JASC 2297
Service difficulty reports · 149
Reports filed under 2297 · Auto Flight 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 = '2297' 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 = '2297' 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 CALA2026040315058Elec Connector · faultedDISCONNECTED ELECTRICAL CONNECTOR D40024P FROM D400424J IAW WDM 22-11-11-2 AND INSTALLED ESDS TAPE FOR CONNECTORS D40024P & D400424J, REPLACED D40024P, SEVERAL LOCKS BROKEN. NEEDS TO BE REPLACED. REPLACED CONNECTOR D40024P IAW WDM 22-12-31 & WDM 22-11-11. SSDR QMLA2026031620017Circuit Breaker · faultedRED A/P TRIM LIGHT WITH ASSOCIATED ALARMS & CHIMES. PITCH TRIM EXCURSIONS CAUSING ALTITUDE DEVIATION. RESET AP TRIM CB OPS CHECKED GOOD. RTSSDR 2025FA0000787Elec Connector · dirtyYAW ACTUATOR LIGHT ILLUMINATED ON AUTO PILOT TEST. INSPECTED, CLEANED, AND RESEATED THE YAW SEMA CANNON PLUG PROBLEM WENT AWAY.SDR 2025FA0000336Terminal Block · faultedPILOT NOTED THE SMELL OF OZONE OR ELECTRICAL CIRCUIT GETTING HOT WHILE DEPARTING NK-71. NO SMOKE OR SYSTEM FAILURE WAS INDICATED. AS HE WAS STILL NEAR BASE OF OPERATION, AT NIGHT OVER A HEAVILY WOODED AREA HE DECIDED TO RETURN TO BASE. DURING INSPECTION THE BSDR GTIA2025041438852Elec Connector · inoperativeIN CRUISE AT FL 340 AUTOPILOT DISCONNECTED AIRCRAFT PITCHED UP AND RIGHT. ECAM ELEC GEN 1 FAULT, AUTO FLT YAW DAMPER 1, RUD TRIM 1 FAULT, RUD TRU CIM 1. FCOM AND EQRH RAN. RESETS SUCCESSFUL. ABOUT 30 MINUTES LATER SAME AXACT ECAMS. ELEC GEN 1 RESET UNSUCCESSFUSDR QMLA2024122420152Connector · dirtyUPON LEVEL OFF AND PRIOR TO FINAL APPROACH THERE WERE TWO CONSECUTIVE UNCOMMANDED RIGHT LATERAL FLIGHT CONTROL INPUTS. CLOSEST PLACE TO LAND WAS BACK AT BASE. NO OTHER EVENTS FOLLOWED. CLEANED CONNECTOR PLUGS ON EHA'S AND TEST FLOWNSDR CALA2024062801929Wire · damagedMACH TRIM FAIL LIGHT AND CA PITCH FD FAILED ON TAKE OFF POSITION TRANSDUCER OR WIRING ISSUE. FOUND P18-1 C5 AFCS SYS A SENS EXC AC OPEN (HAS HISTORY). DFCS BITE SHOWED FCC 1 FAIL (NO POWER DUE TO POPPED BREAKER). CLOSED BREAKER- DFCS BITE PASSES. SEE SSM 22-1SDR UIEA2024051400390Connector · faultedREJECTED TAKEOFF DUE TO NO AUTO THROTTLE AFT ENGAGING, EPR, AND V SPEEDS. DELETE TMC ANNC LIGHT(<P>REMOVED AND REPLACED CONNECTOR D4224P REF WDM 73-21-11. OPS CHECK GOOD AT THIS TIME.</P>)SDR CALA2023110203256Connector · unknownTHRUST MANAGEMENT SYSTEM A/T DISC LIGHT ILLUMINATED WITH AUTOTHR OTTLE ENGAGED IN (STATE MODE) MODE. THRUST REFERENCE MODE DISPLA Y ON EICAS & F/S POINTER DISPLAY ON EADI NORMAL IN VNAV PATH MODE ARRIVAL CREW INFORMATION: A/T DISCONNECTED IN CRUISE, RESET SDR 6CBA2002306070001Pitot System · shortedTHE FLIGHT CREW DEPARTED KIXA WITH A DESTINATION OF KPBI. DURING CLIMB, THE FLIGHT CREW REPORTED SMOKE IN COCKPIT COMING FROM GASPER VENT ON PILOT'S SIDE. ALSO NOTED AN ECB TRIP CYAN CAS STBY PS HEAT FAIL AMBER CAS. FILES WERE DOWNLOADED AND SENT TO PILATUS. SDR 7C7A2022120800036Wire Harness · corrodedAUTO FEATHER DID NOT ARM WHEN T/O POWER APPLIED.SDR ASAA2022120541021Circuit Breaker · faultedLNAV & VNAV WILL NOT ENGAGE. CO-PILOT COURSE WINDOW DISPLAYS ALL 8'S. GROUNDED - YES. RESET C/B IAW FIM 22-11 TASK 803. OPS CK NORMAL.SDR ASAA2022011341520Circuit Breaker · trippedFOUND CB B4 ON P6-2 POPPED. GROUNDED - YES. CB AFCS SYS B "ENGAGE INTLK" POPPED. PERFORMED INSPECTION PER B737-9 AMM 20-61-01. CB STAYS IN AND NO DEFECTS NOTED. PERFORMED DFCS BITE AUTOTEST PER AMM AMM 22-11-00-740-814 STEP B1F SYS A+B. NO FAULTS.SDR YENA2021112200776Fcu · failed(ETOPS) FLT 20, LHR-JFK. P1-TSI R/R FCU DUE TO PREVIOUS WRITE-UP, PLEASE REMOVE AND REPLACE THE FCU PER AMM 22-81-012. PLEASE MARK THE OLD UNIT AS SOS. ; (RESOLVED ON W/O: 1146268 TASKCARD: NR-00001 ) R/R FCU REF AMM 22-81-12/SDR YENA2021112200773Fcu · fault message(ETOPS) FLT 7, JFK-LHR. CREW REPORTED FCU 1 FAULT; PERFORMED POWER DOWN AND POWER UP OF AIRCRAFT. MESSAGE CLEARED. PERFORMED OPS CHECK PER AMM 22-96-00-710-001-A. NO FAULTS NOTED.SDR ASAA2021042134629Connector · corrodedDURING T/S OF 'B' AUTOPILOT ELEVATOR ACTUATOR FOUND CORROSION ON 'A' ELEVATOR AUTOPILOT ACTUATOR. CONNECTOR #. GROUNDED - YES. REMOVED AUTOPILOT ELEVATOR ACTUATOR "A" REF B737-800 AMM 22-11-26-00-801. INSTALLED NEW "A" AUTOPILOT ACTUATOR. LEAK CHECK OK. REF AMSDR 2021F00059Wire · cutPILOTS REPORT HAVING AN UNCOMMANDED AUTOPILOT DISCONNECT THAT RESULTED IN THE AIRPLANE PITCHING UP. THE CAPTAIN PUSHED THE YOKE FORWARD AND GOT SPARKS FROM THE FORWARD SIDE OF THE YOKE. THE AIRPLANE LANDED AT KLAL INSTEAD OF KAPF. IT APPEARS THAT THE SHARP ESDR HYIA20210311002Wire · chafedTHE PILOT REPORTED A BURNING SMELL AFTER THE AUTOPILOT CB POPPED DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND CHAFFED WIRING AT THE PTT SWITCH. THE WIRES WERE REPAIRED WITH NO FURTHER DEFECTS NOTED.SDR ASAA2021021134081Wire · damagedAUTOTHROTTLE FAILED TO ENGAGE PRIOR TO TAKEOFF. GROUNDED - YES. REF B737-700 WDM 22-31-51, FOUND SPLICE SP3101 PULLED ON W0051-0108-22. INSTALLED NEW SPLICE REF SWPM 20-30-12. A/T OPERATIONAL TEST PASS MM 22-31-00-700-801.SDR VNAA202101011111Circuit Card · failedFLIGHT CONTROLS LOCKED AFTER DISCONNECTING AUTOPILOT (PITCH AND ROLL) HAD TO USE SOME FORCE TO UNLOCK CONTROLS. 2020-12-30: REMOVED AND REPLACED FCC CARDS 1 AND 2, IAW CRJ700 AMM 22-12-14-00-000/400-801-A01. OPERATIONS CHECK GOOD. PERFORMED OPERATIONS CHECKSDR ABXA2020081203162Wire · corrodedMAINTENANCE WAS BEING PERFORMED ON AUTO PILOT SYSTEM FOR NO LAND 3 EICAS MESSAGE. RT AUTOPILOT WILL NOT ENGAGE. WIRING WAS FOUND TO BE CORRODED. WIRE W1729-002-20. AIRCRAFT WAS GROUNDED AND SPLICE REPAIR TO WIRING WAS COMPLETED.SDR AALA202003019021Wire · failedAIRCRAFT NOT GROUNDED: AUTO-THROTTLE UNCOMMANDED DISCONNECT. WOULD NOT RE-ENGAGE. FOUND WIRE BAD UNDER NO.1 THROTTLE HINGE POINT. REPLACED THROTTLE LEVER ASSY.SDR JIKA20200227501Wire · damagedDURING TAKEOFF ROLL FROM DFW PITCH TRIM WAS ADJUSTED UP FOR CLIMB. THE TRIM CONTROLS STOPPED WORKING WHILE THE WHEELS LIFTING OFF FROM THE RUNWAY. IT WAS DIFFICULT TO MAINTAIN ALTITUDE ASSIGNED SINCE THE AIRCRAFT KEPT CLIMBING. THE PILOT HAD IMMEDIATELY ADVISESDR ASAA2020020542083Connector · dirtyAFTER AUTO PILOT "A" WAS ENGAGED SPEED TRIM FAIL LIGHT ILLUMINATED. AFTER SEVERAL SECONDS SPEED TRIM FAIL LIGHT EXTINGUISHED LESS THEN 60 SECONDS ELAPSED AND STAB OUT OF TRIM LIGHT ILLUMINATED. WE FOLLOWED PROCEDURE IN QRH. GROUNDED - YES. DIVERSION TIME 52 MISDR ASAA2019103127155Wire · brokenDURING DESCENT THE AUTOPILOT DISCONNECT AURAL WARNING FAILED TO SOUND WHEN AUTOPILOT B WAS DISCONNECTED AT FO YOKE SWITCH. THE DISCONNECT LIGHT DID ILLUMINATE DURING DISCONNECT. SAME RESULT FOR AUTOPILOT A. SAME RESULT WHEN USING DISCONNECT SWITCH ON CAPTAINS SDR AALA201908199001Wire · pulledAIRCRAFT WAS GROUNDED: PILOT REPORTS IN CRUISE, AP 1/2 COULD NOT HOLD LEVEL FLIGHT AFTER INSTRUCTIONS TO INCR/DECR SPEED. ALT TRIM WAS NOT TRIMMING. CHECKED ALT LONG TRIM WITH ALT TRIM SWITCH, NO MOVEMENT UP OR DOWN, ON GROUND SAME. (NO AUTOPILOT TRIM.) MAINTESDR AALA201905069027Connector · faultyAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTS THAT DURING CLIMBOUT FROM SJU WITH AUTOPILOT ENGAGED, A/C HAD 2 UNCOMMANDED ELEVATOR INPUTS WHICH SHOOK THE CONTROL COLUMNS. 1ST TIME WAS AT FL180 AND THE 2ND WAS AT FL260. MAINTENANCE CURRENTLY WORKING THIS EVENT.***SDR ASAA2019041979047Terminal Block · unsecureAT LEVEL CRUISE FLIGHT AUTOPILOT A DISENGAGED. AUTOPILOT A WOULD NOT RE-ENGAGE. COMPLETED FLIGHT ON AUTOPILOT B. GROUNDED - YES. DFCS SHOWS NUMEROUS FAULTS ASSOCIATED WITH SMYDC-1 MSG 22-11081 FOR CH A THROUGH OUT FAULT HISTORY. NO SMYDC FAULT ON CDS BITE OR HSDR HYIA2018101515001Connector · damagedPILOT REPORTED SMOKE IN COCKPIT AND THE AUTOPILOT SYSTEM CIRCUIT BREAKER POPPED. MX PERFORMED INITIAL INSPECTION AND FOUND THE AUTOPILOT INTERFACE CONNECTOR DAMAGED. THE SYSTEM WAS PLACED ON MEL, FURTHER DETAILS WILL BE PROVIDED IF ADDITIONAL FAILED PARTS ARE SDR ASAA2018100926454Wire Harness · shortedDURING ARRIVAL TO SEA 34L, AUTOPILOT WOULD NOT DISCONNECT USING THE AUTOPILOT DISENGAGE BUTTON ON EITHER YOKE. USED DISENGAGE BAR ON THE MCP PANEL TO DISCONNECT A/P, APPROX 300AGL. GROUNDED - YES. REF DFCS BITE FIM 22-11 TASK 801, NO FAULTS LOGGED LAST LEG. VESDR ASAA2018091726138Connector · disconnectedAT CRUISE WITH AUTOPILOT A ENGAGED WE SLOWED DOWN FROM M .77 TO M .69 AT FL400. ACFT PITCH NOSE DOWN AS WE SLOWED. AUTOPILOT WAS MANUALLY DISCONNECTED TO CORRECT ALTITUDE ACFT WAS OUT OF TRIM IN NOSE DOWN. TRIM WAS 5 UNITS FROM CLIMBOUT UNTIL MANUALLY RETRIMMESDR CA180723019Wire · chafed(CAN) ELEC SMOKE ON TAKE OFF BY CAPT LEFT KNEE. FOUND 2 FMS WIRES W09008-815 & W09008-816 CHAFED, BOTH WIRES ISOLATED & SECURED. ALL OTHER LOCAL WIRING INSPECTED. NO FURTHER DAMAGED FOUND NR 2 FMS INOPERABLE, DMI 55164 OPENED, IAW MEL 34-60-1A. INOPERABLE SDR AALA20171204009Wire · shortedAIRCRAFT WAS GROUNDED. AUTO PILOT OFF, CLIMBING THRU 10,000 ADJUSTED RUDDER TRIM WHEN AIRCRAFT BEGAN ROLLING DUE TO RUDDER YAW. YAW DAMP OFF DFG APPEARED TO BE COMPLETED INOPERABLE DUE TO CONTROL ISSUES. DECLARED EMERGENCY, RETURNED TO OMA FOR LANDING AS AIRCRSDR DALA2017042503436Wire · chafedBURNING SMELL IN COCKPIT FROM CB PANEL ABOVE FO. FOUND WIRE FOR CENTER FCC SERVO ON POWER SIDE OF BREAKER CHAFING ON FRAME. PERFORMED REPAIR SPLICE IAW SWPM CH 20-11. OPS CHECKS NORMAL.SDR ASAA2017010219230Wire · unsecureAUTO THROTTLES WILL NOT ENGAGE. ACFT GROUNDED. CONFIRMED FAULT, A/T FAILS BITE TEST. BOTH DFCS & A/T FAULT HISTORY PAGE SHOWS NUMEROUS FAULT MESSAGES 22-31502 ASM-2 & 22-31263 CH-A ARM A/T . ACCOMPLISHED GVI INSPECTION OF A/T DC-1 C/B AT P18-1 (E1). WIRINGSDR DALA2016122610082Wire Harness · burnedAT CRUISE, MASTER WARNING CAME ON OAP DISPLAY MACH TRIM INOP/ YAW DAMP INOP/ IRS1 BATT FAIL/STALL IND FAILURE. BOTH AP AND ATNOP- ATL WINDOW BLANK & COULD NOT ADJUST SPD INDICATOR. MASTER WARNING WOULD NOT RESET C/BS C12 AND C17 POPPED AND WOULD NOT RESET. SDR ASAA2016091918074Circuit Breaker · trippedAUTOTHROTTLE WILL NOT ENGAGE. ACFT GROUNDED. FOUND CIRCUIT BREAKER AFCS SYS A WARN LIGHT (BAT) OUT. RESET PER AMM 20-60-01. LAND VERIFY PASS GROUP 49, IAW AMM 22-11-00, HGS SYSTEM TEST PASS PER MMS 34-36-00. UPGRADES ACFT TO CAT IIIA AUTOLAND & HGS. LWMP SDR 2015FA0000616Connector · wrong partAUTOPILOT UNCOMMANDED ROLL OSCILLATION EXCEEDING BANK LIMITS. FOUND OPEN ROLL LOW SIGNAL BETWEEN NR 1 AHRS AND AUTOPILOT COMPUTER. FURTHER INSPECTION REVEALED INCORRECT SOCKET INSTALLED IN P909, PIN 77. INSIDE DIAMETER WAS TOO LARGE, .063 VS. REQUIRED .040, SDR ASAA2015071712467Connector · dirty"B" AUTOPILOT UNCOMMANDED DISCONNECT AT 13,000 FT DURING VNAV DESCENT, NO OTHER FAULTS NOTED. DESCENT AND SPEED NORMAL AND ON PROFILE. ACFT GROUNDED. REF WDM 27-32-21, FOUND INTERMITTENT 28VDC AT CONNECTOR D3685A PINS 1 & 13 WHILE SHAKING WIRES BEHIND RACK SDR FDEA201507012131Wire · damagedFOUND 14 TWISTED WIRES, OUTER PROTECTIVE INSULATION BADLY DETERIORATED AT ABOUT BS 495 - 555 FLOOR AREA. R & R IAW SWPM 20-10-01. CONTINUITY CHECKED IAW WDM 22-16-02, WDM 27-66-01, WDM 28-48-01, WDM 52-71-02, WDM 73-33-01, WDM 29-31-01 & WDM 79-33-01 FOUND SSDR EBVR20150701001Connector · deterioratedPERFORMED ASCB SELF TESTS IN MAINTENANCE MODE AND INTERMITTENT FAULT CODES 4014-1, 4016-5 AND 4017-5 OCCURRED POINTING TO ADC PRIMARY BUSS AND AFCS BUSS FAULTS. SEVERAL ENVIRONMENTAL SPLICES WERE FOUND IN NEED OF REPLACEMENT. THE SLEEVE PORTION OF THE ENVIROSDR ASAA2014111409664Connector · looseAUTOTHROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. IAW WDM 22-31-41, FOUND CONNECTOR D10027 AT ASM NR 2 LOOSE. SECURED CONNECTOR, ACCOMPLSIHED A/T SERVO MOTOR TEST SEVERAL TIME, TESTS PASSED. CURRENT STATUS TEST PASSED REF MM 22-31-00.SDR SWIA201438098Connector · damagedDURING CLIMBOUT, THE F/O`S ALTITUDE WAS AT 12 DEGREES. CAPTAIN'S AND STBY WERE AT 4 DEGREES PITCH UP. F/O`S SIDE HAD A COMPUTER AND HDG FLAG. AT CRUISE, THE AUTOPILOT KICKED OFF AND WE RECEIVED AN ATTITUDE DISPLAY AND AUTOPILOT FAIL ON MAP. RETURNED TO FIELSDR MDGA201404230091Pin · brokenDURING CLIMB OUT, AUTOPILOT STOPPED RESPONDING TO ALL PITCH COMMANDS. CREW RETURNED TO DEPARTURE. EMERGENCY DECLARED. MAINTENANCE FOUND A PIN ON THE CONNECTOR TO THE AUTOPILOT CONTROLLER NOT SEATED. LOCKING MECHANISM IN THE CONNECTOR FOR THAT PIN WAS BROKESDR CALA2013120293360Connector · unsecureAUTO FLIGHT 'RUDDER TRIM 1 FAULT' DISPLAYED ON UPPER ECAM SCREEN. PLACED RUDDER TRIM 1 ON M EL IAW MEL 2722A DF128. CAT STATUS DOWNGRADED TO AUTO LAND LIMITS CAT 3 SINGLE, AC OK TO CONTINUE. SECURED FAC NR 1 BENCH PLUG, CHECKED GOOD. RETURNED ACFT TO CAT 3SDR 2013FA0000471Wire Harness · detachedDURING PRE-FLIGHT, NOTED MOVEMENT OF AILERON YOKE, FROM LT TO RT, DID NOT FUNCTION FREELY OR CORRECTLY. AT THE NEUTRAL POSITION, ROTATION OF YOKE TO THE RT WAS NOT POSSIBLE AND ACFT DEEMED UNAIRWORTHY AND GROUNDED. ELECTRICAL CONNECTOR TO THE AUTOPILOT COMSDR FDEA201304020714Terminal · looseDURING CRUISE AT FL 350 AUTOPILOT AND AUTO THROTTLES DISCONNECTED, EICAS SHOWED MACH/SPEED TRIM, RT FWD FUEL PUMP, LT AFT FUEL PUMP, AND EQPT COOLING CAUTION LIGHTS. LT AFT FUEL PUMP CB POPPED ALONG WITH THE EQPT COOLING CB. ADDITIONALLY THERE WAS A LOUD CLICSDR FDEA201303010484Wire · failedREPEAT WRITE UP: UNCOMMANDED YAW DURING LOW SPEED AND HIGH SPEED FLIGHT. DIRECTED BY GOC TO RETURN TO DEPARTURE. R & R YAW DAMPER LOWER RUDDER WIRE BUNDLE W325 IAW SWPM 20-10-11 20-10-11.SDR HNAA2013011400007Connector · contaminatedAUTOFEATHER ARM LIGHT WILL NOT EXTINGUISH WHEN AUTOFEATHER IS SELECTED OFF. FOUND AUTOFEATHER STATIC TESTING PROPERLY. FOUND NR 2 TSCU CONNECTOR PLUG OIL SOAKED. CLEANED AND RESEATED CONNECTOR PLUGS. OPS CHECKED GOOD AT THIS TIME.SDR CA121203004Wire · broken(CAN) BROKEN WIRE FOUND IN AFT PITCH BRIDLE CABLE IN AREA OF CABLE CLAMP DURING SCHEDULED MAINTENANCE.
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