JASC 2220

Service difficulty reports · 118

Reports filed under 2220 · Speed-Attitude Correction 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 = '2220'
  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.

SDR SWIA200616500Transducer · malfunctionedSTALL FAIL CAUTION MSG STILL PERSISTS DURING TAXI. REPLACED BOTH NR 1, 2 MACH TRANSDUCERS IAW MM CH 27-35-25-720-801. OPERATIONAL CHECK GOOD. P/N ON 60730-000-1, S/N #1 OFF 2008 S/N #2 OFF 1771.Mar 29, 2006 · N466SW · Cndair CL6002B19SDR MASA200600801Trim System · inoperativeASH 7252 ORD - MACH TRIM INOP. MX CND. OP'S CHECK GOOD.Mar 16, 2006 · N570ML · Cndair CL6002B19SDR MASA200600816Yaw Damper · disconnectedASH 7202 ORD - YAW DAMP 2 DISCONNECT IN FLIGHT. MX CURRENTLY TROUBLESHOOTING. AIRCRAFT IS OUT OF SERVICE. OP'S CHECK GOOD.Mar 15, 2006 · N592ML · Cndair CL6002B19SDR SWIA200616165Transducer · malfunctionedSTAB CH1 INOP MSG, APPEARED DURING CRUISE FLIGHT. REPLACED NR 1 MACH TRANSDUCER IAW 27-35-35 OPERATIONAL CHECK OK. PN ON 60730-000-1 SN ON 1771 OFF 1969Jan 20, 2006 · N466SW · Cndair CL6002B19SDR PIDA06006Control Unit · malfunctionedYAW DAMPER WILL NOT ENGAGE. PLACED ON MEL 22-3-B. 01/16/2006: REPLACED YAW DAMPER CONTROL UNIT. SYSTEM TESTS OK PER MM 22-12-01.Jan 12, 2006 · N250TR · Boeing 7372K5SDR SWIA200515950Control Unit · malfunctionedSTAB TRIM AND MACH TRIM FAILED WILL NOT RE-ENGAGE. REPLACED THE HSTCU IAW MM 27-41-01, OPERATIONAL CHECK GOOD IAW MM 27-40-00.Dec 2, 2005 · N439SW · Cndair CL6002B19SDR SWIA200515586Transducer · malfunctionedSTALL FAIL CAUTION MSG AND YAW NR 2 STATUS MSG. REPLACED NR 2 MACH TRANSDUCER IAW MM 27-35-25. OPERATIONAL CHECK GOOD.Sep 22, 2005 · N465SW · Cndair CL6002B19SDR QXEA200501151Flow Divider · malfunctionedSEA - NR 2 ITT TAKES UP TO 9 SECONDS TO LIGHT OFF FROM THE POINT OF FUEL INTRODUCTION OF ENGINE START. IT IS WITHIN THE TEN SECOND GUIDANCE IN THE ABNORMAL CHECKLIST BUT FOUR TO FIVE SECONDS LONGER THAN THE NR 1 ITT. MAINTENANCE REPLACE NR 2 ENGINE FUEL FLOWAug 4, 2005 · N369PH · Dhav DHC8202SDR DL767050386Yaw Damper · malfunctionedUNCOMMANDED RUDDER INPUT AT ROTATION, THOROUGHLY CHECKED SYSTEM. UNABLE TO DUPLICATE OR FIND FAULT.Jul 20, 2005 · N102DA · Boeing 767232SDR SWIA200515217Switch · malfunctionedON DESCENT AUTOPILOT ON STAB/MACH TRIM 1 AND 2 AND DISCONNECTED. REPLACED CAPT STAB DISCONNECT SWITCH IAW CRJ MM27-41-30. OPERATIONAL CHECK GOOD.Jun 30, 2005 · N923SW · Cndair CL6002B19SDR AALA20050242Computer · inoperativeAFTER TAKEOFF GOT MASTER CAUTION FOLLOWED BY FLIGHT CONTROL AND SPEED TRIM FAIL LIGHT AND WITH AUTO PILOT PITCH ON GOT STABILIZER OUT OF TRIM LIGHT. REPLACED FLIGHT CONTROL COMPUTER SYSTEM A. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)Apr 1, 2005 · N908AN · Boeing 737823SDR DLM88050104Actuator · unknownREQD 6 DEG RT RUDDER, 1 DEG RT AILERON FOR LEVEL AND TRIMMED FLT. RETURNED CVG. REPLACED YAW DAMP ACTUATOR PER MM. PERFORMED RTS ON BOTH DFGC'S GO.Feb 10, 2005 · N964DL · Doug MD88SDR AU510001547Actuator · failedAUTOPILOT STABILIZER TRIM ACTUATOR FAILED DUE TO STRIPPED ROTOR GEAR AND WORN ROTOR BEARING JOURNAL.Jan 7, 2005 · Boeing 737476SDR 04230699Control Unit · defectiveSTAB TRIM FAILURE. DECLARED EMERGENCY AND DIVERTED TO HSV. LANDED UNEVENTFULLY. RESET HSTCU IAW CRJ FIM.Aug 17, 2004 · N699BR · Cndair CL6002B19SDR 04215650Trim System · inoperativeSTAB TRIM FAIL EN ROUTE. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE LOCATION, DECLARED EMERGENCY.Aug 2, 2004 · N650BR · Cndair CL6002B19SDR 371PA0045Sensor · out of adjustAIRCRAFT CLIMBS ON AUTO PILOT DURING CRUISE FLIGHT AT .780 AND ABOVE. STAB OUT OF TRIM ILLUMINATES. PLACED MACH TRIM ON MEL 22-5. 6/26/2004: ADJUSTED BOTH STAB (ELEVATOR) POSITION SENSOR RODS. CHECKED GOOD PER FMC ELEVATOR RIG, AUTO PILOT AND AUTO LAND TEJun 24, 2004 · N371PA · Boeing 737306SDR SWIA200413471Indicator · contaminatedRECEIVED IAS EI MACH TRIM CAUTION MESSAGE ON DESCENT. DRAINED WATER FROM MACH SYSTEM NR 1. RESET CIRCUIT BREAKERS. OPERATIONAL CHECK OK.Jun 18, 2004 · N432SW · Cndair CL6002B19SDR 373PA0050Iru · failedLEFT ADI ROLLED 20 DEGREES PITCH UP AND 45 DEGREES LEFT BANK AT 33,000 FT. AUTO THROTTLES REDUCED TO IDLE. LATER IN LANDING PATTERN THE LEFT IRU FAULTED AND FLAGGED. REPLACED LEFT IRU PER MM 34-28-31. CHECKED IRU AFFECTED SYSTEMS PER WDM 34-26-13 AND RAN BJun 3, 2004 · N373PA · Boeing 7373Y0SDR COMA0460318Actuator · malfunctionedFLIGHT 5405 RUDDER FLUTTER DURING FLIGHT. REPLACED THE YAW DAMPNER ACTUATOR.May 12, 2004 · N965CA · Cndair CL6002B19SDR 04103650Control Unit · inoperativeDURING CRUISE OF FLIGHT 7823 CREW REPORTED A STAB/MACH TRIM FAILURE. CREW DIVERTED TO NEAREST SUITABLE AIRPORT AND FLIGHT LANDED SAFELY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS Apr 12, 2004 · N650BR · Cndair CL6002B19SDR 371PA0040Sensor · inoperativeMACH TRIM INOPERATIVE. ADJUSTED NEUTRAL SHIFT SENSOR IAW MM 22-11-14. OPS CHECKS GOOD.Mar 27, 2004 · N371PA · Boeing 737306SDR MWEA040028Computer · intermittentLOW SPEED HIGH PROTECTION CAME ON TOGETHER AND STICK SHAKER. PERFORMED ADJUSTMENT TEST OF NUMBER 1 FLIGHT CONTROL COMPUTER AND NR 2 FLIGHT CONTROL COMPUTER STALL WARNING SYSTEM BOTH PASSED STALL WARNING CHECK.Mar 20, 2004 · N910ME · Boeing 717200SDR 04FDEA00604Sensor · failedDURING CRUISE FLT AT FL330 AT .82 MACH THE A/C PERF U/C ROLL DOUBLETS (DUTCH ROLL MOTION). A/P AND STAB WAS OUT OF TRIM WITH A PITCH UP ATT DEV. TRIMMED THE STAB AND LEVELED A/C AND RECONN A/P. A/P WAS IN SYS-B. WHEN RECONN, THE A/P TRIMMED NOSE UP, HAD TMar 6, 2004 · N209FE · Boeing 727200SDR BAQA091471Computer · inoperativeMACH TRIM COMPUTER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 12/9/03Nov 7, 2003 · N40DK · Lear 55LEARSDR 373PA0020Computer · failedSPEED TRIM FAIL AND MACH TRIM FAIL ON OVERHEAD PANEL. ENGINES RUNNING, READY FOR TAXI. DEFERRED PER MEL 22-1 AND 22-5-1. 8/18/2003: REPLACED FLIGHT CONTROL COMPUTER IAW MM 22-11-33. FCC BITE TEST GOOD. SPEED TRIM AND MACH TRIM OPS CHECKS NORMAL.Aug 18, 2003 · N373PA · Boeing 7373Y0SDR HEEA088050Amplifier · malfunctionedSCAS AMPLIFIER KICKS OFF LINE.Jul 8, 2003 · Bell 214STSDR 252TR0006Coupler · intermittentMACH TRIM IS INTERMITTENT. PLACED ON MEL 22-5. 7/15/2003; REMOVED AND REPLACED MACH TRIM COUPLER IAW MM 22-21-0 AND CLEARED MEL.Jul 5, 2003 · N252TR · Boeing 737228SDR 03170674Control Box · inoperativeWHILE ON DESCENT WITH AUTOPILOT ENGAGED, STAB FAIL AND MACH FAIL MESSAGES APPEARED. THE STAB AND MACH TRIM WOULD NOT REENGAGE, EMERGERNCY DECLARED AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REPLACED THE HSTCU AND PERFOREMED A SATISFACTOJun 19, 2003 · N674BR · Cndair CL6002B19SDR HEEA087145Amplifier · inoperativeDURING INSTALLATION THE SCAS WOULD NOT COME ON LINE WITH THIS AMP. COULD NOT ALIGN SCAS. ADJUSTMENTS COULD NOT BE MADE USING VARIABLE RESISTORS. SENT TO BELL HELICOPTER TEXTRON FOR WARRANTY REPAIR. REFERENCE: DMR 748396.Jun 9, 2003 · N3897N · Bell 214STSDR 174042903Probe · failedRT AOA PROBE FAILS TO HEAT.Apr 29, 2003 · N562NA · Pilats PC1245SDR ARWA20030406Sensor · failedSTALL WARNING NR 1 CHANEL FAILED IN FLIGHT, CONTINOUS STICK SHAKER IN FLIGHT. DE-SELECTED NR 1 CHANEL AND RETURNED TO MIAMI AS ADVISED BY FLIGHT CONTROL. DUMPED FUEL 1508Z-1520Z DOWN TO LANDING WEIGHT. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK SENSOR IAW Apr 28, 2003 · N307GB · Lkheed 1011385115SDR A6WA200340054Accelerometer · malfunctionedDURING TAKEOFF ROLL AT 70 KNOTS, OBSERVVED N2 ENGINE VIBE 'ICON' ON NR 1 ENGINE BTMS. ALL GREEN BANDS ON ABORTED TAKEOFF. PERFORMED PARTIAL ENGINE BORESCOPE. NO DAMAGE NOTED. REMOVED AND REPLACED NR 1 ENGINE ACCELEROMETER. NO DEFECTS NOTED. (M)Apr 17, 2003 · N422AW · Cndair CL6002B19SDR 223020203Probe · failedRT AOA PROBE DOES NOT HEAT.Apr 2, 2003 · N317NA · Pilats PC1245SDR 249TR0016Warning Light · illuminatedMACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. UNABLE TO DUPLICATE. PERFORMED BITE TEST VIA PDCS CDU, NO FAULTS NOTED.Mar 31, 2003 · N249TR · Boeing 7372K5SDR 249TR0015Warning Light · illuminatedMACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT, THEN WENT AWAY. COMPLETED MACH TRIM TEST PER MM 22-21-0. OPS CHK OK.Mar 30, 2003 · N249TR · Boeing 7372K5SDR 226032303Probe · failedLEFT AOA PROBE FAILS TO HEAT.Mar 23, 2003 · N308NA · Pilats PC1245SDR 730PA0002ComputerOn landing checklist "speed trim fail light" illuminated when recall was pressed. Performed BITE test of DFCS system per MM 22-03-10, Function check normal.Jan 7, 2003 · N730PA · Boeing 7373L9SDR CA030107016Computer · failed(CAN) MACH TRIM LIGHT CAME ON IN FLIGHT, CREW REPORTED ELEVATOR FEEL INOPERATIVE. AIRCRAFT RETURNED TO DEPARTURE STATION. ELEVATOR FEEL COMPUTER REPLACED AS PER AMM. AND OPERATION CHECKED SERVICEABLE.Jan 5, 2003 · Boeing 737217SDR 801DM0004Autopilot SysAircraft will not maintain spped in "SPD" mode. Removed autopilot MCP for bench check. MCP was repaired and installed. Ops ck normal per MM 22-11-02.May 14, 2002 · N801DM · Boeing 757200SDR COMA0260273ComputerFLIGHT 5356 YAW DAMPNER #1 INOP WARNING DURING T/O.RESET IAPS SYSTEM - YAW DAMP SYTEM TEST NORMAL.Apr 22, 2002 · N431CA · Cndair CL6002B19SDR 250TR0001ReceiverMCP panel @ 7000`, engage PDC A/S bug goes to 310K. Speed mode would not engage. When flaps select to 5 auto pilots kick off, would not re-engage. R&R both radio altimeters.Apr 9, 2002 · N250TR · Boeing 7372K5SDR SWIA200110228Trim Switch · malfunctionedSTAB TRIM AND MACH TRIM DISCONNECTED IN FLIGHT. FOLLOWED QRH. ABOUT 1 MINUTE LATER, DISCONNECTED AGAIN AND WOULD NOT RESET. RETURNED TO SLC AND FOLLOWED QRH.FOUND BAD TRIM SWITCH ON FO'S YOKE. R&R SWITCH IAW 27-41-05. OPS CHECK GOOD. SELF TEST OF HSTCU OOct 6, 2001 · N413SW · Cndair CL6002B19SDR P2EA2001M0005CouplerMach Trim "fail" light illumimnates intermitently. Corrective action: Defferred Mach Trim system per MEL 22-5, CI#M005089 per MX CNTL Mic. Removed and replaces Mach Trim Coupler IAW MM 22-21-31, operational check normal. This clears MEL CI#M005089. See 005 LogSep 24, 2001 · Boeing 737297SDR COMA0160582Actuator · faultyBOTH YAW DAMPERS DROPPED OFF LINE DURING TAXI OUT, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #2 YAW DAMPER LINEAR ACTUATOR.Aug 8, 2001 · N814CA · Cndair CL6002B19SDR COMA0160575Actuator · faultyBOTH YAW DAMPERS DROPPED OFF LINE DURING TAXI OUT, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #2 YAW DAMPER LINEAR ACTUATOR.Aug 8, 2001 · N814CA · Cndair CL6002B19SDR COMA0160574ControllerDURING FLIGHT CONTROL CHECK AT FULL DEFLECTION THE #2 YAW DAMPER DROPPED OFF LINE.PERFORMED SYSTEM RESET PER FIM, OPERATIONAL CHECK WAS SATISFACTORY.Aug 8, 2001 · N814CA · Cndair CL6002B19SDR DL777010432Autopilot Sys · malfunctionedON DECENT, MAX SPEED AUTOPILOT EICAS LT ILLUMINATED. AS WENT ABOUT 2 KNOTS HIGH INTO RED-OVERSPEED WARNING TRIED TO SOUND BUT WAS MUFFLED SOUNDING. AN ELECTRICAL SMELL ON LEFT SIDE OF COCKPIT WAS NOTICED SUSPECT OVERSPEED SHAKER FAILURE. T/S AP MTC MSG PER FIMMar 14, 2001 · N860DA · Boeing 777232SDR SWIA972344Damper · failedUNABLE TO ENGAGE YAW DAMPER NUMBER TWO PRIOR TO FLIGHT. POWERED AIRCRAFT DOWN AND BACK UP. CYCLED YAW DAMPER SEVERAL TIMES. BOTH YAW DAMPER ONE AND TWO OPS CHECK GOOD.Feb 9, 2001 · N905SW · Cndair CL6002B19SDR EISA20000192Warning Light · activatedON PREFLIGHT STAB OUT OF TRIM LIGHT ILLUMINATED, WHILE IN PROCESS OF PLACARDING, CREW AND MAINTENANCE SMELLED SMOKE COMING FROM FWD PANEL. CORRECTIVE ACTION: TRANFERED TO PLACARD 445 MEL 22-2, CAT "D" 02-16-01 FOR STAB TRIM LIGHT, COULD NOT DUPLICATE PER M/MOct 19, 2000 · N74318 · Boeing 727231SDR SWIA971998Transducer · failedJUST AFTER LIFT OFF ''''''''STALL FAIL'''''''' MESSAGE. RETURNED TO SLC. REPLACED STALL COMPUTER. FAILED TEST. (P/N 39-951-002-08) ON, (S/N 521) ON, (S/N 589) OFF. REMOVED AND REPLACED NUMBER ONE MACH TRANSDUCER IAW MM 27-35-25. OPS CHECKS GOOD AT THIS TSep 27, 2000 · N417SW · Cndair CL6002B19
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