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 20000913SH015Indicator · malfunctionedPILOT REPORTED CONTINUOUS TRIM INDICATOR MALFUNCTION. AFTER NUMEROUS ATTEMPTS TO RESET INDICATOR, A NEW PART WAS RECEIVED. THE TANG WHICH RIDES IN THE TRIM WHEEL WAS FOUND TO BE SHORT BY 50 PERCENT. NEW INDICATOR INSTALLED WITH NO FURTHER PROBLEMS. (X)SDR 2000UALA00503Warning Light · illuminatedSTAB TRIM EICAS AND OVERLIGHT CAME ON WHILE LEVELING AT FL 330, UNABLE TO DETERMINE TRIM RATE.SDR SWIA971928Sensor · failed''''TO BRAKES, TRIM, FLAPS'''' WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED RIGHT TRIM PROX SENSOR. OPS CHECKS GOOD.SDR SWIA971927Warning System · malfunctionedTRIM WARNING ON TAKEOFF ROLL. ABORTED INSPECTED TRIM WARNING SYSTEM. NO DEFECTS NOTED. PERFORMED EXTENSIVE FUNCTIONAL CHECKS OF THE TRIM WARNING SYSTEM. ALL CHECKS FOUND GOOD IAW MM 27-52-00.SDR SWIA971910Indicator · malfunctionedSTAB TRIM CAUTION MSG APPEARED AFTER TAKEOFF. TWO ATTEMPTS BEFORE STAB TRIM CAUTION CAME ON AGAIN. REMOVED AND REPLACED HSTU AND PERFORMED FUNCTIONAL TEST MM 27-41-01, CAT II.SDR 20000817SH002Control Cable · brokenSTABILIZER TRIM REPORTED INOPERATIVE BY CREW AT 500 FEET FINAL. ON INVESTIGATION, FOUND THAT STABILIZER TRIM FEEDBACK POSITION INDICATOR CABLE BROKEN. AIRCRAFT AOG. CREW REPLACED BROKEN CABLE AND CARRIED NECESSARY TESTS. AIRCRAFT RELEASED TO SERVICE BY CRESDR CA000712006Indicator · malfunctioned(CAN) INDICATOR PART OF ACTUATOR MALFUNCTIONED. THE POINTER FELL TO FULL NOSE UP, THE ACTUATOR ITSELF DID NOT MOVE . IT WAS JUST AN INDICATION PROBLEM. SENDING UNIT IS PART OF THE ACTUATOR ITSELF.SDR SWIA971749Controller · failedSTABILIZER CHANNEL NUMBER TWO WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MCU IAW MM 274201, OPS CEHCKS GOOD CAT II OK HSTA (P/N 83963) ON, (S/N 125) ON, (S/N 876) OFF, MCU (P/N 70623) ON, (S/N 205) ON, (S/N 319) OFF.SDR COMA0060131Warning System · activatedSTABILIZER AND MACH TRIM CAUTION MESSAGE. RESET STAB TRIM SYSTEM. COULD NOT DUPLCIATE. NO FAULT CODES IN TRIM COMPUTER.SDR COMA0010023Prox Sensor · out of adjustTAKEOFF TRIM WARNING, WHEN TRIM SET IN GREEN RANGE. ADJUSTED THE RIGHT HAND ELEVATOR TRIM PROXIMITY SENSOR.SDR RIVA9900001Control Cable · shearedAFTER ARRIVAL OF FLIGHT NR 1 IN SFB, CREW NOTICED TRIM TAB INDICATOR STUCK AT 7.5 UNITS NOSE UP BOTH SIDES (CAPT''S & F/O''S). MAINTENANCE REMOVED AND REPLACED CABLE WITH NEW. ALL WORK AND ADJUSTMENTS DONE IN ACCORDANCE WITH THE BOEING MAINTENANCE MANUAL CHASDR 99UAL900608Controller · failedON APPROACH, STAB-TRIM WENT NOSE-UP. CREW SUCCESSFUL IN RESETTING CIRCUIT-BREAKER. EMERGENCY DECLARED. FLIGHT LANDED WITH NO FURTHER INCIDENT. *S/D* AN INTERNAL FAILURE IN THE LEFT STABILIZER TRIM CONTROL MODULE (STCM) INHIBITED MOVEMENT OF THE HORZ STABSDR ARWA990902Sensor · failedMIA - FLT 601 - AFTER ROTATION STAB CONTINUOUSLY RAN NOSE DOWN AND WARNING HORN RAN CONTINUOUSLY. SPLIT SUITCASE HANDLES AND PULLED 'STAB AND AUTOPILOT' OFF WARNING HORN CIRCUIT BREAKER TO SILENCE HORN. RETURNED TO MIA WITHOUT INCIDENT. REPLACED STAB MOTION SDR AT9900595Shaft · corrodedDURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION ON HORIZONTAL STABILIZER TAKEOFF WARNING MECHANISM AT BS 351 L20R. REMOVED AND REPLACED MANUAL OVERRIDE CONTROL BELLCRANK SHAFT, INTERCONNECT BRACKET, P/N 5915830-501, LIMIT SWITCH CONTROL ARMSDR SCNA99004Switch · frozenDURING TAKEOFF ROLL, THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF. FOUND THE STABILIZER POSITION SWITCH S532 FROZEN. DEICED THE SWITCH AND CLEANED. PERFORMED A TAKEOFF WARNING SYSTEM CHECK WITH NO FAULTS NOTED. ALL SYSTEMS CHECK NORMAL AND OK FOR SERSDR CA981207016Transmitter · failed(CAN) STABILIZER FAILED TO TRIM NOSE DOWN AROUND 10 POINTS WITH FIRST OFFICER AND CAPTAIN THUMB SWITCHES. FOUND CONTROL COLUMN TRIM AND MANUAL LEVER SWITCHES SHOWING ON RIGHT STABILIZER TRIM ELEVATOR ASYMMETRY MODULE. REPLACED M519/M520 STABILIZER POSITION TSDR 98UAL900183Stab Trim Ind · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO STABILIZER TRIM INDICATION.SDR COMA9860023Warning · activatedSTAB TRIM AND MACH TRIM CAUTION MESSAGE. PERFORMED FUNCTIONAL CHECK OF SYSTEM. NO FAULTS FOUND.SDR EISA97280Switch · malfunctionedTAKEOFF, AURAL WARNING SOUNDS AT ALL TIMES. REMOVED AND REPLACED UPPER STABILIZER TRIM SWITCH. (X)SDR QXEA9700633Warning Light · illuminatedSMF - BOTH CHANNEL LIGHTS ILLUMINATED FOR STABILIZER. USED ALTERNATE TRIM PROCEDURES. INSPECTED, NO DISCREPANCIES NOTED. DRAINED AND REPLENISHED FLUID IN STABILIZER ACTUATOR. NO COMPONENTS REPLACED. OPERATION CHECK GOOD.SDR 9710326614Limit Switch · failedDURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE STABILIZER TRIM LIMIT SWITCHES, OPERATIONAL CHECK GOOD.SDR 9706991232Motion Sensor · failedDURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. RECYCLED FLAPS, TRIM, POWER LEVERS, AND PARKING BRAKE, NO HELP. ABORTED TAKEOFF. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER MOTION SENSOR.SDR 9705289985Wire · looseTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 20 KNOTS AND RETURNED TO GATE. MAINTENANCE REPAIRED LOOSE WIRE AT HORIZONTAL STABILIZER POSITION SWITCH IN FORWARD BAG BIN. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR 97ZZZX494Sensor · miswiredCREW REPORTED MACH TRIM FAULT LIGHT AND WARNING TONE ABOVE .74 MACH. REPLACED HORIZONTAL STABLIZER POSITION SENSOR PER LEARJET A.M.M. PROBLEM RECURRED WITH ADDITION OF RAPID NOSE UP OR DOWN TRIM CHANGE ABOVE .69 MACH. AFTER MUCH TROUBLESHOOTING, FOUND NEW SSDR 9626779302Caws Warning · activatedREJECTED TAKEOFF AT APPROX 90 KTS DUE TO STAB CAWS WARNING. FLIGHT RETURNED TO GATE. MAINTENANCE CYCLED STAB TRIM AND CHECKED STAB TAKEOFF WARNING SWITCH. NO DISCREPANCIES FOUND. AIRCRAFT APPROVED FOR FURTHER SERVICE.SDR JBXA00028Warning Light · illuminatedBDL - FLT 373 - AIRCRAFT STARTED TAKEOFF ROLL, HAD A STAB NR 1 AND NR 2 FAULT. PLANE RETURNED TO GATE. MAINTENANCE PERFORMED AFCAS TEST. AIRCRAFT RETURNED TO SERVICE. (X)SDR 9622379868Switch · malfunctionedTAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND STABILIZER POSITION SWITCH S1-141 INOPERATIVE. REPLACED SWITCH, OPERATIONAL CHECK NORMAL.SDR 9619189301Ind Module · malfunctionedSTABILIZER TRIM CHECKED ON TAXI BY ADVANCING LEFT THROTTLE, NO WARNING. WHEN THROTTLES ADVANCED FOR TAKEOFF, RECEIVED STABILIZER TRIM WARNING. CLEARED RUNWAY AND RETURNED TO THE GATE. REPLACED HORIZONTAL STABILIZER POSITION INDICATION MODULE. CHECKED AND TSDR 9604985501Position Trans · failedDURING APPLICATION OF TAKEOFF POWER, STABILIZER WARNING MESSAGE ILLUMINATED AND TAKEOFF WAS ABORTED. VERIFIED STABILIZER TRIM SETTING WAS WITHIN GREEN BAND AND MESSAGE REMAINED. MAINTENANCE REPLACED THE CENTER STABILIZER TRIM POSITION TRANSMITTER AND OPERATISDR GLBA96042Prox Sensor · failedMYR - CREW REPORTED AURAL WARNING INDICATING UNSAFE TRIM SETTING ON TAKEOFF. ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MX REMOVED AND REPLACED LEFT TRIM PROX SENSOR. SYSTEM OPS CHECK GOOD. (M)SDR 96ZZZX146Transmitter · misoverhauledAFTER TROUBLESHOOTING AN AUTOPILOT PROBLEM, ORDERED AN ELEVATOR FOLLOW-UP TRANSMITTER ON AN EXCHANGE BASIS REQUESTING AN OVERHAULED UNIT. AFTER RECEIVING THE PART, THE UNIT WAS NOT OVERHAULED, BUT MERELY 'FUNCTIONALLY TESTED' BACK IN 1989. THE NULL INDEX WASSDR 95ZZZX3819Relay · sticksTRIM MOVEMENT ANNUNCIATION HORN FAILED TO SILENCE AFTER MANUAL PITCH TRIM INPUT. TROUBLESHOOTING DETERMINED THE K134 PITCH TRIM FAIL DETECTION (NORMAL) RELAY REMAINED ENGAGED DUE TO EITHER A WEAK INTERNAL SPRING OR EXCESS FRICTION. REPLACEMENT OF RELAY CUREDSDR P5CA9500056Switch · failedDURING TAXI FOR TAKEOFF, CONSTANT TAKEOFF WARNING. RECYCLED ALL FLIGHT CONTROLS, NO HELP. RETURNED TO BLOCKS, OPERATIONAL CHECK OK PER BOEING MAINTENANCE MANUAL 31-26-00.SDR SCNA95127Switch · failedTAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED. AIRCRAFT RETURNED TO GATE, FOUND UPPER STABILIZER TAKEOFF WARNING SWITCH S532 BAD. REMOVED AND REPLACED SWITCH PER MM 31-26-24 PAGE 401. SYSTEM OPS CHECKED GOOD.SDR 95UAL767020Sam Module · malfunctionedUNWANTED STABILIZER TRIM INDICATION AT 30-40 KNOTS ON TAKEOFF ROLL. WENT OUT WITHIN 2-3 SECONDS, THEN CAME ON AGAIN AT ABOUT 60 KNOTS. AGAIN WENT OUT WITHIN 2-3 SECONDS. ABORTED TAKEOFF. REPLACED THE RIGHT SAM MODULE. OP CHECKS OK.SDR 9505752275Switch · inoperativeDURING APPLICATION OF TAKEOFF POWER, INTERMITTENT WARNING HORN SOUNDED. ABORTED TAKEOFF, RECYCLED FLAP AND SPEED BRAKE CONTROLS. ON SECOND DEPARTURE ATTEMPT, SAME RESULTS OCCURRED. RETURNED TO THE GATE AND DEPLANED AIRCRAFT. MAINTENANCE FOUND S532 UPPER STSDR 95ZZZX1719Potentiometer · shaft shearedELEVATOR POSITION POTENTIOMETER FOR FDR FOUND SHEARED. THIS IS SECOND FAILURE OF THIS TYPE ON SECOND AIRCRAFT. CESSNA ENGINEERING FOUND BRACKET MISALIGNED. THEY READJUSTED TO PREVENT FUTURE FAILURE.SDR COM60381Trim Ind · malfunctionedSTABILIZER TRIM INDICATOR FLUCTUATES RAPIDLY BETWEEN 3 AND 0. COULD NOT DUPLICATE. NO FAULTS FOUND IN STABILIZER TRIM INDICATION.SDR 9500042202Position Switch · malfunctionedDURING 5 DEGREE FLAP TAKEOFF AT 20 KNOTS, CENTRAL AURAL WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE UPPER STABILIZER TRIM POSITION WARNING SWITCH S532. OPERATIONAL CHECK NORMAL PER MM 31-26-24.
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