JASC 2211

Service difficulty reports · 588

Reports filed under 2211 · Autopilot Computer, 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 = '2211'
  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 U30A200200025Computer · malfunctionedDURING CRUISE OF FLT 135 MYNN (NASSAU) TO KBWI (BALTIMORE) NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAULTED ON ECAM. PERFORMED RESET OF SYSTEM AT BWI IN ACCORDANCE WITH TSM TASK 24-00-00-810-818. NO DEFECTS NOTED, MESSAGE CLEARED AND AIRCRAFT WAS RETURNOct 28, 2002 · N260AV · Airbus A320214SDR AUS20021250Controller · faulty(AUS) AUTOPILOT COMPUTER CONTROLLER FAULTY.Oct 21, 2002 · Cessna 208BSDR SWIA200211325Computer · malfunctionedDURING LEVEL FLIGHT AT FL230 AND -12 DEGREES CELSIUS WITH THE A/P SELECTED ON, THE CAPTAIN'S FLIGHT DIRECTOR COMMANDED AN ABRUPT ROLL TO THE LEFT, FOLLOWED BY A PITCH DOWN TO 5 DEGREES. PREVIOUS CREW REPORTED SIMILAR OCCURRENCE AT FL240. REPLACED CAPTAIN'S AOct 12, 2002 · N221SW · Emb EMB120ERSDR SWIA200211261Computer · malfunctionedAUTOPILOT AND TRIM FAILURE MAP LIGHTS ILLUMINATED ON TAKE OFF ROLL. ABORTED TAKE OFF. INSTALLED SERVICEABLE FO'S A/P COMPUTER. AUTO PILOT SELF DIAGNOSTIC AND OPS CHECKS GOOD.Sep 20, 2002 · N223SW · Emb EMB120ERSDR SWIA200211197Pin · backed outCAPTAINS AUTOPILOT DOES NOT CAPTURE GS WITH APPR MODE. CAPTAIN'S AUTOPILOT FAILED WITH AILERON SERVO FAILURE. REPLACED PUSHED OUT PIN 44 ON J3 OF PILOT'S AUTOPILOT COMPUTER RACK. CAPTAIN`S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. TESTED AILERON SERVO WITHAug 30, 2002 · N288SW · Emb EMB120ERSDR U30A200200021Computer · faultyDURING PREFLIGHT FOR FLT 1371 AT ORD, ECAM MESSAGE INDICATED AP2, CAT 3 DUAL. AFS BITE CALLS FOR FMGC NR 2 REPLACEMENT. DEFERRED NR 2 FMGC PER MEL 22-83-01-2. AIRCRAFT OPERATED ORD-CUN-PHL. UPON ARRIVAL AT PHL THE NR 2 FMGC (FLIGHT MANAGEMENT GUIDANCE COMPAug 17, 2002 · N262AV · Airbus A320214SDR HEEA080564Computer · malfunctionedAFCS COMPUTER MALFUNCTIONED, FLIGHT DIRECTOR WON'T HOLD HEADING. REPAIRED.Jul 29, 2002 · N1202T · Bell 412SDR HEEA080563Computer · malfunctionedAFCS COMPUTER CAUSES AIRCRAFT TO CLIMB INSTEAD OF DESCENDING WHEN CAPTURING GLIDE SLOPE ON ILS.Jul 29, 2002 · N142PH · Bell 412SDR HEEA080561Computer · malfunctionedNR 1 AFCS KICKING IN PITCH, ROLL AND YAW.Jul 29, 2002 · N2148K · Bell 412SDR R7MR35530Computer · inoperativeCSAS COMPUTER INOPERATIVE. ROLL CHANNEL OPERATIVES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Jul 8, 2002 · N586BH · Bolkms BK117A4SDR SWIA200210997Computer · failedTRIM FAIL AND AUTOPILOT FAIL MAP LIGHTS ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED FIRST OFFICER'S AUTOPILOT COMPUTER. FLIGHT DIRECTOR SYSTEM TESTS NORMAL PER MM 22-11-00.Jun 29, 2002 · N289YV · Emb EMB120ERSDR 250TR0004Potentiometer"A" Auto-pilot jerky in all modes. R&R stab trim potentiometer.May 31, 2002 · N250TR · Boeing 7372K5SDR RAIA00204127Computer5616-STL - SPARKS AND SMOKE IN COCKPIT COMING FROM AREA OF FLIGHT DIRECTOR. MAINTENANCE REMOVED AND REPLACED DEFECTIVE AUTOPILOT COMPUTER.Apr 17, 2002 · N565HK · Jetair JETSTM4101SDR R7M2002F00021Computer · inoperativeCSAS-COMPUTER INOPERATIVE. CAUSES 1 TO 2 HRTZ PER SECOND ROLL WHILE ROLL MODE ENGAGED. REPLACED WITH NEW UNIT CORRECTED PROBLEM.Apr 2, 2002 · N586BH · Bolkms BK117A4SDR R7M2002F00022Computer · malfunctionedYAW/CSAS COMPUTER INOPERATIVE. ONLY OPERATES IN STANDBY MODE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Mar 28, 2002 · N586BH · Bolkms BK117A4SDR GTIA020254Controller · malfunctionedFLL - FLT 1083 - NR 2 AUTOPILOT VERY JERKY IN LEVEL FLIGHT, YOKE MOVES BACK AND FORTH IN SHORT CHOPPY MOVEMENTS. STP RTS CHECK SHOWED 4 FAULTS A/P, F/D, A/T, S/V, Y/D. REMOVED AND REPLACED NR 2 DFGC. OPS CHECK NORMAL IAW MM 22-01-05. RTS CHECK INDICATES 'GMar 28, 2002 · N602CA · Doug DC983SDR SDRO2002003Control Head · failedPILOT REPORTED THAT 10 MINUTES INTO CRUISE FLIGHT DURING NORMAL CROSS CHECK HE NOTICED HEADING WAS STARTING TO DRIFT. PILOT WAS UNABLE TO RESELECT AUTO PILOT HEADING. AUTO PILOT HAD FAILED. CONTROL HEAD STILL INDICATED THE AUTO PILOT WAS ENGAGED. DID NOT RMar 15, 2002 · N135N · Urocop EC135P1SDR 2002FA0000621Computer · failedTHE AC WAS IN LEVEL FLIGHT WITH AUTOPILOT TURNED OFF. WHEN THE AUTOPILOT COMPUTER, WITHOUT INPUT FROM THE PILOT GAVE AN INDICATION THAT (PITCH WARNING) LIGHT CAME ON WITH A (UP) ARROW. THE PILOT PULLED THE AUTOPILOT CIRCUIT BREAKER TO TURN OFF SYSTEM. ANOTHFeb 22, 2002 · N97TD · Cessna 182SSDR DHL2001715011Computer · faultyWITH AUTO PILOT ENGAGED RAPID DEFLECTION OF CONTROL WHEEL OCCURS BOTH LEFT AND RIGHT OF ABOUT 10 DEGREES. DEFERRED AUTO PILOT SYSTEM AND MX CONTROL WAS NOTIFIED. REMOVED AND REPLACED ROLL CHANNEL COMPUTER, OPS CHECKS GOOD IAW B727 MM 22-11-111.Dec 1, 2001 · N715DH · Boeing 727155CSDR 0104239603Computer · faultyTHE AIRCRAFT WOULD PORPOISE +-100 FEET DURING CLIMBOUT WITH THE AUTOPILOT ON USING THE THUMB WHEEL. THE AIRCRAFT WOULD NOT HOLD ALTITUDE IN LEVEL FLIGHT WITH PITCH HOLD SELECTED. CREW REFUSED TO HAND FLY THE AIRCRAFT AND THE FLIGHT RETURNED TO AN UNEVENTFUL Nov 15, 2001 · N603NW · Doug DC932SDR AUS20011217Computer · failed(AUS) UPPER YAW DAMPER COMPUTER FAULTY.Nov 13, 2001 · Boeing 747SP38SDR DHL2001749001Computer · malfunctionedDESCENDING THRU 12,000 FEET WITH AUTO PILOT ENGAGED, AIRCRAFT WENT INTO UNCOMMANDED ROLL TO THE RIGHT. REMOVED AND REPLACED ROLL CHANNEL, IAW B727 MM 22-11-111, OPS CHECKED GOOD IAW B727 MM 22-10-0. OPS CHECKED GOOD.Oct 23, 2001 · N749DH · Boeing 727200SDR S01422029Computer · malfunctionedB-18273 1.A/P AUTO ENGAGED WITH OUT COMMAND DURING A/C T/O. 2.OCT 02, CAPT REPORT 20011002 IS RECEIVED,IAW CAPT DESCRIPTION,SUSPECT MCP FUNCTION UNSTABLE. 3.MCP WAS REPLACED ON OCT 02. C/A: 1. MCP WAS REPLACED WHEN A/C BACK TO CHECKS AT THE SAME DAY AND PERFSep 27, 2001 · Boeing 747400SDR P2EA01193Computer · faultyFLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHECSep 16, 2001 · N120NJ · Boeing 737297SDR GTIA010875Computer · faultyFLT 273 - TPA - A/P PITCH SERVO IS ERRATIC, HUNTS UP AND DOWN FLT 273. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 22-13-0. OPS CHECK NORMAL. (M)Sep 10, 2001 · N969ML · Doug DC931SDR ABXA010462Computer · defectiveAUTOPILOT EVALUATION REQUESTED PER M1A 028521-64/2. AUTOPILOT EVALUATION WAS UNSATISFACTORY. HEADING BUG DID NOT OVERSHOOT AND THERE WASN'T EXCESSIVE BANK BUT THERE WAS RESISTANT VIBRATION IN THE ELEVATOR WITH AUTOPILOT ENGAGED. REPLACED THE AUTOPILOT PITCHAug 28, 2001 · N966AX · Doug DC941SDR SWIA200110108Computer · malfunctionedUNCOMMANDED PITCH UP WITH AP ENGAGED, AP DISCONNECTED. PERFORMED QRH, RE-ENGAGED AP, AND EXPERIENCED UNCOMMANDED PTICH ROLL. AP DEFERRED ON FO SIDE. MEL 22-11-1 REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-00. OPS CHECK GOOD.Aug 17, 2001 · N1117H · Emb EMB120RTSDR DHL2001805015Computer · faultyIN CRUISE WITH AUTOPILOT IN AUX NAV INS NR 1, AIRCRAFT WOULD SUDDENLY ROLL RIGHT AND DIVERT FROM COURSE. OPS OK ON SYSTEM NR 2. PERFORMED SYSTEM TEST. NR 1 INS SHOWED CODE 4 DURING ALIGNMENT. REMOVED AND REPLACED NR 1 INU. PERFORMED ROLL CHANNEL CHECK; FAJul 6, 2001 · N805DH · Doug DC873FSDR DHL2001715007Computer · faultyWITH AUTOPILOT A SERVO SELECTED, A/C PITCHES UP AND DOWN. OK WITH SERVO B SELECTED. DEFFERED AUTO PILOT A-MODE PER MEL 22-1-11A, CAT C, DMI 6211. PLACARDS INSTALLED. T/S SYS ORDERED PITCH COMPUTER. PARTS IN CVG AS PER MXC DMI 6211 CONTINUES. REMOVED ANDJun 29, 2001 · N715DH · Boeing 727155CSDR DHL2001727021Computer · malfunctionedWHEN IN NAV/LOC MODE A/P CARRIES RIGHT WING 7 DEGREES LOW. WHEN DISENGAGING FROM NAV/LOC MODE TO MANUAL MODE, WINGS RAPIDLY RETURN TO LEVEL. RESEATED AUTOPILOT ROLL COMPUTER PER B-727 MM 22-11-111 AND RESEATED AUTOPILOT MODE CONTROL PANEL PER B-727 MM 22-11-Jun 26, 2001 · N727DH · Boeing 727228SDR DHL2001741011Computer · defectiveWHILE THE AUTO PILOT WAS TURNING AIRCRAFT TOWARD HEADING BUG (APPROX 60 DEG TURN) THE AUTO PILOT PUT THE AIRCRAFT IN A 35 DEG TO 40 DEG BANKING TURN. REMOVED AND REPLACED ROLL CONTROL CHANNEL WITH SERVICEABLE PART IAW MM 22-11-101. OPS CHECK GOOD ON GROUND.Jun 22, 2001 · N741DH · Boeing 7272Q9SDR DHL2001727020Computer · defectiveAUTO PILOT BANKS 10 DEG LEFT IN MANUAL MODE WITH TURN KNOB IN LEVEL DETENT AND OCCASIONALLY BANKS HARD RIGHT IN SAME CONFIGURATION. NAV MODE WORKS NORMALLY. REMOVED AND REPLACED ROLL CHANNEL IAW BMM REF 22-11-1. OPS CHECK GOOD.Jun 22, 2001 · N727DH · Boeing 727228SDR DHL2001362019Computer · malfunctionedNR 1 AUTOPILOT WOULD NOT ENGAGE. RESET NR 1 LOGIC MONITOR COMPUTER GROUND CHECKS GOOD PER M/M 22-10-00.Jun 8, 2001 · N362DH · Airbus A300B4103SDR DHL2001363006Computer · malfunctionedAUTOPILOT NR 1 WILL NOT ENGAGE. RESEATED ALL THREE A/P, F/O COMPUTERS. NR 1 A/P OP CHECKS GOOD PER M/M 22-10-00. NO FAULTS IN SELF TEST.Jun 8, 2001 · N363DH · Airbus A300B4103SDR DHL2001715006Computer · malfunctionedON CLIMBOUT IN A-MODE AUTOPILOT PORPOISED. REPLACED PITCH CHANNEL PER MM 22-11-101. OPS CKS GOOD. THIS CLEARS DMI 5771.May 26, 2001 · N715DH · Boeing 727155CSDR DHL2001727018Computer · malfunctionedAUTOPILOT IN A-MODE HAD UNCONTROLLED ROLLS IN BOTH DIRECTION, B-MODE NORMAL. DEFERRED IAW MEL REF 22-1 CAT B CTL 5716 ASSIGNED. PLACARD INSTALLED. REMOVED AND REPLACED ROLL CHANNEL, OPS CK NORMAL IAW M/M 22-11-0, CLEARS DMI 5716. PLACARD REMOVED.May 23, 2001 · N727DH · Boeing 727228SDR DHL2001707006Computer · malfunctionedWITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER TO GLIDE PATH. REPLACED PITCH CHANNEL COMPUTER WITH A SERVICABLE UNIT IAW B727 M/M 22-11-121. CHECKS GOOD AT THIS TIME IAW B727 M/M 22-11-0May 19, 2001 · N707DH · Boeing 72722SDR DHL2001701011Computer · faultyHDG MODE AIRCRAFT BANKS GREATER THAN 30 DEG ANGLE OF BANK, TRACKS 5 DEG LEFT OF SELECTED HDG, AND OVERSHOOTS IN TURNS TO THE SELECTED HDG BY 25 DEG. REPLACED ROLL CHANNEL (REF ITEM 1P) AND OPS CK PER B-727 MM 72-11-01. OPS CK GOOD.May 18, 2001 · N701DH · Boeing 72730CSDR GTIA010360Connector · dirtyFLL - FLT 1457 - AUTO THROTTLE DISENGAGES IN FLIGHT. CLEANED 'RACK' CONNECTORS OF BOTH NR 1 AND NR 2 DFGC'S. PERFORMED OPERATIONAL TEST OF AT/SC AS PE PARA Z M/M 22-31-00, OPS CHECKED NORMAL. (M)May 15, 2001 · N602CA · Doug DC982SDR DHL2001807013Computer · malfunctionedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS (JERKS CENTER YOKE BACK & FORTH). REMOVED AND REPLACED PITCH CHANNEL 2 COMPUTER IAW DC-8 MM CH 22-13-1. AUTOPILOT PITCH CONTROL OPS CK NORMAL.May 15, 2001 · N807DH · Doug DC873SDR DHL2001364018Computer · malfunctionedNR 2 PITCH TRIM DISCONNECTED TWICE IN FLIGHT. RESET OPS NORMAL. DEFERRED NR 2 PITCH TRIM IAW MEL 22-11-03. C/W S.P. 22-11-03-A.2. REMOVED AND REPLACED NR 2 PITCH COMPENSATION COMPUTER AND OPS CHECK OK PER 22-23-00.May 12, 2001 · N364DH · Airbus A300B4203SDR DHL2001365013Computer · malfunctionedAUTO THROTTLE SYSTEM TRIPPED OFF WHEN ENTERING CLOUDS. RESET AND TRIPPED OFF 2 MORE TIMES WHILE IN CLOUDS. OPERATES NORMALLY IN THE CLEAR. REPLACED SRS COMP. OPS CKS GOOD IAW MM 34-24-11. (WHEN CREW WAS DEBRIEFED THEY INDICATED THAT THE SPD MODE WAS FAULTY May 12, 2001 · N365DH · Airbus A300B4203SDR DHL2001807010Computer · malfunctionedAT 12 DEGREE FLAPS AUTOPILOT CLICKED OFF ON APPROACH. RESET CLICKED OFF AT FLAPS 22. R&R PITCH COMPUTER PER M/M 22-13-01. PERFORMED TEST OF PITCH TRIM PORTION OF A/P IAW 22-13-01. TEST OK USING TIC 30 BOX.May 8, 2001 · N807DH · Doug DC873SDR SWIA972548Computer · malfunctionedWHEN DISCONNECTING AUTOPILOT, AIRCRAFT INSTANTLY ROLLED HARD RIGHT. REQUIRED AN UNUSUAL AMOUNT OF OPPOSING LEFT AILERON TRIM AND AIRCRAFT WAS SLOW TO RECOVER. INSPECTED AUTO PILOT COMPUTER NR 2 RACK CONNECTOR AND WIRING. NO DEFECTS NOTED. REPLACED NR 2 APCMay 4, 2001 · N290SW · Emb EMB120ERSDR DHL2001365010Computer · malfunctionedDURING ALTITUDE CAPTION WITH ALT ACQ GREEN ON THE FPI, A SUBSQUENT CHANGE TO THE ALTITUDE ALERT WINDOW DOES NOT RESULT IN REVERSION TO ALT ACQ AMBER AND PITCH MODE. BUT REMAINS ALT ACQ GREEN WITH LARGE PITCH CHANGES. RERACKED PITCH COMPUTERS AND AP/FD LONG CMay 4, 2001 · N365DH · Airbus A300B4203SDR DHL2001802006Computer · malfunctionedAUTOPILOT SLOW TO LEVEL OFF FROM CLIMB AND DESCENTS. WHEN SELECTED DESCENT ON AUTOPILOT, AUTOPILOT INITIAL CLIMBS IN LEVEL FLIGHT AUTOPILOT SLOWLY CLIMBS AND THEN IS SLOW TO LEVEL OFF. REPLACED PITCH CHANNEL COMPUTER. OPS CHECK GOOD IAW DC-8 MM 22-13-1.May 3, 2001 · N802DH · Doug DC873FSDR DHL2001727015Computer · failedWHEN AUTOPILOT IS SWITCHED FROM NAV/LOC TO HDG SELECT, THE A/C BANKS 20 DEGREES HARD IN THE OPPOSITE DIRECTION. FOUND ROLL CHANNEL FAILED. R&R ROLL CHANNEL. PERFORMED A/P ADJ TEST IAW MM 22-11-01. TESTED NORMAL IN A&B MODES VOR, NAV LOC & HDG SELECT MODES.May 1, 2001 · N727DH · Boeing 727228SDR DHL2001727014Computer · failedAUTOPILOT WILL NOT TRACK VOR AND GPS IN BOTH A AND B MODES. T/S AUTOPILOT SYST. FOUND ROLL CHANNEL FAILED. R&R ROLL CHANNEL. PERFORMED A/P SYSTEM ADJ TEST IAW MM 22-11-01. TESTED NORMAL IN A&B MODES VOR, NAV, LOC, AND HDG SELECT MODES.May 1, 2001 · N727DH · Boeing 727228SDR DHL2001806001Computer · malfunctionedAUTOPILOT WILL NOT BANK GREATER THAN 10 DEGREE WITH GPS 1 OR 2 IN AUX NAV. ALL LATERAL MODES FUNCTION NORMALLY. R&R ROLL CHANNEL COMPUTER PER DC8 M/M REF 22-12-1. OPS CKS SERVICABLE. P/N OFF 2588788-905, S/N OFF 1180385. P/N ON 2588788-905, S/N ON 1070200.Apr 28, 2001 · N806DH · Doug DC873FSDR DHL2001701006Computer · defectiveAT FL330 AT M-805 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECT ON SERVO A. DEFERRED A MODE ON A/P PER DHL MEL 22-1-11A. PLACARD INSTALLED. REPLACED ROLL CHANNEL COMPUTER PER MM 22-11-111. OPS CHECKED GOOD.Apr 28, 2001 · N701DH · Boeing 72730C
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