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 CA130429007Wire Harness · failed(CAN) SLAT FAIL AT 3000 FT ON APPROACH. PAN PAN DECLARED WITH ATC. LANDED WITHOUT INCIDENT. MAINTENANCE DUTY PILOT AND FLIGHT SAFETY HAVE BEEN ADVISED. IAW FIM 27-83-00-810-814 FOUND RT & LT OTBD SLAT SKEW HARNESSES INTERMITTENT. BOTH HARNESSES REPLACED ASDR C77A20130430030Wire · damagedDURING BASIC CHECK 3, RODENT DAMAGE WAS EVIDENT IN THE FWD CABIN CEILING AREA. OPENED ENTIRE INTERIOR CEILINGS AND SIDEWALLS FOR A RODENT DAMAGE INSPECTION. THE INSPECTION RESULTED IN 30 DAMAGED WIRES, THREE WHICH WERE FLY BY WIRE, 20 DAMAGED INSULATION BLANKSDR UALA2013041702629Connector · looseMOMENTARY ELAC 2 PITCH FAULT AFTER LIFT OFF. FAULT CLEARED AFTER A FEW MIN. SAMC TEXT: DUE TO HISTORY NEXT STEP REPLACE NR 1 AND NR 2 SEC'S PCN 482-9549 AND BOTH SDAC'S 482-9503 (P/N 350E5500201). FOUND CONNECTORS (107VC, 109VC, 111VC, 119VC, 115VC, 10VC, SDR USAA2013041500006Wire Harness · defectiveFLIGHT 2025, BOS-DCA - SLAT FAIL MESSAGE ON CLIMBOUT PASSING THROUGH 11,000 FEET. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.SDR UALA2013041102484Connector · damagedSTAB TRIM LIGHT AND UPPER EICAS ILLUMINATED WHEN STAB MOVED. STAB TRIM SHUTOFF LEFT CIRCUIT BREAKER ON P-11 WILL NOT RESET. FOUND D1851 CONNECTOR INSULATION DAMAGED. REPLACED CONNECTOR D1851 PER WDM 27-41-11.SDR SWIA201333167Wire · out of rigON THE CLIMBOUT WITH FLAPS UP, ACCELERATING AT 230 KTS INDICATED, FLAP HIGH SPEED WARNING SOUNDED. SLOWED TO UNDER 230, WENT AWAY. UPON FLAPS SELECTION TO 20, FLAP FAIL CAUTION. RAN QRH, LANDED WITHOUT FURTHER PROBLEM. LEFT FLAP FAILED AT 0°, RIGHT FLAP FSDR MASA2013040352470Wire Harness · faultyRUDDER LIMIT FAULT STATUS MESSAGE ON EICAS. C/W WITH MODSUM IS67027250003 FOR IMPROVEMENT OF THE NR 1 RTL ACTUATOR HARNESS.SDR UALA2013032001728Wire · damagedNR 1 LEADING EDGE SLAT ASYM MESSAGE ON EICAS. PER TROUBLESHOOTING FIM TASK 27-81-05 REMOVED AND REPLACED LT OUTBOARD SLAT LOSS SENSOR SWITCH PER AMM. REPAIRED WIRE WITH ENVIRONMENTAL SPLICE PER SWPD 20-10- 12. SYSTEM OPS CHECKED OKAY.SDR CLCA20130313002Connector · dirtyAFTER TAKEOFF FROM BOG (SKBO), DURING CLIMB, LEVEL 2 AIL DEFLECT DISSAGREE ALERT DISPLAYED. PERFORMED APPROPRIATE CHECK LIST, ALERT REMAINED DISPLAYED. DUMP FUEL, RETURNED TO (SKBO). COMPLIED WITH FIM 27-10-05, FOUND CONNECTOR DIRTY AT LEFT O/B ACTUATOR, CLSDR HNAA2013021900077Wire · brokenAFTER GEAR EXTENSION, CREW HEARD A SINGLE POP NOISE, THEN AFTER ROLL OUT, WHEN FLAPS WHERE SELECTED TO 5 DEGREES FROM 15 DEGREES, FLAPS DID NOT MOVE. BUT WHEN ZERO WAS SELECTED, THE FLAPS RETRACTED FULLY. MOVING FLAP SELECTOR TO ZERO, A RESISTANCE WAS FELT.SDR IPXA3677172Wire · damagedEMERGENCY DECLARED. L/E ASYM AND NOSE A/G DISAGREE FERRY. SLAT SYS WING WIRING REPLACEMENT. C/W EO B767-2780-49951, APPENDIX A.SDR YENA20130214043Wire Harness · shortedFLT 571 HPN-PBI, AIRCRAFT DIVERTED TO JFK DUE TO SLATS WOULD NOT RETRACT AFTER TAKEOFF. ON TROUBLESHOOTING FOUND SKEW SENSOR HARNESS P0893 SHORTED TO SHIELDING AT PINS 1 AND 2. NEED TO REPLACE SKEW SENSOR HARNESS P0893 LEFT WING SKEW SENSOR BETWEEN SLATS 3/4SDR ASOA20130208258TConnector · burnedTHE RT SPOILER DEPLOYED DURING FLIGHT, UNCOMMANDED. ACFT LANDED WHERE MX R & R THE RT INBD PROX SWITCH CONNECTOR PLUG IAW SWPM20-50-00. PERFORMED SPOILER OPS CHECKS IAW AMM 27-63-01. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.SDR CA130206003Wire Harness · failed(CAN) THE FLIGHT CREW ENCOUNTERED A SLAT FAIL MESSAGE ON APPROACH. THIS RESULTED IN A FLAP 2, SLAT ZERO LANDING CONFIGURATION. A PAN PAN WAS DECLARED AS A PRECAUTION FOR PRIORITY AND POSSIBLE HOT BRAKES. ON ARRIVAL. AFTER LANDING RUNWAY 23, THE ACFT WAS MET SDR SWAA2013022112981Connector · corrodedRIGHT WING AILERON ROTARY TRANSDUCER CONNECTOR CORRODED. REMOVED AND REPLACED AILERON ROTARY TRANSDUCER CONNECTOR ON RIGHT WING IAW B717 WDM 22-12-11.SDR CA130204005Connector · mismanufactured(CAN) FLAP ACTUATOR ASSY. HAS 2 MOTORS, A PRIMARY AND STAND-BY, WHICH OPPOSE EACH OTHER AT TRANSMISSION, THEREFORE THEY ARE WIRED OPPOSITE EACH OTHER TO FUNCTION NORMAL. RECEIVED NEW FLAP ACTUATOR ASSY. THE PRIMARY MOTOR WIRE CONNECTOR WAS FOUND WIRED BACKWASDR IPXA3676880Connector · shortedL/E SLAT DISAGREE LIGHT AND NOSE LANDING GEAR A/GROUND DISAGREE MESSAGE, EMERGENCY DECLARED. FOUND CONNECTOR D4378J, PINS 17 & 18 SHORTED TO PINS 21222. REMOVED PINS & WIRES. INSTALLED SHRINK TUBE TO ALL SPLICES, SECURED ALL DISTURBED BUNDLES. OPS CHECKEDSDR DXTA2013013005266Connector · dirtyFLAPS WOULD NOT EXTEND WHEN FLAP LEVER MOVED TO ANY FLAPS DOWN POSITION. HYD PRESS LIGHT REMAINED ILLUMINATED UNTIL FLAP LEVER PLACED BACK TO THE FLAPS UP POSITION. VERIFIED PROPER RIGGING OF FLAP UP AND DOWN CONTROL SWITCHES AND FOLLOW-UP CABLE. CLEANED FLSDR UALA2013011700302Feeder Cable · chafedFOUND FEEDER CABLES IN E&E BAY CHAFING AND BURNED. WIRE REPLACED W230-005 AND W230-006 FROM P34 TO P32.SDR UALA2013011700305Connector · damagedBOTH STAB TRIM INDICATOR SHOWING MOVEMENT DURING TAXI. CLEANED CONNECTORS AT RIGHT AND LEFT STAB POSITION TRANSMITTERS IAW WD 27-48-11. ACCOMPLISHED AMM POSITION SYSTEM TEST AS PER MM 27-48-00-735-053. NORMAL FUNCTIONS NOTED.SDR 2013FA0000277Terminal · looseDISCOVERED LOOSE TERMINAL CONNECTION ON FLAP LIMIT SWITCHES.SDR UALA2013011600254Wire · severedWIRE REPAIR. WIRE #2795-0165 SEVERED AT 42CE3 RELAY POSITION X1 TO 1846VT POSITION 4 PIN D FROM 187VU TO 184 VU. INSTALLED NEW WIRE 2795- 0165 FROM 42CES POSITION X1 TO 1846VT POSITION 4 PIN D AND TERMINATED IAW ESPM 20-53-21. PERFORMED INTEGRITY TEST OF THSDR 39LA2012122500001Wire · brokenDURING TAKEOFF ROLL, SPOILER 1 PUSH OFF LIGHT ILLUMINATED. CREW REJECTED TAKEOFF AND RETURNED TO THE GATE. DURING THE INSPECTION OF SPOILER FLIGHT CONTROL SYS, A BROKEN WIRE WAS FOUND ON THE LT WING SPOILER CLUTCH SWITCH ACTUATOR. THE BROKEN WIRE WAS REPAIREDSDR SIMA20121223008Connector · corrodedRT SPOILER PROXIMITY SENSOR HAS CORRODED CONNECTOR. INSTALLED CONNECTOR IAW EO EM-57MR-663.SDR UIEA2012121000541Connector · contaminatedON DEPATURE EICAS MESSAGE "FLAPS DRIVE" APPEARED AND THE OTBD T/E FLAPS WOULD NOT RETRACT PAST 1 DEGREE OR EXTEND BEYOND 1 DEGREE. RETURNED TO DEPARTURE. MX FOUND THE LT OTBD FLAP POSITION TRANSMITTER ELECTRIC CONNECTOR WAS CONTAMINATED WITH DEICING FLUID. SDR YENA20121209660Connector · corrodedFLT 1226 RDU-BOS, CREW DECLARED EMERGENCY DUE TO "FLAP FAIL" EICAS WHEN FLAP 1 SELECTED FOR APPROACH. DID NOT RESET AFTER QRH. LANDED FLAPS "0" PER QRH PROCEDURE. DURING TROUBLESHOOTING FOUND CONNECTOR P1250 CORRODED AT RIGHT O/B FLAP SKEW SENSOR T4. REMOVSDR CA121115007Connector · damaged(CAN) BACKSHELL FOR LT ELEVATOR HORN HEAT CONNECTOR/WIRING LOCATED ON TOP CENTER OF THE HORIZONTAL STABILIZER SEVERELY CORRODED/CRACKED. BACKSHELL REPLACED.SDR UALA2012111206492Wire · chafedONE WIRE IN BUNDLE BELOW NR 2 SPOILER ACT HAS SIGNS OF CHAFING, WIRE MARKED. REPAIRED WIRE W3306-4252-20 AT LEFT REAR WING SPAR WSTA 258. PERFORMED REPAIR OF INSULATION IAW SWPM 20-10-13 AND WDM 27-51-61.SDR UALA2012110806429Wire · brokenNUMEROUS BROKEN WIRES AT 7506VP CONNECTOR.SDR CA121109001Wire · damaged(CAN) DURING CLIMB, FLIGHT CREW NOTICED THE FLAPS WERE STUCK AT 5. FUEL CALCULATION WAS MADE AND DECISION TAKEN TO CONTINUE WITH THE FLIGHT. ACFT LANDED WITHOUT FURTHER INCIDENT. AN ELECTRICAL WIRE AT THE FLAP SELECTOR WAS REPAIRED, THE SYS TESTED SERVICEABSDR UALA2012110606364Pcu · faultyPER CMC1 TESTS OF RT INBD FLAPERON PCU SHOWS RAM POSITION TRANSDUCER SIGNAL OUT OF RANGE. PER FIM NEEDS ACCESS TO RT INBD FLAPERON PCU CONNECTOR AND REMOVAL OF ACE L2 SUSPECT PCU. REPLACED RIGHT WING FLAPERON INBD. PCU IAW AMM.SDR UALA2012110506326Terminal Block · crackedTB190 BLOCK 5-6 IS CRACKED AND UNUSABLE.SDR UALA2012110506335Wire Harness · faultySENSOR EXC 1 CB TRIPPING ON P310 PANEL. REPLACED WIRE HARNESS FROM D2181P TO SKEW SENSOR M27325 AND CHECKED OKAY.SDR UALA2012102506120Wire · shortedL/E ASSY MSG, FLT DIVERTED.AFTER TAKEOFF IN ROUGH AIR, L/E ASSYMETRY MESSAGE ON EICAS WITH L/E LIGHT ILLUMINATED. NO ABNORMAL FLIGHT CONTROL ISSUES. MAINT TEXT: PILOT DEBRIEF - PILOT HAND FLYING, ON INITIAL CLIMB, CLEARED UP 10-15 MIN INTO FLIGHT BETWEEN 28 SDR CA121023009Connector · failed(CAN) DURING FLIGHT, THE ACFT EXPERIENCED A STICK SHAKER WITH NORMAL AIRSPEED DISPLAYED, FLIGHT CREW RESPONSE, AFFECTED CIRCUIT BREAKER PULLED, AS WELL AS INTERMITTENT AUTO PILOT RESPONSE AND INDICATION OF FORWARD POSITION OF THE TRIM. THE INDICATED TRIM POSITSDR FDEA201210033545Wire · damagedDURING CLIMBOUT FL 210 L/E SLAT ASYM EICAS LIGHT AND L/E CAUTION LIGHT CAME ON. PRIOR TO LIGHTS FLAPS WERE UP, FLAP HANDLE UP AND FLAP INDICATOR INDICATED FLAPS UP. REDUCED SPEED TO 240 IAS LIGHTS STAYED ON DURING FLIGHT. NEEDED TO USE QRH PROCEDURES TO CSDR AALA20120925004Wire · brokenLHR - CREW REPORTED LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PROXIMITY SENSOR S279 THAT HAD BROKEN WIRE. SYSTEM GROUND CHECK NORMAL OPSDR ERAA20120067Wire · chafedNR 1 SPOILER FLIGHT CONTROL PUSH-OFF LIGHT ILLUMINATED IN FLIGHT, NO ROLL CONTROL ISSUES. FOUND LEFT SPOILER DISCONNECT WIRE CHAFED AT LEFT 5 WING STA YW 232.0 APPROX. REPAIRED WIRE WITH ENVIROMENTAL SPLICE IAW STANDARD PROCEDURES, OPS CHECKS GOOD ON GROUND.SDR R61A201209200517Wire Harness · faultyCREW REPORTED THAT ON FINAL APPROACH AT 3,000 FEET RECEIVED A SLAT FAIL INDICATION. THE SLATS WERE ALMOST IN THE FULL POSITION. THE CREW BROKE OFF THE APPROACH, DECLARED AN EMERGENCY, AND RAN THE CHECKLIST. AFTER RUNNING THE CHECKLIST THEY WERE ABLE TO SAFESDR CA120904007Connector · corroded(CAN) DURING APPROACH WHEN THE FLAPS WERE SELECTED TO UNIT 1 THE FLIGHT CREW NOTICED THE FLAP INDICATOR DID NOT MOVE AND REMAINED IN THE FLAPS UP POSITION. THE APPROPRIATE CHECKLIST WAS CARRIED OUT AND THE ACFT MADE A SUCCESSFUL LANDING. MAINTENANCE CARRIED OSDR HNAA2012082900935Connector · failedAFTER TAKEOFF, ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED INTERMITTENTLY, THEN CONTINOUS. R & R CONNECTOR 2761P1 AT INBD ROLL SPOILER HYD PRESSURE SWITCH. GROUND RAN AND CHECKED GOOD.SDR YENA20120813576Wire Harness · defectiveFLT 956 MCO-BOS, RETURNED TO MCO DUE TO SLAT FAILED UPON RETRACTION. REMOVED AND REPLACED RIGHT OUTBOARD SLAT HARNESS IAW AMM 27-83-07 AND SLAT POSITION SENSOR IAW AMM 27-83-06. OPS CHECK NORMAL.SDR AALA20120811004Wire · shortedMIA - CREW REPORTED FLAP ASYMMETRY INDICATION. EMERGENCY DECLARED FLIGHT LANDED MIA WITHTOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SHORTED WIRE. REPLACED WIRE W33256-4251. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CA120917012Wire Harness · shorted(CAN) ON APPROACH, THE CREW RECEIVED A FLAP FAIL MESSAGE AT 0 DEGREES WHEN THEY SELECTED FLAPS TO 8 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE FLAPS WERE RESET AND PLACED ON MEL. THE OPERATOR REPORTED THAT THE ACFT HAD REPEATED SDR CA130124013Connector · damaged(CAN) WHILE TROUBLESHOOTING A SNAG RELATED TO NO CHIME WHEN DATALINK MESSAGE RECEIVED ON DATALINK NR 1 ON AIRCRAFT, IT WAS FOUND THAT THE FEMALE FORK PINS OF THE FUSELAGE HARNESS CONNECTOR WERE IMPROPERLY CRIMPED. FORK CONNECTORS IMPROPERLY CRIMPED WERE A411PSDR JIKA2012071101Wire · brokenWIRES UNDER CAPTAINS SIDE YOKE SPARKED AND BEGAN TO SMOLDER. LOST PRIMARY TRIM, PULLED CIRCUIT BREAKER AND CONTINUED ON AUX TRIM. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE WIRING, AND FOUND A BROKEN WIRE ON THE MAIN TRIM ON THE CAPTAINS SIDSDR AALA20120704011Connector · corrodedBNA - CREW REPORTED WHEN SELECTING FLAPS FOR LANDING FLAPS WOULD NOT COME OUT OF UP POSITON. EMERGENCY DECLARED FLIGHT LANDED BNA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 3 FLAP ASKEW SENSOR ELECTRONIC CONNECTOR CORRODED. REPLACED CONNSDR AALA20120627002Connector · dirtyDEN - CREW REPORTED FLAPS DID NOT EXTEND TO POSITION 1 OR ANY FURTHER WITH FLAP HANDLE. LEADING FLAP TRANSIT LIGHT STAYED ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED DEN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BITE OF FLAP SLAT ELECSDR REXA2012052400771Wire Harness · chafedFLAPS FAIL AT 25,000 FEET -26C AT CRUISE SPEED. PERFORMED TROUBLESHOOTING PER FIM REV 39. FOUND CONTROL CABLE PULLEY WEDGED AGAINST RT BPSU HARNESS, CAUSING FLAP FAIL DISCREPANCY. REMOVED PULLEY, OPS CHECK FLAPS IAW AMM 27-54-00. OP CHECKED GOOD, OK FOR SESDR UALA2012051602805Circuit Breaker · malfunctionedELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET ELAC1 CIRCUIT BREAKER, OP CHECKED REF MM 27-93-00-401. ALSO, RAN BOTH ENGINES AND NO FAULTS FOUND OR PRESENT ON ENGINE RUNS OR GROUND CHECKS, NO PRIOR HISTORY.
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