# Service difficulty reports: JASC 2722

A list on [JASC 2722](https://openairdocs.org/jasc/2722.md).

Reports filed under 2722 · Rudder Actuator, newest first.

Page 1 of 6 · 284 reports

- [SDR QXEA2026080700172](https://openairdocs.org/sdr/QXEA2026080700172.md): Pcu · malfunctioned · Aug 5, 2026 · N637QX · Emb ERJ170200LR
  > FLIGHT 2152. DURING FLT HAD TWO EVENTS OF EXCESSIVE RT YAW MOVEMENTS. FIRST EVENT FL280 IN CRUISE FOR ABOUT 5 SECS, EVENT SELF CORRECTED. SECOND EVENT ON INITIAL DESCENT SUDDEN MOVEMENT TO RT. LASTED 2-3 MINUTES. AP WAS MANUALLY DISCONNECTED & YAW TRIM USE
- [SDR SIMA20260626001](https://openairdocs.org/sdr/SIMA20260626001.md): Actuator · leaking · Jun 26, 2026 · N748RR · Emb ERJ170100SE
  > HYD LO QTY 3 RECEIVED IN FLIGHT. 18% INITIAL. DOWN TO 14% UPON LANDING. EMERGENCY VEHICLES SAW HYDRAULIC FLUID LEAKING AT A SIGNIFICANT RATE FROM THE TAIL SECTION OF THE AIRCRAFT. IT IS STILL DRIPPING WITH AIRCRAFT DE-ENERGIZED AND POWERED OFF. "TRANSFERRED TO
- [SDR DALA2025061204479](https://openairdocs.org/sdr/DALA2025061204479.md): Servo Control · excess play · Jun 11, 2025 · N362NB · Airbus A319114
  > SHIP 3162 EMPENNAGE RUDDER YELLOW SERVO CONTROL HAS PLAY, IT HAS 11,40MM. CORRECTIVE ACTION: PERFORMED FUNCTIONAL CHECK OF RUDDER SERVO CONTROL AND HINGE LINE BEARINGS FOR EXCESSIVE PLAY I.A.W A319 AMM TASK 27-24-00- 200-803-A. REE PLAY WAS 8,02MM REV 131 DATE
- [SDR DALA2025061204470](https://openairdocs.org/sdr/DALA2025061204470.md): Servo Control · excess play · Jun 11, 2025 · N362NB · Airbus A319114
  > SHIP 3162 EMPENNAGE RUDDER GREEN SERVO CONTROL HAS PLAY, IT HAS 12,18MM. CORRECTIVE ACTION: PERFORMED FUNCTIONAL CHECK OF RUDDER SERVO CONTROL AND HINGE LINE BEARINGS FOR EXCESSIVE PLAY I.A.W A319 AMM TASK 27-24-00- 200-803-A. FREE PLAY WAS 8,33MM REV 131 DATE
- [SDR DALA2025061204469](https://openairdocs.org/sdr/DALA2025061204469.md): Servo Control · excess play · Jun 11, 2025 · N362NB · Airbus A319114
  > SHIP 3162 EMPENNAGE RUDDER BLUE SERVO CONTROL HAS PLAY, IT WAS 11,30MM. CORRECTIVE ACTION: PERFORMED FUNCTIONAL CHECK OF RUDDER SERVO CONTROL AND HINGE LINE BEARINGS FOR EXCESSIVE PLAY I.A.W A319 AMM TASK 27-24-00- 200-803-A. FREE PLAY WAS 8,20MM REV 131 DATED
- [SDR COEA2025060404913](https://openairdocs.org/sdr/COEA2025060404913.md): Skin · punctured · Feb 24, 2025 · N913FX · Aerosp ATR42300
  > WO 262007 NR 5 HEAVY CHECK COE/MAJOR REPAIR: R/H ELEVATOR LOWER MAIN SKIN PUNCTURED. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00256910_01...25117 ISS A, DATED 5/21/2025.
- [SDR DALA2024121711763](https://openairdocs.org/sdr/DALA2024121711763.md): Actuator · leaking · Dec 15, 2024 · N317US · Airbus A320211
  > UPON ARRIVAL AT GATE FLIGHT ATTENDANTS IN AFT REPORTED SMELLING WET SOCK ODOR AND FLIGHT ATTENDANTS IN THE FORWARD SMELLED SAME ODOR UPON OPENING DOOR. FLT CREW DID NOT COMPLETELY FILL OUT SMOKE AND FUME QUESTIONNAIRE. RAN PACKS OFF ENG1 BLEED, ENG 2 BLEED, A
- [SDR 2024F00259](https://openairdocs.org/sdr/2024F00259.md): Switch · faulted · Oct 18, 2024 · N365M · Bombdr BD1001A10
  > AIRCRAFT DEPARTED KHOU AND WAS AT CRUISE ALTITUDE. THE RUDDER TRIM WENT FULL RIGHT WITHOUT ANY INPUT. THE FLIGHT CREW DISENGAGED THE AUTOPILOT AND YAW DAMP, THEN RE-ENGAGED AUTOPILOT AND YAW DAMP. THE ISSUE WENT AWAY. THE FLIGHT CREW THEN RETURNED BACK TO KHOU
- [SDR DALA2024062406452](https://openairdocs.org/sdr/DALA2024062406452.md): Actuator · excess play · Jun 22, 2024 · N361NB · Airbus A319114
  > EXCESSIVE PLAY ON SERVO CONTROL ACTUATOR BLUE HYDRAULIC SYSTEM UPPER POSITION ON VERTICAL STABILIZER. REPAIRED PER AMDS CARD 2724-2010.
- [SDR SWIA20240301228](https://openairdocs.org/sdr/SWIA20240301228.md): Control Panel · faulted · Feb 28, 2024 · N823SK · Cndair CL6002D24
  > ON CLIMB OUT, RUDDER TRIM RAN AWAY NOSE RIGHT, COMPENSATED WITH RUDDER, WE RAN IT BACK TO CENTER, BEGAN TO RUN AWAY AGAIN AFTER RE-CENTERING. NO LONGER RAN AWAY, QRH RUN, RETURNED TO FIELD. (FLIGHT 3785 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITE
- [SDR SWIA202402290008](https://openairdocs.org/sdr/SWIA202402290008.md): Trim System · malfunctioned · Feb 28, 2024 · N823SK · Cndair CL6002D24
  > ON CLIMB OUT, RUDDER TRIM RAN AWAY NOSE RIGHT, COMPENSATED WITH RUDDER, WE RAN IT BACK TO CENTER, BEGAN TO RUN AWAY AGAIN AFTER RE-CENTERING. NO LONGER RAN AWAY, QRH RUN, RETURNED TO FIELD. (FLIGHT 3785 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
- [SDR AALA202402267978](https://openairdocs.org/sdr/AALA202402267978.md): Actuator · defective · Feb 22, 2024 · N823AW · Airbus A319132
  > AIRCRAFT WAS GROUNDED: DURING CLIMB WHEN ENGAGING AUTOPILOT, RUDDER TRIM RESET TO 0.0 (ZERO) AND AIRCRAFT WAS IN AN AIRCRAFT WAS GROUNDED: SLIP WITH SEVERAL DEGREES OF BANK. DISENGAGED AUTOPILOT, MANUALLY TRIM THE RUDDER, AND RE-ENGAGED THE AUTOPILOT. RUDDER T
- [SDR DALA2024013101404](https://openairdocs.org/sdr/DALA2024013101404.md): Servo · faulted · Jan 31, 2024 · N336NB · Airbus A319114
  > SHIP 3136 AIRFRAME VIBRATION STARTED AT 13000'. CORRECTIVE ACTION: REMOVED AND REPLACED BLUE AND GREEN RUDDER SERVOS PER AMDS CARD 2720-7001. (4203608)
- [SDR DALA2024010200014](https://openairdocs.org/sdr/DALA2024010200014.md): Unknown · unknown · Dec 31, 2023 · N506DN · Airbus A350941
  > SHIP 3506 - ATB - DUE TO (F/CTL RUDDER DOUBLE ACTUATOR FAULT) ECAM MESSAGE. CORRECTIVE ACTION: REPLACED YELLOW RUDDER ACTUATOR 2034CY, RCCB AND EHA. (LP 5103453)
- [SDR DALA2023092908034](https://openairdocs.org/sdr/DALA2023092908034.md): Unknown · unknown · Sep 27, 2023 · N169DZ · Boeing 767332
  > SHIP 1601 -MISC/DE- CREW ELECTED DE DUE TO LT HYD QTY DECREASE DURING FLIGHT. C/W QRH AND LANDED AND TAXIED IN NORMALLY. / CORRECTIVE ACTION: REPLACED LEFT HYDRAULIC SYSTEM RUDDER PCA.
- [SDR SWI2023F00417](https://openairdocs.org/sdr/SWI2023F00417.md): Unknown · chafed · Jul 25, 2023 · N728SK · Cndair CL6002C10
  > RUDDER LEADING EDGE SHROUD RH SIDE CHAFED. (C-CHECK RO 10/4/2023) BLENDED OUT RUDDER LEADING EDGE SHROUD RH SIDE PER CRJ-700 SRM 51-12-00-001-001-A01 REF-CRJ-700 SRM 51-12-00-001-001 A01, REO 670-55-41-123 REV -- DATE 2023-08-15COMPLIED WITH TASK 51-900
- [SDR AALA202307203630](https://openairdocs.org/sdr/AALA202307203630.md): Actuator · malfunctioned · Jul 18, 2023 · N679AW · Airbus A320232
  > AIRCRAFT WAS GROUNDED: AT FL 310 UNCOMMANDED RUDDER L1.5 ON RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR F3LA2023031000030](https://openairdocs.org/sdr/F3LA2023031000030.md): Ruddervator · uncontrollable · Mar 8, 2023 · N323FR · Airbus A320251N
  > DISCREPANCY: RUDDER TRIM SYSTEM MADE 4 UNCOMMANDED TRIM INPUTS BETWEEN 1.3 AND 1.9 UNITS RIGHT. RUDDER TRIM RETURNED TO NEUTRAL WITHIN 1 MINUTE OF EACH EVENT. CORRECTIVE ACTION: AS PER TSM 22-62-00-810-809-A STEP 4A CONTINUITY CHECK PERFORMED. REMOVED AND REP
- [SDR CALA2022100602729](https://openairdocs.org/sdr/CALA2022100602729.md): Limiter · warning message · Oct 6, 2022 · N440UA · Airbus A320232
  > RUD TRVL LIMITER CAUTNIFLIGHT. RAN ECAM. DIDNOT RESOLVE. RUDDER A CTED NORMAL ON LNDING FLT CREW REPORTED ''RUD TRV LIM SYS'' FAULT. CYCLED FAC1&2 TWICE, NO HELP. LOCKED FOR POSITIVE FIX. PILOT DECLARED AND EMERGENCY COMING. INTO SFO. CANNOT JUST TEST AND S
- [SDR SWIA202164508](https://openairdocs.org/sdr/SWIA202164508.md): None · cracked · Dec 22, 2021 · N771SK · Cndair CL6002C10
  > RH RUDDER FEEL UNIT SUPPORT STRUCTURE OTBD LOWER CHANNEL AT APPROX. FS202.75 - FS222.76 RBL26.00 IS CRACKED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW FABRICATED RH RUDDER FEEL UNIT SUPPORT STRUCTURE OTBD LOWER CHANNEL PN: CC670-94231-4 AT APPROX.
- [SDR RJEF20210707001](https://openairdocs.org/sdr/RJEF20210707001.md): Actuator · malfunctioned · Jul 6, 2021 · N522TA · Airbus A319132
  > DURING FLIGHT AFTER 10000FT RH AILERON WITH RUDDER TRIM MAKE THE PLANE TO FLIGHT WITH APROX 10DEG BANK ANGLE. FOLLOWING TSM 27-20-00-810-804-A REV 56 THE RUDDER TRIM ACTUATOR (10CC) WAS REMOVED AND REPLACED IAW AMM 27-22-51-000-001-A REV 56 AND AMM 27-22-51-4
- [SDR AALA202103159003](https://openairdocs.org/sdr/AALA202103159003.md): Actuator · defective · Mar 13, 2021 · N925UY · Airbus A321231
  > AIRCRAFT WAS GROUNDED: DURING CRUISE, RUDDER HAD 2 SMALL UNCOMMANDED INPUTS THAT NOTICEABLY MOVED NOSE APPROXIMATELY 2-3 DEGREES WITHIN 1 SECOND. AUTO PILOT ON. REPLACED RUDDER TRIM ACTUATOR (10CC)AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-22
- [SDR CNQR](https://openairdocs.org/sdr/CNQR.md): Sensor · misinstalled · Feb 11, 2021 · Cessna 680CE
  > RUDDER POSITION SENSOR ATTACHMENT TO THE RUDDER HAS A SPACER THE IS INSTALLED BETWEEN THE POSITION SENSOR PUSHROD AND ATTACH BRACKET. THIS INCORRECT INSTALLATION OF THE SPACER WOULD NOT ALLOW THE RUDDER TO GO FULL LEFT TRAVEL. THE PUSHROD WOULD CONTACT THE
- [SDR 9JLA2021020425650](https://openairdocs.org/sdr/9JLA2021020425650.md): Actuator · defective · Jan 15, 2021 · N800WS · Cessna 680SOV
  > THE FLIGHT CREW REPORTED THAT ON PREFLIGHT CHECKS THAT THE RUDDER BIAS CONTROLS FELT VERY WEAK ON BOTH SIDES. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE RUDDER BIAS ACTUATOR WAS DEFECTIVE. THE RUDDER BIAS ACTUATOR WAS REMOVED AND REPLACED WITH
- [SDR 9JLA2020120929950](https://openairdocs.org/sdr/9JLA2020120929950.md): Actuator · leaking · Nov 24, 2020 · N307RM · Raythn HAWKER800XP
  > THE FLIGHT CREW REPORTED THAT DURING POST FLIGHT CHECKS HYDRAULIC FLUID LEAKING FROM BOTH SIDES OF THE VERTICAL STAB AND UNDERNEATH THE HORIZONTAL STAB. THE MAINTENANCE VENDOR DISCOVERED THAT THE RUDDER SERVO ACTUATOR WAS LEAKING EXTERNALLY. THE SERVO WAS RE
- [SDR AALA202010119013](https://openairdocs.org/sdr/AALA202010119013.md): Actuator · faulty · Oct 10, 2020 · N124US · Airbus A320214
  > AIRCRAFT WAS GROUNDED. MILD UNCOMMANDED LEFT YAW AT 23500 FT IN CLIMB. NO RUDDER LIMIT ECAM. AT 27000 FT CRUISE, UNCOMMANDED RIGHT YAW TRIM FROM 0.2L TO 1.2R AND HELD. AUTO PILOT OFF AND RETURNED. AUTOPILOT ON RETURNED NORMAL. FOUND AFS TEST FAULTING RUD
- [SDR QXEA2020080500231](https://openairdocs.org/sdr/QXEA2020080500231.md): Control Panel · inoperative · Aug 5, 2020 · N440QX · Bombdr DHC8402
  > RUDDER TRIM SWITCH INOPERATIVE WHEN ATTEMPTING TO MOVE RUDDER TO THE LEFT. TRIM SWITCH DRIVES RUDDER TO THE RIGHT NORMALLY. WHEN ATTEMPTING TO RECENTER RUDDER THERE IS NO MOVEMENT ON PFCS. REMOVED FROM SERVICE. R & R AILERON / RUDDER TRIM CONTROL PANEL IAW AM
- [SDR AALA201907119010](https://openairdocs.org/sdr/AALA201907119010.md): Actuator · faulted · Jul 10, 2019 · N822AW · Airbus A319132
  > AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING CLIMB OUT WE HAD AN AUTO FLT RUD TRV LIM SYS ECAM, THE FIRST STEP OF THE ECAM ACTION WAS FAC1 ON/OFF WHICH CAUSED THE RUDDER TO JUMP SOME, THEN CLEARED THAT ECAM BEFORE COMPLETEING FURTHER STEPS. WHEN THE INFLIGHT RU
- [SDR A6WA201904126549](https://openairdocs.org/sdr/A6WA201904126549.md): Elevator System · abnormal · Apr 10, 2019 · N440AW · Cndair CL6002B19
  > ON TAKE OFF AC REQUIRED EXCESSIVE BACK PRESSURE TO ROTATE. ELEVATOR CONTROLS FEEL HEAVY AND SLOW TO REACT TO CONTROL WHEEL INPUTS. AC CAN BE TRIMMED FOR FLT. DID NOT ENGAGE AUTOPILOT. THERE IS SLACK IN THE CONTROLS (EXCESSIVE HYSTERESIS) COORDINATED WITH DISP
- [SDR IPXA2018081762888](https://openairdocs.org/sdr/IPXA2018081762888.md): Skin · dented · Aug 9, 2018 · N424UP · Boeing 75724APF
  > RUDDER HAD A DENT BETWEEN RUDDER STA. 131.108. 20 INCHES FROM THE TE, 31 INCHES TO THE LOWER EDGE OF PANEL. REPAIRED IAW RCD 097310, EO B757-5540-69569-A, AND EA 757-5540-27-A2303, REV-.
- [SDR HALA2018070700322](https://openairdocs.org/sdr/HALA2018070700322.md): Actuator · leaking · Jul 7, 2018 · N592HA · Boeing 7673CB
  > AIR TURN BACK LEFT HYD QTY LOSS TO.70RF (STARTED FLIGHT WITH.94) REPEAT WRITEUP SEE PAGE 731445 AIR TURN BACK. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW AMM 27-21-15. OPS CHECK NORMAL.
- [SDR RAIA201805180001](https://openairdocs.org/sdr/RAIA201805180001.md): Actuator · faulty · May 18, 2018 · N14116 · Emb EMB145XR
  > AIRCRAFT REPORTED RUDDER SHAKING VIOLENTLY/VIBRATING. R&R RUDDER ACTUATOR. OPS CHECK PENDING ARRIVAL OF NEW BUSHING. OPS CHECK GOOD. WILL UPDATE LATER WITH INFORMATION ON ACTUATOR CHANGE.
- [SDR CALA2017102703772](https://openairdocs.org/sdr/CALA2017102703772.md): Pca · leaking · Oct 25, 2017 · N69059 · Boeing 767424ER
  > C HYD QTY EICAS ENROUTE. EMERGENCY DECLARED. INSPECTED AND FOUND HYD. LEAK AT RT ELEVATOR INBD PCA. LEAK COMING FROM PISTON ACTUATOR HOUSING. REMOVED AND REPLACED RIGHT ELEVATOR INBD PCA IAW AMM 27-31-05. ALL OPS CHECK AND LEAK CHECKED GOOD.
- [SDR DALA2017102107760](https://openairdocs.org/sdr/DALA2017102107760.md): Bearing · migrated · Oct 20, 2017 · N823DX · Boeing 75726D
  > INPUT BELLCRANK BEARINGS HAVE PLAY BETWEEN INNER AND OUTER RACES WITH THE RT BEARING MIGRATING IN BORE ON THE CENTER PCU. REMOVED AND REPLACED THE RUDDER CENTER PCU INPUT BELLCRANK IAW AMM 27-21-52, PERFORMED A SATISFACTORY OPS CHECK IAW AMM 27-21-20.
- [SDR PNSA2016100502](https://openairdocs.org/sdr/PNSA2016100502.md): Switch · malfunctioned · Oct 5, 2016 · N665PA · Saab 340B
  > ON SHORT FINAL WITH Y.O. OFF, RUDDER TRIM MOVED FULL SCALE LEFT. UNABLE TO USE TRIM SWITCHES TO RETURN TO CENTER. UPON SHUT DOWN RUDDER TRIM FULL SCALE RIGHT UNABLE TO USE TRIM SWITCHES TO RETURN TO CENTER AFTER DE PLANNING RUDDER SWITCHES HAD AN UNCOMMANDED R
- [SDR DALA2016090606420](https://openairdocs.org/sdr/DALA2016090606420.md): Spring Assy · corroded · Sep 5, 2016 · N901DE · Doug MD88
  > RUSTED PISTON END AT RUDDER TRIM TAB ACTUATOR ON AFT ACCESSORY COMPARTMENT. RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REMOVED AND INSTALLED IAW AMM 27-207. AREA AT SHAFT OF RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REWORKED MEASUREMENT ORIGINAL 0.686" AND MINIMUM RE
- [SDR IPXA2016061804758](https://openairdocs.org/sdr/IPXA2016061804758.md): Actuator · inoperative · Jun 18, 2016 · N292UP · Doug MD11F
  > YAW UPPER A "OFF" USING AP/2. AFTER THIS FAILED, RUDDER CONTINUED TO KICK, PULSATE, EVERY 20-30 SEC'S. NO EMERGENCY DECLARED. REMOVED UPPER RUDDER ACTUATOR IAW MM 27-23-30, MW 13151255 6/11/16, PERFORMED A GVI ON ALL HOOK UP POINTS OK TO INSTALL. TRANSFERR
- [SDR CA151230004](https://openairdocs.org/sdr/CA151230004.md): Control Servo · leaking · Dec 30, 2015 · Airbus A320211
  > (CAN) ACFT DECLARED AN EMERGENCY DUE TO THE LOSS OF THE GREEN HYD SYS. ACFT DID REQUIRE A TOW OFF THE RUNWAY AS THEY WERE UNABLE TO STEER ACFT. RESOLUTION FOUND GREEN HYD SYS RUDDER SERVO CONTROL LEAKING. REPLACED GREEN SYSTEM RUDDER SERVO CONTROL IAW AMM 2
- [SDR RJEF20150928001](https://openairdocs.org/sdr/RJEF20150928001.md): Actuator · faulty · Sep 26, 2015 · N687TA · Airbus A320233
  > PREVIOUS TO DEPART AS FLIGHT TA561. THE ACFT SHOWED THE FOLLOWING NO DISPATCH FAILURE MSGS. FLIGHT CONTROL RUDDER TRAVEL LIMIT 2 FAULT MSG ON ECAM. FOR THIS FAILURE IT WAS PERFORMED FAULT ANALYSIS IAW TSM 22-61-00-810-804-A BY RESETTING THE FAC 2 & TESTING
- [SDR DXTA2015052206021](https://openairdocs.org/sdr/DXTA2015052206021.md): Actuator · failed · May 18, 2015 · N385QS · Cessna 680CE
  > NO TAKEOFF MSG, DUE TO ROLL SYS. UPON INITIAL OPS CHECKS NOTED NO CAS MSGS. REMOVED THE ACCESS PANEL & INSPECTED THE PROXIMITY SWITCH & TARGET. NOTED THE TARGET IS NOT FULLY CENTERED ON THE PROXIMITY SWITCH. REMOVED THE BELLY PANEL & FURTHER INSPECTED. CO
- [SDR DXTA2015031605995](https://openairdocs.org/sdr/DXTA2015031605995.md): Actuator · leaking · Mar 13, 2015 · N307QS · Cessna 680CE
  > RUDDER LOCKED UP IN FLIGHT. AT LANDING STAGE AFTER 5 HR FLIGHT AUTOPILOT YAW DAMP OFF, REALIZED RUDDER COMPLETELY LOCKED UP. COULD NOT MOVE AT ALL. UPON MAIN GEAR TOUCHDOWN RUDDER RELEASED & OPERATED NORMALLY THROUGH ROLLOUT & TAXI IN. MOVES FREELY ON GND.
- [SDR HALA2015030700030](https://openairdocs.org/sdr/HALA2015030700030.md): Actuator · leaking · Mar 7, 2015 · N583HA · Boeing 76733AER
  > ETOPS SIGNIFICANT SYSTEM, CENTER HYD QTY LOW ON ARRIVAL.55 RF STARTED FLT WITH 1.05. FOUND UPPER RUDDER PCA LEAKING. R & R RUDDER PCA IAW AMM 27-21-02-001, AMM 27-21-02-422-038 LEAK, OPS CHECK OK.
- [SDR WX0A2015030972458](https://openairdocs.org/sdr/WX0A2015030972458.md): Actuator · out of adjust · Mar 5, 2015 · N301NV · Airbus A319112
  > DURING CLIMB OUT & CRUISE WITH AUTO PILOT ON THE ACFT DID NOT SEEM TO TRIM OUT RUDDER. ONCE DESCENDING THE AUTO PILOT DUE TO SIDE SLIP CONDITION WE WERE ABLE TO TRIM OUT THE RUDDER. IT TOOK MORE THAN 2 FULL UNITS TO THE RT TO CTR IT. OVER THE COURSE OF THE
- [SDR ANCF201412121](https://openairdocs.org/sdr/ANCF201412121.md): Actuator · faulty · Dec 11, 2014 · N603AV · Airbus A320233
  > DURING FLIGHT RUDDER TRIM LIMITER FAULT 1 & UNCOMMANDED RUDDER TRIM INPUTS. IAW AMM 27-22-51-000-001-A THE RUDDER TRIM ACTUATOR WAS REMOVED & IAW AMM 27-22-51-400 001-A THE RUDDER TRIM ACTUATOR WAS REPLACED. OPERATIONAL TEST OK. ACTUATOR RUDDER TRIM PN 6137
- [SDR CA140623017](https://openairdocs.org/sdr/CA140623017.md): Control Servo · failed · Jun 22, 2014 · Airbus A320211
  > CREW REPORTED UNUSUAL VIBRATION IN CLIMB AT FL190. THEY BACKED OFF ON SPEED AND PROBLEM DISAPPEARED. WHEN SPEED WAS INCREASED THE SAME PROBLEM RE-OCCURRED. CREW SUSPECTED FLIGHT CONTROL PROBLEMS AND ELECTED TO RETURN. CREW DECLARED A PAN PAN WITH ATC. ACFT LA
- [SDR USAA2014062000006](https://openairdocs.org/sdr/USAA2014062000006.md): Actuator · unserviceable · Jun 18, 2014 · N829AW · Airbus A319132
  > ON TAKEOFF RUNWAY 25R, CREW FELT A HARD PULL TO THE RT. CREW ABORTED TAKEOFF ON RUNWAY & TAXIED BACK TO GATE. BRAKE TEMP ON THE HIGHEST WHEEL WAS 675 ON NR 4 WHEEL WHILE WAITING FOR INSPECTION ON TAXIWAY. INSPECTED FOR EMER APPLICATION OF BRAKES, NO DEFECTS
- [SDR CA140528005](https://openairdocs.org/sdr/CA140528005.md): Actuator · failed · May 25, 2014 · Cndair CL2156B11215
  > (CAN) PILOT REPORTED THAT RUDDER JAMMED AFTER SCOOPING, WHILE TRYING TO MAKE A RT TURN. SELECTED MANUAL MODE AND RUDDER WAS ABLE TO BE MOVED TO THE RT, NOT ABLE TO DUPLICATE ON GROUND.
- [SDR SIMA20140224001](https://openairdocs.org/sdr/SIMA20140224001.md): Actuator · out of adjust · Feb 24, 2014 · N653AE · Emb EMB145LR
  > ON TAKE OFF A/C YAWED TO THE RIGHT ABRUPTLY. WE WERE ABLE TO APPLY LEFT RUDDER PRESSURE AND CONTROL THE AIRPLANE WITH RUDDER, BUT YAW TRIM WAS STUCK IN FULL RIGHT POSITION. AFTER SEVERAL MINUTES OF FLYING WE WERE ABLE TO GET YAW TRIM TO WORK NORMALLY AND RECE
- [SDR USAA2014022700007](https://openairdocs.org/sdr/USAA2014022700007.md): Actuator · faulty · Feb 24, 2014 · N659AW · Airbus A320232
  > DURING CLIMB OUT LT AILERON DEPLOYED ABOVE NORMAL IN FLIGHT LEVEL & MOVES ALONG WITH A CORRESPONDING RT RUDDER DEPLOYMENT RESULTING IN A SKID WHILE CLIMBING. AFTER LEVEL OFF FLIGHT CONTROLS RETURN TO NORMAL & COORDINATED FLIGHT. ADJUSTED RUDDER CABLE & REPLA
- [SDR CA140210003](https://openairdocs.org/sdr/CA140210003.md): Actuator · malfunctioned · Feb 9, 2014 · Cessna 650
  > (CAN) DEPARTING, EXPERIENCED AN UNCOMMANDED RUDDER DEFLECTION TO THE RT SHORTLY AFTER TAKEOFF. AN EMERGENCY WAS DECLARED. THE ACFT CLIMBED TO 8000 FT WITH A UNCOMMANDED RT RUDDER. THE UNCOMMANDED RT RUDDER RETURNED TO NEUTRAL RUDDER. THE ACFT RETURNED.

Next page: https://openairdocs.org/jasc/2722/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 = '2722'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/2722/reports

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