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 2003UALA00252Wire · failedCREW RECEIVED L/E SLAT ASYMMETRY DISAGREEMENT EICAS MESSAGE. FOUND WIRES FOR 12R OUTBOARD SLAT SKEW LOSS SW S2314 AND FLEX CONDUIT BROKEN APPROXIMATELY 3 FEET INBOARD OF SWITCH. REPAIRED WIRES AND INSTALLED INTERIM CONDUIT. ENTERED CF ITEM TO MAKE PERMANENTSDR SWIA200311805Circuit Breaker · trippedFLAP FAIL AFTER TAKEOFF. RETURNED TO FIELD. RESET CIRCUIT BREAKER 1F4 AND 2F4. OPS CHECK GOOD AFTER RESET OF CIRCUIT BREAKERS.SDR SWIA200311790Connector · contaminatedFLAP DISAGREEMENT ON FLAP RETRACTION ON TAKEOFF, OUTBOARD FLAPS. RETURNED TO SLC. INSPECTED OUTBOARD FLAPS CONNECTORS, FOUND GLYCOL IN LEFT OUTBOARD CONNECTOR. CLEANED LEFT OUTBOARD CONNECTOR AND RAN FLAPS 10 CYCLES. OPS CHECK GOOD. NO FAULTS AT THIS TIMESDR SWIA200311732Wire · chafedSTAB CHANNEL NR 1 FAILED ON PUSHBACK. FOUND A CHAFED WIRE AT CONNECTOR J3CP WIRE CD83622WHT. RE-PINNED WIRE IAW CRJ WM 20-00-00. PERFORMED OPS CHECK OF STAB TRIM SYSTEM IAW CRJ MM 27-41-00. CHECKS GOOD. 1/26/2003 - STAB TRIM CHANNEL 1 FAILED.SDR SWIA200311708Wire · chafedFLUTTER DAMPER STATUS MESSAGE IN FLIGHT, AMBER ARC ON L AILERON ON FLIGHT CONTROL SYNOPTIC PAGE. NO CHANGES TO CONTROLLABILITY ON CONTROL FEEL NOTED. FOUND CHAFED WIRE IN MIDDLE WING SECTION LEADING EDGE. REPAIRED WIRE IAW WMM 20-16-00. OPS CHECK GOOD.SDR SWIA200311685Connector · shortedSTAB TRIM CH. 2 WILL NOT ENGAGE. FOUND BURNED AND SHORTED PIN B AT J6CD. REPLACED CONNECTOR AND REPAIRED WIRING. STAB TRIM OPS CHECKS GOOD.SDR CA030106004Connector · burned(CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR AND 3 INCHES OF ASSOCIATED WIRING DAMAGED ATA/P STAB TRIM MOTOR CONNECTION. WIRING REPAIRED, CONNSDR SWIA200311675Connector · wornFLAPS WOULD NOT RETRACT, DISAGREEMENT WITH THE OUTBOARD PAIRS, WOULD NOT CORRECT. FOUND LEFT OUTBOARD FLAP CONNECTOR TO HAVE FLUID INSIDE AND WORN BACKSHELL. REPLACED CANNON PLUG AND BACKSHELL. APPLIED SUPER CORR-B TO CANNON PLUG AND CONNECTORS. OPS CHECK SDR SWIA200211668Wire · damagedFLAPS INDICATE DIFFERENT VALUES AT 20 DEGREE SETTING. RETURNED TO GATE. REINSTALLED WIRE AT PIN 40 P211, RE-POWERED AND INITIALIZED FLAP SYSTEM. PERFORMED EXTENSIVE OPS CHECK OF FLAPS. ALL INDICATION FOUND TO BE MATCHED AND NORMAL.SDR SWIA200211623Wire · chafedAFTER TAKEOFF RECEIVED A TRIM FAIL AURAL WARNING AND THE TRIM FAIL LIGHT ON THE MAP CAME ON AND CONTINUED FOR APPROXIMATELY 5 MINUTES. RETURNED TO LAX. INSPECTED ELEVATOR TRIM WIRING ON TOP OF TAIL. FOUND CHAFED WIRE TO LEFT PROXIMITY SENSOR AND CORRODED COSDR SWIA200211628Wire · frayedDURING FIRST FLIGHT OF THE DAY AUTOPILOT TEST, RECEIVED -YAW DIS- ON FIRST OFFICER'S FLIGHT CONTROL PANEL AND ASSOCIATED -YAW DIS- ON AP CONTROL PANEL. ALSO -R- ON AUTOPILOT CONTROL PANEL. UPON INSPECTION FOUND RUDDER TRIM ACTUATOR CABLE WIRE FRAYED AND BINDSDR CA030106006Connector · damaged(CAN) UPON LANDING ONE OF THE RT SPOILERS DEPLOYED ON THE TAXI IN FOR NO APPARENT REASON. RT O/B SPOILERON PCU FOUND TO HAVE A NUMBER OF PINS IN THE CONNECTOR PLUG PUSHED BACK IN. THE SPOILER ELECTRONIC CONTROL UNIT PN 4916405, SN 0599 WAS ALSO REPLACED DUE TSDR 02FDEA00943Wire · failedON ARRIVAL, WHEN TRAILING FLAPS EXTENDED TO 5 DEG, THE AMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINATED ON FO PANEL AND THE NR 5 LEADING EDGE FLAP LIGHT (BOTH GREEN AND AMBER), DID NOT ILLUMINATE ON SO PANEL. RAN QRH PROCEDURE AND DIVERTED. ON ARRIVAL, FSDR 02FDEA00924Wire · damagedON CLIMBOUT, DURING FLAP RETRACT, MOVED HANDLE FROM FLAP 5 TO FLAP 2 AND 6. LEADING EDGE FLAP SHOWED IN TRANSIT ON S/O AUX PANEL WITH AMBER LEADING EDGE FLAP LIGHT ON FOWARD PANEL. INSTALLED JUMPER CABLE ON NR 6 LEADING EDGE FLAP IAW MM. MAINTENANCE ANDSDR RAIA00211334Computer · inoperative5256-PIT- STALL PROTECTION SYSTEM WARNING INDICATION.MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION COMPUTER, OPS CK OK.SDR DLM88021357Wire Harness · damagedPRIMARY TRIM CAUSED A/P AND A/T TO KICK OFF WHEN ACTUATED.CPTS PFD AND NAV DISPLAY BLANKED OUT AND ALL COCKPIT LIGHS DIMMED WHEN TRIM ACTUATED. UPON INSPECTION FOUND WIRE BUNDLE AT PRIMARY AND ALTERNATE TRIM BURNT. SUSPECT WIRES CHAFED DUE TO CONTACT WITH ONESDR SWIA200211484Wire · brokenWITH AUTO PILOT SELECTED TO CAPTAIN'S SIDE, RECEIVED RED ''TRIM FAIL'' ON MAP, WITH TRIPLE CHIME AND AURAL WARNING AFTER ROTATION AND DURING LANDING ROLLOUT. REPAIRED WIRING TO NR 1 TRIM SWITCH AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00.SDR CA021115001Wire Harness · failed(CAN) AFTER TAKE OFF, WHEN FLAPS WERE RETRACTED, STALL FAIL CAUTION MESSAGE APPEARED ACCOMPANIED BY HYD CAUTION FOR HYD PUMP 1B & 3B. STALL TAPE ON CAPTAINS & F/O'S PFD APPEAR TO RUN FULL LENGTH OF AIR SPEED INDICATOR. AIRCRAFT FERRIED FOR TROUBLESHOOTING. SDR AUS20021196Connector · contaminated(AUS) CONNECTOR "H" LOCATED AT 162-00-00 IN THE RT MAIN LANDING GEAR BAY MOISTURE CONTAMINATION.SDR CA021015008Wire · pinched(CAN) DURING RETURN TO SERVICE TESTING AFTER A MAINTENANCE DOWNTIME, THE FLAPS WERE OPERATED AND WHEN THEY REACHED APPROXIMATELY 30 DEGREES, AN AVIONICS SMOKE MESSAGE WAS OBSERVED. PRIOR TO POWER BEING REMOVED FROM THE A/C, A SLAT/FLAP HALF SPEED MESSAGE WAS SDR SWIA200211238Wire · brokenRUDDER TRIM WILL MOVE LEFT, BUT NOT RIGHT. SOLDERED BROKEN TERMINAL/WIRE CONTACT ON RUDDER TRIM CONTROL KNOB. OPS CHECK GOOD.SDR SWIA200211213Wire · brokenRUDDER TRIM INOP, WILL NOT MOVE LEFT OR RIGHT. FOUND WIRE BROKEN OFF OF RUDDER TRIM SWITCH. SOLDERED WIRE BACK ONTO SWITCH. OPERATED RUDDER TRIM & CHECKED NORMAL.SDR KC82002F00004Terminal · corrodedNORMAL PITCH TRIM FAILED SHORTLY AFTER TAKE OFF. MAINTENANCE REPORTED FINDING MAIN TRIM POWER WIRE CORRODED AND LOOSE ON RELAY NR 354 LOCATED IN HELL HOLE AREA. TERMINAL END WAS CLEANED AND RESECURED. PERFORMED TRIM SYSTEMS OPERATIONAL CHECK IAW SRM.SDR KBMA115445Bonding Jumper · wornBONDING BRAID WORN, BEYOND LIMITS. (BROKEN) REPLACED WITH NEW BONDING BRAID.SDR SWIA200211154Wire · damagedRUDDER TRIM INOP. INSPECTED RUDDER TRIM CONTROL SWITCH PANEL. REPAIRED WIRE CONNECTION. OPS CHECK GOOD.SDR SWIA200211103Wire · disconnectedRUDDER TRIM WILL ONLY GO NOSE RIGHT. SOLDERED WIRE BACK ON CONTROL POTENTIOMETER. OPS CHECK GOOD.SDR SWIA200211069Wire · shortedAT ROTATION, WINDSHEAR FAIL STATUS MESSAGE AND STICK SHAKER ACTUATION UP TO 180 KNTS. RETURNED FOR LANDING AT SLC. FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG P1CF. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOCKETS ON ALL WIRES TOSDR CA020715007Wire Harness · chafed(CAN) DURING INSPECTION, AN ELECTRICAL SHORT WAS NOTICED AT THE BASE OF THE PILOTS CONTROL COLUMN. WIRING BUNDLE RUNNING UP THE CONTROL COLUMN WAS CHAFING ON THE STRINGER TO WHICH THE CONTROL COLUMN IS MOUNTED. THE CO-PILOTS COLUMN WAS INSPECTED AND SIMILAR CHSDR SWIA200211054Wire · shortedUPON ROTATION IN OKC, THROUGH 10 DEGREE PITCH UP, STICK SHAKER ACTIVATED. WINDSHEAR FAIL STATUS MESSAGE AND CONTINUOUS IGNITION, AIRSPEED WAS ROUGHLY 165 KTS. THEN ON FINAL IN SLC, GEAR WAS COMING DOWN, WINDSHEAR FAIL MESSGE APPEARED AGAIN, CONTINUOUS IGNITISDR USAASB02122Wire · chafedPIT - FLT 1591 - ON CLIMB-OUT FROM PHL, EN ROUTE TO ORD, CAPTAIN REPORTED THE NR 3 LEADING EDGE SLAT WAS INDICATING INTRANSIT AND WOULD NOT RETRACT. LEFT AILERON TRIM OF 1.5 TO 2 UNITS WAS REQUIRED TO LEVEL WINGS AT 230 KNOTS. DECISION WAS MADE TO DIVERT TO SDR GTIA020688Wire · brokenDEN - FLT 980A - SETTING MAX POWER FOR DEPARTURE GOT THE FLAP AURAL WARNING WITH FLAPS SELECTOR 4.5 OPTIUM. TROUBLE SHOT SYSTEM FOUND FLAP TAKEOFF SETTING WARNING S/W AT CONNECTOR AT D-1 1194 PINE BROKEN WIRE REPAIRED IAW MM CH 20 TAKEOFF WARNING SYSTEM. OPSSDR C1HA200288013Wire Harness · damagedFLAP DID NOT AGREE WITH INDICATOR FLAP NR 1 LEADING EDGE SLAT WAS UP BUT INDICATED DOWN. FOUND WIRE BUNDLE BETWEEN NR 3 SLAT ACTUATOR & OUTBOARD SLAT TRACK ARCED THROUGH MULTIPLE WIRES. REPAIRED WIRES IN AREA USING STD PRACTICES IN MM 20-11-31.SDR GTIA020520Wire · brokenRSW - FLT 926 - CAPTAINS LONGITUDINAL TRIM SWITCH WILL NOT WORK IN THE NOSE DOWN POSITION. REPAIRED BROKEN WIRE C1209A20 IN FORWARD CARGO PIT RIGHT TUNNEL FOR CAPTAINS PRIMARY TRIM, OPS CHECK NORMAL. (M)SDR 02FDEA00315Wire · damagedDURING TAXI ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON. LOW PRESS LIGHT C/B ON. HYD A & B FILTERS CHECK GOOD. PITOT TUBES ON TAIL WERE CLEAN. SPLICED IN NEW SECTION OF WIRE PER SMP, OPS CHECK NORMAL.SDR GTIA020406Wire · brokenFTW - FOUND ALTERNATE TRIM CONTROL LEVERS ON CONTROL PEDESTAL INOPERATIVE. TROUBLESHOT, FOUND 4 SPLICE IN THE TAIL (HORIZ STAB) PULLED OUT, NEED TO RESPLICE. REPAIRED BROKEN WIRES RESPLICED. (M)SDR SWIA200210802Wire · brokenFLAP CONTROL FAULT ON FLAP INDICATOR PANEL AND FLAP/ADVANCED STALL WARNING ON MAP. ABORTED TAKEOFF. REPAIRED BROKEN WIRE AT NR 8 PIN ON LEFT OUTBOARD ACTUATOR. OPERATED FLAPS. OPS CHECK GOOD.SDR GTIA020449Wire · brokenFTW - FOUND LEFT ELEVATOR POSITION SENSOR FAILS DFDR TEST, OCTAL DISPLAY DOES NOT CHANGE. T/S FOUND 2 WIRES BROKEN. REPAIRED BROKEN WIRES. (M)SDR SWIA200210744Wire · chafedAFTER ENGINE START, CONTROL FAULT FLAP AND ADV SWS ILLUMINATED AND WOULD NOT RESET. INSPECTED RIGHT INBOARD WIRE BUNDLE FROM P1756 TO P0366 AND FOUND WIRES CHAFING INTO W602-0007-22. REPAIRED WIRE AND RECONNECTED. OPS CHECKED FLAPS 20 TIMES. NO DEFECTS NOTSDR AC2A0000345Connector · inoperativeREMOVED AND REPLACED CONNECTOR.SDR SWIA200210712Wire · brokenWIRES BROKEN OFF OF THE ROLL DISCONNECT SWITCH. REMOVED AND REPLACED ROLL DISCONNECT SWITCH IAW CRJ MM 27-12-10. OPS CHECK GOOD.SDR AUS20020109Wire · mismanufactured(AUS ) SPOILER SYSTEM WIRING INCORRECT. MANUFACTURING ERROR.SDR SWIA200210564Wire · brokenON TAKEOFF ROLL, CONTROL DISENGAGE MAP LIGHT ILLUMINATED. ABORTED TAKEOFF. REPAIRED BROKEN WIRE ON CONTROL DISENGAGE CONNECTOR 2P1421. OPS CHECK GOOD. PLACARD REMOVED.SDR MEX2002263Wire · brokenDURING TAXI CAPTAIN INFORMED THAT THE LIGHT OF RUDDER TRAVEL UNRESTRICTED DID NOT TURN ON. PROXIMITY SWITCH WAS VERIFIED AND FOUND A FAILURE IN THE CARD 706. PROXIMITY SWITCH WAS REPLACED BUT FAILURE DID NOT CORRECT. PROXIMITY SENSORS WERE VERIFIED AND SOMESDR MALA010728Connector · dirtyAFTER T/O ON FLIGHT 2904 MAIN PITCH TRIM FOUND TO BE INOP. MAIN PITCH TRIM FAILED ON CLIMBOUT, INOP FROM BOTH CAPTS AND F/O'S SIDE. STANDBY TRIM OPERATES NORMALLY AFTER ABOUT 10 MINUTES MAN TRIM STARTED WORKING MOMENTARILY. AIR TURNBACK TO DTW. MAINTENANCESDR DHL2001712015Wire · brokenON WALK AROUND FOUND LT AILERON BUSS CABLE BROKEN, LT MLG W/W.R&R LT AILERON BUSS CABLE (CORRODED)R&R RT AILERON BUSS CABLE AS PRECUTION.SDR BJNA010901Connector · dirtyWING FLAP POSITION INDICATOR SHOWED FLAPS NOT RETRACTED THE LAST 5 DEGREES IN FLIGHT. FUNCTIONAL TEST OF FLAP RETRACTION AND EXTENSION SYSTEM BY MAINTENANCE OK. REMOVED FLAP POSITION INDICATOR TRANSMITTER ELECTRICAL CONNECTOR, CLEANED, INSPECTED AND RECONNECSDR 2001UALA02058Connector · looseSTATUS MESSAGE ON TAKEOFF, FLAPS CONF WITH FLAPS IN POSITION 10 DEGREES. ABORTED TAKEOFF AT 100 KTS. FOUND LEFT OUTBOARD TRAILING EDGE FLAP DRIVE CANNON PLUG NOT SECURED. SECURED CONNECTOR MESSAGE CLEARED. FLAPS OPS NORMAL NOW.SDR AUS20010699Wire · broken(AUS) FLAP SELECTOR LOOM WIRE BROKEN FROM CRIMP TO FLAP MICROSWITCH.SDR DL767002243Wire · shortedAFTER FINDING CONDENSATION DRIPPING FROM COCKPIT OVERHEAD PANEL AT THE TOP OF C/B PANEL FOUND NUMEROUS BURNT WIRES ON P6-15 PANEL. REPAIRED WIRES PER MM CHAP 20.SDR AU000066Wire Rope · frayed(AUS) RT AILERON CONTROL CABLE A4B-3 FOUND FRAYED AT WING STATION 531 FAIR LEAD. ALL STRANDS EXCEPT THE HEART STRAND WERE BROKEN. THE ADJACENT WIRE ROPE A4A-3 HAD BROKEN WIRES AND THE ENTIRE LENGTH OF BOTH WIRE ROPE RUNS WAS WORN AT THE FAIR LEAD LOCATIONS.
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