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 SIMA202001274001Connector · corrodedFOUND RH INBOARD, LH OUTBOARD, LH INBOARD SPOILER PROX SENSOR CONNECTORS CORRODED.-C/A-REMOVED AND REPLACED R/HAND INBOARD, L/HAND INBOARD, LH OUTBOARD PROX SENSORS, (FOR SPOILERS), CONNECTORS IAW EMB140 SPWM 20-50-01.SDR SWAA2020012240674Connector · faultyDECLARED EMERGENCY, UPON INITIAL FLAP EXTENSION ONLY 1/2 DEGREES OF FLAPS CAME OUT. ALSO THERE WAS AN ASYMMETRY CONDITION. LEADING EDGE. DEVICES DID NOT EXTEND. FOLLOWED QRH PROCEDURES FOR TRACKING EDGE FLAP / ASYMMETRY LEADING US TO TRACKING EDGE FLAPS UP SDR FDEA2020012100177Connector · misroutedMDIS 631 27-40 8820 20JAN20 ANC FACT U FOUND ELECTRIC CONNECTORS FOR #1 & #2 HORIZONTAL STABALIZER TRIM MOTORS ROUTED INCORRECTLY AND CROSSED. DISCOVERED WHILE WORKING WRI 27-40/8819 SDR SELECTED DUE POSSIBILITY OF FUTURE TRIMSDR AALA202001139034Connector · looseAIRCRAFT WAS GROUNDED: TRAILING EDGE FLAP LIGHT ILLUMINATED WHILE EXTENDING FLAPS. FLAP INDICATION WOULD NOT INDICATED MORE THAN 1 FLAP POSITION. ACCOMPLISHED BITE OF FSEU NO FAULT FOUND C/P AT T/E FLAP BYPASS VLV LOOSE SECURED AND OPS CHK OK IAW AMM 25-51-32 SDR VNAA2020010951102Connector · dirtyON THE ARRIVAL AT FL060, STAB TRIM RUNAWAY. THE CREW RAN THE QRH AND DECIDED TO DIVERT TO IAD FOR THE LONGER RUNWAY. CREW DECLARED AN EMERGENCY. CABI DID NOT BRACE, TRUCKS DID ROLL. FLIGHT LANDED ON RWY 1C WITHOUT FURTHER INCIDENT AND WAS ABLE TO TAXI TO GASDR RU3A201910243055Connector · dirtyRUDDER BOOST LIGHT ACTIVATED IN FLIGHT FOR 40 MINUTES. MAINTENANCE CLEANED CONNECTORS AND INSPECTED RUDDER BOOST SYSTEM, NO FAULT WAS DISCOVERED. WILL CONTINUE TO MONITOR FOR FURTHER DISCREPANCIES.SDR AWKA2019100401Ground Stud · dirtyDURING RETURN TO LNK AND WHILE CONDUCTING A MX CONFIDENCE FLIGHT FOR FLAP ISSUE, FLIGHT CREW RECEIVED AN AMBER FLAP FAIL CAS MESSAGE. CREW RAN THE APPROPRIATE CHECKLIST AND THEN DECLARED AN EMERGENCY. SEVERAL MINUTES FOLLOWING, CREW WAS ABLE TO LOWER THE FLAPSSDR AALA201907239045Wire · shortedAIRCRAFT WAS GROUNDED: PILOT REPORTS SHORTLY AFTER TAKEOFF CADC DATA FAIL MESSAGE WITH LOSS OF DFGC DISPLAYS. RETURNED TO DFW. CB C17 DIGITAL FLIGHT GUIDANCE SYSTEM - SWITCH A FOUND OPEN. MAINTENANCE REMOVED AND REPLACED #1 AND #2 DFGCS IAW AMM 22-01-01. ACCOSDR AALA201907019054Connector · looseAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY INBOUND TO CLT ON ACCOUNT OF FLAPS ASYMMETRY ISSUE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED VISUAL CHECK OF FLAPS IAW AMM 27-51-00. NO OVER TORQUE INDICATORS TRIPPED. CONFIRMED FAILURE. TROUBLESHOT SDR 2019FA0000195Wire · brokenFOUND LEFT AILERON SHUTOFF SWITCH HARNESS TO BE FRAYED AND SHORTING TO GROUND NEAR SHUTOFF SWITCH. VERIFIED THE BLUE WIRE 1D2-22, IN WIRE HARNESS 1D1ZB22 (WHT) TO BE COMPLETELY CUT OFF. THIS CONDITION CAUSES THE LEFT AILERON HARD OVER PROTECTION TO BE INOPERSDR UIEA201906214537Wire · damagedFLAPS DRIVE EICAS MESSAGE. TROUBLESHOT FLAP FAULT IAW FIM 27-58 TASK 826 AND 827, FOUND WIRE W4515-304-20R AND 305-20B SHORTED TO SHIELDING BETWEEN CONNECTORS D44002J AND DM788P. REMOVED AND REPLACED WIRE IAW WDM 27-58-22. PERFORMED FLAPS OPS CHECK IAW MM 27-SDR SIMA201906132002Connector · looseIN FLIGHT PTRIM BACK INOP AND PTRIM MAIN INOP WARNING MESSAGE IN FLIGHT. PERFORMED GVI BEHIND TRIM PANEL AND FOUND LOOSE CONNECTION. RECONNECTED PLUG. REINSTALLED TRIM PANEL IAW EMB 140 AMM 20-13-10. PERFORMED OPS CHECK W/CREW. OPS CHECK GOOD. AIRCRAFT OK FOSDR DALA2019060903462Wire · pinchedON TAXI OUT WHEN CHECKING CONTROLS THE WHEEL BECAME STUCK FULL RIGHT. FOUND WIRING INTERNAL ON DUAL AILERON SERVO PINCHED AND WIRING EXSPOSED. DUAL AILERON SERVO WAS REPLACED PER B717 AMM 22-12. FAILED AILERON RTS TEST. REPLACED THE SERVO A SECOND TIME PER B71SDR CA190531004Wire Harness · damaged(CAN) AFTER TAKE-OFF FLAPS WERE SELECTED TO 0*. FLAPS BEGAN TO TRANSIT FOLLOWED BY FLAPS FAIL MESSAGE. BOTH LEFT AND RIGHT FLAPS INDICATED 5. FOUND R/H O/B HARNESS WITH HIGH RESISTANCE. (TC# 20190531004)SDR DALA2019053003315Wire · burnedREF WDM 30-31-03 PG 2 WIRE F1551B20 FOUND BURNT THROUGH IN OVERHEAD F/C CABIN. RAN AND SPLICED WIRE F1551B20 IAW SWPM 20-10. TERMINATED AT R5-1201 IAW SWPM 20-31. 903393. WIRING CKS C/W IAW WDM 30-31-03. 399270. OPS CHECK PRIM STAM TRIM MOTOR HEATER PER AMM 27SDR CA190530002Interface Unit · degraded(CAN) THIS SDR IS SUBMITTED PER CSALP PROCEDURES UPON THE OPENING OF CONTINUING AIRWORTHINESS PROJECT NUMBER CAW-BD5-27-0169. THE INCEPTOR INTERFACE MODULE NO. 3 (IIM 3) COMMAND BOARD SEPARATION PROCESS WAS FOUND TO INDUCE MECHANICAL STRESS ON FOUR CERAMIC CASDR Q2SA20190518417Connector · looseAIRCRAFT GROUNDED. TRAILING EDGE FLAPS WOULD NOT EXTEND PAST 2 IN NORMAL; WOULD EXTEND TO 15 USING ALTERNATE FLAPS. C/W INSPECTION OF ALL RELATED FLAP COMPONENTS FOR DEFECTS. UPON INSPECTION, FOUND LH FLAP POSITION TRANSMITTER CONNECTOR LOOSE WITH RED BAND SHOSDR HNAA2019051600145Wire · damaged658 27-70 0001800 05MAY19 RIC CLOSE GUST LOCK SYSTEM OPERATIONAL CHECK FAILED. GUST LOCK LEVER DOES NOT LOCK WHEN TAKING TARGET OUT FROM WOW PROX SWITCH.DISCOVERED PIN 57 , WIRE W102-13771-22, CONNECTOR DFRL 05MAY19 11:00 RIC P0838 BARE AND MAKING CONSDR CA190502007Wire Harness · damaged(CAN) ARRIVED WITH A `FLTCTRL FAULT` CAS MESSAGE. THE FAULT WAS `THE SECONDARY POWER OF REU UNIT 5 IS DISCONNECTED OR FAILED` AFTER A LENGHTY INVESTIGATION FOUND WIRE C60BA22 DAMAGED FROM CONTACT WITH THE AFT MAIN SHIP BATTERY. THIS WIRE RUNS FROM PIN 77 AT COSDR AALA201904259008Wire · shortedAIRCRAFT WAS GROUNDED: PILOT REPORTS RETURNED TO PHL ON ACCOUNT OF FLAP PROBLEM (FLAPS AND SLATS JAMMED AFTER TAKEOFF). EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TSM TASK 27-51-00-810-818-A. ACCOMPLISHED VISUAL INSPECTION OF FLAP TRSDR CA190423006Wire · damaged(CAN) DURING CLIMB, APPROXIMATELY 15 MINUTES INTO THE FLIGHT AN (AMBER) `FLAPS FAIL` CAS MESSAGE POSTED ON EICAS. CREW ELECTED TO RETURN TO HOME BASE. AIRCRAFT RETURNED HOME ON FRIDAY. DURING THE VISIT A REPAIRED FLAP ACTUATOR PN 2253A0000-01 SN 00895 WAS INSTSDR DJSR2019050800001Wire · shortedTRIM RUNAWAY NOSE DOWN. FOUND AND REPAIRED SHORTED WIRE ON 3A 21 TERMINAL STRIP.SDR UIEA2019040503807Pin · damagedDURING DISARM OF OFF WING ESCAPE SYSTEM FOR MAINT. FOUND LH SPOILER OVERRIDE ACTUATOR SQUIB PINS PUNCHED AND BENT. REMOVED AND REPLACED LH SPOILER OVERRIDE ACTUATOR SQUIB IAW AMM 25-65-10. OPS CHECKED GOOD IAW AMM 25-65-00.SDR YBBA2019050800001Wire · brokenDURING MX PRE FLIGHT OPS CHECK FLAPS, OPERATION OF FLAPS ERRATIC, DURING INSPECTION L/N FLAP FOUND BROKEN BROKEN WIRE ON MICRO SWITCH, REPAIRED AND FUNCTIONALLY TESTED NO FAULT FOUND, AIRCRAFT RELEASED TO SERVICE 04/01/2019.SDR DALA2019032902016Connector · dirtyTE FLAP ASYMMETRY WITHOUT TE FLAP ASYMMETRY LIGHT. DEFINITE LEFT ROLLING MOMENT WITH AUTOPILOT OFF. LANDED WITH LEFT FLAP BETWEEN ONE AND FIVE AND RIGHT FLAP AT FIVE. FLAPS CAME UP NORMALLY AFTER LANDING. REMOVED CONNECTOR FROM OUTBD LT FLAP TRANSMITTER POS 1.SDR CALA2019031500413Connector · brokenLE SLAT ASYM EICAS MSG DISPLAYED AT FL350 NO SLAT OR FLAP MOVEMENT NOTED PERFORMED BITE OF FSEU1(-40) & FSEU2(-40) PER FIM 27-51-00-815- 805. FOUND "SLAT LOSS" FAULT ON FSEU1, "SLAT ARM DISAGREE" FAULT ON FSEU2, AND NO FAULT ON FSEU3. UPON CHECKING L/E SLAT LOSDR AALA2019031439011Wire · shortedTHE PILOT REPORTED THAT THE DIGITAL FLIGHT GUIDANCE CIRCUIT BREAKER -B- TRIPPED INFLIGHT AND WOULD NOT RESET. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND RUDDER POSITION SENSOR WIRING 2C61033RD CONDUCTOR SHORTED TO AIRCRAFT FRAME IN TWO PLACES. REPAIRED TSDR HNAA2019030700061Connector · shortedPDIS 683 27-60 1854021 06MAR19 PHL CLOSE CLIMBING THROUGH 18000FT SPOILER FAIL AND THEN NOTICED C/B F-22 WAS POPPED. SPOILER INDICATION WAS OPEN. HISTORY: YES FACT 06MAR19 04:08 PHL MX INSP FOUND RT OB SPOILER PLUG 1166 SHORTED TO GROUND AT PIN A RSDR DALA2019030601488Wire · burnedAUTO GROUND SPOILER SYSTEM. WHILE T/S BURNED WIRES ON LOG 5845168 FOUND WIRE G508H24 BURNED IN HALF, REPAIRED WIRE PER WSPM CHAP 20 AND WDM 27-61 AUTOGORUND SPOILERS NOW CK GOOD. (LP5845162)SDR CA190226013Connector · failed(CAN) CREW REPORTED THEY LANDED WITH SPLIT TRAILING EDGE FLAPS, WHICH SPLIT PRIOR TO FLAPS 2. BOTH LH AND RH FLAP POSITION TRANSMITTERS WERE REPLACED IAW AM 27-58-01. PN: OFF 18-1738-10 SN #`S: 3950 AND 3954. SNAG REPEATED ON TWO FLTIGHTS LATER WHEN ON APPROACSDR JIKA2019020901Connector · contaminatedTHE PILOT REPORTED WHILE ON FINAL APPROACH INTO KSMX THAT THE AIRCRAFT MADE AN UNCOMMANDED NOSE PITCH DOWN ATTITUDE AT APPROXIMATELY 200’ AGL. THE PILOT DECLARED AN EMERGENCY THEN LANDED WITHOUT INCIDENT IN KSMX. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THSDR YENA2019020130050Connector · unsecureFT # 1336, DTW-BOS. SLAT FAIL ON APPROACH TO BOSTON.INDICATED SLATS AT O FOLLOWED QRH PROCEDURE; FOUND SLAT SKEW SENSOR 2-3 RH ELECTRICAL CONNECTOR BACKED ALL OF THE WAY OFF. THE OTHER 3 SLAT SKEW SENSOR ELECTRICAL CONNECTORS WERE ALSO BACKED OFF BUT NOT ALL OSDR SIMA20190103001Connector · defectiveSUPPLEMENTAL SPOILER FAIL ON EICAS DURING FLIGHT "TRANSFERRED TO NRWC 803-DFW-02162" C/A- REMOVED AND REPLACED CONNECTOR ON LT OUTBOURD SPOILER PROX SWITCH IAW SWPM 20-50-00 OPS CHECKS GOOD IAW AMM 27-63-01. REMOVED AND REPLACED CONNECTOR ON LT O/B SPOILER PROSDR AALA201901049004Connector · burnedSPOILER 11, ELECTRICAL CONNECTOR PINS BURNED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE NR 11 SPOILER ACTUATOR HARNESS IAW AMM 20-14-11 AND SPOILER ACTUATOR IAW AMM 27-61-09.SDR COEA2018121215921Connector · unsecureFLIGHT 8298, ENROUTE AFW-TUL DISCREPANCY: DURING CLIMB, CREW RECEIVED AN IN FLIGHT PITCH TRIM ASYMMETRY FAULT. IN ADDITION THE BREAKER H1 POS ID TRIPPED IN FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT IN TUL. CORRECTIVE ACTION: MAINTENANCE FOSDR R61A2018113091184Wire Harness · malfunctionedSLAT FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R HARNESS W611 AND SKEW SENSOR ON RH SLAT 2/3 IAW AMM 27-83-01 AND 27-83-07.SDR VNAA2018112611102Pin · disconnectedTHE AIRCRAFT DIVERTED DUE TO LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGE AND FLAPS FAIL. MAINTENANCE WAS DISPATCHED AND FOUND PIN 4 ON CONNECTOR A105P1. RECONNECT PIN AND ALL PROBLEMS OPERATIONAL CHECK GOODSDR ASMF20190109009Connector · disconnectedAIRCRAFT WAS SENT TO THE HANGAR DUE TO AIRCRAFT ON GROUND HANDLING, CAPTAIN REPORT THAT LT AND RT WING DOWN DOES NOT OPERATED (AILERON TRIM) SHOWING FRM 271 050 48; MAINTENANCE PERSONNEL PERFORMED WIRING INSPECTION IAW WDM 27-11-11 AND FIM PROCEDURE 27-11 TASKSDR WX0A2018112173373Connector · dirtyFLAPS STUCK AND DID NOT EXTEND. EMERGENCY DECLARED. CLEANED BOTH CONNECTORS ON THE LT WTB. LUBRICATED THE FLAP TRACK CARRIAGE ROLLERS.SDR AALA201810264008Connector · dirtyFLAPS WOULD NOT RETRACT. EMERGENCY WAS DECLARED AND FLIGHT WILL NOT LAND. FLAPS DID NOT EXTEND BEYOND 15 DEGREES AFTER BEING COMMANDED ON APPROACH. THE AIRCRAFT WAS GROUNDED. CLEANED THE T427 CONNECTOR. OPS CHECKED THE FLAPS IAW FIM 27-51-00-818-813. OPSSDR FDEA201810132874Wire · shortRECEIVED LEVEL 2, SLAT DIAG, ALERT ON APPROACH AFTER SELECTING FLAPS 15 DEG. ISOLATED SHORT IN N011-10-20RD NEAR CLAMP UNDER PANEL 517CT AT TRANSITION POINT BETWEEN NR 1 ENGINE PYLON AND OUTBOARD LEADING EDGE. REMOVED AND REPLACED 3 FOOT SECTION OF TWISTED PAISDR R61A201810111016Connector · unsecureSLAT FAIL IN FLIGHT. FLAPS DEPLOYED TO "2" MAX BRAKE TEMP ON LANDING 290 C ON RIGHT MAIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND LT OUTBOARD SLAT SKEW SENSOR CONNECTOR OFF. RE-SECURED CONNECTOR ON LT OB SKEW SENSOR IAW AMM 27-83-01.SDR HNAA2018091100219Connector · dirtySPOILER FAIL EICAS MSG AFTER T/O WITH SPOILERS INDICATING INTERMITTENTLY OPEN-CLOSE. INSPECTED AND CLEANED ALL INBOARD SPOILER CONNECTORS. PERFORMED OPS CHECK OF SPOILER SYSTEM IAW AMM 27-63-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OKAY FOR SERVICE.SDR HALA2018090800418Wire · brokenRUDDER RATIO EICAS IN FLIGHT. AIR TURNBACK, TROUBLESHOT TO A BROKEN WIRE W1261-304R-22. REMOVED THE WIRE & CAPPED. INSTALLED THE SPARE WIRE. OPS CHECKED THE RUDDER RATIO, AND YAW DAMP SYSTEM, ALL OPS NORMAL, OK FOR SERVICE IAW AMM 27-21-13.SDR AALA2018090649041Wire Splice · faultyAFTER TAKE OFF, AND DURING CLIMB OUT, EICAS MESSAGE LEADING EDGE SLAT ASSEMTRY MESSAGE ILLUMINATED. EMERGENCY DELCARED AND AC RETURNED TO THE FIELD, FLIGHT LANDED WITHOUT ISSUE. THE AIRCRAFT WAS GROUNDED. DURING TROUBLESHOOTING, FOUND A BAD SPLICE SM7 AND SDR AALA20180817001Connector · damagedAT FL 350, AN L/E SLAT ASSEMBLY EICAS MESSAGE WAS INTERMITTENT, FLAP INDICATION NEEDLE ERRATIC, LEADING EDGE WARNING LIGHT INTERMITTENT, CLICKING NOISE IN THE OVERHEAD CIRCUIT BREAKER PANEL. AN EMERGENCY WAS DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCISDR ASAA2018080635675Terminal · looseLE FLAP TRANSIT LIGHT REMAINED ILLUMINATED AFTER TAKEOFF, WHEN SELECTED FLAPS 5 TO FLAPS 1. ACFT GROUNDED. EMERGENCY DECLARED. PERFORMED FIM 27-51, TASK 801. RECEIVED FAULT CODE 27-81217 IN HISTORY. IAW FIM 27-88, TASK 806, SENSOR S169 SHOWS FAR WHEN SHSDR QXEA2018073100270Connector · dirtyNR 1 RUD HYD ILLUMINATED DURING CRUSE FLIGHT AT 14,000. RETURNED TO THE FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND HI RESISTANCE IN WIRE 2700-P4 PIN 2 TO 2700-P1 PIN 6. CLEANED CONNECTORS AND RECHECKED AND CHECKED GOOD. COMPLYED WITH OPS TEST OF RUSDR RAIA201807260002Connector · loosePITCH TRIM MAIN INOP. INSPECTED HSCU, FOUND CONNECTOR J2 LOOSE. SECURED CONNECTOR, RESET SYSTEM, OPS CHECK GOOD AT THIS TIME.SDR CALA2018062201513Wire · brokenLEFT ELEVATOR PITOT PROBE LIGHT ILLUMINATED. FOUND A BROKEN WIRE ON THE ELEVATOR FEEL PROBE CONNECTOR. REPLACED THE CONNECTOR IAW SWP 20-64-15. ELEVATOR PROBE HEAT CHECKED NORMAL. SYSTEM LEAK CHECKED NORMAL IAW AMM 27-31-17. OK FOR SERVICE.
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