JASC 2720

Service difficulty reports · 3,130

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 DALA2026101405650Reu · faultedDIVERTED TO XYX, DUE TO RUDDER FAIL MESSAGE. EMERGENCY DECLARED. REMOVED & REPLACED THE NR 2 AFT REU. (LP# 8954060; AIRCRAFT WAS GROUNDED)Oct 12, 2026 · N308DU · Airbus BD5001A11SDR AJXA2026100600049Yaw Damper · failedCASS MESSAGE "YD FAIL UPPER A" AFTER TAKOFF. AFTER TAKING OFF FROM KMDW WITH THE CASS MESSAGE THE PILOTS RETURNED TO KMDW. ONCE THE PILOTS WERE ON THE GROUND THEY PERFORMED A REBOOT OF THE ELECTRICAL SYSTEM AND THE FAULT DID NOT RETURN.Oct 5, 2026 · N736XJ · Cessna 750SDR FDEA202610021468Rudder Control · abnormalUPON TAKEOFF, ONCE AIRBORNE RUDDER BEGAN YAWING LEFT AND RIGHT AT ABOUT 1 HZ. CONTINUED YAWING LEFT RIGHT LEFT RIGHT THE ENTIRE DURATION OF THE FLIGHT. LEVELED OFF AT 8000 FEET AND SLOWED TO 230 KN AND CONTINUE TO BRING THE SPEED BACK TO TRY TO KEEP AERODYNOct 2, 2026 · N988FD · Boeing 757222SDR SIMA20260917001Rudder · faultedRUDDER FAULT IN FLIGHT. FOLLOWED QRH. MESSAGE DID NOT DISTINGUISH UNTIL LANDING. THEN FLIGHT CONTROL NO DISPATCH MESSAGE APPEARED. EMERGENCY DECLARED. PERFORMED FIM TASK 27-03-00-810-84N-A, MESSAGED EXTINGUISHED, PERFORMED POWER RESET PER AMM 49-10-00. FOUND TSep 17, 2026 · N202NN · Emb ERJ170200LRSDR ABXA20260903393Module · faultedRUDDER RATIO EICAS MSG APPEARED AFTER BLOCK OUT. CREW RETURNED TO THE GATE (BTB). MTC PERFORMED B767 FIM 27-09 FT 803 CLEARED FAULT BALLS ON RUDDER RATIO CHANGING MODULES. RAN BOTH ENGINES IAW B767AMM 71-00-00 MESSAGE DID NOT RETURN NO FURTHER ACTION REQUIREDSep 3, 2026 · N362CM · Boeing 767338SDR FE6R2026082701Control Cable · severedDURING THE INITIAL 50 HOUR INSPECTION AT FRAME STATION 282.0 WE FOUND THE RUDDER CABLE SEVERED. PROBABLE CAUSE IS DUE TO INCORRECT ROUTING AT MANUFACTURING. IT APPEARS THAT THE CABLE WAS ROUTED UNDER THE RETAINING PIN ON THE BOTTOM OF THE PULLEY WHICH PUSHED TAug 27, 2026 · N302WA · PiperSDR AALA202608273802Rudder · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING ON CLIMBOUT OF DFW AT 250 KNOTS THEY ENCOUNTERED AIRFRAME AND RUDDER VIBRATION WHICH COULD BE FELT IN THE BACK CABIN AND THE RUDDER PEDDALS - THEAug 24, 2026 · N986AN · Airbus A321231SDR HNAA2026082400745Pcu · illuminatedDURING CLIMB RUDDER SYSTEM 1-2 INOPERATIVE MESSAGE ON EICAS. R & R PRESSURE SWITCH IAW AMM 27-23-04-000/400-801-A. FOUND SYS 1 SOLENOID IN PCU MAKING BUZZING SOUND WHILE HYD SYS 1 ENGAGED. R & R PCU IAW AMM 27-22-03-000/400-801-A. OPS CHECKED GOOD. LEAK CHECKAug 23, 2026 · N939AE · Emb EMB145LRSDR ASAA2026080966254Actuator · faultedACFT ROLLED 15*, RT WING DOWN WITH CLEAN CONFIG TRIM (AILERON& RUDDER) WITH FLAPS 40* & GEAR DOWN AFTER HANDS OFF CONTROLS FOR 10 SECS. GROUNDED - YES. PERFORMED FUNCTIONAL TEST OF RUDDER CONTROL SYS & RUDDER TRIM SYS IAW AMM 27-20-00-720-802/803. TESTED WITHAug 9, 2026 · N489HA · Boeing 717200SDR 2026F00125Rudder · no discrepancyTHE PILOT DEPARTED RWY 9 ON THE SUNNY TRANSITION TO VQS AND AT APPROXIMATELY 1 MILE NORTH OF PUNTA LAS MARIAS, THE PIC DECIDED TO RETURN TO SIG DUE TO STIFFNESS OF THE RIGHT RUDDER PEDDLE. AN EMERGENCY WAS NOT DECLARED DUE TO THE PIC HAVING FULL CONTROL OF THJun 16, 2026 · N908VL · Bnorm BN2B26SDR DXTA2026061508426Warning Message · false activationDURING TAXI OUT WE RECEIVED A VENTRAL RUDDER FAIL CAS FOLLOWED BY AP FAIL AND YD FAIL. WHEN WE STOPPED TAXIING, ALL MESSAGES DISAPPEARED. WHEN WE STARTED TO TAXI AGAIN, THEY IMMEDIATELY CAME BACK. CORRECTIVE ACTION: POWERED ON AND NO CAS MESSAGE PRESENTED. PERJun 13, 2026 · N343QS · Emb EMB505SDR DXTA2026060508327Actuator · faultedON TAKEOFF JUST AFTER POWER WAS SET, NOSE PULLED HARD TO THE LT. LT RUDDER PEDAL ALSO WENT FULL. CORRECTED WITH RIGHT RUDDER & ABORTED TAKE OFF. RUDDER BIAS CHECK BEFORE WAS GOOD. PERFORMED RUDDER BIAS CHECK AFTER AND IT WAS GOOD. PERFORMED A DETAILED INSPEJun 2, 2026 · N696QS · Cessna 680ASDR AALA202605206036Spring · brokenAIRCRAFT WAS GROUNDED: DURING DVI FOUND ONE BROKEN ELEVATOR CONTROL MECHANISM SPRING ON RIGHT HAND ELEVATOR. REMOVED AND REPLACED SPRING FOR RIGHT HAND ELEVATOR TAB CONTROL MECHANISM. PER AMM 27-31-34.May 15, 2026 · N817NN · Boeing 737823SDR CALA2026051316218Gcu · faultedCREW REPORTED AT FL 340 UNCOMMANDED RUDDER INPUTS. AUTOPILIT , AUTOTHRUST DISCONNECTED. THE PFD ND FMGC FCU EWD LOWER ECAM BLANKED FLASHED MULTIPLE TIMES. CRC TRUMPETED MULTIPLE TIMES ECAM POPULATED. SOME RETURTNED MULTIPLE TIMES. SOME OF THE ECAMS WERE AUTO FMay 10, 2026 · N449UA · Airbus A320232SDR SWAA2026051195709Yaw Damper · faultyAT FL400; CREW NOTED THAT YOKE WAS DISPLAYED TO RIGHT 3 UNITS; CORRECTED USING RUDDER TRIM. APPROX. 1 MINUTE LATER; CREW OBSERVED UNCOMMANDED RUDDER INPUT (SHARP YAW TO THE LEFT.) OCCURRED 3 TIMES. OCCURRED A TOTAL OF 3 TIMES IN FLIGHT.<[01] INTERROGATED #1 SMMay 5, 2026 · N435WN · Boeing 7377H4SDR ABXA20260413161Module · faultedAFTER BLOCK OUT AND LT & RT ENGINES STARTED, RUDDER RATIO EICAS CAUTION MESSAGE APPEARED. ACFT RETURNED TO GATE AND MTX GROUNDED ACFT . MTX RESET LT & RR RUDDER RATIO MODULE AND PERFORMED ENGINE RUNS AND NO RUDDER RATIO FAULT IAW FIM 27-09 FT 814 AND AMM 71-00Apr 13, 2026 · N1427A · Boeing 767306SDR DALA2026032301955Reu · failedDIV - TO CLE DUE TO "RUDDER FAIL" WARNING MESSAGE. REPLACED #1 AFT REU. OK FOR SERVICE. (LP# 8384156)Mar 23, 2026 · N102DU · Airbus BD5001A10SDR HNAA2026031900227Pressure Switch · faultedRUDD SYS 1-2 INOP DISPLAYED ON DEPARTURE. MESSAGE PERSISTED FOR 3 MINUTES, THEN WENT AWAY. STARTED AT 800' AGL AND 170 KTS. NO CMC MESSAGES. TROUBLE-SHOT PER FIM TASK 27-22-00-810-804-A BLOCK 1 & 8. R & R RUDDER SYSTEM 2 PRESSURE SWITCH IAW 27-23-04. OPS CHMar 18, 2026 · N941LT · Emb EMB145LRSDR GTIA2026031239296Rudder · faultyDURING CLIMB RUDDER MOVED TO L4 WITHOUT INPUT IN BOTH MANUAL AND A.P. CAME BACK TO NORMAL ABOVE (L270 MANUAL) TRIM DID NOT HELP--Mar 12, 2026 · N993NK · Airbus A320271NSDR DALA2026031001636Control Box · faultySHIP 3149 DSC: AFTER T/O AUTO FLT RUD TRV LIM SYS ECAM MESSAGE. FOLLOWED THE ECAM RESET PROCEDURE BUT THAT WAS NOT SUCCESSFUL. T/S PER A319 TSM 22-61-00-810-803-A. FOUND FAULT FAC 1/RTL ACTR 4CC. UNABLE TO RESET/HARD FAULT. NEXT STEP IS TO R/R ELECTRONIC MODUMar 10, 2026 · N349NB · Airbus A319114SDR VNAA2026031014206Actuator · faultedCAUTION RUDDER LIMITER MSG IN FLIGHT. / REMOVED THE (LH) RTLA 1 FROM STEPS 4A (5) THROUGH COMPLETION AND REPLACED LH RTLA 1 IAW CRJ900 AMM 27-25-03-000/400-801-A04. ALL OPS CHECKED GOOD.Mar 9, 2026 · N583NN · Cndair CL6002D24SDR ABXA20260219073Pca · faultedAFTER BLOCK OUT, A "RUDDER RATIO" EICAS MSG AND DISCREET LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). PERFORMED FIM 27-21 FT 804 FOUND PCA BALL, RESET BOX EICAS MESSAGE NO LONGER SHOWING. AIRCRAFT RETURNED TO SERVICE.Feb 19, 2026 · N744AX · Boeing 767232SDR ABXA20260218072Module · faultedCREW REPORTED RUDDER RATIO MESSAGE DESCRITE LIGHT ILLUMINATED. MAINTENANCE PERFORMED FIM TASK 27-21 FAULT TREE 804 AND RESET LT AND RT RRCM MODLES. FAULTS CLEARED AT THIS TIME. A/C OK TO CONTINUE.Feb 18, 2026 · N744AX · Boeing 767232SDR HNAA2026021600128Switch · abnormalYAW DAMPER FAIL'D JUST BEFORE RUD SYS 1-2 INOP DISPLAYED. C/W QRH. R&R RUDDER SYSTEM 2 PSI SWITCH IAW 27-23-04 OPS AND LEAK CHECK GOOD. PERFORMED INTEGRATED COMPUTOR OPS CHECK IAW AMM 31-42-00 AND FOUND NO DEFECTS. MX ACTION COMPLETE SUBJECT TO SAT EVAL Feb 14, 2026 · N935AE · Emb EMB145LRSDR AJXA2026020500042Rvdt · pilot errorPILOT REPORTED YAW DAMPER UPPER A FAIL CYAN EICAS MESSAGE IMMEDIATELY AFTER TAKEOFF. THE PILOT ALSO REPORTED AN OVERSPEED MESSAGE WHICH WAS DETERMINED TO BE CAUSED BY THE CREW EXCEEDING 250 KNOTS BELOW 10,000 FEET. (PILOT ERROR)Jan 31, 2026 · N736XJ · Cessna 750SDR WX0A2026030232746Bushing · out of limits(AIRCRAFT GROUNDED) STRONG AIRFRAME VIBRATION FROM 330 KTS - 260 KTS AT FL250. VIBRATION WAS FROM TAIL OF AIRCRAFT ON UP AND DOWN MOTION. / FOUND L/H ELEVATOR HINGE FITTING BUSHINGS 1-5 OUT OF LIMITS PER AMM 27-34-41-200-001-A, BUSHINGS OR ELEVATOR REQUIRES REJan 1, 2026 · N331NV · Airbus A319111SDR VNAA20260205004Fitting · brokenDURING GAPS MEASSUREMENT ON REPLACEMENT OF RUDDER PRIMARY FEEL UNIT SHAFT IN REF TO_27-079-001-20-REQ, PIN FITTING LH SIDE WAS BROKEN. PIN FITTING LH SIDE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-13-001-001-A01 AND (ET) HFEC IDec 19, 2025 · N525AE · Bombdr CL6002D15SDR ANCF202512221840Bearing · excess playHIGH AIR FRAME VIBRATION AT: ALT 17000, ALT 27000, SPD 330 KTS, SPP 310KTS. IAW AMM 27-34-00-200-001-A FUNCTIONAL CHK OF ELEV SERVO CONTROL BEARINGS FOR EXCESSIVE PLAY & CONDITION. IAW AMM 27-24-00-210-001-A VISUAL INSP OF RUDDER SERVO CONTROLS FOR HYD LEAKSDec 18, 2025 · N207FR · Airbus A320214SDR J4YR202512084112Control Arm · brokenPILOT NOTICED THAT THE RUDDER TRIM SYSTEM WAS UNRESPONSIVE WHEN RUDDER TRIM ADJUSTMENT WAS MADE. UPON CLOSER EXAMINATION THE ARM THAT CONNECTS TO THE RUDDER TRIM ACTUATOR ON THE RUDDER CONTROL ARM ASSY (PN 63457-003) HAD SEPARATED FROM THE TUBE ADJACENT TO THEDec 8, 2025 · N132GT · Piper PA32R301TSDR 2025FA0000792Rudder Pedal · obstructedFIRST OFFICER’S RUDDER PEDALS STIFF AND REQUIRE EXTRA FORCE. IAW AMM 27-21-05-214-033. RUDDER PEDALS OPERATED THROUGH FULL TRAVEL RANGE, NO OBVIOUS STIFFNESS NOTED. PEDALS MOVED FREELY THROUGH THEIR FULL RANGE WITH RUDDER OPERATING CORRECTLY WITH THE POSITIONov 30, 2025 · N363UP · Boeing 767346SDR F3LA20251201033Actuator · faultedACFT WAS GROUNDED AS A RESULT OF EVENT. 5 UNCOMMANDED RUDDER MOVEMENT DURING FLIGHT. 1ST 2 INITIALLY THOUGHT TO BE WX/WIND RELATED. LAST 3 HAPPENED DURING DESCENT & FINAL APPROACH WITH AP ON AND OFF. 4 WERE LEFT MOVEMENT, 1 WAS RIGHT MOVEMENT. FIRST ONE HAPPENNov 28, 2025 · N719FR · Airbus A321211SDR F3LA202512010333Rudder · malfunctionedACFT WAS GROUNDED AS A RESULT OF THIS EVENT. 5 UNCOMMANDED RUDDER MOVEMENT DURING FLIGHT. FIRST 2 INITIALLY THOUGHT TO BE WX/WIND RELATED. LAST 3 HAPPENED DURING FINAL APPROACH WITH AP ON AND OFF. 4 WERE LEFT MOVEMENT, 1 WAS RIGHT MOVEMENT. FIRST ONE HAPPENED Nov 28, 2025 · N719FR · Airbus A321211SDR SWAA2025120139743Counterweight · corrodedTHE RUDDER COUNTER BALANCE WEIGHT CORRODED AND MISSING PAINT. REPLACED THE RUDDER COUNTER BALANCE WEIGHT IAW CMM 55-40-09.Nov 26, 2025 · N7857B · Boeing 73779PSDR AALA202511250586Hinge Fitting · excess playAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED 3 AIRFRAME VIBRATION EVENTS 1. FL180 310KTS 1600VSI2. FL260 290KTS 1600VSI3. FL318 275KTS 1000VSI. MAINTENANCE INSPECTED THE LEFT-HAND ELEVATOR HINGE FITTINGS AND FOUND EXCESSIVE PLAY IN ALL 6 HINGE FITTINGS. (OPEN)Nov 21, 2025 · N119NN · Airbus A321231SDR AJXA2025112100039Rudder · malfunctionedTHE CREW REPORTED THAT AFTER 50 MINUTES THE RUDDER TRIM BEGAN TO TURN TO THE LEFT & THEN TO THE RIGHTNov 21, 2025 · N750GM · Cessna 750SDR J7SA2025112400463Torque Tube · damagedBINDING NOTED ON TWO SEPARATE FULL RIGHT RUDDER FULL RIGHT BRAKE APPLICATIONS. ACCOMPLISHED A GIV OF THE CONTROL PEDALS IAW AMM 27-01-02 AND THE RUDDER FORWARD TORQUE TUBE IAW AMM 27-21-06. FOUND THE TOP BRACKET HOLDING THE CENTER RUDDER FORWARD TORQUE TUBE FLNov 20, 2025 · N344FX · Emb EMB505SDR AALA202511187613Rudder · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF AT APPROXIMATELY 100KTS DUE TO A VERY HARD YAW TO THE RIGHT THEN A REVERSAL TO THE LEFT. FELT LIKE WE POSSIBLY HAD A FLIGHT CONTROL ISSUE WITH THE RUDDER. FIRST OFFICER SAID THE FOOT PEDALNov 17, 2025 · N339TP · Boeing 7378SDR HNAA2025111700741Warning Message · false activationRUDDER SYS 1 INOP MESSAGE ON T/O ROLL AND REJECTED T/O. PERFORMED RUDDER SYSTEM OPERATIONAL TEST IAW AMM 27-23-00. OPS CHECK GOOD. A/C OK FOR SERVICENov 16, 2025 · N698CB · Emb EMB145LRSDR HNAA2025111700740Pressure Switch · faultedRUDDER SYSTEM 2 INOP DISPLAYED DURING TAKE-OFF AT ABOUT 50 KNOTS. R&R RUDDER PRESSURE SWITCH IN REF WITH 27-23-04-000-A/400-801-A. R&R RELAY K0387 IN REF WITH AMM TASK 20-13-02-000/400-801-A. R&R RUDDER SHUTOFF SYS 2 PB SWITCH IN REF WITH AMM 20-13-04-000/4Nov 16, 2025 · N640AE · Emb EMB145LRSDR AJXA2025111800038Actuator · malfunctionedTHE PILOT REPORTED UPON DEPARTURE WHETHER TURNING RIGHT OR LEFT, THE UPPER RUDDER / AIRCRAFT SWAYED LEFT AND RIGHT BEFORE CORRECTINGNov 14, 2025 · N750GM · Cessna 750SDR DALA2025111208303Warning Message · false activationATO- APPROX 85KTS DUE TO RUDDER RESTRICTED MESSAGE. PERFORMED RUDDER THROW LIMIT FUNCTIONAL TESTS AND RUDDER INSPECTIONS. NO DEFECTS NOTED, OPS NORMAL. (7585374)Nov 11, 2025 · N893AT · Boeing 717200SDR FXTA20251029001Cylinder · leakingPILOT FELT STRONG LEFT RUDDER PRESSURE ON TWO CONSECUTIVE TAKE OFFSOct 29, 2025 · N409BA · Textrn 408SDR QXEA2025101700321Rudder Pedal · mismatchedFO RUDDER PETAL MISMATCH. AFTER FLIGHT FO DETERMINED THE MISMATCH WOULD HAVE BEEN PROBLEMATIC DURING LANDING IF CROSSWIND IMPUTS WOULD HAVE BEEN NECESSARY. FO ALSO REPORTED EVEN BRAKING DURING LANDING ROLLOUT WAS NEAR IMPOSSIBLE. RUDDERS ARE MISMATCHED BY APROOct 16, 2025 · N668QX · Emb ERJ170200LRSDR DXTA2025101305252Line · looseRUDDER BIAS CHECKED GOOD ON TAXI OUT, ADVANCING POWER , RIGHT RUDDER STIFFENED AS IF JAMMED. REMOVED RH UPPER AND LOWER ENGINE COWLS. UPON CLOSE INSPECTION, TECHNICIAN FOUND 1 BLEED LINE LOOSELY CONNECTED, AND ONE BLEED LINE DISCONNECTED. INSPECTED THE RH ENOct 9, 2025 · N975QS · Cessna 680ASDR DALA2025100607268Bearing · wornEMPENNAGE RUDDER SERVO CONTROLS WITH PLAY OUT OF LIMITS. ACCOMPLISHED DELTA WC #2724-2010 AND REPLACED BEARINGS AND HARDWARE OF THE RUDDER SERVO CONTROLS SEE DELTA WC #2724-2013 AND PERFORMED CHECK OF THE RUDDER T/E PLAY IAW A319 AMM TASK 27 -24-00-200-002-AOct 4, 2025 · N351NB · Airbus A319114SDR SWIA2025092600024Computer · looseEXPERIENCED THE RUDDER OSCILLATIONS IN FLIGHT, WITH THE RUDDER RANDOMLY SWINGING TO ONE SIDE. IT SEEMED AS IF THE RUDDER IS LOOSE, WHERE YOU COULD FEEL IT HIT A STOP. (FLIGHT 5832 - FILED CLOSED)PLEASE REFERENCE AML 1712505 PLEASE REFERENCE AML 1712677. REMSep 24, 2025 · N453SW · Cndair CL6002B19SDR QXEA2025092300308Rudder Pedal · out of alignmentF.O.'S RH RUDDER PEDELS SRE NOT ALIGNED. REMOVED FROM SERVICE. REF W/O 355992, N/R'S - 00001 THROUGH-00007 FOR RUDDER QUDRANT RIGGING VERIFICATIONS AND ADJUSTMENS MADE TO FO'S R/H PEDEL. AFTER ADJUSTMENT PEDELS STILL NOT COMPLETELY ALIGNED. REF W/O 355992, TC Sep 21, 2025 · N668QX · Emb ERJ170200LRSDR 2025FA0000763Arm · brokenARM ASSEMBLY - CONNECTOR (PART NUMBER 6661-000) BROKE WHERE ASSEMBLY MATES WITH THE RUDDER PEDAL ASSEMBLY (PART NUMBER 63459-019) WHILE A FLIGHT INSTRUCTOR AND STUDENT PILOT WERE FIGHTING OVER PEDALS. ALTHOUGH THE PART FAILED BY FORCE A VISUAL INSPECTION OF TSep 19, 2025 · N3024M · Piper PA28181SDR QXEA2025091900306Rudder · fluctuatesFLIGHT 2193. ON TAKEOFF: ABNORMAL + FLUCTUATING OF RIGHT RUDDER NEEDED FOR CENTERLINE. ON LANDING: ABNORMAL AMOUNT OF RIGHT RUDDER NEEDED FOR CENTERLINE. ON TAXI: TRACKS STRAIGHT WITHOUT TILLER ENGAGING THE AIRCRAFT TRACKS LEFT. REMOVED FROM SERVICE. PERFORMESep 19, 2025 · N652MK · Emb ERJ170200LRSDR 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 EMB145LR
Back to JASC 2720