N524MD, cancelled Sep 12, 2013

Service difficulty reports · 43

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N524MD' AND deregistration_id = 'N524MD-2013-09-12'
  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 22AA201000068Stud · damagedOIL PRESSURE NR 2 GAUGE DROPPED TO ZERO AND NR 2 OIL PRESS LOW LIGHT CAME ON, ENGINE SHUTDOWN IAW CHECK LIST. FOUND OIL LEAK COMING FROM CRANK PAD COVER, INSTALLED 1EA COVER PAD STUD, REINSTALLED 1EA COVER PAD STUD IAW GE SPM 70-48-01, REINSTALLED COVER PAD IAApr 25, 2010 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR 22AA201000067AControl Cable · brokenACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPOILERS NOT DEPLOYING FULLY & SPOILER HANDLE NOT RETRACTING AUTOMATICALLY. ALSO SPOILER PANEL 1 & 2 NOMar 28, 2010 · N524MD · Doug DC1030 · Aileron Control SystemSDR 22AA201000048Frame · corrodedDURING "C" CHECK , AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD CORRODED AT LBL 15 TO RBL 15 AS MARKED. NON-ROUTINE NR 0610, AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD, LBL 15 TO RBL 15 CORROSION, REMOVED AND REPROTECTED IAWFeb 13, 2010 · N524MD · Doug DC1030F · Fuselage Main, FrameSDR 22AA201000047Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000046Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE RT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000045Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000044Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000043Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL FOUND UPPER LONGERON WITH CRACK. NON-ROUTINE NR 393, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW ENGINEERING NOTE (EN) 1006-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000042Skin · wornDURING "C" CHECK , NR 2 ENGINE LT CORE COWL UPPER SKIN FOUND WITH WEAR MARKS. NON-ROUTINE NR 440, WEAR MARKS ON NR 2 ENGINE LT CORE COWL UPPER SKIN AREA REPAIRED IAW EN 1007-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000041Fairing · crackedDURING "C" CHECK, NR 1 ENGINE PYLON FWD FAIRING FWD SIDE FOUND WITH CRACK. NON-ROUTINE NR 224, CRACK AREA AT NR 1 ENGINE PYLON FWD FAIRING FWD SIDE AREA REPAIRED IAW EN 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 22AA201000040Skin · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL FWD LOWER SKIN FOUND WITH CRACK. NON-ROUTINE NR 439, CRACK AREA AT NR 2 ENGINE RT CORE COWL FWD LOWER SKIN AREA REPAIRED IAW EN 1009-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000039Fairing · crackedDURING "C" CHECK, NR 3 PYLON FWD FAIRING FOUND WITH CRACKED AT 02 LOCATIONS. NON-ROUTINE NR 227, 02 EACH CRACK LOCATIONS AT NR 3 ENGINE PYLON FWD FAIRING AREA REPAIRED IAW 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3, DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 22AA201000038Skin · crackedDURING "C" CHECK, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN FOUND CRACK. NON-ROUTINE NR 372, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN REPAIR IAW EN 1003-10 AND FAA APPROVED FORM 8110-3 DATED 24 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Wing, Plate/SkinSDR 22AA201000036Duct · damagedINDICATION OF NR 2 ENGINE FIRE, SEVERED DAMAGE/SEPARATION CHECK LIST, COMPLETED FIRED BOTH BOTTLES, FIRE LIGHTS STILL ON, DECLARED AND EMERGENCY AND LANDED. FOUND NR 2 ENG PRE COOLER PENUAMTIC DUCT DAMAGED, REMOVED AND REPLACED PRE COOLER PNEUMATIC DUCT ASSY Feb 4, 2010 · N524MD · Doug DC1030 · Pneumatic Distribution SystemSDR 22AA201000035Line · leakingDURING CLIMB OUT, NR 1 HYD SYS START LOOSING FLUID, INITIATION PROCEDURE ON ALT PROCEDURES CHECK LIST, HYD FLUID LOST, DURING CLIMB OUT TO CRUISE NR 2 ENG FAIL, SECURED ENGINE IAW CHECK LIST. DUMP FUEL TO MAX LANDING WEIGHT TO LANDING, DURING POST FLIGHT FOUNJan 22, 2010 · N524MD · Doug DC1030 · Hydraulic System, MainSDR 22AA200900030Lamp · inoperativeEMERGENCY LIGHTS DISARMED LT INOP. REMOVED AND INSTALLED LAMP, TEST OK IAW AMM 33-50-02.Nov 7, 2009 · N524MD · Doug DC1030 · Emergency LightingSDR 22AA200900026Line · damagedAIR TURN BACK, DURING CLIMB OUT LOST HYD. QUANTITY NR 1 SYSTEM REF. TO ABNORMAL, ALTERNATE CK. LIST. FOUND LINE FROM OUTBOARD SLAT HYD DRIVE CYLINDER TO CHECK VALVE LEAKING, REMOVED LINE FROM O/B SLAT DRIVE CYLINDER TO CHECK VALVE IAW MM 20-10-01. INSTALLED RSep 24, 2009 · N524MD · Doug DC1030 · Hydraulic System, MainSDR 22AA200900025Tire · failedON LANDING, NR 4 TIRE FAILED. DEBRIS FROM TIRE CAUSED SLIGHT DAMAGE TO LWR OTBD GEAR DOOR. REMOVED NR 4 TIRE ASSY AND INSPECTED RT LANDING GEAR AXLE, NO DEFECT NOTED. REPLACED NR 4 TIRE ASSY IAW MM 32-41-02, REMOVED AND REPLACED NR 3 MAIN TIRE ASSY IAW MM 3Sep 20, 2009 · N524MD · Doug DC1030 · TireSDR 22AA200900002Engine · stalledNR 2 ENGINE COMPRESSOR STALLED ABRUPTLY AFTER TAKEOFF. REDUCED POWER AND PROCEEDED WITH ABNORMAL CHECK LIST. ENGINE SHUTDOWN AT 03:18Z. SHUT DOWN NR 2 ENGINE DUE TO SEVERE COMPRESSORS STALLS, EVEN AT FLIGHT IDLE. ENGINE SHUTDOWN OCCURED AFTER TAKEOFF DURING INJun 21, 2009 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR 22AA20090202Pump · failedNR1 ENGINE HAS A VIBRATION. LOSS CHANNEL 3 IN FLIGHT. RUDDER TRIM LOCKED UP IN FLIGHT AT ZERO POSITION AND FLIGHT CONTROL BECAME STIFF WITH SOME VIBRATION AFTER FLAP EXTENSION. PERFORMED VIBRATION CHECK ON ENGINE S/N 517620 NR1 POSITION IAW AMM 72-00-00 PAGE Feb 15, 2009 · N524MD · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 22AA20090101Bracket · brokenCTR LANDING GEAR JACK BRACKET BROKEN ON LANDING GEAR; CTR LANDING GEAR DOORS DAMAGED. REMOVED CENTER LANDING GEAR BROKEN RETRACT CYLINDER JACK BRACKET IN ACCORDING WITH MM 32-00-00.Jan 4, 2009 · N524MD · Doug DC1030F · Fuselage Miscellaneous StructureSDR 22AA20081202Engine · failedON TAKEOFF AT 800FT NR 1 ENGINE FAILED. ENGINE REPLACEMENT IN PROGRESS. ACCOMPLISHED RED BORDER 025093. REMOVED AND REPLACED NR 1 ENGINE IAW WORK CARD 141R7101M, PERFORMED ENGINE RUN UP IAW MM 71-00-00, 71-06-00; OPERATION NORMAL, NO LEAKS NOTED.Dec 11, 2008 · N524MD · Doug DC1030F · Engine (Turbine/Turboprop)SDR ARW2008F00001Windshield · crackedCAPTAIN`S WINDSHIELD ARCED; IT APPEARS TO HAVE AN APPROXIMATELY 6 INCH CRACK ON OUTER PANEL. PERFORMED ATT PROCEDURE "WINDSHIELD OR CLEARVIEW WINDOW CRACKED OR ARCING; FLIGHT RETURNED TO DEPARTURE IAW COMPANY`S REQUEST. REMOVED CAPTAIN`S WINDSHIELD IAW AMM 56Aug 27, 2008 · N524MD · Doug DC1030 · Flight Compartment WindowsSDR ARW2008F00000Indicator · failedF/O ALTIMETER FAILED IN TAKEOFF; WORKED OK IN CLIMB AND CRUISE. REMOVED AND REPLACED ALTIMETER INDICATOR IAW MM 34-02-01; PERFORMED OPS CHECK IAW M34-12-00; FOUND NORMAL. (K)Jul 23, 2008 · N524MD · Doug DC1030 · Altimeter, Barometric/EncoderSDR ARWA20080604Connector · looseNR 3 ENGINE EGT ERRATIC DURING LANDING ROLLS. FOUND LOOSE CONNECTOR PI-8036. RE-SECURED IT IN ACCORDANCE WITH MM 20-30-02. OPERATIONAL CHECK SYSTEM FOUND NORMAL IAW MM 71-00-00. (A)Jun 25, 2008 · N524MD · Doug DC1030 · Engine Indicating System WiringSDR ARWA20080602Connector · looseEGT FAILED IN FLIGHT, PERFORMED ENGINE FAILURE SHUTDOWN IN FLIGHT CHECK LIST. LANDED UNEVENTFUL. TIGHTENED NR 3 ENGINE CONNECTOR PL-8036 IN ACCORDANCE WITH M/M 20-30-01. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 77-21-004 WD 77-21-01 PG 005. (A)Jun 21, 2008 · N524MD · Doug DC1030F · Engine Indicating System WiringSDR ARWA20080203Indicator · malfunctionedNR 2 ENGINE NO EGT INDICATOR FOUND ON POINTER OR DIGITAL READ OUT ON ENGINE START, ALL OTHER PARAMETERS NORMAL START. SHUTDOWN ENGINE. REMOVED AND REPLACED EGT INDICATOR CHECKED GOOD IN ACCORDANCE WITH M/M 77-20-00 AND M/M 71-00-00.Feb 13, 2008 · N524MD · Doug DC1030 · Engine EGT/TIT Indicating SystemSDR ARWA20080104Tail Cone · damagedON POST FLIGHT, FOUND TAIL CONE COWLING DAMAGE ON NR 1 ENGINE. PERFORMED GENERAL AREA INSPECTION AND CHECK PNEU DUCTING FOR CONDITION, NO DAMAGE FOUND. REMOVED AND REPLACED NR 1 ENGINE O/B AFT CORE COWLING IN ACCORDANCE WITH DC-1030 M/M REF 71-13-01.Jan 29, 2008 · N524MD · Doug DC1030 · Engine Exhaust SystemSDR ARWA20071202Fuel Sys · low pressureDURING TAXI, NR 2 ENGINE FUEL PRESSURE INITIALLY INDICATING 20 PSI, THEN DROPPED TO ZERO, AS PER MEL 73-4 CATEGORY "C". REMOVED AND REPLACED # 2 ENGINE FUEL INTERSTAGE PRESSURE TRANSMITTER IAW MM 73-33-01. FUEL PRESSURE INDICATION NORMAL; CLEARED DMI 21297.Dec 13, 2007 · N524MD · Doug DC1030 · Fuel Pressure IndicatingSDR ARWA20071201Pin · installedDURING FLIGHT CONTROL CHECK UNABLE TO MOVE CONTROL COLUMN FORE AND AFT. FOUND ELEVATOR LOCKING PIN ON ELEVATOR POSITION P-6. REMOVED AS REQUIRED IN ACCORDANCE WITH DC-10 M/M 27-31-00. OPERATIONAL CHECK OK IN ACCORDANCE WITH DC-10 M/M 27-31-00Dec 10, 2007 · N524MD · Doug DC1030 · Elevator StructureSDR ARWA20071102Valve · erraticON INITIAL TAKEOFF ROLL, UPON ADVANCING THE POWER LEVERS TO MAX TAKEOFF THRUST NR 1 ENGINE REVERSER PRESSURE LIGHT ILLUMINATED; CANCELLED THE TAKEOFF. LIGHT WENT OUT WHEN POWER WAS REDUCED TO IDLE. REVERSER NR 1 PREVIOUS DEACTIVATED AND SECURED LOCK, TRANSFENov 20, 2007 · N524MD · Doug DC1030 · Engine Thrust ReverserSDR ARWA20071002Engine · vibrationDURING CLIMB-OUT, NR 3 ENGINE HEAVY VIBRATION. TROUBLESHOT NR 3 ENGINE PER TAFI 72-00-00; FOUND VIBRATION AT FUEL LEVER AND THROTTLE, OUT OF ADJUSTMENT. ADJUSTED FUEL LEVER PER DC-10 M/M 76-12-00 AND THROTTLE PER DC-10 M/M 76-11-00. OPERATIONAL CHECK NORMALOct 18, 2007 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR ARWA20070402O-Ring · unknownNR 1 ENGINE PRECAUTIONARY ENGINE SHUTDOWN, LOW OIL PRESSURE INDICATIONS. C-SUMP TUBE AT 6 O'CLOCK POSITION SLEEVE AND O-RING DAMAGED. REPLACE O-RINGS AND SECURED SLEEVE IN ACCORDANCE WITH ARROW M/M 70-00-00. DURING RUN-UP, NO LEAKS FOUND AND OIL PRESSURE NOApr 25, 2007 · N524MD · Doug DC1030 · Engine Oil Indicating SystemSDR ARWA20070308Antenna · inoperativeRADAR NR 2 DOES NOT PAINT AND WEATHER IN FLIGHT TEST PATTERN OK ON THE GROUND. REMOVED AND REPLACED WEATHER RADAR ANTENNA IN ACCORDANCE WITH M/M 34-41-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-41-00.Mar 27, 2007 · N524MD · Doug DC1030 · Weather Radar SystemSDR ARWA20060308Antenna · faultyRADAR NR 2 DOES NOT PAINT AND WEATHER IN FLIGHT TEST PATTER OK ON THE GROUND. REMOVED AND REPLACED WEATHER RADAR ANTENNA IN ACCORDANCE WITH M/M 34-41-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-41-00.Mar 27, 2007 · N524MD · Doug DC1030 · Weather Radar SystemSDR ARWA20070303Support · chafedDURING "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP "A" SUPPORT IN FLAP WELL CHAFED. BLEND-OUT AREA FOUND WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8.Mar 15, 2007 · N524MD · Doug DC1030 · Trailing Edge FlapsSDR ARWA20070302Fitting · gougedDURING AN "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP I/B THE UNIT FITTING WAS TWO GOUGES. BLEND-OUT AREAS, FOUND WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8.Mar 13, 2007 · N524MD · Doug DC1030 · Trailing Edge FlapsSDR ARWA20051103Drive Assy · damagedDURING APPROACH, AUTO PILOT OUT OF TRIM LIGHT ILLUMINATED; DISCONNECTED STABILIZER JAMMED AT 1 DEGREE NOSE UP. REMOVED AND REPLACED HORIZONTAL STABILIZER CHAIN DRIVE UNIT IN ACCORDANCE WITH DC-10 M/M 27-44-05. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH Nov 24, 2005 · N524MD · Doug DC1030 · Stabilizer Position IndicatingSDR ARWA20051003Valve · failedAPPROACHING TOP OF CLIMB (TOC) OUT OF TJSJ; DENSE WHITE SMOKE ENTERING THE COCKPIT AREA WHILE PERFORMING SMOKE SOURCE 10 CHECKLIST, SMOKE STOPPED; FLIGHT CONTINUED OK. PERFORMED T/S DC-10 M/M TAFI 21-50-00; FOUND NR 3 PACK EXHAUST DOOR STAYING CLOSED; DEFERREOct 11, 2005 · N524MD · Doug DC1030 · Ice DetectionSDR ARWA20050701Bungee Cord · brokenDURING PRE-FLIGHT, FOUND NOSE GEAR, ONE OF THE SPRINGS FOUND BROKEN (RT NOSE SPRING BUNGEE). REMOVED AND REPLACED RT BUNGIE SPRING IN ACCORDANCE WITH M/M 32-22-01. NO ADJUSTMENT REQUIRED.Jul 19, 2005 · N524MD · Doug DC1030 · Landing Gear Retraction/Extension SystemSDR ARWA20050407Indicator · faultyDURING ENGINE START & FUEL LEVER ON NR 2 ENGINE EGT RISE RAPIDLY; ENGINE SHUTDOWN AT 700 FT AFT ENGINE SHUTDOWN EGT INDICATION CONTINUED TO MAX LIMITS. REMOVED AND REPLACED NR 2 ENGINE EGT INDICATOR; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC-10 M/M 77-10Apr 30, 2005 · N524MD · Doug DC1030 · Engine EGT/TIT Indicating SystemSDR ARWA20050406Inu · failedREJECTED TAKEOFF AT 95 KTS. CAPTAIN'S (ADI) ATTITUDE DIRECTOR INDICATOR TUMBLED. REMOVED AND REPLACED INU-3 IAW MM 34-43-04 SYSTEM GROUND TEST OK IAW LTN-72 MM 34-43-04. THIS CLEARS DMI 19174Apr 29, 2005 · N524MD · Doug DC1030 · Attitude and Direction Data SystemSDR ARWA20050204Smoke Detector · malfunctionedDURING DESCENT TIME 02:34 LOWER FORWARD CARGO SMOKE LIGHT COMES ON. PROCEEDED TO ACCOMPLISHED EMERGENCY CHECKLIST. DISCHARGED CYL NR 1. TRANSFERRED TO DMI 18988 IN ACCORDANCE WITH MEL 26-21 CAT-C PLACARD INSTALLED LOWER CARGO COMPARTMENTS MUST REMAIN EMPTY. Feb 12, 2005 · N524MD · Doug DC1030 · Smoke Detection
Back to N524MD, cancelled Sep 12, 2013