JASC 2210
Service difficulty reports · 4,016
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 ASAA2019050729261Unknown · malfunctionedMODE CONTROL PANEL AIRSPEED CONTROL KNOB INTERMITTENT. GROUNDED - YES. CYCLED POWER TO MCP. PERFORMED FIM 22-11 TASK 803 & MCP TESTS PASSED. A/C KNOB & DISPLAY WINDOW ON MCP OPS NORMAL.SDR ASAA2019050529251Computer · failedENGAGED AUTOPILOT A AT FL340 TWO SECONDS LATER DISENGAGED. MADE TWO ATTEMPTS, BOTH TIMES DISENGAGED AFTER TWO SECONDS. RESUMED AUTOPILOT B OPERATIONS. GROUNDED - YES. REMOVED FLIGHT CONTROL COMPUTER CH A IAW AMM 22-11-33. REPLACED FCC A IAW AMM 22-11-33-400-80SDR ASAA2019050429234Unknown · malfunctionedMCP ALTITUDE DISPLAY SHOWS AN APPARENT MINUS (-) SIGN. PFD DISPLAYS NORMAL. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019050329247Fcu · malfunctionedFCU 1 INOP GROUNDED - YES. PERFORMED FCU 1 RESET, FAULT COULD NOT DUPLICATED. AFS TEST ACCOMPLISHED PER AMM 22-96-00-710-001-A, TEST OK.SDR ASAA2019050329233Unknown · malfunctionedLNAV AND VNAV WILL NOT ENGAGE WITH EITHER FLIGHT DIRECTORS. GROUNDED - YES. CYCLED POWER ON AIRCRAFT PER AMM 20-60-99. LNAV AND VNAV NOW OPERATE NORMALLY PER PILOT PREFLIGHT CHECK.SDR HALA2019050300215Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - IN DESCENT COPILOTS MCDU PAGE SHOWED 2000' LOW ON VDEV READOUT CAPTS SIDE WAS ON VDEV + - 10'. DID AUTOLAND TEST IAW AMM 22-96 AND 22-97 UNABLE TO DUPLICATE ON GROUND NO RELATED MSG OK TO CONTINUE SVC.SDR ASAA2019050129232Unknown · malfunctionedF.O. CRS SELECT WINDOW IS BLANK, YET ILLUMINATES DURING LIGHT TEST. GROUNDED - YES. ACCOMPLISHED DFCS BITE GROUP #60, DFCS LRU REPLACEMENT TEST BITE GROUP # 35 FOR FCC/AT ALL TEST PER AMM 22-00-01-730-803. ALSO ACCOMPLISHED HGS SYSTEM AND OPS TESTS PER SMM 34-SDR ASAA2019050129217Unknown · malfunctionedCA FLIGHT DIRECTOR BARS INOP. GROUNDED - YES. ACCOMPLISHED AMM 22-00-01-730-807. ALL TEST PASS NO OTHER RELATED FAULTS.SDR HALA2019050400213Cdu · malfunctionedETOPS SIGNIFICANT SYSTEM - NR 3 MCDU SCREEN WENT BLANK INTERMITTENTLY. REMOVED & REPLACED NR 3 MCDU PER AMM 22-82-12. OPS CHECK GOOD.SDR HALA2019050400212Cdu · malfunctionedETOPS SIGNIFICANT SYSTEM - CAPT MCDU WHEN ATC COMM BUTTON PUSHED, SUBSYSTEM NOT AVAILABLE MSG POPS UP. RESET MCDU AND OPS CK GOOD. AFS TEST PASSED, NO FAULT NOTED PER AMM 22-96-00-740-801-A. OK FOR SVC.SDR AALA201905019001Unknown · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS TWICE DURING FLIGHT AT CRUZE, BOTH MCDU'S WENT INTO MENU SCREEN, ALL FMC RIGHT DATA WAS LOST AND THE AIRCRAFT WENT INTO CONTROL WHEEL STEERING. VTK MESSAGE APPEARED ON CA.S ND. ALL RETURNED TO NORMAL IN 30 SEC. PERFORMED DSDR ASAA201904292156Autoland Sys · malfunctionedHGS/AUTOLAND FAIL-APPROACH WARN RECEIVED AT CAT2 MINIMUMS AND AUTPILOT KICKED OFF. GROUNDED - YES. DFCS LOGGED 22-11479 , 22-11414 NO HISTORY. PERFORMED DFCS BITE, LRU TESTS AND LAND VERIFY REF B737-800 FIM 22-11 TASK 801 AND GROUP #49 ALL TESTS NORMAL, NO FAUSDR AALA201904229003Computer · faultyAIRCRAFT WAS GROUNDED: DURING DECENT IN VNAV MODE AIRCRAFT SUFFERED UNCOMMANDED ELEVATOR INPUTS FROM THE AUTO PILOT. THESE UNCOMMANDED INPUTS WERE MODERATE, AUTO PILOT CMD - A THE FIRST ONE WAS PASSING 25,000 FEET THE SECOND ONE WAS PASSING 18,000 FEET. ACCSDR ASAA2019042272946Autopilot Sys · disconnectedENROUTE CRUISE FLIGHT FL360 AUTOPILOT A DISCONNECTED & RE-ENGAGED AUTOPILOT A AND REMAINED ENGAGED FOR THE REST OF THE FLIGHT. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019041629026Autopilot Sys · malfunctionedON THREE SEPARATE OCCASIONS, THE MCP ALTITUDE SELECTOR WAS SET TO A NEW ALTITUDE AND THE ALT INTV BUTTON WAS PRESSED. ON ALL THREE OCCASIONS, THE CRZ ALT THAT APPEARED ON THE CRUISE PAGE IN THE FMC DID NOT MATCH THE MCP SELECTED ALTITUDE, IT WAS DIFFERENT BY 1SDR CA190416017Cable · slipped(CAN) WHEN PERFORMING SERVO MOUNT CLUTCH SLIP TEST ON APS-65 AUTOPILOT SYSTEM INSTALLED ON DHC6-300 AIRCRAFT IN ACCORDANCE WITH APS-65 MAINTENANCE MANUAL COLLINS PUBLICATION 523-0771867 PARA 5.4.2 THE BRIDAL CABLE CLAMPS ON THE MAIN CONTROL CABLES SLIPPED ALONSDR AALA20190416002Computer · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS FLIGHT DIVERSION ON ACCOUNT OF MANY CAUTION LIGHTS; DFCG WAS BLANK, NAV BLANK, WINDSHEAR, YAW DAMPENER OFF, AUTO THROTTLE OFF, A/P OFF MACH TRIM LIGHT, AT 18,000-20,000 LOW FUEL LEVEL LIGHT ON SHOWING (11.1) POUNDS OF FUEL.SDR ASAA2019041658996Control Panel · degradedDFCS MODE CONTROL PANEL VERTICAL SPEED WINDOW LCD DEGRADED AND LAST TWO DIGITS HARD TO READ. GROUNDED - YES. REMOVED AND REPLACED DFCS MCP PER B737-800 AMM 22-11-34-000-801/AMM 22-11-34-400-801. PERFORMED DFCS GROUP #32 (MCP LRU REPLACEMENT) TEST PER AMM 22-11SDR CA190410021Autopilot Sys · malfunctioned(CAN) APS-65 AUTOPILOT INSTALLED IN DHC6-300 BY MANUFACTURERS SERVICE BULLETIN SB 6-505 IS NOT MENTIONED IN THE AIRCRAFT MAINTENANCE MANUAL, HAS NO INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OR INSPECTION REQUIREMENTS. THERE IS NO PROCEDURE FOR TESTING SYSTEM POSDR ASAA2019040848905Control Panel · malfunctionedVERTICAL SPEED WINDOW ON MCP HAS MARKS ON IT WHEN IT SHOULD BE BLANKED. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL PER B737-900 AMM 22-11-34, PERFORMED INSTALLATION TEST, NO FAULTS NOTED. PERFORMED LAND VERIFY PER AMM 22-11-00 TEST GROUP 49 NSDR AALA201904039013Control Unit · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS REJECTED TAKEOFF ON ACCOUNT OF NO TAKEOFF MODE ON FLIGHT MODE ANNUNCIATORS. MAINTENANCE REPLACED THE FLIGHT CONTROL UNIT IAW AMM 22-81-12. OPS TEST GOOD.SDR ASAA201904028849Control Panel · inoperativeCAPTAINS COURSE SELECTOR IS INOP ALL MODES. GROUNDED - YES. REMOVED & REPLACED MCP. OP CK NORMAL. REF B737-800 AMM 22-11-34-000-801 & 22-11-34-400-801. BITE GROUPS 32, 49 & 70.SDR ASAA201904028848Autopilot Sys · malfunctionedAP #1 (AUTOPILOT A) DISENGAGED TWICE WHILE AT CRUISE (FL350) WITHOUT ANY PILOT INPUT OF ANY KIND. THERE WAS NO TURBULENCE WHEN THE DISCONNECT OCCURRED. GROUNDED - YES. PERFORMED DFCS BITE AND FOUND NO CURRENT FAULTS PER B737-900 FIM 22-11 TASK 801. FOUND DIFFESDR ASAA2019040188820Warning Light · false activationON AFTER START RECALL "MACH TRIM FAIL" LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET. GROUNDED - YES. T/S PER B737-900 FIM 22-13 TASK 817 AND 22-16 TASK 835. REVERSED CONFIGURATION CHANGES, REMOVED COLLARS AND RESET MACH TRIM AC+ DC C/B'S. "MSDR ASAA2019040188806Light · inoperativeA/P ENGAGE CMD B LIGHT DOES NOT ILLUMINATE WHEN A/P IS SELECTED ON. GROUNDED - YES. ACCOMPLISHED DFCS FLIGHT FAULT REVIEW BITE GROUP #20, NO FAULTS LOGGED. ACCOMPLISHED B737-900 FIM 22-11 TASK 803 MCP, ALL OPS NORMAL.SDR ASAA2019032828807Unknown · malfunctionedAUTOLAND TOUCHDOWN ABOUT 40' LEFT OF CENTERLINE. STARTED DEVIATION FROM CENTERLINE AT ABOUT 50' AGL. GROUNDED - YES. ACCOMPLISHED LLM MX PRACTICES FOR INBOUND CONDITION RELATED TO AUTOLAND AMM 22-00-01-730-807 NO CURRENT FAULTS AND ALL TESTS PASS. ACCOMPLISHEDSDR Q2SA20190325415Control Panel · failedAIRCRAFT GROUNDED. MCP, AUTOPILOT AND FLIGHT DIRECTOR FAILED IN FLIGHT ON CLIMB OUT. REPLACED MCP IAW AMM 22-11-34. OPS CK NORMAL. (LP 71462 ITEM 2) REF LP 71462 ITEM #1 - AUTOPILOT FAIL INFLIGH . CHANGE FCC B PRECAUTIONARY PER MX CTL. R & R FCC B REF AMM 22-1SDR AALA201903259005Actuator · inaccurateUNCOMMANDED RIGHT AUTOPILOT DISCONNECT. CONNECTED, AND DISCONNECTED AGAIN. REMOVED AND REPLACED THE LOWER LCCA IN THE LT WHEEL WELL IAW MM 27-11-14. OPS & LEAKED CHECKED IAW MM 27-11-14, AND MM 22-00-02.SDR ASAA2019032428772Control Panel · malfunctionedMCP HEADING DISPLAY WINDOW IS CORRUPTED. GROUNDED - YES. REMOVED AND REPLACED MCP REF AMM 22-11-34. MODE CONTROL PANEL INSTALLATION TEST PASSED REF AMM 22-11-34-740-801.SDR ASAA2019032328737Warning System · false activationDURING AFTER START CHECKLIST FLOW, THE "MACH TRIM FAIL" LIGHT ILLUMINATING DURING MASTER CAUTION RECALL. GROUNDED - YES. CYCLED POWER PER AMM 20-60-99 ALL OPS RESTORED. ACCOMPLISHED DFCS BITE SHOWS NO FAULTS MACH TRIM SYS TEST PASSES, BOTH CHANNELS PER FIM 22-SDR CA190325004Autopilot Sys · malfunctioned(CAN) BA SER CASE : 43361 SER - UNCOMMANDED PITCH-UP ON RH AP DURING FINAL PILOTS REPORT: UNEXPECTED AIRCRAFT PITCH-UP WHILE LEVEL AND ON LH AP DURING FINAL TO DAR. ILS LOC WAS CAPTURED AND GS ARMED, PLANE SUDDENLY PITCHED UP 10 DEG, ABOVE THE FD WHICH REMAINSDR HALA2019032500144Fcu · faultedETOPS SIGNIFICANT SYSTEM - ECAM AUTO FLT FCU FAULT- BARO REF CHECK ILLUMINATED AT FL230 IN LEVEL FLIGHT. POST FLT REPORT SHOWS AUTO FLT FCU FAULT & FCU (3CA) CLASS 1 FAULT. T/S PER TSM 22-81-00-810*801A. PERF AFS SYS TEST. TEST OK. OK FOR SVC.SDR AALA201903259003Autopilot Sys · malfunctionedHAD AN UNCOMMANDED AUTOPILOT DISCONNECT, LT AUTOPILOT, 4 HOURS INTO FLIGHT. TURNED BACK ON DURING THE DESCENT AND WORKED REMAINDER OF FLIGHT. MAINTENANCE ACCOMPLISHED MCDP GROUND TEST 01 , L FCC IAW FIM 22-03-00-805-827, NO FAULTS FOUND . PERFORMED MCDP GROUSDR ASAA2019032128715Unknown · malfunctionedUNSUCCESSFUL AUTOLAND ON SEA RWY 16R EXCEED GREATER THAN 35FT FROM CENTERLINE ON TOUCHDOWN. WAS CLEAR, WIND 190/11. GROUNDED - YES. ACCOMPLISHED AMM 22-00-01-730-803 MAINTENANCE TESTS FOR MEL 22-99C DFCS BITE GROUPS #60 AND 35. ALL DFCS BITE TESTS PASSED. ALSOSDR HALA2019032200140Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM AUTO FLT FCU FAULT- BARO REF CHECK ILLUMINATED AT FL230 IN LEVEL FLIGHT. POST FLT REPORT SHOWS AUTO FLT FCU FAULT & FCU (3CA) CLASS 1 FAULT. T/S PER TSM 22-81-00-810*801A. PERFORMED AFS SYSTEM TEST. TEST OK. OK FOR SERVICE. NO 3SDR VNAA2019031511101Circuit Breaker · trippedDURING APPROACH THE CREW RECEIVED MULTIPLE PITCH FEEL CAUTION AND RUDDER / LIMIT FAULT MESSAGES. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT / INCIDENT. THE AIRCRAFT WAS ABLE TO TAXI TO THE GATE. TRUCKS ROLLED. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE FORSDR FDEA201903150644Transducer · out of adjustA/P ON IN VNAV, BELOW PATH, THROTTLES IDLE AIRCRAFT NOSE PITCHES DOWN RESULTING IN 6000' FPM DESCENT WITH AIRSPEED INCREASING AND SPEED BRAKES OUT. AIRCRAFT DOES NOT HONOR AIRSPEED, VNAV PATH, OR VERTICAL SPEED. AUTOPILOT DISENGAGED WITH VERY HEAVY NOSE DOWINSDR HALA2019031500126Relay · failedETOPS SIGNIFICANT SYSTEM - AFTER START STATUS PAGE INDICATING CAT 3 SINGLE ONLY/INOP SYSTEM, CAT3 DUAL NOTE AND GROUND POWER FAILED AT GATE PRIOR TO APU START. AS PER CREW MSG CLEARED AFTER ENGINE SHUTDOWN, UNABLE TO DUPLICATE FAULT, RESTARTING ENGINE AT GATE SDR AALA201903139002Autopilot Sys · malfunctionedTHE PILOT REPORTED THAT THE RT AUTOPILOT UNCOMMANDEDLY DISCONNECTED. MAINTENANCE PERFORMED AN FCC TEST THROUGH MCDP. NO FAULTS. ENGAGED THE RT AUTOPILOT AND MOVED FLIGHT CONTROLS. DID NOT DISCONNECT. NO FAULTS CAN BE DUPLICATED.SDR HNAA2019031100071Warning System · false activationPDIS 692 22-10 1874591 10MAR19 PHL CLOSE UNCOMMANDED AUTO PILOT FAIL IN FLIGHT WITH ASSOC. EICAS MSGS FACT 10MAR19 08:20 PHL
FUNCTIONAL TESTED AUTO PILOT AIW AMM 22-11-00-700-803-A FUNCTIONAL TEST GOOD WITH NO DEFECTS NOTED, OK FOR SERVICE AT THIS TISDR ASAA2019030928548Unknown · malfunctionedTHE 'A' AUTO PILOT IS NOT WORKING. THE 'B' AUTOPILOT OPERATES NORMALLY. GROUNDED - YES. PERFORMED DFCS BITE PROCEDURE REF FIM 22-11 TASK 801. CURRENT STATUS SHOWED NO FAULTS. FAULT HISTORY HAD ONE OCCURRENCE OF FAULT #22-11251 AFCS ENGAGE INTLK ON LEG 14 (09 MSDR ASAA2019030928549Computer · intermittentAUTOPILOT B WILL NOT ENGAGE IN FLIGHT. GROUNDED - YES. DFCS FAULT REVIEW SHOWS NUMEROUS FAULT MSG #22-11340 (CH-B R SNSR EXC INV) & MSG #22-11338 (CH-B P SNSR EXC INV). ACCOMPLISHED FIM 22-16 TASK 829 & FIM 22-16 TASK 828. GVI FCC -B INTLK CB'S & CHECKED POWERSDR HNAA2019031100070Warning System · false activationNDIS 636 22-99 0023230 09MAR19 PHL CLOSE **** THIS DISCREPANCY CREATED FOR MIR PURPOSES **** CREW PREVIOUSLY HAD ISSUE WITH OH BIN PRIOR TO DEPARTURE. CREW C/W MEL PROCEDURE. THEN CREW ABORTED T/O FOR AUTOPILOT MSG AT TAKEOFF, CREW RESET SYSTEM ALL SYSTESDR ASAA2019030728517Unknown · malfunctionedFIRST OFFICER FD FLAG DISPLAYED. GROUNDED - YES. DFCS SHOWS NO B CHANNEL. FOUND AFCS SYS B FCC DC C/B ON P6-3 OUT. ACCOMPLISHED C/B RESET REF AMM 20-60-01. OPS CHECK NORMAL REF AMM 22-11-33/401. BITE TEST GROUP 35. GROUND VERIFICATION TEST GOOD.SDR ASAA2019030528483Unknown · malfunctionedFD ON FO SIDE. GROUNDED - YES. REL PER MEL 34-12D FO FD INOP AND 22-99B AUTOLAND NOT AUTHORIZED AND 34-99B CAT III HGS NOT AUTH. REFER TO LOG 12044905, F/O'S FD OPS NORMAL PER FIM 22-11 TASK 801 CLEARS MELS 34-12D, 22-99B AND 34-99B.SDR ASAA2019030528478Warning System · false activationAFTER PUSH-BACK AND MASTER CAUTION RECALL, FLT CREW OBSERVED SPEED TRIM AND MACH TRIM CAUTION LIGHT. GROUNDED - YES. FOUND DFCS SYS "B" INOP. CYCLED C/B'S ON P6-2 B1,B2,B4,C1, C2 AND C3 REF FIM 22-11 TASK 826 AND DFCS "B" POWERED UP. PERFORMED FCC INSTALLATIONSDR ASAA2019022428377Control Panel · brokenSMALL PIECE OF GLARESHIELD TRIM BROKE OFF JUST ABOVE ALTITUDE WINDOW. GROUNDED - YES. REPLACED MCP, REF B737-900 AMM 22-11-34-400-801. MCP INSTALLATION TEST NML, REF AMM 22-11-34-740-801. LAND VERIFY TEST FAILED WITH SPOILER 4 POS SENSOR 2, MSG 22-11158. AC CHSDR ASAA2019022428341Computer · malfunctionedFMGC NR 2 INOP. GROUNDED - YES. RESET NR 2 FMGC IN REF TO AMM 22-70-00. OPS CHECK GOOD.SDR ASAA2019022548326Sensor · out of adjustTRANSFERRED FROM MIG-2C S/N 40-0016298, ITEM 2: ELEVATOR DUAL AUTHORITY CHECK FAILS STEP 52.27. GROUNDED - YES. ADJUSTED "B" STABILIZER POSITION SENSOR REF B737-800 AMM TASK 22-11-31-820-801. ADJUSTED ELEVATOR NEUTRAL SHIFT SENSOR REF TASK 22-11-14-820-801. ADSDR ASAA2019022538306Lever · excess playELEVATOR AUTOPILOT SYSTEM "A" ACTUATOR LEVER HAS PLAY, LLM TESTS REQUIRED AT COMPLETION. GROUNDED - YES. REMOVED AND REPLACED THE "A" SYSTEM AUTOPILOT ACTUATOR LEVER ASSY REF B737-800 AMM 22-11-26/401. VERIFIED ADJUSTMENT REF AMM 22-11-26-820-801. NOTE: NO ADJ
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