# Service difficulty reports: JASC 2710

A list on [JASC 2710](https://openairdocs.org/jasc/2710.md).

Reports filed under 2710 · Aileron Control System, newest first.

Page 1 of 60 · 2,967 reports

- [SDR DXTA2026101510145](https://openairdocs.org/sdr/DXTA2026101510145.md): Aileron Sys · jammed · Oct 11, 2026 · N116QS · Bombdr BD7001A11
  > AILERON JAMMED IN CRUISE FLIGHT. BOTH SIDES AFFECTED. WAS ABLE TO SLOWLY TURN THE AIRCRAFT. POURING RAIN FOR HOURS BEFORE OUR DEPARTURE. PICTURES ARE OF WATER DRAINING FROM AILERON AT DESTINATION.
- [SDR AALA202609292228](https://openairdocs.org/sdr/AALA202609292228.md): Bearing · excess play · Sep 25, 2026 · N945AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: CAPTAIN'S YOKE HAS ABNORMAL TRAVEL WHEN HAND FLYING. WITH AUTO PILOT OFF, SMOOTH NON TURBULENT AIR, AND NO CONTROL INPUTS, THE YOKE CAN BE ROCKED FORWARD AND BACKWARD, ABOUT THE VERTICAL CONTROL COLUMN. THE BASE OF THE YOKE IS NOT FULLY
- [SDR CALA2026092219658](https://openairdocs.org/sdr/CALA2026092219658.md): Flt Controls · faulted · Sep 18, 2026 · N73270 · Boeing 737824
  > EXCESSIVE AMOUNTS OF TRIM REQUIRED TO MAINTAIN STRAIGHT FLT. UNABLE TO INPUT REQUIRED TRIM, NECESSARY TO MAINTAIN LEVEL FLIGHT. DEBRIEF OF CREW. FLIGHT CREW REPORTED EXCESSIVE AILERON TRIM TO MAINTAIN LEVEL FLT. AUTOPILOT WAS NEVER ENGAGGED. FOUND ACFT WAS
- [SDR SIMA20260910002](https://openairdocs.org/sdr/SIMA20260910002.md): Yoke · loose · Sep 10, 2026 · N781EJ · Emb ERJ170100SU
  > YOKE LOSE AFTER TAKEOFF AS SOON AS ACFT ROTATED CA YOKE JERKED TO THE RT. CONTINUED FLYING, YOKE WAS ABNORMALLY LOOSE & MORE PRONOUNCED WITH RT INPUT AND FO SIDE YOKE WAS NOT RESPONDING TO THE LEFT SIDE YOKE IN SYNC. ACFT WAS CONTROLLABLE WITH ENOUGH INPUT ON
- [SDR CALA2026091119369](https://openairdocs.org/sdr/CALA2026091119369.md): Pca · faulted · Sep 10, 2026 · N664UA · Boeing 767300
  > REPEAT WRITEUP. LT WING INBD AILERON NOT FULLY STOWED INFLIGHT. MULTIPLE FLT CONTROL ISSUES ON FINAL DUE TO WINGS HAVING MISMATCHED AILERON POSITIONS & RT WING HAVING TO CORRECT FOR LT WINGS POSITION. LT INBD AILERON SITTING HIGH IN FLT, ACRT ON RT AUTOPIL
- [SDR AALA202609079995](https://openairdocs.org/sdr/AALA202609079995.md): Aileron Sys · out of adjust · Sep 2, 2026 · N986AN · Airbus A321231
  > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT ROLLS RIGHT 4 DEGREES WHENEVER THE AUTOPILOT IS DISENGAGED AND ROLL MUST BE MANUALLY CORRECTED - MAINTENANCE ADJUSTED THE LEFT AILERON *AALA202609073540* AND THE RIGHT AILERON *AALA202609079995* PER AMM 27-14-00-820-001-A
- [SDR AALA202609073540](https://openairdocs.org/sdr/AALA202609073540.md): Aileron · out of adjust · Sep 2, 2026 · N986AN · Airbus A321231
  > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT ROLLS RIGHT 4 DEGREES WHENEVER THE AUTOPILOT IS DISENGAGED AND ROLL MUST BE MANUALLY CORRECTED - MAINTENANCE ADJUSTED THE LEFT AILERON *AALA202609073540* AND THE RIGHT AILERON *AALA202609079995* PER AMM 27-14-00-820-001-A
- [SDR REXA2026091401769](https://openairdocs.org/sdr/REXA2026091401769.md): Bearing · failed · Aug 24, 2026 · N549CA · Cndair CL6002D24
  > RUDDER PCU SYSTEMS NR 1 & 2 FAILED BOTH PCU AND BEARING BACKLASH. SYSTEM NR 1 PCU MEASURED 0.330IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.180IN WITH A MAX OF 0.120IN. SYS NR 2 PCU MEASURED 0.273IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.135IN
- [SDR CALA2026072117914](https://openairdocs.org/sdr/CALA2026072117914.md): Packing · torn · Jul 21, 2026 · N673UA · Boeing 767322
  > C HYD QTY EICAS. FOUND HYD LEAK AT RT WING. SERVICED CENTER HYD SYSTEM TO.70 FOR TROUBLESHOOTING LEAK CHECK. IAW AMM 12-12-01. FOUND RT WING INBD AILERON INBD ACTUATOR ACTIVELY LEAKING. R & R RIGHT WING INBD AILERON INBD ACTUATOR PACKING IAW ECRA 2710
- [SDR ASAA2026071967455](https://openairdocs.org/sdr/ASAA2026071967455.md): Pcu · faulty · Jul 19, 2026 · N457AS · Boeing 737990ER
  > AIRCRAFT ROLLED RIGHT AS AIRSPEED INCREASED USED EXCESSIVE AILERON TRIM, ATTEMPTED TO COMPENSATE WITH RUDDER TRIM. AT CRUISE THERE WAS (FL360) SHUDDERING AT.78 SLOWED TO.75 AND SHUDDERING WAS SIGNIFICANTLY LESS. USED AILERON TRIM W/ A/P OFF BUT DID NOT CORRE
- [SDR DXTA2026070608655](https://openairdocs.org/sdr/DXTA2026070608655.md): Actuator · failed · Jul 2, 2026 · N956QS · Cessna 680A
  > DURING TAKEOFF & CRUISE, RETRIMED R WING DOWN CAS MSG CONSTANTLY DISPLAYED. RAN QRH BUT MSG WOULD NOT CLEAR. DISCONNECTED AUTOPILOT & PLANE ROLLED LEFT. AFTER ADDING ADDITIONAL AILERON TRIM RT, WAS ABLE TO FLY STRAIGHT & LEVEL. DURING ARRIVAL, W/ AUTOPILOT
- [SDR DALA2026070203885](https://openairdocs.org/sdr/DALA2026070203885.md): Computer · faulted · Jul 1, 2026 · N342DN · Airbus A321213
  > DE - DUE TO F/CTL AIL SERVO FAULT ECAM WARNING. CORRECTIVE ACTION: RIGHT GREEN INBOARD AILERON SERVOCONTROL (33CE2) PLACED ON MEL AND CONTINUE. LATER, WIRING CHECK PERFORMED BETWEEN ELAC 1 AND SERVOCONTROL (33CE2), NTF. REPLACED ELAC 1. (LP 8344088 - AIRCRAFT
- [SDR JR2R20260701868](https://openairdocs.org/sdr/JR2R20260701868.md): Fitting · cracked · Jul 1, 2026 · N86324 · Emb ERJ170200LL
  > RIGHT MLG W/W, AILERON QUADRANT CRACKED ON THE O/B SIDE. REPLACED
- [SDR 5OKA202606250133](https://openairdocs.org/sdr/5OKA202606250133.md): Skin · debonded · Jun 22, 2026 · N713BL · Gulstm G280
  > MULTIPLE STRUCTURAL FAILURES OF THE R/H AILERON DUE TO DELAMINATION/DEBONDING. THESE EVENTS HAVE OCCURRED ON THE SAME AILERON THREE SEPARATE TIMES, AND A LOANER AILERON ONCE. ADDITIONALLY, THERE HAVE BEEN TWO IMPROPER AILERON RIGGING EVENTS BY GULFSTREAM TECHN
- [SDR CALA2026062217255](https://openairdocs.org/sdr/CALA2026062217255.md): Computer · faulty · Jun 21, 2026 · N433UA · Airbus A320232
  > AILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F- CTL F/CTL AIL SERVO FAULT IN FLIGHT ON CLIMB OUT DURING MOD TURBULENCE. REMOVED AND REPLACED ELAC1 REF AMM TASK 27-93-34-400-001-A, OPS. CHECK SAT, NO FURTHER DEFECTS NOTED.
- [SDR 4TXA2026062200531](https://openairdocs.org/sdr/4TXA2026062200531.md): Control Cable · broken · Jun 21, 2026 · N624XA · Boeing 73786J
  > AFTER TAKE OFF FROM ELP NOTICED A SLIGHTLY UNUSUAL AMOUNT OF AILERON TO MAKE A TURN AND RETURN TO STRAIGHT AND LEVEL. UPON DESCENT WITH SPEED BRAKE DEPLOYED, THE AELERON DEFLECTED FULL RIGHT. UPON LANDING HAD TO USE FULL DEFLECTION TO MAINTAIN CENTERLINE. ON T
- [SDR DALA2026061103531](https://openairdocs.org/sdr/DALA2026061103531.md): Solenoid · faulted · Jun 11, 2026 · N509DT · Airbus A321271NX
  > ATB - DUE TO AIRFRAME VIBRATIONS THAT WORSENED ABOVE 300KTS. CREW NOTICED RT AILERON INDICATION FLUTTERING AFTER LANDING. REPLACED RH AILERON CONTROL SOLENOID AND SERVO VALVE ON 33CE4.
- [SDR SWIA2026052576035](https://openairdocs.org/sdr/SWIA2026052576035.md): Aileron · stuck · May 25, 2026 · N626SY · Emb ERJ170200LL
  > RIGHT AILERON STUCK (FLIGHT 5940) INTERROGATED CMC AND FOUND FAULT CODE 27030528FCS FORCE FIGHT BETWEEN RIGHT AILERON PCUS ON RIGHT WING PER FIM 27-03-00. ALONG WITH FLIGHT CONTROL NO DISPATCH. REMOVED AND REPLACED RIGHT AILERON OUTBOARD PCU PER AMM 27-12-
- [SDR VNAA202606300014](https://openairdocs.org/sdr/VNAA202606300014.md): Hinge Fitting · corroded · May 14, 2026 · N530EA · Cndair CL6002C10
  > CORROSION AROUND OF THE BOLTS AND RUSTED BOLTS ON BONDING JUMPERS 1,2,3,4, LT AILERON HINGE FITTING. HINGE FITTING NBR 3 ON LH AILERON WAS CLEANED AROUND OF THE BOLTS OF BONDING JUMPER AND AFTER CLEAN DVI WAS PERFORMED AND NOT CORROSION WAS FOUND IAW SRM 51-2
- [SDR IPXA2026052405432](https://openairdocs.org/sdr/IPXA2026052405432.md): Control Wheel · corroded · May 9, 2026 · N412UP · Boeing 75724APF
  > COPILOTS CONTROL WHEEL OUTER SKIN CORRRODED RH SIDE. INSTALLED SERVICEABLE COPILOTS AILERON CONTROL WHEEL AND ADAPTER IAW AMM 27-11-02-424-010 TW ID:19-983 DD:09/03/2026
- [SDR IPXA2026051661700](https://openairdocs.org/sdr/IPXA2026051661700.md): Actuator · leaking · May 7, 2026 · N301UP · Boeing 76734AF
  > FOUND LT OUTBOARD AILERON OUTBOARD SIDE ACTUATOR LEAK. AMM 27-11-49-422-028 REV.148 STEP 3A TO 3H(7) INSTALL LT WING OUTBOARD AILERON OUTBOARD SIDE PCA.
- [SDR IPXA2026051661667](https://openairdocs.org/sdr/IPXA2026051661667.md): Pca · leaking · May 7, 2026 · N301UP · Boeing 76734AF
  > FOUND LT INBD AILERON INBOARD SIDE ACTUATOR LEAK. IAW AMM 27-11-48-422-040 REV.148 STEP 3A TO 3H(7) INSTALLED LT WING INBOARD AILERON INBOARD SIDE PCA.
- [SDR IPXA2026042428272](https://openairdocs.org/sdr/IPXA2026042428272.md): Actuator · leaking · Apr 16, 2026 · N332UP · Boeing 76734AF
  > FOUND THE OUTBOARD SIDE PCA OF LEFT WING OUTBOARD AILERON HYDRAULIC LEAK. I.A.W AMM 27-11-49-422-028 REV.147 STEP 3.A TO 3.H(7) INSTALLED LH WING OUTBOARD AILERON OUTBOARD SIDE PCA.
- [SDR IPXA2026042471246](https://openairdocs.org/sdr/IPXA2026042471246.md): Actuator · leaking · Apr 13, 2026 · N332UP · Boeing 76734AF
  > FOUND RT LCC ACTUATOR LEAKING. IAW AMM 27-11-14-424-016 REV.147 STEP 3.A TO STEP 3.F(9), INSTALLED RH WING LCCA.
- [SDR UIEA2026040200119](https://openairdocs.org/sdr/UIEA2026040200119.md): Aileron Sys · deflection · Apr 2, 2026 · N485MC · Boeing 74745EF
  > UPON LANDING, ACFT REQUIRED NEARLY FULL RT AILERON DEFLECTION DURING ROLLOUT TO KEEP WINGS LEVEL. WINDS WERE SUCH THAT LT AILERON DEFLECTION SHOULD HAVE BEEN REQUIRED. SUSPECT A POSSIBLE SPOILER OR LE FLAP ISSUE. PERFORMED C/B RESET & SPEED BRAKE GROUND OPS
- [SDR 2026FA0000250](https://openairdocs.org/sdr/2026FA0000250.md): Cable · frayed · Mar 30, 2026 · N811CP · Cessna 182T
  > WHILE TROUBLESHOOTING A FUEL LEAK THE MECHANIC NOTICED THAT THE AILERON CARRY THROUGH CABLE WAS FRAYED.
- [SDR JR2R20260303391](https://openairdocs.org/sdr/JR2R20260303391.md): Fitting · cracked · Mar 3, 2026 · N86312 · Emb ERJ170200LL
  > RH W/W AILERON QUADRANT FITTING CRACKED. REPLACED
- [SDR 2026FA0000088](https://openairdocs.org/sdr/2026FA0000088.md): Fairlead · frayed · Feb 5, 2026 · N9347T · Cessna 172S
  > WE HAVE NOTICED A TREND IN (STAINLESS STEEL) AILERON CABLE WEAR ON RH AILERON CROSSOVER CABLE P/N 0510106-365 AT FAIRLEAD P/N 0560065-2 RH WING STATION 57.68. ON OUR AIRCRAFT, N9347T 172S S/N 11166 TT: 6524, THE CABLE HAS FRAYED WIRES DUE TO WEARING ON THE FAI
- [SDR 2026FA0000087](https://openairdocs.org/sdr/2026FA0000087.md): Fairlead · frayed · Feb 5, 2026 · N172HG · Cessna 172S
  > WE HAVE NOTICED A TREND IN (STAINLESS STEEL) AILERON CABLE WEAR ON RH AILERON CROSSOVER CABLE P/N: 0510106-365 AT FAIRLEAD P/N 0560065-2 RH WING STATION 57.68. ON OUR AIRCRAFT, N172HG 172S S/N 11139 TT: 7109.8, THE CABLE HAS FRAYED WIRES DUE TO WEARING ON THE
- [SDR DALA2026012700613](https://openairdocs.org/sdr/DALA2026012700613.md): Strut · corroded · Jan 21, 2026 · N377NW · Airbus A320211
  > CORROSION ON INTERCONNECT STRUT LT WING. REFERENCE RII AMDS CARD 27 51-9202. REMOVED INTERCONNECT STRUT LT WING ON UNSERVICEABLE CONDITION IAW AMM 27-51-44-000 -001-A. REPLACED THE INTERCONNECT STRUT LT WING IAW AMM 27-51-44 -000-001-A & INSTALLATION TO
- [SDR 1Q2R2026080550084](https://openairdocs.org/sdr/1Q2R2026080550084.md): Lock Tab · broken · Jan 12, 2026 · N523AE · Cndair CL6002C10
  > LEFT AILERON PCU TENSION REGULATOR TO PCU LINK ASSY HAS BOTH LOCK TABS BROKEN OFF. PERFORMED PERMANENT REPAIR WITH REPLACEMENT OF TENSION REGULATOR TO PCU LINK ASSY IAW RFTS-126593, REV. 0, AND EA 2711-2026-0040, REV-.
- [SDR ASAA2025122063292](https://openairdocs.org/sdr/ASAA2025122063292.md): Pcu · faulty · Dec 20, 2025 · N625AS · Boeing 737790
  > UPON DISENGAGED AUTOPILOT A THE A/C WOULD NOT RESPOND TO CONTROL INPUTS TO TURN LEFT. ACFT COULD TURN RT. ATTEMPTED ANOTHER TURN TO THE LT AT APPROXIMATELY 3 UNITS OF AILERON ROLL THE ROLL STOPPED. ROLLED RIGHT TO THE LEFT SEVERAL TIMES BEFORE WE HAD CONTROL;
- [SDR ABXA20251215341](https://openairdocs.org/sdr/ABXA20251215341.md): Bearing · corroded · Dec 15, 2025 · N219CY · Boeing 767383
  > ON TAXI OUT, CONTROL CHECK ON AILERON DID NOT PASS CHECK. CAME BACK TO GATE FOR HELP WITH MAINTENANCE. (BTB). FOUND AILERON CENTERING MECHANISM CENTERING CAM FOLLOWER BEARING CORRODED. REMOVED AND REPLACED BEARING IAW B767 AMM 20-11-00. FURTHER T/S REQUIRE
- [SDR DALA2025112608645](https://openairdocs.org/sdr/DALA2025112608645.md): Rod End · excess play · Nov 26, 2025 · N346NB · Airbus A319114
  > LEFT AILERON WITH PLAY AT PCA ROD ENDS. CORRECTIVE ACTION: R/R LT INBD AND LT OTBD SERVO CONTROL ACTUATORS PER WC 2714-4001. (7652718).
- [SDR FDEA202511262208](https://openairdocs.org/sdr/FDEA202511262208.md): Aileron Sys · abnormal · Nov 26, 2025 · N175FE · Boeing 7673S2F
  > DURING THE BEFORE TAKEOFF CHECKLIST ON THE FLIGHT CONTROL CHECK, THE AILERONS TOOK ABNORMALLY EXCESSIVE FORCE TO ACTIVATE THE SYSTEM ON BOTH CA & FO YOKE. PERFORMED TROUBLESHOOTING OF AILERONS. PERFORMED GVI OF ALL ACCESSIBLE PULLYS AND CABLES. MEASURED FO
- [SDR ABXA20251112295](https://openairdocs.org/sdr/ABXA20251112295.md): Warning Message · illuminated · Nov 12, 2025 · N760CK · Boeing 767341
  > ON CLIMB OUT, RECEIVED AILERON LOCKOUT EICAS MESSAGE. AFTER LANDING, MTX DEFERRED AILERON LOCKOUT SYSTEM IAW MEL ABX 27-11-2 PLACARD INSTALED MX PROCEDURES ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE.
- [SDR DALA2025111208289](https://openairdocs.org/sdr/DALA2025111208289.md): Servo Control · excess play · Nov 11, 2025 · N354NB · Airbus A319114
  > RIGHT WING AILERON SERVO CONTROL GREEN HAS PLAY, IT HAS 10.38 MM. R & INBD AILERON SERVO CONTROL (33 CE2) IAW DELTA WORK CARD 2714-4001. (1299294).
- [SDR DALA2025111208288](https://openairdocs.org/sdr/DALA2025111208288.md): Servo Control · excess play · Nov 11, 2025 · N354NB · Airbus A319114
  > RIGHT WING AILERON SERVO CONTROL BLUE HAS PLAY, IT HAS 10.01 MM. REPLACED OTBD AILERON SERVO CONTROL (33 CE2) IAW DELTA WORK CARD 2714-4001. (1299284).
- [SDR DALA2025111408347](https://openairdocs.org/sdr/DALA2025111408347.md): Servo Control · faulted · Nov 10, 2025 · N333NB · Airbus A319114
  > ATO - AT 60 KNOTS DUE TO F/CTL AIL SERVO FAULT ECAM WARNING. RIGHT GREEN AILERON SERVOCONTROL (33CE2) PLACED ON MEL. REPLACED RIGHT INBOARD AILERON ACTUATOR. (LP 7734854)
- [SDR ABXA20251024279](https://openairdocs.org/sdr/ABXA20251024279.md): Aileron Sys · faulted · Oct 24, 2025 · N290CM · Boeing 767383
  > AT 10000 FT SPD 240KTS EICAS MESSAGE AILERON LOCKOUT MSG APEARED..ACFT LANDED SAFELY. MTX GROUNDED ACFT AND MTX DEFERRED THE AILERON LOCKOUT SYSTEM.IAW ABX MEL-27-11-2. AND RETURNED AC TO SERVICE.
- [SDR ABXA20251023278](https://openairdocs.org/sdr/ABXA20251023278.md): Warning Message · illuminated · Oct 23, 2025 · N219CY · Boeing 767383
  > AILERON LOCKOUT EICAS WHEN SLOWED TO 250 KTS. AFTER AC LANED MTX GROUNDD ACFT AND TOUBLESHOT IAW FIM 27-11 FT 804, FOUND FAULT BULB ON LT SAM. SWAPPED SAM P/N 285T001S-117 / S/N. 000276 WITH SAM S/N D01364 / P/N 285ST001S-116. NO HELP. ORIGINAL SAM REINSTALLED
- [SDR 2025FA0000690](https://openairdocs.org/sdr/2025FA0000690.md): Mec · smoke · Oct 8, 2025 · N100AL · Gulstm GVI
  > CREW MET ON ARRIVAL, LT AILERON MCE CONFIRMED TO HAVE STRONG BURNED ODUR AND SOOTING EVIDENT ABOVE UNIT AND ON ADJACENT STRUCTURE. WIRING HARNESS VISUALLY INSPECTED, NO DEFECTS APPARENT. EBHA CB'S INSPECTED IN TAIL COMPARTMENT. L AILERON BRAKER FOUND TO HAVE T
- [SDR J7SA2025090500457](https://openairdocs.org/sdr/J7SA2025090500457.md): Control Cable · low tension · Aug 26, 2025 · N532FX · Bombdr BD1001A10
  > DURING SCHEDULED MAINTENANCE WHILE RE-TENSIONING AILERON CABLE, DISCOVERED LH WING CABLE SAWING THROUGH PULLEY BRACKET. REPLACED LH AILERON WING PULLEY BRACKET IAW CL300 SRM 51-40-08 AND 51-42-36. LH WING AILERON CABLE REPLACED AND TENSIONED IAW AMM 27-11-35-0
- [SDR F3LA202508200285](https://openairdocs.org/sdr/F3LA202508200285.md): Servo Valve · failed · Aug 19, 2025 · N341FR · Airbus A320251N
  > AIRCRAFT WAS UNDERGOING SERVICE CHECK DURING RON MAINTENANCE AND WORKING MDDR# 1235083, NO FLIGHT DELAY. LP599245 ITEM 1 F/CTL AIL SERVO FAULT PLACED ON MEL 27-14-01B CN 1235081 PLACARD INSTALLED AND R/H WING INBOARD SERVO VALVE 33CE2 DEACTIVED. REMOVED AND
- [SDR CALA2025080707427](https://openairdocs.org/sdr/CALA2025080707427.md): Aileron Sys · malfunctioned · Aug 3, 2025 · N13110 · Boeing 757224
  > AS PER CAPTAIN: AFTER AIRBORNE, ACFT PULLED VERY STRONG TO THE RT. CAPTAIN ENGAGED AUTOPILOT CAUSING ACFT TO PULL EVEN HARDER TO RT. CAPTAIN DISENGAGED AUTOPILOT. ACFT PULLED TO LT. CAUSING TO ABORT FLT & RETURN TO GATE. PERFORMED MCDP BITE, LAST FLT FA
- [SDR ABXA2025081167](https://openairdocs.org/sdr/ABXA2025081167.md): Warning Message · illuminated · Aug 1, 2025 · N783AX · Boeing 767281
  > DURING TAXI, LEFT INBOARD AILERON POSITION DISAGREEMENT WITH THE INDICATOR ON THE LOWER STATUS PAGE. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-27-08-1. AIRCRAFT RETURNED TO SERVICE.
- [SDR IPXA2025071825183](https://openairdocs.org/sdr/IPXA2025071825183.md): Aileron Sys · no discrepancy · Jul 14, 2025 · N578UP · Boeing 74745E
  > DURING CLIMB OUT AILERON FORCE WERE A LITTLE HEAVIER THAN NORMAL AND RIGHT AILERON REQUIRED SIGNIFICANTLY MORE FORCE THEN LEFT AILERON. PERFORM ROTATIONAL TORQUE CK OF BOTH YOKES IAW AMM 27-11-00-705-091. WITH IN LIMITS.
- [SDR F3LA202507140268](https://openairdocs.org/sdr/F3LA202507140268.md): Servo Valve · faulted · Jul 11, 2025 · N341FR · Airbus A320251N
  > LP461953 #2 ON CLIMB OUT IN A RIGHT TURN PLANE SHOOK VIOLENTLY SPEED 320 ALT 260 FOLLOWED BY FLT CTL AIL SERVO FAULT. FOLLOWED TSM 27-10-00-810-820-A, REMOVED AND REPLACED RH AILERON INBD SERVO CONTROL (33CE2) PER A320 AMM 27-14-51-000-001-A, 27-14-51-400-00
- [SDR N6WA2025071002](https://openairdocs.org/sdr/N6WA2025071002.md): Link · corroded · Jul 8, 2025 · N513GJ · Cndair CL6002C11
  > LH AILERON PCU LINKS HAVE CORROSION INSIDE DIAMETER. REMOVED AND REPLACED LH AILERON PCU LINKS, BUSHINGS AND HARDWARE IAW CRJ AMM 27-15-14.
- [SDR N6WA2025071001](https://openairdocs.org/sdr/N6WA2025071001.md): Bushing · corroded · Jul 8, 2025 · N513GJ · Cndair CL6002C11
  > RH AILERON PCU LINK HAVE CORROSION ON THE INSIDE DIAMETER. REMOVED AND REPLACED AILERON BUSHINGS AND HARDWARE IAW CRJ AMM 27-14-15.

Next page: https://openairdocs.org/jasc/2710/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/jasc/2710/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
