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 DALA2025012100473Elec Connector · corrodedSHIP 3147 CORROSION ELECTRICAL CONNECTOR FIN: 7543VC AND 7541VC ON I/B FLAP LH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR FIN: 7543VC AND 7541VC ON I/B FLAP LH WING AS PER AIRBUS ESPM 20-44-10. (0770509)SDR SWAA2025010683424Elec Connector · faultyUPON ARRIVAL; FLAPS LOCK OUT JUST BEFORE 2 DEGREE. USED ALT FLAPS TO 15 DEGREE.<[01] R&R?D RH T/E FLAP POSITION TRANSMITTER PER AMM 27-58-01; R&R?D FLAP/SLAT ELECTRONIC UNIT PER AMM 27-51-01 & R&R?D CONNECTOR & BACKSHELL @ D229 PER WDM 27-52-11.SDR DALA2024111911079Wire · chafedSHIP 0691 -MISC/DE- DUE TO LEADING EDGE ASYMMETRY MESSAGE ON DECENT WITH FLAPS UP. CORRECTIVE ACTION: REPAIRED WIRE CHAFING ON BACKSHELL TO LEFT SLAT POSITION SENSOR.SDR DALA2024111210874Elec Connector · corrodedSHIP 3160 CORROSION ON CONNECTOR 7542VC, 7540VC AND CORROSION ON METALLIC CONDU IT OF CONNECTOR 7540VC AND 7542VC AT RH WING. CORRECTIVE ACTION: REPLACED CONNECTORS 7542VC, 7540VC AND METALLIC CONDUIT OF CONNECTORS 7540VC AND 7542VC AT RH WING AS PER AIRBUS ESSDR DALA2024110610691Wire · damagedSHIP 1803 -ATB- FLIGHT RETURNED TO ATL DUE TO MULTIPLE EEC, AFDS AND FMS FAULTS. / CORRECTIVE ACTION: EXTENDED AOS WITH MULTIPLE PARTS CHANGED. FOUND GDX3 IN P36 WITH PIN UNLOCKED (GND FOR K310 F/O P/S CURRENT SENSE) AND 2 WIRES BROKEN AT GDX7 (GND FOR K10437 SDR CALA2024102900948Circuit Breaker · trippedNO FLAP GAUGE MOVEMENT DURING EXTENSION. FLAPS WERE FELT MOVING JUST NO INDICATION. LOG PAGE MARKED AS SDR UPON INITIAL TROUBLESHOOTING FOUND CIRCUIT BREAKERS LEFT OPEN ON THE P6-2 A11/A12 FC TE FLAP POS/SKEW SNSR & IND RIGHT / LEFT. REF AMM 27-58-02-400-801 SDR CALA2024102900947Pcb · faultedREJECTED TAKE OFF DUE TO UNSCHED STAB TRIM EICAS MSG.AIRSPEED APROX 50 KTS RIGHT SAM MODULE HAS A SPM YELLOW BALL SHOWN, REPLACED RIGHT SPM CARD ASSY, GND TEST PASSED BUT YELLOW BALL DOES NOT DISAPPEAR. GND TEST OF RIGHT GPM WAS DONE PER AMM 27-48-03-424-009. SDR DALA2024101410089Elec Connector · corrodedSHIP 3144 CORROSION ELEVATOR CONNECTOR INBOARD ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REMOVED WIRING ON CONNECTOR 34CE2 C ACTUATOR INBOARD ON RH HORIZONTAL STABILIZER AND INSTALLED NEW CONNECTOR AS PER AIRBUS ESPM 20-44-11 PB 0101 AND A320 FAM AWM 27-SDR ABXA20240930180Pin · out of positionSTAB TRIM EICAS MESSAGE AND DESCRETE LIGHT AFTER ENGINE START WHILE TAXI OUT ,AC RETURNED TO GATE AND MTX GROUNDED AC. MTX FOUND PINS 2&3 SWAPPED ON PRESSURE SWITCH 527. CONNECTED PINS. REF BOEING SWM 20-61. STAB TRIM FUNCTIONS & INDICATIONS CORRECT REF B7676SDR DALA2024100109591Elec Connector · corrodedSHIP 3148 CORROSION ON ELECTRICAL CONNECTOR INTERCONNEC TING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR FIN: 7543VC AT AREA FLAP INTERCONNECTING STRUT ON LH WING AS PER A320 FAM AMM 27-51-44- 000-001-A AND AMM 27-51-44-400-001-A. (05831SDR DALA2024092309299Connector · corrodedSHIP 3148 CORROSION ON CONNECTORS 75 42VC AND 7540VC OF INTERCONNECTING STRUT INBOARD FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CONNECTORS 7542VC AND 7540VC OF INTERCONNECTING STRUT INBOARD FLAP ON RH WING AS PER A320 FAM ESPM-20-44-11. (0569139)SDR SWAA2024082730301Wire · chafedSTAB TRIM FAIL DURING DEPARTURE. REMAINED INOP IN CUT OUT. STAB TRIMMED MANUALLY STAB TRIM FAILED DURING DEPARTURE. REMAINED INOP IN CUTOUT. STAB TRIM MANUALLY.<[01] FOUND CHAFFED WIRE W628-0611-20. PERFORMED WIRE REPAIR PER SWMP 20-30-12. VERIFIED SYSTEM AND SDR CALA2024080902187Connector · dirtyLE FLAP TRANSIT LIGHT ON DURING DESCENT CLEANING PINS, H12 WAS STILL OUT OF RANGE AT 84 OHMS. G12 CAME WITHIN RANGE. H12 READ 84 OHMS THROUGHOUT CLEANING ATTEMPTS. AFTER CLEANING, THE INTRANSIT LIGHT OPERATED NORMALLY AND THERE ARE NO EXISTING FAULTS ON FSEU. SDR HNAA2024073100634Connector · looseFLAP FAILED ON TAKEOFF. FLAPS STUCK AT 9 DEGREES AND WOULD NOT MOVE. CMC MSG FLAP LH TRANSMISSION FAIL. CMC SHOWED NO NEW MESSAGES, PERFORMED OPS CHECK I.A.W AMM 27-51-00-700-801-A. OPS CHECK GOOD. INSPECTED APPLICABLE CANNON PLUGS FOR LOOSENESS FOUND P1247 SDR IPXA2024072662192Connector · damagedDURING T/S OF FLAP / SLAT ELEC STATUS MESSAGE FOUND BURNED PINS ON PLUG D464 (S28 AIR HYD PUMP PRESS SWITCH) SECURED D464 WITH CONNECTOR BACC63BP12R3S10 IAW WDM 29-11-32. OPERATION CHECK GOOD. REVERSED DMP AND REMOVED PLACARD.SDR DALA2024071607205Connector · faultedSHIP 1707 -ATO- DUE TO T/O CONFIG WARNING FOR FLAPS AT 20-25 KTS. CORRECTIVE ACTION: T/S PER B767-300 FIM 31-51 FSEU FAULTS 27-51101. REPLACED CONNECTOR D2674 AND REPLACED FLAP/SLAT MODULE. (LP 6192322)SDR DALA2024071107029Elec Connector · corrodedSHIP 3137 CORROSION SERVO CONTROL ACTUATOR ELEVATOR IB AND OB ELECTRICAL CONNECTOR FIN 34CE2-B AND 34CE4-B ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTORS 34CE2-B INBOARD ACTUATOR AND 34CE4-B OUTBOARD ACTUATOR ON RH HORIZONTAL STSDR ABXA20240624123Connector · dirtyDURING TAXI OUT I NOTICED THE RUDDER TRIM ACTUATE TO LEFT DOES NOT GOING TO RIGHT. RETURN TO GATE. MAINTENANCE GROUNDED AC AND T/S PER FIM 27-21 FT 806 & 806 AND WD 27-21-11. REMOVED, CLEANED AND RESECURED ALL CONNECTORS. OP'S CHECK RUDDER TRIM GOOD PER AMM 27SDR IPXA2024061915026Wire · damagedATB, ON DEPARTURE, WHILE STILL CONFIGURED, GOT A LEVEL 1 AIL DEFLECT INOP. AFTER FLAP RETRACT, GOT A LEVEL 2 AIL DEFLECT DISAG. WE ENGAGED A/P 2 AND THE AIRCRAFT ROLLED RIGHT AND THE A/P DISCONNECTED. WET. REPAIRED DAMAGED WIRE N316-27-18RD AND REPLACED DAMAGSDR DALA2024070106611Wire Harness · burnedWHILE WORKING MEL 5104106 PRIMARY FLIGHT CONTROL INPUT REDUNDANCY. LOOKING FOR REU ELECTRICAL CONNECTORS. FOUND BURNT WIRES 6IN FROM CONNECTOR A809P1, DIODE SHUNT 1B REU. ACCOMPLISHED TIME LIMITED REPAIR PER ER/A 618850-14 REV. ORIGINAL. PERMANENT REPAIR DUE ASDR IPXA2024061410153Warning Message · false indicationAIR TURN BACK* LE SLA ASYMMETRY AFTER TAKEOFF: AIR TURN BACK TO VIENNA CARRIED OUT SLAT #8 WEAR LIMIT CHECK PER AMM TASK 27-81-02-226-001 AND WEAR LIMIT CHECK FOR #8 SLAT TRACK PER AMM TASK 27-81-34-226-002. NO FINDINGS. FURTHER PERFOMRED INDUCTANCE / RESISTSDR SWAA2024061199730Connector · dirtyON APPROACH; WITH FLAPS 30 SELECTED; FLAPS WOULD ONLY GO TO FLAPS 15<[01] CLEANED LEFT FLAP TRANSMITTER ELECTRICAL CONNECTOR AND PERFORMED OPS TEST IAW AMM 27-58-01. OPS TEST GOOD. A/C OK FOR SERVICESDR CALA2024061001751Wire · shortedLE FLAP TRANSIT LIGHT AT 15000 MAINTENANCE MESSAGE: 27-81213 LE SLAT 7 INBOARD SENSOR SIGNAL [HISTORY]. NO CURRENT FAULT; BUT BITE CHECK INDICATES MOST ORIGINAL: FLIGHT CREW INDICATES THAT SLAT #7 WOULD NOT RETRACT SEE LOG PAGE HISTORY #8134788. FIM TASK WORKSDR 2024F00144Connector · damagedDURING INVESTIGATION OF ACTIVE CMC MAINTENANCE MESSAGE 'FCS-EBMCE 4/ROB SPLR LVDT FAULT', FAULT ISOLATION TRACED THE FAULT TO CABLE 654-3S3 WHICH WAS DISPLAYING SHORT TO GROUND AND WIRE TO WIRE SHORTS. CONNECTOR 681DB04J2 WAS DISASSEMBLED AS PART OF THE FAULT SDR 2024F00143Cable · shortedDURING INVESTIGATION OF ACTIVE CMC MAINTENANCE MESSAGE 'FCS-EBMCE 4/ROB SPLR LVDT FAULT', FAULT ISOLATION TRACED THE FAULT TO CABLE 654-3S3 WHICH WAS DISPLAYING SHORT TO GROUND AND WIRE TO WIRE SHORTS. CONNECTOR 681DB04J2 WAS DISASSEMBLED AS PART OF THE FAULT SDR CWQA20240528001Connector · damagedDURING DESCENT CREW RECEIVED A FLAPS FAILS AMBER CASS MESSAGE WITH SLATS INDICATING OUT AND FLAPS INDICATING 0 DEGREES. CHECKLIST FOLLOWED, EMERGENCY DECLARED, AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION FOUND PIN 3 CONTACT OPEN/BROKEN IN CONNECTSDR SWAA2024052889796Circuit Breaker · trippedSET FLAP HANDLE TO 5; FLAP INDICATOR DID NOT MOVE. RAN QRH. WITH ALTERNATE FLAP POSITION SWITCH TO DOWN; RECEIVED SLIGHT ASYMMETRY. LANDED NO FLAPS; RAN BRAKE COOLING.<[01] FOUND C/B P6-2 A12 POPPED. RESET C/B AND RAN FSEU BITE IAW FIM 27-51 TASK 801 FOUND CODSDR VNAA2024052111101Wire Harness · damagedRUDDER LIMITER CAUTION MSG IN FLIGHT RAN QRH LANDED AT FLAPS 20 / INTERROGATED MDC FOUND B1 CODE 233326, TROUBLESHOT IAW CRJ 700 FIM 27-61-05-810-852-A01. POSSIBLE CAUSES HAVE ALREADY BEEN RULED OUT, PERFORMED INSULATION WIRE CHECKS IAW CRJ 700 FIM 27-61-05-81SDR ABXA20240516591Wire · brokenLE FLAP SLAT DISAGREE AFTER START CHECKLIST. AC RETURNED TO BLOCK AND MAINTENANCE GROUNDED AC T/S IAW WDM 27-81-11, REPLACED RELAY K624 NO HELP. FOUND THE INBD SLAT BYPASS VALVE IN POS 1 NO POWER FOUND ON PIN 2 CONN D1515 FOUND OPEN. CK FROM CONN D5316P PIN 42SDR CALA2024042601243Control Module · defectiveSTAB TRIM LIGHT CAME ON AFTER T/O WITH FLAPS OUT. WITH FLAPS UP EICAS WENT OUT LEFT AND RIGHT EICAS COMPUTERS. PERFORMED FIM TASK 27-48FT809, FOUND COL TRIM SW FAULT BALL PERFORMED FIM TASK 27-48FT809, COMPLETED TEST 30 MCPD TEST, TEST PRESENT ON RT SAM, NO FASDR SIMA20240323003Wire Harness · failedDURING CRUISE FLIGHT AT FL290 EICAS MESSAGE SLAT FAIL ALERTED. ALONG WITH AMBER SLAT AND ZERO BOX. BOTH WERE AMBER "TRANSFERRED TO NRWC 766-ORD-01305" CMC SHOWS F/C 27831005ACE TROUBLESHOT PER EMB 170 FIM 27-83-00-810-814 REVEALED WIRES SHORTED BETWEEN CANNON SDR SIMA202403253004Wire Harness · damagedDURING CRUISE FLIGHT AT FL290 EICAS MESSAGE SLAT FAIL ALERTED. ALONG WITH AMBER SLAT AND ZERO BOX. BOTH WERE AMBER. CMC SHOWS F/C 27831005ACE TROUBLESHOT PER EMB 170 FIM 27-83-00-810-814 REVEALED WIRES SHORTED BETWEEN CONNECTOR PLUGS P0992 AND P0892. REPLACEDSDR HNAA2024031200191Switch · warning lightGUST LOCK ILLUMINATED AT PWR APPLICATION ON TAKE OFF. ELECTRO-MECHANICAL GUST LOCK SYSTEM. R & R SWITCHES IAW MM 27-71-14-05, RIGGED NEW SWITCHES IAW MM 27-71-14-05. SWITCHES S0657 AND S0659. OPS CK GOOD CLEAR MEL.SDR WWQA202402156124Connector · looseTHE CREW REPORTED THAT INBOUND TO BLK THEY DROPPED FLAPS TO 10, WHEN MOVING TO 20 THEY GOT A FLAPS ASYM MSG AND FLAPS WOULD NOT MOVE OUT OF 10, THEY MADE SEVERAL ATTEMPTS TO RESET TO NO AVAIL. THEY DIVERTED TO CLE FOR THE LONGER RUNWAY. AN EMERGENCY WAS DECLSDR 2024F00021Connector · disconnectedAIRCRAFT ARRIVED ON LFBF AIRPORT ON 20 DEC 2023 FROM UNITED STATES. THE LEADING EDGE STANDBY SHUTOFF VALVE WAS FOUND DISCONNECTED AT THE ARRIVAL OF THE AIRCRAFT (ELECTRICAL CONNECTOR DISCONNECTED). THE INVESTIGATION SHOWS THAT THE ISSUE OCCURRED PRIOR TO THESDR SWAA2024012943900Connector · damagedCB POPPED; TRAILING EDGE FLAPS WOULD NOT EXTEND<[01] R&R CONNECTOR D40024P PER SWPM 20-61-11. REPAIRED WIRES W1022-2009R-20 AND W1022-2009B-20 PER SWPM 20-10-04. OPS CHECK GOOD PER AMM 27-51-00. NO OTHER DEFECTS NOTED. NO C/B POPPED.SDR SWAA2024012946071Wire · damagedCB POPPED; TRAILING EDGE FLAPS WOULD NOT EXTEND<[01] R&R CONNECTOR D40024P PER SWPM 20-61-11. REPAIRED WIRES W1022-2009R-20 AND W1022-2009B-20 PER SWPM 20-10-04. OPS CHECK GOOD PER AMM 27-51-00. NO OTHER DEFECTS NOTED. NO C/B POPPED.SDR DALA2023122810684Unknown · unknownSHIP 3120 CORROSION ON ELECTRICAL CONNECTOR 7540VC AT INTERCONNECTING STRUT AREA IB FLAP RH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR 7540VC AT INTERCONNECTING STRUT AREA IB FLAP RH WING AS PER AIRBUS ESPM 20-44-11 AND AS PER A320 FAM AWM 27-51-11SDR SIMA20231223001Wire Harness · failedSLAT FAIL EICAS ON TAKE OFF. SLAT STUCK IN POSITION (3) DECLARED EMERGENCY. EQP SWAP FLT.-C/A-RAR SLAT #4 HARNESS IAW E170/175 AMM 27-83-07. OPS CHECK GOOD.SDR AALA202311299457Wire · damagedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON CLIMB THE STABILIZER DID NOT TRIM WITH BOTH CAPTAIN AND FIRST OFFICER TRIM SWITCHES. AIRCRAFT LANDED SAFELY AT VQQ WITHOUT FURTHER INCIDENT. FOUND DAMAGED WIRE W4222-1006-18 IN STAB CONTROL COMPARTMENSDR CALA2023101603065Circuit Breaker · trippedSTAB OUT OF TRIMLIGHT ELECTRIC TRIM INOP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003088021 AND PRTR FOUND STAB TRIM ACTUATOR C/B OUT (P6-2,D10) PERFORMED STAB TRIM MOTOR OPS CHK SDR DALA2023100308102Unknown · unknownSHIP 3126 - ATO - AT 60 KTS DUE TO A FLAP FAULT. FOUND WIRE SHORTED IN THE LT WING REAR SPAR RACEWAY WIRING. CORRECTIVE ACTION: FAILURE MESSAGE, FLP LH PROX SNSR 1 37CV OR LGCIU 1 FAULT. FOUND CHAFED WIRES UNDER RECEPTACLE 7541VC BACK SHELL. REMOVED DAMAGED ENSDR DALA2023092207814Unknown · unknownSHIP 3129 CORROSION INBOARD FLAP CONNECTORS 7541VC AND 7543VC ON LH WING. CORRECTIVE ACTION: REPLACED INBOARD FLAP CONNECTORS 7541VC AND 7543VC ON LH WING AS PER AIRBUS ESPM 20-44-11. (2980689)SDR DALA2023092207813Unknown · unknownSHIP 3129 CORROSION INBOARD FLAP CONNECTORS 7542VC AND 7540VC ON RH WING. CORRECTIVE ACTION: REPLACED INBOARD FLAP CONNECTORS 7542VC AND 7540VC ON RH WING AS PER AIRBUS ESPM 20-44-11. (2980665)SDR SWAA2023080284905Connector · faultyFLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/17SDR AALA202307289930Transformer · shortedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED. AIRCRAFT RETURN TO DFW DUE TO TRAILING FLAPS DISAGREE. AIRCRAFT LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT FOR AALA202307269930: REMOVED AND REPLACED T52 TRANSFORMER, RESET CIRCUIT BREAKER.** (CLOSED)SDR DALA2023060504482Unknown · unknownSHIP 3116 CORROSION IB FLAP CONNECTORS 7541VC AND 7543VC ON LH WING. CORRECTIVE ACTION: COMPLIED WITH AMDS 2751-9202-DE. (2797256)SDR DALA2023060504481Unknown · unknownSHIP 3116 CORROSION IB FLAP CONNECTORS 7542VC AND 7540VC ON RH WING. CORRECTIVE ACTION: REPLACED IB FLAP CONNECTORS 7542VC AND 7540VC ON RH WING. (2797252)SDR SIMA202301265001Wire Harness · damagedDECLARED AN EMERGENCY INTO ORD FOR A SLAT ISSUE. FLT LANDED SAFELY -C/A-RAR RH WING #4 SLAT HARNESS IAW ERJ 175 AMM 27-83-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.SDR SWAA2023010386854Wire · chafedSTAB TRIM CIRCUIT BREAKER POPPED IN FLIGHT. STAB TRIM C/B P6-2 B10 POPS WHEN TRIMMING NOSE DOWN. WITH THE S272 STAB TRIM SWITCH IN CUTOUT THE C/B CONTINUES TO POP TRIMMING NOSE DOWN THIS TAKES OUT THE S245 LIMIT SWITCHES AND MOTOR FROM THE CIRCUIT. ALSO WIT
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