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 REXA201000004Fcu · failedFLAPS FAIL AT ZERO DURING CRUISE FLIGHT. FLAPS 0-0 M.73 IAS 270 1 THS 424.FL310 SAT -49 DEGREES C.1825-30Z. PERFORMED T/S PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) PER AMOC DATED MARCH 27,2009 AND PAAD27-052F. FOUND CODES 1 5 1A,152A PROBABLE CAUSDR MASA2010010900037Bpsu · malfunctionedASH FLT 2982 PHX TO SLC. FLAPS FAILED DURING RETRACTION OUT OF PHX. FLIGHT CREW DECLARED AN EMERGENCY ON APPROACH INTO SLC. FLAPS WERE RESET W/ FLIGHT CREW AND MX REPLACED NR 1 BPSU.SDR MASA2010010900036Bpsu · malfunctionedASH FLT 2818 DSM-RON. FLAPS FAILED AT ZERO ON EXTENSION IN FLIGHT. RESET THE FLAPS AND REPLACED THE RT BPSU.SDR CA100128001Bpsu · malfunctioned(CAN) FLT CREW REPORTED FLAP FAIL AT 8 DEG WHEN FLAP LEVER WAS MOVED TO 0 DEG AFTER TAKEOFF FROM. ACFT RETURNED TO GROUND AND LANDED OVERWEIGHT BUT WITHOUT INCIDENT. USING AMM AND FIM, MX R & R THE RT BPSU. CHECKS WERE MADE AND AN OVERWEIGHT LANDING INSP WAS SDR VNAA2010011400005Bpsu · failedCREW REPORTED FLAPS FAILED AT 8° WHEN THE FLAP LEVER WAS MOVED TO 0° AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED OVERWEIGHT, BUT WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL, MAINTENANCE REMOVED AND REPLASDR ASOA201000021Flap System · failedRECEIVED FLAP FAIL CAUTION MESSAGE DURING APPROACH. FLAPS FAILED AT ZERO. (EMERGENCY DECLARED) COMPLIED WITH EC/TC AD 2009-06-12.SDR REXA201000001Bpsu · failedFLAPS FAIL CAUTION MESSAGE, FLAPS FAIL AT 20 DEGS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). PER AMOC DATED MARCH 27 2009 AND PA AD27-052F. REMOVED AND REPLACED LT BPSU IAW CRJ AMM 27-51-10. RIGGED LT BPSU ISDR COMA2010010250003Flap · malfunctionedRECEIVED A FLAP FAIL CAUTION DURING YYZ APPROACH, CREW PERFORMED AN EMERGENCY DESCENT AND DECLARED AN EMERGENCY. COMPLIED WITH AD 2009-06-12 PARAGRAPHS H6 & H7: MAINTENANCE FOLLOWING A FLAP FAILURE USING FIM 27-50-00. TASK CARD SI-2-27-50-00.SDR COMA2010010250001Flap · malfunctionedRECEIVED A FLAP FAIL CAUTION DURING DTW APPROACH, CREW PERFORMED AN EMERGENCY DESCENT AND DECLARED AN EMERGENCY. COMPLIED WITH AD 2009-06-12 PARAGRAPHS H6 & H7: MAINTENANCE FOLLOWING A FLAP FAILURE USING FIM 27-50-00. TASK CARD SI-2-27-50-00.SDR CA100129001Fcu · malfunctioned(CAN) FLAP FAIL AT 12 DEG DURING RETRACTION AFTER TAKEOFF. UNSCHEDULED LANDING, ABNORMAL LANDING CONFIG, MX R & R THE FECU. CHECKS WERE CARRIED OUT IAW THE AMM. ACFT WAS RELEASED FOR SERVICE.SDR VNAA2010010600003Ecu · failedCREW REPORTED FLAPS FAILED ON RETRACTION AT 12°. AIRCRAFT RETURNED TO PNS LANDING WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. CHECKS WERE MADE PER THE SDR CA091231003Drive Unit · failed(CAN) CREW SELECTED FLAP 45 AND FOUND THAT THE FLAPS STOPPED AND STAYED AT 30 DEGREES. THIS WAS DISCOVERED ON APPROACH AT APPROX 2000 FT. THE CREW OVERSHOT DUE TO A SMALL TAILWIND ON RUNWAY 07 AND THEN GOT THEMSELVES RE-ESTABLISHED FOR THE APPROACH ONTO RUNWASDR QXEA2009010401099Flap System · malfunctionedRECEIVED A FLAP POWER CAUTION MESSAGE. PERFORMED A ZERO FLAP LANDING WITHOUT INCIDENT. PERFORMED RESET PROCEDURE IAW DH8-400-SL-27-002A. NO DEFECTS NOTED. NO FAULTS NOTED IN CDS. SENT CDS INFO TO TECH FOR ANALYSIS. RETURNED TO SERVICE. NO PARTS REPLACEDSDR MASA2009122800126Bpsu · malfunctionedFLAPS FAIL AT 5 DEG 8 SELECTED. WILL FERRY TO PHX FOR REPAIRS; R2 RT BPSU & C/W EO.SDR CA100104005Spindle · cracked(CAN) SPINDLE BROKE IN AREA OF AD 2003-24-08 PRIOR TO THE INSP THRESHOLD OF 3000C. UNIT HAD BEEN O/H, FAILED PART IS CURRENTLY WITH QA AND WILL BE SHIPPED TO MFG UNLESS OTHERWISE INSTRUCTED. FLAP SPINDLE CRACK OCCURRED AT CRITICAL "A" AREA SPECIFIED IN ASB 73SDR MASA2009122700363Flap · failedASH FLT 2721 PHX-LAX-SBA. AIRCRAFT DIVERTED TO LAX EN ROUTE FROM PHX TO SBA DUE TO FLAPS FAIL. CREW DECLARED AN EMERGENCY BUT DID NOT BRACE PASSENGERS. PERFORMED RESET PROCEDURE WITH THE CREW AND PLACED THE EO COMPLIANCE ON MEL.SDR MASA2009122500360Flap · failedASH FLIGHT 2721 PHX - SBA DECLARED AN EMERGENCY AND DIVERTED TO BFL FOR A FLAPS FAIL CAUTION MESSAGE IN FLIGHT WHEN THE FLAPS WERE EXTENDED FOR LANDING. THE AIRCRAFT LANDED IN BLF WITHOUT INCIDENT. THE FLAPS FAIL RESET.SDR COMA2009122350305Unknown · malfunctionedDURING PHL APPROACH WHEN FLAPS WERE SELECTED TO 20 DEGREES A ROLLING MOTION WAS FELT IN THE AIRCRAFT, CREW DECLARED AN EMERGENCY, FLIGHT LANDED WITHOUT INCIDENT. PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM, NO DEFECTED NOTED.SDR U5QA06022Flap · malfunctionedON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.SDR U5QA06021AAFlap System · malfunctionedON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.SDR SWIA200923323Flap · failedFLAPS FAILED AT 0° ON EXTENSION. TOWER DECLARED EMERGENCY. (FLT 6154) RESET PER FORM M-267. OPERATIONAL CHECK NORMAL.SDR MASA2009121800124Pdu · malfunctionedFLAPS FAILED AT 22 ON FINAL. R2 PDU.SDR UALA2009122103951Switch · out of positionT/E FLAP DISAGREE. FLAP OVERRIDE SWITCH IN OVERRIDE. REPOSITIONED SWITCH. PERFORMED FSEU BIT. NO FAULTS. RAN FLAPS ON GROUND, NO FAULTS. LUBED TRAILING FLAPS. SYS GROUND CKS OKAY. NO PREVIOUS HISTORY.SDR 2010FA0000031Switch · crackedOWNER COMPLAINT - WHEN FLAPS "DOWN" WAS SELECTED, SPARKS CAME OUT AROUND HANDLE. FOUND MICROSWITCH PN S1906-1, BROKEN IN HALF, AND SHORTING OUT ON MOUNTING BRACKET. SWITCH BELIEVED TO BE ORIGINAL. REPLACED SWITCH, ALL OPS NORMAL.SDR USAA20091216BB163Transformer · faultyCLT FLT 1728 EN ROUTE MCO TO CLT. DURING APPROACH, TRAILING EDGE AND LEADING EDGE FLAPS FAILED TO EXTEND NORMALLY. LEADING EDGE EXTENDED BY ALTERNATE. TRAILING EDGE FLAPS NEVER INDICATED MOVEMENT, EVEN AT ALTERNATE 15 FLAP GAUGE NEVER MOVED. TRAILING EDGESDR ASOA200901380Flap · failedFLAP FAIL AT 0 DEGREES ON APPROACH FWA, FOLLOWED QRH FOR 0 FLAPS LANDING (EMERGENCY DECLARED).SDR CA091215004Drive Shaft · sheared(CAN) RT OB FLAP WOULD NOT MOVE WHEN SELECTED. MAINTENANCE DISCOVERED THE RT OB FLEXIBLE FLAP DRIVE SHAFT SEVERLY CORRODED AND SHEARED OF. THIS IS THE SECOND INSTANCE OF FLAP FLEXIBLE DRIVE SHAFTS SEVERLY CORRODED CAUSING FAILURE.SDR ASOA200901374Flap System · malfunctionedON APPROACH FLAPS FAIL AT 0 DEGREES WHEN SELECTING FLAPS 8 (EMERGENCY DECLARED) C/W EC TC AP 2009-06-12 ACFT OK FOR SVC. CLOSED.SDR C77A214342Bolt · misinstalledFLAP FAIL IN FLIGHT DURING RETRACTION. PRELIMINARY FINDINGS WERE THE TORQUE TUBE F6 CAME OUT OF INBD SIDE OF THE 2R FLAP ACTUATOR. THE SAFETY IS A BOLT AND WAS FOUND TO BE IMPROPERLY INSTALLED. TORQUE TUBE SLIDES OVER THE SPLINE SIDE OF THE ACTUATOR AND IS SECSDR MASA2009120800122Flap · lack of lubeFLAPS FAIL CAUTION. LUBE & C/W EO OPS CHECK GOOD.SDR REXA200900130Fcu · failedFLAPS FAILED AT 2 ON RETRACTION 120 KNOTS 3HR 10MIN 1C. REMOVED AND REPLACED FECU IAW AMM 27-51-05 OPC NORMAL. PERFORMED TS PER BOMBARDIER FIM REV 3 9 IAW AD 2009-06-12 PARAGRAPH H 6 I PER AMOC DATED MAR 27 2009 & PA AD 27-05 2F 860D100-18ABCD.SDR FDEA200912084385Actuator · malfunctionedDURING T/O AND FLAP RETRACTION AMBER FLAP LIGHT REMAINED ON AT FLAPS 2. SLATS 2367 WERE OUT AND THE AMBER LIGHT UNDER NR 6 SLAT POS ON SO PANEL WAS ON. ATTEMPTED TO RECTIFY WITH THE QRH. NO LUCK. PUT FLAPS BACK TO 5 AND LANDED AT BIL IAW GOC DIRECTIVES. RASDR ASOA200901360Transmitter · failedAFTER TAKEOFF AT FLAP RETRACTION, LT FLAP FROZE AT 4 DEGREES FOR APPROX 5-8 MINUTES. NO FLAP FAIL MSG RCVD. BUT ACFT HAD A RT ROLL TENDENCY. FLAP DID EVENTUALLY RETRACT WE DID NOT OPERATE FLAPS FURTHER AND LANDED FLAPS 0 DEGREES WITH TOUCHDOWN OF LESS THAN SDR SIMA200934103Flap System · malfunctionedON FLIGHT 3579 ON DESCENT THE CAPTAIN REPORTED THAT WHEN SELECTING FLAPS 9, RECEIVED A FLAP FAIL MESSAGE IMMEDIATELY. THE FLAPS DID NOT MOVE FROM THE ZERO POSITION. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. IT WAS NOT AN OVERWEIGHT LANDSDR MASA2009120500121Bpsu · malfunctionedFLAPS FAIL CAUTION AT 0 IN FLIGHT. PLACED ON MEL THEN REPLACED RT BPSU.SDR SIMA200934303Flap System · malfunctionedDURING FLIGHT 4546 WHILE ON APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESSAGE INDICATED THAT THE FLAPS WERE ON 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP RESET. PESDR MYWA09058Flap · malfunctionedETOPS SIGNIFICANT SYSTEM - FLAPS STUCK AT FLAPS 2 DURING APPROACH WITH FLAP HANDLE AT 30 SETTING. FLAPS REMAINED AT 2 AFTER FLAP HANDLE WAS RETRACTED FOR GO AROUND. ALTERNATE FLAP METHOD USED.SDR ASOA200901342Flap System · failedFLAPS FAIL AT 30 DEG ON APPROACH (EMERGENCY DECLARED).SDR SIMA200933803Brake · failedDURING FLIGHT 4485 ON APPROACH THE CREW REPORTED A FLAP FAIL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW LEFT FLAP TRANSMISSION BRAKE IAW EMB AMM 27-51-01. OPERATIONAL CHECK WAS GOOD. SDR ASOA200901341Flap System · failedFLAPS FAILED IN FLIGHT AT 0. FLAPS WERE RETRACTED AFTER TAKEOFF -THATS WHEN THEY FAILED AT 0. (EMERGENCY DECLARED) PERFORMED GROUND MX TEST IAW FIM 27-50-00 PARAGRAPH 21. ALL LRU'S PASSED. OPERATED FLAPS UP AND DOWN NO FAULT MESSAGES NOTED AT THIS TIME.SDR CA091202006Flap System · malfunctioned(CAN) YYC TO SEA START OF CRUISE FLAP FAILURE CREW RETURNED TO YYC. DECLARED EMERGENCY AND LANDED WITH FLAPS 0 WITHOUT INCIDENT. (TC NR 20091202006)SDR CA091202007Flap System · warning message(CAN) YYZ TO SEA ON APPROACH FLAP FAIL MESSAGE, GO AROUND CARRIED OUT AND EMERGENCY DECLARED. NORMAL LANDING FLAPS 1 (TC NR 20091202007)SDR VNAA2009112400005Control Lever · failedCREW REPORTED FLAP FAIL AMBER CAUTION MESSAGE IN FLT OCCURRED WHEN SELECTING FLAPS TO 20 DEG FLAPS FAIL AT 8 DEG. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE PERFORMED FAULT ISOLATION OF FLAP SYSTEM USING THE AIRCRAFT FAULT ISOLATION MANUAL. MAINTESDR VNAA2009112300004Fcu · failedCREW REPORTED FLAPS FAIL AT 8°. AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. MX PERFORMED FAULT ISOLATION OF FLAP SYS USING THE ACFT FAULT ISOLATION MANUAL. MX REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW THE ACFT MM. CHECKS WERE MADE IAW THE ACFSDR HALA2009111900533Electronic Unit · inoperativeETOPS SIGNIFICANT SYS - FLAP/SLAT ELECTRIC STATUS MESSAGE DISPLAYED. FOUND FLAP SLAT ELECTRIC UNIT INOP- UNABLE TO BITE. REMOVED AND REPLACED FLAP SLAT ELECTRONIC UNIT IAW AMM 27-51-01-024-001. OPS CHECK GOOD.SDR CA091130003Shaft · broken(CAN) NR 3 FLAP FLEX SHAFT (RT INBD) SHEARED CAUSING SPLIT FLAP PROTECTION TO SHUTOFF FLAP SYSTEM. (TC NR 20091130003)SDR TRBA2009111Flap System · malfunctionedFLAP UNLK WARNING ON SHORT FINAL AT PUJ. FLAP GAUGE SHOWED FLAPS RETRACTED TO AROUND 20 DEGREES. EMERGENCY DECLARED AND GO AROUND PROCEDURE APPLIED. LANDED WITH 0 FLAPS IAW AOM. ACFT INSPECTED FOR FERRY FLIGHT BAC. COMPLIED WITH BLEEDING OF HYD FLAPS CONTRSDR USAA2009111993171Strut · out of rigFLT 42 - PHX - EMERGENCY LANDING - CAPTAIN RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT WHILE ATTEMPTING TO LAND. PERFORMED A MISSED APPROACH, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE FAULT BUT FOUND RT FLAP ISDR QMLA2009111709042Computer · intermittentFLAPS SET AT 15 DEGREES FOR NORMAL TAKEOFF ACCORDING TO PC12 SOP. AFTER LIFTOFF AND PASSING 100 KNOTS, FLAPS WERE SELECTED TO ZERO. SHORTLY AFTER MOVING FLAP HANDLE, SINGLE CHIME SOUNDED AND "FLAPS" AND "PUSHER" CAWS LIGHTS ILLUMINATED. LOOKED AT FLAP POSITSDR FDEA200911133948Actuator · leakingCOMPLETE LOSS OF SYS A HYDRAULICS DURING FLAP RETRACTION. FOUND ACTUATOR ABOVE TAIL SKID LEAKING OUT OF THE HSG. ORDERING NEW ACTUATOR. R&R TAIL SKID ACTUATOR PER MM 32-71-012-4 AND HAD TO ADJUST ACTUATOR PER MM 32-71- 001-5 LEAK AND OPS CKS GOOD. RAN NR 1
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