JASC 2741
Service difficulty reports · 889
Reports filed under 2741 · Stabilizer Position Indicating, 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 = '2741' 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 = '2741' 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 CALA2022112103189Trim Motor · failedSTABILIZER FAILS TO TRIM NOSE UP AND NOSE DOWN AFTER DEPARTURE SPEED TRIM DO NOT ARM LIGHT CAME ON.STAB TRIM F AILUR E.SMOOTH 153.5 OVRWT LDG PERFORMED FIM TASK PER FIM 27-32 TASK 801 NO HELP STILL NO STAB TRIM MANUAL OR ELECTRIC. ALSO PERFORMED FIM TASK 27-4SDR HNAA2022111600306Module · faultedPITCH TRIM MAIN INOP EICAS MESSAGE DISPLAYED ON T/O. R AND R PITCH TRIM MODULE ASSY AS REQUIRED OPS CHECK GOOD ACFT OK FOR SERVICESDR ABXA20221028120Control Module · faultyDURING TAXI OUT STAB TRIM CAUTION MSG AND STAB TRIM STATUS MSG CAME ON. AIRCRAFT BACK TO BLOCK AND MESSAGES DISAPPEARED AFTER LEFT ENGINE WAS SHUTDOWN. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE PERF MCDP TEST 65 TEST PASSED. PERF MCDP 30/40 FAULT RETURNEDSDR CALA2022093002583Stabilizer · noneSTAB OUT OF TRIM LIGH ILLUMINATED RESET STAB TRIM CBS P6-2 B10, D10, AND P18-1 C2. PERFORMED LAMD VERIFY CHECK PER AMM22-11-00. ACFT IS FULL CAT CAPABLE. OPERATION NORMAL. OK TO CONTINUE PER TOMC.SDR SWIA202266462None · failedAFTER TAKEOFF DURING NORMAL TRIM OPERATION, THE TRIM CLACKER SOUNDED. AIRCRAFT WAS SPEEDING UP THROUGH ABOUT 190 KNOTS. FLIGHT DIRECTOR WAS ON IN SPEED MODE AND NAV MODE WITH AUTOPILOT DISENGAGED. CAPTAIN MOVED TRIM SWITCH BOTH DIRECTION AND TRIM CONTINUED MOVSDR CALA2022090202236None · noneSTAB OUT OF TRIM MSG DIS PLAYED. UNABLE TO USE EL EC TRIM NOSE U P OR OVERRIDE. PILOT STATED STAB OUT OF TRIM LIGHT EXTINGUISHED WHEN ELECTRIC DFCS BITE SHOWS NO FAULTS ON CURRENT LEG. LEG 02 SHOWS FAULTS, CUTOUT SWITCHES ACTIVATED. WAS ABLE TO TRIM MANUALLY.SDR ABXA2022082985Switch · stickingDURING T.O. ROLL, AIRSPEED ,80KTS. UNSCHEDULED STAB TRIM EICAS/ MASTER CAUTION. ABORTED TAKE-OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENACE. MAINTENANCE REMOVED + REPLACED ALT STAB TRIM SWITCH ASSY PER B767 AMM 27-41-03 OPS NORMAL NO DEFECTS.AIRCRAFT RSDR SWIA202266319None · crackedHSTA UPPER FITTING CROSS TIE BRACKET FOUND CRACKED AND REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED AND REPLACED HASTA UPPER TIE ROD PER AMM 27-42-01SDR SWIA202266297None · gougedGOUGE DAMAGE FOUND TO THE HSTA LOWER FITTING P/N AV670-21125-007, ON THE LH SIDE INBOARD FLANGE FACE. DAMAGE MEASURES 0.375"L X 0.92"W X 0.0295" D, AND IS OUT OF THE ALLOWABLE DAMAGE LIMITATIONS OF SRM 55-31-27. (FILED CLOSED) GOUGE DAMAGE FOUND TO THE HSTSDR CALA2022080801997None · faultyMAIN TRIM ON BOTH COLUMNS WOULD TRIM NOSE UP BUT NOT NOSE DOWN REPLACED STAB. TRIM MOTOR ASSY. OPS OPERATIONAL STATUS. CHECKS ALL GOOD.SDR SWIA202266145None · fluctuatesD: THIS IS AN **ODI EVENT** - UPPER MGMT /SMOD APPROVAL REQ'D TO RTS THIS A/C AFTER CAMPS COMPLETE / C: MCI / SEE A/C MX LOG'S 956358 & 955518 (FLIGHT 5123 - FILED CLOSED) DID OPERATIONAL CHECK OF THE STAB-TRIM SYSTEM REFERENCING THE APPLICABLE STEPS INSDR SWIA202266379None · wornHORIZONTAL STABILIZER, LH FRAME 100 HINGE POINT, BUSHING BORE HAS WEAR/SCORING AND CORROSION (C-CHECK RO 8/29/2022) TEMPORARY REPAIR OF LH FRAME 100 HINGE POINT, BUSHING BORE BY REAMING, BUSHING FABRICATION AND INSTALLATION REF ETD 2022-170-021921 REVSDR CALA2022060801458Trim Motor · failedAS PRECAUTIONARY MEASURE DUE TO AIR RETURN REMOVE AND REPLACE HORIZONTAL STABILIZER TRIM MOTOR. MFG 10-62233-6 M&E 29-2741-9-0011 REPLACED STABALIZER TRIM MOTOR IAW AMM 27-41-71-400, READY FOR AFTER NEW MOTOR INSTALLED, SWITCHES ON BOTH CONTROL COLUMNS WILL OPSDR DALA2022052403607None · noneSHIP 3102 - CORROSION ON RECEPTACLES OF CONNECTORS 7542VC AND 7540VC IB FLAP RH WING. CORRECTIVE ACTION: REPLACED RECEPTACLES OF CONNECTORS 7542VC AND 7540VC IB FLAP RH WING AS PER A320 FAM ESPM 20-44-10.(2246152)SDR J7SA2022052000319Trim Switch · failedCAPTAIN SIDE TRIM SWITCH WILL NOT TRIM NOSE DOWN. REPLACED FAILED TRIM SWITCH IAW CL350 AMM 27-41-01. OPS TEST GOOD. PN OFF: 83452541 SN OFF: 01160 PN ON: 403-4300 SN ON: NSN. NOTE: BOMBARDIER SB 100-27-21 AND 350-27-011.SDR UIEA2022050600438Stab System · warning messageSTAB TRIM ADVISORY EICAS MESSAGE UPON LANDING. T/S FIM 27-48- F/T 809 FOUND SYSTEM OK PER AMM 27-41-00/715 E/O 6722A008CSSDR CALA2022042501075Stabilizer · inoperative*EMERGENCY DECLAERD* NO TRIM ON EITHER SIDE USED CAPT ATHORITY PULLED BREAKER ONCE NO JOY LOCKING UNLOCKING REPLACED STAB TRIM MOTOR. REF MM 27-41-71-400-801. COMPLETED PERFORMED STAB TRIM MOTOR AUTOPILOT TEST PER AMM 22-11-81; TEST STAB TRIM LIMIT SWITCH TESSDR J7SA2022031400311None · noneDIVERTED DUE TO UNCOMMANDED STABILIZER CAS MESSAGE ILLUMINATED PASSING FL 280. CREW DECLARED EMERGENCY AND LANDED SAFELY AT KSLC. REPLACED HSEMU ASSY IAW G450 AMM 27-41-03. OPS CHECK GOOD. P/N 1159SCC610-13; S/N 0216A.SDR A6WA202203088120None · noneDURING CLIMB OUT RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. ALSO RECEIVED AP PITCH TRIM CAUTION MSG. DISCONNECTED AP. C/W QRH. MESSAGES REMAINED. AIR RETURN TO DAY. LANDED UNDER 47000 LBS. ***AIRCRAFT REMOVED FROM SERVICE **** R&R CA PITCH TSDR J7SA2022031000310None · noneDIVERTED DUE TO UNCOMMANDED STABILIZER CAS ILLUMINATED PASSING FL300. AIRCRAFT LANDED SAFELY AT KBOI. REPLACED HSEMU IAW G450 AMM 27-41-03. OPS CHECK GOOD. P/N 1159SCC610-13; S/N 0187.SDR HNAA2022021400077Not Reported · not reportedPDIS 907 27-41 2476641 10FEB22 CLT CLOSE
PTRIM MAIN INOP DISPLAYED ON EICAS.
FACT 10FEB22 17:27 CLT
PERFORMED FIM TASK 27-43-00-810-801-A STEP 1.NO MESSEGES ON EICAS.PERFORMED OPS IAW EMB AMM 27-40-00-700-802-A/500.OPS CHECK SDR SWIA202265200None · nicked* FOUND TWO NICKS ON THE LH TRUNNION OF THE HSTA ATTACH FITTINGS.(AREA MARKED) (C-CHECK RO 3-25-22) BLENDED DAMAGES ON LH TRUNNION OF THE HSTA ATTACH FITTINGS REF CRJ200 SRM 51-12-00. WITHIN LIMITS, RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-3SDR CALA2022020400310Motor · failedFULL AUTO TRIM FAILUE WE COULD TRIM USING MANUAL TRIM. CHECKED POWER TO ELECTRICAL CONNECTOR, FOUND OK. REQUIRES STABILIZER TRIM MOTOR REPLACEMENT PER FIM TASK 27-41 TASK 804 REPLACED STAB TRIM MOTOR AS PER AMM 27-71-41 PB401. OPS TES GOOD FOR SVC ROTABLE PASDR SWIA202265020None · gouged*HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB, SUPPORT PLATE INNER FWD EDGE GOUGED (MARKED) (C-CHECK RO 3/14/2022) REPAIRED GOUGING ON INNER FWD EDGE OF SUPPORT PLATE AT HSTA TRIM ACTUATOR LH PIVOT FITING ON V-STAB PER MHIRJ REO 601R-55-31-394 REV -- DSDR SWIA202265017None · gouged*HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB, OUTER DOUBLER FWD UPPER EDGE GOUGED (MARKED) (C-CHECK RO 3/14/2022) REMOVED DAMAGE FROM HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB OUTER DOUBLER FWD UPPER EDGE REF. SRM 51-12-00, NO DEFECTS NOTED, FINISHSDR A6WA202201108056Trim Switch · faultedRECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES AT CRUISE. QRH DIRECTED FLAPS 20 LANDING, WHICH WAS SUCCESSFUL WITH NO ISSUES. ATTEMPTED TO REENGAGE MULTIPLE TIMES WITHOUT SUCCESS. AIRCRAFT REMOVED FROM SERVICE. ACARS EMAILS REPORT FO STAB TRIM DISCONNESDR A6WA202201048048Warning Message · illuminatedSTAB TRIM CAUTION MSG IN FLT COULD NOT ENGAGE CHANNEL 1 OR 2 AT FLT LEVEL 340. CW QRH L.5 HRS LATER AT 6000 FT BOTH CHANNELS REENGAGED AND STAYED ENGAGED THE REMAINDER OF THE FLT. NORMAL LANDING FLAPS 20. AIRCRAFT REMOVED FROM SERVICE. PERFORMED SUP 05-0SDR CALA2022010300014Stabilizer · out of trimELECTRIC TRIM FAILED IN FLT STAB OUT OF TRIM CYCLED SYSTEM CB,S PER AMM 27-41 TASK804. SYSTEM CHECKS NORMAL AFTER RESET.SDR 2022F00036None · damagedDURING TRANSIT CHECK THE STABILIZER TRIM WITHOUT MOVEMENT, DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW FIM 27-41 TASK 805 PROCEDURE; DETECTING THE LEFT HORIZONTAL STABISDR 2022FA0000067Trim Motor · failedDURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW FIM 27-41 TASK 805 PROCEDURE; DETECTING THE RIGHT HORIZONTAL STABILIZER TRIM MOTOR DAMAGED; SO THE HORIZONTAL STABILIZER TRISDR 2022F00041None · damagedDURING TRANSIT CHECK THE STABILIZER TRIM WITHOUT MOVEMENT, DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW FIM 27-41 TASK 805 PROCEDURE; DETECTING THE RIGHT HORIZONTAL STABSDR HNAA2021111600560None · nonePDIS 686 27-41 2395231 15NOV21 CLT CLOSE
DECENTING THROUGH 12000 FEET. SPEED BRAKES DEPLOYED. TCS BUTTON PRESSED. IDLE THRUST. PTRIM MAIN INOP MSG WITH MATER CAUTION DISPLAYED. C/W QRH PTRIM MAIN MSG REMAINED.
FACT 15NOV21 14:04 CLT
SDR SWAA2021111743066Indicator · faultyON APPROACH WENT FROM FLAPS 5 TO 15; FLAPS SPLIT AT FLAPS 10; FLAPS LOCKED OUT; UNEVENTFUL LANDING; PSEU LIGHT ILLUMINATED AFTER LANDING. ; / [01] R&R FLAP POSITION INDICATOR;PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACEDSDR CALA2021111102095None · missingPDA 3 SEAL/PANEL MISSING ON RIGHT LOWER STABILIZER SEE PHOTO. ADDED PHOTO. REPLACED SEAL ASSY REF IPC 27-41-11-08 ITEM 110.SDR HNAA2021080200350Control Unit · malfunctionedPITCH TRIM MAIN INOP. R+R HSCU IRW EMB 145 AMM 27-40-01. OPS CHECK GOOD(MX CTRL NOTE: HSCU WAS CHANGED AS A PRECAUTION. FIM TASK 27-43-00-810-801-A WAS FOLLOWED TO BLOCK 7 WHICH DETERMINED AS A TRANSITORY CONDITION.)SDR HNAA2021061400260Warning Message · false indicationDURING LANDING WHEN SELECTING FLAPS TO 45 MAIN PITCH TRIM AND BACK UP PITCH TRIM INOP BOTH APPEARED ON EICAS. PER FIM TASK 27-43-00-810-820-A FIM PROCEDURES BLOCK DIAGRAM BLOCKS 3&8 HORIZONTAL STAB ELECTRNIC OPERATIONAL TEST AMM TASK 27-40-00-802-A/500 TRANSISDR HNAA2021060900235Actuator · faultedPITCH TRIM BACK UP INOP. R&R HORIZONTAL STABILIZE ACTUATOR IAW EMB 145 AMM 27-40-02-000/A00-801A REQUIRES ZERO RIG CHECK AMM TASK 27-40-02-700-801-A/500. PERFORMED ELECTRICAL ZERO POSITION OF HORIZONTAL STABILIZER IAW AMM 27-40-02-801-A/500 OPS CHECK GOOD P/N SDR ASMF202106017Control Cable · damagedDURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITH SLOW MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FWD DRUM STABILIZER CONTROL CABLE DAMAGED; SO THE STABILIZER CONTROL CABLE P/N 251A4910-5, S/S, MANUFACTURER BOEINGSDR 2021F00169Stabilizer · damagedDURING TRANSIT CHECK THE STABILIZER TRIM WITH SLOW MOVEMENT DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITH SLOW MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FWD DRUM STABILIZER. DURING TRANSIT CHECK THE STABILISDR ASAA2021052834963Motor · failedNO ELECTRIC YOKE TRIM ( BOTH YOKES) ON TAKE OFF. QRH COMPLETED WITH. MANUAL STABILIZER TRIM FUNCTIONED NORMALLY. GROUNDED - YES. REMOVED AND REPLACED STAB TRIM MOTOR IAW B737-800 AMM 27-41-71 OPS CHECK OK.SDR A6WA202105287791Switch · malfunctionedMACH TRIM STAB TRIM CASS MESSAGES IN FLT. C/W QRH, MESSAGES REMAINED. OCCURRED DURING CRUISE AFTER NORMAL TAKE OFF. C/W QRH AND SET FLAPS TO 20. CONTROLS DIFFICULT TO MOVE BUT FELT SAFE TO PROCEED. LANDED WITHOUT ISSUES, SMOOTH LANDING BUT DID DECLARE AN EMSDR 2021F00160Motor · failed24.05.2021 12:00 DURING TRANSIT CHECK THE STABILIZER TRIM WITHOUT MOVEMENT DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING HORIZONTAL STABILIZER FAIL TO TRIM NOSE UP ANDSDR J7SA2021041300284Trim Switch · failedDURING CLIMB, CYAN STAB TRIM FAULT CAS MESSAGE POSTED. MDC INDICATED PILOT MANUAL TRIM SWITCH FAULT DETECTED BY HSTECU. WHEN THE AUTOPILOT WAS DISCONNECTED PRIOR TO LANDING, THE HORIZONTAL STABILIZER TRIMMED TO 0.0. NEITHER THE PILOT'S NOR THE COPILOT'S TRIM SSDR HNAA2021031600099Button · faultedMAIN PITCH TRIM INOPERATIVE EICAS MESSAGE DURING CRUISE FLIGHT WITH OUT SELECTING A CHANGE OF TRIM AND A/P ON FO'S SIDE. T/S IN REF TO FIM TASK 27 43 00 STEPS 1-4/10-11. FOUND CONTINUITY DEFECT ON PUSH BUTTON MAIN CUTOUT. R & R THE PUSH BUTTON IAW AMM 20 13 0SDR HNAA2021031600098Control Unit · failedMAIN PITCH TRIM INOP EICAS MESSAGE IN CRUISE FLIGHT WITHOUT SELECTING A CHANGE OF TRIM AND A/P ON FO'S. T/S FOUND HOR STAB CTL UNIT FAILURE TWICE ON MFD, R&R STAB CTL UNIT IAW EMB 145 AMM 27-40-01 NO FIX. REMOVED PANEL 324EL CLEANED CP'S ON STAB ACTUATOR AS RSDR AALA202101059007Position Switch · out of positionAIRCRAFT WAS GROUNDED. AT BOS, CREW REJECTED TAKEOFF AT 90 KNOTS DUE TO FEEL DIFFERENTIAL WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE. FLIGHT CONTROL SWITCH A FOUND IN OFF POSITION WITH GUARD DOWN COVERING SWITCH. SYSTEM TESTS NORMAL, PER FIM 27-3SDR CALA2020100701156Switch · defectiveELECTRIC TRIM WILL NOT TRIM UP STAB OUT OF TRIM SPEED TRIM FAIL T/S, IAW FIM 27-41-00-810; WDM 27-41-11, WDM 27-41-12. FOUND F/O COLUMN SWITCHING MODULE(M1201) AT FAULT STAB TRIM PITCH UP WORKED, IAW MM 27-41-51. PITCH TRIM UP WORKED CONSISTANTLY, BUT LAND VSDR SWIA2020082752083Pitch Control · malfunctionedPITCH TRIM FAIL CAUTION MESSAGE DURING CLIMBOUT. UNCOMMANDED NOSE DOWN PITCH TRIM OCCURRED. QRH PROCEDURES RESOLVED PITCH TRIM PROBLEM. FLIGHT 4089. TROUBLESHOT PER ERJ FIM TASK. A/P QUICK DISCONNECT OPERATE AS REQUIRED. PERFORMED ERJ FIM TASKS. OPS CHECK GSDR HNAA2020080300240Warning Message · false activationDURING CLIMB WHILE MOVING PITCH TRIM NOSE DOWN THE PITCH TRIM MAIN INOP DISPLAYED. SELECTED PITCH TRIM BACKUP AND IT OPS NORMAL. MAINTENANCE: INSP'D FOR DEFECTS. NONE NOTED. T/S IAW FIM TASK 27-43-00-810-801-A. SYSTEM CHECKED GOOD PER OPS CHECK TASK 27-40-00-7SDR O2GA2020072750101Position Switch · out of adjustSTAB MIS-COMPARE ANNUNCIATOR ILLUMINATED WHEN FLAP SELECTOR WAS SELECTED TO ZERO POSITION. AIRSPEED WAS BELOW 200 KYS. EMERGENCY DECLARED BY ATC AND DIVERTED TO ALTERNATE DESTINATION. MAINTENANCE ADJUSTED THE HORIZONTAL STABILIZER POSITION SWITCH. GROUND OPERA
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