JASC 2710

Service difficulty reports · 2,967

Reports filed under 2710 · Aileron 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 = '2710'
  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 DXTA2025070204085Trim System · faultedIN CRUISE AT FL260 AND 310KTS. EXCESSIVE RIGHT WING TRIM REQUIRED FOR STRAIGHT AND LEVEL. AT LOWER ALTUTUDE AND SLOWER SPEEDS LESS RIGHT AILERON TRIM REQUIRED PERFORMED RIGGING OF THE LH AILERON BALANCE GEARED-TAB IN REFERENCE TO AMM 27-11-21-220-801. ADJUSTEDJun 29, 2025 · N796QS · Bombdr BD1001A10SDR DALA2025062004645Bracket · out of limitsR/H AILERON ANTI-MIGRATION BRACKETS CLEARANCE TOLERANCES OUT OF LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0004:2715-4001-RH/003 00541 ADJUSTED R/H AILERON ANTI-MIGRATION BRACKETS CLEARANCE REF A220 AMP 27Jun 17, 2025 · N107DU · Airbus BD5001A10SDR RJEF20250601001Servo Control · failedF/CTL R AILERON WITH OSCILATION AFTER TAKE OFF INCREASING WITH AIRSPEED INCREASE.THIS CONDITION PRODUCE HIGHT VIBRATION ON THE AC//REMOVED AND REPLACED AILERON SERVO CONTROL 33CE4 PER AMM A320 27-14-51-400-001-A TOOL USED QD2R200 SN 12046034907 02 NOV 2025 PN Jun 15, 2025 · N788AV · Airbus A320251NSDR QXEA2025061700261Aileron Sys · faultedFLIGHT 2377. DURING AUTOLAND APPROACH TO 16R AT KSEA, AILERON DEFLECTED TO TO 80 DEGREES TO THE RIGHT NO LOCALIZER FAULT OBSERVED ON APPROACH. AILERONS STAYED UP TO 80 DEGREES RIGHT TO TOUCHDOWN. CONSIDER AUTOLAND UNSUCSESSFUL. REMOVED FROM SERVICE. NO FAULTS Jun 12, 2025 · N620QX · Emb ERJ170200LRSDR VNAA20250610028Cable · frayedHN00215951 S/N: 415 DISCREPANCY: LH AILERON CABLE HAS A FRAY AT PULLEY IN BETWEEN BL 0.0 AND LH WING STATION 29.0 MARKED WITH RED TAPE AND CORROSION FOUND ON BOTH LH CABLES AT WS 40.0Jun 10, 2025 · N513AE · Cndair CL6002C10SDR VNAA20250610027Cable · frayedHN00215951 S/N: 415 DISCREPANCY: LH AILERON CABLE HAS A FRAY AT PULLEY IN BETWEEN BL 0.0 AND LH WING STATION 29.0 MARKED WITH RED TAPE AND CORROSION FOUND ON BOTH LH CABLES AT WS 40.0 PNJun 10, 2025 · N513AE · Cndair CL6002C10SDR DALA2025061004428Servo · excess playSHIP 3162 RIGHT WING, T/E, O/B AILERON SERVO CONTROL WITH PLAY. CORRECTIVE ACTION: REPLACED R/H WING O/B AILERON SERVO CONTROL IAW A319 AMM TASK 27 -14-51-000-001-A AND 27-14-51-400-001-A. (1014247).Jun 9, 2025 · N362NB · Airbus A319114SDR DALA2025061004427Servo · excess playSHIP 3162 RIGHT WING, T/E, I/B AILERON SERVO CONTROL WITH PLAY. CORRECTIVE ACTION: REPLACED R/H WING I/B SERVO AILERON IAW A319 AMM TASK 27-14-51- 000-001-A AND 27-14-51-400-001-A. (1014235).Jun 9, 2025 · N362NB · Airbus A319114SDR DXTA2025052303582Servo · faultedDURING STRAIGHT AND LEVEL FLIGHT AT FL430, BOTH PILOT AND COPILOT CONTROL YOKES WERE CANTED TO THE RIGHT ABOUT 5-10 DEGREES WHILE ALL AILERON INDICATIONS APPEARED TO BE CENTERED. REPLACED FAILING ROLL SERVO. PREFORMED SOFTWARE/CONFIG LOADS AND OPS CHECK WITH May 21, 2025 · N501QS · Cessna 680ASDR KCSA20250527029Aileron · stuckFAILS CONTROL CHECK RIGHT OUTBOARD AILERON REMAINS UP. REFERENCE LOGBOOK ENTRY 100231222/100231226 FOR AILERON CONTROL CABLE REPLACEMENT, AILERON ADJUSTMENT AND TEST. PERFORMED AILERON ADJUSTMENT TEST IAW B747-400 AMM 27-11-00 ALL CHECKS GOOD. 100231223- REFERMay 20, 2025 · N742CK · Boeing 747446SDR SWAA2025060570883Balance Weight · corrodedDOT #114-041. RIGHT WING MOST INBOARD AILERON BALANCE BAY; INBOARD TWO WEIGHTS SHOW EVIDENCE OF CORROSION. <[01] REMOVED AND REPLACED RIGHT WING AILERON BALANCE BAY#5 BOTTOM AILERON; INBOARD TWO WEIGHTS IAW AMM 27-11-31-000-801 STEP 2. E. (1) (C) AND SRM 51-60May 14, 2025 · N961WN · Boeing 7377H4SDR DXTA2025042303176Actuator · defectiveRIGHT AILERON TRIM: DURING DESCENT THROUGH FL230 AILERON TRIM WAS APPLIED TO CORRECT A LEFT YOKE DISPLACEMENT AND FAILED TO RESPOND. AILERON TRIM WAS INOPERATIVE FOR CORRECTIVE TRIM IN BOTH DIRECTIONS. CORRECTIVE ACTION; REPLACED RH AILERON TRIM ACTUATOR IAW CApr 22, 2025 · N827QS · Textrn TEXTRON700SDR 2025FA0000275Control Cable · brokenAILERON CARRY THROUGH CABLE HAS BROKEN STRANDS IN THE LEFT WING AT STATION 71.125.Apr 15, 2025 · N197MC · Cessna 172SSDR AALA202504285876Rod · excess playAIRCRAFT IN BASE MAINTENANCE: RIGH HAND WING LOWER TRANSLATETING PANEL JUST INBOARD OF PYLON INBOARD FORWARD AND MIDDLE SUPPORT RODS HAVE PLAY AT LOWER ENDS. REMOVED AND REPLACED WITH NEW BEAM AT THE RIGTH HAND WING LOWER TRANSLATING PANEL JUST INBOARD OF PYLOApr 13, 2025 · N847NN · Boeing 737823SDR AALA202504130655Computer · faultedAIRCRAFT WAS NOT GROUNDED: DFW-GDL AIR INTERRUPTED BACK TO DFW ON ACCOUNT OF MAINTENANCE:FLIGHT CONTROL ELAC 1 FAULT. MAINTENANCE REPLACED ELAC 1 IAW AMM TASK 27-93-34.Apr 11, 2025 · N809AW · Airbus A319132SDR UIEA2025040300432Pca · leakingRH WING, REAR SPAR, INBOARD AILERON, BOTH PCA´S WITH HYDRAULIC LEAK.(<P>AILERON PCAS (2 EAS) WERE REPLACED (SN: 1133 PN: 282800-1009 & SN: 1196 PN: 282800-1009). CHECKED FOR LEAKS & NO LEAK FOUND. ADJUSTMENT AND TESTS WERE SATISFACTORY. ALL WORKS IAW AMM 27-11Apr 5, 2025 · N1381A · Boeing 767316SDR UIEA2025040400434Pbe · leakingWING LH, INBOARD AILERON, BOTH PCA'S WITH LEAK.(<P>BOTH PCA'S, WERE REPLACED, ADJUSTED AND TESTED. (SN: 0683 PN: 282800-1011 & SN: 280 PN: 282800-1007) TEST WAS SATISFACTORY AND NO LEAK FOUND. ALL WORK IAW AMM: 27-11-48-022-003, AMM 27-11-48-422-040 AND 27-11-Apr 5, 2025 · N1381A · Boeing 767316SDR BIGA20250328001Control Cable · frayedAILERONS WERE BEING MOVED THROUGH THEIR RANGE DURING STATIC TRAINING AND IT WAS NOTED THAT THEY WERE STIFF AND AN ODD SOUND WAS REPORTED. UPON INVESTIGATION A TECHNICIAN FOUND THAT THE ROUTING THROUGH THE CENTER WING BOX PULLEY AT STATION 442 WAS INCORRECT, LMar 24, 2025 · N991BH · Dhav DHC8106SDR DXTA2025031802688Bearing · bindingCAPTAIN CONTROL YOKE: CAPTAINS CONTROL YOKE HAS A VERY PRONOUNCED CLICKING SOUND JUST BEFORE YOU REACH FULL LEFT AND RIGHT DEFLECTION CORRECTIVE ACTION; REMOVED AND REPLACED THE WORN BEARINGS P/N MB540 DDNFC AND MB541 DDNFC, SHAFT P/N 600-90103-3 & QUADRANT ASMar 14, 2025 · N234QS · Cndair CL6002B16SDR F3LA202503170200Servo · faultedLEFT AILERON SERVO (33CE3) REQUIRES REPLACEMENT DUE TO F/CTL AIL.SERVO FAULT. REF LP 346030-1 FOR CONTINUED T/S. REF 1226683. REMOVED AND REPLACED LH AILERON SERVO (33LE3) IAW AMM 27-14-51-000/400-001-A OPS TEST GOOD. TW: F9TAB13169C DD: 09-2025) TW: F9TAB12Mar 11, 2025 · N364FR · Airbus A320251NSDR DXTA2025030302545Actuator · intermittentAILERON CNTRL FAULT AMBER CAS: AILERON CNTRL FAULT AMBER CAS DISPLAYED IN FLIGHT AFTER DEPARTURE. REPLACED AILERON RATIO CHANGER ACTUATOR IAW CE-680A AMM 27-17-00, 27-17-20. OPS CHECK SATISFACTORY. NO DEFECTS NOTED.Feb 28, 2025 · N631QS · Cessna 680ASDR CALA2025031900489Control Servo · damagedFOUND RH INBOARD AILERON SERVO CONTROL ROD UNABLE TO FULLY RETRACT. INSPECTED ATTACH POINTS, HARDWARE AND VERIFIED NEW SERVO CONTROL SN# 5430 EFFECTIVE FOR AC AND POSITION 33CE2 "RH INBOARD" PER RII 09-25-05 REMOVED RIGHT INBOARD AILERON SERVO CONTROL ACTUATORFeb 27, 2025 · N819UA · Airbus A319131SDR ABXA20250221048Aileron Sys · malfunctionedDURING FLIGHT CONTROL CHECK ON TAXI OUT THE AILERONS WOULD NOT MOVE. AFTER APPROX 5 ATTEMPTS THE AILERONS (YOKE) OPERATED NORMALLY.A/C RETURNED TO THE GATE (BTB) MTX GROUNDED A/C. MTX PERFORMED OPERATIONAL TEST IAW B767 AMM 27-11-00 OPS CHECK GOOD AT THIS TIMFeb 21, 2025 · N774AX · Boeing 767281SDR UIEA2025021600149Pcu · faultedRT INBOARD AILERON INDICATION MISSING. FLT CONTROL HYD POWER WING SHUTOFF SWITCHES SELECTED TO CLOSED ON P61 PANEL.(<P>1.PARTIALLY REMOVED INBD ALERON POWER CONT PACKAGE PER AMM 27-11-12-002-001 STEP F(1)(I). ACCOMPLISHED REMOVAL OF INBD AILERON AS PER AMM 2Feb 16, 2025 · N445MC · Boeing 7474B5FSDR ABXA20250130026Control Cable · dirtyDURING TAXI CREW PERFORMED FLIGHT CONTROL CHECKS AND REPORTED FLIGHT CONTROLS BINDING WHEN TURNING YOKE TO THE LEFT , SAME WITH FLAPS 0+5. AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC .PERFORMED GVI OF INBOARD AND OUTBOARD AILERON AND COMPONENTS. ALL LOOKJan 30, 2025 · N317CM · Boeing 767338SDR UIEA2025011600071Pca · leakingRIGHT WING INBOARD AILERON, PCA´S WITH LEAK EVIDENCE.(<P>RIGHT WING INBOARD AILERON, PCA´S LH, AND RH WERE REPLACED I.A.W AMM 27-11-48-022-003. NO FURTHER DEFECTS NOTED</P>)Jan 22, 2025 · N1399A · Boeing 767306SDR UIEA2025012000090Pca · leakingLH WING INBOARD AILERON INBOARD PCA WITH EVIDENCE HYDRAULIC LEAK.(<P>INBOARD PCA WAS REPLACED I.A.W. AMM 27- 11-48-422-040, REV. 144, DATE: DEC. 22, 2024. TORQUE APPLIED: ROD END: 1200 IN- LB, S/N: 0808504320. INBOARD AILERON ADJUSTMENT AND OPERATIONAL TEST WEJan 22, 2025 · N1399A · Boeing 767306SDR DXTA2025012702083Gust Lock · installedAILERON CONTROL: PLEASE EVALUATE THE AILERONS AND CABLES. THE PLANE WAS LEFT OVERNIGHT WITH THE GUST LOCK ENGAGED AND THE YOKE LEVEL. WHEN WE ARRIVED TO PREFLIGHT THE NEXT DAY, WE FOUND THE GUST LOCK STILL ON, THE YOKE MOVED FULL LEFT, THE LEFT AILERON UP AND Jan 22, 2025 · N779QS · Bombdr BD1001A10SDR 4DPA2025012200001Actuator · no discrepancyTASK 27-12-01-720-001-A04 AILERON DAMPER ACTUATOR FUNCTION CHECK DISCOVERED OVERDUE. HAD CREW RETURN TO BURBANK. CORR ACTION MX COMPLETED FNC CHECK NO DEFECTS NOTED AND VDRP BEING FILED.Jan 22, 2025 · N915JX · Emb EMB145LRSDR SCNA20250102001Aileron · lack of lubeON APPROACH WITH FLAPS 30, GEAR EXTENDED, HYD B QTY WAS 69-70% AND PRESSURE AT 2870. AILERONS BEOND 10-15 DEGREES OF BANK WERE VERY STIFF AND HARD TO GET BEOND. CONTROLS REMAINED STIFF ON ROLL OUT UNTIL FLAPS RETRACTED. LUBRICATED AILERON POGO QUADRANT PER AJan 1, 2025 · N825SY · Boeing 7378F2SDR QXEA2025010200338Pcu · out of rigCONTROL WHEEL HAS SPONGY RESISTANCE JUST PRIOR TO LEFT HARDSTOP. REMOVED FROM SERVICE. RFORMED AILERON CONTROL SYSTEM OPERATIONAL TEST REF AMM TASK 27-10-00-710-801-A. NOTED BOTH CONTROL YOKES HAVE MORE SPONGY RESISTANCE PRIOR TO HARDSTOPS ON LEFT DEFLECTIONSDec 31, 2024 · N656QX · Emb ERJ170200LRSDR QXEA2024123000325Control Cable · out of adjustFLIGHT 2115. LEFT AILERON STOP SPONGEY INDICATES FULL DEFLECTION ON FLT CONTROL PAGE REMOVED FROM SERVICE. INSPECTED EXTERIOR PORTION OF AILERON CABLES AND CHECKED FOR FREEDOM OF MOVEMENT. NO ADDITIONAL DEFECTS NOTED. CHECKED AILERON CABLE TENSION AND FOUNDDec 29, 2024 · N656QX · Emb ERJ170200LRSDR DALA2024122411993Seal · failedSHIP 3737 -MISC- DECLARED EMERGENCY INTO ATL DUE TO ABNORMAL FLIGHT CONTROL FEEL DURING ROLL MANEUVERS. CHECKED AILERON SPRING CARTRIDGE, RATIO CHANGER INPUT ROD, VERIFIED CABLE TENSIONS, GREASED AILERON POWER LEVER. FOUND UPPER AILERON POWER CONTROL UNIT B Dec 23, 2024 · N3737C · Boeing 737832SDR DALA2024122311909Receptacle · corrodedSHIP 3136 CORROSION ELECTRICAL RECEPTACLE FIN (7541VC) AND (7543VC) INTERCONNECTING STRUT I/B FLAP LH WING (2 EA). CORRECTIVE ACTION: REPLACED ELECTRICAL RECEPTACLE FIN (7541VC) AND (7543VC) ON INTERCONNECTING STRUT I/B FLAP LH WING (2 EA) AS PER A320 FAM AWM Dec 21, 2024 · N336NB · Airbus A319114SDR DXTA2024122001565Servo Control · inoperativeCLIMBING THROUGH 39,000 FT WHILE DOING A LEFT TURN. WHEN WINGS ARE RETURNING TO LEVEL THERE IS A BIND IN THE CONTROLS AND THEN A RELEASE. ONLY HAPPENS WITH AUTOPILOT ON AND TURNING LEFT. REMOVED SUSPECT FAILED ROLL SERVO GEARBOX PN: 011-02214-10 SN:2Q700885Dec 16, 2024 · N931QS · Cessna 680ASDR VLAR20241211001Control Cable · brokenAUTOPILOT FAILED, WILL HOLD ALTITUDE, WILL NOT TRACK HEADING BUT OR NAV TRACK. SQUAWK WAS ENTERED ON 12/5/2024 AT 2117, SQUAWK UPDATED ON 12/06/2024.REMOVED ACCESS PANELS ON RH WING, FOUND CABLE PN 0522647-3 BROKEN.THE CABLE HAS TWO PARTS: A SHORT CABLE (PN: 0Dec 9, 2024 · N110S · Cessna 172SSDR DALA2024120611497Actuator · no testSHIP 6804 AILERON TRIM ACTUATOR FAILED FREE PLAY CHECK OF BEARING AT STEP 9(A) PER CC# 2711-01030-01. CORRECTIVE ACTION: AILERON TRIM ACTUATOR FAILED FREE PLAY CHECK OF BEARING AT STEP 9(A) PER CC# 2711-01030-01. AILERON TRIM ACTUATOR WAS REPLACED ON CC # 0015Dec 4, 2024 · N706TW · Boeing 7572Q8SDR YENA2024120201523Pressure Switch · leakingFLT#1203, EWR-SDQ. (AIRCRAFT DIVERTED TO MCO) 'HYD Y RSVR LO LVL ECAM AT FL 350 1 HOUR INTO FLIGHT. PERFORMED ECAM ACTIONS AND QRH; FOUND YELLOW HYD MANIFOLD PRESS SWITCH LEAKING OUT OF SPLIT ORING AT (10CE1) REPLACED ORING PER AMM 27-92-01 REPLENISHED Y HYD RNov 26, 2024 · N524JB · Airbus A320232SDR SCNA20241126377Aileron Sys · lack of lubeDEFECT 777651: AILERONS REQUIRE EXCESSIVE FORCE TO CONTROL AIRPLANE IN ROLL AXIS. RESOLUTION: PERF AILERON CONTROL WHEEL FORCE TEST IAW AMM 27-11-00. FORCE REQUIRED IS WITHIN LIMITS ABOUT 1LBS BELOW TRESHOLD. PER FIM 27-11 TASK 804. PULLEYS AND CABLES ON BOTH Nov 25, 2024 · N7949A · Boeing 73786NSDR 2024F00300Control Cable · chafedDURING TASK 27-60-00-2200, FOUND RH WING AILERON OUTPUT CABLE CHAFFING DRAIN TUBE NEXT TO SPOILER MIXER BOX. REMOVED EXISTING DRAIN TUBE FROM AIRCRAFT. REPAIRED DRAIN TUBE PER NJA RFTS-112277, REV 0, TITLE: N315QS (680-0220) WATER DRAIN LINE CHAFE, DATED: 15NONov 21, 2024 · N315QS · Cessna 680ASDR ASAA2024111453842Aileron Sys · unknownON DEPARTURE NOTICED EXTENSIVE PLAY IN CONTROL YOKE LATERAL MOVEMENT. BOTH PILOTS CONFIRMED ABNORMAL AILERON FEEL. AILERON FELT AS THOUGH IT WAS STICKING IN POSITION. CONDITION PERSISTED AT ALL SPEEDS FLOWN AND WITH FLAPS UP AND IN THE EXTENDED POSITION. RETURNov 14, 2024 · N309AS · Boeing 737990SDR 2025F00001Control Cable · wornAILERON 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 FLNov 4, 2024 · N208AV · Cessna 560CESSNASDR 2025F00000Control Cable · wornAILERON 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 FLINov 4, 2024 · N208AV · Cessna 560CESSNASDR 2024FA0000989Control Cable · wornRIGHT WING UPPER INBOARD AILERON CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED AT WS 111.62. THE MANUFACTURER HAS NO APPROVED REPAIR OR ALTERATION FOR THIS ISSUE OTHER THAN REPLACING THE CABLE. THNov 4, 2024 · N208AV · Cessna 560CESSNASDR 2024FA0000988Control Cable · wornLEFT WING UPPER INBOARD AILERON WING CONTROL CABLE FREQUENTLY WEARS BEYOND MANUFACTURER'S LIMITS WHERE THE CABLE PASSES THROUGH A FAIRLEAD LOCATED AT WS 111.62. PROPER FLIGHT CONTROL RIGGING HAS BEEN VERIFIED MULTIPLE TIMES. THE MANUFACTURER HAS NO APPROVED RENov 4, 2024 · N208AV · Cessna 560CESSNASDR SCNA20241104355Bearing · lack of lubeDEFECT 735267: FLIGHT CONTROLS ARE EXTREMELY STIFF ON ROLL AXIS. - - RESOLUTION: INSPECTED AILERONS AND AILERON FEEL AND CENTERING UNIT SPRINGS IAW AMM 27-11-81. NO DEFECTS NOTED. LUBED AILERON POWER OUTLET LEVERS AND BEARINGS IAW AMM 12-22-11. PERFORMED OPS CNov 3, 2024 · N7949A · Boeing 73786NSDR DXTA2024110401002Disconnect Unit · defectiveDURING CONTROL CHECK CAP`S YOKE TURNED RT, THEN LT, THEN BACK TO CENTER, COPILOTS YOKE STAYED IN A FULL LT TURN WHEN CAPS WAS BROUGHT BACK TO CENTER. DURING TAXI BACK, WAS A NOTICEABLE CLICKING SOUND ANYTIME YOKE MOVED. DUPLICATED SQK. PER ENGINEERING, CHKD Oct 30, 2024 · N932QS · Cessna 680ASDR QXEA2024090900206Unknown · unknownMORE ROLL FORCE THAN USUAL NEEDED WHILE HAND FLYING ON APPROACH/LANDING. REMOVED FROM SERVICE. PERFORMED OPS TEST OF AILERON CONTROL SYSTEM PER E175 AMM 27-10-00-710-801-A. OPS TEST GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.Sep 9, 2024 · N639QX · Emb ERJ170200LRSDR 2024FA0000702Control Cable · frayedFOUND BOTH AILERON CABLES P/N MC0510105-324 FRAYED AT OUTBOARD PULLEY. AILERON CABLES TSN: 2973.9Sep 9, 2024 · N73707 · Cessna 172NSDR FDEA202409051244Actuator · failedAFTER STARTING #1 ENG, AILERONS DEFLECTED FULL LEFT AND WOULD NOT RETURN TO CENTER. AUTOPILOT WAS VERIFIED OFF. . WITH ALL HYD SYSTEMS PRESSURIZED AND THE GREEN AND YELLOW SERVOS OFF THE RIGHT AILERON IS DEFLECTING RIGHT WING UP. NOTED HYD LINES AT THE AUSep 5, 2024 · N667FE · Airbus A300F4605R
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