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.

SDR QXEA200501387Wire · shortedPDX FLIGHT NR 2133 PFCS - PUSH OFF SPOILER NR 2 LIGHT ILLUMINATED, COMPLIED WITH CHECKLIST. MAINTENANCE TROUBLESHOT, INSPECTED AND FOUND LEFT WING OUTBOARD SPOILER CLUTCH SWITCH WIRES AT 27-15-01. 19G22 AND 23C22N SHORTED TOGETHER FROM CORROSION IN ENVIROMENTOct 28, 2005 · N346PH · Dhav DHC8202SDR COMA0560566Wire · brokenFLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU.Oct 25, 2005 · N952CA · Cndair CL6002B19SDR CA051024003Relay · failedDURING APPROACH, AIRCRAFT ENCOUNTERED FLAP ASYMMETRY. THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE CARRIED OUT TROUBLESHOOTING AND SUSPECTED THE FLAP ASYMMETRY SHUT OFF RELAY TO BE AT FAULT. THE RELAY WAS REPLACED AND THE FLAPS CYCLED NUMEROUS TIMES WITHOUOct 16, 2005 · Boeing 737522SDR SWIA200515623Wire · broken"CPLT ROLL CMD" ADVISORY MESSAGE. CAPTAIN'S AILERONS WORK NORMAL, NO JAM. REPAIRED WIRE CN619A22 AND CN620A22 IAW WDM 20-11-00. OPERATIONAL CHECK GOOD IAW 27-61-20.Sep 29, 2005 · N913SW · Cndair CL6002B19SDR RAIA00509049Wire · unsecureFLT 3518-PIT-MAIN PITCH TRIM INOP. MAINTENANCE RESECURED WIRE ON PITCH TRIM CIRCUIT BREAKER.Sep 29, 2005 · N807HK · Emb EMB145SDR 09132005AGround Wire · looseFLAP WILL NOT GO DOWN WHEN SELECTED 17 DEGREES. MEL'ED FLAP SYSTEM. C/W MEL ON 9/15/2005 FOUND LOOSE GROUND, RESECURED, OPS CHECK GOOD.Sep 12, 2005 · N60MJ · Beech 1900DSDR TAMF20050005OWire · chafedDURING TAKEOFF EICAS MSG L/E SLAT ASSYM DISPLAYED & LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. THE AIRPLANE WAS RETURNED TO RNG FRM 27810500. WIRING W176-102-24 IN P-36 WAS REPAIRED IAW WDM 32-09-11 PAGE 1 SH 2. FIMSep 5, 2005 · N768QT · Boeing 767200SDR 2005FA0001305Wire · damagedINVESTIGATED REPORT OF HORIZONTAL STABILIZER TRIM INOPERATIVE AND SYSTEM CIRCUIT BREAKER TRIPPING WHEN TRIM ACTUATED ON LANDING. CREW REPORTED NORMAL TRIM OPERATIONS SLOW JUST PRIOR TO FAILURE. FOUND BARE WIRING IN COPILOTS CONTROL WHEEL AT PITCH TRIM SWITCHAug 30, 2005 · N494CW · Beech 400ASDR SWIA200515459Wire · brokenDURING RUDDER TRIM TEST, RUDDER TRIM STICKS NL. REPAIRED WIRE ON RUDDER TRIM SWITCH, OPERATIONAL CHECK GOOD.Aug 24, 2005 · N963SW · Cndair CL6002B19SDR S2YA05048Wire · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE FOUND A CHAFED WIRE AT THE LT SAFETY SWITCH. MAINTENANCE REPAIRED THE WIRE, OPS CHECKED THEAug 15, 2005 · N91SK · Beech 1900DSDR GUU2005F00045Connector · looseFLT - 9292 - JAX/TPA - AFTER TAKEOFF, WHILE ADJUSTING THE ELEVATOR TRIM FROM CLIMB TO LEVEL FLIGHT, THE YOKE WAS PULLED AWAY FROM THE FIRST OFFICERS HANDS. IT WAS IF THE TRIMMING CABLE SNAPPED INTO A NEW POSITION. DETERMINED BACK SHELL WIRE BUNDLE CLAMP EAR Aug 11, 2005 · N231YV · Beech 1900DSDR SWIA200515324Socket · damaged"CONTROL FAULT" IN CRUISE PORTION OF FLIGHT OF BOTH OUTBOARD AND NACELLE FLAPS. REPLACED ALL SOCKETS IN ALL 6 FLAP ACTUATOR CONNECTORS. OPERATIONAL CHECK GOOD. REF EMB 120 WDM 20-21-00 AND 20-50-00 AND MM 27-50-00.Jul 28, 2005 · N215SW · Emb EMB120ERSDR SWIA200515347Wire · brokenAFTER DEPARTURE AND MOVING FLAP HANDLE TO 0 RECIEVED A FLAP CONTROL FAULT. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.Jul 25, 2005 · N295SW · Emb EMB120ERSDR AALA20050461Wire · shortedTPA INFLIGHT T2247/25JUL CLIMBING THROUGH FLIGHT LEVEL 220 AUTO PILOT DISENGAGED. CAPTAIN SAYS FLIGHT WAS HARD TO CONTROL IN THE ROLL AND YAW MODE. CAPTAIN DECLARED AND EMERGENCY AND RETURNED TO TPA. FLT LANDED WITHOUT INCIDENT. FOUND SHORTED WIRE IN TAIL COMJul 25, 2005 · N513AA · Doug DC982SDR AWXA200500756Connector · dirtyON LANDING, FLAPS AT ZERO, HOT LANDING. LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED FLAP PROBLEM TO TOWER PRIOR TO LANDING. CREW REQUESTED PRIORITY LANDING DUE TO FLAP PROBLEM. UPON LANDING, CREW WROTE UP FLAP INDICATOR SHOWS SPILT FLAPS AT FLAPS UP POJun 24, 2005 · N174AW · Boeing 73733ASDR SWAA051842Terminal · faultyAIR TURNBACK, AFTER DEPARTURE, L/E FLAPS TRANSIT LIGHT AND NR 1 FLAP OVERHEAD LIGHT STAYED ILLUMINATED. RECYCLED FLAPS, NO CHANGE. REMOVED AND REPLACED NR 1 FLAP GROUND TERMINAL PER MM.Jun 22, 2005 · N373SW · Boeing 7373H4SDR DXTA200500793Ground Wire · faultyDURING CLIMB AROUND FL270, OBSERVED AN AMBER "FLAPS FAIL" CAS MESSAGE. IT RESET/WENT OUT WHEN PRESSED THE FLAP RESET BUTTON. THIS HAPPENED 4 TIMES. ON APPROACH AND LANDING THE FLAPS OPERATED NORMALLY. FOUND FAULTY GROUND AT G7048-COMMON GROUND FOR RESOLVERJun 20, 2005 · N962QS · Cessna 750SDR SWIA200515142Connector · dirtyIN CRUISE FLIGHT, RECEIVED CONTROL FAULT ON FLAPS. REPLACED STALL WARNING TEST PANEL ON CENTER PEDESTAL. CLEANED LEFT WING OUTBOARD FLAP CONNECTOR. OPERATIONAL CHECK GOOD.Jun 13, 2005 · N296SW · Emb EMB120ERSDR PCSA06080501Connector · dirtyFLIGHT 8113 TTPP/SVMC - AFTER DEPARTURE FROM TTPP, CREW REPORTED UNABLE TO RETRACT OUTBOARD FLAPS FROM 5 DEGREES. RETURNED AIRCRAFT TO TTPP USING THE SPLIT FLAP ALTERNATE PROCEDURE IAW AMERIJET 727 AIRCRAFT OPS MANUAL CHAPTER 5 PAGE 53 AND 54. AIRCRAFT LANDEJun 6, 2005 · N495AJ · Boeing 727233SDR 2005FA0000836Circuit Board · looseELECTRIC PITCH TRIM SYSTEM RAN AWAY ON APPROACH. AUTOPILOT/ TRIM DISCONNECT HAD NO EFFECT. PILOT DISENGAGED PITCH TRIM CIRCUIT BREAKER TO STOP THE RUNAWAY. AFTER THE CIRCUIT BREAKER WAS DISENGAGED, THE CONTROL WHEEL VIBRATED ON THE APPROACH AT APPROXIMATELYJun 1, 2005 · N6033N · Cessna T210MSDR SWIA200515070Wire · damagedFLAP DEGRADED STATUS MESSAGE. REPLACED R4 SKEW SENSOR IAW 27-51-15. REPAIRED WIRE CONNECTOR AT R4 SKEW SENSOR IAW 27-51-10. OPERATIONAL CHECK GOOD.May 19, 2005 · N442SW · Cndair CL6002B19SDR MASA200500358Connector · looseASH 7041 RDU TO ORD. THE CREW ABORTED THE TAKEOFF DUE TO THE RUDDER AND AILERON CONFIG TRIM MESSAGE. MAINTENANCE FOUND THE CONNECTOR ON THE AILERON ACTUATOR LOOSE. MAINTENANCE TIGHTENED THE CONNECTOR, SYSTEM AND OPS CHECKED GOOD.May 14, 2005 · N507MJ · Cndair CL6002C10SDR SB05057Connector · intermittentMHT - FL 725 - ON APPROACH, THE FLAPS LOCKED OUT WHEN SELECTED TO 25. THE CREW NOTED A 3 DEGREE SPLIT BETWEEN THE LEFT AND RIGHT FLAPS. CREW PERFORMED A GO-AROUND DURING WHICH THE FLAPS BEGAN OPERATING NORMALLY. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINMay 6, 2005 · N519AU · Boeing 7373B7SDR ARWA20050404Connector · dirtyDURING TAXI, ELEVATOR POSITION INDICATOR (EPI) FAILED DURING FLIGHT CONTROL CHECK. TRANSFERRED TO DMI NR 19171 AS PER MEL 27-9 CAT "C". CLEANED AND SECURED ELEVATOR EPI INDICATOR IN ACCORDANCE WITH M/M 31-10-30. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/Apr 28, 2005 · N441J · Doug DC863FSDR SWIA200514825Wire · brokenON TAXI CHECK, FLAPS SET 15 DEGREES; OUTBOARD FLAPS CONTROL FAULT. REPAIRED BROKEN WIRES ON CONNECTOR CONNECTED TO THE RIGHT HAND OUTBOARD FLAP IAW WM 20-21-00. OPERATIONAL CHECK GOOD.Apr 1, 2005 · N189SW · Emb EMB120ERSDR DHL2005770004Connector · dirtyWHEN FLAPS SELECTED TO 2DEG INBD FLAP ASSYMETRIC PERFORMED ABNORMAL PROCEDURE ISOLATING INBD FLAP MOTOR CONTROL WHEN FLAP SELECTED 5 DEG ASSYMETRIC INBD FLAP LOWERED TO 5 DEG AND OUTBDS LOCKED OUT. ADJUSTED IND AND OUT FLAP XMITTERS AND CLEANED CONNECTORS, OPApr 1, 2005 · N770AT · Boeing 7272B7SDR GTIA050076Wire · brokenUPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K)Mar 26, 2005 · N808NK · Doug DC983SDR CA050328003Fairlead · chafed(CAN) PRESUMED THAT RH AILERON CABLE BROKE DUE TO CHAFFING ON A THE FAIRLEAD. MORE DETAILS WILL FOLLOW ON REVISION 1 OF THE INCIDENT REPORT FILED BY AIR GUYANE SP WITH THEIR LOCAL AVIATION AUTHORITY.Mar 23, 2005 · Dhav DHC6300SDR ARWA20050302Wire · damagedWING SLOT LIGHT DID NOT COME ON. REPAIR WIRES 2F MAIN CONNECTOR P1-10 IN ACCORDANCE WITH M/M 20-50-1. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 27-52-3.Mar 18, 2005 · N906R · Doug DC863FSDR SWIA200514796Connector · failedFLAP CONTROL FAULT. REPLACED CONNECTOR ON LEFT AND RIGHT OUTBOARD ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00.Mar 14, 2005 · N584SW · Emb EMB120ERSDR HNAA0500008Pin · damagedOUTBD ROLL SPLR CAUTION LIGHT ILLUMINATED ON T/O LIGHT WENT OUT ON TOUCH DOWN. MX DUPLICATED PROBLEM ON GROUND USING PITOT PRESSURE. FOUND PIN A ON C/P 9811-J31, NOT SEATED PROPERLY IN PLUG. REMOVED AND REPLACED PIN A. OPS CHECK GOOD. CND AFTER REPINNING.Feb 8, 2005 · N335EX · Dhav DHC8311SDR SWIA200514428Wire · looseTAKEOFF AURAL WARNING TAKEOFF TRIM HEARD ON TAKEOFF ROLL. TRIM WAS INSIDE GREEN BAND. ABORTED, RETURNED TO GATE. REPAIRED SENSOR WIRING WITH NEW CONNECTOR. OPERATIONAL CHECK GOOD.Jan 21, 2005 · N235SW · Emb EMB120ERSDR SWIA200514341Wire · chafedAFTER SELECTING FLAPS 15, CONTROL FAULT LIGHT ILLUMINATED. REPAIRED CHAFED WIRES AT RIGHT OUTBOARD FLAP ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD.Jan 1, 2005 · N189SW · Emb EMB120ERSDR XN0A1216Wire · chafedNR 3 WITH SLAT RETRACTION LOW SPEED AILERONS (RED LIGHT) & CONFIG LIGHT ON FWD PANEL ILLUMINATED. TRANFERED TO DMI LIST IAW ENA A300 MEL 27-11-01, CAT "B" DMI 4824 S.P. 27-11-01 C/W. REPAIRED CHAFED WIRE ON HARNESS TO LSA SERVO OF THE LT WING, SYSTEM OPS CK NDec 14, 2004 · N472AS · Airbus A300B4203SDR SWIA200414095Wire · brokenF/O TRIM SWITCH IS INTERMITTENT. RESOLDERED WIRES TO BACK OF SWITCH. OPERATIONAL CHECK GOOD.Nov 10, 2004 · N932SW · Cndair CL6002B19SDR SWIA200414102Wire · brokenCONTROL FAULT ON FLAPS. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD.Nov 9, 2004 · N291SW · Emb EMB120ERSDR SWIA200414011Wire · twistedFLUTTER DAMPER STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR FLUTTER DAMPER IAW 27-34-05. REPAIRED TWISTED WIRE PAIR CR7B22WHY & CR81322BLU BETWEEN CONNECTORS J300 AND P268. OPERATIONAL CHECK GOOD.Oct 21, 2004 · N430SW · Cndair CL6002B19SDR SWIA200413989Wire · brokenAILERON DISCONNECT LIGHT DOES NOT LIGHT WHEN AILERON DISCONNECTED. REPAIRED BROKEN WIRES AT CONNECTOR ON AILERON QUADRANT. OPERATIONAL CHECK GOOD.Oct 20, 2004 · N251YV · Emb EMB120ERSDR 2005FA0001273Wire · shortedWHILE TROUBLESHOOTING INTERMITTENT UPPER BEACON CIRCUIT BREAKER FAULT, DISCOVERED LT ELEVATOR CONTROL CABLE HAD TORN THROUGH WIRING CONDUIT IN VERTICAL STABILIZER. THE CABLE WORE THROUGH THE CONDUIT AND SHORTED OUT THE WIRING FOR THE UPPER BEACON. REPAIRED WOct 15, 2004 · Cndair CL6013ASDR ASMF200410011Switch · damagedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING TAKE OFF ALARM WAS ON COULD NOT CANCEL IT. TECHNICAL PERSONNEL PERFORMED TAKE OFF CONFIGURATION TEST AND CHECK SLAT, FLAPS, AND SPOILERS, PARKING BRAKES, STABILIZER AND AURAL WARNING WERE CHECK BUT FAIL CONTINUED. DOct 14, 2004 · N751RA · Doug DC987SDR SWIA200413932Wire · broken(STALL FAIL) CAUTION MESSAGE DURING CLIMB. REPAIRED A BROKEN WIRE AND INSTALLED NEW PIN AND CONNECTOR ON FO'S STICK SHAKER. OPERATIONAL CHECK GOOD.Oct 13, 2004 · N959SW · Cndair CL6002B19SDR ARWA20040807Buss Cable · brokenUPON INSPECTION, FOUND LT (LT) AILERON BUS CABLE BROKEN. ALSO FOUND LT AILERON BUS CABLE CRANK PULLEYS WORN. REMOVED DAMAGE CABLE AS REQUIRE IAW MM 27-10-0. FABRICATED NEW CABLE IAW SAMPLE IAW MM 91-10-12. INSTALLED NEW CABLE, ADJUSTMENT AND TEST FOUND NORMAug 31, 2004 · N906R · Doug DC863FSDR CA040831014Terminal Block · shorted(CAN) THE AILERON TRIM FUNCTIONED ONLY IN ONE DIRECTION. THE TERMINAL BLOCK ON THE ELECTRIC CIRCUIT WAS FOUND BURNED (SHORTED) AND WAS REPLACED. AN OPERATIONAL TEST WAS CARRIED OUT OLD PART WAS REPLACED BY A NEW PART AND THE SYSTEM WAS FOUND SATISFACTORY.Aug 28, 2004 · Pilats PC1245SDR SWIA200413758Wire · damagedFLAP FAIL CAUTION WHEN SELECTING FLAPS FROM 0 DEGREES TO 8 DEGREES. REPAIRED WIRING AND REPLACED RIGHT BPSU IAW WM 20-00-00 AND 27-51-10. OPERATIONAL CHECK GOOD.Aug 27, 2004 · N407SW · Cndair CL6002B19SDR SWIA200413706Wire · brokenRUDDER TRIM WILL NOT MOVE NOSE RIGHT. REPAIRED BROKEN WIRE AT RUDDER TRIM SWITCH IAW CRJ WM CHAPTER 20-10-00. OPERATIONAL CHECK GOOD.Aug 16, 2004 · N930SW · Cndair CL6002B19SDR 5336001Wire Harness · shortedAFTER DEPARTURE AND DURING CLIMB (TEB) NOTICED STAB CH 1 INOP ANNUNCIATION ON EICAS. RETURNED TO AIRPORT (TEB). MAINTENANCE TROUBLESHOT TO MCU (MOTOR CONTROL UNIT), REPLACED MCU, OPS CHECK AND RETURN TO SERVICE. DEPARTED TEB AND UPON ARRIVING BAF, STAB CH 1Aug 12, 2004 · N212RR · Cndair CL6002B16SDR SWIA200413665Wire Harness · damagedTRIM RUNAWAY ALARM AND TRIM INDICATOR ERRATIC, MACH TRIM MESSAGE. REMOVED AND REPLACED CHANNEL 1 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. REMOVED AND REPLACED CHANNEL 2 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONAug 1, 2004 · N915SW · Cndair CL6002B19SDR SWIA200413573Wire · brokenCONTROLS DISENGAGE LIGHT ON MAP COMES ON INTERMITTENTLY. REPAIRED BROKEN WIRE NEAR AILERON DISCONNECT IAW 20-00-00, OPERATIONAL CHECK GOOD.Jul 13, 2004 · N561SW · Emb EMB120ERSDR SWIA200413564Wire · brokenNO LIGHTS OR ALARMS SOUNDED DURING AILERON/ELEVATOR DISCONNECT OPERATION. REPAIRED TWO BROKEN WIRES WERE NEAR THE CONNECTOR AT THE ELEVATOR DISCONNECT. OPERATIONAL CHECK GOOD REFERENCING MM 27-13-01.Jul 9, 2004 · N576SW · Emb EMB120ERSDR SWIA200413510Wire · brokenFIRST OFFICER'S ELECTRIC TRIM WHEN PUSHED FORWARD, SETS OFF THE TRIM FAIL WARNING. REPAIRED WIRE AT TRIM SWITCH.Jun 23, 2004 · N188SW · Emb EMB120ER
Back to JASC 2797