JASC 2797
Service difficulty reports · 920
Reports filed under 2797 · Flight Control System Wiring, 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 = '2797' 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 = '2797' 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 SWAA2018061122645Wire · shortedDIVERSION/DECLARED EMERGENCY, TRAILING EDGE FLAP ASYMMETRY. GOING THROUGH FL 200 FIRST OFFICER NOTICED RIGHT FLAP INDICATOR AT 0 AND LEFT FLAP INDICATOR AT 15'. R&R WIRE PER WDM.SDR EVGR201806080001Wire · disconnectedEXPERIENCED A STABILIZER TRIM RUNAWAY AFTER LANDING AND SHUTDOWN. COULD HEAR THE STABILIZER TRIM MOTOR RUNNING CONTINUOUSLY AND THAT THE INDICATOR IN THE COCKPIT SHOWED NOSE DOWN. AFTER TROUBLESHOOTING, DISCONNECTED THE TRIM CONTROL SWITCHES ON EACH OF THESDR R61A201803280416Connector · dirtyFLAP FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS, CLEANED THE CONNECTORS, OPS CHECKED GOOD.SDR HNAA2018030900055Connector · contaminatedEICAS SPOILER FAILED MESSAGE WITH SPOILER DEPLOYMENT, DURING CLIMB OUT. HAPPENED AROUND 3000 FEET, SPOILERS FELT DEPLOYED, CIRCUIT BREAKERS WERE PULLED IAW QRH. TROUBLESHOT IAW FIM 27-63-00-810-802-A AND DETERMINED TO BE TRANSITORY CONDITION. PERFORMED SDR DALA2018021400883Wire · shortedDURING SLAT RETRACTION, AFTER TAKEOFF RECEIVED A PSEU FAIL CAUTION INDICATION. DURING APPROACH, EXTENSION OF SLATS, DOWN ARROW STAYED ON, THOUGH INTERMITTENT. PERFORMED A NO FLAP, NO SLAT LANDING IAW QRH. REPLACED THE LT SLAT A SENSOR D1-65 IAW AMM 27-84 WSDR AALA20180214011Connector · contaminatedDECLARED EMERGENCY ON APPROACH, TRAILING FLAPS STOPPED AT 5, ALTERNATE EXTENSION IAW QRH FLAPS STOPPED AT 12. LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. PERFORMED PSEU BITE TEST IAW FRM/FIM 32-09-00-810-801, SHOWED FAULT MESSAGES 32-62009 & 32-62010. SDR HALA2018013000023Connector · damagedATB DURING FL410 CRUISE, RECEIVED A F/CT ELEVATOR SERVO FAULT ON ECAM. REMOVED AND REPLACED THE FLT CONTROL PRIM 1 PB IAW ESPM 20-45-11. OPS CHECKED GOOD IAW AMM 27-96-00 AND CONTINUITY CHECK. FOUND PIN C ON B CONNECTOR LOOSE TENSION. REMOVED AND REPLACEDSDR SWAA2019011428405Wire · damagedDECLARED EMERGENCY, AFTER TAKEOFF THE FLAPS DID NOT RETRACT. FLAPS REMAINED AT 5 DEGREES. FOUND CIRCUIT BREAKER P6-2-A-12 POPPED. RESET CIRCUIT BREAKER AND IT IMMEDIATELY TRIPPED AGAIN. REPAIRED WIRING AT NR 3 FLAP SKEW SENSOR PER SWPM.SDR SWIA201844126Wire Harness · failedFLAPS FAILED ENROUTE. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE RT BPSU WIRE HARNESS IAW AMM. CYCLED FLAPS NUMEROUS TIMES WITHOUT FAILURE. OPS CHECKED GOOD.SDR DALA2017112908378Connector · dirtyATB DUE TO L/E ASYMMETRY MSG ILLUMINATED. NO FLIGHT CONTROL ISSUES. CREW DECLARED AN EMERGENCY AND LANDED APPROXIMATELY 66,000 LBS. OVER WEIGHT. BITE OF PSEU SHOWED ONLY SENSOR S277 NR 2 SLAT OB AT FAULT. NO OTHER FAULTS NOTED. PERFORMED W/C 2780-7590 FOUNSDR AALA201711169022Connector · not seatedTHE AIRCRAFT WAS GROUNDED. AFTER TAKEOFF WHEN RETRACTING FLAPS FROM 5 TO 1, FLAPS SPLIT BETWEEN 1 AND 2, LEFT FLAP STOPPED AT 1.8, RIGHT FLAP AT 1.2. RAN TRAILING EDGE FLAP ASYMMETRY QRH PROCEDURE. THE FERRY FLIGHT CONTINUED TO TUL, DECLARED AN EMERGENCY, ANSDR 2018FA0000020Wire Harness · chafedDURING DECENT, SPEED BRAKE PANELS FAILED TO DEPLOY. UPON TROUBLE-SHOOTING FOUND AFT WING FLAP WELL SPEED BRAKE WIRING BUNDLE PROTECTIVE SLEEVE CHAFED THROUGH ALONG WITH THE WIRING RESULTING IN AN ELECTRICALLY SHORTED SYSTEM AT WIRE-TIE ANCHOR POINTS. THIS ISSUSDR AALA201711069044Wire · damagedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ACCOUNT FLAP/SLAT ASYMMETRY. LANDING UNEVENTFUL. AIRCRAFT FERRIED. REMOVED AND REPLACED 4 DAMAGED WIRES ON THE LEFT WING ROOT PER CHAP20N 20-10-11. OPERATIONAL CHECK GOOD. SEE ALSO AALA201710279035, AALA2017110SDR AALA201711069043Wire · damagedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ACCOUNT FLAP/SLAT ASYMMETRY. LANDING UNEVENTFUL. AIRCRAFT FERRIED. REMOVED AND REPLACED 4 DAMAGED WIRES ON THE LEFT WING ROOT PER CHAP20N 20-10-11. OPERATIONAL CHECK GOOD. SEE ALSO AALA201710279035, AALA2017110SDR AALA201711069042Wire · damagedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ACCOUNT FLAP/SLAT ASYMMETRY. LANDING UNEVENTFUL. AIRCRAFT FERRIED. REMOVED AND REPLACED 4 DAMAGED WIRES ON THE LEFT WING ROOT PER CHAP20N 20-10-11. OPERATIONAL CHECK GOOD. SEE ALSO AALA201710279035, AALA2017110SDR JIKA2017100301Wire · looseTHE PILOT REPORTED, DURING APPROACH, SELECTED THE LANDING GEAR DOWN AND RECEIVED A THREE GREEN DOWN AND LOCKED INDICATION, WHEN SELECTED THE FLAPS TO FULL THE LANDING GEAR SELECTOR HANDLE ILLUMINATED, INDICATING A GEAR IN TRANSIT CONDITION. FOLLOWED PROC6EDSDR DALA2017092207035Connector · damagedWHILE SLOWING FOR APPROACH ON A DOWNWIND, FLAP LEVER GAUGE REMAINED LESS THAN 1 DEGREE WITH FLAP HANDLE AT 5 DEGREES. RAN TRAILING EDGE FLAP DISAGREE CHECKLIST AND LANDED WITH FLAPS 15 DEGREES. USED ALTERNATE EXTENTION CHECKLIST. MAINTENANCE REPLACED THE COSDR DALA2017062205025Wire · misinstalledDURING TEST OF SLIDE DEPLOYMENT, THE INBD GROUND SPOILER NR 6 FAILED TO RETRACT. THE BLOW DOWN ACTUATOR EXTENDED, YET THE SPOILER STAYED UP. FOUND WIRES W1104-023-20 AND W1060-588 20 MISWIRED, REPAIRED. SYSTEM OPERATION IS NORMALSDR CALA2017051201365Pin · looseLEADING EDGE SLATS TRANSIT LIGHT STAYS ON 4. EMERGENCY DECLARED. FOUND CONNECTOR SECURE D40160P. DURING PERFORMING T/S FOUND INTERMITTENT FAULT SHOWING F4 PROX. EXTEND SENSOR SHOWING FAR WHEN SLATS EXTENDED, WHEN LOCATING WIRES 2152R-24/2152B-24 AT CONNECTOR DSDR SCNA20170509057Connector · defectiveFLAP ASYMMETRY OFF OF "UP" AT GATE. REMOVED AND REPLACED SKEW NR 5 CONNECTOR D11822. COMPLETED FLAP SKEW FUNCTIONAL TEST. OPS TEST NORMAL.SDR ASMF201704010Connector · looseDURING TRANSIT CHECK, IT WAS DETECTED THE STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE CONNECTOR D381 LOOSE, THEREFORE THE CONNECTOR WAS TIGHTENED IAW AMM 27-41-00,TESTED CORRECT. AS A PRECAUTIONARY ACTION, THE STAB SDR DALA2017022701629Connector · disconnectedWHEN FLAPS SELECTED TO ONE, FLAPS FROZE HALFWAY TO ONE. TE FLAP ASYMETRY AND TRAILING EDGE LIGHT & MESSAGE. COMPLIED WITH QRH, LANDED NO FLAPS. FSEU NR 1 MESSAGE RT FLAP TRANSMITTER WIRE MESSAGE 313. FSEU NR 2, NO FAULTS. IAW FIM 27-51-00-815-805. FOUNSDR AALA20170105018Splice · faultyAIRCRAFT WAS GROUNDED. DURING FCF AFTER 9 MINS IN CRUISE AT FL380 THE LEADING EDGE SLAT ASYMMETRY ANNUNCIATED ON EICAS. REPEATED SEVERAL TIMES THEN REMAINED ANNUNCIATED. EMERGENCY DECLARED. RETURNED TO TUL. MAINTENANCE FOUND SPLICE SM8 ON WIRE W430-008-18 FORSDR AALA201612309001Wire · brokenSETTING TAKEOFF POWER WE GOT SPOILERS CAUTION AND CONFIGURATION WARNING WITH HORN. ABORTED TAKEOFF, WENT TO RUNUP AREA AND GOT THE SAME SYMPTONS WHEN THRUST IS ABOVE 1.5 EPR. AIRCRAFT WAS GROUNDED. MAINTENANCE FIXED A BROKEN WIRE AT TBL190 FOR SPOILER HANDSDR R61A201612180742Connector · looseDURING FLIGHT, CREW RECEIVED A SLAT FAIL MESSAGE. CREW EXECUTED A MISSED APPROACH TO RUN QRH. CREW THEN RECEIVED FLAP/SLAT FAIL MESSAGE, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND RIGHT INBOARD SKEW SENSOR CONNECTOR LOOSE. SDR AALA20161205002Connector · defectiveAIRCRAFT WAS GROUNDED. LAX, AIR INTERRUPT, DFW-SNA. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH EXTENDED FLAPS TO 1 TRAILING EDGE. FLAPS LOCKED DUE TO ASYMMETRY. RIGHT FLAP WENT TO 1, LEFT STOPPED HALF WAY BETWEEN 0 AND 1. REPLACED LEFT FLAP POSITISDR AALA20161128008Wire Harness · damagedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DURING APPROACH WHEN FLAPS 5 DEGREES SELECTED RECEIVED EICAS MESSAGE "TE FLAP ASYM" AND FLAPS STOPPED AT 2 DEGREES. FOUND DAMAGE TO #7 SKEW HARNESS AT CONNECTOR D8970. REPAIRED HARNESS IAW AMM 20-10-13 AND ACCOMPLISHESDR C77A20161031003Wire Harness · faultedDURING DESCENT, THE CREW RECEIVED A FLAP/SLAT FAIL MESSAGE AT 4000 FT. DECLARED AN EMERGENCY AND MANAGED TO GET A NO SLAT/FLAP FAIL MESSAGE PRIOR TO LANDING. THE FLIGHT LANDED SAFELY. MAINTENANCE TROUBLESHOT AND FOUND LEFT OTBD NR 4 SLAT HARNESS AT FAULT. R &SDR AMCR20161031003Wire · corrodedCREW EXPERIENCED AN AILERON TRIM FAIL. INVESTIGATION REVEALED NO CONTINUITY IN TRIM WIRE FROM THE AILERON TRIM ACTUATOR. VISUAL INSPECTION REVEALED A NICK IN WIRE NEXT TO CONNECTOR WITH APPARENT CORROSION. STRIPPING THE WIRE BACK FROM CONNECTOR PIN FOUND CORROSDR AALA20161013011Wire Harness · shortedAIRCRAFT WAS GROUNDED. NRT, AIR INTERRUPT, PVG-LAX. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CRUISE RECEIVED SPOILERS EICAS MESSAGE BUFFETING AT AIRFRAME. VISUALLY CONFIRMED SPOILER 4 AND 11 RAISED FROM WING. MAINTENANCE FOUNDSDR AALA20161003005Connector · damagedEMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH TRAILING EDGE FLAPS FAIL TO EXTEND WHEN SELECTED. FLAPS LOCKED OUT AT 1 DEGREE. MAINTENANCE REMOVED AND REPLACED SKEW SENSOR NR 1 IAW AMM 27-59-01 AND CONNECTOR D400024P IAW AMM 20-61-11. OPERATIONAL CHECSDR HNAA2016092800300Elec Connector · damagedDURING CLIMBOUT, ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED THE CONNECTOR. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2016091300351Connector · damagedAILERON LOCKOUT EICAS MESSAGE ON CLIMB AT 12000 FEET AND 290KT. AIL LOCK LIGHT ON OVERHEAD PANEL. FOUND RT AILERON LOCK ACTUATOR FSEU FAULT BALL ON LEFT SAM. FOUND PIN B12, CONNECTOR D665B OF L SAM PUSHED BACK. REINSERTED PIN, SECURITY CHECK OK. CONTINUITYSDR FDEA201609103176Connector · damagedSPARKS FROM THE BOOT AT THE BOTTOM OF THE CO-PILOTS YOKE. RETERMINATED CONNECTOR R5-932 AT F/O'S CONTROL COLUMN. REF STD MX PRACTICES AND WDM 31-31-11. SECURED R5-932 AND CONTROL COLUMN BOOT. F/O CONTROL WHEEL POSITION READOUT NORMAL. REF MM 31-31-00-5. SDR ABXA20160811132Wire · damagedTHE HORIZONTAL STABILIZER TRIM FAILED TO OPERATE USING CONTROL WHEEL SWITCHES. MANUAL CONTROL WAS NORMAL. AILERON LOCKOUT AND RUDDER RATIO EICAS MESSAGE DISPLAYED. AUTOPILOT DISENGAGED AND WOULD NOT RE-ENGAGE. ACCOMPLISHED WAS REPAIRING SHORTED WIRING IN TSDR JJBA20160809007Wire · disconnectedSPOILER NR 1, NR 2 ILLUMINATED ON TAKEOFF. INSP FOUND WIRES IN THE MICROSWITCH DISCONNECTED. RECONNECTED AND SPLICED WIRES. OPS CK SAT NO DEFECTS NOTED AT THIS TIME.SDR AALA20160725003Connector · damagedDURING TROUBLE SHOOTING FOR A "FLT CTL SYS" EICAS STATUS MESSAGE. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND CONNECTOR M27313 ON THE CONTROL STABILIZER TRIM MODULE TO HAVE PIN DAMAGE AND SIGNS OF BURNING. REMOVED AND REPLACED CONNECTOR AND REPLACED PINS IAW SDR JIKA2016071801Wire · shortedSHORTLY AFTER TAKE-OFF, THE PILOT REPORTED THAT FORWARD PRESSURE ON THE CONTROLS WAS REQUIRED TO KEEP THE AIRCRAFT AT A NORMAL CLIMB PITCH ATTITUDE. THE PILOT SELECTED TRIM DOWN AND THAT CORRECTED THE CONDITION ONLY TO HAVE IT RETURN. IT WAS DISCOVERED AT THATSDR AALA20160616013Connector · contaminatedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT NOT OVERWEIGHT. DURING APPROACH, FLAPS 1 SELECTED AND GOT SPLIT NEEDLE ON T/E FLAP. MAINTENANCE FOUND PSEU RETURNED MESSAGE 27-53252, "FLAP 3 SCEW". ACCOMPLISHED FIM TASK 27-59-00-81SDR R61A201605290441Connector · corrodedDURING HEAVY CHECK, UPPER AND LOWER CONNECTORS ON OUTBOARD PCU FOR LT ELEVATOR ARE CORRODED. MX REMOVED AND REPLACED UPPER AND LOWER CONNECTORS IAW SWPM 20-61-20, 20-62-00.SDR UIEA2016052700354Wire · corrodedON APPROACH SPOILER EICAS MSG. INSPECTED & CONFIRMED NR 3 & NR 10 SPOILERS WOULD NOT DEPLOY. FOUND WIRES FROM CONNECTOR D82195 - D5463J HAD CORROSION. R & R WIRE IAW AMM 27-61-15 & SWP MANUAL 20-61-1. PERFORMED OPERATIONAL CHECK IAW 27-61-00. OPERATIONS CSDR YENA20160504373Circuit Card · failedAFTER SELECTING FLAPS 1 RECEIVED AMBER SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, COMPLIED WITH QRH AND FAULT/FAIL REMAINED. EMERGENCY DECLARED, ACFT LANDED UNEVENTFULLY. R & R WIRING HARNESSES W611 & W612, R & R BOTH RT OTBD SKEW SENSORS IAW AMM 27-83SDR YENA20160504371Wire Harness · failedAFTER SELECTING FLAPS 1 RECEIVED AMBER SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL,COMPLIED WITH QRH AND FAULT/FAIL REMAINED. EMERGENCY DECLARED, ACFT LANDED UNEVENTFULLY. I R & R WIRING HARNESSES W611 & W612, R & R BOTH RT OTBD SKEW SENSORS IAW AMM 27-83-SDR QXEA2016043000285Wire Harness · looseON DEPARTURE, RUDDER APPEARED TO STICK MOMENTARILY THEN RELEASED. CHECKED FOR OBJECTS BEHIND BOTH SETS OF RUDDER PEDALS, NOTHING OBSERVED. RUDDER APPEARED TO FUNCTION NORMALLY DURING REMAINDER OF FLIGHT. ACCOMPLISHED RUDDER CHECK AFTER LANDING WITH NO ISSUESDR 2016FA0000199Wire Harness · mismanufacturedFLIGHT CREW REPORTED THAT THE PITCH TRIM SYSTEM OPERATED IN REVERSE DURING AUTOPILOT USE. TROUBLESHOOTING REVEALED THAT PINS C & D WERE SWAPPED ON THE HARNESS CONNECTING THE ELECTRONIC PITCH TRIM AMP AND THE TRIM SERVO.SDR ASOA20160429028Wire · burnedTHE CREW REPORTED CLIMBING OUT THROUGH 6000 FT, THEY SMELLED A FOUL ODOR AND RECEIVED A PITCH TRIM MAIN FAIL MESSAGE. NONE OF THE TRIM SWITCHES WOULD WORK. PITCH TRIM BREAKER POPPED AND SMELL WENT AWAY. MAINTENANCE INSPECTED AND REPAIRED BURNED PITCH TRIM SDR GR422016041400002Wire Harness · misinstalledTIE WRAP AROUND WIRING HARNESS IN LT AFT WING AT STATION RBS 255 WAS TIED AROUND LT AILERON TRIM CABLE. THE ACFT HAS NOT FLOWN SINCE BEING INDUCTED INTO THE REPAIR STATION. THE TIE WRAP WAS DISCOVERED DURING AN INDUCTION INSPECTION AFTER ACFT HAD RECEIVED ITSDR UIEA2016041000238Jumper · openDURING TAKEOFF ROLL RECEIVED AURAL WARNING, MASTER CAUTION LIGHT & EICAS ALERT MSG CONFIG. PERFORMED REJECTED TAKEOFF AT APPROX 145 KNOTS. FOUND CMC MSG 277791. PERFORMED TROUBLESHOOTING IAW AMM 27-00-00 & FOUND JUMPER AT LE PANEL OPEN. R & R JUMPER WERE PSDR CA160222003Connector · contaminated(CAN) UPON SELECTING FLAPS 30 DEGREES DURING THE APPROACH, FLIGHT CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE APPROACH WAS CONTINUED AND THE AIRCRAFT LANDED WITH FLAPS AT 20 DEGREES WITHOUT FURTHER INCIDENT. TROUBLESHOOTING DETERMINED THE FLAPS FAIL SDR AALA20160220001Wire · damagedAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE THE FLAP SOV CB TRIPPED NECESSITATING A NO FLAPS LANDING. R & R SOV V51 IAW AMM 27-81-91-201. DID NOT FIX, ITEM REPEATED DURING NEXT DAY MX CHECK. TR
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