHER CONDITION/FUEL CONSUMPTION WAS ASSESSED AND FLIGHT CONTINUED TO DESTINATION, ACFT LANDED WITHOUT FURTHER INCIDENT. DECISION WAS LATER TAKSDR ASMF20130523005Sensor · damagedCAPTAIN REPORTED THAT AFTER START ENGINES, THE L/E FLAPS TRANSIT LIGHT TURNED ON. DURING MX REVISION, THE SENSOR FLAP SKEW NR 6 WAS DETECTED DAMAGED; SO THE SENSOR WAS REPLACED IAW AMM 27-59-01, TESTED CORRECT.SDR UALA2013042602926Motor · inoperative'FLAPS PRIMARY' EICAS CAUTION MESSAGE DISPLAYED. INBOARDD OR OUTBOARD TRAILING EDGE HYD FLAP DISAGREE OR LEADING EDGE PNEU FLAP DISAGREE (INHIBITED BY 'FLAPS DRIVE' L27108 AND 'FLAPS CONTROL' L27109). ON RETRACTION ON GROUND FOUND RIGHT I/B DRIVE MOTOR INOPSDR UALA2013042502899Computer · faultyPFR SHOWS "GPSW FLP MODE PB SW (7WZ)-SFFC1( 21CV)-GPWC(1WZ) 34-48-08" "SFCC1-2(21CV-22CV)-ADIRU2(1FP2) AOA I NPUT A & B 27-51-34" AND "SFCC1 21CV 27-51-34". PERFORMED GPWS, ADR2, SFC C2 BITES - NO FAULTS. RAN FLAPS NO MSGS. INSTALLED NEW SFCC 1 AND FINAL SDR SWIA201333335Flap · vibrationAS FLAPS EXTEND THROUGH 20 DEGREE AIRCRAFT BEGINS TO SHUTTER AND VIBRATES EXCESSIVELY. (FLT 4826) INSPECTED FLAPS ATTACHING HARDWARE, FAIRING GAPS, ALL ACCESS PANELS, GEAR DOORS AND GEAR, NO DEFECTS NOTED. CYCLED FLAPS SEVERAL TIMES WITH NO ABNORMAL NOISE OSDR CVGA201304024Controller · failedFLAPS FAILED AT 25 DEGRESS WHILE ON APPROACH.SDR CA130508006Flap System · failed(CAN) CREW REPORTED "FLAPS FAIL" CAUTION MESSAGE RIGHT AFTER LEVEL OFF AT FL 380 A/C PREFORMED A ZERO FLAPS LANDING. PART REMOVED: DETECTOR, SKEW, FLAP TRACK, INBD PN 5915549 REMOVED.SDR CA130508005Flap System · failed(CAN) CREW REPORTED ENROUTE AFTER FLYING AT FL 390 FOR 20 MINUTES WE RECEIVED CAUTION MESSAGE, FLAPS FAIL, IT NEVER WENT AWAY. ACFT DID A ZERO FLAPS LANDING. MAINTENANCE CLEARED FLAPS INHIBITS THROUGH THE MDC AND PERFORMED AN OPS CHECK OF THE FLAPS IAW AMM 27SDR UALA2013042302815Computer · faultyF-CTL FLAP SYS 1 FAULT ECAM. REPLACED NR 1 SFCC REF AMM 27-51-34-000-001-A.SDR SAJF2013042302014Electrical Box · malfunctioned(B-18606) PERFORMED A HIGH SPEED RTO DUE TO TAKEOFF CONFIG, WARNING SOUND CAME ON AND RTO SPEED AT ABOUT 140KTS IAW AMM05-51-07 PFM HIGH ENERGY STOP. FOUND MAINT MESSAGE 31-53010 (L/E FLAP NOT EXT) IAW FIM27-51 TASK 801 PFM FSEU BITE FOUND MSG 27-81218 (PROXSDR AALA20130420010Relay · failedBOS - CREW REPORTED WHEN SELECTING FLAPS 25 TRAILING EDGE FLAP DIAGREE MESSAGE APPEARED. EMERGENCY DECLARED FLIGHT LANDED BOS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOAD RELIEF RELAY K10245 BAD. REPLACED RELAY K10245. SYSTEM GROUND CHECK NSDR ASMF201305002Sensor · damagedCAPTAIN REPORTED THAT DURING APPROACH, T/E FLAPS ASYMMETRY LEVER DID NOT COMMAND, FLIGHT CREW ACCOMPLISHED QRH 9.28 PROCEDURE, LANDING WITH SLATS DOWN AND FLAPS UP IAW SUCH QRH PROCEDURE. MX PERSONNEL PERFORMED FLAP CONTROL SURFACE VERIFICATION FOR CONDITION SDR UALA2013041902715Computer · failedFLAP SYSTEM 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. INSTALLED NEW UNIT IN POS 1. IAW MM27-51-34. BITE AND OPS TESTED OK. ACCOMPLISHED LAND TEST.SDR SWAA2013050715721Bellcrank · crackedRIGHT WING I/B MAIN FLAP I/B AND O/B AFT FLAP BELL CRANKS CHAFED AT CLEVIS ATTACH POINTS. REPAIRED BELL CRANKS IAW EA.SDR R61A201304180415Torque Tube · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING F5 FLAP TORQUE TUBE SPLINE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT WING F5 FLAP TORQUE TUBE IAW EMB 170 AMM 27-51-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR CA130422013Shaft · failed(CAN) DURING THE CHECK FLIGHT TURNING FINALS FOR LANDING, SET 10 FLAPS THEN PILOT FLYING CALLED FOR 20 FLAPS. WHEN 20 WAS SELECTED AND RUNNING HEARD A BANG/SNAP SOUND FROM THE OVERHEAD CABIN ROOF. CONTINUED THE APPROACH AND LANDING WITHOUT FURTHER INCIDENT. SDR CA130430016Rod · out of adjust(CAN) CREW REPORTED THAT ACFT ROLLED HARD RT WHEN FLAPS WERE SELECTED. ADJUSTED RT FLAP TO WALKING BEAM CLEVIS OUT 2 TURNS. TEST FLIGHT COMPLETED AND CHECKED SERVICABLE. ACFT RETURNED TO SERVICE.SDR GTIA20130412639Power Unit · faultedPRIMARY FLIGHT CONTROL SYS MALFUNCTION. FLAPS ZERO. WING TIP BRAKES LOCKED. SHOWS RT WING APPU "30CV" AT FAULT. R & R APPU IAW MM. PERFORMED OPS TEST OF FLAP SYS, TEST OK, ACFT OK FOR SERVICE.SDR UALA2013041102487Bypass Valve · failedTRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN FLAPS MOVED HYDRAULICALLY. REMOVED AND REPLACED TRAILING EDGE FLAP BYPASS VALVE IAW AMM. OPS AND LEAK CHECKED GOOD.SDR UIEA2013040900188Transmitter · failedEICAS FLAPS DRIVE, DURING RETRACTION FROM 20 TO 10. OTBD T/E FLAPS STOPPED. SEEMED LT T/E FLAP REMAINED LOWER THAN RT. EXPANDED VIEW AND STATUS T/E FLAPS INDICATED. APPROX 50-55 MIN INTO FLT. EXPANDED VIEW EXTINGUISHED AND SYS APPEARED NORMAL. DURING HOLDSDR REXA2013040800733Flap System · malfunctionedFLIGHT 3733, FLAP FAILED ON APPROACH AT 30 DEGREES. LANDED WITH NO ISSUES. PERFORMED FLAP CONTROL LEVER SELF TEST. ALL OP CHECKED GOOD IAW AMM 27-51-01-740-801.SDR CA130409002Flap System · failed(CAN) ON APPROACH THE CREW REPORTED THE FLAPS HAD FAILED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS. BY CMC FAULT CODE - 27512014ACE. FIM TASK- 27-51-00-810-802-A. FAULT ISOLATION PROCEDURE CARRIED OUT. TRANSITORY CONDISDR REXA2013040600728Bpsu · failedFLIGHT 3629, CREW REPORTED FLAPS FAILED MESSAGE IN FLIGHT ON EXTENSION, POSITION AT TIME OF FAILURE 36 DEGREES AT 160KTS, APPROXIMATELY 1 HOUR INTO FLIGHT, AND OAT 7*C. FLIGHT CONTINUED TO DESTINATION. PULLED CODES AND COMPLETED FLAP EVENT SHEET ENTER CODE.SDR REXA2013040600731Flap · malfunctionedON FLIGHT 3711 (BWI TO RDU) ON APPROACH INTO RDU RECEIVED FLAP FAIL AT 30 AT 170 KTS. AIRCRAFT LANDED SAFELY. RESET FLAPS PER OA AD27-052K AND DEFERRED PER MEL 27-50-00 FOR 10 CYLCES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIMREV44 IAW AD 2009-06-12 PARA SDR CA130410002Flap System · out of rig(CAN) ON THE CLIMBOUT, WITH FLAPS UP ACCELERATING AT 230 KTS INDICATED, FLAP HIGH SPEED WARNING SOUNDED. SLOWED TO UNDER 230 WENT AWAY. UPON FLAP SELECTION TO 20, FLAP FAIL CAUTION ON RETURN TO FIELD. RAN QRH, LANDED WITHOUT FURTHER A-DO. LEFT FLAP FAILED SDR REXA2013040100709Flap · malfunctionedON FLIGHT 3743/ (YYZ- DTW) FLAPS FAIL AT 20 DEGREES ON APPROACH INTO DTW WHILE PASSING 20 WITH A COMMAND OF 40. AIRCRAFT LANDED SAFELY. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH (H) (6)(I) AMOC DATED DECEMBER 07,2012, AN
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