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.

SDR SWIA200110337Control Cable · wornRIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF THE WING BOX IS WORN NEAR LIMITS. REPLACED RIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF WING BOX IAW EMB120 MM 27-00-01.Oct 22, 2001 · N565SW · Emb EMB120ERSDR COMA0160832RudderFLIGHT #5775 - CONFIG RUDDER WARNING DURING T/O.C.N.D. NO CONFIG WARNING WITH T/O POWER.Oct 21, 2001 · N954CA · Cndair CL6002B19SDR COMA0160827Trim Switch · faultyFLIGHT #5280. DURING CRUSIE FLIGHT DESTINATION CVG, THE STABILIZER AND MACH. TRIM CAUTION MESSAGES ACTIVATED, CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT.REPLACED THE CAPTIANS PITCH TRIM SWITCH.Oct 18, 2001 · N796CA · Cndair CL6002B19SDR COMA0160824RudderFLIGHT 5412. DURING CRUISE FLIGHT ABOVE 280 KNOTS, THE AIRCRAFT ENCOUNTERED UNCOMMANDED RUDDER MOVEMENTS.PERFORMED ON OPERATIONAL CHECK OF THE YAW DAMPER SYSTEM, INCLUDING SVL-4000 COMMAND AND FEED BACK TEST. DISCREPANCY COULD NOT BE DUPLICATED.Oct 18, 2001 · N971CA · Cndair CL6002B19SDR MWEA011401Tab · debondedRUDDER TAB, FIXED TAB IS DEBONDED AT LEFT LOWER END. -- REMOVED AND REPAIRED FLAME SPRAY AND INSTALLED RUDDER CONTROL TAB.Oct 17, 2001 · N601ME · Doug MD88SDR ACE1016011Bracket · frozenPILOT REPORTED RUDDER FROZEN IN FLT. UNEVENTFUL LANDING. MAINTENANCE INITIALLY CONFIRMED THE RUDDER COULD NOT BE MOVED, THEN IT FREED UP. REMOVED CARGO COMPARTMENT FLOOR AT CARGO DOOR AND OBSERVED WATER FROZEN AROUND RUDDER CABLE PULLEYS AT FUSELAGE STA 495Oct 16, 2001 · N4632C · Cessna 170BSDR CA021114007Control Cable · frayed(CAN) LT AND RT RUDDER CABLES FRAYED AT CABIN PULLEY. BOTH CABLES MADE OF STAINLESS STEEL.Oct 10, 2001 · Bbavia 8GCBCSDR SWIA200110287Control Cable · wornRIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES WORN FORWARD OF WING BOX AT CABIN AREA. REPLACED RIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ERSDR SWIA200110283Control Cable · wornLEFT AND RIGHT OUTBOARD AND INBOARD RUDDER CABLES IN TAIL WORN AT PRESSURE SEAL. REPLACED RUDDER CABLES IAW EMB120 MM 27-00-01.Oct 4, 2001 · N218SW · Emb EMB120ERSDR MALA010748Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, LT FUSELAGE CIRCUIT I AFT RUDDER CABLE CHAFED. MAINTENANCE REPLACED LT CIRCUIT I AFT RUDDER CABLE P/N 7227105-582 IAW SF340 AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR MALA010749Control Cable · chafedDURING 4K-CHECK IN CWA, MAINTENANCE FOUND LT O/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MX REPLACED LT O/B CIRCUIT I DUAL RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR MALA010750Control Cable · chafedLT I/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE REPLACED LT I/B CIRCUIT I RUDDER CABLE P/N 7227105-571 IAW SF340 AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR MALA010753Control Cable · chafedDURING 4K- CHECK IN CWA, DISCOVED RT CIRCUIT I AFT SINGLE RUDDER CABLE CHAFED. MAINTENANCE REPLACED CIRCUIT I AFT SINGLE RUDDER CABLE REPLACED P/N 7227105-582, IAW SF340AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR MALA010754Control Cable · chafedRT I/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE INSTALLED RT I/B DUAL CIRCUIT I RUDDER CABLE P/N 7227105-571 IAW SF340AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR MALA010755Control Cable · chafedRT O/B CIRCUIT I DUAL FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE INSTALLED NEW RUDDER RT O/B CIRCUIT I FUSELAGE CABLE. P/N 7227105-562 IAW SR 340 AMM 27-21-25-4.Oct 4, 2001 · N99XJ · Saab SF340ASDR CA021114005Control Cable · frayed(CAN) LT AND RT RUDDER CABLES FRAYED AT CABIN. PULLEY CABLES MADE FROM STAINLESS STEEL.Oct 2, 2001 · Bbavia 8GCBCSDR CA011120003Cable · frayed(CAN) BOTH LT AND RT CABLES FRAYED JUST INCHES FWD OF BAGGAGE COMPARTMENT PULLEYS.Oct 2, 2001 · Bbavia 8GCBCSDR UPS01237063Structure · corrodedINSPECTION TYPE:C SUSPECT CORROSION ON AFT RUDDER CONTROL QUADRANT. REPAIR CARRIED OUT IAW MM 27-20-71, 27-20-00 & DRW 65-20879.Oct 2, 2001 · N913UP · Boeing 72762CSDR CA011018014Tube · cracked(CAN) TUBE CRACKED FROM BOLT HOLE TO LOWER EDGE OF TUBE.Sep 28, 2001 · Cessna U206GSDR 2001FA0000353Control Cable · looseROUTINE ANNUAL INSPECTION REVEALED AFT RUDDER CABLE THIMBLE EYES WERE LOOSE IN THE LOOP AT THE ATTACHMENT TO THE RUDDER. THE THIMBLE COULD BE REMOVED FROM THE LOOP. THE NICROPRESS CRIMP WAS MADE TOO FAR FROM THE THIMBLE. REPLACED THE RUDDER CABLES WITH NEW ONESep 28, 2001 · N25AP · Rhnflu EA300LSDR AUS20011092Servo · faulty(AUS) YAW DAMPER SERVO FAULTY. DUST COVER OVER THE MOTOR COLLECTING WATER (CONDENSATION). THE MOISTURE DRAIN HOLE IS LOCATED AT THE 12 O'CLOCK POSITION INSTEAD OF THE 6 O'CLOCK POSITION. AS A RESULT THE SERVO MOTOR IS BADLY CORRODED AND BURNT.Sep 25, 2001 · Piper PA46500TPSDR MALA010734Control Cable · chafedDURING 4K-CHECK IN CWA, FOUND LT I/B FWD FUSELAGE RUDDER CIRCUIT 1 CABLE CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE RUDDER PN 7227105-571 CIRCUIT 1 CABLE IAW SF3 AMM 27-21-25.Sep 22, 2001 · N110XJ · Saab SF340ASDR MALA010733Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B RUDDER SYSTEM CABLE OF DUAL CIRCUIT IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT O/B DUAL CIRCUIT CABLE PN 7227105-562 IAW SF340 AMM 27-21-25.Sep 21, 2001 · N110XJ · Saab SF340ASDR MALA010732Control Cable · chafedDURING 4K-CHECK IN CWA, FWD RT FUSELAGE RUDDER CIRCUIT AFT SINGLE CABLE IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT SINGLE AFT RUDDER CABLE PN 7227105-582 IAW SF340 AMM 27-21-25.Sep 21, 2001 · N110XJ · Saab SF340ASDR GTIA010873Arm · dirtyMACH TRIM INDICATION INOPERATIVE IN OVERRIDE WILL NOT RETRACT. CLEANED MACH TRIM ROCKER ARM, OPS CHECK GOOD IAW DC9 MM 27-20-1. (M)Sep 11, 2001 · N133NK · Doug DC932SDR MALA010714Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED LT O/B RUDDER CABLE P/N 7227105-562 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4.Sep 11, 2001 · N438XJ · Saab 340BSDR MALA010713Control Cable · chafedDURING 4K-CHECK IN CWA, LT RUDDER AFT SINGLE CABLE OF DUAL CIRCUIT I IS CHAFFED. MX REPLACED LT RUDDER AFT SINGLE CABLE CIRCUIT I P/N 7227105-582 IAW SF340 AMM 27-21-25-4.Sep 11, 2001 · N438XJ · Saab 340BSDR MALA010712Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT I/B RUDDER CABLE P/N 7227105-571 IAW SF340 AMM 27-21-25-4.Sep 11, 2001 · N438XJ · Saab 340BSDR MALA010711Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MX REPLACED RT O/B RUDDER CABLE P/N 7227105-562 OF DUAL CIRCUIT I IAW SF340 AMM 27-21-25-4.Sep 11, 2001 · N438XJ · Saab 340BSDR MALA010710Control Cable · chafedDURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MX REPLACED RT RUDDER SINGLE CABLE P/N 7227105-582 OF CIRCUIT I IAW SF340 AMM 27-21-25-4.Sep 11, 2001 · N438XJ · Saab 340BSDR MWEA011249Control Valve · out of adjON TAXI OUT, FLAP/RUDDER STOP INOP LIGHT ILLUMINATED, RETURNED TO GATE. SHIMMED AUX RUDDER THROW LIMITER CONTROL VALVE PER MM 27-20-0. OPERATIONS CHECK GOOD.Sep 8, 2001 · N501ME · Doug DC932SDR SWIA200110210Pulley · nickedAFT RUDDER RIGHT INBOARD CABLE PULLEY HAS NICK. REPLACED RIGHT AFT INBOARD CABLE AFT PULLEY.Sep 7, 2001 · N564SW · Emb EMB120ERSDR SWIA200110207Control Cable · wornRIGHT MID INBOARD AND OUTBOARD RUDDER CABLES WORN. RIGHT AFT INBOARD AND OUTBOARD RUDDER CABLES WORN. REPLACED RIGHT MID INBOARD, OUTBOARD AND AFT INBOARD, OUTBOARD RUDDER CABLES.Sep 7, 2001 · N564SW · Emb EMB120ERSDR COMA0160695Damper · faultyFLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 YAW DAMPER ACTUATOR. (SVL-4000).Sep 6, 2001 · N431CA · Cndair CL6002B19SDR COMA0160694Damper · faultyFLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #1 YAW DAMPER ACTUATOR. (SVL-4000).Sep 6, 2001 · N431CA · Cndair CL6002B19SDR COMA0160693Card · faultyFLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #1 FCC CARD. (FCC-4000)Sep 6, 2001 · N431CA · Cndair CL6002B19SDR COMA0160692Card · faultyFLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 FCC CARD. (FCC-4000)Sep 6, 2001 · N431CA · Cndair CL6002B19SDR MALA010688Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25.Sep 3, 2001 · N439XJ · Saab 340BSDR MALA010687Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B DUAL CIRCUIT I FUSELAGE RUDDER CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B DUAL CIRCUIT 1 FUSELAGE RUDDER CABLE P/N 7227105-562 IAW SF340 AMM 27-21-25.Sep 3, 2001 · N439XJ · Saab 340BSDR COMA0160671Damper · faultyFLIGHT #5889. DURING CRUISE FLIGHT AT 20,000 FEET, AIRSPEED 250 KNOTS AIRCRAFT ACQUIRED A RYTHMIC YAW, AIRCRAFT RETURNED TO ORIGINATION CITY CVG.REPLACED THE #2 SVL-4000 YAW DAMPER.Sep 2, 2001 · N932CA · Cndair CL6002B19SDR 2001F00485Mount · defectiveFLT 4810 - FLT FROM DFW-TUL, THE A/C WAS HARD TO CONTROL. WHEN THE A/P WAS DISCONNECTED, ELEVATOR AND RUDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE A/P. CREW PULLED THE A/P CIRCUIT BREAKERS, BUT DID NOT FIX THE PROBLEM. DECLARED AN EMERGENCY AND A/CAug 31, 2001 · N275AS · Emb EMB120SDR MALA010686Control Cable · chafedDURING 4K-CHECK IN CWA, LT CIRCUIT I AFT SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT CIRCUIT 1 AFT SINGLE RUDDER CABLE P/N 7227105-582 IAW SF340 AMM 27-21-25.Aug 30, 2001 · N439XJ · Saab 340BSDR RK287Computer · failedRUDDER BOOST FAIL ON TAKEOFF ROLL. MASTER CAUTION FOLLOWED BY RUDDER BOOST FAIL ANNUNCIATOR.Aug 30, 2001 · N361AS · Beech 400ASDR 2001FA0000373Rod · failedACTUATION ROD TO RUDDER PEDAL BROKE AT BASE OF THREADS AT FORK. THERE WAS NO DAMAGE TO RUDDER PEDAL OR BRAKE MOUNT FOUND.Aug 29, 2001 · N51403 · Cessna 172PSDR MALA010674Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE INSTALLED RT O/B RUDDER CABLE P/N 7227105-562, IAW SF3 AMM 27-21-25.Aug 24, 2001 · N437XJ · Saab 340BSDR MALA010673Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT O/B RUDDER CABLE IN DUAL CIRCUIT I IAW SAAB AMM 27-21-25-4 P/N 7227105-562.Aug 23, 2001 · N437XJ · Saab 340BSDR UPS01236693Control Unit · malfunctionedWITH RUDDER TRIMMED TO ZERO 12 DEGREE LEFT AILERON REQUIRED TO HOLD WINGS LEVEL DEPLOYING SPEED BRAKE SLIGHTLY FIXES PROBLEM. INSPECTED SPOILERS NO DEFECTS FOUND INSPECTED FLIGHT CONTROLS GEN MX PRACTICES 27-00-00 PAGE 201, 203 NO DEFECT FOUND HOWEVER SUSAug 23, 2001 · N918UP · Boeing 72730CSDR COMA0160634Bolt · mislocatedFLIGHT #5424. DURING CRUISE FLIGHT DESTINATION YYZ WITH THE AUTOPILOT ENGAGED, RT RUDDER TRIM OF 1.5 UNITS AND LT. DOWN AILERON TRIM OF .5 UNITS HAD TO BE SET TO KEEP STRAIGHT AND LEVEL FLIGHT.UPON INVESTIGATION FOUND THE LOWER MOUNTING BOLT FOR THE #1 YAW DAMAug 22, 2001 · N960CA · Cndair CL6002B19SDR AUS20011122Control Cable · misinstalled(AUS) RT REAR RUDDER CABLE INCORRECTLY ROUTED. CABLE EXCESSIVELY WORN.Aug 21, 2001 · Beech 58SDR MALA010672Control Cable · chafedDURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MAINTENANCE REPLACED RT RUDDER AFT SINGLE CABLE P/N 7227105-582 OF CIRCUIT I IAW SF340 AMM 27-21-25.Aug 21, 2001 · N437XJ · Saab 340B
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