# Service difficulty reports: N524MD, cancelled Sep 12, 2013

A list on [N524MD, cancelled Sep 12, 2013](https://openairdocs.org/deregistered/N524MD-2013-09-12.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 22AA201000068](https://openairdocs.org/sdr/22AA201000068.md): Stud · damaged · Apr 25, 2010 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > OIL 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 IA
- [SDR 22AA201000067A](https://openairdocs.org/sdr/22AA201000067A.md): Control Cable · broken · Mar 28, 2010 · N524MD · Doug DC1030 · Aileron Control System
  > ACFT 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 NO
- [SDR 22AA201000048](https://openairdocs.org/sdr/22AA201000048.md): Frame · corroded · Feb 13, 2010 · N524MD · Doug DC1030F · Fuselage Main, Frame
  > DURING "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 IAW
- [SDR 22AA201000047](https://openairdocs.org/sdr/22AA201000047.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "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.
- [SDR 22AA201000046](https://openairdocs.org/sdr/22AA201000046.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "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.
- [SDR 22AA201000045](https://openairdocs.org/sdr/22AA201000045.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "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.
- [SDR 22AA201000044](https://openairdocs.org/sdr/22AA201000044.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "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.
- [SDR 22AA201000043](https://openairdocs.org/sdr/22AA201000043.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "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 2
- [SDR 22AA201000042](https://openairdocs.org/sdr/22AA201000042.md): Skin · worn · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/Skin
  > DURING "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.
- [SDR 22AA201000041](https://openairdocs.org/sdr/22AA201000041.md): Fairing · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main Frame
  > DURING "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.
- [SDR 22AA201000040](https://openairdocs.org/sdr/22AA201000040.md): Skin · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/Skin
  > DURING "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.
- [SDR 22AA201000039](https://openairdocs.org/sdr/22AA201000039.md): Fairing · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main Frame
  > DURING "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.
- [SDR 22AA201000038](https://openairdocs.org/sdr/22AA201000038.md): Skin · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Wing, Plate/Skin
  > DURING "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.
- [SDR 22AA201000036](https://openairdocs.org/sdr/22AA201000036.md): Duct · damaged · Feb 4, 2010 · N524MD · Doug DC1030 · Pneumatic Distribution System
  > INDICATION 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
- [SDR 22AA201000035](https://openairdocs.org/sdr/22AA201000035.md): Line · leaking · Jan 22, 2010 · N524MD · Doug DC1030 · Hydraulic System, Main
  > DURING 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 FOUN
- [SDR 22AA200900030](https://openairdocs.org/sdr/22AA200900030.md): Lamp · inoperative · Nov 7, 2009 · N524MD · Doug DC1030 · Emergency Lighting
  > EMERGENCY LIGHTS DISARMED LT INOP. REMOVED AND INSTALLED LAMP, TEST OK IAW AMM 33-50-02.
- [SDR 22AA200900026](https://openairdocs.org/sdr/22AA200900026.md): Line · damaged · Sep 24, 2009 · N524MD · Doug DC1030 · Hydraulic System, Main
  > AIR 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 R
- [SDR 22AA200900025](https://openairdocs.org/sdr/22AA200900025.md): Tire · failed · Sep 20, 2009 · N524MD · Doug DC1030 · Tire
  > ON 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 3
- [SDR 22AA200900002](https://openairdocs.org/sdr/22AA200900002.md): Engine · stalled · Jun 21, 2009 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > NR 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 IN
- [SDR 22AA20090202](https://openairdocs.org/sdr/22AA20090202.md): Pump · failed · Feb 15, 2009 · N524MD · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main
  > NR1 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
- [SDR 22AA20090101](https://openairdocs.org/sdr/22AA20090101.md): Bracket · broken · Jan 4, 2009 · N524MD · Doug DC1030F · Fuselage Miscellaneous Structure
  > CTR 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.
- [SDR 22AA20081202](https://openairdocs.org/sdr/22AA20081202.md): Engine · failed · Dec 11, 2008 · N524MD · Doug DC1030F · Engine (Turbine/Turboprop)
  > ON 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.
- [SDR ARW2008F00001](https://openairdocs.org/sdr/ARW2008F00001.md): Windshield · cracked · Aug 27, 2008 · N524MD · Doug DC1030 · Flight Compartment Windows
  > CAPTAIN`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 56
- [SDR ARW2008F00000](https://openairdocs.org/sdr/ARW2008F00000.md): Indicator · failed · Jul 23, 2008 · N524MD · Doug DC1030 · Altimeter, Barometric/Encoder
  > F/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)
- [SDR ARWA20080604](https://openairdocs.org/sdr/ARWA20080604.md): Connector · loose · Jun 25, 2008 · N524MD · Doug DC1030 · Engine Indicating System Wiring
  > NR 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)
- [SDR ARWA20080602](https://openairdocs.org/sdr/ARWA20080602.md): Connector · loose · Jun 21, 2008 · N524MD · Doug DC1030F · Engine Indicating System Wiring
  > EGT 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)
- [SDR ARWA20080203](https://openairdocs.org/sdr/ARWA20080203.md): Indicator · malfunctioned · Feb 13, 2008 · N524MD · Doug DC1030 · Engine EGT/TIT Indicating System
  > NR 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.
- [SDR ARWA20080104](https://openairdocs.org/sdr/ARWA20080104.md): Tail Cone · damaged · Jan 29, 2008 · N524MD · Doug DC1030 · Engine Exhaust System
  > ON 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.
- [SDR ARWA20071202](https://openairdocs.org/sdr/ARWA20071202.md): Fuel Sys · low pressure · Dec 13, 2007 · N524MD · Doug DC1030 · Fuel Pressure Indicating
  > DURING 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.
- [SDR ARWA20071201](https://openairdocs.org/sdr/ARWA20071201.md): Pin · installed · Dec 10, 2007 · N524MD · Doug DC1030 · Elevator Structure
  > DURING 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 27-31-00
- [SDR ARWA20071102](https://openairdocs.org/sdr/ARWA20071102.md): Valve · erratic · Nov 20, 2007 · N524MD · Doug DC1030 · Engine Thrust Reverser
  > ON 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, TRANSFE
- [SDR ARWA20071002](https://openairdocs.org/sdr/ARWA20071002.md): Engine · vibration · Oct 18, 2007 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > DURING 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 NORMAL
- [SDR ARWA20070402](https://openairdocs.org/sdr/ARWA20070402.md): O-Ring · unknown · Apr 25, 2007 · N524MD · Doug DC1030 · Engine Oil Indicating System
  > NR 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 NO
- [SDR ARWA20070308](https://openairdocs.org/sdr/ARWA20070308.md): Antenna · inoperative · Mar 27, 2007 · N524MD · Doug DC1030 · Weather Radar System
  > RADAR 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.
- [SDR ARWA20060308](https://openairdocs.org/sdr/ARWA20060308.md): Antenna · faulty · Mar 27, 2007 · N524MD · Doug DC1030 · Weather Radar System
  > RADAR 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.
- [SDR ARWA20070303](https://openairdocs.org/sdr/ARWA20070303.md): Support · chafed · Mar 15, 2007 · N524MD · Doug DC1030 · Trailing Edge Flaps
  > DURING "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.
- [SDR ARWA20070302](https://openairdocs.org/sdr/ARWA20070302.md): Fitting · gouged · Mar 13, 2007 · N524MD · Doug DC1030 · Trailing Edge Flaps
  > DURING 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.
- [SDR ARWA20051103](https://openairdocs.org/sdr/ARWA20051103.md): Drive Assy · damaged · Nov 24, 2005 · N524MD · Doug DC1030 · Stabilizer Position Indicating
  > DURING 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
- [SDR ARWA20051003](https://openairdocs.org/sdr/ARWA20051003.md): Valve · failed · Oct 11, 2005 · N524MD · Doug DC1030 · Ice Detection
  > APPROACHING 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; DEFERRE
- [SDR ARWA20050701](https://openairdocs.org/sdr/ARWA20050701.md): Bungee Cord · broken · Jul 19, 2005 · N524MD · Doug DC1030 · Landing Gear Retraction/Extension System
  > DURING 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.
- [SDR ARWA20050407](https://openairdocs.org/sdr/ARWA20050407.md): Indicator · faulty · Apr 30, 2005 · N524MD · Doug DC1030 · Engine EGT/TIT Indicating System
  > DURING 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 77-10
- [SDR ARWA20050406](https://openairdocs.org/sdr/ARWA20050406.md): Inu · failed · Apr 29, 2005 · N524MD · Doug DC1030 · Attitude and Direction Data System
  > REJECTED 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 19174
- [SDR ARWA20050204](https://openairdocs.org/sdr/ARWA20050204.md): Smoke Detector · malfunctioned · Feb 12, 2005 · N524MD · Doug DC1030 · Smoke Detection
  > DURING 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.

## 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 n_number = 'N524MD' AND deregistration_id = 'N524MD-2013-09-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N524MD-2013-09-12/reports

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