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 CA050819008Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR XN0A1259Control System · malfunctionedDURING TAKEOFF, FLARE ROLL ELEVATOR CONTROL WAS VERY DIFFICULT TO MANEUVER THE AIRCRAFT. CARRIED OUT INSPECTION PER A300 FIM CHAPTER 27-31-00 FIGURE 101 SHEET NR 1 & 2 NO FAULTS FOUND. CARRIED OUT INSPECTION PER A300 AMM CHAPTER 27-33-14 & 27-33-00 OF THE ARTSDR DXTA200500905Actuator · failedRUDDER LIMIT FAIL A EICAS MESSAGE. CONTROL PAGE SHOWS 43 PERCENT RUD LIMIT. REMOVED UPPER RUDDER -A- LINEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED OVERHAULED UNIT. OPERATIONAL CHECK WAS GOOD. WORK WAS DONE IAW CE-750 MM 27-23-00.SDR DL764050455Lock · looseDURING TAKEOFF NOTICED CAPTAINS RUDDER PEDALS SHIFT FORWARD ABOUT AN INCH, NORMAL T/O. INSPECTED PEDAL MECHANISIM AND TIGHTEND LOCK. PDEAL NOW LOCKS INTO DESIRED POSITION.SDR SWIA200515436Bearing · wornAFTER PUSHBACK FROM SLC, HEARD AUDIBLE CLICKING SOUND AS WELL AS BUMPING FEEDBACK FROM PEDALS. REPLACED LEFT RUDDER PEDAL PIVOT BEARINGS AND PEDAL ADJUSTMENT YOKE. OPERATIONAL CHECK GOOD.SDR 2005UALA00820Flt Controls · malfunctionedTHREE UNCOMMANDED RUDDER MOVEMENTS ON APPROACH. MECHANICS PERFORMED CAT3 CHECKS PER AMM 22-11-00 PG 501, AMM 22-31-00 AND RUDDER ACTUATOR CONFIDENCE CHECK ON MAT, ALL OPS CHECKS NORMAL. ENGINEERING REVIEWED MAINTENANCE RECORDS AND DOWN LINKED CMC FAULT DATA SDR QXEA200501172Regulator · malfunctionedSEA - THE "RUD FULL PRESS" CAUTION LIGHT ILLUMINATED DURING CRUISE FLIGHT, FOLLOWED IMMEDIATELY BY THE "RUD PRESS" CAUTION LIGHT. COMPLETED EMERGENCY AND ABNORMAL CHECKLIST FOR BOTH LIGHTS. MAINTENANCE REPLACED RUD FULL PRESS SWITCHES NO HELP. TROUBLESHOT TO RSDR DXTA200500887Rudder · oscillatesUPPER RUDDER OSCILLATING FULL DEFLECTION WITH IN GREEN ARC AT HIGH SPEED LIMITS CHANGED FGC WITH NO CHANGE.SDR QXEA200501155Regulator · unknownPDX FLIGHT NR 2169 - RUDDER PRESSURE AND RUDDER FULL PRESSURE AT SPEEDS ABOVE 140 KTS. REPLACED RUDDER DUAL PRESSURE REGULATOR AND ACTUATOR ISOLATE SOLNOID VALVES FOR PRECAUTIONARY MEASURES. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.SDR MASA200500607Warning Light · false activationASH 6484 PHX - ELEVATOR SPILT CAUTION MESSAGE. MX RESET THE SYSTEM WITH THE HELP OF BOMBA REP AND ALL OPS CHECKS WERE GOOD.SDR DXTA200500877Yaw Damper · malfunctionedIN FLIGHT YAW DAMPER DOES NOT APPEAR TO OPERATE IN COORDINATION WITH FLIGHT CONTROLS. LAGS AND OVERCORRECTS. SEVERAL TIMES IN FLIGHT, BOTH ON AUTO-PILOT AND WHEN HAND FLOWN, YAW DAMPER APPEARS TO OPERATE UNCOMMANDED. OVERCOMPENSATING APPEARS WORSE ON B FGC.SDR QXEA200501145Pressure Switch · malfunctionedBOI FLIGHT NR 2204, RUDDER FULL PRESSURE CAUTION LIGHT AFTER TAKEOFF. THIS WAS ACCOMPAINIED BY A RUDDER PRESSURE CAUTION LIGHT. MAINTENANCE REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. GROUND RAN AIRCRAFT. OPERATED RUDDER THRU SEVERAL CYCLES. ALSO, C/SDR CA050727002Yaw Damper · leakingIN CRUISE, YELLOW HYD SYSTEM LEAK TURNED OFF ENG GREEN PUMPS 1 & 2. NO NOSE STEERING ON LANDING. FOUND HYD LEAK IN THS COMPT YAW DAMPER ACTUATOR 19CS1. REPLACED AS PER J/C 9-227L-01.SDR SWIA200515339Pedal · blockedRUDDER ON LANDING JAMMED ON RIGHT SIDE 1/4 TRAVEL ONLY. FOUND CAMLOCK ON RT SIDE OF CENTER CONSOLE OUT AND INHIBITING RUDDER PEDAL DEFLECTION. SECURED CAMLOCK AND RAN RUDDER PEDALS IN BOTH DIRECTIONS AT FULL DEFLECTION WITH NO DEFECTS NOTED.SDR DXTA200500860Fitting · loose"RUD STBY SYS FAIL" CAS MESSAGE ILLUMINATED TWICE IN FLIGHT. RSS PRESSURE FLUCTUATED 2200 TO 3800 PSI. DUPLICATED SQK ON GROUND. FOUND RUDDER STANDBY ACCUMULATOR PRESSURE LOW SERVICED ACCUMULATOR IAW 750 MM CHAP 12-10-16. TIGHTENED LOOSE FITTING ON ACCUMULSDR QXEA200501131Regulator · malfunctionedSEA FLIGHT NR 2180, AFTER TAKEOFF, NR 2 RUDDER HYDRAULIC PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE RUDDER DUAL PRESSURE REGULATOR IAW -8(200) AMM 27-20-38, PAGES 40-405. PERFORMED OPERATIONAL TEST. NO DEFTECTS NOSDR CLC2005F00003Control Cable · corrodedDURING PREFLIGHT, FOUND RUDDER NOSE RIGHT CABLE 2D BROKEN. FOUND RT RUDDER CONTROL CABLE 2D CORRODED AND BROKEN. REMOVED AND REPLACED RUDDER CONTROL CABLE NOSE RT 2D IAW AMM. ACCOMPLISHED RUDDER CONTROL SYSTEM OPERATIONAL, CHECK AND FOUND NORMAL. AIRCRAFT SDR MASA200500554Pressure Switch · failedA RUDDER SYS 1-2 INOP EICAS MESSAGE. MX REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. NO FURTHER DEFECTS NOTED.SDR COMA0560393Trim Switch · malfunctionedFLIGHT 5662- RUNAWAY RUDDER TRIM. REPLACED THE TRIM SWITCH PANEL.SDR DXTA200500843Strut · inoperativeRUDDER BIAS ACTIVATES WITH BOTH POWER LEVERS AT T/O POWER. GOT FULL RIGHT DEFLECTION OF THE RUDDER, ABORTED AT 50 KTS. - REMOVED AND REPLACED RIGHT HAND RUDDER BIAS STRUT PERFORMED FUNCTION TEST. FUNCTION TESTED GOOD ALL WORK PERFORMED IAW HAWKER 800XP MM 27-SDR SWIA200515288Transmitter · inoperativeAFTER ENGINE START, RUDDER INDICATION SHOWED NO MOVEMENT DURING TEST. REPLACED RUDDER POSITION TRANSMITTER IAW CRJ MM 27-24-05. OPERATIONAL CHECK GOOD.SDR DXTA200500836Bungee Cord · stiffAFTER DEPARTURE, FULL RUDDER TRIM TO LT REQUIRED IN ORDER TO KEEP ACFT COORDINATED. CLIMBING THRU FL 200 AT 250 KIAS, RUDDER KICKED BACK TO NORMAL. HAD TO TRIM RUDDER BACK TO CENTER. OPS CK OF RUDDER SYSTEM ON GROUND REVEALED NO DEFECTS. REMOVED ACCESS PANESDR DXTA200500832Rudder · malfunctionedON TAKEOFF ROTATION ACFT YAWED HARD TO LEFT. INSPECTED RIGGING OF RUDDER AND RUDDER TRIM SYSTEM. CHECKED CABLE TENSIONS AND TRAVELS. CHECK GOOD. INSPECTED RUDDER BIAS SYSTEM. OPS CHECKED GOOD. NO DEFECTS NOTED IAW C560XL MM 27-20-05.SDR DXTA200500828Actuator · failedRUDDER LIMIT FAIL -B- CAS MESSAGE ILLUMINATED DURING FLIGHT. RUDDER LIMIT WAS 28 PERCENT T/S TO BAD ACTUATOR REMOVED AND REPLACED LOWER RUDDER LIMIT ACTUATOR SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 750 M/M 27-23-00.SDR DXTA200500827Actuator · failedAMBER "RUB LIMIT FAIL B" CAS MESSAGE WITH A AMBER "RUDDER LIMIT 18%" MESSAGE IN EICAS CNTRL POSITION PAGE. EVENT MARKER PUSHED. COULD NOT DUP FLT CREWS DISCREPANCY ON ARRIVAL. RANG OUT WIRING FROM LOGIC MODULE TO LWR RUDDER LIMIT ACT WITH NO DISCREPANCYS FOUNSDR ASMF200507002Pseu · failedAIRCRAFT RETURNED TO PLATFORM DUE TO RUDDER TRAVEL UNRESTRICTED, FLAP SLAT DISAGREE AND BOTH MAIN LANDING GEAR RED LIGHTS TURNED ON. BITE TO SWC AND PSEU PERFORMED, NOT CONFIRMING FAILURE. TECHNICAL PERSONNEL SENT TO STATION AND PSEU REPLACED IAW MM 32-60-04,SDR SWIA200515244Transmitter · malfunctionedON PUSHBACK LOST RUDDER INDICATION ON EICAS. REPLACED RUDDER POSITION CONTROL TRANSMITTER IAW MM 27-24-05 OF THE MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD.SDR SWAA051940Connector · faultyDIVERSION/DECLARED EMERGENCY. RUDDER TRIM FAILED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR CONNECTOR PER MM.SDR DXTA200500809Control Cable · shearedLT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PEDAL AND FIREWALL. FOUND RUDDER CONTROL CABLE ASSY (UPPER) BROKEN AT 9 O' CLOCK POSITION. REPLACED RSDR DXTA200500834Actuator · failedRUD LIMIT FAIL B AMBER CAS MESSAGE IN CRUISE FLIGHT, FAILED AT 18%. INSTALLED OVERHAULED LWR RUDDER TRAVEL LIMITER ACTUATOR IAW 750 M/M 27-23-00, AND 27-20-00-720. OPS CHECK GOOD.SDR SWIA200515190Actuator · malfunctionedRUDDER LIMIT FAULT MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. P/N OFF BA620-93490-3, S/N OFF 0535.SDR SWIA200515187Pulley · obstructedLEFT RUDDER BINDS. REMOVED DEBRIS FROM AFT LEFT RUDDER PULLEY, OPERATIONAL CHECK GOOD IAW 27-21-00.SDR 2005FA0001001Control Cable · wornLT FORWARD RUDDER CABLE WORN AT FAIRLEAD PASSING THROUGH CENTER WING SPAR AT FS 108.17. THE CABLE BECAME WORN DUE TO CONTINUOUS CHAFING ON THE PHENOLIC FAIRLEAD. THE CABLE IS NOT CENTER IN THE FAIRLEAD OPENING EITHER THROUGH IMPROPER POSITIONING OF THE FAIRLSDR 2005FA0000881Control Cable · frayedLEFT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000880Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT AFT PULLEYS.SDR 2005FA0000884Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000879Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT AFT PULLEYS.SDR 2005FA0000885Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000878Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT AFT PULLEYS.SDR 2005FA0000877Control Cable · frayedLEFT RUDDER CABLE FOUND FRAYED AT AFT PULLEY. RIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000858Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000865Control Cable · frayedLEFT CABLE FOUND FRAYED AT AFT PULLEY. RIGHT CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000857Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.SDR 2005FA0000876Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT AFT PULLEYS.SDR 2005FA0000855Control Cable · frayedLEFT AND RIGHT RUDDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEYS.SDR 2005FA0000875Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEYS.SDR 2005FA0000854Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEY POSITIONS.SDR 2005FA0000851Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLLEY POSITIONS.SDR 2005FA0000850Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEY POSITIONS.SDR 2005FA0000883Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEY POSITIONS.
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