# Service difficulty reports: N583MD, cancelled Oct 28, 2011

A list on [N583MD, cancelled Oct 28, 2011](https://openairdocs.org/deregistered/N583MD-2011-10-28.md).

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

Page 1 of 2 · 63 reports

- [SDR 2ARF201101005](https://openairdocs.org/sdr/2ARF201101005.md): Plate · broken · Jan 15, 2011 · N583MD · Doug MD83 · Aileron Control System
  > CAPTAIN REPORTED THAT DURING CRUISE, ACFT REQUIRED 4 GRADES OF AILERON COMPENSATOR TO MAINTAIN STRAIGHT AND LEVELED FLIGHT. DURING MX REVISION, THE SPIRAL DRIVE PLATE WAS DETECTED BROKEN; SO THE SPIRAL DRIVE PLATE WAS REPLACED IAW MM 27-10-07, TESTED CORRECT.
- [SDR 2ARF201101003](https://openairdocs.org/sdr/2ARF201101003.md): Water Separator · leaking · Jan 10, 2011 · N583MD · Doug MD83 · Humidity Control System
  > ACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO LOSS OF CABIN PRESSURE AT 36,000 FT. DURING MX REVISION, THE LT WATER SEPARATOR DUCT WAS DETECTED LEAKING; SO THE AIR CONDITIONING, PNEUMATIC AND ANTI ICE SYS LEAK CHECKS WERE PERFORMED IAW MM 21-00-00, 36-00-00 AN
- [SDR 2ARF201012003](https://openairdocs.org/sdr/2ARF201012003.md): Motor · damaged · Dec 13, 2010 · N583MD · Doug MD83 · Stabilizer Position Indicating
  > ACFT PERFORMED AN UNSCHEDULED LANDING; DURING LANDING THE STAB OUT OF TRIM LIGHT TUNED ON. MX REPLACED THE STABILIZER TRIM MOTOR IAW MM 27-41-71, TESTED CORRECT.
- [SDR 2ARF201012002](https://openairdocs.org/sdr/2ARF201012002.md): Drive Unit · damaged · Dec 5, 2010 · N583MD · Doug MD83 · AC Generator-Alternator
  > CAPTAIN REPORTED THAT DURING CLIMB THE RT UVC AND GENERATOR WERE DISCONNECTED BY HIGH TEMPERATURE; SO THE FLIGHT CREW PERFORMED THE DRIVE GENERATOR MALFUNCTION PROCEDURE, CONFIRMING THE FAILURE AND SHUT DOWN THE UVC AND GENERATOR, CONTINUING TO DESTINATION. DU
- [SDR 2ARF201010003](https://openairdocs.org/sdr/2ARF201010003.md): Radome · cracked · Oct 13, 2010 · N583MD · Doug MD83 · Aerodynamic Fairings
  > DURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON ACFT RADOME. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING A CRACK OF 21 INCHES LENGTH AND 15 INCHES WIDE IN THE MENTIONED RADOME, OUT OF OPERATION LIMITS. TECH REPLACED RADOME IAW MM 53-51-00, ALL C
- [SDR 2ARF201008001A](https://openairdocs.org/sdr/2ARF201008001A.md): Pump · failed · Aug 14, 2010 · N583MD · Doug MD83 · Fuel Boost Pump
  > AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE CENTRAL TANK FUEL PUMP FAILED AND THE BACK PUMP BREAKER THREW OUT. MAINTENANCE PERSONNEL DEFERRED THE REPORT IAW MEL 28-2 CAT C. AT GDL MAINTENANCE BASE, TECHNICAL PERSONNEL REPLACED THE AFT CENTRAL FUEL BOO
- [SDR 2ARF201007001](https://openairdocs.org/sdr/2ARF201007001.md): Transceiver · faulty · Jul 10, 2010 · N583MD · Doug MD83 · Weather Radar System
  > AIRCRAFT RETURNED DUE TO DURING CLIMB, THE RADAR MONITOR IMAGE DISAPPEARED, INDICATING "ANT FAULT". MAINTENANCE PERSONNEL REPLACED AND TESTED THE WEATHER RADAR ANT AND RECEIVER TRANSMITTER IAW MM 34-41-01/-04 AND MM 34-41-00, ALL CORRECT. THE OVERWEIGHT INSP
- [SDR 2ARF201006004](https://openairdocs.org/sdr/2ARF201006004.md): Valve · open · Jun 12, 2010 · N583MD · Doug DC983 · Fuel Storage
  > DURING FUELING, A FUEL LEAK OCCURRED IN THE LEFT WING WHILE FILLING THE RIGHT TANK DUE TO AIRCRAFT WAS PARKED ON UNEVEN RAMP AND THE SUPPLY VALVE DID NOT CLOSE. THE LEFT WING SPILL WAS ABOUT 2 GALLONS.
- [SDR ASMF201002001](https://openairdocs.org/sdr/ASMF201002001.md): Duct · broken · Jan 28, 2010 · N583MD · Doug MD83 · Air Distribution System
  > ACFT RETURNED TO PLATFORM DUE TO AFTER ENGINES START, THE "TAIL COMP TEMP HI" LIGHT TURNED ON. MX REPLACED THE THERMO SWITCHES ON BOTH SIDES IAW MM 36-20-02 AND THE ACFT WAS DISPATCHED. AFTER THAT, THE ACFT RETURNED TO DEPARTURE, DURING CLIMB AT 9,000 FEET, TH
- [SDR EE4Y090277](https://openairdocs.org/sdr/EE4Y090277.md): Skin · delaminated · Sep 21, 2009 · N583MD · Doug MD83 · Wing Structure
  > RT WING INBOARD VANE FLAP OUTER AND INNER SKIN DELAMINATED.
- [SDR EE4Y090272](https://openairdocs.org/sdr/EE4Y090272.md): Stringer · corroded · Sep 17, 2009 · N583MD · Doug MD83 · Wing, Longeron/Stringer
  > RT WING FUEL TANK, AT STR 18R WITH CORROSION FROM XRS 69.000 TO XRS 91.000.
- [SDR EE4Y090298](https://openairdocs.org/sdr/EE4Y090298.md): Tee Fitting · corroded · Sep 16, 2009 · N583MD · Doug MD83 · Wing Miscellaneous Structure
  > LT WING, STA XTE 342, TRAILING EDGE TEE FLANGE CORRODED.
- [SDR EE4Y090271](https://openairdocs.org/sdr/EE4Y090271.md): Stringer · corroded · Sep 16, 2009 · N583MD · Doug DC983 · Wing, Longeron/Stringer
  > LT WING FUEL TANK INTERNAL STRUCTURE FROM XRS 69.000 TO XRS 137.750, STGR 18L, 19L, 20L, 21L AND 22L, CORRODED.
- [SDR EE4Y090250](https://openairdocs.org/sdr/EE4Y090250.md): Stringer · corroded · Sep 16, 2009 · N583MD · Doug DC983 · Wing, Longeron/Stringer
  > LT WING FUEL TANK INTERNAL STRUCTURE FROM XRS 69.000 TO XRS 137.750, STGR 18L, 19L, 20L, 21L AND 22L, CORRODED.
- [SDR EE4Y090270](https://openairdocs.org/sdr/EE4Y090270.md): Floor Support · cracked · Sep 14, 2009 · N583MD · Doug MD83 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE, STA 332 FWD CARGO COMPARTMENT, FLOOR SUPPORT PN 5936597-535 FLANGE CRACKED.
- [SDR EE4Y090269](https://openairdocs.org/sdr/EE4Y090269.md): Fitting · cracked · Sep 14, 2009 · N583MD · Doug DC983 · Fuselage Miscellaneous Structure
  > PAX CABIN, STA 1346 PASSENGER AFT ENTRANCE STAIRWELL DOOR, FITTING CRACKED.
- [SDR 2ARF200908001](https://openairdocs.org/sdr/2ARF200908001.md): Spoiler Sys · out of adjust · Aug 22, 2009 · N583MD · Doug MD83 · Drag Control System
  > ACFT RETURNED TO PLATFORM DUE TO SPOILER DEPLOYED LIGHT TURNED ON AND LEFT SPOILER PARTIALLY EXTENDED. MX ADJUSTED THE RT OTBD SPOILER, DEPLOYED SENSOR IAW MM 27-61-05 AND CHECKED SPOILER ACTUATORS MECHANISM IAW MM 27-60-00, ALL CORRECT.
- [SDR ASMF200803003](https://openairdocs.org/sdr/ASMF200803003.md): Switch · burned · Mar 30, 2008 · N583MD · Doug DC983 · Ignition System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE IN THE CABIN. MAINTENANCE DETECTED A SHORT CIRCUIT IN THE LT ENGINE SYS (A) IGNITION SWITCH, SO BREAKERS K-26 AND L26 WERE PULLED OUT AND AC WAS SENT TO THE HANGAR. AT HANGAR, SWITCH S1-35 WAS DETECTED BURNED SO IT WA
- [SDR ASMF200802005](https://openairdocs.org/sdr/ASMF200802005.md): Unknown · unknown · Feb 13, 2008 · N583MD · Doug DC983 · Standard Practices/Structures
  > AC RETURNED TO PLATFORM DUE TO IGNITION FAILURE IN LT ENGINE. MAINT REPLACED IGNITION BOX IAW MM 74-10-01, TESTED CORRECT. AC WAS DISPATCHED AND RETURNED TO PLATFORM AGAIN DUE TO THE SAME FAILURE. LT ENGINE WAS STARTED WITH EMERGENCY INVERTER, AND BREAKERS R2-
- [SDR ASMF200707013](https://openairdocs.org/sdr/ASMF200707013.md): Valve · unserviceable · Jul 16, 2007 · N583MD · Doug DC983 · Aircraft Fuel Distribution System
  > DURING TRANSIT CHECK A FUEL SPILLAGE OCCURRED AT PLATFORM. SPILLAGE STARTED WHEN THE AIRCRAFT WAS BEING REFUELED AND FUEL WAS TRANSFERRED FROM CENTRAL TANK TO LT TANK. MAINTENANCE PERSONNEL REPLACE THE LT FUEL FILL VALVE IAW MM 28-20-02 AND PERFORMED AN INDICA
- [SDR ASMF200707006](https://openairdocs.org/sdr/ASMF200707006.md): Spar Cap · cracked · Jul 9, 2007 · N583MD · Doug DC983 · Horizontal Stabilizer, Spar/Rib
  > COMPLEMENTING THE REPORT ASMF200707004 DATED ON JULY 5, 2007 WHICH INDICATES THAT (DURING THE INSPECTION OF THE HORIZONTAL STABILIZER REAR SPAR UPPER CAPS), REQUIRED BY THE AD 2007-10-04, DETECTED A CRACK OF (2) INCHES LONG AT STATION XH = 6.5 INCHES. MAINTEN
- [SDR ASMF200707004](https://openairdocs.org/sdr/ASMF200707004.md): Stabilizer · cracked · Jul 5, 2007 · N583MD · Doug MD83 · Horizontal Stabilizer, Spar/Rib
  > DURING THE INSPECTION OF THE HORIZONTAL STABILIZER REAR SPAR UPPER CAPS, REQUIRED BY THE AD 2007-10-04, DETECTED A CRACK OF (2) INCHES LONG AT STATION XH = 6.5. THE REPAIR IS IN PROCESS, DETAILED INFORMATION WILL BE SUBMITTED IN A SUPPLEMENT AS SOON AS ITS CO
- [SDR ASMF200704012](https://openairdocs.org/sdr/ASMF200704012.md): Engine · unknown · Apr 17, 2007 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)
  > AIRCRAFT REJECTED TAKEOFF DUE TO LT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE: LT ENGINE WITH EPR 1.40 AND RT ENGINE WITH EPR 1.86 AND T/O FLX TEMP 50. DURING MAINTENANCE CHECK, THE ACCELERATION CHAMBER AND MOISTURE TRAMP SERVICES WERE PERFORMED IAW MM 7
- [SDR ASMF200612003](https://openairdocs.org/sdr/ASMF200612003.md): Cadc · failed · Dec 11, 2006 · N583MD · Doug DC983 · Airspeed/Mach Indicator
  > AIRCRAFT REJECTED TAKEOFF AT 90 KNOTS DUE TO A 15 KTS OF DIFFERENCE BETWEEN SPEED INDICATORS. CADC AND RT AIR SPEED INDICATOR WERE REPLACED IAW MM 34-16-01 AND 34-13-01, TESTED CORRECT.
- [SDR ASMF200611008](https://openairdocs.org/sdr/ASMF200611008.md): Actuator · failed · Nov 18, 2006 · N583MD · Doug DC983 · Leading Edge Slat Actuator
  > CAPTAIN REPORTED THAT AFTER TAKEOFF AT GDL THE (AUTO SLATS FAIL) LIGHT TURNED ON IN LOW SPEED (150-230 KIAS) AND FLIGHT CONTROLS WITH VIBRATION. THE STALL COMPUTERS WERE TESTED AND SLATS ACTUATORS FAILED IN BOTH COMPUTERS. AIRCRAFT WAS SENT TO THE HANGAR AND
- [SDR ASMF200610012](https://openairdocs.org/sdr/ASMF200610012.md): Powerplant · power loss · Oct 28, 2006 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)
  > AIRCRAFT REJECTED TAKEOFF AT 40 KNOTS DUE TO THE LT ENGINE DID NOT ACCELERATE MORE THAN 1.2 EPR’S. AT PLATFORM, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. DURING OVERNIGHT CHECK, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00 AND 71-00-01,
- [SDR ASMF200607016](https://openairdocs.org/sdr/ASMF200607016.md): Unknown · unknown · Jul 22, 2006 · N583MD · Doug DC983 · Standard Practices/Structures
  > AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE STARTING SPEED AND F/D FLAGS WERE SHOWN IN ADI AND FLIGHT GUIDANCE COMPUTER WITHOUT INDICATION IN FMA NR 2. AC POWER SWITCH WAS RESET CORRECTING THE FAILURE, TESTED CORRECT IAW MM 24-20-00.
- [SDR ASMF200606015](https://openairdocs.org/sdr/ASMF200606015.md): Cowling · damaged · Jun 25, 2006 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, A LOSE OF MATERIAL IN THE LT ENGINE NOISE SUPPRESSOR WAS DETECTED. AN INSPECTION WAS PERFORMED AND DAMAGE WAS OUT OF LIMITS, THEREFORE, THE AIRCRAFT WAS SENT TO THE HANGAR AND THE LT ENGINE NOSE COWLING WAS REPLACED IAW MM 71-10-01, TESTE
- [SDR ASMF200606012](https://openairdocs.org/sdr/ASMF200606012.md): Annunciator · malfunctioned · Jun 20, 2006 · N583MD · Doug DC983 · Flight Management Computing Hardware System
  > AIRCRAFT RETURNED TO PLATFORM, FMA FAILURE WITH RT SPD FLAGS AND FD IN RT ADI WERE SHOWED. THE FLT GUIDE SYSTEM WAS RESEATED AND AUTO LAND IN BOTH SYSTEM WERE PERFORMED IAW MM 22-13-00, ALL CORRECT.
- [SDR ASMF200603007](https://openairdocs.org/sdr/ASMF200603007.md): Window · broken · Mar 16, 2006 · N583MD · Doug DC983 · Passenger Compartment Windows
  > CAPTAIN REPORTED THAT DURING FLIGHT AT 320 FEET, WITH 7.7 OF CABIN DIFFERENTIAL PRESSURE A STRONG NOISE WAS HEARD IN THE PASSENGERS CABIN DUE TO THE 32 WINDOW WAS BROKEN. THE WINDOW WAS REPLACED, TESTED CORRECT.
- [SDR ASMF200603003](https://openairdocs.org/sdr/ASMF200603003.md): Target · failed · Mar 8, 2006 · N583MD · Doug DC983 · Nose/Tail Landing Gear
  > CAPTAIN REPORTED THAT AFTER MAIN LANDING GEAR EXTENSION, THE GEAR DOOR OPEN LIGHT TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED BUT THE LIGHT CONTINUED ON, SO THE AIRCRAFT LANDED AT ONT WITH THE MAIN LANDING GEAR DOORS OPEN AND THE ALTERNATE LEVER PULLED. VISU
- [SDR ASMF200512008](https://openairdocs.org/sdr/ASMF200512008.md): Bungee Cylinder · leaking · Dec 8, 2005 · N583MD · Doug DC983 · Landing Gear Retraction/Extension System
  > DURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED A HYDRAULIC LIQUID LEAK IN THE RT MAIN LANDING GEAR. BUNGEE CYLINDER WAS REPLACED IAW MM 32-32-02, TESTED CORRECT.
- [SDR ASMF200508005](https://openairdocs.org/sdr/ASMF200508005.md): Csd · malfunctioned · Aug 10, 2005 · N583MD · Doug DC983 · AC Generation System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS CONSEQUENCE OF OVERTEMPERATURE ON LEFT CONSTANT SPEED DRIVE (CSD). LEFT CHIP DETECTORS WERE CHECKED, ALL CORRECT. CSD WAS DETECTED OVERFILLED. CSD WAS DRAINED UNTIL CORRECT LEVEL AND LEFT ENGINE RUN WAS CORRE
- [SDR ASMF200507019](https://openairdocs.org/sdr/ASMF200507019.md): Engine · failed · Jul 25, 2005 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING LEFT ENGINE STARTING AND SHUT OFF, VIBRATION WAS FELT IN THE HOLE AIRCRAFT. THE LEFT ENGINE VIBRATION ABSORBERS, BARS AND ACCESSORIES WERE INSPECTED, BEING ALL CORRECT. THE LEFT ENGINE WAS STARTED DETECTING VIBRATION. THE UVC WAS D
- [SDR ASMF200506022](https://openairdocs.org/sdr/ASMF200506022.md): Transmitter · inoperative · Jun 19, 2005 · N583MD · Doug DC983 · Hydraulic Pressure Sensor
  > CAPTAIN REPORTED RT HYDRAULIC BRAKE PRESS INDICATION SYSTEM INOPERATIVE. WIRING SYSTEM CHECK DETECTED ELECTRICAL LINE DAMAGED ON RT BRAKE PRESS TRANSMITTER CONNECTOR. ELECTRICAL LINE, RT BRAKE TRANSMITTER AND PRESS INDICATOR REPLACED IAW MM 32-42-00, OPS CH
- [SDR ASMF200506005](https://openairdocs.org/sdr/ASMF200506005.md): Computer · failed · Jun 3, 2005 · N583MD · Doug DC983 · Stall Warning System
  > AIRCRAFT RETURNED OF FLIGHT, AFTER ROTATION, THE DISAGREE IN SLAT PANEL, AUTO SLAT FAIL AND STALL INDICATION FAILURE IN ANNUNCIATOR PANEL LIGHTS COME ON. BOTH COMPUTERS WERE VERIFIED AND IN THE NR 1 APPEARED SIF LIGHT WITH FAILURE AND IN THE NR 2 AUTO SLAT LIG
- [SDR ASMF200505007](https://openairdocs.org/sdr/ASMF200505007.md): Connector · failed · May 5, 2005 · N583MD · Doug DC983 · Attitude Gyro and Indicating System
  > AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF VOR NR 2 WITH OSCILLATIONS OF 30 RADIALS AND RIGHT EHSI WITH OFF FLAG IN LEFT RMI. AIRCRAFT WAS SENT TO THE HANGAR AND RMI INDICATOR WIRING WAS CHECKED DETECTING THE LEFT RMI CONNECTOR FAILED, LINES 36, 37 AND 45. CONN
- [SDR ASMF200501008](https://openairdocs.org/sdr/ASMF200501008.md): Duct · damaged · Jan 15, 2005 · N583MD · Doug MD83 · Engine Cranking
  > DURING ENGINES STARTING, RT ENGINE DID NOT STARTED BECAUSE N1 WAS OUT OF SERVICE. DURING MAINTENANCE REVISION WAS DETECTED 8TH STAGE DUCT BROKEN. DUCT WAS REPLACED AND TESTS WERE PERFORMED IAW MM 71-00-01, ALL CORRECT.
- [SDR ASMF200410015](https://openairdocs.org/sdr/ASMF200410015.md): Shutoff Valve · failed · Oct 19, 2004 · N583MD · Doug DC983 · Hydraulic System, Main
  > CAPTAIN REPORTED LOSS OF HYDRAULIC FLUID OF THE RT SYSTEM AND LANDING GEAR DOORS DID NOT OPEN IN A NORMAL WAY, OPENING THEM MANUALLY. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, RUDDER SHUTOFF VALVE WAS REPLACED IAW MM 27-20-09 AND MAIN LAND
- [SDR ASMF200406032](https://openairdocs.org/sdr/ASMF200406032.md): Cadc · failed · Jun 27, 2004 · N583MD · Doug DC983 · Pitot/Static System
  > CAPTAIN REPORTED THAT DURING CRUISE AT 35,000 FEET, VERTICAL VELOCIMETER BAR FD TRI WAS OUT OF SERVICE AND CADC ABNORMAL PROCEDURE WAS PERFORMED. DURING TRANSIT CHECK AT TIJ, PITOTS AND STATIC PORTS WERE CHECKED BY OVERHEAT AND NO DAMAGE WAS DETECTED. PITOTS A
- [SDR ASMF200406030](https://openairdocs.org/sdr/ASMF200406030.md): Selector Switch · failed · Jun 26, 2004 · N583MD · Doug DC983 · AC Generator-Alternator
  > AIRCRAFT RETURNED TO PLATFORM, APU OUT OF SERVICE AND ENGINE GENERATORS WITHOUT INDICATION OF VOLTAGE AND FREQUENCY. CIRCUIT BREAKERS B1-204, B1-205 AND B1-206 WERE CHECKED AND SWITCH SELECTOR S1-99 WAS REPLACED IAW MM 24-21-01, TEST CORRECT.
- [SDR ASMF200403011](https://openairdocs.org/sdr/ASMF200403011.md): Pressure Switch · malfunctioned · Mar 20, 2004 · N583MD · Doug DC983 · Engine Oil Pressure
  > DURING TRANSIT CHECK THE LEFT OIL LOW PRESSURE LIGHT TURNED ON. THE SWITCH WAS DEFERRED IAW MEL 79-2. DURING OVERNIGHT SERVICE THE LOW PRESSURE SWITCH WAS REPLACED IAW MM 79-34-01, TEST CORRECT.
- [SDR MEX2003440](https://openairdocs.org/sdr/MEX2003440.md): Pump · failed · Sep 21, 2003 · N583MD · Doug DC983 · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE AT 33,000 FT, THE RUDDER TRAVEL UNRESTRICTED LIGHT TURNS 'ON'. AFTER LANDING THE HYDRAULIC PRESSURE INDICATES 2500 PSI. THE ELECTRIC MOTOR DRIVEN PUMP WAS REPLACED IAW MM 29-10-06, THE PRESSURE TRANSMITTER WAS REPLACED IAW MM 29-30-02 AND THROW
- [SDR MEX2003271](https://openairdocs.org/sdr/MEX2003271.md): Suppressor · damaged · Jul 7, 2003 · N583MD · Doug DC983 · Engine Noise Suppressor
  > AIRCRAFT AIR TURN BACK DUE TO ENGINE 2 FAILURE DURING INITIAL CLIMB, REACHING 660 DEGREE C OF EGT EMERGENCY PROCEDURE WAS PERFORMED. DURING REVISION THE EXHAUST CONE, SUPPRESSOR AND TURBINE FAN WITH DAMAGE. ENGINE NR 2 WAS REPLACED IAW MM, OPERATIONAL TEST
- [SDR MEX2003285](https://openairdocs.org/sdr/MEX2003285.md): Amplifier · faulty · Jul 3, 2003 · N583MD · Doug DC983 · Fire Detection
  > DURING TRANSIT CHECK DETECTED THAT DURING TEST ENGINE FIRE ALARM SYSTEM NR 2 NOT CANCELL AURA WARNING. DURING REVISION BREAKER AND AMPLIFIER A2-6 WERE WITH DAMAGES. THE FIRE ENGINE NR 2 AMPLIFIER WAS SWAPPED WITH APU AMPLIFIER IAW MM 26-10-01, ALL TESTS CORR
- [SDR MEX2003263](https://openairdocs.org/sdr/MEX2003263.md): Proximity Switch · failed · Apr 7, 2003 · N583MD · Doug DC983 · Landing Gear Position and Warning
  > AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT DURING FINAL APPROACH THE NOSE LANDING GEAR LIGHT TURNED RED AND NOSE LANDING GEAR ALARM CAME ON. AFTER MISSED APPROACH AND A NOSE LANDING GEAR CYCLE, THE GREEN LIGHTS COME ON. AIRCRAFT WAS SENT TO THE HANGAR FOR ITS
- [SDR MEX2002307](https://openairdocs.org/sdr/MEX2002307.md): Pump · failed · Sep 22, 2002 · N583MD · Doug DC983 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT RETURNED FROM FLIGHT AS CONSEQUENCE OF THE LIGHT (RT HYD PRESS LOW) AT PLATFORM, TECH SUPPLIED 14 QTS OF HYDRAULIC FLUID. RIGHT ENGINE WAS STARTED BUT THE PRESSURE INDICATION OF MAIN PUMP WAS NOT SHOWN. SUCH PUMP WAS REPLACED AND DURING THE TESTS A
- [SDR MEX2002305](https://openairdocs.org/sdr/MEX2002305.md): Switch · failed · Sep 18, 2002 · N583MD · Doug DC983 · Cabin Pressure Control System
  > AIRCRAFT RETURNED OF FLIGHT AS CONSEQUENCE OF PRESSURIZATION FAILURE. AT PLATFORM TECH DETECTED THAT THE LIGHT (FLOW) TURNED ON IN PRESSURIZATION SELECTOR AND TRANSFER LOCK OUT. WITH ENGINES OPERATING, THERE WAS PERFORMED AT BITE AND CONTROLLER 2 FAILED, IT
- [SDR 971355015](https://openairdocs.org/sdr/971355015.md): Skin · corroded · Aug 28, 1997 · N583MD · Doug DC983 · Wing, Plate/Skin
  > PREVIOUSLY EXISTING BLENDOUT REPAIRS OF WING LOWER SKINS REQUIRE MAPPING AND DISPOSITION. MAPPED BLENDOUTS AND REPORTED TO DACO -- MOST ACCEPTABLE AS IS, FOUR AREAS REPAIRED BY EXTERNAL DOUBLER PER SRM 57-03 FIG 24A, ONE AREA REPAIRED BY REMOVAL OF DAMAGE AND
- [SDR IH971355014](https://openairdocs.org/sdr/IH971355014.md): Dome · cracked · Aug 12, 1997 · N583MD · Turbine Engine Air Inlet Section
  > NR 2 ENGINE FRONT BULLET IS CRACKED AROUND RIVETS, 2 CRACKS WERE FOUND IN THE 5930646-25 DOME SKIN. CRACKS WERE COMMON TO THIS SKIN ONLY. THE INNER DETAILS OF THE 5930646 DOME ASSEMBLY WERE REMOVED, CRACKS STOP DRILLED AND THEN WELDED PER DPS 10.301. SKIN A

Next page: https://openairdocs.org/deregistered/N583MD-2011-10-28/reports.md?page=2

## 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 = 'N583MD' AND deregistration_id = 'N583MD-2011-10-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N583MD-2011-10-28/reports

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