# Service difficulty reports: JASC 2213

A list on [JASC 2213](https://openairdocs.org/jasc/2213.md).

Reports filed under 2213 · Flight Controller, newest first.

Page 1 of 3 · 148 reports

- [SDR 2023FA0000798](https://openairdocs.org/sdr/2023FA0000798.md): Control Tube · sheared · Nov 29, 2023 · N2358Z · Beech 23
  > AIRCRAFT WAS IN DECENT, WHEN PILOT INPUTTED 1/4 TO 1/2 INCH MOVEMENT OF THE CONTROL WHEEL, CONTROLS BECAME LIGHT FOLLOWED BY THE AIRCRAFT SHAKING VIOLENTLY. THE CONTROL YOKE FLUCTUATED BETWEEN FULL FORWARD AND FULL AFT REQUIRING BOTH PILOT AND INSTRUCTOR PILOT
- [SDR AALA202207057998](https://openairdocs.org/sdr/AALA202207057998.md): Control Unit · none · Jul 3, 2022 · N995AN · Airbus A300*
  > AIRCRAFT WAS GROUNDED: APPROXIMATELY 30 MINUTES PRIOR TO LANDING AUTO FLIGHT, #1 FLIGHT CONTROL UNIT (FCU) ECAM FAULT. QRH SYSTEM RESET OK BUT ONLY 5 MINUTES THEN FAULT RE-OCCURRED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT DFW SAFELY WITHOUT FURTH
- [SDR OEJA202202150001](https://openairdocs.org/sdr/OEJA202202150001.md): Control Box · faulted · Feb 10, 2022 · N475FX · Lear 45LEAR
  > WHILE ATTEMPTING T/O FORM JAX TO BNA. IMMEDIATELY AFTER SELECTING T/O POWER, CASS SYSTEM GENERATED A RED "PRIM TRIM INOP" A YELLOW "SEC TRIM FAIL" AND A WHITE "PRI TRIM FAIL". CREW ABORTED TAKE OFF AND TAXIED BACK TO THE FBO. I WAS NOTIFIED RIGHT AWAY AND WE D
- [SDR HALA2022020300033](https://openairdocs.org/sdr/HALA2022020300033.md): None · none · Feb 1, 2022 · N386HA · Airbus A330243
  > SHIP 386 - ATO - DUE TO FMA MALFUNCTION. CORRECTIVE ACTION: NO FAULTS FOUND IN PFR. PERFORMED AUTOLAND TEST. PERFORMED RTO INSPECTION. (8452195)
- [SDR YENA2021111800771](https://openairdocs.org/sdr/YENA2021111800771.md): Fcu · fault message · Nov 18, 2021 · N4058J · Airbus A321271N
  > FLT 20, LHR-JFK. "AUTO FLT FCU 1 FAULT" ECAM MSG ON DESCENT TROUGH 10,000 FT.; TROUBLESHOT PER TSM 22-81-00-810-802-A. R/R FCU PER AMM 22-81-12. ALL FUNCTIONAL TESTS PASSED AT THIS TIME. TSI C/W.
- [SDR YENA2021061800376](https://openairdocs.org/sdr/YENA2021061800376.md): Controller · faulted · Jun 16, 2021 · N763JB · Airbus A320232
  > FLT 150, GND-JFK. WHILE AIRBORNE COMING IN FOR LANDING THERE WAS NO LOCALIZER INFO CORRECT FREQ HAND TUNED STILL NO LOCALIZER GLIDE SLOPE DID DISPLAY BUT NO COURSE GUIDEANCE NO FLAGS, ECAMS OR ANY OTHER MESSAGES; FOUND FMGC2 FAULT ON PFR, RESET FMGC2 PER TSM
- [SDR DALA2021041302176](https://openairdocs.org/sdr/DALA2021041302176.md): Autopilot Sys · failed · Apr 9, 2021 · N695DL · Boeing 757232
  > SHIP 695 CRUSING AT FL 380 SAW A MOMENTARY PUFF OF SMOKE (5 SEC) BEHIND AUTOPILOT SWITCHS ON MCP. SIMULTANEOUSLY ALTITUDE WINDOW CHANGED TO FL 35.5. AIRPLANE REMAINED LEVEL. ALL LIGHTS ON MCP AT1/2 BRIGHTNESS. NO.ODOR. CORECTIVE ACTION: R/R MCP REF B757 AMM 22
- [SDR ASAA2021022234191](https://openairdocs.org/sdr/ASAA2021022234191.md): Dfgs · failed · Feb 22, 2021 · N467AS · Boeing 737990ER
  > MODE CONTROL PANEL ALTITUDE WINDOW FLICKERING. GROUNDED - YES. INITIAL EVALUATION, CONFIRMED DEFECT. REMOVED AND REPLACED DFCS MCP IAW B737-900 AMM 22-11-34-000/400-801, FLICKERING STOPPED. PERFORMED DFCS LRU REPLACEMENT FOR MCP AND LAND VERIFY IAW AMM 22-11-0
- [SDR ASAA2021022234189](https://openairdocs.org/sdr/ASAA2021022234189.md): Dfgs · failed · Feb 22, 2021 · N467AS · Boeing 737990ER
  > HEADING DISPLAY PANEL MODE CONTROL IS FLICKERING. GROUNDED - YES. INITIAL EVALUATION, CONFIRMED DEFECT. REMOVED AND REPLACED DFCS MCP IAW B737-900 AMM 22-11-34-000/400-801, FLICKERING STOPPED. PERFORMED DFCS LRU REPLACEMENT FOR MCP AND LAND VERIFY IAW AMM 22-1
- [SDR 120B2020041500024](https://openairdocs.org/sdr/120B2020041500024.md): Display · inoperative · Apr 11, 2020 · N36NE · Boeing 767323
  > #2 FMS (TIMEOUT) MESSAGE & FMS WOULD NOT AUTO SEQUENCE ON THE POSITION REPORT PAGE.
- [SDR AALA2019081539030](https://openairdocs.org/sdr/AALA2019081539030.md): Controller · unreliable · Aug 11, 2019 · N652AW · Airbus A320232
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 37.0 MANAGED SPEED AT.78, SPEED VAIRIES FROM.76. TO.79 CONTINUOUSLY IN SELECTED SPEED MAINTAIN.78. MAINTENANCE REPLACED FLIGHT CONTROL UNIT IAW AMM-22-81-12. OPS CHECKS GOOD.
- [SDR ASAA2019041172894](https://openairdocs.org/sdr/ASAA2019041172894.md): Sensor · faulted · Apr 7, 2019 · N483AS · Boeing 737990ER
  > WHILE PERFORMING LAND VERIFY AND FMS TC 78222000 - FOUND LEFT AILERON POSITION SENSOR A FAULTY. GROUNDED - YES. PERFORMED AILERON POSITION SENSOR ADJUSTMENT PER B737-900 AMM 22-11-29-820-801, ADJUSTMENT CK'S GOOD. PERFORMED AILERON POSITION SENSOR TEST PER AMM
- [SDR ASAA2019020728126](https://openairdocs.org/sdr/ASAA2019020728126.md): Control Unit · inoperative · Feb 7, 2019 · N923VA · Airbus A321253N
  > FCU 1 INOP GROUNDED - YES. REMOVED AND REPLACED FCU PER AMM 22-81-12. CAT 3 OPS CHECK OK.
- [SDR IPXA2019020138563](https://openairdocs.org/sdr/IPXA2019020138563.md): Computer · odor · Jan 31, 2019 · N256UP · Doug MD11F
  > INSPECTION TYPE:FUMES / ODOR IN COCK PIT. TECH RECOMMENDS: PERFORM BOW TS MD11-3610-00487 TO INSPECT FOR PNEUMATIC DUCT INTGRITY AND TO ASSURE THERE IS NOT ANY FOREIGN OILS. C/W WAN 2859911. C/W WAN 2859911. R/R #2 FCC PER MM 22-11-01-004-026 AND MM 22-11-01-
- [SDR UIEA2017092001749](https://openairdocs.org/sdr/UIEA2017092001749.md): Servo · no test · Sep 17, 2017 · N1327A · Boeing 76737D
  > CENTER AUTOPILOT RUDDER SERVO M278 FAIL DURING TEST. THE SERVO WAS REPLACED.
- [SDR UIEA2017092001751](https://openairdocs.org/sdr/UIEA2017092001751.md): Servo · failed · Sep 17, 2017 · N1327A · Boeing 76737D
  > RIGHT AUTOPILOT RUDDER SERVO M279 FAIL DURING TEST. THE SERVO WAS REPLACED.
- [SDR RJEF20160419001](https://openairdocs.org/sdr/RJEF20160419001.md): Fcu · faulty · Apr 15, 2016 · N687TA · Airbus A320233
  > DURING CLIMB OF FLIGHT TA588, THE PILOT REPORTED FCU ALTITUDE UNABLE TO CHANGE ALTITUDES. DUE THAT SITUATION THE ACFT RETURNED. AFTER AN UNEVENTFUL LANDING, ONCE THE ACFT PARKED AT THE GATE, PERFORMED FAULT ANALYSIS IAW TSM 22-81-00-810-801-A. REPLACED THE
- [SDR CA160222005](https://openairdocs.org/sdr/CA160222005.md): Computer · malfunctioned · Feb 19, 2016 · Boeing 7572B7
  > (CAN) ON DESCENT A "BURNED INSULATION" ODOR WAS NOTED, THE ODOR PERSISTED, BUT NO SMOKE WAS EVIDENT. ON THE GROUND, TROUBLESHOOTING REVEALED THE RT FLIGHT CONTROL COMPUTER HAS INTERNALLY MALFUNCTIONED, CAUSING THE ODOR. THE FCC WAS REPLACED.
- [SDR A6WA201542983](https://openairdocs.org/sdr/A6WA201542983.md): Actuator · failed · Aug 12, 2015 · N438AW · Cndair CL6002B19
  > FLIGHT 3926, WITH AUTOPILOT OFF, RECEIVED UNCOMMANED YAW. COMPLIED WITH IAC & QRH, ISSUE CLEARED WITH YAW DAMPER OFF. INTERROGATED FCC & FOUND NR 2 YAW DAMPER FAILED. R & R NR 2 LINEAR YAW DAMPER ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.
- [SDR CA150112002](https://openairdocs.org/sdr/CA150112002.md): Fmc · failed · Jan 9, 2015 · Airbus A321211
  > (CAN) FMGC 2 AND NAV IR2 FAULT ENROUTE. RESET UNSUCCESSFUL.. FMGC 2 CIRCUIT BREAKER RESET. NO HISTORY. AFS BITE CARRIED OUT THROUGH MCDU NO FAULT. SERV - NAV IR2 RESET. GROUND SCAN AND INTERFACE TEST BITES CARRIED OUT THROUGH MCDU. NO FAULT. CONSIDER SERV.
- [SDR CA150105002](https://openairdocs.org/sdr/CA150105002.md): Fmc · failed · Jan 3, 2015 · Airbus A319114
  > (CAN) AFTER DEPARTING WITH FMGC 2 UNDER MEL THE CREW REPORTED THAT FMCG 1 HAD ALSO FAILED. THE FLIGHT RETURNED TO YVR AND LANDED APPROXIMATELY 3000KG OVERWEIGHT. NO EMERGENCY WAS DECLARED. RESOLUTION NAV DATA SOFTWARE FOUND CORRUPT---LAST MONTHS SOFTWARE RELO
- [SDR CA141229005](https://openairdocs.org/sdr/CA141229005.md): Power Supply · failed · Dec 28, 2014 · Boeing 767375
  > (CAN) AIRCRAFT LOST THE FIRST OFFICER`S FLIGHT DIRECTOR, COMMAND BARS LOST AND AUTOLAND STATUS TO NO LAND 3 THE CREW ALSO HAD A FAINT ELECTRICAL ODOR IN THE COCKPIT. ELECTED TO DIVERT AND DECLARED AN EMERGENCY. RT FCC FOUND TO HAVE A BURNED OUT POWER SUP
- [SDR CA141229004](https://openairdocs.org/sdr/CA141229004.md): Fmc · failed · Dec 28, 2014 · Airbus A319114
  > (CAN) AFTER DEPARTURE, EXPERIENCED NR 1 FMGC FAILURE, A PATCH WAS DONE WITH MOC AND CREW ELECTED TO RETURN TO DEPARTURE. FLIGHT LANDED. NR 1 FMGC WAS REPLACED AND OPS TESTED SERVICEABLE IAW AMM 22-83-34 PB 401.
- [SDR CA140926013](https://openairdocs.org/sdr/CA140926013.md): Fmc · failed · Sep 25, 2014 · Boeing 777333ER
  > (CAN) INCIDENT DETAILS:PAN PAN DECLARED AT 40W DUE TO LOSS OF 2 FMCS. AUTOPILOT SERVICEABLE.REBOOTED SYSTEM,NOW OK,CANX PAN PAN WITH ATC.CARRYING ON RESOLUTION ON THE MAT FOUND MSG 31-83172 NOT ACTIVE. GRND TEST THROUGH MAT TEST PASS. NO FAULT HISTORY.
- [SDR CA140908025](https://openairdocs.org/sdr/CA140908025.md): Computer · failed · Sep 3, 2014 · Cndair CL6002C10
  > (CAN) NON-COMMANDED CHANGE OF FLIGHT DIRECTOR PASSING FL170 IN DESCENT TO FL120, NOTICED CHANGE OF FLIGHT DIRECTOR MODE FROM NAV/VS TO NAV/ALTSCAP, GREEN, WITH A VARIATION OF PITCH FROM -2 DEGREES TO -8 DEGREES, VERTICAL SPEED GOING FROM -2500 FT/MIN TO -4500
- [SDR CA140827004](https://openairdocs.org/sdr/CA140827004.md): Fmc · defective · Aug 26, 2014 · Airbus A319114
  > (CAN) INCIDENT DETAILS: JUST BEFORE TOP OF DESCENT FMGC 2 FAILED, FMGC 1 WAS ALREADY UNSERVICEABLE AND ON MEL RELIEF. THE CREW DECLARED PAN PAN AND AN UNEVENTFUL LANDING WAS CARRIED OUT. NIL ADVERSE REACTION WAS REPORTED BY THE CAPTAIN. RESOLUTION FMGC #1 (FL
- [SDR DALA2014072904255](https://openairdocs.org/sdr/DALA2014072904255.md): Annunciator · failed · Jul 26, 2014 · N922DL · Doug MD88
  > DIVERTED DUE TO SMOKE IN THE COCKPIT. THE CREW REPORTED THE CAPTAIN`S FLIGHT MODE ANNUNCIATOR SMOKING AND ARCING. MAINTENANCE REPLACED THE CAPTAIN`S FMA ALL RTS WERE GOOD.
- [SDR CA140709004](https://openairdocs.org/sdr/CA140709004.md): Indicator · failed · Jul 7, 2014 · Cndair CL6002C10
  > (CAN) CLIMBING IN SPEED MODE WITH THE SPEED BUG SET AT 250 KNOTS THE SPEED BUG MADE AN UNCOMMANDED CHANGE TO 79 KNOTS. NO VERTICAL SPEED CHANGES HAD BEEN MADE RECENTLY ALTHOUGH WE WERE MAKING LATERAL CHANGES OF HEADING AND ALSO INTERCEPTING AN FMS COURSE AROUN
- [SDR CA140926010](https://openairdocs.org/sdr/CA140926010.md): Computer · malfunctioned · Jun 25, 2014 · Cndair CL6002D24
  > (CAN) DURING CLIMB PASSING FL 140. SPEED 290 KNOT. AUTOPILOT ENGAGED (RIGHT PILOT FLYING). SPEED AND NAV. MODE. UNCOMMANDED SPEED CHANGE OBSERVED. SPEEDBUG, JUMPED FROM 290 TO 60 KNOT. FMA SHOWING PITCH - MODE. SPEED MODE REENGADED AND 290 KNOT SET. EVENT BUT
- [SDR CA140306007](https://openairdocs.org/sdr/CA140306007.md): Control Panel · failed · Feb 28, 2014 · Cndair CL6002D24
  > (CAN) UNCOMMANDED FD CHANGE: A SPEED BUG.
- [SDR CA140306006](https://openairdocs.org/sdr/CA140306006.md): Control Panel · malfunctioned · Feb 28, 2014 · Cndair CL6002D24
  > (CAN) UNCOMMANDED FD CHANGE: A FLIGHT MODE CHANGE.
- [SDR SWIA201436230](https://openairdocs.org/sdr/SWIA201436230.md): Circuit Card · failed · Feb 2, 2014 · N495CA · Cndair CL6002B19
  > AUTOPILOT PITCH TRIM CAUTION, AIRCRAFT PITCHED DOWN WHEN AUTOPILOT DISCONNECTED. FLT 2583 REPLACED NR 2 FCC CARD IAW AMM, PN 622-9815-904, SN ON 12TBG & SN OFF 1F3J.
- [SDR CA140207003](https://openairdocs.org/sdr/CA140207003.md): Director · malfunctioned · Jan 28, 2014 · Cndair CL6002C10
  > (CAN) FLIGHT DIRECTOR UNCOMMANDED CHANGE. ON CLIMB, SPEED WENT FROM 280 KTS TO 040 KTS.
- [SDR SWIA201335769](https://openairdocs.org/sdr/SWIA201335769.md): Control Panel · failed · Dec 27, 2013 · N794SK · Cndair CL6002C10
  > AIRCRAFT OSCILLATES UP & DOWN WHEN USING AUTOPILOT. AIRCRAFT FLIES NORMALLY WHEN AUTOPILOT SELECTED OFF. FLT 5652 REPLACED FCP IAW AMM & REPLACED BOOTH FCC CARDS IAW AMM. PN1 822-0044-001, SN1 ON 414, SN1 OFF 18G8Y, PN2 822-1308-320, SN2 ON 21H1N, SN2 OFF 3
- [SDR CA131118017](https://openairdocs.org/sdr/CA131118017.md): Indicator · erratic · Nov 9, 2013 · Cessna 208B
  > (CAN) ON GPS APPROACH, VFR CONDITIONS, THE PILOT NOTICED THAT THE FLIGHT COMMAND INDICATOR WAS OSCILLATION VERTICALLY PRIOR TO THE AUTO PILOT DISCONCERTING. THE APPROACH WAS CARRIED OUT MANUALLY WITH OUT INCONTINENT. MAINTENANCE REPLACED THE FLIGHT COMMAND IN
- [SDR CA131101010](https://openairdocs.org/sdr/CA131101010.md): Indicator · inoperative · Nov 1, 2013 · Cessna 208B
  > (CAN) ON ENGINE START UP AND TAXI THE PILOT NOTICED THE FLIGHT COMMAND INDICATOR NOT RESPONDING TO THE ACFT MOVEMENT. THE ACFT RETURNED TO THE BLOCKS AND MAINTENANCE REPLACED THE UNIT WITH AN O/H UNIT. THE SYSTEM FUNCTION CHECKED SERVICEABLE.
- [SDR CA130621001](https://openairdocs.org/sdr/CA130621001.md): Director · failed · Jun 20, 2013 · Cndair CL6002B19
  > (CAN) DURING CLIMB THROUGH 31,600 CREW OBSERVED PITCH UP COMMAND ON THE FLT DIRECTOR, WITH SPEED INDICATING 59 KTS. SPEED BUTTON SHOWED. 17 KTS. EVENT BUTTON PUSHED AT 1757Z DEFECT RAISED TO PROVIDE DATA FOR OPERATOR ACTION IAW SL 440-SL-22-014A WITH DEFECT NR
- [SDR SIMA20130309001](https://openairdocs.org/sdr/SIMA20130309001.md): Controller · malfunctioned · Mar 9, 2013 · N922AE · Emb EMB145LR
  > ON FLIGHT 3570 THE CREW REPORTED AN ELECTRICAL ODOR FROM THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. VERIFIED STRONG ELECTRICAL BURNT SMELL FROM THE FLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER IAW AMM II CH 22-11-
- [SDR SIMA20130303001](https://openairdocs.org/sdr/SIMA20130303001.md): Controller · faulty · Mar 3, 2013 · N6760A · Piper PA23250
  > ON FLIGHT 2830 THE CREW REPORTED AN UNIDENTIFIABLE ODOR IN THE COCKPIT- POSSIBLY ELECTRICAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ODOR TO BE ORIGINATING FROM THE FLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER IAW EMB-
- [SDR SIMA20130211002](https://openairdocs.org/sdr/SIMA20130211002.md): Controller · malfunctioned · Feb 11, 2013 · N696AE · Emb EMB145LR
  > ON FLIGHT 3307 THE CREW REPORTED THAT ON FINAL APPROACH THEY NOTICED STRONG ELECTRICAL FUMES IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL SMELL COMING FROM AUTOFLIGHT GUI
- [SDR CA130118011](https://openairdocs.org/sdr/CA130118011.md): Control Panel · failed · Jan 18, 2013 · Airbus A319114
  > (CAN) AFTER DEPARTURE, THE FLIGHT CREW ENCOUNTERED FAILURES OF BOTH FLIGHT DIRECTORS AND THE AUTOPILOT SYSTEM. THE FLIGHT CREW DIVERTED BACK AND LANDED APPROXIMATELY 3000 KGS OVER THE MAXIMUM STRUCTURAL LANDING WEIGHT. THERE WAS NO EMERGENCY DECLARED AND THER
- [SDR 2013F00012](https://openairdocs.org/sdr/2013F00012.md): Potentiometer · malfunctioned · Dec 11, 2012 · N42CF · Piper PA31310
  > SMOKE COMING FROM AUTOPILOT CONTROLLER.
- [SDR UALA2012111406557](https://openairdocs.org/sdr/UALA2012111406557.md): Fcu · malfunctioned · Nov 13, 2012 · N461UA · Airbus A320232
  > FCU DISPLAY MALFUNCTIONING CLIMB-DESCENT. VERTICAL SPEED WINDOW SHOWS ZEROS IN OPEN CLIMB. REPLACED FCU PER MM WITH KNOWN GOOD UNIT FROM ACFT 4019. ACCOMPLISHED OPERATIONAL TEST OF THE AFS PER 22-96-00 AND LAND CAT III CAPABILITY TEST PER MM 22-97-00, OPS
- [SDR GN0A20120930001](https://openairdocs.org/sdr/GN0A20120930001.md): Control Panel · failed · Sep 30, 2012 · N652CT · Emb EMB120ER
  > AUO TO (UOX): AFTER TAKEOFF WHILE CLIMBING THROUGH 3500FT THE AUTO-PILOT WAS ENGAGED. WHEN PASSING 5000FT THE LEFT FLIGHT DIRECTOR BARS PITCHED DOWN 2.5° WHICH CAUSED THE AUTO-PILOT TO COMMAND THE AIRCRAFT FOLLOW. THE LEFT AUTO-PILOT WAS DISENGAGED AND AIRC
- [SDR USAA2012032600034](https://openairdocs.org/sdr/USAA2012032600034.md): Fcu · malfunctioned · Mar 24, 2012 · N722US · Airbus A319112
  > ELECTRICAL & CHEMICAL ODORS DETECTED ON FLIGHT DECK. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-400-001. OPS CHECKED GOOD.
- [SDR USAA2012010600001](https://openairdocs.org/sdr/USAA2012010600001.md): Fcu · defective · Jan 4, 2012 · N543UW · Airbus A321231
  > AT GATE IN CLT, SMOKE (PERCEIVED AS ELECTRICAL) WAS COMING FROM MODE CONTROL PANEL. HAD TO SHUT OFF ALL ELECTRICAL TO GET IT TO STOP. MAINTENANCE REMOVED AND REPLACED THE FLIGHT CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 22-81-12-0401.
- [SDR UALA2012010400085](https://openairdocs.org/sdr/UALA2012010400085.md): Servo Valve · no test · Jan 2, 2012 · N174UA · Boeing 747422
  > LEFT AILERON SERVO FAILED OPERATIONAL TEST AND FCC BITE TEST. REMOVED SERVO IAW AMM. INSTALLED LT LCCA SERVO VALVE PER AMM. LEAK CHECKED GOOD, FAILED OPERATIONAL TEST WITH CMCS MESSAGE "AILERON SERVO-L, FCC-L INTERFACE FAIL SERVO POSITION 22055." REPLACED
- [SDR E81R2011122232191](https://openairdocs.org/sdr/E81R2011122232191.md): Circuit Card · failed · Dec 22, 2011 · N493TM · Beech 400A
  > FLIGHT CREW REPORTED ACFT STARTED "PORPOISING" +/- 300 FT AT 800 FPM WHILE IN CRUISE FLIGHT AT FL400. COPILOT'S SIDE DISPLAY SIMULTANEOUSLY DISPLAYED "PITCH TRIM FAIL" INDICATION. ACFT DIVERTED. FOUND ELEVATOR CABLES AND ELEVATOR SERVO BRIDLE CABLE TENSIONS
- [SDR SIMA201135503](https://openairdocs.org/sdr/SIMA201135503.md): Controller · malfunctioned · Dec 19, 2011 · N728AE · Emb EMB135LR
  > ON FLIGHT 4554 THE CREW REPORTED THAT AT 30,000 FEET IN LIGHT CHOPPY WEATHER HAD AN UNCOMMANDED RIGHT TURN FOLLOWED BY RED "AP" ON PFD AT 2,500 FEET. THE AIRCRAFT YAWED NOSE RIGHT WITH ONLY YAW DAMP ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RE
- [SDR HALA2011101000447](https://openairdocs.org/sdr/HALA2011101000447.md): Computer · faulted · Oct 10, 2011 · N380HA · Airbus A330243
  > ETOPS SIGNIFICANT SYS - FLIGHT CONTROL COMPUTER FAULTED. R & R FLIGHT CONTRL COMPUTER IAW AMM 27-93-34. OPS CHECKED & TESTED GOOD IAW AMM 27-93-00.

Next page: https://openairdocs.org/jasc/2213/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 = '2213'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/2213/reports

---
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