JASC 2700

Service difficulty reports · 1,745

Reports filed under 2700 · Flight 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 = '2700'
  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 JGVR20201016001Balance Weight · inadequateWHILE COMPLYING WITH EMBAER SB 505-55-0004 FOUND THE FOLLOWING, FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE AND REQUIRING REPLACEMENT. THREE RT ELEVATOR ADJUSTABLE BALANCE WEIGHTS P/N PE915109-L33 AND TWO LT ELEVATOR ADJUSTABLE BALANCE WEIGHTS P/N PE915109-Oct 16, 2020 · N420QS · Emb EMB505SDR 2A6R2020100657701Control Rod · crackedMULTIPLE CRACKS FOUND ON THE LONGITUDINAL SAS CONTROL ROD P/N: L221M1041104 AT THE 11 O`CLOCK POSITION (IF LOOKING AFT). ONE CRACK BEGINS AT A RIVET LOCATION AND CONTINUES PAST AN ADJACENT RIVET. THE SECOND CRACK PROPAGATES FROM THE EDGE OF THE TUBE PORTION,Oct 6, 2020 · N253AM · Urocop EC135P2SDR JGVR20200921001Balance Weight · unserviceableWHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE PER SB AND REPLACED WITH NEW PARTS. ONE LT ELEVATOR HORN WEIGHT P/N PE915109-L42, ONE LT ELEVATOR OB INTERNAL WEIGH P/N PE915109-L41, FOUR LT ELEVATOSep 21, 2020 · N407QS · Emb EMB505SDR 2020FA0000418Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (9 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PASep 18, 2020 · N309QS · Emb EMB505SDR J7SA2020091800222Unknown · malfunctionedAT CRUISE 43,000 FT, RECEIVED A STALL WARNING, PITCH TRIM BACK UP FAIL, FLAP FAIL, AND SPOILER FAULT. RAN THE QRH, THEN DESCENDED BY HAND DUE TO AUTOPILOT ONLY WORKING FOR ALTITUDE HOLD. RAN THE QRH FOR NO FLAP NUMBERS BELOW 18,000 FT THEN DECLARED AN EMERGESep 16, 2020 · N374FX · Emb EMB505SDR CALA2020091501112Trim System · malfunctionedCREW REPORTS STAB TRIM WILL NOT ELECTRICALLY IN THE UP POSITION PERFORMED FIM 27-41-00-810-800. OPS CHECK GOOD AND PERFORMED CAT III TEST, PER AMM 22-11-00.Sep 15, 2020 · N37419 · Boeing 737924ERSDR QXEA2020090700277Tab · out of adjustON CLIMBOUT WITH AP ON THROUGH 8500 MSL, RUDDER TRIM RUNAWAY, FULL RIGHT DEFLECTION. AT CRUISE WITH AP ON MISTRIM LT WING DN CAUTION PFD. THROUGHOUT FLIGHT LT AILERON PRESSURE REQUIRED TO HOLD WINGS LEVEL, ESPECIALLY AT HIGH POWER SETTINGS. REPLACED AILERON Sep 2, 2020 · N405QX · Bombdr DHC8402SDR QXEA2020090200273Control Panel · malfunctionedAIRPLANE REQUIRED MORE THAN 3/4 SCALE DEFLECTION OF THE LEFT AILERON TRIM. DURING CRUISE AND DESCENT GOT MISTRIM MESSAGE ON PFD, RAN CHECKLIST. SPOILERS INDICATED NORMAL, KEPT SPEED AT AROUND 230 FOR BETTER CONTROL. DID NOT DECLARE EMERGENCY. DESCENT AND LANSep 2, 2020 · N405QX · Bombdr DHC8402SDR 4USA2020090200002Control Unit · malfunctionedCLIMBING TO FL430 NOTICED THE STABILIZER TRIM CACKLE WAS SOUNDING RATHER EXCESSIVELY. IT SOUNDED 4 TIMES, THE 4TH TIME FOR MORE THAN 10 SECONDS. IMMEDIATELY DISENGAGED THE AUTOPILOT AND PRIMARY TRIM, STOPPED THE CLIMB, LEVELED OFF, AND ENGAGED THE SECONDARY Aug 25, 2020 · N713FL · Cessna 750SDR SIMA202008164002Unknown · multiple failDECLARED EMERGENCY INBD GCK PITCH TRIM MAIN INOP/BACKUP INOP PTRIM MAIN INOP ON FINAL-C/A-RESET A/C POWER AND PERFORMED HORZ STAB OPS CHECK IAW EMB 140 AMM 27-40-00-700-802-A. OPS CK GOOD, NO DISCREPANCIES NOTEDAug 14, 2020 · N816AE · Emb EMB135KLSDR HNAA2020072800235Warning Light · false activationGUST LOCK LIGHT ILLUMINATED DURING TAKE OFF ROLL. MAINTENANCE: PERFORMED OPS CHECK OF GUST LOCK MECHANISM IAW AMM TASK 27-70-00-700-802-A. OPS CHECK GOOD. LIGHT ILLUMINATED NORMALLY. OK FOR SERVICE AT THIS TIME. CLEARS MEL 27-11.Jul 27, 2020 · N654AE · Emb EMB145LRSDR O2GA2020070250101Printed Ckt Board · inoperativeSTAB MIS-COMPARE ANNUNCIATOR ILLUMINATED AFTER FLAP RETRACTION DURING INITIAL CLIMB. AIRSPEED LIMITS WERE NOT EXCEEDED. HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED UNTIL GEAR EXTENSION FOR LANDING. EMERGENCY WAS DECLARED AND AFM CHECKLIST PROCEDURE WAS FOLLOJun 28, 2020 · N501UP · Cessna 560XLSDR AALA202006309015Fault Message · illuminatedAIRCRAFT NOT GROUNDED: FLT CNTL ELAC 2 PITCH FAULT, TAKE OFF REJECTED AT 50KTS. QRH RESET, OPS NORMAL.Jun 26, 2020 · N724UW · Airbus A319112SDR AALA202006229003Module · contaminatedAIRCRFT WAS GROUNDED: AIR RETURNED TO DFW ACCOUNT FLIGHT CONTROL INDICATION MESSAGE. FLIGHT DECLARED EMERGENCY AND AIRCRAFT LANDED OVERWEIGHT. FCE-R CABINET, ACE MODULE HAS EVIDENCE OF MOISTURE EGRESS. REPLACED FCE-R CABINET ACE MODULE IN THE AFT E/E COMPARTMEJun 19, 2020 · N816AA · Boeing 7878SDR R61A2020032420450Mau · failedAVNX MAU 1A FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RESET.Mar 22, 2020 · N117HQ · Emb ERJ170200LRSDR AALA202003069020Control Stick · defectiveAIRCRAFT WAS NOT GROUNDED: FLIGHT CONTROL SENSOR FAULT ON ECAM ON LANDING ROLLOUT. INFO: AIRCRAFT DID HAVE ROLL OSCILLATION WITH FLAPS EXTENDED FOR LANDING. ACCOMPLISHED TSM 27-93-00-810-828-A NO FAULTS CONFIRMED. REPLACED CAPTAINS SIDE STICK ASSEMBLY AND ACCOMar 5, 2020 · N285AY · Airbus A330243SDR ASMF20200602012Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE MESSAGE IN EICAS AND STATUS OF SPOILER APPEARS AND FLAPS/SLATS INDICATOR STAYS IN POSITION 1 AND FLAP/SLAT LEVER IN POSITION 5. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING MESSAGE OF FAILURFeb 25, 2020 · N957AM · Boeing 737852SDR JGVR20200129001Balance Weight · corrodedDURING COMPLIANCE OF SERVICE BULLETIN 505-55-A004 REV 5 MASS BALANCE AND ATTACHMENT PARTS - (INSPECTION, CORROSION FOUND ON ALL BALANCE WEIGHTS. WEIGHTS WERE CLEANED AND TREATED PER SB INSTRUCTIONS. NO FLIGHT CONTROL WEIGHT CHANGES AT THIS TIME.Jan 29, 2020 · N336QS · Emb EMB505SDR RU3A202001274006Actuator · failedTAKEOFF WARNING HORN SOUNDED WITH FLAPS 20 DEGREES DURING TAKEOFF ROLL AT 135 KIAS. STAB ACTUATOR WAS REPLACEDJan 24, 2020 · N55 · Lear 60LEARSDR COEA201912204807Aoa · faultedFLIGHT 1700, AIR TURNBACK, ON TAKEOFF, THE MASTER CAUTION, FLIGHT CTR ON CAS AND STICK PUSHER SHAKER FAULT LIGHTS ILLUMINATED. AIRCRAFT WAS RETURNED TO DEPARTURE, NO EMERGENCY WAS DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EXTENSIVE TROUBLESHOOTDec 31, 2019 · N807HC · Aerosp ATR72212SDR 2019FA0000399Bracket · wornRUDDER AILERON INTERCONNECT STOPPED FUNCTIONING. DISCOVERED BRACKETS WORN THROUGH. NO CHAFING ON CONTROL CABLES FORTUNATELY. PART NO LONGER MANUFACTURED.Dec 9, 2019 · N2075T · Cirrus SR20SDR CALA2019111101965Warning Message · false activationFLIGHT CONTROL SYS EICAS STATUS ANY CONDITION OF THE FLIGHT CONTROL SYSTEM OR IT''S SYSTEM INTERF ACES WHICH WOULD PREVENT DISPATCH. FLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. FLIGHT CONTROL STATUS MESSAGE CLEARED WITH FLAPERONS REPAIRED.Nov 11, 2019 · N76010 · Boeing 777224SDR R61A2019110861220Wire · not reportedFLIGHT CONTROL ISSUE, PITCH UP. DECLARED EMERGENCY, RETURNED TO ATL, LANDED WITHOUT INCIDENT. C/W FIM 27-43-00 AND CYCLED TRIM SYSTEM CUTOUTS, ALL MESSAGES CLEARED. FOUND TO BE TRANSITORY. REVIEWED DATA. TROUBLESHOT AND DETECTED PITCH TRIM WIRES FROM HS-ACE PENov 6, 2019 · N117HQ · Emb ERJ170200LRSDR AALA201910029015Unknown · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS INFLIGHT F/O SIDE STICK WHEN ROLLING TO THE RIGHT, THERE IS NO RESPONSE FOR 1/2 OF SIDE STICK MOVEMENT, LEFT ROLL IS NORMAL. MAINTENANCE ACCOMPLISHED POST FLIGHT REPORT, NO FAULTS MESSAGES OR WARNINGS. ACCOMPLISHED OPERATIOct 1, 2019 · N139AN · Airbus A321231SDR O2GA2019092489101Actuator · lack of lubeAT ALTITUDE ALL 3 TRIM WHEELS BECAME VERY RIGID AND DIFFICULT TO ROTATE. 'AP HOLDING ND' AND 'MISTRIM' ANNUNCIATOR ILLUMINATED. DIVERTED TO SMF. ON DESCENT TRIM WHEELS FREED UP. MAINTENANCE INSPECTED ELEVATOR, AILERON AND RUDDER TRIM ACTUATORS FOR MOISTURE. NOSep 19, 2019 · N891UP · Beech B300SDR FDEA2019081541879Unknown · unknownIN DECENT FROM FL340 TO 14000, CLEAN CONFIG, PASSING APPROX FL 190 A/C PITCHED NOSE DOWN TO APPROX 9, AIRSPEED STARTED TO INCREASE INTO ZIPPER APPROX 5 KTS FOR 5 SEC UNTIL AP WAS DISCONNECTED AND SPEEDBRAKES DEPLOYED. INSPECTED AIRCRAFT NO ABNORMALITIES Aug 14, 2019 · N977FD · Boeing 757236SDR AALA2019081429020Unknown · vibrationAIRCRAFT NOT GROUNDED: PILOT REPORTS APPROX. 1500 FT AGL, A/C FULLY CONFIGURED FLAPS FULL 143 KNOTS, MEDIUM TO SEVERE VIBRATION IN RUDDER PEDALS. ON LDG FELT LIKE RUDDER MADE UNCOMMANDED MOVEMENT. NO FAULTS NOTED. PERFORMED RUDDER CONTROL ADJUSTMENTS AND TESTAug 11, 2019 · N163US · Airbus A321211SDR CALA2019072901277Accelerometer · inoperativeAIRCRAFT CLIMBS UNLESS FORWARD PRESSURE IS KEPT ON STICK. NOT NORMAL SEE TSM TASK 27-30-00-810-853-A, PFR SHOWS ACCLRM 4 12CE4 FAILED. TOMC RECOMENDS REPLACING 12CE3 AND 12CE4 REMOVED #3 AND #4 FLIGHT CONTROL ACCELEROMETER 27-92-16 REPLACED BOTH FLT CONT ACCELJul 29, 2019 · N895UA · Airbus A319132SDR 2019FA0000210Turnbuckle · crackedWHILE RETENSIONING THE LOWER STABILATOR TURN BUCKLE AFTER STABILATOR REPLACEMENT THE AFT CABLE END APPEARED BENT. CLOSE INSPECTION SHOWED A CRACK AND PARTIAL PARTING OF THE SWAGED CABLE END. THE CRACK WAS BETWEEN THE THREADS AND SAFETY WIRE HOLE IN THE AREA Jun 21, 2019 · N181WM · Piper PA28180SDR AALA2019061979017Battery · no testAIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS FLY-BY-WIRE BACK-UP BATTERY FAILS FUNCTIONAL TEST. REMOVED AND REPLACED FLY-BY-WIRE BACK-UP BATTERY IAW AMM 27-03-05. OPS CHECK GOOD.Jun 16, 2019 · N944UW · Emb ERJ190100IGWSDR CA190613007Reu · failed(CAN) THE FBW SUPPLIER HAS IDENTIFIED A LACK OF MONITOR COVERAGE TO ADDRESS FAILURE MODES ON THE EHSV LVT SENSOR. AS SUCH, WITH THE CURRENT FBW SYSTEM, THE EHSV POSITION SENSING PATH (LVT) CAN FAIL IN A MANNER THAT IS NOT DETECTABLE (DORMANT). THIS EHSV LVT SEJun 13, 2019 · BombdrSDR CA190607008Control Unit · malfunctioned(CAN) FLT CTRL FAULT AFCU INOP DURING CLIMB CREW HAD FLIGHT CONTROL ADVISORY POST ON EICAS DURING CLIMB - FLIGHT CREW HAD ADVISORY - FLT CTRL FAULT WITH INFO 27 FLT CTRL FAULT AFCU INOP AND MAINTENANCE MESSAGE - HSTA (MPE1) POSITION SENSOR 3 RVDT ELECTRICAL FJun 6, 2019 · Airbus BD5001A11SDR CA190614011Flt Controls · binding(CAN) THE CREW NOTED THE FLIGHT CONTROLS WERE EXTREMELY STIFF ABOUT PITCH AND ROLL AXIS WITH OR WITHOUT AIR LOAD. THE AIRCRAFT HYDRAULIC PRESSURE SHOWED NORMAL IN ALL THREE SYSTEMS. UPON LANDING THE FLIGHT CREW VERIFIED THE PROBLEM PERSISTED WITHOUT AIR LOADJun 3, 2019 · Cndair CL604SDR CA190603009Control Unit · inoperative(CAN) PILOT REPORTED A AFCU INOP AFCU REPLACED. TESTED AND AIRCRAFT BACK IN SERVICE.Jun 2, 2019 · Airbus BD5001A11SDR AALA201905179002Unknown · vibrationAIRCRAFT NOT GROUNDED: PILOT REPORTS ON APPROACH, GEAR DOWN, FLAPS 25, SPEED (IAS) APPROX. 140-145 KT, WHEN CONTROL WHEEL TURNED LEFT, BUFFET FELT ON RIGHT SIDE OF AIRCRAFT. MAINTENANCE PERFORMED SATISFACTORY INSPECTION AND OPERATIONAL CHECK OF FLAPS/AILERONS/May 16, 2019 · N379AA · Boeing 767323SDR 2019FA0000152Control Cable · crackedFLIGHT CONTROL CABLE FOUND CRACKED DURING ANNUAL INSPECTION. AD 2013-02-13/ SB 1245A PREVIOUSLY COMPLIED WITH. 2000 HOUR 7-YEAR INSPECTION NOT DUE AT THE TIME THE CRACK WAS FOUND. CRACK BECAME EVIDENT WHEN A SLIGHT BENDING LOAD WAS PLACED ON THE CONTROL CABLEMay 14, 2019 · N2172G · Piper PA32300SDR 2019FA0000151Control Cable · crackedFLIGHT CONTROL CABLE FOUND CRACKED DURING ANNUAL INSPECTION. AD 2013-02-13/ SB 1245A PREVIOUSLY COMPLIED WITH. 2000 HOUR 7-YEAR INSPECTION NOT DUE AT THE TIME THE CRACK WAS FOUND. CRACK BECAME EVIDENT WHEN A SLIGHT BENDING LOAD WAS PLACED ON THE CONTROL CABLEMay 14, 2019 · N2172G · Piper PA32300SDR 2019FA0000150Control Cable · crackedFLIGHT CONTROL CABLE FOUND CRACKED DURING ANNUAL INSPECTION. AD 2013-02-13/ SB 1245A PREVIOUSLY COMPLIED WITH. 2000 HOUR 7-YEAR INSPECTION NOT DUE AT THE TIME THE CRACK WAS FOUND. CRACK BECAME EVIDENT WHEN A SLIGHT BENDING LOAD WAS PLACED ON THE CONTROL CABLEMay 14, 2019 · N8193B · Piper PA32R300SDR SWAA2019050632317Switch · faultyAIR TURNBACK, ON TAKEOFF MASTER CAUTION LIGHT ILLUMINATED WITH STANDBY RUDDER ON LIGHT ILLUMINATED. R&R SWITCH PER AMM.May 4, 2019 · N710SW · Boeing 7377H4SDR SWAA2019050632316Control Panel · faultyAIR TURNBACK, ON TAKEOFF MASTER CAUTION LIGHT ILLUMINATED WITH STANDBY RUDDER ON LIGHT ILLUMINATED. R&R FLIGHT CONTROL PANEL PER AMM.May 4, 2019 · N710SW · Boeing 7377H4SDR DJFA20190503001Fcu · malfunctionedDURING DESCENT RECEIVED FLAP FAIL, PTRIM BKP FAIL, SWPS FAULT, AND SPOILER FAULT CAS MESSAGES. REMOVED AND REPLACED FCE NR 1 IAW MM 27-03-01. COMPLIED WITH RIGGING OF THE FLAP SYSTEM AND FLAP SYSTEM OPERATIONAL CHECK IAW MM 27-50-00. COMPLIED WITH PITCH TRIMMay 3, 2019 · N354FX · Emb EMB505SDR CHIA201904298889Bolt · brokenLONGITUDINAL RIGID LINK AFT BOLT ON FORWARD HEAD WAS MAKING WEAR DUST/GREASE FROM THE BOLT HEAD. PROCEEDED TO REMOVE THE BOLT, AND WHEN THE TECHNICIAN STARTED TO LOOSEN THE BOLT, THE HEAD SNAPPED OFF. REMOVED THE REST OF THE REMAINING HARDWARE AND REPLACED WITApr 28, 2019 · N188CH · Boeing 1072SDR CA190417010Flt Controls · malfunctioned(CAN) CREW REPORTS HAVING ISSUES IN CONTROLLING THE AIRCRAFT ON CLIMB OUT PASSING FL100, DECLARED EMERGENCY AND RETURN TO DEPARTING FIELD. AIRCRAFT LH AND RH WING TOUCHING THE RUNWAY PRIOR TO HARD LANDING.Apr 16, 2019 · Bombdr BD7001A10SDR HALA2019041820190Sensor · faultedETOPS - BTB FLT CONTROL SENSOR FAULT ECAM // T/S PER A330 TSM 27-93-00. GROUND SCAN FAULTED FCPC2. SWAPPED POSITIONS FCPC2 W/FCPC3, FAULT DID NOT FOLLOW. AFTER RESETS OF PRIM 1+2, SEC'S AND DOWN POWER A/C MSG CLEARED AND GROUND SCAN ECPC'S BOTH SHOW NO FAULTApr 12, 2019 · N395HA · Airbus A330243SDR A6WA2019040446528Unknown · unknownON APPROACH, THE AIRCRAFT EXPERIENCED AN UN-COMMANDED YAW MOTION. THE FLIGHT CREW REFERENCED THE QRH, STABILIZED THE AIRCRAFT, CONTACTED ATC AND DISPATCH, DECLARED AN EMERGENCY AND DIVERTED.Mar 31, 2019 · N431AW · Cndair CL6002B19SDR DJFA2019041722001Control Unit · failedBACKUP PITCH TRIM FAIL CAS MESSAGE ON PDFS. POWERED AIRCRAFT DOWN AND BACKUP, MESSAGE STILL THERE ON PDFS. REMOVED AND REPLACED #1 FCE AND ACCOMPLISHED ELECTRONIC RIGGING PROCEDURE. ACCOMPLISHED IAW PHENOM 300 AMM 27-03-00. OPS CHECKS GOOD IAW PHENOM 300 AMM 2Mar 22, 2019 · N351FX · Emb EMB505SDR IU6R2019031502Manifold · corrodedMALFUNCTION: CORROSION ON THE SEAL SURFACE. PROBABLE CAUSE: FLUID OTHER THAN SPECIFIED GETTING IN AFFECTED AREA. RECOMMENDATION: MAKE SLEEVES FOR MANIFOLD OR OTHER MATERIAL THAT WON’T BE AFFECTED.Mar 14, 2019 · N626 · Boeing 737SDR IU6R2019031501Manifold · corrodedMALFUNCTION: CORROSION ON THE SEAL SURFACE. PROBABLE CAUSE: FLUID OTHER THAN SPECIFIED GETTING IN AFFECTED AREA. RECOMMENDATION: MAKE SLEEVES FOR MANIFOLD OR OTHER MATERIAL THAT WON’T BE AFFECTED.Mar 14, 2019 · N626N · Boeing 737SDR E07A201902270001Trim System · malfunctionedDESCENDING THROUGH APPROXIMATELY 10,000’ CREW RECEIVED A AP ROLL MISTRIM. CREW CORRECTED THE TRIM BASED ON THE ARROW IN THE TRIM WINDOW OF THE MFD AND SHORTLY THERE AFTER CREW RECEIVED YAW MISTRIM CAS. THESE TRIM CAS MESSAGES BECAME MORE IN MORE FREQUENT OVER Feb 26, 2019 · N362AS · Emb EMB505SDR NI6R201902280053Control Rod · crackedA CRACK WAS DISCOVERED IN THE FERRULE OF ROD PN B6037-330. AN INSPECTION OF OUR FLEET (9 AIRCRAFT) FOUND A TOTAL OF 10 PN B6037-330 RODS WITH CRACKED FERRULES. THE ROD IS PART OF THE ROLL SPOILER SYSTEM. THE AIRCRAFT MANUFACTURER ISSUED SB27-140 ORIGINALLY IFeb 22, 2019 · Bac 146200A
Back to JASC 2700