JASC 2742
Service difficulty reports · 610
Reports filed under 2742 · Stabilizer Actuator, 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 = '2742' 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 = '2742' 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 WH6A20261021999LRActuator · failedON MAY 18 2026, N999LR HAD A FLIGHT CONTROL MALFUNCTION HORIZOTAL STABILIZER ACTUATOR (HSTA) WHICH LED TO THE CREW DECLARING AN EMERGENCY. THE FLIGHT DEPARTED KHPN ENROUTE TO KBCT. DURING THE APPROACH INTO KBCT WHILE CONFIGURING FOR LANDING FLIGHT CREW SEES ANSDR CALA2026030314244Actuator · faultedHORIZONTAL STAB VISUAL INSPECTION, FOUND HAND ETCHED MARKING AT TOP OF JACKSCEW, FOUND ADDITONAL ETCHING ON SECOND THREAD DOWN, FOUND SCRATCH ON CREST OF JACKSCREW THREAD NEAR TOP OF JACKSCREW. DAMAGE FROM ETCHING & BALLSCREW FOUND PAINTED WITH PRIMER. STSDR CALA2025052905056Control Servo · faultedTEST FLIGHT DISCREPANCY. . RSP3 ON RIGHT SIDE FLOATED WITH BLUE HYD DEPRESSURIZED. REFLY R EQD. REMOVED AND REPLACED RH #3 SPOILER ACTUATOR IAW A320 AMM 27-64-5 1-400-004-A, 27-64-51-000-004-A OP & ADJUSTMENT CHK GOOD. ACMP B Y V914957 INSP BY V925611ROTABLE PSDR DALA2025021001018Ballnut · leaking(LOG 0800558) HORIZONTAL STABILIZER TRIM ACTUATOR BALLNUT HAS RAISED/LEAKING RETURN TUBE. HORIZONTAL STABILIZER TRIM ACTUATOR REPLACED PRIOR TO FLIGHT IN ACCORDANCE WITH AA 2740-01077 SECTION 3 ON WORK CARD 2740-01077-0301 FORECAST NUMBER 36-0527-8-0080.SDR DALA2024102110231Actuator · making metal(LOG 0616130) FOUND METALLIC DEBIS IN THE GREASE OF THE BALL NUT. (REF) AA 2740-0177-0101. HORIZONTAL STABILIZER TRIM ACTUATOR REQUIRES REPLACEMENT PRIOR TO FLIGHT I.A.W. AA 2740-0177. REMOVED AND REPLACED HORIZ STAB ACTUATOR TO BE ACCOMPLISHED ON CC 2740-0177SDR DALA2024051405170Jackscrew · nicked-AD- A NICK WAS FOUND ON THREAD OF THE ACME SCREW AT THE HORIZONTAL STAB. SUMMARY OF NRC 00485: HORIZONTAL STABILIZER ACTUATOR JACKSCREW ASSY WAS REPLACED FOR SERVICEABLE ACTUATOR JACKSCREW. WAS INSTALLED PER B717 AMM 27-41-04 AND TESTED OK. ALSO, TRIM GEARBOXSDR DALA2023101908621Unknown · unknownSHIP 3129 CORROSION ELEVATOR ACTUATOR CONNECTOR O/B SIDE ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SERVO CONTROL ACTUATOR ELEVATOR CONNECTOR O/B POSITION 34CE3-B ON LH HORIZONTAL STABILIZER AS PER A320 FAM ESPM 20-48-21 AND ESPM 20-44-11 AND AWMSDR DALA2023101908620Unknown · unknownSHIP 3129 CORROSION SERVO CONTROL ACTUATOR ELEVATOR CONNECTOR I/B POSITION ON RH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED SERVO CONTROL ACTUATOR ELEVATOR CONNECTOR I/B POSITION 34CE2-B AND 34CE2-A ON RH HORIZONTAL STABILIZER AS PER A320 FAM ESSDR DALA2023101908619Unknown · unknownSHIP 3129 CORROSION SERVO CONTROL ACTUATOR ELEVATOR CONNECTOR O/B POSITION ON RH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED SERVO CONTROL ACTUATOR ELEVATOR CONNECTOR O/B POSITION 34CE4-C AND 34CE4-B ON RH HORIZONTAL STABILIZER AS PER A320 FAM ESSDR DALA2023080706382Unknown · unknown(LOG 2899657) HORIZONTAL STABILIZER BALLSCREW FITTING UPPER GIMBAL FWD ATTACHMENT NUT IS NOT ENGAGED IN COTTER PIN REF. AA 2740-01077, WORK CARD 2740-0107. INSTALLED ANOTHER WASHER ON H/S BALLSCREW FITTING UPPER GIMBAL FWD ATTACHMENT NUT AND INSTALLED NEW PIN SDR AALA202304136836Motor · failedAIRCRAFT WAS GROUNDED: AFTER TAKEOFF THE STABILIZER TRIM TOTALLY FAILED WITH SPEED TRIM FAILED ANNUNCIATION. EMERGENCY DECLARED, FLIGHT RETURNED TO LGA LANDING SAFELY. MAINTENANCE REPLACED HORIZONTAL STABILIZER TRIM MOTOR PER AMM 27-41-71.SDR AALA202303272555Trim Motor · faultyAIRCRAFT WAS GROUNDED: AFTER TAKEOFF NO ELECTRIC TRIM WITH YOKE SWITCH. MANUAL TRIM WORKED NORMAL. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. MAINTENANCE REPLACED STABILIZER TRIM MOTOR PER AMM 27-41-71. ACCOMPLISHED SATISFACTORY OPERATIONAL CHESDR AALA202303017930Trim Motor · stuckAIRCRAFT WAS GROUNDED: ON CLIMB UNABLE TO TRIM STABILIZER WITH YOKE TRIM SWITCHES OR MANUALLY WITH TRIM WHEEL. PITCH TRIM WAS STUCK. FIGHT RETURNED TO DFW LANDING SAFELY. REMOVED AND REPLACED STAB TRIM MOTOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER SDR DALA2023012200465Bolt · damagedDURING INSPECTION, FOUND DAMAGE THREADS ON THE BOLT OF THE HORIZONAL STAB TRIM ACTUATOR SUPPORT PLATE. DAMAGE TRIM ACTUATOR WAS REMOVED. SAME SERVICEABLE STAB TRIM ACTUATOR WAS AS REINSTALLED IAW AMM 27-41-81. TESTED OK.SDR DALA2022123008498Jackscrew · corroded(LOG 2559400) DURING ACCOMPLISHMENT OD AD CARD 2740-01077-0101, FOUND LIGHT CORROSION AROUND THE THREADS OF THE HORIZONTAL STAB JACKSCREW. REMOVED AND REPLACED HORIZONTAL STABILIZER BALL SCREW ACTUATOR IAW AMDS 2740-01077-0301.SDR DALA2022120807922Bushing · gougedDURING REMOVAL OF HORIZONTAL STABILIZER TRIM ACTUATOR, GOUGES WERE FOUND ON RH INBDOARD BUSHING OF UPPER JACKSCREW FITTING AT AFT ACCESORIES COMPARTMENT. RH INBDOARD NEW BUSHING OF UPPER JACKSCREW FITTING AT AFT ACCESORIES COMPARTMENT WAS REPLACED PER SOPM 20-SDR 2022FA0000335None · failedPILOT REPORTED PTITCH TRIM FAILS INFLIGHT. MX REMOVED AND REPLACED FAILED PITCH TRIM ACTUATOR WITH OVERHAULED UNIT IAW TASK CARD 27.914 POST ACTION RIGGING AND TRIM TRAVEL CHECKS GOOD.SDR 9JLA2022071238675Actuator · failedTHE FLIGHT CREW REPORTED AN AMBER PITCH TRIM ANNUNCIATOR ILLUMINATED IN CRUISE FLIGHT WHILE TRIMMING. THE MAINTENANCE PROVIDER TROUBLESHOT AND DETERMINED A FAULT WITH THE STAB ACTUATOR WAS REMOVED AND REPLACED WITH AN AS REMOVED UNIT PER THE AMM. OPS CHECKS WESDR F3LA2022070500068Rudder · misriggedDISCREPANCY: REFERENCE LP 231897 ITEM 1; CLIMBING THROUGH FL300 MODERATE AIRFRAME VIBRATION @ MACH.79 SLOWED TO .7 AND THE VIBRATION WENT AWAY.
CORRECTIVE ACTION: C/W TSM05-50-00-810-801-A FOR AIRFRAME VIBRATION/ C/W TYPE (5) INSPECTION. PERFORMED ADJUSTMENT SDR DALA2022061004084Ball Joint · leaking(LOG 2268162) LARGE AMOUND OF GREASE IS PRESENT AROUND THE STABILIZER TRIM ACTUATOR DUE GREASE IS ESCAPING FROM BALL NUT PER AMDS 2740-01077-0101. HORIZONTAL STABILIZER TRIM ACTUATOR WAS REPLACED PER AMDS 2740-01077-0301 DUE TO A LARGE AMOUNT OF GREASE PRESENTSDR AALA202205105758Actuator · faultyAIRCRAFT WAS GROUNDED: DURING DESCENT INTO CLT, AUTOPILOT #2 DISCONNECTED; SOON AFTER, BOTH ELAC'S FAILED. DECLARED AN EMERGENCY AND LANDED SAFELY. TROUBLESHOT PER TSM 27-40-00-810-802-A. REPLACED #2 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34 (AALA20220SDR HALA2022042500142None · noneSHIP 378 WHILE WORKING W/C 2740-2101-HAL FOUND METAL PARTICLES AT THE BASE OF THE ROD SPHERE. CORRECTIVE ACTON: REMOVED AND REPLACED THS ACTUATOR PER AMDS 2740-4001. (8462634)SDR 9JLA2022042631165Actuator · defectiveTHE FLIGHT CREW REPORTED THAT UPON BATTERY POWER UP IMMEDIATE CLICKING NOISE HEARD FROM TAIL SECTION WHILE IN PRIMARY TRIM MODE. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE HORIZONTAL STAB PITCH TRIM ACTUATOR WAS DEFECTIVE. THE DEFECTIVE UNIT WASDR N6WA2022021402None · failedIB FLT SPOILER, IB SPOILERONS, PITCH FEEL, IB GND SPOILER, AND AP PITCH TRIM CAUTION MSGS. T/S THRU MDC B1 CODE 007992 FOUND SSCU 1 FAILED. RAR #1 SSSCU IAW CRJ-AMM-27-61-05. OPS CHECKS GOOD.. NO FURTHER DEFECTS OR MSGS NOTED. ALSO PERFORMED SPOST 1 AND SPOST2SDR 9JLA2021120831806Actuator · defectiveTHE FLIGHT CREW REPORTED THAT THE HORIZONTAL STABILIZER TRIM FAILED IN FLIGHT, THE FLIGHT CREW ELECTED TO DIVERT FLIGHT AND LAND TO INVESTIGATE THE FAULT. THE APPROACH AND LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE HORIZONTALSDR 2022F00050Stabilizer · failedWHILE CRUISING AT 38,000 FT. WE HAD A MACH TRIM FAIL INDICATION. AUTO PILOT KICKED OFF AND AIRCRAFT STARTED TO PITCH UP. WE NO TRIM CONTROL AND TOOK BOTH PILOTS TO PUSH THE YOKE FORWARD TO KEEP AIRPLANE LEVEL.SDR VNAA202111231111Control Unit · unserviceableENROUTE TO CLT THE CREW RECEIVED A STAB TRIM/MACH TRIM FAIL MESSAGES. THE CREW RAN THE QRH AND THE RESET WAS UNSUCCESSFUL. THEY DECLARED EMERGENCY AND WERE CLEARED DIRECT TO CLT. THEY LANDED AND TAXIED TO THE GATE WITHOUT FURTHER ISSUE. NO FURTHER INFORMATION.SDR AALA202110200390Motor · leakingAIRCRAFT GROUNDED: BURNING ODOR AFTER T/O, SMELLED LIKE OVEN, BUT NONE WERE ON. LASTED 3-5 MINS. F/AS IN AFT GALLEY SAID SMELL VERY STRONG, NOT AS MUCH IN FWD GALLEY. F/AS REPORTED THAT AFT CHILLER WAS ON DURING TAKEOFF BUT WAS NOTED TO BE OFF AFTER EVENT. NOSDR AALA202110200960Motor · leakingAIRCRAFT GROUNDED: BURNING ODOR AFTER T/O, SMELLED LIKE OVEN, BUT NONE WERE ON. LASTED 3-5 MINS. F/AS IN AFT GALLEY SAID SMELL VERY STRONG, NOT AS MUCH IN FWD GALLEY. F/AS REPORTED THAT AFT CHILLER WAS ON DURING TAKEOFF BUT WAS NOTED TO BE OFF AFTER EVENT. NOSDR JIKA2021072801Actuator · inoperativeSHORTLY AFTER TAKEOFF FROM KSTT, PITCH TRIM FAILED IN TAKEOFF POSITION. THE PILOT THEN FOLLOWED A QRH BUT UNABLE TO RESET THE HORIZONTAL STABILIZER CONTROL SYSTEM. THE PILOT REQUESTED RETURNING TO KSTT AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN KSSDR SCNA20210125003Actuator · faultedDURING CRUISE STAB OUT OF TRIM ILLUMINATED UNABLE TO MOVE TRIM MANUALLY. DIVERTED TO MEM. EMERGENCY DECLARED. FLIGHT LANDED SAFELY. REMOVED AND REPLACED STAB TRIM ACTUATOR.SDR 3WTR20201211Actuator · bindingAIRCRAFT HAD HISTORY OF INTERMITTENT PITCH TRIM FAULT ON ECAS. TROUBLESHOT AND FOUND HORIZONTAL STABILIZER ACTUATOR P/N 66274010000-00, S/N B0293 WOULD OCCASIONALLY BIND AND CREATE A LOUD NOISE. DEFECTIVE HORIZONTAL STABILIZER ACTUATOR REPLACED WITH AN OVERHSDR F3LA202007300032Actuator · leakingTHS ACTUATOR LEAKING AND SIGHT GLASS READS MIN. REMOVED AND REPLACED ACTUATOR PER A320 AMM 27-44-51-000-001-A & 27-44-51-400-001-A. OPS & LEAK CHECK GOOD.SDR HYIA20200716001Actuator · excess playCREW REPORTED EXCESSIVE VIBRATION IN FLIGHT DURING CRUISE CONFIGURATION. THE VIBRATION WAS FELT IN YOKE, RUDDER PEDALS, AND SEAT MOUNTS. BOTH SIDES OF HORIZONTAL STABILIZER WERE OBSERVED TO BE OSCILLATING UP AND DOWN AT OUTBOARD SECTIONS. THE FLIGHT CONTINUSDR FDEA2020061621211Trim Motor · dirtyRECEIVED "HYD 3 ELEV OFF" IN CLIMB. FOUND NR 3 SYSTEM DECREASING. RECEIVED "HYD 3 OFF" AND "HYD 3 FAIL" IN TURN AS LEVEL DECREASED TO 0. COMPLIED WITH QRH AND LANDED UNEVENTFULLY. REMOVED RT SIDE HORIZONTAL STABILIZER TRIM MOTOR IN REFERENCE AMM 27-43-30-SDR FDEA2020060321107Sprocket · damagedFOUND RT THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING, FOUND DURING HORZ STAB LUBE.SDR AALA202005299008Trim Motor · defectiveAIRCRAFT WAS NOT GROUNDED: DURING ILS 35R STAB OUT OF TRIM LIGHT CAME ON JET DID NOT INTERCEPT GS AND TRIM WHEEL WAS NOT MOVING WITH AUTOPILOT ON, DISCONNECTED AUTOPILOT AND A VERY SHARP PITCH UP FOLLOWED, BUT WAS ABLE TO TRIM WITH YOKE SWITCH, LANDED NORMALSDR FDEA2020050410890Trim Motor · cracked2:00 INTO FLT, FLT 370 HYD 3 ELEV OFF ALER. HYD SYS 3 WAS AT 3.9 OVER NEXT FIVE MINUTES DROPPED TO 3.6. DEPRESSURIZED SYS UNTIL LANDING. AFTER LANDING QTY WAS DOWN TO 1.0 FOUND HYDRAULIC FLUID MISTING IN TAIL AREA AROUND HORIZONTAL STABILIZER TRIM MOTORSSDR SWIA2020041350118Trim Switch · failedUPON TAKEOFF, PLANE CONTINUED TO PITCH UP. WHILE AP ON PLANE CONTINUED TO PITCH HIGH WITH AIRSPEED FROZEN TO LOWER NUMBERS. MANUAL SPEED TO RETRACT FLAPS- PLANE CONTINUED TO PITCH HIGH- FOLLOWED MEMORY ITEMS FOR SUSPECTED PITCH TRIM. DISCONNECTED ALL AND HAND SDR CALA2020032100660Trim Motor · malfunctionedSTAB TRIB RUNAWAY WHILE HANDFLYING FLAPS 0 SPEED TRIM FAIL LIGHT BOTH TRIMS MANUEL DISCNT CREW REPORTS THAT INITIALLY AFTER DEPARTURE WITH FLAPS NOT UP, THE PILOT FLYING WAS TRIMMING NOSE DOWN AND WHEN HE RELEASED THE TRIM. THE SPEED TRIM FAIL LIGHT WAS ON THESDR DALA2019110406395Brake · malfunctionedDESCENDING THRU FL240 STAB TRIM FAIL EICAS MESSAGE. FAULT CODES 2741F0013, 2741F0013, 2741F0036 AND 274F0037 IN FAULT MSG SUMMARY. SUSPECT AFT 1 REU OR HSTA MOTOR BRAKE. T/S PER EFIM REU CHECKS GOOD. FOUND HSTA BRAKE TO FAIL STATIC TORQUE - FUNCTIONAL TEST. RESDR O2GA2019111651101Trim Motor · faultyDURING DESCENT FROM FL410 TO FL310 THE CREW RECEIVED A PITCH TRIM AMBER ANNUNCIATION ON THE PFD'S AT AROUND FL320. AUTOPILOT WAS DISCONNECTED. MANUAL AND ELECTRIC PITCH TRIM WAS UNRESPONSIVE. EMERGENCY WAS DECLARED AND CHECKLIST FOLLOWED. AS THE AIRCRAFT DESCESDR RAIA201909230002Control Unit · inoperativePITCH TRIM MAIN INOP FOLLOWED BY PITCH TRIM BACKUP INOP. RETURNED FROM FLIGHT AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. R&R HSCU AND MAIN PITCH TRIM CUTOUT SWITCH. OPS CHECK GOOD.SDR ESMR2019092601Actuator · defectivePILOT ABORTED TAKEOFF DUE TO ABNORMAL PITCH CONTROL PRESSURE NEEDED TO ROTATE / TAKEOFF. THE LT MAIN WHEEL / TIRE ASSEMBLY WAS LOCKED UP IN THE PROCESS OF STOPPING THE AIRCRAFT WITH THE BRAKES. THE ENSUING 2100 + FOOT SKID DESTROYED THE TIRE, AND SEVERELY DAMASDR AALA201909179007Trim Motor · failedAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO ABQ ON ACCOUNT OF STABILIZER ELECTRIC TRIM INOPERATIVE. AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED HORIZONTAL STABILIZER TRIM MOTOR IAW AMM 27-41-71 AND ACCOMPLISHED FUNCTIONAL TEST, SYSTEM CHECKS NORMAL.SDR ASAA2019091330699Trim Motor · failedAFTER DEPARTURE ELECTRIC TRIM INOP ON BOTH CONTROL COLUMNS. ENGAGED AUTOPILOT PER QRH & STAB OUT OF TRIM LIGHT ILLUMINATED. GROUNDED - YES. AIR TURNBACK. DIVERSION TIME 51 MINUTES - VERIFIED DEFECT, ACCOMPLISHED FIM 27-41 TASK 804 VERIFIED 115VAC ON D700 PINS SDR SIMA20190912001Actuator · failedPTRIM MAIN INOP "TRANSFERRED TO NRWC 698-ORD-04545". WLS 1 HEAT FAIL. C/A-REMOVED AND REPLACED HORIZONTAL-STABILIZER ACTUATOR IAW AMM 27-40-02 PERFORMED ELECTRICAL ZERO POSITION OF THE HORIZONTAL STABILIZER IAW AMM 27-40-02. OPS CHECK GOOD. PERFORMED OPERATIONSDR SIMA20190903001Actuator · failedPITCH FEEL CAUTION MSG IN FLIGHT. QRH COMPLIED WITH. EMERGENCY DECLARED. C/A-REMOVED AND REPLACED LINEAR PITCH TRIM ACTUATOR IAW AMM 27-31-23 OPS CHECK GOOD.SDR YENA201909020500Actuator · failedFLT 2824, MEX-MCO. WHILE ACCOMP T.C A32-027-49-00-710-00 ITEM 7 STEP 1 THE ELAC 2 PITCH FAULT MESSAGE DID NOT COME ON AN DTHE THS ACTUATOR DOES NOT COME TO A COMPLETE STOP. PER ENGINEERING REQUEST ACCOMPLISH TASK 27-44-00-710-001 A OPS TEST OF JAMMING PROTECTISDR CALA2019072401235Trim Motor · inoperativeNO ELECTRIC OR AP STAB TRIM AFTER TAKE OFF REPLACED STAB TRIM MOTOR IAW AMM27-41-71-000-801 AND STAB INTERLOCK RELAY PER AMM 27-41-98-000-801. OPS CHKD OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1025506 SN OFF 3342 MOTOR, STAB, HO OFF 29-2741-9-0011 3342
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