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 FDEA201107152752Connector · damagedAFTER T/O WHEN RETRACTING FLAPS FROM 2 TO 0 DEG NBR 2 SLAT LIGHT REMAINED ON. QRH ACTIONS ACCOMPLISHED AND LIGHTS REMAINED ON. RETURNED TO LAND. SLAT LIGHT EXTINGUISHED AFTER LANDING FOUND 4 OF THE 5 PINS PUSHED BACK IN CONNECTOR AT THE NR 2 SLAT ACTUATOSDR MASA2011071103177Connector · dirtyFLAP FAULT STATUS ON LANDING. CLEANED BOTH CONNECTORS AND RE-SECURED.SDR C2XA11IA142Connector · misalignedIAH - FLIGHT 2020, DURING CRUISE FLIGHT THE CREW REPORTED AN SPS ADVANCE MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND CONNECTOR SP7148 TO BE MISALIGNED, MAINTENANCE CORRECTLY INSTALLED SDR EIAA2011078Connector · disconnectedCREW REPORTED TO TECH CENTER THAT THE NR 3 RT LED GROUP WAS STUCK IN TRANSIT. LIGHTS ON FLIGHT ENGINEERS PANEL INDICATED GROUP IN TRANSIT WHILE ALL OTHERS INDICATED STOWED (GREEN) PERFORMED AIR TURNBACK. FOUND CONNECTOR FOR NR 3 RT GROUP DISCONNECTED. CONNESDR USAA2011062700012Connector · shortedFLT 1944 - DFW-CLT - FLIGHT CONTROL - CREW REPORTED THE FLAPS WOULD NOT EXTEND NORMALLY. USED ALTERNATE METHOD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CONNECTOR D4325J SHORTED AT PIN 29 TO PIN 16. REPLACED CONNECTOR D4532J IAW SWPM 20-61-11. ALSO, RSDR UALA2011062103053Wire Harness · corrodedSPOILER NR 4 HARNESS M27825 FOUND CORROSION AT CONNECTOR D2129J WD27-61-13. HARNESS CORROSION CLEANED PER MT. HARNESS REPLACEMENT REQUIRED. PLAN 3 SHIFT SLOT FOR HARNESS REPLACEMENT. HARNESS P-N 23354-001 IPC 27-61-09-010 IS LOB. CABLE ASSY IS ABOUT 40 FESDR USAA20110616SB101Connector · shortedCLT - DURING APPROACH INTO CLT, CAPTAIN ADVISED THE FLAPS WOULD NOT RESPOND. DECLARED AN EMERGENCY AND LANDED AT FLAPS 15 USING ALTERNATE FLAP EXTENSION. THE FLIGHT LANDED AND TAXIED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND THE E3-2 RACK CONNECTOSDR HALA2011061100262Connector · dirtyETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ILLUMINATED ON EICAS. C/W FIM 27-21-00/101, FIG 104 CLEANED CONNECTORS ON RUDDER RATIO ACTUATOR, OK FOR SERVICE.SDR HNAA2011061300163Wire · brokenDURING RETURN TO FIELD, FLAPS WOULD NOT EXTEND, FOUND C/B L7 ON LT ESSENTIAL POPPED. FOUND WIRE BROKEN AT FLAP ARMING SWITCH, WILL SOLDER AND OPS CHECKED FLAP. NO FIX. REMOVED RELAY 2752 K1 CIRCUIT BREAKER STILL POPS, REINSTALLED RELAY.SDR HALA2011052700231Wire · damagedAUTO TRIM FAIL - BOTH ALTERNATE TRIM CB'S POPPED (D-10 & 11). REMOVED AND REPLACED THE ALTERNATE TRIM DRIVE MOTOR IAW AMM 27-43-01. COND. SAME. FOUND WIRES E9401-1-16,-2-16,-3-16,-4-20,-5-20,-6-16,-7-16,-8-16,-14-20 & E9412-35-20 DAMAGED. AREA OF DAMAGE IS ONSDR UALA2011052002486Wire Harness · faultyFLIGHT CONTROL SYS STATUS MSG. NEED TO REPLACE ACE L2 FOR T-S. REPLACED ACE L2 PER MM. LRU REPLACEMENT TEST PASSED. REPLACED PCU BORROWED FROM EVA & TEST STILL FAILED, REINSTALLED ORG PCU PER MM. REPLACED SHORT HARNESS W8797 PCN 585-2189, ACES LRU REPLACESDR SWIA201126281Connector · dirtyFLAPS DISAGREEMENT THEN TURNED TO ASYMMETRY. (FLT 7004) CLEANED FLAP TRACKS AND ROLLERS. CLEANED AND RE-RACKED ACTUATOR CONNECTOR. CYCLED FLAPS NUMEROUS TIMES, OPS CHECK GOOD.SDR MASA2011051902777Connector · disconnectedRTG AIL AND RUDDER TRIM INDICATION FAILED. RESET CONNECTOR ON POWER SUPPLY.SDR CA110509007Wire Harness · failed(CAN) ON DEPARTURE CREW RECEIVED SLATS/FLAP FAIL MESSAGE. FLIGHT CONTINUED AND LANDED IAW QRH. EMERGENCY DECLARED AS PRECAUTION. SLAT HARNESS LT WING OTBD NR 4 W512 REPLACED IAW AMM 27-83-07-000-801-A. NO MESSAGE ALL OTHER FAULTS, NO FAULTS NOW. SERVICEABSDR C2XA11CL118Connector · corrodedDAY FLT 5857 THE CREW REPORTED THE SPOILERS DEPLOYED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT SPEED BRAKE PROXIMITY SWITCH AND CONNECTOR P1166. OPERATIONAL CHECKS WERE GOOD.SDR YENA20110429245Wire Harness · faultyFLT 69 SYR-JFK, CREW DECLARED EMERGENCY DUE TO, SLAT FAIL EICAS MSG IN FLIGHT. REMOVED AND REPLACED SLAT HARNESS W612 RT AND PERFORMED OPERATIONAL TEST OF THE SLAT CONTROL SYS IAW 27-80-00-710-801 NO FAULTS NOTED AT THIS TIME, A/C OK FOR CONTINUED SERVICE.SDR C2XA11CL105Connector · corrodedTHE CREW REPORTED A TAKEOFF CONFIG WARNING MESSAGE FOR SPOILERS OPEN ON TAKEOFF ROLL.SPOILERS THEN KEPT ALTERNATING OPEN/CLOSED. THE CREW ABORTED TAKEOFF. MX INSPECTED AND REPLACED RT INBD SPOILER PROXIMITY SWITCH CONNECTOR. THE CONNECTOR WAS CORRODED AND WISDR FDEA201104161505Wire · damagedON CLIMBOUT, FLAPS WOULD NOT RETRACT PAST THE "2" POSITION. RAN THE QRH AND FOUND NR 8 SLAT WAS STILL OUT. IAW QRH, PLACED THE FLAPS AT "5" AND RETURNED TO DEPARTURE. UPON TROUBLESHOOTING, DETERMINED THAT NR 1 SLAT WAS SHOWING "GREEN" AND DOWN AT FLAPS "2"SDR UALA2011040701688Wire · shortedSFCC 1-FLAP FAULTS. MEGGERED WIRES WITH CON OFF AND NR 1 LGCIU OUT FOUND WIRE 2751-5907B BETWEEN CONNECTOR 7541VC AND 7505VC SHORTED TO GROUND. REF AWD27-51-11. REPLACED R&B WIRES 2751-5907B AND 2751-5907R BETWEEN CONNECTORS 7541VC AND 7505VCA. REF WD AND ESPSDR HNAA2011032000059Wire · brokenFLAPS WILL NOT GO TO 35 DEGREES. REMOVED 2 PANELS AT CTR CONSOLE. INSPECTED AND CLEANED FLAP TRIGGER MICRO SWITCH. GROUND RAN ACFT, OPERATED FLAPS THROUGH FULL TRAVEL, OPS CHECKED GOOD IAW -8 MM 27-51-00. REINSTALLED PANELS, OK FOR SERVICE. ON TAKEOFF, FSDR UALA2011031601283Wire Harness · damagedEICAS STATUS MSG FLIGHT CONTROL SYS NOTE. NR 1 SPOILER DOESN'T FULLY STOW. REPLACED ACTUATOR. DURING OPS TEST FOUND RVDT OUT OF RANGE. CHANGED HARNESS, NO HELP. CONTINUING TO T-S. REPLACED PCU NR 1 SPOILER, CHECKED ADJUSTMENTS FELL WITHIN LIMITS IAW AMM.SDR FDEA201103080904Connector · dirtyAFTER TAKEOFF KRUGER FLAPS DID NOT RETRACT. CYCLED TO NO AVAIL. AFFECTED SURFACE DEACTIVATED IN RETRACTED POSITION. OBSERVE AFM PERFORMANCE LIMITATIONS FOR INOPERATIVE KRUGER FLAPS." REACTIVATED KRUEGER FLAPS IAW MM 27-87-00-09-0. FOUND CONNECTOR ON KRUEGSDR CA110303005Circuit Board · smoke(CAN) DURING A WALK AROUND, THE PILOT TURNED ON THE COCKPIT LIGHTS. SMOKE WAS EMITTED FROM THE PEDESTAL, BATTERY POWER WAS TURNED OFF. MAINTENANCE INVESTIGATED AND FOUND THAT THE SMOKE WAS CAUSED BY A BURNED WHEAT, BULB, PN D158/-100-5T1 ON THE PITCH TRIM LIGSDR T17A20110217001Bonding Jumper · brokenSHORTLY AFTER TAKEOFF THE PILOT NOTICED A SLIPPAGE IN THE THE CONTROL PRESSURE WHEN A LT ROLL WAS INPUT ON THE YOKE. AFTER 15 DEGREES OF YOKE TRAVEL, CONTROL PRESSURE RELEASED AND THEN CAUGHT WITH CONTINUED INPUT. CONTROL PRESSURE BEYOND THAT POINT WAS NORMASDR CA110217005Wire · shortedAFTER T/O FLAPS FAILED TO RETRACT TO "0" MOC AND DISPATCH CONTACTED QRH PROCEDURE C/O RETURED TO BASE WITH SLATS AT 2, FLAPS" 0" +1 AMBER WIRE NR 2751-5906R BETWEEN CONN. 7540VC & 7504VCA, WIRE NR 2751-5910R BETWEEN CONN 7542VC & 7502VCA FOUND SHORTED TO GRD.SDR E81RJW304203Pcb · intermittentINVESTIGATED FLIGHT CREW REPORT OF ROLL TRIM NOT RESPONDING TO SELECTED INPUTS AFTER 10 DEGRESS FLAPS SELECTED ON APPROACH. ROLL TRIM OPERATING NORMAL AFTER LANDING. FOUND INTERMITTENT OPERATION OF A194 ROLL TRIM PC BOARD ASSY. REPLACED A194 PC BOARD WITH NSDR USAA20110126SB017Connector · dirtyALB - CREW REPORTED A FLAP ASYMMETRY DURING APPROACH WITH FLAPS 30 SELECTED. ASYMMETRY OCCURRED AT FLAPS 25. CONDITION CLEARED ITSELF DURING GO-AROUND. FLIGHT LANDED WITHOUT INCIDENT AT FLAPS 30. MAINTENANCE VISUALLY INSPECTED FLAP SYSTEM. REMOVED, CLEANESDR CA110125022Wire · chafed(CAN) DURING APPROACH AND AFTER SELECTION OF FLAP 15 FOR LANDING, THE FLAP INDICATOR SHOWED ASSYMETRY AND THE FLAPS REMAINED AT FLAP SETTING 5. AN EMERGECNY LANDING OCCURED WITHOUT ANY FURTHER INCIDENT. THE PSEU LIGHT ILLUMINATED AFTER LANDING. MAINTENANCE WASSDR YENA20110123184Wire Harness · shortedFLT 1732 BDA-JFK, CREW DECLARED EMERGENCY DUE EICAS SLAT FAIL WITH NO ACTION ON SLAT/FLAP LEVER. FOUND SHORT ON SLAT HARNESS 2/3 RT SIDE. REPLACED HARNESS 2/3 RT SIDE AND OPS CHECK GOOD.SDR CA110107009Connector · contaminatedCREW REPORTED STAB OUT OF TRIM LIGHT ILLUMINATED ON APPROACH. ELECTRIC TRIM INTERMITTENT DURING MISSED APPROACH. MAINTENANCE CARRIED OUT DFCS BITE TEST IAW FIM TASK 22-11 TASK 801. LAST FLT LEG FAULTED STAB TRIM "A" MOTOR MSG, FAULT CODE 22-11177. CLEANED SDR CA110103003Wire Harness · failedON APPROACH, WHEN FLAPS WERE SELECTED, A SLAT FAILURE OCCURRED. THE FLIGHT CONTINUED DOWNWIND AND COMPLETED THE QRH. THE LANDING WAS CARRIED OUT IN A FLAP 2/SLAT 3 CONFIGURATION. ERS VEHICLES WERE CALLED OUT BUT AN EMERGENCY WAS NOT DECLARED. THERE WAS NO SDR UALA2010122304703Coax · failedUNSCHEDULED STAB TRIM DISP. CHANGED THE STAB COAX CABLE.SDR C77A347797Wire Harness · unknownSLAT FAIL ON FLAP EXTENSION DURING LANDING. W/O 347799 ADDITION MESSSAGES APPEARED SPOILER FAULT, AOA LIMIT FAIL, SHAKER ANTICAPATED, SLAT-FLAP LEVER DISAGREE. GROUND PROX FAIL AND WINDSHEAR FAIL ON EICAS. PERFORMED FIM 27-81-00-810-805-A00, 27-50-00-810-802SDR CA101217005Connector · broken(CAN) SINCE DELIVERY OF SHIP 1011 WE HAVE BEEN PLAUGED WITH FLAP CAS FAIL MESSAGES. EACH TIME THE FLAPS FAIL IN FLIGHT THE CREW HAS NO OPTION TO LAND WITHOUT FLAP EXTENSION AND DO A FLAP RESET PROCEDURE ON THE GROUND. EACH TIME AN INSPECTION HAS BEEN CARRIED OSDR CA101119006Wire Harness · failed(CAN) THE FLT EXPERIENCED SLAT 3 FLAP 2 SNAG DURING DESCENT. EMERGENCY VEHICLES DISPATCHED AS A PRECAUTION. TOW CREW ON STD BY. LANDED WITHOUT INCIDENT AND TAXIED UNDER ITS` OWN POWER TO GATE. ALL PAX AND CREW OK. PAX REACTION GOOD. AIRCRAFT REMOVED FROMSDR FDEA201011184422Connector · damagedPASSING 17000FT, FLAPS RETRACTED, CLEAN CONFIGURATION, RECEIVED L/E SLAT ASYM EICAS ALONG WITH T/E CAUTION LIGHT. AT DESTINATION, FLAPS COULD NOT EXTEND WITH HYD EXTENDED FLAPS IAW QRH ELE WITH ALTN FLAP SWITCH. PERFORMED BITE ON ALL 3 FSEU'S. NO CURRENT FSDR CA101108001Wire Harness · failed(CAN) APPROACH TO RWY05 SLAT FAILURE (SLAT FAIL MSG WHEN FLAP 1 SELECTED), GO AROUND AND LANDED 05 SECOND ATTEMPT, EMERGENCY EQUIPMENT WERE ON STANDBY. RT SLAT HARNESS W611 AND W612 REPLACED AS PER AMM 27-83-07. CKS SERVICEABLE, P/N 171-00186-401 (RT SLAT NRSDR SIMA201030505Connector · looseON FLIGHT 2915 DURING CRUISE THE CREW REPORTED FLAP INDICATOR INDICATED SEVERAL DIFFERENT DEGREE POSITION FROM 1 DEGREE TO 43 INTERMITTENTLY. EN ROUTE FLAPS DID NOT MOVE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVESDR UALA2010102503925Connector · shortedT/E FLAP DISAGREE, FLT DIVERTED. FSEU NR 1 BITE SHOWS FLAP FAIL MSG 217. ACCOMPLISHED FIM 27-51-00, FIG 107 FOR FSEU-1 , NO FAULTS FOUND, ACCOMPLISHED FIM FOR FSEU-2 , NO FAULTS FOUND. FOUND *EXISTING FAULT* 'LT FLAP XMT WIRE' MSG 220 FOR FSEU-2 ONLY, REPLASDR UIEA201000235Conduit · damagedDURING WALKAROUND INSP, MX FOUND THE ELECTRICAL CONDUIT AND CONNECTOR MOUNT HOUSING AT THE NOSE GEAR DAMAGED (REF FIG 1). DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPEAT INSPECTIONS AT EVERY 5 FLIGSDR TSAA1027018Connector · damagedNON-ETOPS CARGO FLIGHT 551. DURING LANDING, WHEN THE CREW LOWERED THE FLAPS, THERE WAS A FLAP ASYMMETRY INDICATION AT FLAPS 1. THE CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PIN 5SDR CALA2010101800485Connector · corrodedFLAPS UP LANDING NO MOVEMENT FOLLOWED QRH TR EDGE FLAPS POS/SQEW SENSOR C/B OUT WOULD NOT RESET PER FIM 27-57-00-810-822 AND WDM 27-52-11. RESET BREAKER WITH NO CURRENT FAULTS ON FSEU. FLT CONTROL FLAP/SLATS CHECK NORMAL.SDR COMA2010101450221Wire Harness · faultyEN ROUTE FROM CVG TO BWI RECEIVED FLAPS FAIL MSG, FLAPS AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY IN BWI. REMOVED AND REPLACED RIGHT WING BPSU WIRE HARNESS.SDR AALA20101011DFW10Connector · burnedDFW - CREW REPORTED RIGHT WING SPOILERS WOULD NOT STOW ON APPROACH. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BURNED PLUG ON NUMBER 3 SPEED BRAKE POWER CONTROL MODULE. REPLACED PLUG. SYSTEM GROUND CHECK NORMAL OPSDR CA101007012Connector · burnedCREW NOTED A FLAP INDICATION DISCREPANCY, DIVERTED AND LANDED WITHOUT INCIDENT. MX DISCOVERED SEVERAL BURNED PINS IN A CONNECTOR IN THE LT WHEEL WELL THAT HOUSES WIRING FOR MULTIPLE SYS INCLUDING FLAP INDICATION. CONNECTOR D4654J WAS REPLACED AND ACFT RETURNESDR 2010FA0001125Diode · brokenMASTER SWITCH TURNED ON TO START ENGINE FOR FLT RESULTING IN VISIBLE SMOKE & ODOR IN CABIN. RETURNED TO HANGAR & FOUND IMPROPER RESPONSE & FUNCTION OF MASTER SWITCH. INVESTIGATION REVEALED THE MASTER CONTACTOR CONTROL WIRE FROM AIRFRAME GROUND POINT BEHIND ISDR NSVA2010139Wire · brokenNOSE PITCH TRIM INTERMITTENTLY ACTUATES NOSE DOWN IN FLIGHT. FIXED BROKEN WIRE ON SERVO ACTUATOR.SDR SFOA67Wire · chafedDURING POST ENGINE START/PREFLIGHT CHECKS, NOTED THE "SPEED BRAKE EXTENDED" ANNUNCIATOR FAILED TO ILLUMINATE. VISUAL INSPECTION CONFIRMED THE BRAKES EXTENDED, & "HYD PRESS" LIGHT EXTINGUISHED CONFIRMING SYS HAD COMPLETED IT’S CYCLE. ANNUNCIATOR LIGHT TEST PERSDR RAIA201008110002Connector · dirtyDURING LANDING THE RUDDER SYSTEM 1/2 INTERMITTENT FAILED. MAINTENANCE INSPECTED AND CLEANED CONNECTORS AT PRESSURE SWITCHES. SYSTEM OPS CHECKED GOOD.SDR DALA1018351607Connector · disconnectedON CLIMBOUT SLAT HANDLE IN FULL UP POSITION WITH 1 DISPLAYED ON INDICATOR. SLAT WOULD NOT RETRACT. L/E DISAGREE NOTED. QRH PROC ACCOMPLISHED. C/B 6F24 FOUND OUT. BIT PSEU/FSEU NO FAULTS. RESET C/B RAN FLAPS. FLAPS OK NO FAULTS OR MESSAGES. LUBRICATED O
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