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 DXTA20082936Connector · unsecureON CLIMBOUT, PASSING 4000 FT, RECEIVED PITCH FEEL FAIL AMBER CAS MSG. FOUND PIN *14 & 1 CONNECTOR PQ016 UNLOCKED AND RECESSED. LOCKED PIN CONNECTOR SYSTEM OPS CHECKS GOOD IN REF FT CES-750-071.SDR 2008UALA01195Connector · failedFLIGHT CONTROL SYS STATUS MSG ON PUSHBACK, WILL NOT CLEAR. AFTER EXTENSIVE TROUBLE SHOOTING FOUND BAD CONNECTOR. REPLACED ACE L2 BENCH PLUG DM27122AC. PERFORMED ACE LRU TEST,ACE ACTUATOR MONITOR TEST PER MM 27-02-02-501,AND ACE ACTUATOR CONFIDENCE TEST.ALL TSDR DXTA20082878Wire · broken(H) STAB FAIL) LIGHT ILLUMINATED IN FLIGHT. INSPECTED AND FOUND BROKEN WIRE AT P540 CONNECTOR PLUG. REPAIRED WIRE IAW MM 20-20-04. PERFORMED PITOT TEST, SYSTEM PASSED. PERFORMED GROUND CHECK, OPS CHECK GOOD. DONE IAW AMM 30-12-00.SDR 200802131Wire Harness · faultyFLIGHT 7722 ORD TO IND DURING APPROACH CREW SELECTED 5 FLAPS AND RECEIVED A "SLAT FAIL" CAUTION AND ASSOC AMBER BOX ON SLAT/FLAP INDICATION. CREW DECLARED AN EMERGENCY AND THEN LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD SKEW SENSORSDR DXTA200802815Connector · looseDURING T/O POWER APPLICATION HYD PRESS LIGHT CAME ON AT APPX 80 PERCENT N1. ABORTED T/O. GAINED ACCESS TO SPEED BRAKE SWITCHES. FOUND CONNECTOR FOR SWITCH WIRING IN LT SPEED BRAKE COVE NOT FULLY SEATED. C/W SPEEDBRAKE SWITCH RIG. SECURED CONNECTORS. C/W SSDR C2XA08IA047Wire · brokenIAH - FLIGHT 2392, THE CREW REPORTED A SPOILER FAIL WITH A SPOILER OPEN INDICATION WITH THE SPOILERS CLOSED. THE CREW PERFORMED AN EMERGENCY DESCENT, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE LEFSDR 200801232Wire Harness · defectiveFLIGHT 7501 DEN TO ABQ - ON APPROACH CREW SELECTED FLAPS POSITION 1. DURING TRANSITION CREW RECEIVED SLAT FAIL EICAS MESSAGE. CREW RAN QRH CHECKLIST, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT SLAT 3 AND 4 SKEW SENSOR HARSDR CA080110003Connector · failed(CAN) FLAP FAIL MESSAGE ON POWER UP. CODES READ AND BPSU NR 2 WIRING FAILED. MEL 27-51-02-1 APPLIED. WILL PROVIDE UPDATE WHEN MORE INFO BECOMES AVAILABLE (TC NR 20080110003)SDR FDKA200801015Connector · dirtyFDM 6188 JFK (1223 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT. MX CLEANED CONNECTORS AND OPS CHECKED GOOD.SDR FDKA200712403Connector · dirtyFDM 6208 ATL - FLAP LOW SPEED ADVISORY MESSAGE AFTER LANDING DURING FLAP RETRACTION. MX CLEANED AND RESECURED FECU CONNECTOR, SYS OPS CHECKED GOOD.SDR SIMA200734407Ground Stud · shortedON TAKEOFF ROLL AT 10 KTS IN THRUST SET POSITION GOT NO TAKEOFF CONFIGURING EICAS SPOILER SHOWED OPEN. GOT NO SPOILER AURAL WARNING. ABORTED TAKEOFF AND SPOILER CLOSED AT IDLE THRUST. FOUND GROUND BLOCKS GS0163 DC AND GS 0186 DC TO HAVE HIGH OHMS TO GROUND.SDR CA071206007Wire Harness · worn(CAN) AFTER ROTATION, HEAVY LT AILERON INPUT NEEDED IN FLIGHT. AILERON TRIM WAS CENTERED BUT HAD NO EFFECT. FLIGHT RETURNED TO DEPARTURE AIRPORT SAFELY WITH NO NEED TO DECLARE AN EMERGENCY. MAINT TROUBLESHOOTING, FOUND WIRE HARNESS ON AILERON TRIM ACTUATOR WORSDR SIMA200733708Ground Stud · looseCREW ABORTED T/O AT 30 KNTS FOR UNCOMMANDED SPOILER DEPLOYMENT. TROUBLESHOT PER EMB 145FIM27-63-00. FOUND LOOSE GROUND STUD. TIGHTENED. GROUND STUD IAW EMB AMM 20-10-01. OPS CK GOOD OF SPOILER SYSTEM IAW AMM27-62-00. AIRCRAFT RETURNED TO SERVICE.SDR FDKA200711347Connector · dirtyFDM 6150 TYS. RUDDER SYSTEM NR 1 WILL NOT SHUT OFF. MX CLEANED CONNECTORS ON CONTROL PANEL SWITCH AND NR 1 PRESSURE SWITCH. OPS CK GOOD.SDR YENA2007111Wire Harness · defectiveSLAT FAIL EICAS MESSAGE AFTER SELECTING FLAPS 1. SLAT POSITION SHOWED LOCKED SOMEWHERE BETWEEN THE 0 AND 1 POSITION WITH - DISPLAYED IN THE SLAT POSITION BOX. FURTHER MOVEMENT OF FLAP HANDLE HAD NO EFFECT ON SLAT POSITION. MESSAGE OCCURED AROUND 210 KTS DURSDR 2008FA0000090Wire · chafedPITCH TRIM INOPERATIVE REMOVED RT FWD GALLEY AND RT FWD PARTITION. FOUND WIRE BUNDLE CHAFED BEHIND PARTITION. REPAIRED (3) WIRES THAT WERE CHAFED THROUGH TO THE CONDUCTORS. PROVIDED CLEARANCE BETWEEN WIRE BUNDLE AND PARTITION. INSTALLED ANTI-CHAFE MATERIALSDR 2007FA0001015Connector · crackedBACK SHELL IS BROKEN/CRACKED AND SEPARATED FROM CONNECTOR PLUG ASSY. POSSIBLE CAUSE IS WIRE BUNDLE TO CONNECTOR PLUG STRESSES AND PULLING ON BACK SHELL. BACK SHELL IS MADE ON PLASTIC NOT METAL. IF BACK SHELL WAS MADE OF METAL IT WOULD HOLD UP AS A STRAIN RELSDR 2007UALA04592Wire Harness · damagedFLAP SLAT SKEW MSG IN VIEW. FOUND WIRE HARNESS DAMAGED ON RT OUTBOARD FLAP-SLAT SKEW. REPLACED SKEW SENSOR NR 7 WIRING HARNESS. OP CHECKED PASSED. AC OK FOR SERVICESDR COEA0709902Connector · contaminatedFLT 8788 -WHILE PERFORMING TAXI CHECKS AFTER A/C DEICING, CREW OBSERVED THAT THE FLAPS WOULD NOT EXTEND. THE CREW RETURNED TO RAMP. CLEANED CONNECTORS, DEICE FLUID CONTAMINATION. (M)SDR 2007UALA04382Connector · looseFLAP - SLAT ELEC EICAS MSG DISPLAYED. REPLACED FLAP POSITION TRANSMITTER. SECURED CONNECTOR ON FLAP POSITION TRANSMITTER 1L ON LEFT WING. OPERATED FLAPS, NO MESSAGES, BITE TEST OF FSEU SHOWED NO FAULTS.
SDR FDKA200710561Connector · unsecureFDM 9960 BNA (1445 PHX LCL) - FLIGHT SPOILERS FAILED IN FLIGHT. MX RESECURED CONNECTOR ON CONTROLLER, OPS CK GOOD.SDR 2007F00066Wire Harness · shortedON THE IB FLIGHT, THE NR 1 PITCH TRIM CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS TAKEN TO MFG AND THE TECHNICIANS WERE UNABLE TO DUPLICATE THE PROBLEM. AT MAINTENANCE REQUEST,THE TAIL WIRE HARNESS (FROM THE PRESSURE BULKHEAD TO THE STABILIZER TRIM ACTUATOR) WAS SDR 200700026Wire · chafedTRAILING EDGE FLAPS ASYMMETRY LOCKOUT BETWEEN ZERO AND ONE DEGREE. THERE IS A SPLIT IN T/E FLAP INDICATION, LT T/E FLAPS INDICATE ONE DEGREE AND RT T/E FLAPS INDICATE ZERO. FLIGHT CREW EXPERIENCED AN UNEVENTFUL LANDING AND NO UNCOMMANDED ROLL. MAINTENANCE DSDR FDKA200710545Connector · looseFDM 9963 MCO - SPOILER FAIL EICAS MESSAGE. MX RESECURED SPOILER PROX SWITCH CONNECTOR AND APPLIED HEAT SHRINK.SDR 2007FA0000923Connector · misinstalledPRIMARY STAB TRIM FAILED CLIMBING THROUGH FL280 AT 300 KTS. NO CAS MESSAGE WAS PRESENT. CLACKER WAS STUCK ON. STAB WAS NOT MOVING WHEN CLACKER WAS GOING OFF. AUTO PILOT DISENGAGED ON ITS OWN DUE TO HEAVY NOSE CONFIG. AFTER TROUBLESHOOTING SHOULD THE ECM TOSDR 2007UALA03936Connector · faultyAILERON LOCKOUT MSG. *S/D* PERFORMED EXTENSIVE TROUBLESHOOTING. BOTH AIL-LOCKOUT ACTUATOR CONNECTORS WERE REPLACED. ALSO REPLACED INOPERATIVE RIGHT AIL-LOCKOUT ACTUATOR. AIL-LOCKOUT SYS OPERATED NORMALLY PER MM 27-11-44 (3H).SDR DXTA200702497Connector · corrodedNO TAKEOFF ANNUNCIATOR AND AURAL WARNING TRIGGERED UPON APPLICATION OF TAKEOFF POWER. ABORTED TAKEOFF. REPLACED SPEED BRAKE CONNECTOR IAW MM 20-10-04. SPEED BRAKES OP'S OK IAW MM 27-61-00.SDR COMA0760580Wire · looseFLIGHT 5671- AT 40 KTS RECEIVED STAB TRIM CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. RESOLDERED LOOSE WIRE ON CAPTAIN'S PITCH DISCONNECT SWITCH. NO FURTHER DEFECTS.SDR FDKA200708468Connector · dirtyFDM 6114 RDU - RUDDER HARDOVER PROTECTION FAIL MESSAGE. MX CLEANED FADEC CONNECTOR, RESET AND OPS CHECKED.SDR 2009FA0000443Wire · looseROLL TRIM ACTUATOR HAS MALFUNCTIONED ON 3 OCCASSIONS SINCE BUYING ACFT NEW IN 02. IN EACH CASE THE WIRES LEADING TO THE ELECTRIC MOTOR HAD COME LOOSE CAUSING THE TRIM ACTUATOR TO HOLD FULL LT AILERON. WITHOUT OVERPOWERING THE UNIT A FATAL CRASH WOULD HAVE RESUSDR YENA2007079Wire Harness · damagedSLAT FAIL MESSAGE WHEN GOING FROM POSITION 0 TO 1. QRH COMPLIED WITH. SLAT FAIL REMAINED. PERFORMED TSM 27-81-00-810-805A. FOUND SKEW SENSOR HARNESS LT WING OUTBOARD SLAT 3/4 DEFECTIVE HIGH MILLIVOLTS & CRIMPED AND CHAFING. REMOVED AND REPLACED LT OUTBOARSDR TRBA2007070Wire · openFLAPS DID NOT MOVE FROM "0" TO "15" DEGREES ON APPROACH. PERFORMED "0" FLAPS LANDING AT SJU. AFTER TROUBLESHOOTING FOUND AND REPAIRED OPEN WIRE NR 2571-2588 AS PER STANDARD PRACTICES JIC NR 20-25-22.SDR AALA20071550Circuit Card · inoperativeLAX INFLIGHT T003/15AUG - ON APPROACH WHEN SELECTING FLAPS 20 DEGREES THE MASTER CAUTION LIGHT AND LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. LANDED LAX WITHOUT INCIDENT. BITE CHECK OF PROXIMITY SENSOR ELECTRONIC UNIT FOUND FAULT OF CARDS 001 ANDSDR AALA20071480Relay · inoperativeYYZ INFLIGHT T1084/10AUG - SPEED TRIM FAIL LIGHT ILLUMINATED DURING CLIMB IN CONJUNCTION WITH THE STABILIZER TRIM INOPERATIVE. LANDED YYZ WITHOUT INCIDENT. REPLACED STABILIZER TRIM CUTOUT RELAY R64 AND ACCOMPLISHED STABILIZER TRIM CUTOUT TEST. SYSTEM GROUNDSDR IXXA070037OWire · arcedDURING APPROACH INTO KBWI, THE FLIGHT ATTENDANT NOTICED A FLASH AT THE CIRCUIT PANEL ABOVE THE RIGHT AFT SERVICE DOOR. THE CREW CONTINUED WITH THE APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND POWER WIRES CONTACTING LATCH OTHER BEHIND SDR 2007UALA02883Ground Wire · disconnectedNR 3 LE FLAP FULL EXTEND AND FWD PNL INTRANSIT LIGHTS ON WITH FLAPS RETRACTED. ALL WIRE BUNDLE CLAMPS FROM S173 SENSOR TO SPLICES AT PRESSURE FEED THRU LOCATED 3 FEET OB OF WING ROOT ARE LOOSE. GROUND WIRES AT GD148AC ARE ALSO DISCONNECTED. SECURED WIRING ANSDR C8GA20070007Connector · dirtyFLT 738 FROM SLW TO GDL, DURING CLIMB-OUT FROM SLW, THE INBOARD FLAPS WOULD NOT RETRACT BEYOND 15 DEGREES. APPROPRIATE CHECKLIST WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SLW WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT PERFORMED THOROUGH INSPECTION CHECSDR CA070724004Wire · damaged(CAN) IN CRUISE GEAR/FLAPS/BTMS INDICATIONS APPEARED WITH FLAP INDICATION SHOWING BOTH SIDES. FLAPLESS LANDING WAS SAFELY PERFORMED. MAINTENANCE FOUND WIRE CF61A22WHT AT CONNECTOR P2CF OF RT FLAP POSITION TRANSDUCER WITH DAMAGED INSULATION AND TOUCHING THE SHISDR HALA0700295Cable · brokenDURING FLAP RETRACTION AFTER LANDING FLAP/SLAT DISAGREE ALERT ILLUMINATED. FOUND FLAP BUSS CABLE RUN 33B AND 34A BROKEN. REVD CABLES, FABRICATED CABLES 33B AND 34A PER AMM 91-10-05 AND AMM 20-00-03. INSTALLED AND ADJUSTED PER AMM 27-50-00. OPS CHK OK. (CHSDR DLM88070934Buss Cable · brokenMOVING RT AILERON HAD NO EFFECT ON LT AILERON. FOUND AILERON BUSS CABLE BROKEN IN RT W/W. FOUND AILERON BOSS CABLE 36B BROKEN. REPLACED SAME ADJ/TEST AMM 460188. RII DEPT 625 B/O INSTALLATION AND ADJUSTMENT OF CABLE PER M/M 1506.SDR UPS07650332Connector · corrodedINSPECTION TYPE:ETOP BLOCK TURN BACK DUE TO EICAS MSG FLAP/SLAT ELEC DISPLAYED. BITE CHECK FSEU-FAULT-1 LT O/B TRANSMITTER. FOUND CORROSION IN CONNECTOR. CLEANED. OPS CHECK PER MM 27-58-00-5. CHECKED OK.SDR 2007UALA02463Wire Harness · failedRUDDER TRAVEL LIM MESSAGE RECEIVED. FOUND A BROKEN WIRE IN STA2456-FR53. REPAIRED WIRE IN BUNDLE AND REPLACED RUDDER TRAVEL LIMITATION UNIT AS PRECAUTION.SDR CA070717010Connector · corroded(CAN) AFTER FLAP 25 TAKEOFF, WHEN FLAP RETRACTION INITIATED, FLAP ASYMMETRY INDICATED AND TE FLAP SKEW SENSOR CB POPPED. AIRCRAFT RETURNED TO JTR. SFCC BITE TEST CARRIED OUT, MSG 27-51407 INTERMITTENT. FIM TASK 27-51-00-810-848 CARRIED OUT WITH NO FINDINGS. VISDR COMA0760463Wire · nickedFLIGHT 5589 - FLAP FAIL MESSAGE RECEIVED. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPAIRED NICKED WIRE (SHORTING) AT PRESSURE BULKHEAD AFT OF WHEEL WELL.SDR DXTA200702311Circuit Board · inoperativeIN FLIGHT AT FL 430, MASTER CAUTION LIGHT ILLUMINATED, ACCOMPANIED BY AUDIBLE GONG. (FLAP ASYSTEMMETRY) CAUTION LIGHT ILLUMINATED (5) SECONDS LATER FLAP CONTROL CIRCUIT BREAKER IN OVERHEAD C/B PANEL POPPED. LANDED NO FLAP. REPLACED PCB CARD (50WW) WITH A NEW SDR COMA0760460Wire · nickedFLIGHT 5169 - FLAP FAIL MESSAGE RECEIVED. LANDED WITHOUT INCIDENT. REPAIRED NICKED WIRE (SHORTING) AT PRESSURE BULKHEAD AFT OF WHEEL WELL.SDR YENA2007062Wire Harness · faultyDURING CONFIGURATION FROM FLAPS 3 TO FLAPS 5 GOT FAIL MESSAGE. AIRSPEED WAS APPROX 150 KTS. QRH ACCOMPLISHED AND LANDED AT FLAPS 5 SETTING. REMOVED AND REPLACED RIGHT WING HARNESS (W611) IAW 27-83-01. RESET INHIBITS & OPS CHECKED PER AMM 27-83-02. NO FAULSDR COMA0760454Wire Harness · shortedFLIGHT 9456 - FLAP FAIL MESSAGE RECEIVED AT CRUISE. DECLARED EMERGENCY. LANDED AT CVG WITHOUT INCIDENT. REPLACED RIGHT WING BPSU HARNESS. NO FURTHER DEFECTS.SDR YENA2007059Wire Harness · defectiveSLAT FAIL AFTER TAKEOFF. FLT 1094, CMH-JFK RETURNED FOR LANDING AT CMH. REPLACED RIGHT SLAT 2/3 & 3/4 SKEW SENSOR HARNESSES PER AMM 27-83-07-400-801. CLEARED SF-ACE INHIBITS. NO EICAS MSG PRESENT. OPS CHECK OF SLATS IS NORMAL PER AMM 27-710-801. OK FOR RSDR YENA2007058Wire Harness · defectiveSLAT FAIL AFTER TAKEOFF. FLT 1094, CMH-JFK RETURNED FOR LANDING AT CMH. REPLACED RIGHT SLAT 2/3 & 3/4 SKEW SENSOR HARNESSES PER AMM 27-83-07-400-801. CLEARED SF-ACE INHIBITS. NO EICAS MSG PRESENT. OPS CHECK OF SLATS IS NORMAL PER AMM 27-80-710-801. OK FO
Back to JASC 2797