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 2007UALA02156Wire · shortedL/E SLAT ASYMMETRY LIGHT AND EICAS MESSAGE ON PRIOR TO DEPARTURE. [07-20-07] FOUND SHORT IN WIRE SPLICE. REPLACED SPLICE SM7, WIRE W480-007-18, AND SHIELD ASSEMBLY. REINSTALLED D4378 CONNECT OR ASSY, AND SECURED WIRE BUNDLE. SYSTEM CHECKED OK FOR SERVICSDR CA070601004Wire · burned(CAN) FLAP FAIL MESSAGE COME ON DURING CRUISE AT ALT FL330 WITH NO FLAP SELECTION MADE. AIRCRAFT RETURN TO ORIGINATING STATION, MAINTENANCE REPLACED THE BPSU AND FECU BUT NO FIX. FURTHER INVESTIGATION REVEALED SOME BURNED WIRES AT LT BPSU CONNECTOR. TEMPORASDR FDKA200705216Connector · dirtyFDM 6178 JFK (1415 PHX LCL) RETURNED TO GATE DUE TO RUDDER PRESS LIGHT FAILED TO ILLUMINATE. MX CLEANED CONNECTOR.SDR RAIA00705039Connector · dirtyFLT NR 8000 - IAD - SPOILER FAIL & INTERMITTENT UNCOMMANDED SPOILER DEPLOYMENT DURING TAXI. MAINTENANCE CLEANED CONNECTOR ON SPOILERS AND WHEEL SPEED TRANSDUCER, ALL CHECK NORMAL.SDR SWAA072410Wire · brokenAIR TURNBACK, ON FLAP RETRACTION RIGHT WING NR 5 L/E SLAT WOULD NOT RETRACT. CYCLED FLAPS PER QRH, NO HELP. FOUND BROKEN WIRE AT NR 5 L/E SLAT ACTUATOR, REPAIRED WIRE PER MM.SDR GAI2007F00001Connector · dirty(REF NR: GAIA 07-05 OP) DURING CLIMB THE FLIGHT CREW RETRACTED THE FLAPS NORMALLY HOWEVER, AT ZERO DEGREES FLAPS THE AMBER LIGHT REMAINED ILLUMINATED ON THE FRONT PANEL. FE PANEL INDICATED NR 4 SLAT EXTENDED. FOLLOWED OPS PROCEDURE AND CYCLED FLAPS WITH SAMESDR DXTA200702170Connector · corrodedDURING TAKEOFF ROLL, ABORTED TAKEOFF (BELOW 70KTS) DUE TO ILLUMINATION OF NO TAKEOFF ANNUNCIATOR AND NO TAKEOFF HORN. TROUBLESHOT SYSTEMS. FOUND EXCESSIVE MOISTURE AND CORROSION IN THE LT SPEEDBRAKE DISCONNECT PLUG PL001. REPLACED PINS, SOCKETS AND PLUG BACSDR CA070404003Wire Harness · damaged(CAN) DURING AN INSPECTION, THE RUDDER POSITION TRANSMITTER HARNESS WAS FOUND TO BE DAMAGED. THE CAUSE OF THE DAMAGE WAS FOUND TO BE IMPROPER ROUTING BY COMPARING WITH ANOTHER A/C S/N 7163. THE ACTUAL ROUTING DRAWING WHERE REQUESTED FROM BOMBARDIER AND THE HARSDR COMA0760298Connector · failedFLIGHT 5577 - FLAPS FAILED CAUTION MESSAGE, FAILED AT 45 DEGREES. REMOVED AND REPLACED RIGHT BPSU CONNECTOR.SDR YENA2007012Wire Harness · damagedAT 1500 FT FLAPS SELECTED 5. SLATS TRAVELLED TO FULL ON EICAS WHILE FLAPS INDICATED SOMEWHERE BETWEEN 1/2 AND FULL. EXECUTED QRH CHECKLIST. AFTER CHECKLIST COMPLETED, SLATS INDICATED FULL WHILE FLAPS WERE AT 5. NORMAL LANDING. FOUND SLAT NR 2 HARNESS W611SDR FDKA200702067Wire · damagedFDM 6181 ALB-JFK (1356 PHX LCL). CONTROL YOKE DIFFICULT TO MOVE IN AIR TO RIGHT AND AILERON TRIM INOP. MX SPLICED WIRE ON AILERON TRIM POT.SDR CA070201004Wire · broken(CAN) APPROX 1 MILE OUTSIDE THE OUTER MARKER AT 3000 AGL, THE AMBER FLAP CAUTION LIGHT ILLUMINATED. THE CREW SELECTED FLAP 20 AND THE FLAPS WENT TO 20. WHEN THE LIGHT ILLUMINATED THE CREW WENT THROUGH THEIR EMERGENCY CHECKLIST AND CARRIED OUT AN UNEVENTFUL LASDR CHQA200700002Connector · dirtyFLIGHT 6420 - TRI-CVG - ON APPROACH, WHEN PLACING FLAPS FROM "9" TO "22" RECEIVED "FLAP FAIL" ON EICAS WITH "9" INDICATED. BROKE OFF APPROACH AND RAN QRH. DECLARED EMERGENCY AND LANDED SUCCESSFULLY. MAINTENANCE CLEANED AND RESET FECU CONNECTOR AND OPS CHECKSDR HALA0700031Wire · damagedFLT CREW REPORTS, STALL WARNING FAULT LEVEL ONE ALERT ANNUNCIATED, NO TAKEOFF. FOUND WIRES TO FO STICK SHAKER N/G. REPAIRED WIRES PER SWPM 20-10-03. RTS FOR STALL WARNING SYSTEM CHECK OK.SDR FDKA200701014Connector · dirtyFDM 5969 AVL-ATL (0620 PHX LCL) AILERON SYSTEM 2 INOP. MX CLEANED CONNECTOR & RESECURED AT HYD MANIFOLD.SDR YENA2007003Wire Harness · intermittentSLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (LT HARNESS INTERMITTENT). REMOVED AND REPLACED LT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A OPS CHECK OK. NO FAULTS FSDR YENA2007002Wire Harness · intermittentSLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (RT HARNESS INTERMITTENT). REMOVED AND REPLACED RT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-810-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A, OPS CHECK OK, NO FAULSDR HALA0700024Cable · damagedON APPROACH WHEN FLAPS WERE SEL TO 13 GOT A SLIGHT ROLL TO LEFT. AFTER LDG WHEN FLAPS WERE SEL TO 18 GOT FLAP DISAG ALEART AND CONFIG PG SHOWED L FLAP AT 13 AND R FLAP AT 19. FOUND FLAP BUS CABLE 3XA BROKEN AND BUSS 33B CRUSHED. REMOVED AND REPLACED FLAP BUSDR ASMF200701002Connector · intermittentDURING TRANSIT CHECK, THE ALT LONG TRIM STABILIZER WAS OUT OF SERVICE. CIRCUIT BREAKER WAS RESEATED BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING WIRING CHECK WAS DETECTED THE CONNECTOR P10-41 PIN A WITH INTERMITTENT CONTACT. PIN A WAS REPLSDR SIMA200635501Ground Stud · shortedFLAP FAIL MESSAGE ON EICAS AT 230 KNOTS. FOUND INTERMITTENT RESISTANCE ON GS0352 DC GROUNDING POINT FOR LEFT TRANSMISSION BRAKE. CLEANED BONDING JUMPERS AT GROUND STUD. SWAPPED LEFT AND RIGHT FLAP MOTOR UNITS. OPERATIONAL CHECK GOOD IAW EMB AMM 27-50-00. SDR FDKA200612358Wire · damagedFDM 6131 JFK-PWM (1312 PHX LCL). ONBD ROLL SPOILER NOT INDICATING DEPLOYED. MX REPAIRED SPOILER SYSTEM WIRING. OPS CHECK GOOD.SDR SWIA200617423Connector · dirtyAFTER TAKEOFF RETRACTING FLAPS CONTROL FAULT ON OUTBOARD PAIR, RETURNED TO SFO. CLEANED TRACKS AND CONNECTORS FOR OUTBOARD FLAPS. OPERATIONAL CHECKS GOOD.SDR MASA200602628Connector · dirtyASH 7114 RDU. STAB CH 2 WILL NOT ENGAGE. MX CLEANED HORIZONTAL STABILIZER MCU ELECTRICAL CONNECTORS. NO FURTHER DEFECTS NOTED.SDR MASA200602608Connector · dirtyASH 7251 CHS. RIGHT FLAP POSITION INDICATION FLUX IN CRUISE FLIGHT. MX CLEANED AND RESECURED CONNECTOR TO FLAP POS TRANSMITTER, OPS CHECK NORMAL.SDR MASA200602599Connector · disconnectedASH 2640 CLT. SLAT FAIL EICAS CAUTION. MX FOUND CONNECTOR OFF LT BPSU AND REINSTALLED.SDR C1HA200682019Wire · broken"UPON RETRACTION OF FLAPS AFTER TAKEOFF, AMBER NR 7 LEADING EDGE LIGHT REMAINED ILLUMINATED, RUN COM PROCEDURE 2.27.12, DUMPED FUEL RETURN TO DEW. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER MM 27-81-32, OPS CHECK LEAK CHECK OK WHILE RARE ACTUATOR MX FOUND FOSDR NSVA200600204Circuit Breaker · unknownRELEASED GUST LOCK AND RUDDER STAYED LOCKED. RESET C/B G/4, PERFORMED OPS GUST LOCK CK IAW AMM 27-70--00.SDR 2006FA0001147Wire · shortedAIRCRAFT ABORTED TAKEOFF DUE TO BOTH STALL WARNINGS ILLUMINATED ON DEPARTURE ROLL. C/B LEFT AND RIGHT STALL C/B POPPED. AUTOPILOT, FLIGHT DIRECTOR AND PRIMARY YAW DAMPER INOPERATIVE. (K)SDR MASA200602503Connector · looseASH 7010 CLT. CREW REPORTED STAB CHANNEL NR 1 WILL NOT ENGAGE. MX RE-SECURED A LOOSE YOKE ELECTRICAL CONNECTOR.SDR YENA200683Wire Harness · shortedSLAT FAILED AT 0 DURING CLIMB OUT AT 5500 FT WITH SLAT/FLAPS AT 0/0. ACCOMPLISHED ELECTRICAL CK OF THE OB SLAT SKEW SENSOR AND WIRE HARNESS. IAW FIM 27-83-00-810-814-A. REPLACED FAULTED RT WIRE HARNESS (W612) IAW M/M 27-83-07 FOR SLATS 3/4 SKEW SENSOR. OPERATISDR DXTA200601693Electrical Box · shorted(FLAPS FAIL) AMBER CAS MESSAGE POSTED ATTEMPTING FLAPS 7: FLAPS WERE RESET AND FAILED AGAIN AT FLAPS 7. FLAPS WERE RESET AND FAILED AT FLAPS 15: FLAPS WERE RESET AND DID NOT FAIL AFTER FLAPS 35 WERE INDICATED. CHECKED BITE ON FLAP CONTROLLER, BITE 5 TRIPPEDSDR MASA200602482Connector · dirtyASH 7253 GSP. FLAPS 1/2 SPEED STATUS MESSAGE. MX CLEANED CONNECTOR ON BPSU.SDR ASMF200610010Wire · brokenAIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT REMAINED OFF. PROXIMITY SWITCH WAS REPLACED AND TESTED, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND WIRING WAS CHECKED, DETECTING A SENSOR LINE BROKEN. WIRING SENSOR WAS REPAIRED SDR AWXA200601767Wire · brokenFLIGHT 180; - DURING CLIMB OUT, THE CREW REPORTED THE LOSS OF AILERONS. ON MEL THE OPPOSITE SIDE FAULTED WHICH RESULTED IN THE REPORT OF THE (LOSS OF AILERONS). THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITH NO REPORT OF DIFFICULTIES CONTROLLINSDR FDKA200610288Connector · dirtyFDM 6058 NAS. FLAP FAIL MESSAGE IN FLIGHT WITH FLAPS AT 9 DEGREES. MX CLEANED C/P TO RIGHT FLAP MOTOR.SDR NOCA14406Connector · damagedRUDDER RATION LIGHT ILLUMINATED AT 1000 FEET AFTER TAKEOFF. PERFORMED FIM 27-21-00. NO FAULTS NOTED, CHECKED WIRING IAW WDM 29-11-12. FOUND PIN NR 2 AT PLUG D56 PUSHED BACK, SECURED PIN IAW 20-11-00, OPS NORMAL.SDR A6WA200640359Connector · looseFLAP FAIL MESSAGE DURING FLAP RETRACTION FROM 8 DEGREES TO 0 DEGREES, FLAP INDICATOR INDICATES 20 DEGREES. CHECKED FECU WHICH LED TO NR 1 OR LEFT BPSU. FOUND CONNECTOR TO BPSU LOOSE WITH MOISTURE INSIDE. CLEANED CONTRACTS AND RECONNECTED. REF 27-51-00, OPSSDR NSVA200600164Wire · brokenFLAPS WILL NOT RETRACT LESS THAN 17 DEGREES. UPON INSPECTION FOUND LT FLAP SAFETY SWITCH TO HAVE ONE BROKEN WIRE AND WORN ROLLER. REPAIRED WIRE IAW BAMM 20-13-00 AND REPLACED WORN CAM BY REMOVING BOLT AND NUT AND REINSTALLING. OPS CHECK GOOD, P/N OFF/ON 101SDR CBR2006F00015Connector · dirtyABORTED TAKEOFF, PFCS SPOILER DID NOT MOVE IN THE UPWARD POSITIONS ON TAKEOFF ROLL. CLEANED PFCS INDICATOR CONNECTOR IAW MM AND OPS CHECK GOOD IAW MM. (K)SDR CA060925003Connector · broken(CAN) WHEN MANUAL RUDDER TRIM WAS APPLIED THE RUDDER FAILED TO RESPOND. SUBSEQUENT INSPECTION FOUND THAT THE ARM THAT CONNECTS THE TRIM ACTUATOR TO THE RUDDER CONTROL ASSEMBLY HAD BROKEN OFF THE ASSEMBLY AT THE EDGE OF THE WELD. THE COMPLETE RUDDER TRIM ARM ASSDR DL757060684Connector · faultyON T/O WHEN FLAPS RET FROM 5 TO 1, TE FLAPS ASSYM LIGHT AND EICAS MSG DISPLAY. RTN TO LAND. FOUND CONNECTOR D1802 ON RT FLAP POS XMITTER BAD. REPLACED PLUG AND BIN. MEGGED OUT WIRING FROM XMITTER TO FSEU. ALL CKS OK. NO HELP. REPLACED RT TE FLAP POS X-MSDR FDKA200608221Connector · dirtyFDM 6083 TRI. CREW REPORTED A SPOILER FAIL ON GROUND. MAINTENANCE SECURED AND CLEANED THE CONNECTOR.SDR A6WA200640313Connector · looseUNCOMMANDED ROLL FLAPS 45 AIRSPEED MANEUVERING OR GREATER, R-TURN 10-15 DEGREES BANK ANGLE AIRCRAFT CONTINUES TO ROLL INTO TURN. INSPECTED RIGHT SPOILER OUTBOARD PCU AND FOUND CANNON PLUG LOOSE. RESECURED AND PERFORMED OPS CHECK OF RT SPOILERON IAW AMM 27-60SDR FDKA200608185Connector · unknownFDM 6085 MCO - THE CREW REPORTED THE RUDDER SYSTEM 2 INOPERATIVE. MAINTENANCE CLEANED PRESSURE SWITCH CONNECTOR.SDR MASA200601990Wire · damagedASH 6309 PHX - SLAT FAULT STATUS MESSAGE. MX PLACED SYSTEM ON DEFERRAL. MX REPAIRED WIRE.SDR MASA200601861Connector · corrodedASH 6286 PHX - FLAP DRIVE CAUTION MESSAGE. MX FOUND THE FLAP DRIVE CONNECTOR CORRODED. MX CLEANED CORROSION AND SECURED CANNON PLUG.SDR 1350502N781EACircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER.SDR AMW78361Wire · chafedCREW EXPERIENCED UNCOMMANDED ELECTRIC TRIM MOVEMENT INBOUND TO CNY. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND CHAFED WIRES AT CONNECTOR FOR F/O'S YOKE. REMOVED AND REPLACED THE CONNECTOR AND PINS. ALL OPS CHECKS NORSDR 200606291Connector · disconnectedFLIGHT 7590 ORD TO GRR SLAT FAIL EICAS MESSAGE ON TAXI INTO GRR. OCM REPORTED, NO DEFECTS FOUND. A/C BEING PREPARED FOR MAINTENANCE FERRY TO IND FOR FURTHER TROUBLESHOOTING. IND MAINTENANCE FOUND THE RT CONNECTION ON THE PDU DISCONNECTED. FURTHER INSPECTIOSDR 2006FA0000648Connector · damagedINVESTIGATED REPORT OF FLAP ASYMMETRY ANNUNCIATOR LIGHT FLICKERING IN-FLIGHT. FOUND WIRE C458A22 ROUTED SO THAT EXCESSIVE WIRE TENSION AT P156 PLUG WAS CAUSING INTERMITTENT CONTACT WITH A156 PC BOARD J1 CONNECTOR. REROUTED WIRING AS REQUIRED FOR REVEALING WI
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