JASC 2731
Service difficulty reports · 1,297
Reports filed under 2731 · Elevator Tab Control System, 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 = '2731' 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 = '2731' 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 UIEA2023011500043Pca · out of adjustRH HORIZONTAL STABILIZER, INBOARD PCA FREEPLAY OUT LIMIT.(<P>PCA WAS REPLACED AND THE PCA INPUT ROD WAS ADJUSTED PER AMM 27-31-05-424-027 REQUIREMENTS)SDR AALA202301231567Relay · faultyAIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPSDR AALA202301232322Relay · faultedAIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPSDR AALA202301235481Motor · faultedAIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPSDR AALA202301238165Relay · faultedAIRCRAFT WAS GROUNDED: DURING CLIMB OUT MACH ELECTRIC STAB TRIM FAILED. AUTOPILOT TRIM OK. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM FLAPS RELAY R1192 PER SWPM 20-81-16. ACCOMPLISHED SATISFACTORY STABILIZER TRIM SDR 2022FA0000699Control Cable · low tensionELEVATOR TRIM CONTROL SURFACE ARE NOT CONNECTED, THERE IS NO TENSION IN THE CABLES. WITH THE ELEVATOR LEADING EDGE DEFAULT POSITION IS POINTED DOWN.SDR YQSA2022091900001None · bindingAFTER TAKEOFF OUT OF KBNA AND ON CLIMBOUT THE CREW NOTED THE ELEVATOR TRIM WAS STUCK AND COULDN'T BE OPERATED NOSE UP OR NOSE DOWN BY HAND OR BY USING ELECTRIC TRIM. CREW LANDED BACK AT KBNA AND FOUND ELEVATOR TRIM STILL INOPERABLE AFTER ENGINES WERE SHUT DOWNSDR UIEA2022090900951None · noneRIGHT ELEVATOR ACTUATOR INPUT ROD, RIGHT CENTER OUT OF LIMITS (COLLAPSING DIRECTIONS 65.5LBS/0.845")(<P>RIGHT ELEVATOR ACTUATOR INPUT ROD WAS REPLACED 27-31-07-424-016 REV136. OPS CHECK GOOD</P>)SDR 3KUA20220808001Actuator · bindingN350WC DECLARED AN EMERGENCY DUE TO THE ELEVATOR TRIM MALFUNCTIONING AS THE CREW WAS PREPARING THEIR DESCENT INTO DESTINATION AIRPORT, KRIC. THE CREW FOLLOWED THE EMERGENCY CHECKLIST AND LANDED WITH NOT PROBLEMS. WHEN MAINTENANCE CHECKED TRIM SYSTEM, THEY FOSDR UIEA2022070100706Hydraulic Line · leakingAREA AFT OF PRESS BULK HEAD TO BS 1725.5, ELEVATOR FEEL COMPUTER, EVIDENCE OF LEAK ON LOWER HYD TUBES. (BTW STA 1702.2 AND 1725.5, LH SIDE).(THE ELEVATOR FEEL COMPUTER WAS INSTALLED CORRECTLY AS PER AMM 27-31-19-424-015, REV 136</P>)SDR CALA2022062901600Spring · damagedLOG PAGE CREATED FOR SDR RECORD OF LT ELEVATOR TAB MECHANISM SPRING FOUND BROKEN DURING GV AND FOUND DAMAGE ON MECHANISM FROM BROKEN SPRING.SDR QXEA2022062300228Autopilot Sys · inoperativeAFTER TAKEOFF, RECEIVED AP FAIL AND PITCH CONTROL DISC EICAS MESSAGES. A/C THEN BEGAN UNCOMMANDED ROLL TO THE RIGHT. FLIGHT CONTROLS REQUIRED CONTINUOUS LEFT INPUT FOR LEVEL FLIGHT. CONDITION CONTINUED THROUGH TOUCHDOWN.
DIVERTED. EMERGENCY DECLARED. LANDINGSDR VNAA202206191111Elevator System · out of adjustDURING CLIMBOUT OUT OF SGF THE ELEVATOR SPLIT CAUTION MSG OCCURRED AT APPROXIMATELY 9,000 TO 10,000 FT. THE CREW RAN THE QRH AND HELD TO BURN FUEL BEFORE LANDING FOR STRUCTURAL CONCERNS. THE A/C DID NOT LAND OVERWEIGHT AND THE PAX DID NOT BRACE FOR LANDING. EMSDR P5CA2022051800128Actuator · out of limitsLH ELEVATOR INNER ACTUATOR OUT OF LIMITS IAW TASK THE ELEVATOR SURFACE FREEPLAY(REMOVED AND REPLACED ACTUATOR PER AMM 27-31-05-424-027)SDR 2022F00152None · noneWHILE ON-ROUTE TO KMDT WE RECEIVED AN AP PITCH MISTRIM ANNUNCIATION AND ASSOCIATED MASTER CAUTION. IN ACCORDANCE WITH THE CHECKLIST, AUTOPILOT WAS DISCONNECTED AND THE PITCH TRIM WAS COMMANDED MANUALLY NOSE-DOWN. THE TRIM WHEEL HOWEVER FAILED TO ROTATE VIA THESDR 2022F00148None · openON SUNDAY, MARCH 20TH, TMB420, A HONDA JET (HA-420) OPERATED BY FLYDREAMS, LLC (DBA VOLATO) ACC 4F1A515O DEPARTED KAPF (NAPLES, FL) FOR KEYW (KEY WEST, FL). UPON DEPARTURE THE AIRCRAFT EXPERIENCED A CONTROLLABILITY ISSUE. SPECIFICALLY, THE TRIM SYSTEM FOR AISDR HNAA2022040400152None · noneE909326 - RH ELEVATOR SERVO TAB TRAILING EDGE DOES NO ALIGN WITH THE ELEVATOR TRAILING EDGE....COMPLETE: RAR RH ELEVATOR UPPER AND LOWER AFT CENTER SKIN PANELS IAW PIEDMONT EO1-27-22-0064. RH ELEVATOR TRAILING EDGE NOW PROPERLY ALIGNS WITH THE SERVO TAB TRAILISDR AALA202202164259Actuator · faultedAIRCRAFT WAS GROUNDED: FLIGHT CONTROL ELAC 1 AND 2 ECAM FAULT DURING CRUISE. FLIGHT DECLARED AN EMERGENCY, LANDING SAFELY AT BOS. REPLACED TRIMMABLE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR PER AMM 27-44-57. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR VNAA202201311111Actuator · misriggedEMERGENCY DECLARED GOING INTO JAX DUE TO A REPEAT PITCH FAIL MESSAGE. TRUCKS WERE ROLLED AND FLIGHT LANDED SAFELY. MX HAS BEEN ADVISED. / INTERROGATED MDC FOUND B1 007975. TROUBLESHOT IAW CRJ 900 FIM 27-31-23-810-802-A01. FOUND ACTUATOR TO BE OUT OF RIG. REMOSDR AALA202201268580Switch · faultedAIRCRAFT WAS GROUNDED: ELEVATOR TRIM SWITCHES ON BOTH YOKES INOPERATIVE, MANUAL ELEVATOR TRIM UNAFFECTED; FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD. ACCOMPLISHED LOGIC RESET OF STAB TRIM MOTOR IAW FIM 27-41-00, OPS CHECK GOOD.SDR CALA2022010500023Elevator · puncturedRIGHT ELEVATOR HAS A PUNCTURE FROM HAIL 8 1/2 INCHES OUT FROM INBOARD END AND 16 INCHES FROM TRAILING EDGE DIAMETER ABOUT .75 REF SRM 55-20-01-1A-1 FIGURE 102 , NO DELAMINATION NOTED OUTSIDE DAMAGE, SEALED WITH SPEED TAPE REVIEWED, LOCKED FOR MAINTENANCE FERRYSDR JJBA202201020002Control Unit · inoperativePITCH TRIM BACKUP INOPERATIVE ON EICAS IN FLIGHT. R&R HSCU. ADJUSTMENT TEST CARRIED OUT. REPLACED HAS. OPS CHECK SAT.SDR CALA2021121402367Panel · missingPDA 3 FOUND PANEL ON RIGHT HAND ELEV MISSING NO DAMAGE NOTED IN AREA TOCS LOG CREATED FOR THIS PDA 3 ITEM. LAS MM INSTALLED PANEL REF AMM 55-10-11-400 ON LOG PAGE 7620695. NO FUTHER DEFECTS NOTED. ARMENTA TOMC 14DEC21SDR N6WA2021111201Water System · leakingPITCH FEEL FAULT CAUTION MSG// INB GROUND SPOILER/IB SPOILERON CAUTION MSG. INSPECTED AND FOUND WATER IN AVIONICS BAY, REMOVED WATER AND DRIED AREA, SWAPPED SSCU1 AND 2 IAW CRJ 550 AMM 27-61-05, OPS CHECK GOOD AND ALL MESSAGES CLEAREDSDR 2021FA0000411None · bindsDISCRPANCY:PILOT NOTIFIED MAINTENANCE AND OPERATIONS IN FLIGHT THE #1 & # 2 FLIGHT GUIDANCE COMPUTER IS INTERMITTENT, AND THE PITCH TRIM DISENGAGED. CORRECTIVE ACTION:GULFSTREAM MAINTENANCE FOUND A PITCH TRIM SERVO DRUM AT FAULT. THE PITCH TRIM SERVO DRUM AND SDR J7SA2021112200302Mount · crackedUNCOMMANDED PITCH TRIM DOWN DURING FLIGHT. FOUND ELEVATOR TRIM SERVO MOUNTING BRACKET CRACKED. REMOVED CRACKED BRACKET; LOCATED, DRILLED, AND INSTALLED NEW ELEVATOR TRIM SERVO MOUNTING BRACKET IAW GULFSTREAM GV SRM 51-42-00. P/N 1159C50423-129.SDR VNAA202110171111Warning Message · false activationON FINAL APPROACH TO RWY 35 IN PHL THE CREW RECEIVED A PITCH FEEL FAULT MESSAGE. FOLLOW QRH AND DECLARE EMERGENCY AND LANDED WITHOUT ISSUE. F/A'S DID NOT HAVE PAX BRACE. AAN-PITCH FEEL FAULT (C) MSG IN FLIGHT / PERFORMED OPERATIONAL TEST OF THE PITCH FEEL SYSTSDR CALA2021092201635Pitot Head · noneFEEL DIFF PRESS LITE ON ROTATE CLIMB OUT FOUND BUILDUP AT INLET OF RT ELEV PITOT PROBE. CLEANED AND FLUSHED ELEV FEEL PITOT PROBES PER AMM 27-31-17. PERFORMED PRESSURIZATION CHK PER SAME. PRESS READS SAME AND INDICATIONS NORMAL. OK TO CONTINUE.SDR ABXA202194088Warning Message · false activationARRIVED WITH ELEV FEEL EICAS STATUS MESSAGE.PERFORMED FIM 27-31 F/T 806 - MSG CLEARED SYSTEM OK. AFTER BLOCK OUT, AIRCRAFT RETURNED TO BLOCKS WITH AIL LOCKOUT AND RUDDER RATIO EICAS MESSAGES AND THE RIGHT ENGINE #1 IGNITION SYSTEM FAILED. AICRAFT GROUNDED BY MSDR F27A2021090200002Pointer · bindingFLIGHT CREW REPORTED THAT THE PITCH TRIM WAS BINDING AND COULD NOT MOVE THE TRIM OUT OF THE NOSE UP CONFIGURATION, CREW DECLARED EMERGENCY AND LANDED AIRCRAFT AT KIND WITH NO DAMAGE/INJURY TO AIRCRAFT OR PERSONS. UPON INSPECTION OF TRIM SYSTEM FOUND PITCH TRIMSDR IPXA2021060970321Shutoff Valve · out of toleranceINSPECTION TYPE:NA**ATB-NO EMERG DECL'D-NO EQUIP USED-LANDED UNEVENTFULLY**STAB OUT OF TRIM LEVEL 2 ALERT UPON AUTOPILOT ENGAGEMENT. RAN CHECKLIST AND CAUTION REMAINED. A/P 2 WILL STAY ENGAGED. ATTEMPTED AP 1 ENGAGEMENT WHICH RESULTS IN IMMEDIATE DISCONNECT WISDR 2021FA0000156Control Cable · brokenLEFT ELEVATOR TRIM CABLE FAILED UNDER SAFETY WIRE WRAP. SAFETY WIRE WAS HOLDING SYSTEM TOGETHER. FOUND DURING ANNUAL INSPECTION. SAME FAILURE TYPE AS ADDRESSED IN AD 2019-23-10. I HAVE PICTURES BUT SEE HOW TO ATTACH TO FORM.SDR K11A2021051900049Trim Tab · looseABNORMAL VIBRATION ON TAKEOFFSDR AALA202105129003Motor · failedAIRCRAFT WAS GROUNDED: STAB OUT OF TRIM ILLUMINATED AT LEVEL OFF FL 300. FOLLOWED QRH PROCEDURES AUTOPILOT AND AUTO THROTTLE DISENGAGED AIRCRAFT TRIMMED NORMALLY. RETURNED TO DFW. REPLACED STAB TRIM MOTOR PER AMM 27-41-71.SDR N6WA2021051001Motor · faultedSTAB TRIM RUNAWAY. R&R HORIZ STAB MOTOR #1 IAW CRJ AMM 27-42-03.SDR 2021FA0000042Rod · corrodedELEVATOR TRIM ROD, P/N - 71032-1 SHOULD HAVE SEALANT IN THE LOWER HOLE DOWN INSIDE THE CLEVIS WHERE IT IS WELDED TO THE TRIM ROD. IT APPEARS THAT THIS CLEVIS HAS A FEMALE THREADED HOLE WHICH WHEN WELDED TO THE ROD LEAVES ACCESS TO THE INSIDE OF THE TRIM ROD. ISDR 3EJA789/2/12/20Cable · misinstalledPITCH TRIM TRAVELS IN OPPOSITE DIRECTION. WHEN CB IS PULLED, MANUAL TRIM TRAVELS .. MOVES OPPOSITE DIRECTION ON POST FIT WITH AP ON, TRIM MOVES IN CORRECT DIRECTION.
CONFIRMED CREWS DISCREPANCY, RESEARCHSDR MTNA20210209001Indicator · faultedPITCH TRIM ASYMMETRY MASTER CAUTION IN FLIGHT. FOUND TRIM INDICATOR CIRCUIT BREAKER POPPED. INSPECTED AND CLEANED CANNON PLUGS FOR RIGHT AND LEFT ELEVATOR TRIM ACTUATOR. INSPECTED ASSOCIATED WIRING AND VARISTORS IN TAIL CONE FOR
CORROSION. REPLACED TRIM INDICSDR ASAA2021020534057Spring · brokenINCOMING FCF ITEM #24; ELEVATOR POWER OFF TEST FLIGHT REQUIRED 15 TURNS NOSE DOWN GROUNDED - YES. AFTER REMOVING THE LEFT ELEVATOR TAB MECHANISM ACCESS PANEL DISCOVERED THE FORWARD AND AFT INBOARD TAB MECHANISM SPRINGS BROKEN. THE AFT SPRING WAS HANGING FROM TSDR JJBA20201230032Switch · failedPITCH TRIM MAIN INOPERATIVE IN FLIGHT. REMOVED AND REPLACED FO YOKE PITCH TRIM SWITCH. OPERATIONS CHECK GOOD.SDR DXTA2020090904076Trim System · malfunctionedCLIMBING THROUGH 27,500 FT, THE PITCH TRIM ANNUNCIATOR ILLUMINATED ON BOTH PFDS. THE AUTOMATION WAS DISENGAGED. WE LEVELED AT FL 280. WE ATTEMPTED TO MOVE THE THE TRIM VIA THE YOKE SWITCH AND IT DID NOT RESPOND. WE WERE ABLE TO MANIPULATE THE MANUAL TRIM WSDR QXEA2020082700264Control Unit · malfunctionedPITCH TRIM MASTER CAUTION AND AUTO TRIM FAIL ON FMA DURING CLIMBOUT . ELEVATOR TRIM INDICATOR SHOWED FULL NOSE UP. NO CIRCUIT BREAKERS POPPED. REMOVED FROM SERVICE. FOUND FAULTS ON CDS IFC FAILURE X2, FCECU FAILURE 67, 63, E7, AND E3 REF Q400 FIM 27-30-00-810-SDR 2020FA0000312Actuator · wornDURING GROUND GROUND RUN/ PRE FLIGHT, IT WAS DISCOVERED THE RT ELEVATOR TRIM WAS VERY DIFFICULT TO OPERATE. UPON INVESTIGATION, IT WAS DISCOVERED THE RT ELEVATOR TRIM ACTUATOR HAD INTERNAL WEAR THAT CREATED SIGNIFICANT DAMAGE TO THE ACTUATOR AND OPERATION.SDR CALA2020062001019Motor · inoperativeELECTRIC STAB TRIM FAILED AFTER T/O RAN ELECT STAB TRIM INOP CHE CKLST RETURNED GDL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE REPLACE THE ELECTRIC STAB TRIM MOTOR PER AMM 27-41-71-400 -801 REPLACED STAB TRIM MOTOR REF AMM 27-41-71-400-801. OPS CHECKSSDR HYIA20200415001Actuator · faultyDURING A FUNCTIONAL CHECK FLIGHT FOR AN UNRELATED ITEM AND WHILE PERFORMING MANEUVERS INCLUDING 30 DEGREE TURNS IN CLIMB AND DESCENT, THE ELEVATOR TRIM POSITION MOVES INDEPENDENTLY WITHOUT INPUT FROM CREW; TENDS TO MOVE 3/4 TO FULL NOSE DOWN POSITION. THE AIRSDR HYIA20200407002Actuator · faultyDURING A TRAINING FLIGHT WHILE PRACTICING MANEUVERS, THE ELEVATOR TRIM POSITION MOVES INDEPENDENTLY WITHOUT INPUT FROM CREW; TENDS TO MOVE TO FULL NOSE DOWN POSITION. THE AIRCRAFT WAS CONTROLLABLE AND LANDED SAFELY. THE AIRFRAME OEM INSTRUCTED THE REPLACEMENSDR HYIA20200402001Actuator · faultyDURING A TRAINING FLIGHT WHILE PRACTICING STALL RECOVERY, THE ELEVATOR TRIM POSITION INDICATOR MOVED 'UNCOMMANDED' TO THE FULL NOSE DOWN POSITION AND THE WEIGHT OF CONTROLS CONFIRMED THE CORRECT POSITION OF TRIM INDICATOR. THE AIRCRAFT WAS CONTROLLABLE AND LASDR QXEA2020012700047Relay · malfunctionedPITCH TRIM CAUTION CAME ON 12K AND 250 KNOTS IN DESCENT ELEVATOR TRIM INDICATOR SHOWED FULL NU PITCH TRIM DID NOT WORK AUTO TRIM FAIL ALSO CAME ON THE PFD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED PITCH TRIM ACTUATORS IAW Q400 AMM TASK 27-32-06-000/4SDR QXEA2020012300041Control Unit · inoperative"ON DESCENT, GOT " PITCH TRIM" CAUTION. "AUTO TRIM FAIL" ON PFDS TRIM INDICATOR IN FULL NU POSITION. PITCH TRIM DID NOT WORK." REMOVED FROM SERVICE. "DID RETRIEVAL OF DATA FROM CDS. PERFORMED OPERATIONAL CHECK OF ELEVATOR PITCH TRIM. PITCH TRIM CAUTION AND AUTSDR 9PER202011700003Relay · faultedDURING CRUISE THE ELEVATOR TRIM WENT IN TO A FULL NOSE TRAVEL ATTITUDE. TROUBLESHOOTING FOUND THE TRIM RELAY FAILED CAUSING THE ELEVATOR TRIM TO GO IN TO A RUNAWAY ACTION.
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