JASC 2210
Service difficulty reports · 4,019
Reports filed under 2210 · Autopilot 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 = '2210' 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.
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 = '2210' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL2001707007Autopilot Sys · malfunctionedWHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEFFERED TO DMI 5936, PER MEL 22-1 CAT B, ITEM PLACARD. OPS CHECKED IAW MM 22-11-01, SYSTEM GROUND CHECKS GOOD. PER CREW COMMENT & B727 AUTO-SDR DHL2001805013Autopilot Sys · malfunctionedAUTOPILOT BANKS 40 DEGREES TO LEFT IN HDG MODE. OVERSHOOTS HEADING SELECTED BY 10 - 12 DEGREES. SWAPPED NR 1 & 2 FOGS. BOTH CK OK IAW LITTON EO 41007 DOC 464544. A/P CKS OK ON BOTH SIDES IAW 22-10-00. ROLL CHANNEL BITE CKS OK IAW 22-12-00.SDR DHL2001743008Control Panel · dirtyAUTOPILOT VERTICAL SPEED KNOB DOES NOT FOLLOW VERTICAL SPEED. UNABLE TO ENGAGE AUTOPILOT. CLEANED AND RESEATED MODE CONTROL PANEL OPS CHECK NORMAL IAW MM 22-11-101. TESTED SYSTEM IAW 22-11-01. SYS CKS NORMAL. NO DEFECTS NOTED.SDR GTIA010436Relay · failedEWR - AP AUTOPILOT WAS NOT TRIMMING NOSE UP. REMOVED AND REPLACED TRIM RELAY R20-12 PER WDM 27-43-02. PERFORMED OPS CHECK A/P SYSTEM PER MM 22-21-00 SOUND NORMAL. (M)SDR CA010629036Servo · failed(CAN) ELEVATOR HEAVY OPERATION AFTER TAKE OFF. FLIGHT WAS ABORTED. LANDING WAS UNEVENTFUL. MAINTENANCE TESTS REVEALED THAT THE AUTO PILOT ELEVATOR SERVO MOTOR'S CLUTCH WAS STILL ENGAGED. ELEVATOR ACTUATOR SERVO MOTOR IS BEING REPLACED.SDR DHL2001362016Autopilot Sys · malfunctionedAUTOPILOT HAS DIFFICULTY MAINTAINING ALTITUDE PLUS OR MINUS 200 FT WITH CONFIGURATION CHANGES IE, FLAPS 0 DEGREE TO FLAPS 8 DEGREE. RESEATED NR 1 AND 2 ADC ALTITUDE ACO AND HOLD OPS CHECKED GOOD AS PER MM 22-13-00.SDR 2001UALA00876Autopilot Sys · malfunctionedON DESCENT OUT OF 8,000 FEET AUTOPILOT SPD 210, FLAPS 5-WHEN SPEED BRAKE DEPLOYED PAST 1-2 TOWARDS FULL. AC REMAINED WINGS LEVEL, BUT YOKE SHOWED 2 1-2 TO 3 DEG ON STATUS PG RT INBOARD AILERON ALMOST FULLY DEFLECTED DOWN. OK WITH NO SPEED BRAKE. UNEVENTFUL SDR DHL2001742007Autopilot Sys · malfunctionedAUTOPILOT INTERMITTENTLY WOULD NOT ENGAGE IN A AND B MODE. RAN SYSTEM NUMEROUS TIMES. SYSTEM OPS CHECKED NORMAL.SDR DHL2001727019Autopilot Sys · malfunctionedAUTOPILOT OVERBANKS. COULD NOT DUPLICATE ON GROUND. AUTOPILOT OPS CKS GOOD IAW B727 MM 22-11-01.SDR DHL2001807022Autopilot Sys · malfunctioned1) STEADY WARNING HORN DURING CLIMBOUT WITH GEAR UP AND FLAPS RETRACTED. AIR TURNBACKED TO ORD. 2) TROUBLESHOOTING FOUND ITEM RELATED TO AUTOPILOT DMI 5739. SEE ITEM 2D FOR AUTOPILOT CORRECTIVE ACTION. AT THIS TIME AUTOPILOT WARNING HORN OPERATES NORMSDR R7MR33480Head · inoperativeDISPLAY INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR DHL2001365016Computer · malfunctionedA/P NR 1 WILL NOT STAY ENGAGED IN ARCH MODE. COULD NOT DUPLICATE ON GROUND. SWAPPED LOCK MONITOR COMPUTERS FOR TROUBLESHOOTING PURPOSES. OPS NORMAL AT THIS TIME.SDR DHL2001807019Computer · malfunctionedAUTOPILOT WILL NOT LEVEL OFF FROM CLIMB OR DESCENTS EVEN WITH MIN RATE ON INITIATION LEVEL OFF. CLEANED AND RE-SEATED A/P PITCH COMPUTER IN RACK. PERFORMED TEST OF A/P PITCH CHANNEL PER M/M 22-13-0. ALL TESTS GOOD.SDR GLBA2001107Relay · intermittentYAW DAMP ENGAGED ON T/O, REPLACE RELAY DMO8 PN LMD-7111-P AND MODULE K010 PN# LMD-5000-P OPS CHECK SYSTEM SATISFACTORYSDR DHL2001364019Computer · malfunctionedDURING TAXI THE PITCH FEEL NR 1 LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE AND SYS WAS RECOVERED. LIGHT EXTINGUISHED. RE-RACKED NR 1 ART FEEL COMPUTER AND CHECKED PER M/M 27-33-00. OK FOR CONTINUED SERVICE.SDR DHL2001745005Autopilot Sys · malfunctionedAUTOPILOT WILL NOT MAINTAIN LOCALIZER ON APPROACH BELOW 2000 FT ABOVE AIRPORT. PERFORMED OPS CHECK OF A/P NAV/LOC. CHECKS GOOD WITH COMPANY EQUIPMENT.SDR WVBA2001034Switch · failedPILOT REPORTED SWITCH WOULD NOT TEST IN EITHER POSITION. SWITCH WAS REMOVED FROM SERVICE. PARTS TAKE FROM 3 TO 12 WEEKS TO BE DELIVERED RENDERING THE AUTOPILOT INOPEATIVE FOR THAT TIME FRAME. WITH SWITCHES FAILING RIGHT OUT OF THE BOX OR VERY FEW HOURS IN SSDR DHL2001701010Head · malfunctionedAUTOPILOT MAKES GRADUAL UNCOMMAND RIGHT TURNS IN MANUAL MODE. DEFERRED IAW DHL MEL 22-1 CAT B MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED, DMI 5661. REMOVED AND REPLACED AUTOPILOT CONTROL HEAD CKS GOOD PER 22-00. THIS CLEARS DMI 5661. PLACARD SDR DHL2001804009Autopilot Sys · malfunctionedAUTOPILOT MADE AN UNCOMMANDED DESCENT FROM 4000 FT LEVEL FLIGHT. COULD NOT DUPLICATE ON GROUND. AUTOPILOT CHECKS GOOD IAW DC-8 MM 22-10-0. BITE CHECK ALSO GOOD.SDR DHL2001743006Autopilot Sys · malfunctionedFL 330 FT MACH .80, AUTOPILOT ENGAGED. AIRCRAFT STARTED TO DUTCH ROLL, DISENGAGED AUTOPILOT. DUTCH ROLL STOPPED. NOTED, NO RUDDER MOVEMENT. TRANSFERRED PER MEL 22-1. DMI 5665, PLACARD INSTALLED. TESTED AUTOPILOT. SYSTEM OPS CKS GOOD IAW B727 MM 22-11. SDR DHL2001743007Coupler · defectiveDURING DESCENT THRU 14000 FT AT 280KTS SPEEDBRAKE DEPLOYED AIRCRAFT BEGAN TO YAW AFTER TURNING LOWER YAW DAMPER OFF. DUTCH ROLL STOPPED. REPLACED LOWER RUDDER YAW DAMPNER COUPLER IAW B727 M/M 22-11-131. OPS CHECK GOOD.SDR DHL2001367005Computer · malfunctionedAUTOPILOT NR 2 WOULD NOT TRACK LOCALIZER IN APPR MODE. DEVIATED UP TO 10 DEG LEFT AND RIGHT OF LOC HDG WITH CALM WIND. DURING TROUBLESHOOTING, FOUND MA TRIPPED FOR NR 2 AP/FD LOGIC/MONITOR COMPUTER ON AFCS TEST PANEL. PERF COMP TEST WITH FAULT CODE OF 52. SDR DHL2001807018Autopilot Sys · malfunctionedAUTOPILOT WHILE ON FINAL APPROACH BELOW 1000 FT ALT CONTINUED TO DIVERGE BELOW GLIDESLOPE WITHOUT CORRECTION. REPOSITIONED LINKAGE ABOVE SERVO MICROSWITCH, OPS CKD OK IAW MM 22-20-0.SDR DHL2001807017Linkage · out of positionAUTOPILOT EXCEEDED 35 DEG BANK DURING TURNS. REPOSITIONED LINKAGE ABOVE SERVO MICROSWITCH. OPS CK''D OK IAW MM 22-20-0.SDR DHL2001807014Linkage · jammedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS JERKS CONTROL YOKE BACK AND FORTH. FOUND JAMMED LINKAGE ABOVE SERVO MICRO-SWITCH. REMOVED AND PROPERLY REPOSITIONED LINKAGE. CLEANED CONNECTOR TO MICROSWITCH AND SERVO. OPS CK''D OK IAW MM 22-20-0.SDR R7MR33351Bushing · wornBUSHINGS WORN BEYOND SERVICEABLE LIMITS AND ALSO LEAKS HYDRAULIC FLUID. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR DHL2001807012Control Panel · malfunctionedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS. R&R A/P CONTROL PANEL IAW 22-10-2. A/P CHECKS GOOD.SDR DHL2001365012Dampener · malfunctionedNR 1 YAW DAMPNER DIFFICULT TO ENGAGE. DROPS BACK OFF BEFORE CATCHING. COULD NOT DUPLICATE PROBLEM. SWAPPED NR 1 & NR 2 YAW COMPUTERS. OPS CKS GOOD ON GND IAW A300 MM 22-21-00.SDR DHL2001365011Warning System · malfunctionedWITH A/P ENGAGED DURING DESCENT ERROR MESSAGE SINGLE FMS OPERATION. DISENGAGED AUTOPILOT NR 2. TEMP RESTORED NAV MODE THEN A/P NR 1 DISENGAGED, SAME ERROR MSG. SET FMS MASTER SWITCH YP FMC1. THIS ENGAGED BOTH A/P. RE-ENGAGED A/P NR 2. OPERATED NORMAL. BOTHSDR DHL2001727017Autopilot Sys · out of adjAUTOPILOT TRACKS 1/2 TO 1 MILE LT OR RT OF COURSE IN NAV/LOC MODE AT CRUISE ON GPS INFO. GPS PARALLEL TRACK SET TO 1 MILE LEFT OF COURSE SELECTED TO STANDBY. OPS CHECK GOOD IAW DHL B727 S/M 34-59-0.SDR DHL2001717007Autopilot Sys · malfunctionedAUTOPILOT WILL NOT TRACK A VOR OR LOCALIZER. DEFERRED PER DHL MEL 22-1-7. PLACARD INSTALLED. REPLACED NR 1 NAV AND TESTED PER MM 2200 OP NORMAL TRACK AND CAPTURE.SDR DHL2001743005Damper · failedAIRCRAFT REQUIRED 4.0 UNITS OF LEFT RUDDER TRIM IN FLIGHT. LOWER RUDDER INDICATES SPLIT WITH UPPER. YAW DAMPER ON LOWER WOULD NOT CHECK ON TAXI IN. LOWER YAW DAMPER COMP. FAILED. R&R LWR YAW DAMP COMP IAW M/M 22-11-131 AND 22-11-01. OPS CK''D NORMAL. OK FOSDR DHL2001364017Autopilot Sys · malfunctionedNR 2 PITCH TRIM DISCONNECTED IN FLIGHT. WOULD NOT RESET. COULD NOT DUPLICATE DISCREPANCY. OPS CK NORMAL. SWAPPED NR 1 AND NR 2 PITCH TRIM COMPUTERS FOR TROUBLE SHOOTING. OPS CK IS GOOD IAW MM 22-23-34.SDR DHL2001743004Coupler · faultyON APPROACH WITH AUTOPILOT ENGAGED, FELT UNCOMMANDED RUDDER INPUTS. DISENGAGED AUTOPILOT AND 30 SECONDS LATER INPUTS STOPPED. CORRECTIVE ACTION - DEFERRED YAW DAMPERS PER DHL MEL 22-6. PLACARD INSTALLED. R&R LOWER YAW COUPLER. PERFORMED BITE TEST IAW MM 22-SDR DHL2001365009Autopilot Sys · malfunctionedAUTOPILOT NR 1 WILL NOT ENGAGE. MEL 22-11-01. REMOVED AND REPLACED A/P MODULE ENGAGE OPS CK AS PER MM 22-10 GOOD. AC OK FOR SERVICE.SDR ZYWA100164Actuator · inoperativeUNUSED FREQ ADAPTER, MATERIAL. RETURNED FOR RESTOCK AND CREDIT.SDR DHL2001727013Autopilot Sys · malfunctionedA/P WILL NOT TRACK GPS WHEN SWITCHING FROM NAV/LOC TO MANUAL. A/P TURNS A/C INTO 30 DEGREE LEFT BANK TURN. OPS CHECK A/P NO DEFECTS NOTED IAW B-M/M 22-11-11.SDR DHL2001364016Autopilot Sys · malfunctionedPITCH TRIM 2 FAILED. OPS CHECK PERFORMED COULD NOT DUPLICATE ON GROUND. SWAPPED PITCH TRIM COMPUTERS FOR TROUBLESHOOTING IAW M/M 22-23-00. NO DEFECTS NOTED.SDR 20010608CW005Housing · crackedCRACKS IN SERVO BODY.SDR 20010608CW004Housing · crackedCRACKS IN SERVO BODY.SDR GTIA010243Autopilot Sys · malfunctionedDTW - FLT 476 - DESCENDING INTO DTW, ALTITUDE ARMED, ALTITUDE DISARMED ITSELF WITHOUT PILOT INTO SHOWING TO 210 KTS AT 12,000 FT. AUTOPILOT WOULD NOT MAINTAIN ALTITUDE DFGC NR 1. CHECKED STP, NO FLIGHT FAULTS LOGGED, PERFORMED A RETURN TO SERVICE BIT CHECK OSDR UPS01435764Card · defectiveINSPECTION TYPE :W/E, ON DEPARTURE THE CREW BEGAN TO NOTICE A SLIGHT ELECTRICAL SMELL, NOTHING OUT OF ORDINARY WAS NOTICED, APPROACHING LEVEL OFF SMELL DISAPPEARED. SHORTLY AFTER ''B'' A/P DISENGAGED FOR NO APPARANT REASON. COULD NOT REENGAGE A/P B, NOTE: B SDR DHL2001365006Autopilot Sys · malfunctionedNR 2 AUTOPILOT WOULD NOT STAY ENGAGED DURING APPROACH. RESEATED NR 2 LOGIC COMPUTER AND PERFORMED OPS TEST PER 22-13-00. CHECKED GOOD ON GROUND.SDR DHL2001365004Autopilot Sys · malfunctionedNR 1 AUTOPILOT WOULD NOT STAY ENGAGED DURING APPROACH. RESEATED NR 1 LOGIC COMPUTER AND PERFORMED OPS TEST PER MM 22-13-00. CHECKED GOOD ON GROUND.SDR DHL2001701007Sensor · looseAT FL330 AT M.78 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECTED ON SERVO-A. TIGHTENED CRANK ON A-SYS ELEVATOR POSITION SENSOR IAW B727 22-11-77 OP CK GOOD. NORMAL ON GROUND IAW B727 M/M 22-11-71.SDR DHL2001807009Autopilot Sys · defectiveAUTOPILOT WILL NOT ENGAGE. DMI 5372 - ASSIGNED CVG MX CTRL, MEL 22-1. PLACARD INSTALLED.SDR GTIA010242Autopilot Sys · malfunctionedEWR - FLT 294 - GOING THROUGH 15,000 FT LOST AUTO PILOT, AUTO THROTTLE, YAW DAMPNER AND MACH TRIM. ALSO, ABILITY TO ADJUST SPD/MACH AND LIGHTING ON FMA FOR ALTITUDE. TESTED DIGITAL FLIGHT GUIDANCE SYSTEM. RTS CHECK. ALL CHECK NORMAL PER MM 22-01-05. (M)SDR DHL2001804006Computer · malfunctionedAUTOPILOT ELEVATOR SERVO TRIM METER OSCILLATES FULL DEFLECTION UP AND DOWN WHILE AIRCRAFT IS LEVEL FLIGHT. RERACKED PITCH CHANNEL COMPUTER. SYSTEM OP CHECKS NORMAL PER MM 22-13-1.SDR DHL2001804005Computer · defectiveIN LEVEL FLIGHT AT CRUISE ALTITUDE THE AUTOPILOT ROWS THE AIRCRAFT 2 DEG LEFT AND RIGHT CONTINUOUSLY. REMOVED AND REPLACED ROLL CHANNEL COMPUTER PER MM 22-12-1. OPS NORMAL.SDR 20010608CW006Housing · crackedCRACK IN SERVO BODY.
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