JASC 2700
Service difficulty reports · 1,743
Reports filed under 2700 · Flight 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 = '2700' 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 = '2700' 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 R61A2026031100060Torque Tube · faultedFLAP FAIL EICAS MSG ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TRANSITORY CONDITION OF FLAP CONTROL SYSTEM. INSTALLED CORBAN, TORQUED, AND COTTER PINNED LT TORQUE TUBE BOLTS.SDR DALA2026030501528Computer · faultedDECLARED EMERGENCY DUE TO AN ELAC 1 + 2 PITCH FAULT DURING THE APPROACH TO ATL. CORRECTIVE ACTION: REPLACED ELAC 1 AND 2. (LP 8282220)SDR DALA2026030301466Motor · leakingSHIP 3034 - SMOKE - CREW REPORTED SMOKE FILLED THE FLIGHT DECK AND CABIN AFTER LANDING. REPORTS OF DEBRIS COMING FROM THE VENTS WAS OBSERVED. ECAM AIR PACK 1 REGULATION FAULT AFTER LANDING. POSSIBLE BIRD INGESTION WAS REPORTED BY THE TOWER. SMOKE DISSIPATED QUSDR CALA2026030314294Control Module · faultedSTAB TRIM CAUTION ON EICAS NO MESSAGE ACTIVE ON ARRIVAL , PERFORMED TEST 65 NO FAULTS OBSERVED . FOUND ONE (1) FAULT BALL ON THE LT STABILIZER TRIM, AILERON LOCKOUT MODULE, RESET SYSTEM TEST PASSED. AS A PRECAUTION WILL REPLACED LT SAM.SDR HNAA2026022400151Control Unit · faultedPTRIM BACK UP INOP IN FLIGHT AND RTF. T/S SYST3M WIRES AND CONNECTORS IAW FIM 27-43-00-810-802-A OPS CHECK GOOD COULD NOT DULICATE EICAS OR CMC MESSAGE DURING T/SPER MOC POITIVE MAINT R/R HSCU IAW AMM 27-40-01 OPS CHECK IAW AMM 27-40-00-700-802A OPS CHECK GOSDR AALA202602236941Computer · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO CLT DUE TO THE FLIGHT CREW REPORTING AN SLAT/FLAPS LOCK ON APPROACH >2 <2-3. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT.MAINTENANCE FOUND DEBRIS BETWEEN PROXIMITY SENSOR 40CV OF RIGHSDR VNAA2026021612301Control Unit · faultedRUDDER LIMITER, PITCH FEEL, SLATS FAIL, STALL FAIL, FLAPS FAIL CAUTION MSGS AFTER TAKEOFF. REMOVED AND REPLACED SFECU 1 IAW AMM 27-51-05-000/400-801. OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED AT THIS TIME. SELF TEST PASSED.SDR DALA2026021601052Servo Valve · faultedATO, AT THROTTLE UP DUE TO F/CTL ELAC 1 PITCH FAULT ECAM WARNING. RESET NORMAL AND OK TO CONTINUE, LATER IN ATL, REPLACED SERVO VALVE AT RIGHT OTBD SERVO CONTROL (34CE4). (LP 1451639, 8412055)SDR J7SA2026020600473Fce · faultedP TRIM NML FAIL CAS DISPLAYED. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKS GOOD. NO FAULTS NOTED AT THIS TIME.SDR AALA202601302286Hinge Fitting · wornAIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **ORIGINAL REPORT WAS AALA202601260827 SUBMITTTED 1/26/2026 BY TUL** MAINTENANCE REPLACED THE LEFT-HAND ELEVATORSDR AALA202601303571Hinge Fitting · wornAIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **ORIGINAL REPORT WAS AALA202601260827 SUBMITTTED 1/26/2026 BY TUL** MAINTENANCE REPLACED THE LEFT-HAND ELEVATORSDR AALA202601302510Hinge Fitting · wornAIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **ORIGINAL REPORT WAS AALA202601260827 SUBMITTTED 1/26/2026 BY TUL** MAINTENANCE REPLACED THE LEFT-HAND ELEVATORSDR AALA202601300827Hinge Fitting · wornAIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **SUPPLEMENTAL REPORT FOR AALA202601260827 SUBMITTTED 1/26/2026 BY TUL: MAINTENANCE REPLACED THE LEFT-HAND ELEVASDR DALA2026012200500Cable · corrodedFOUND CABLE 129F CORRODED. REF AMDS CARD 2000-9000-04 REMOVED AND REPLACED CABLE (1408307)SDR AALA202601121362Flt Controls · malfunctionedAIRCRAFT WAS GROUNDED, AN EMERGENCY WAS NOT DECLARED DUE TO: FLIGHT CONTROL SYSTEM-B LOW PRESSURE INDICATION LIGHT CAME ON DURING CLIMB OUT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT AUS. PERFORMED CHECK OF FLIGHT CONTROL SYSTEM-B LOW PRESSURE LIGSDR AALA202601237496Bolt · wornAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAX DUE TO THE FLIGHT CREW REPORTING THAT INFLIGHT VIBRATIONS FELT FROM ABOUT 13,000 THROUGH CLIMB OUT 30,000 FEET APPROXIMATE SPEED 340. VIBRATION WAS FELT ON LEFT SIDE ON BOTH RUDDSDR JIKA2026012301Trim System · out of alignmentDURING CLIMB, THE FLIGHT CREW NOTED THAT THE AIRCRAFT ROLLED TO THE LEFT AND REQUIRED FULL INPUT TO LEVEL OFF THE WINGS. THE CREW CALLED IT IN, AND AIR RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM, CHECKED ALL FLIGHT CONTROL CABLES FORSDR AALA202512296931Flt Controls · malfunctionedAIRCRAFT WAS NOT GROUNDED: WHILE DESCENDING IN VNAV FROM FL280 TO FL 220 THE AIRCRAFT DID AN UNCOMMANDED LEVEL OFF AT FL 240 (THERE WERE NO RESTRICTIONS TO MAKE THE PLANE LEVEL OFF). LATER IN THE FLIGHT WHEN AT FL220 TRYING TO DESCEND TO 11000FT, PASSING THROUSDR J7SA2025120500464Fce · faultedWHILE DOING THE FLIGHT CONTROL CHECK AFTER STARTUP, GND SPOILER FAIL CAS. REPLACED FCE #2 IAW EMB 505 AMM TASK 27-03-01-400-801. RIGGING AND OPS CHECK SATISFACTORY AT THIS TIME.SDR CALA2025120511815Trim System · faultedUNSCHED STAB TRIM EICAS MSG ON T/O ROLL APPROX 65KTS. T/O ABORTE D. RTG UNSHED STAB TRIM T/S PFMD IAW FIM 22-05 FAULT TREE 809. FCC COMMUNICATION AND STAB TRIM MSG ON MCDP CLEARED. CHK SATIS. WORKED TWO FIM TASKS "UNSCHED STAB TRIM" PROBLEMS REF 27-09 FAULT TRSDR DALA2025120408847Computer · inoperativeAIRCRAFT ROLLED UP TO 15 DEGREES RT UNCOMMANDED, AWAY FROM FLIGHT DIRECTOR WHEN SPEEDBRAKES DEPLOYED AT FLAPS 1, 210 KNOTS , ACFT ROLLED ABOUT 15 DEGREES LT WHEN SPEEDBRAKES DEPLOYED AT 180 KNOT, FLAPS 2. LAST LEG ECAM REPORT SHOWS NO FAULTS. AFS/LAST LEG REPSDR AALA202512047099Flt Controls · flutterAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT ON CLIMB THRU FL 200 AT 325 IT'S INDICATED WE GOT FLIGHT CONTROL FLUTTER. WE BROUGHT SPEED BACK AND IT WENT AWAY. FLIGHT ATTENDANTS FELT IT AS WELL. (OPEN)SDR YENA2025120101133Computer · malfunctionedFLT#1970, BOS-PHX. WHILE DESCENDING AND SLOWING TO 210 KTS AT 9000 FEET, SELECTED FLAPS 1 AND RECEIVED ELAC 1 FAULT. PLANE ROLLED APPROX 15 DEGREES RIGHT. DISCONNECTED A/P AND HAND FLEW PLANE TO NORMAL LANDING; REF LG # 4520823 ITEM #2, # 4520824 ITEM #1 FOSDR J7SA2025111000458Fce · faultedCREW RECEIVED SPOILER FAULT ON GEAR RETRACTION. AIRCRAFT LANDED WITHOUT INCIDENT AT PLANNED DESTINATION. REPLACED #2 FCE IAW AMM 27-03-01. RIG AND OPERATIONAL CHECKS GOOD.SDR YENA2025110301080Computer · failedFLT#1230, CUN-EWR. (AIRCRAFT DIVERTED TO TPA) "F/CTL ELAC 2 PITCH FAULT AIRCRAFT PITCHED DOWN UNCOMMANDED IN CRUISE FLIGHT. AUTOPILOT STAYED ON; PERFORMED INTEROGGATION OF FCDC SYS #2 IAW TSM 27-00-00-810-801-A. ACCORDING TO DFDR REPORTS, TECH SUPPORT IDENTIFISDR CALA2025103010737Computer · failedFLIGHT CONTROLS TOO HARD IN FLIGHT.DEBRIEF CREW ON ARRIVAL FLIGHT CREW REPORTED ON TAKE OFF THE ELEVATOR WAS HARD TO PULL BACK ALSO THE AILERONS AND RUDDER HARDER THAN NORMAL TO MOVE. NO EICAS MSG OR OTHER FAULTS SHOWING IN FLT OR ON GND FOLLOWING CONSULTATIONSDR 3M3A13040017Actuator · malfunctionedPILOT REPORTED CYCLIC JERKED LEFT WHILE IN FORWARD FLIGHT AND FELT AS IF TRIM WAS IN FULL LEFT POSITION. UPON INITIAL INSPECTION OF AIRCRAFT PERFORMED A FUNCTIONAL CHECK OF TRIM ACTUATORS. CONFIRMED TRIM MOTOR TO BE CORRECTLY CORRESPONDING TO INPUTS MADE TO CYSDR CALA2025102810668Speed Brake · faultedSPEEDBRAKE DO NOT ARM LIGHT ILLUMINATED AT 70KTS DURING TAKEOFF. REQ MEL 2707F. VERIFIED MANUAL SPEEDBRAKE DEPLOYED AND STOWED. OPENED AND COLLARED C/B PER THE MEL. PLACARD APPLIED. PERFORMED FIM TASK 27-62 TASK 802 STEP E (2) . NO FURTHER ACTION REQUIRED . NSDR DXTA2025102005335Warning Message · illuminatedNO T/O CONFIG RED CAS APPEARED IMMEDIATELY UPON TAKEOFF (NORMAL AURAL TAKEOFF OK ON THE GROUND). FLAP FAIL YELLOW CAS, PTRIM BKP FAIL YELLOW CAS, SWPS FAULT YELLOW CAS, SPOILER FAULT WHITE CAS, & YELLOW X'S ON FLAP INDICATORS ALL UPON FLAP RETRACTION. REPAIRSDR YENA2025101701043Secu · failedFLT#373, BOS-AUA. "F/CTL/SEC FAULT ALSO WAS AN ELECTRIC BURING SMELL FOR 5 MIN ; REMOVED AND REPLACED SEC 2 IAW AMM 27-94-34 OPS GOOD AT THIS TIME."SDR WX0A2025101332595Actuator · faulted(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) ON ROTATION HAD A BRIEF MASTER CAUTION. SHORTLY AFTER, LOST ALL MAIN ELECTRIC STAB TRIM. AP WOULD NOT TRIM. WINDOWS WERE BOTH AMBER. INTERMITTENT SPEED TRIM FAIL LIGHT. PERFORMED SPEED TRIM IN FLT SYS TEST IAW IFIM 22SDR J7SA2025111000461Fce · faultedPTRIM BKP FAIL CAUTION CAS ILLUMINATED ON ROTATION; REMAINED ON AFTER POWER CYCLE AT DESTINATION. REPLACED FCE IAW AMM 27-03-01. PERFORMED FLAP SYSTEM ELECTRONIC RIGGING. OPERATIONAL TESTS SATISFACTORY.SDR SWIA2025F01329Jackscrew · damagedUPON INSPECTION, FOUND DAMAGE TO THE HSTA RH SCREW JACK TOP ATTACHMENT AND BACKUP STRUCTURE IN MULTIPLE AREAS.DAMAGE UPPER CENTER AREA OF MATING SURFACE "FOOT" MEASURES 0.25" L X 0.062" W BY 0.0010 DEEPDAMAGE ON UPPER RH CORNER OF MATING SURFACE "FOOT" MEASURESDR SWIA2025F01328Jackscrew · damagedUPON INSPECTION, FOUND DAMAGE TO THE HSTA RH SCREW JACK TOP ATTACHMENT FITTING ASSY.DAMGE ON THE OTBD FWD SIDE NEAR THE MOUNT HOLES FOR THE RH UPPER FITTING TIE ROD MEASURING 0.35" L X 0.125 " W X 0.03125" D. (FILED CLOSED)COMPLIED WITH REO 670-55-11-425, REPSDR SWIA2025F01327Jackscrew · damagedUPON INSPECTION, FOUND DAMAGE TO THE HSTA LH SCREW JACK FITTING AND BACKUP STRUCTURE IN MULTIPLE AREAS.UPPER MOUNTING FACE:DENT/GOUGE #1 0.5"L X 0.1"WDENT/GOUGE #2 0.1"L X 0.1" WDENT/GOUGE #3 0.4"L X 0.15"WDENT/GOUGE #4 0.65"L X 0.2" WSCRATCH #1 1.55"L X 0.01"SDR CALA2025091508919Control Cable · out of limitsAILERON SLOW RESPONSE TO CONTOL WHEEL MOVEMENT, HYD POWER ON RT AILERON NO RESPONSE TIL 2-3 UNITS INPUT. THEN BINDING. LT SIDE NO TENSION CONTROL WHEEL FORCE SLIGHTLY HEAVY WHEN TURNING RT USING EITHER CONTROL WHEEL,WHETHER HYD ON OR OFF. CYCLED CONTROL WHEELSDR CALA2025090908673Indication Sys · malfunctionedWHEN GEAR RAISED ALL NORMAL INDICATIONS BUT SPEED TAPE STAYED AT 270 EVEN W/ GEAR CYCLED AFTER TAKEOFF, RAISED GEAR & THEN FLAPS PER NORMAL PROCEDURES. ALL INDICATORS NORMAL FOR GEAR & FLAPS SHOWING FULLY RAISED OR STOWED. HOWEVER THE SPEED TAPE WHEN RAISING FSDR AALA202509028008Elevator · excess playAIRCRAFT WAS GROUNDED: CLIMBING THRU FL230 WE HAD A VIBRATION FOR ABOUT 10-15 SECONDS, FLIGHT CREW REPORTED THAT THE AIRCRAFT WAS GOING THRU A LITTLE WIND SHIFT AND CLIMBING WITH COST INDEX 70 AND M.78. ALL INDICATIONS ON ECAM WAS NORMAL. WE THEN ENCOUNTERED ISDR AALA202509024542Elevator · excess playAIRCRAFT WAS GROUNDED: CLIMBING THRU FL230 WE HAD A VIBRATION FOR ABOUT 10-15 SECONDS, FLIGHT CREW REPORTED THAT THE AIRCRAFT WAS GOING THRU A LITTLE WIND SHIFT AND CLIMBING WITH COST INDEX 70 AND M.78. ALL INDICATIONS ON ECAM WAS NORMAL. WE THEN ENCOUNTERED ISDR CALA2025082808235Unknown · abnormalDURING CLIMB HAD VERTICAL BOUNCING. STARTED AFTER FLAPS UP, STOPPED AT 1ST LE VELOFF, STARTED NXT CL DEBRIEFED CREW THERE WAS CONSTANT VERTICAL BOUNCING DURING CLIMB LESS AT SLOWER SPEED AND GOT WORSE THE FASTER THEY CLIMBED FLAPS UP. CREW TRIED TO ISOLATE SDR DXTA2025082604714Flt Controls · faultedCLEARED FOR VISUAL APPROACH, DISCONNECTED AUTOPILOT ON LEFT BASE LEG (YD AND AT STILL ENGAGED). AT APRX 1800FT INITIATED A LT TURN & NOSE DOWN PITCH WITH YOKE. ACFT UNRESPONSIVE & WOULDN'T ROLL OR PITCH. ACFT FELT SLUGGISH. CHECKED SPEED, ASKED FO IF CONFIGURESDR J7SA2025082600454Fce · faultedDIVERTED DUE TO PTRIM NML FAIL CAS ON CLIMBOUT. CREW FOLLOWED THE QRH, DISENGAGED THE AUTOPILOT, AND USED BACKUP PITCH TRIM BEFORE LANDING WITHOUT INCIDENT. NO FAULTS NOTED DURING INITIAL OPS CHECKS. SWAPPED FCE 1 AND FCE 2. FLAP FAIL CAS MESSAGE POSTED AFTER SDR J7SA2025082600453Fce · faultedAP FAIL CAS FOLLOWED BY SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT CAS ILLUMINATED WHILE CRUISING AT FL450. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. DURING DESCENT, THE SPEED TAPE DISPLAYED A CONTINUOUS MAX SPEED CAUTION UNTIL 3000 FT DSDR YENA2025081800844Computer · failedFLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTSSDR YENA2025081800843Computer · failedFLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTSSDR YENA2025081900851Computer · failedFLT #2144, PBI-EWR. DURING CLIMBOUT 310KTS FL260 SHIMMY SHUDDER FELT LIGHT INTONSITY WITH MANUAL ROLL INPUTS VIBRATION STOPED RETURED WITH AP ON DIMINISHED CLIMBING THROUGH FL330 SURVEY FORM COMPLETED DFDR PUSHED; INSPECTED AILERON SERVO AND HINGE BEARINGS FORSDR YENA2025081900850Computer · failedFLT #2144, PBI-EWR. DURING CLIMBOUT 310KTS FL260 SHIMMY SHUDDER FELT LIGHT INTONSITY WITH MANUAL ROLL INPUTS VIBRATION STOPED RETURED WITH AP ON DIMINISHED CLIMBING THROUGH FL330 SURVEY FORM COMPLETED DFDR PUSHED; INSPECTED AILERON SERVO AND HINGE BEARINGS FORSDR CALA2025081407729Sensor · faultedSTABILIZER CONTROL CHANNEL (L2) HAS BEEN DEFERRED IN COMPLIANCE WITH MEL CARD 27105. DEACTIVATED THE INOPERATIVE STAB CONTROL CHANNEL AS REQUIRED ON CARD 27105, IAW AMM DDG 27-41-03. INSTALLED INOPERATIVE STICKER ADJACENT TO AFFECTED L2 STAB CUTOUT SWITCH ONSDR SWIA2025F01368Jackscrew · gougedH-STAB RH SCREW JACK FITTING NUMEROUS GOUGES ON INBOARD SIDE (MARKED RED) (C-CHECK RO 09/24/2025)REPAIRED NUMEROUS GOUGES ON INBOARD SIDE H-STAB RH SCREW JACK FITTING AT MARKED LOCATIONS REF CRJ200 SRM 51-12-00 REV 39, DATED 10/21 AND REO 601R-55-11-803 REV--SDR SWIA2025F01367Jackscrew · gougedH-STAB LH SCREW JACK FITTING NUMEROUS GOUGES ON INBOARD SIDE (MARKED RED) (C-CHECK RO 09/24/2025)REPAIRED NUMEROUS GOUGES ON INBOARD SIDE H-STAB LH SCREW JACK FITTING AT MARKED LOCATIONS REF CRJ200 SRM 51-12-00 REV 39, DATED 10/21 AND REO 601R-55-11-803 REV--
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