JASC 2720
Service difficulty reports · 3,131
Reports filed under 2720 · Rudder 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 = '2720' 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 = '2720' 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 MASA200601600Pressure Switch · failedASH 7332 PIT - RUDDER SYSTEM 1 AND 2 INOPERATIVE EICAS MESSAGE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 RUDDER PRESSURE SWITCH.SDR MASA200601598Pressure Switch · failedASH 7211 IAD - RUDDER SYSTEM 1 AND 2 INOPERATIVE AND YAW DAMP FAIL. MAINTENANCE REMOVED AND REPLACED NR 2 RUDDER PRESS SWITCH.SDR DJFA2006262Rudder Pedal · stuckTRIP ID NR 1032333, FOLLOWING TAKEOFF AND DURING CLIMB CRUISE AND DESCENT BOTH PILOT AND CO-PILOT RUDDER PEDALS COULD NOT BE MOVED MORE THAN APPROXIMATELY 2 INCHES AND MOVING THE PEDALS REQUIRED A LARGE AMOUNT OF FORCE. BOTH THE AUTO PILOT AND YAW DAMPER SYSSDR MASA200601592Warning System · malfunctionedASH 6185 OKC - RUDDER LIMIT FAULT. CONTRACT MX PERFORMED SPOST 1/2. NO FURTHER DEFECTS NOTED.SDR 2006FA0000674Spring · brokenFLIGHT INSTRUCTOR WAS DEMO-ING A STALL TO STUDENT. MANUVER STARTED AT 2700 FT. CONTROLS LOCKED UP- AC WENT NOSE DOWN. FLT INST RECOVERED AT 700 FT. (K)SDR MASA200601589Rudder · malfunctionedASH 7290 IAD - RUDDER SYSTEM NR 1 AND NR 2 INOP. MX RESET SYSTEM. OP'S CHECK GOOD.SDR MASA200601573Warning System · malfunctionedASH 6128 LAS - CAPTAIN REPORTED RUDDER LIMIT FAULT STATUS MSG. MX PERFORMED S-POST. ACFT CONTINUED OPERATIONS.SDR MASA200601557Warning System · malfunctionedASH 6580 LAS - RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR 0609200601Control Unit · failedAPPROXIMATELY ONE HOUR AFTER DEPARTURE FROM ELIX, NR 3 HYD SYSTEM LOSS. AS PER CHECK SHEET NR 3 EDP TO -SUPPLY OFF-, NR 3 ENGINE RUNNING. RETURN TO ELIX, NO FURTHER INCIDENT. FOUND INOPERATIVE RUDDER POWER CONTROL ASSY. REMOVED INOPERATIVE UNIT, AND REPLACSDR MASA200601546Warning System · malfunctionedASH 7136 DEN - RUDDER LIMIT FAULT MESSAGE. MX RESET THE SYSTEM. OP'S CHECK GOOD.SDR MASA200601547Warning System · malfunctionedASH 6294 PHX - RUDDER LIMIT FAULT STATUS MESSAGE. MX PERFORMED SPOST TEST. OP'S CHECK GOOD.SDR MASA200601533Warning System · malfunctionedASH 5054 CLT - RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET THE SYSTEM.SDR MASA200601532Computer · malfunctionedASH 7141 IAD - RUDDER HAD OVER PROTECTION FAIL MESSAGE. MX RESET THE FADEC.SDR DL76L060472Warning Message · pilot errorRUDDER RATIO MESSAGE APPEARED AFTER ENGINE START - RTB. L RUDDER RATIO MODULE FOUND IN TEST MODE. CLEARED FAULT BALLS RAN RUDDER FULL DEFLECTION. ALL CHECKS GOOD.SDR ZLWA0601Servo · failedON TAKEOFF RUDDER OSCILLATES WHEN YAW DAMPNER ENGAGED.SDR MASA200601525Warning System · malfunctionedASH 6119 PHX - RUDDER LIMIT FAULT. MX RESET SYSTEM. OP'S CHECK WAS GOOD. ACFT CONTINUED OPERATIONS.SDR MASA200601516Actuator · malfunctionedASH 5093 CLT - RUDDER LIMIT FAULT STATUS MESSAGE. MX REPLACED THE RTL ACTUATOR.SDR CA070502013Control Cable · broken(CAN) THE BOLT THAT ATTACHES THE LT FORWARD RUDDER CABLE TO THE RUDDER PEDAL SETUP WAS ORIGINALLY TOO TIGHTLY DONE UP. THE CABLE ATTACHMENT FORK WAS NOT ABLE TO MOVE FREELY ON END, IN THE FORK, AND BREAK UNDER LOAD. (TC NR 20070502013)SDR MASA200601485Status Message · false activationASH 7405 MEM - RUDDER LIMIT FAULT STATUS MESSAGE. PERFORMED S-POST. OP'S CHECK GOOD.SDR MASA200601479Warning Light · false activationASH 6433 PHX - RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR MASA200601465Warning System · malfunctionedASH 6092 SAT - RUDDER LIMIT FAULT. PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR 2006FA0000568Spring · looseTHIS HAS TO DO WITH RUDDER CENTERING BUNGEES OR SPRINGS THERE IS ONE ON BOTH SIDES OF THE RUDDER. AFTER FLT, MECHANIC NOTICED SOME PARTS SETTING ON RUDDER HORN AS IF THEY HAD BEEN REMOVED AND PUT THERE, AN INSP OF RUDDER, IT WAS DETERMINED THAT THEY FELL OFFSDR CA060608010Channel · brokenPILOTS REPORTED THAT WHEN THE RUDDER PEDALS ARE BOTH PUSHED, THE CO-PILOT'S INSTRUMENT LIGHTS DIM. INVESTIGATION REVEALED THAT THE PILOT'S RUDDER SUPPORT BRACKET WAS BROKEN AT THE TOP OF THE ATTACH CHANNEL. THE CO-PILOTS INSTRUMENT LIGHT RHEOSTAT WAS ALSO DASDR MASA200601444Transmitter · failedASH 7141 IAD - AIRCRAFT HAS NO EICAS RUDDER INDICATION. MAINTENANCE REMOVED AND REPLACED TRNASMITTER.SDR AWXA200600881Control Servo · out of tolerancePHX - VIB - FLT# 771 - ON CLIMB-OUT AT SPEEDS GREATER THAN 300KTS IAS, HAD LIGHT TO MODERATE AIRFRAME VIBRATION FELT BY ALL CREW MEMBERS. WENT AWAY LESS THAN 300 KTS. ALL ENG PARAMETERS NORMAL. ALL VIBRATION READINGS LESS THAN 1.0 EACH ALERT MOC AT 2150Z. SDR MASA200601401Status Message · illuminatedASH 6551 PHX - RUDDER LIMIT FAULT STATUS MESSAGE. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR MASA200601397Warning System · false activationASH 7277 BOS - RUDDER HARDOVER PROTECT FAIL. MX RESET SYSTEM. OP'S CHECK GOOD.SDR FDKA200605101Control Module · malfunctionedMAINTENANCE REPORTED RUDDER SYSTEM 2 WILL NOT SWITCH OFF WITH HYDRAULICS ON. MAINTENANCE REMOVED AND REPLACED FLIGHT CONTROL MODULE ASSY, OPS CHECKED GOOD.SDR MASA200601385Warning System · false activationASH 7340 PIT - RUDDER HARDOVER PROTECTION FAIL MESSAGE. MX DID A ELECTRICAL RESET. OP'S CHECK GOOD.SDR FDKA200605096Rudder · malfunctionedTHE CREW REPORTED THAT THE RUDDER SYSTEM 2 WON’T SHUT OFF WITH HYDRAULICS ON. MAINTENANCE RESET THE SYSTEM AND OPS CHECKED.SDR MASA200601377Limiter · malfunctionedASH 5058 GSO - RUDDER TRAVEL LIMITER FAULT. MX RESET SYSTEM. OP'S CHECK GOOD.SDR MASA200601375Controller · malfunctionedASH 7141 IAD - RUDDER HARD OVER PROTECTION FAIL MESSAGE. MX RESET THE FADEC.SDR MASA200601362Warning Message · false activationASH 7243 IAD - THE CAPTAIN ABORTED THE TAKEOFF DUE TO A CONFIG RUDDER EICAS MESSAGE ON TAKE OFF. UPON RETURNING TO THE GATE THE CAPTAIN CONTACTED MX CONTROL AND REPORTED THE RUDDER HAD BEEN BUMPED CAUSING THE CONFIG RUDDER MESSAGE. MX PERFORMED AN OPERATIONASDR HALA0600386Warning System · malfunctionedBTB, DUE TO RUDDER RATIO LIGHT ILLUM ON GROUND EICAS MSG RUDDER RATIO DISPLAYED. PERFORMED FIM 27-21-00. FOUND BOTH PCA FAULT BALLS ON RUDDER RATIO MODULES. CLEARED FAULT BALLS. PERFORMED FIM 27-09-00, RUDDER RATIO SYS OPS NORMAL, MSG EXTINGUISHED, NO FAULSDR FDKA200605091Warning System · malfunctionedTHE CREW REPORTED A RUDDER HARD OVER PROTECTION MESSAGE ON EICAS. MAINTENANCE RESET WITH THE CREW.SDR SIMA200613601Bushing · wornCLIMBING THROUGH 27,000 FT AT .56 MACH VIBRATION IN YOKE WITH OR WITH OUT AUTOPILOT ENGAGED. THROUGH 16,000 FEET AT 250KTS THE VIBRATION SUBSIDED DURING DESCENT. THE VIBRATION SEEMED TO BE ONLY FORWARD TO AFT ON YOKE. CREW TRIED DIFFERENT PITCH SETTINGS WITSDR QXEA200601256Check Valve · malfunctionedSEA - ON FLIGHT 2133, DIVERTED FROM SEA-EUG, TO PDX, NR 2 RUD HYDRAULIC CAUTION LIGHT WITH ASSOCIATED LIGHTS ON SHORT FINAL. MAINTENANCE, REMOVED AND REPLACED CHECK VALVE. SERVICED AND BLED NR 2 HYDRAULIC SYSTEM. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICSDR MASA200601315Warning System · malfunctionedASH 5025 PHX - RUDDER LIMIT FAULT STATUS MSG. MX PERFORMED S-POST TEST FAULT CLEARED. ACFT CONTINUED OPERATIONS.SDR 2006FA0000545Rudder Pedal · crackedSIGNIFICANT CORROSION NOTED AT HORIZONTAL BASE OF LEFT RUDDER PEDAL. RUDDER PEDAL CRACKED AND STARTED TO DEFORM SLIGHTLY IN THE VICINITY OF THE CRACK. THE RUDDER PEDAL IS PLATED AND THE CORROSION APPEARED TO HAVE STARTED FROM THE INSIDE BUT THE EXACT CAUSE HSDR 06FDEA1782Computer · faultedON T/O AT LAX, DID A RTO AT 90 KTS THE ECAM ALERT WAS BOTH PITCH 1/2 AND BOTH RUDDERS 1/2 FAULTED. REMOVED AND REPLACED NR 1 AND NR 2 FEEL LIMITATION COMPUTERS PER M/M 27-23-26-4. OPS CK'S NORMAL. PERFORMED AFTER BRAKE OVERHEAT INSP REF MM 05-51-16-0-01. SDR MASA200601307Warning Message · illuminatedASH 5048 CLT - RUDDER LIMIT FAULT STATUS. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR MASA200601284Warning System · malfunctionedASH 7222 IAD - RUD LIMIT FAULT STATUS MSG. MX RESET AND PERFORMED SPOST TEST. NO FURTHER ACTION REQURIED.SDR CA060517003Damper · leakingPILOT FELT A YAW ON APPROACH, AND AFTER CONFIRMING A YAW HARDOVER, SWITCHED OFF AUX HYDRAULICS, AND CONTINUED TO LAND. ON INSPECTION IT WAS FOUND THAT THE PEDAL DAMPER WAS LEAKING EXCESSIVELY DUE TO A BROKEN BOLT AND CAP.SDR MASA200601266Pcu · inoperativeRUDDER SYSTEM 1 INOPERATIVE. MX REPLACED THE PCU.SDR MASA200601226Warning Message · illuminatedHARD OVER RUDDER FAIL MESSAGE. MX RESET THE SYSTEM, OP'S CHECKED GOOD.SDR MASA200601225Pressure Switch · malfunctionedRUDDER PRESS ANNUNCIATOR DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE SWITCHES.SDR MASA200601207Warning System · malfunctionedASH 5041 SAV - RUDDER LIMIT FAULT STATUS FAULT. RESET DURING SPOST TEST NO FURTHER ACTION REQUIRED.SDR QXEA200601329Pressure Switch · malfunctionedPDX FLIGHT NR 2050 RUDDER FULL PRESSURE CAUTION. MAINTENANCE REPLACED PRESSURE SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR DL764060328Rudder Control · noisyDURING TAXI OUT, FLT CONT CHK WITH FULL RUDDER DEFLECTION, METALLIC CLANG IS HEARD IN F/OS RUDDER PEDAL BAY. INSTALLED RIG PIN IN RUDDER SYS FWD PERF STATIC RIG CHK OF RUDDER CONT SYS FROM FWD QUADRANT TO AFT QUADRANT. ALL RIG PINS INSTALL AT QUADRANTS. REMOSDR MASA200601164Warning System · malfunctionedASH 5057 LGA - CAPTAIN REPORTED RUDDER LIMIT FAULT STATUS MESSAGE. MX CONTROL PERFORMED SYSTEM RESET AND SPOST WITH FLIGHT CREW. OP'S CHECK GOOD.
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