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 HNAA2025091100615Pressure Switch · corrodedRUDDER SYSTEM 1-2 INOP MSG DISPLAYED AT APROX 3000FT 210K. T/S IRW FIM 27-22-00-810-804-A R&R #2 RUDDER PSI SWITCH IAW AMM 27-23-04 OPS CHECK AND LEAK CHECK GOOD. ACFT OK FOR SERVICE AT THIS TIMESep 9, 2025 · N673AE · Emb EMB145LRSDR BAGA2025090900001Pcu · failedRUDDER FAIL AT 30,000 FEET. FOLLOWED CHECKLIST AND LANDED AT NEAREST SUITABLE AIRPORT. LANDED WITH OUT RUDDER. REMOVED AND REPLACED UPPER PCU. ALL RUDDER OPS CHECKS AND PCU AUTO RIGGING CHECKS GOOD.Sep 8, 2025 · N226BZ · Airbus BD5001A11SDR C1CB2025090800628Warning Message · false activationAFTER DEPARTURE AND DURING THE CLIMB OUT, N284CP EXPERIENCED MULTIPLE AMBER MAINTENANCE MESSAGES THAT INCLUDED #1/2 RUDDER SYS INOP, AUTOPILOT INOP AND PITCH TRIM INOPERATIVE. THE CREW HELD ALTITUDE AT 16,000FT TO PERFORM THE STEPS IN THE QRH TO CLEAR THE MESSep 8, 2025 · N284CP · Emb EMB145XRSDR CALA2025081807898Limiter · faultedACFT HAS REPEAT HIT OF AUTO FLT RUD TRV LIM SYS. BEFORE FURTHER FLIGHT, REPLACE RUDDER TRAVEL-LIMIT UNIT FIN 4CC REF AMM 27-23-51. CARRIED BY ELB R&R THE RUDDER TRAVEL-LIMITATION UNIT REF AMM: 27-23-51. C/W THE RUDDER TRAVEL-LIMITATION UNIT OPS CHECK REF AMMAug 15, 2025 · N482UA · Airbus A320232SDR 2025FA0000543Control Arm · crackedARCHER RUDDER TRIM CONTROL ARM ASSEMBLY, CRACKED DUE TO METAL FATIGUE IN THE PART.Aug 13, 2025 · N4402A · Piper PA28181SDR DALA2025081106005Control Cable · out of adjustSHIP 3146 EMPENNAGE RUDDER CABLE HAS LOW TENSION. CORRECTIVE ACTION: PERFORMED THE ADJUSTMENT OF THE RUDDER CONTROL CABLE LENGTH IAW A319 AMM TASK 27-21-00-820-002-A. (1135858).Aug 10, 2025 · N346NB · Airbus A319114SDR HNAA2025080500535Warning System · false activationABORTED TAKE OFF DUE TO RUD SYS 1 INOP CAUTION MSG R & R #100 AND AT 00 RUDDER PRESSURE SWITCHES IRT AMM 27-23-04. OPS CHECK OF RUDDER SYSTEMS SATISFACTORY IRT AMM 27-23-00. BOTH SYSTEMS BLED AS NECCESSARY. NO ABNORMAL MSGS SEEN DURING HIGH POWER CHECK. OK Aug 4, 2025 · N679AE · Emb EMB145LRSDR SWAA2025072895488Pcu · faultyDURING CLIMB OUT AT 14000 AND AGAIN AT 16000 FT THE RUDDER KICKED LEFT WITHOUT PILOT INPUT. OCCURRED AGAIN AT FL370 APPROX 30 MINUTES LATER. AUTOPILOT DID NOT DISENGAGE<[01] REMOVED AND REPLACED MAIN RUDDER PCU PER AMM 27-21-91. ALL OPS CHECKS NORMAL.;[02] REMJul 25, 2025 · N914WN · Boeing 7377H4SDR 3EJA8202508150001Shutoff Valve · failedON TAKEOFF RUNWAY 14L, REACHED TAKEOFF POWER DETENT, FELT A SMALL LURCH OF IN RUDDER PEDALS. MASTER CAUTION ILLUMINATED. REMOVED AND REPLACED RUDDER BIAS SHUT OFF VALVEJul 7, 2025 · N842JS · Cessna 560XLSDR GCXA202507020001Control Cable · brokenRIGHT RUDDER FAILS DURING FLIGHT CONTROL CHECK - FOUND BROKEN RUDDER CONTROL CABLE IN AFT SECTION OF TAIL FR71Jul 2, 2025 · N282GX · Airbus A320214SDR DALA2025070104905Reu · faultedSHIP 8113 - MISC - DECLARED EMERGENCY DUE TO "RUDDER FAIL" WARNING MESSAGE ON FINAL. CORRECTIVE ACTION: REPLACED AFT REU-1 AND CLEARED THE LATCHED MESSAGES. (LP# 6754140)Jul 1, 2025 · N113DQ · Airbus BD5001A10SDR CALA2025063006075Control Cable · out of rigON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH FULL LH RUDDER PEDAL INOUT ON ROLL OUT FOR TAKE OFF CREW REPORTS AC PULLING TO THE RIGHT WITH FULL LH RUDDER PEDAL INPUT CHECKED RIG OF AFFECTED SYSTEM AND FOUND CABLES NWSA AND NWSB TO BE MISRJun 25, 2025 · N78866 · Boeing 75733NSDR HNAA2025080500488Control Rod · out of limitsF050662 RUDDER II UPPER CONTROL ROD FITTING IS OUT OF LIMITS PER WC 27-20-04 STEP X. AND ALSO HAS A GOUGE AROUND HOLE FOR UPPER HAT BUSHING. REMOVED AND REPLACED RUDDER II UPPER CONTROL ROD FITTING IAW EMB 145 SRM 55-40-02.Jun 1, 2025 · N918AE · Emb EMB145LRSDR DXTA2025052703590Rudder · faultedWHILE IN FLIGHT VENTRAL RUDDER FAIL WHITE CAS MESSAGE POSTED. WE RAN THE CHECKLIST. IT EXTINGUISHED BEFORE LANDING. CORRECTIVE ACTION: PERFORMED OPERATIONAL CHECK OF THE VENTRAL RUDDER IAW PHENOM 300 AMM 27-26-01-710-80-A WITH NO DEFECTS NOTED. CAS MESSAGE NEMay 22, 2025 · N460QS · Emb EMB505SDR DXTA2025052203568Rudder · faultedDURING TAKEOFF I PROGRESSIVELY LOST AUTHORITY OF THE RIGHT RUDDER PEDAL. I WAS NOT ABLE TO PUSH THE PEDAL TO MAINTAIN CENTERLINE LEADING TO AN ABORTED TAKEOFF. CORRECTIVE ACTION; TIGHTENED LOOSE CONNECTION ON LINE FROM RUDDER BIAS TO THE ENGINE AND PERFORMED SMay 20, 2025 · N633QS · Cessna 680ASDR DALA2025052203939Torque Tube · corrodedSHIP 9572 ON REF AMDS 2027-2004 CORROSION ON SPLINE AND BORE OF RUDDER DRIVE TORQUE TUBE P/N 5912802-13, ALSO CORROSION ON WASHER LOWER BRG P/N 2913035-1 OF RUDDER CONTROL AFT FUSELAGE // EMPENNAGE. CORRECTIVE ACTION: RUDDER TORQUE TUBE WAS REPLACED BY SERVICEMay 20, 2025 · N927AT · Boeing 717200SDR DXTA2025052103571Bungee · defectiveCAPTAIN RUDDER PEDAL: DURING TAXI AND WHILE STATIONARY, WE GET A NOISE IN WHEN YOU MOVE RUDDER PEDALS BACK AND FORTH. YOU CAN HERE THE NOISE FROM THE OUTSIDE IN THE NOSE GEAR WELL. IT APPEARS TO BE COMING FROM THE DAMPNER CYLINDER. CORRECTIVE ACTION; VERIFIED May 20, 2025 · N643QS · Cessna 560XLSDR DXTA2025052103550Servo · defectiveVENTRAL RUD FAIL CAS APPEARED THREE TIMES IN FLIGHT. FIRST, CLIMBING BELOW 10,000, APPROX 200 KNOTS, THIS MESSAGE APPEARED ALONG WITH AP FAIL AND YD FAIL. ALL MESSAGES RESET IN ONLY A FEW SECONDS. SECOND, CLIMBING BETWEEN 10-20,000 FEET AND APPROX 220 KNOTS, TMay 18, 2025 · N332QS · Emb EMB505SDR BAGA2025052100008Rudder Control · malfunctionedUNCOMMANDED RUDDER INPUTS OR YAW MOTION INFLIGHT. BECOMING LARGER DURING DESCENT THROUGH 10000 AND COINCIDING WITH SPEED REDUCTION (AUTOPILOT IN CONTROL). PERFORMED AUTOFLIGHT CONTROL SYSTEM TEST, WITH NO ANNOMOLIES NOTED AND NO FAULTS.May 17, 2025 · N206BZ · Airbus BD5001A11SDR SWIA202505060001Pcu · brokenDURING TROUBLESHOOTING OF STIFF RUDDER DURING OPERATION, FOUND #1 RUDDER PCU ROD END BROKEN. (FLIGHT 6425) REMOVED AND REPLACED NO.1 RUDDER PCU IAW CRJ 700 AMM 27-23-01. RIGGED RUDDER SYSTEM IAW CRJ 700 AMM 27-21-00. OPS CHECKS GOOD IAW CRJ 700 AMM 27-32-01. May 1, 2025 · N753SK · Cndair CL6002C10SDR SWIA20250501001Rod End · brokenREFERENCE AML 1594668 DURING TROUBLESHOOTING OF STIFF RUDDER DURING OPERATION, FOUND #1 RUDDER PCU ROD END BROKEN. (FLIGHT 6425 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSMay 1, 2025 · N753SK · Cndair CL6002C10SDR ABXA202504076070Module · defectiveON TAXI OUT, RUDDER RATIO LIGHT ILLUMINATED AFTER ENGINE START AND WOULD NOT EXTINGUISH. A/C RETURNED TO BLOCKS (BTB). VERIFIED SHUTOFF, SERVO, AND LVDT WIRING. FOUND MODULE FAULT BALL ON LEFT UNIT. REMOVED AND REPLACED THE LEFT RUDDER RATIO MODULE, REF. BApr 5, 2025 · N317CM · Boeing 767338SDR YENA2025040200359Screen · looseFLT#420, LAX-BOS. 'AFTER TAKE OFF (GW193800) A CONSTANT VIBRATION ON THE RUDDER PEDALS (BOTH). THE VIBRATION LASTED DURING THE CLIMB, DIFFERENT PITCH ON THE AC. DID NO ATTENUATE THE VIBRATION. AT CRUISE THE VIBRATION WAS MUCH LESS THAN CLIMBING PHASE. AN AIRCMar 31, 2025 · N2169J · Airbus A321271NXSDR UIEA2025031100259Actuator · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN SERVO VALVE.(<P>RUDDER RATIO CHANGER ACTUATOR WAS REPLACED I.A.W AMM 27-21-15-422-024 OPERATONAL TEST WAS PERFORMED AND NO LEAKS FOUND, TORQUE APPLIED 280 LB-IN, 360 LB-IN S/N 0823114404 DATE 12DEC2026.</PMar 24, 2025 · N642GT · Boeing 7673Y0SDR DXTA2025032402749Actuator · defectiveRUDDER BIAS: AS POWER WAS APPLIED DURING TAKEOFF, A NO TAKE OFF AURAL WARNING WAS SOUNDED. ON THE NO TAKE OFF PAGE, A RUDDER BIAS WITH ASTRIX WAS PRESENT. A LOW SPEED ABORT WAS COMPLETED. GROUND SPEED DID NOT EXCEED 30 KNOTS. ATTEMPTS TO CLEAR THE MESSAGE FAILMar 19, 2025 · N307QS · Cessna 680SOVSDR HNAA2025043000290Bushing · migratedF033969 RUDDER I LOWER HINGE FITTING UPPER DOUBLE HAT BUSHING LOWER HAT BUSHING MIGRATED. REAMED RUDDER 1 LOWER HINGE FITTING POSITION 2 HOLE, FABRICATED AND INSTALLED NEW DOUBLE HAT BUSHINGS IAW EMB 145 SRM 55-00-02 ITEM 3, FIG. 202 SHEETS 4,5,6 AND EO1-55-2Mar 16, 2025 · N677AE · Emb EMB145LRSDR DALA2025031101861Controller · faultySHIP 3301 - ATB/FCNT - DUE TO UN-COMMANDED RUDDER MOVEMENT. CORRECTIVE ACTION: R/R RATE GYRO UNIT, BITE AND OPS TEST GOOD. (5700206)Mar 11, 2025 · N801NW · Airbus A330323SDR FDEA202502280306Actuator · failedON FINAL, WITH AUTOPILOT OFF, RUDDER WAS VERY DIFFICULT TO OPERATE ON THE RIGHT PEDAL BUT THEN FELT LIKE IT PUSHED THROUGH SOMETHING AND WAS LESS STIFF BUT STILL MORE THAN NORMAL. LEFT PEDAL FELT NORMAL. ON TAXI OUT RUDER CHECK FELT NORMAL, TAXI IN, TRIEDFeb 28, 2025 · N690FE · Airbus A300F4605RSDR HNAA2025021900089Pressure Switch · faultedDURING CLIMBOUT APPOX 210 KNTS AT 2K FT EXPERIENCE YAW DAMPNER FAIL FOLLOWED BY RUDDER 1/2 FAIL FOLLOWED QRH WITH RUD SYS 2 DEACTIVATED FACT 18FEB25 16:14 CLT R&R RUDDER PRESSURE SWITCH IAW AMM 27-23-04. LEAK CHECK & OPS CHECK REQUIRED.(885751) OPS AND LEAFeb 18, 2025 · N684JW · Emb EMB145LRSDR DALA2025021001044Reu · failedSHIP 8316 - DIV - TO CHS DUE TO RUDDER FAIL MSG WILL BE DECLARING AN EMERGENCY. CORRECTIVE ACTION: REMOVED AND REPLACED AFT REU #2 AND LOWER RUDDER PCU. OK FOR SERVICE. (LP# 6706442)Feb 9, 2025 · N316DU · Airbus BD5001A11SDR DALA2025020300804Computer · faultedSHIP 9556 -MISC/DE- THE FLIGHT CREW NOTICED THAT THE AIRCRAFT WAS FLYING UNCOORDINATED DURING THE DESCENT AND THEN THEY RECEIVED "RUDDER RESTRICTED" MESSAGE ON APPROACH. AN EMERGENCY WAS THEN DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAJan 31, 2025 · N896AT · Boeing 717200SDR YENA2025012900123Control Rod · out of adjustFLT#1703, SJU-MDE. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) 'WITH A/P ON AIRCRAFT IS FLYING OUT OF TRIM. THE SIDE SLIP INDICATOR INDICATED VERY LARGE SIDE SLIP WHICH WAS NOT CORRECTED BY THE RUDDER TRIM. WITH A/P OFF MANUAL TRIM OF THE RUDDER WAS DONE TO AJan 28, 2025 · N821JB · Airbus A320232SDR DALA2025012400603Reu · faultedSHIP 8120 - DIV - TO PHL DUE TO INTERMITTENT "27 FLT CTRL FAULT PRIM REU INOP" MESSAGE FOLLOWED BY "RUDDER FAIL" MESSAGE. CORRECTIVE ACTION: CLEARED THE LATCHED FAULT FROM PRIMARY FLIGHT CONTROL COMPUTER (PFCC), REPLACED AFT REMOTE ELECTRONICS UNIT (REU) 1, PEJan 23, 2025 · N120DU · Airbus BD5001A10SDR DALA2025012400587Pushrod · corrodedSHIP 3136 CORROSION ON ROD END PUSH ROD RUDDER CONTROL MECHANISM LOC. THS COMPARTMENT. CORRECTIVE ACTION: REPLACED CONTROL ROD OF THE RUDDER MECHANICAL CONTROL ON THS COMPARTMENT AS PER A320FAM AMM 27-21-00-840-001-A AND AMM27-21-00-820-001-A. (0775794)Jan 23, 2025 · N336NB · Airbus A319114SDR HNAA2025012100046Pressure Switch · failedRUDDER SYSTEM 1 INOP MESSAGE DISPLAYED DURING TAKE OFF ROLL. FACT 17JAN25 21:34 CAE R&R'D RUDDER SYS 1 PRESSURE SWITCH IAW AMM 27-23-04. OPS & LEAK CHECK GOOD.Jan 17, 2025 · N641AE · Emb EMB145LRSDR UIEA2025011000025Pca · leakingRUDDER, LOWER PCA WITH HYDRAULIC LEAK.(<P>RUDDER, LOWER PCA WAS ADJUSTED PER AMM 27-21-02-422-038. LEAK CHK GOOD. NO FURTHER DEFECTS NOTED.</P>)Jan 15, 2025 · N641GT · Boeing 76738ESDR UIEA2025011300037Servo · leakingVERTICAL STABILIZER, OUTBOARD YAW DAMPER WITH LEAK EVIDENCE.(<P>VERTICAL STABILIZER OUTBOARD YAW DAMPER WAS REPLACED, REMOVED I.A.W AMM 22-21-02-014-001 AND WAS INSTALLED I.A.W AMM 22-21-02-414-016 REV.143 DATE 22 AUG 22, TORQUE APPLIED 140 LB/LN, 170 LB/IN, 1Jan 14, 2025 · N664GT · Boeing 76731BSDR UIEA2025011300036Servo · leakingVERTICAL STABILIZER, INBOARD YAW DAMPER WITH LEAK EVIDENCE.(<P>INBOARD YAW DAMPER WAS REPLACED IAW AMM 22-21-02414-016 REV. 143 DATE: 22 AUG 24 AND 22-21-02-014-001 REV. 143 DATE: 22 AUG 24 TORQUE APPLIED 140LB- IN /170 LB -IN /80LB-LN WITH TOOL SIN 0524121887Jan 14, 2025 · N664GT · Boeing 76731BSDR 2024FA0000991Control Cable · wornRUDDER LEFT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLIGDec 31, 2024 · N208AV · Cessna 560CESSNASDR 2024FA0000990Control Cable · wornRUDDER RIGHT CENTER CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED ROUGHLY AT FS 415. THE MANUFACTURER HAS NO APPROVED REPAIR OR ALTERATION ASIDE FROM CABLE REPLACEMENT. THIS CABLE HAS BEEN REPLACEDec 31, 2024 · N208AV · Cessna 560CESSNASDR DXTA2024122001559Adc · failedON MISSED APPROACH WE LOST OUR STBY ATTITUDE INDICATOR AIRSPEED FOLLOWED BY A RUDDER A & B FAIL. THAT THEN CHANGED TO A RUDDER REV A. REMOVED PART NO: 011-02337-01 REMOVED SERIAL NO: 1U6103649, DUE TO RUDDER MAINTENANCE CAS. INSTALLED CUSTOMER SUPPLIED REPAIRDec 16, 2024 · N839QS · Textrn TEXTRON700SDR DXTA2024121601523Ahrs · defectiveVENTRAL RUD FAIL WHITE CAS: REPEAT WRITE UP. CAS ILLUMINATED IN FLIGHT, STARTED WITH YELLOW HDG FLAG FOLLOWED BY AP/YD/SWPS FAIL CAS MESSAGE. ALSO RECEIVED AHRS 2 FAIL, CAS MESSAGE CLEARED A FEW MINUTES ADTWR REVERTINF TO AHRS 1 CORRECTIVE ACTION; REPLACED #2 Dec 13, 2024 · N314QS · Emb EMB505SDR YENA2024120201516Autopilot Sys · abnormalFLT#2062,SJU-BOS. 'WHILE CLIMBING RECEIVED ECAM AUTO FLT RUD TRV LIMITER 1 ( RUDDER TRAVEL LIMITER SYSTEMS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)Dec 1, 2024 · N562JB · Airbus A320232SDR DALA2024112511208Module · faultedSHIP 0685 -DIV- DIVERTED TO CAE DUE TO RUDDER RATIO MESSAGE AND CROSSWIND RESTRICTIONS. CORRECTIVE ACTION: REPLACED LEFT RUDDER RATIO CHANGER MODULE.Nov 22, 2024 · N685DA · Boeing 757232SDR DXTA2024111201094Servo · damagedSHORTLY AFTER TAKEOFF THE VENTRAL RUD FAIL CAS MESSAGE ILUMINATED. THE MESSAGE CLEARED IT SELF SEVERAL MINUTES LATER AND THEN CYCLED ON AND OFF SEVERAL TIMES OVER THE COURSE OF THE 45 MINUTE FLIGHT AT FL370. WE THEN RECIEVED AN AP FAIL AND YD FAIL CAS ALONG WNov 8, 2024 · N438QS · Emb EMB505SDR 2024FA0000992Control Cable · wornRUDDER RIGHT FORWARD CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH FAIRLEAD LOCATED IN CONTROL LOCK SYSTEM. THIS CABLE AVERAGES ROUGHLY 1200 HOURS BEFORE REPLACEMENT IS NECESSARY. PROPER CONTROL LOCK RIGGING AND FLINov 4, 2024 · N208AV · Cessna 560CESSNASDR DXTA2024110701046Rudder · no discrepancyRUDDER: DURING APPROACH WITH 15 KTS LEFT CROSSWIND THE RUDDER PEDAL SEEM TO BE BINDING AND HARD TO PUSH FOR CROSSWIND ALIGNMENT. THE YAW DAMPER WAS VERIFIED OFF. AND THERE WERE NO CAS MESSAGE. BUT FELT LIKE RUDDER WAS BEING LIMITED. SEEMS TO FUNCTION FINE ON GNov 3, 2024 · N694QS · Cessna 680ASDR IPXA2024103046577Actuator · faultedAIR TURN BACK, RUDDER RATIO SINGLE EICAS MESSAGE. RESULTED IN ATB. REMOVED AND REPLACED UPPER RUUDER RATIO CHANGER ACTUATOR SERVO M520 IAW AMM 27-21-12, OPS CHECK GOOD MSG CLEARED. RIG PIN R4 REMOVED. C/W RII REQUIREMENTS, VERIFIED RIG PIN R4 REMOVED, REF GMMOct 30, 2024 · N634UP · Boeing 7478FSDR GTIA2024102838488Servo Control · faultyMODERATE VIBRATION REPORTED IN THE AFT AREA AFTER T/O DURING CLIMB-FOR CORRECTIVE ACTION PLEASE REFERENCE LOG BOOK PAGES 3629277-2, 369277-1 AND 3629278-1 A/C OK FOR CONT. SVC. REMOVED AND REPLACED RUDDER SERVO CONTROL (1025GM)IAW AMM 27-24-51. ALL CHECKS AND Oct 26, 2024 · N536NK · Airbus A319132SDR AALA202410039158Pressure Switch · inoperativeON TAKEOFF ROLL FLIGHT CONTROL SYSTEM B LOW PRESSURE LIGHT ILLUMINATED CONTINUED TAKEOFF. RAN THE QRH AIRCRAFT WAS GROUNDED: CHECKLIST AND STANDBY RUDDER LIGHT AND YAW DAMPER LIGHT ILLUMINATED . FLIGHT ATTENDANTSREPORTED UNUSUAL HEAVY HUMMIMG NOISE FROM THE Oct 2, 2024 · N983NN · Boeing 737823
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