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 CA140526012Wire Harness · out of position(CAN) UPON DEPARTING THE GATE FOR FLIGHT, THE CREW, WHILE PERFORMING FLIGHT CONTROL CHECKS EXPERIENCED RESTRICTED LT AILERON CONTROL DEFLECTION AND FULL RT AILERON CONTROL DEFLECTION. THE ACFT RETURNED TO THE GATE. MAINTENANCE DISCOVERED THE AILERON BELLCRANSDR CA140521006Wire Harness · broken(CAN) WIRE FOUND BROKEN DURING FLEET CAMPAIGN TO CHECK FOR BROKEN WIRES. FLAP OPERATED NORMALLY.SDR CA140505011Wire · broken(CAN) FLAP STUCK AT FULL FLAP. WOULD NOT MOVE UP OR DOWN. NO INDICATION IN COCKPIT. FOUND WIRE AT SYMMETRY SWITCH BROKEN. THE SYMMETRY UNIT MOVES WITH EACH CYCLE OF THE SYSTEM. THE WIRE GETS BENT EACH TIME EVENTUALLY CAUSING FAILURE AT THE TERMINAL END.SDR SAJF2014042803014Connector · defectiveDURING FLAP SET 1, FLAP ASYMMETRY, LT FALL BELOW 0 DEG, RT AT 0 DEG, CREW PERFORMED ALL FLAP UP LANDING PROCEDURE. IAW AMM 27-51-00 CHECK FCU RIGGING PIN NML. IAW AMM 27-51-00 CHECK FLAP TRACKS DIM Y WITHIN LIMIT. IAW AMM 27-59-00 PFM FLAP SKEW DETECTION SYSDR HALA2014032500040Wire · damagedECAM MESSAGE PRIM 1 FAIL. F/O SIDE STICK FAILED. MCC SWAPPED FCPL 1 & 3. PERFORM SIDESTICK OPS TEST AMM 27-92-41&27-93-34 CAPT SIDESTICK TEST OK. F/O SIDESTICK FAILS VERTICAL COMMAND. PERFORMED GROUND SCAN OF EFCS 1 & 2 IAW AMM 27-96. FAULT MESSAGE FCPC1 (SDR CA140319008Splice · broken(CAN) SPLICE IN WIRING FOR LOWER RUDDER PCU JAM INDICATOR MICRO SWITCH, WIRES BROKEN OFF.SDR SIMA20140214016Connector · corrodedLEFT GND SPOILER PROXIMITY CONNECTOR & BACK SHELL P1167 CORRODED. R & R THE LT GND SPOILER PROXIMITY CONNECTOR & BACK SHELL P1167 IAW SWPM 20-50-01 STEP 23, 20-50-05, 20-50-00 STEP 9.SDR P5CA2014021400002Connector · burnedRUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. TROUBLESHOOTING FOUND E1-2 SHELF WIU 1420 CONNECTOR D1288A PINS; A1 AND A2 BURNED. RELOCATED PINS TO A6 AND A7 OF SAME CONNECTOR IAW EO 4424A053, REV 0. RUDDSDR P5CA2014021000001Wire · burnedRUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. CIRCUIT BREAKER FOR THE RUDDER RATIO CHANGER CONTROL WAS FOUND TO BE TRIPPED AND WOULD NOT RESET. FURTHER INVESTIGATION FOUND WIRES AND POSTS IN THE WIRE INTSDR AALA20140208015Connector · defectiveMIA CREW REPORTED FLAPS FAILED TO EXTEND DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. WIRE INTERMITTENTLY OPEN FROM FLAP SLAT ELECTRONICS UNIT RACK CONNECTOR TO SKEW CONNECTOR. REPLACED SKEW SENSOR SDR C77A20140203004Wire Harness · failedSLAT FAIL EICAS MESSAGE.SDR C77A20140203003Wire Harness · failedSLAT FAIL EICAS MESSAGESDR C77A20140203002Wire Harness · failedSLAT FAIL EICAS MESSAGE.SDR C77A20140203001Wire Harness · failedSLAT FAIL EICAS MESSAGE.SDR VNAA2014012200012Wire · pulledCREW REPORTED SLAT FAULT STATUS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, FOUND PULLED WIRE ON SENSOR SPLICE, R & R SPLICE AND PINS, RESET BOTH LT OTBD SLAT ACTUATORS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASESDR CA140122004Connector · burned(CAN) WHILE IN CRUISE, THE LEFT AC BUS CAUTION LIGHT ILLUMINATED ALONG WITH ASSOCIATED TRU AND LT ELEVATOR HORN HEAT CAUTION LIGHT. MAINTENANCE TROUBLESHOOTING REVEALED THE RT AC CONTACTOR PANEL CONNECTORS 2421-J6, MS 3476L22-41S AND 2421-P6, MS 3474L22-41P, SDR CALA201401090001Connector · corroded01/09/2014 DEN, FLAPS STUCK AT 15, CORRECTED 01/09/2014 DEN, FOUND FLAP FUNCTION NORMAL AFTER ARRIVAL & POWER SWITCHED. PERFORMED FSEU BITE. FOUND TE FLAPS SENSOR DISAGREE INACTIVE INTERMITTENT IAW FIM 27-51-00-810-801. CORRECTED 01/22/2014 EWR CORROSION SDR SIMA20131225003Connector · contaminatedSPOILER FAIL IN FLIGHT DURING DESCENT WITH REDUCED POWER, THEY DID NOT DEPLOY. CLEANED CONTAMINATION FROM SPOILER PROX SENSOR CONNECTOR. R & R LT INBD SPOILER PROX SWITCH IAW 140 AMM 27-63-04, OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20131223004Connector · looseON DESCENT, SPOILER FAIL MESSAGE ON EICAS. SPOILERS WERE NOT SELECTED BUT WERE INDICATING OPEN. FOUND LT INBD SPOILER PROX SWITCH CONNECTOR LOOSE. SECURED CONNECTOR IAW 140 AMM 27-63-04. PERFORMED OPERATIONAL CHECK IAW 140 AMM 27-63-01, OPERATIONS CHECKED SDR CALA2013122393873Connector · defectiveAUTO SPEED BRAKE DID NOT DEPLOY ON LANDING. REPLACED S10697 & CONNECTOR RT GEAR TILT SWITCH IAW WDM 27-62-01. AUTO SPEED BRAKE OPERATIONS CHECKED GOOD.SDR HNAA2013121600617Connector · dirtyRUDDER TRIM INOPERATIVE. INSPECTED AND CLEANED ACTUATOR CONNECTOR. OPS CHECKED GOOD.SDR CALA2013120693506Wire Harness · damagedFLAPS LOCKED UP ON FLAP EXTENSION ON TAXI OUT. REPLACED THE WIRE HARNESS FROM THE PROX SENSOR FOR THE FLAP INTERCONNECT CONNECTOR TO THE CONNECTOR IN THE INBD CANOE, 7541VC-7505VC-A & 7543VC-7503VC-A IAW AMM MT 27-019. IAW PTT SEQ 4948004 & 4948005.SDR CALA2013120593484Wire Harness · out of positionSPEED BRAKE HANDLE COVER REMOVED FOR ACCESS. WIRE BUNDLE SHOWS EVIDENCE OF WEAR & INTERFERING WITH HANDLE OPERATION. FOUND NO WIRE DAMAGE REPOSITIONED WIRE BUNDLE TO CLEAR HANDLE.SDR CA131129008Wire Harness · failed(CAN) JUST AFTER TAKEOFF CREW RECEIVED A WING A/ICE 1 LEAK EICAS. QRH DIRECTED CREW TO EXIT/AVOID ICING CONDITIONS. AFTER CONSULTATION WITH SOC/DISPATCH, CREW DIVERTED. W513 HARNESS REPLACED AND OPS NORMAL. AMM 30-11-02.SDR SWIA201335602Connector · chafedRT WING SLAT NR 3 HAS CONNECTOR MT175P2 CHAFED THROUGH. C-CHECK REPLACED RT WING SLAT NR 3 CONNECTOR IAW ESPM & AMM.SDR UIEA2013111900562Wire · chafedREF: SPOILER PCU NR 7 PROBLEM HISTORY. DURING TROUBLESHOOTING CABLE W27R4-30-20R, CHAFED UNDER P-CLIP REF WDM 27-61-31 PAGE 1;SAME WIRE TEMPORARILY REPAIRED IAW EO 4827A014, REV 0, PART 1, PART 2, PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 10 FLIGHT CYCLES.SDR SIMA20131118024Connector · corrodedRUDDER POSITION TRANSMITTER CONNECTOR CORRODED. CLEANED THE RUDDER POSITION TRANSMITTER CONNECTOR OF MINOR SURFACE OXIDATION, DIRT, GRIME & THEN APPLIED A SURFACE CORROSION PREVENTATIVE. ALL WORK DONE IAW CRJ ESPM CHAPTER 20-26-00.SDR CALA2013112193153Wire · unsecureONE OR MORE PFCS INTERFACE SIGNALS INOPERATIVE. SECURED JUMPER WIRE BETWEEN CB C23403 & C9117 IN P210. ALL MESSAGES CLEARED SYS OPERATIONS NORMAL.SDR AALA20131118001Wire Harness · chafedSTL PILOT REPORTED 2 OF 3 PRIMARY TRIM CIRCUIT BREAKERS POPPED. AIRCRAFT REMOVED FROM SERVICE. UPON MAINTENANCE CHECK, FOUND WIRE BUNDLE FOR PRIMARY TRIM MOTOR ARCED AGAINST FRAME. REPAIRED WIRING AT P10-399 PR1 STAB MOTOR. SYSTEM GROUND CHECKED NORMAL OPESDR AALA20131109018Wire · damagedLAX CREW REPORTED LE FLAP ASYMMETRY. EMERGENCY DECLARED FLIGHT PERFORMED GO AROUND & LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HIGH RESISTANCE FROM PROXIMITY S297 TO D4378J PLUG. REPLACED WIRE, SYSTEM GROUND CHECKED NORMAL OPERATIONSDR UHLA2013110700575Connector · unsecureSLAT FAIL MESSAGE IN FLIGHT AFTER F/O SELECTED FLAPS UP. DECLARED AN EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. FOUND RT NR 3 SKEW SENSOR CONNECTOR LOOSE. CLEANED AND RESECURED CONNECTION IAW SWPM CHAPT 20-61-20 MM, OPS CHECK GOOD. CLEANED ANSDR NOCA2013102615Circuit Breaker · openL/E SLAT DISAGREE STATUS MESSAGE AT FL 350. FOUND CIRCUIT BREAKER DC STANDBY A2 ON P6-1 PANEL OPENED. RESET CIRCUIT BREAKER IAW AMM 20-60-01 ACCOMPLISHED FIM TASK 27-51-00, FIG 104. NO FAULTS FOUND.SDR CALA2013101892177Wire · damaged"STAB TRIM" STATUS MESSAGE DISPLAYED UPON T TRIMMING STAB NOSE UP WITH "ALTERNATE STAB TRIM SWITCHES" ON PEDESTAL. CMC SHOWS MESSAGE 27147. WITH NR 2 CUTOUT SW ENGAGED ONLY NR 3 IN CUTOUT POS STAB TRIM FAILS TO MOVE TO THE NOSE UP POSITION WITH "ALTERNATE STSDR DALA13051103269Connector · failedDURING APPROACH FOR LANDING AND AFTER COMMANDING FLAPS 2 DEG, 30 SEC LATER FLT/CTL FLAPS FAULT APPEARED ON THE UPPER ECAM SCREEN. CREW FOLLOWED QRH PROCEDURE, DECLARED EMERGENCY AND LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED CONNECTOR 7541VC, 7505VC, 7543VSDR RAIA201309040002Connector · corrodedSPOILER FAIL MESSAGE IN FLIGHT, SPOILERS SHOW OPEN ON GROUND. MX REPLACED CONNECTOR AT RT INBD SPOILER PROXIMITY SWITCH, OPS CHECK GOOD.SDR CA130801008Wire · chafed(CAN) REF: DEFECT-1125200 AFTER T/O IN CLIMB FELT STIFF ROLL CONTROL. DISCONNECT EXECUTED AND JAM DETERMINED TO BE ON RHS. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT (AILERON TRIM INDICATOR) (RESOLVED ON W/O: 393834 TASKCARD: NR-00001) FOUND AILERON TRIM SDR UALA2013071805038Wire Harness · damagedFLAP FAULT ON ECAM, RETURNED TO FIELD. REPLACED WIRE HARNESS, OPS OK IAW AMM 27-54-00-710-002-A.SDR UALA2013071204865Connector · unsecureORT AILERON SERVO VALVE FAULTED PERFORMED AILERON SERVO VALVE REMOVAL UP TO STEP 4A.(2). LOOSENED MOUNTING SCREWS. FOUND CONNECTOR NOT LOCKED ON OTBD AILERON SERVO LOCKED PLUG, OPS CHECKED GOOD IAW AMM.SDR AALA20130706001Pin · damagedRT SPOILER OVER RIDE ACTUATOR CANNON PLUG HAS A BENT PIN PREVENTING INSTALLATION OF SHORTING CAP. R&R RT WING SPOILER OVER RIDE ACTUATOR.SDR CA130626005Wire · failed(CAN) DURING A PREFLIGHT CHECK THE PILOT COULD NOT OPERATE THE PITCH TRIM AND FOUND THE BREAKER CHANNEL NR 2 POP OUT. AFTER THE INVESTIGATION BY THE AME HE FOUND THAT THE BUNDLE WIRES THAT GOES ON THE CANNON PLUG P8CD ATTACH TO THE TRANSIENT SUPPRESSOR BOX WASSDR UALA2013062104319Conduit · damagedFOUND SMALL CONDUIT DAMAGED FROM 7543VC LEADING AFT INTO MAIN CONDUIT THAT LEADS TO 7503VC. DAMAGED WIRE IN CONDUIT HAS BEEN REPLACED. REQUIRES NEW CONDUIT AND 7543VC RECEPTACLE REPINED. CONDUIT PINNED. R & R CONDUIT AND REPINED 7503VC RECEPTACLE REF ESPM ASDR AWKA201306180001Pin · bentCLIMBING THROUGH 2000 MSL ON DEPARTURE, ENROUTE, FLIGHT CREW RECEIVED AN AMBER PITCH FEEL FAIL MESSAGE. DIVERTED. THE APPROACH AND LANDING WERE UNEVENTFUL. DURING INSPECTION, TWO PINS ON CIRCUIT BOARD NK122 WERE BENT. PINS WERE REALIGNED, PCB REINSTALLED, ASDR CHQA20130604195Connector · dirtyCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AS A PRECAUTION AND LANDED WITHOUT INCIDENT AT THEIR INTENDED DESTINATION. MX CLEANED AND RESEATED THE CONNECTOR PLUGS ON THE FLAP ELECTRONIC CONTROL UNIT AND RESESDR UALA2013053103796Wire · shortedDURING FLAP SELECTION FROM 1 TO 5, EICAS L/E SLAT ASSYM INDICATED. FOUND SPLICE SP2198 SHIELDING SHORTING TO CENTER CONDUCTOR, REPAIRED IAW WDM 27-81-31 AND SWP 20-10-15, OPS CHECKED GOOD. NO FAULTS ON FSEU AND NO EICAS MESSAGES NOTED AT THIS TIME.SDR UALA2013052203545Wire Harness · faultedFLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FLAP WIRING AND OPS CHECKED GOOD.SDR UALA2013052303560Wire · damagedNR 1 FLAP SLAT SENSOR CIRCUIT BREAKER WILL NOT RESET. ACCOMPLISHED SLICE REPAIR ON WIRES W3326-2510, R20 AND W3326-2510 B20 IAW WDM 27-51-41. IAW BSWPM 20-30-19, SPLICE NEW WIRES FROM FSS 720 TO FSS 812 AND TERMINATED AT CONNECTOR D2984, REF BSWPM 20-10-11. SDR CA130508008Connector · failed(CAN) DURING CLIMB, FLIGHT CREW RECEIVED A, FLAP POWER, CAUTION MESSAGE AFTER SELECTING FLAP, FROM 5. FLIGHT CREW TRIED TO MOVE THE FLAPS BACK TO 5 DEGREES WITH NO SUCCESS, FLAPS REMAINED AT 3. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINSDR HNAA2013050300251Connector · dirtyFLAP DRIVE CAUTION LIGHT FLICKERING DURING CRUISE FLIGHT. ON CONTINUOUSLY FOR APPROX 30 MINUTES. STAYED OUT AFTER LANDING. FLAP OPS NORMAL. INSPECTED AND CLEANED CONNECTOR ON TORQUE SENSOR. GROUND RAN AIRCRAFT. FLAPS OPS CHECKED NORMAL AT THIS TIME. LIGSDR CA130506005Wire · broken(CAN) FLAPS 0 INDICATION CAME ON IN DESCENT THRU FL250 THEN FLAP FAIL MSG POSTED. FLAPS REMAINED AT 0. FLAP 0 LANDING COMPLETED. RESOLVED ON W/O: 382391, TASKCARD: NR-00002, TROUBLESHOOTING ON W/O: 382391, TASKCARD: NR-00001, FLAPS SET TO 8DEG IAW RJ-SL-2SDR SIMA20130429005Wire Harness · faultyON FLIGHT 4477 THE CREW REPORTED THE MAIN PITCH TRIM WAS INOPERABLE DURING CLIMBOUT. BACKUP PITCH TRIM WORKED FINE. THE CREW DECLARED AN EMERGENCY AND FOLLOWED AOM-1 PROCEDURES. THE CREW REQUESTED FOR CFR TO STANDBY FOR LANDING AS A PRECAUTIONARY MEASURE.
Back to JASC 2797