# N505MD: Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-09-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 25, 2013 - Status when cancelled: N-number assigned, not yet registered - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49149 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 21, 1995 - Last registry action: September 25, 2013 - Mode S code: A64D9A - The mark today: https://openairdocs.org/aircraft/N505MD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=505MD - Page: https://openairdocs.org/deregistered/N505MD-2013-09-25 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200505009](https://openairdocs.org/sdr/ASMF200505009), May 6, 2005: COMPUTER. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING TO AUTO SLAT FAIL AND AUTO SLAT DISAGREE LIGHTS COME ON. SYSTEM WAS RESET AND TESTED BUT FAILURE - [SDR ASMF200505001](https://openairdocs.org/sdr/ASMF200505001), May 2, 2005: COOLER. FAILED. DURING TRANSIT CHECK, IT WAS DETECTED OIL LEAK IN THE LEFT ENGINE FUEL-OIL COOLER AND THE OIL TANK OVERFILLED WITH FUEL SMELT. FUEL-OIL COOLER OF THE LEFT ENGIN - [SDR ASMF200504014](https://openairdocs.org/sdr/ASMF200504014), Apr 16, 2005: LINE. DAMAGED. CAPTAIN REPORTED THAT DURING FLIGHT LOT HYDRAULIC LIQUID IN THE LEFT SYSTEM WITH HYDRAULIC PRESSURE CORRECT. DURING REVISION WAS DETECTED THE HYDRAULIC TANK LEF - [SDR ASMF200409007](https://openairdocs.org/sdr/ASMF200409007), Sep 19, 2004: LINK. JAMMED. CAPTAIN REPORTED THAT AFTER TAKEOFF, NOSE LANDING GEAR NOT RETRACTED, LIGHT ON, ABNORMAL PROCEDURE PERFORMED. AIRCRAFT SENT TO THE HANGAR AND NOSE LANDING GEAR - [SDR ASMF200408013](https://openairdocs.org/sdr/ASMF200408013), Aug 14, 2004: COMPENSATOR. FAILED. CAPTAIN REPORTED DIFFERENCE BETWEEN LT AND RT FUEL INDICATORS. DURING COMPENSATORS TEST WAS DETECTED THAT THE RIGHT TANK HAD 2500 LBS, LT TANK HAD 2600 LBS AND - [SDR ASMF200408011](https://openairdocs.org/sdr/ASMF200408011), Aug 12, 2004: REGULATOR. OPEN. CAPTAIN REPORTED THAT AT FL 330 FLOWS LIGHT TURNED ON DUE TO PRESSURIZATION FAILURE PERFORMING AN ABNORMAL AND EMERGENCY PROCEDURE. ANTI-ICE WAS APPLIED TO ENGI - [SDR ASMF200407030](https://openairdocs.org/sdr/ASMF200407030), Jul 25, 2004: SLIDE. DISLODGED. DURING TRANSIT CHECK, CAPTAIN REPORTED THAT FOOD SERVICES COMPANY PERSONNEL FELL DOWN THROUGH LT SERVICE DOOR SLIDE. LT SERVICE DOOR SLIDE WAS REINSTALLED IAW M - [SDR ASMF200407002](https://openairdocs.org/sdr/ASMF200407002), Jul 1, 2004: ACTUATOR. DAMAGED. DURING OVERNIGHT SERVICE, GROUND SPOILER WAS DETECTED OUT OF SERVICE, AUTO SPOILER ACTUATOR WAS REPLACED AND SPOILER TRIMMING WAS PERFORMED AND TESTED AND FAILU - [SDR ASMF200406031](https://openairdocs.org/sdr/ASMF200406031), Jun 27, 2004: LEVER. DEFECTIVE. CAPTAIN REPORTED, SPEED BRAKES AND GROUND SPOILERS SYSTEM OUT OF SERVICE DURING FLIGHT. SYSTEM WAS CHECKED AND LEVER WAS DETECTED VERY HARD AND OCCASIONALLY JAM - [SDR ASMF200406012](https://openairdocs.org/sdr/ASMF200406012), Jun 13, 2004: DOOR. UNLOCKED. AIRCRAFT RETURNED, ELECTRIC/ELECTRONIC DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION WAS DETECTED THAT ELECTRIC/ELECTRONIC DOOR WAS NOT LOCKED. DOOR WAS COR - [SDR ASMF200406006](https://openairdocs.org/sdr/ASMF200406006), Jun 7, 2004: COMPUTER. FAILED. AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN LT FLIGHT GUIDANCE SYSTEM INDICATION. SYSTEM WAS REACTIVATED AND ELECTRICAL BUSS TURNED OFF, AUTO TEST I - [SDR ASMF200405018](https://openairdocs.org/sdr/ASMF200405018), May 15, 2004: BUSS. LOOSE. AIRCRAFT RETURNED TO PLATFORM BECAUSE BUSS WERE LOOSEN. GCU´S WERE CHECKED, ALL CORRECT. FLIGHT DIRECTOR BUSS WAS CHECKED AND IT WAS DETECTED WITH FAIL. DFGC NR - [SDR ASMF200403019](https://openairdocs.org/sdr/ASMF200403019), Mar 30, 2004: SKIN. DENTED. CAPTAIN REQUESTED A CHECK FOR DENTS IN RIGHT SIDE OF FUSELAGE NEAR TO THE STATIC PORTS. AIRCRAFT WAS CHECKED BY DENTS IAW SRM 53-04 AND DENTS WERE WITHIN LIMITS - [SDR MEX2004066](https://openairdocs.org/sdr/MEX2004066), Feb 17, 2004: PUMP. FAILED. FLT 351 - MEX-ZIH - AIRCRAFT RETURNED TO PLATFORM, DUE TO LOSS OF HYDRAULIC PRESSURE. CAPTAIN REPORTED THAT THE LEFT HYDRAULIC SYSTEM WITH 1100 PSI ON HIGH, LOW - [SDR MEX2004060](https://openairdocs.org/sdr/MEX2004060), Feb 15, 2004: HYDRAULIC SYSTEM. LEAKING. DURING TRANSIT CHECK, THE LEFT HYDRAULIC SYSTEM WAS EMPTY. DURING REVISION AT THE TAIL AREA IN THE VENTRAL STAIR WAS DETECTED A HYDRAULIC LIQUID LEAK. THE AREA - [SDR MEX2004057](https://openairdocs.org/sdr/MEX2004057), Feb 14, 2004: SENSOR. FAILED. FLT 256 - MEX-HMO - DURNIG APPROACH THE RED MAIN LANDING GEAR LIGHT TURNED ON. DURING REVISION IN HANGAR THE MLG SENSOR WAS CALIBRATED IAW MM 32-60-05 AND CHAFI - [SDR MEX2003549](https://openairdocs.org/sdr/MEX2003549), Dec 11, 2003: ADAPTER. LEAKING. THE DISPENSER FUEL NOZZLE WAS REMOVED INADEQUATELY AFTER THE FUEL REFILLING SERVICE, THE ADAPTER CHECK VALVE SEAL WAS REMOVED AND A LITTLE FUEL LEAKAGE APPEARED - [SDR MEX2003537](https://openairdocs.org/sdr/MEX2003537), Nov 27, 2003: SENSOR. DIRTY. FLIGHT RETURNED DUE TO THE 'E/E DOOR OPEN' LIGHT TURNED ON AFTER 15 MINUTES. DURING REVISION AT MLM STATION THE DOOR WAS FOUND CLOSED. THE MECHANISM, DOOR AND T - [SDR MEX2003442](https://openairdocs.org/sdr/MEX2003442), Sep 22, 2003: COOLING TURBINE. FAILED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, AT FL290 LIGHT FLOW CAME ON AND THE CABIN PRESSURE STARTED TO CLIMB OF 1500 FT/MIN, UNABLE TO CONTROL IT IN MANUAL AN - [SDR MEX2003367](https://openairdocs.org/sdr/MEX2003367), Aug 14, 2003: SKIN. DAMAGED. DURING OVERNIGHT CHECK WAS DETECTED LIGHTNING IMPACT AT FUSELAGE LEFT SIDE. LIGHTNING INSPECTION WAS DETECTING DAMAGES AT STATION Y332 AND LONGERON 15 WITH EIGH - [SDR MEX2003270](https://openairdocs.org/sdr/MEX2003270), Jul 7, 2003: CONTROL UNIT. FAILED. DURING PREFLIGHT TRANSIT CHECK WAS DETECTED THE ENGINE FIRE ALARM SYSTEM DID NOT CANCEL AURAL WARNING. DURING REVISION RIGHT ENGINE LOOP B, BREAKER B-1 AND AMPL - [SDR MEX2003190](https://openairdocs.org/sdr/MEX2003190), May 23, 2003: VALVE. MALFUNCTIONED. HMO - FLT 104 - GDL - DURING DESCENT, INDICATION STARTED TO CLIMB AND LOW FLOW LIGHT TURNED ON WITH PRESURIZATION VALVE CLOSED, ENGINE ACCELERATED TO 1.5 EPR AN - [SDR MEX2003060](https://openairdocs.org/sdr/MEX2003060), Mar 4, 2003: FUEL CONTROL. FAILED. FLT 189 - TIJ-MEX - AIRCRAFT RETURNED TO PLATFORM, OSCILLATION IN ENGINE PARAMETERS. OIL FILTER, OIL MAIN FILTER AND CHIP DETECTOR WERE VERIFIED. N2 WAS ADJUSTE - [SDR MEX2003049](https://openairdocs.org/sdr/MEX2003049), Feb 28, 2003: RECORDER. INOPERATIVE. AIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN DISCONTINUE ENGINE NR 1 STARTING, FOR FIRE DURING STARTING OF ENGINE NR 2, WITH INDICATION AT CABIN. ENGINES WERE I - [SDR MEX2002359](https://openairdocs.org/sdr/MEX2002359), Nov 12, 2002: PRESSURE SWITCH. FAILED. FLT 210 - MEX-CUU - AIRCRAFT ABORTED TAKEOFF DUE TO BOTH AIR CONDITIONING PACKAGES SHUTOFF AND FLOW LIGHT TURN ON AT 132 KTS. AIRCRAFT WAS SENT TO THE HANGAR AN - [SDR MEX2002248](https://openairdocs.org/sdr/MEX2002248), Jul 30, 2002: LINE. DAMAGED. ON DEPARTURE, CAPTAIN REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN. THE HYDRAULIC SYSTEM WAS VERIFIED TO BE LEAKING AND THE APU WAS SHUTDOWN DUE TO HYD - [SDR MEX2002218](https://openairdocs.org/sdr/MEX2002218), Jul 14, 2002: VALVE. FAILED. FLT 132 - MEX-BJX - WHEN THE ANTI-ICE SYSTEM IS ON, THE LIGHT CABIN FLOW WAS TURNED ON. AT RON MEX 14/15, IT WAS PERFORMED THE ANTI-ICE TEST IN MODE 1 AND 2. TH - [SDR MEX2002168](https://openairdocs.org/sdr/MEX2002168), May 21, 2002: CONTROL VALVE. FAILED. FLT 315 - MEX-ACA - CAPTAIN REPORT THAT DURING DESCENT WITH INDICATIONS OF 22 AND 19 IN BOTH AIR CONDITIONING PACKAGES AND WITH ALL VALVES CLOSED THE FLOW LIGHT - [SDR ASM2002F00000](https://openairdocs.org/sdr/ASM2002F00000), May 18, 2002: COMPUTER. FAILED. AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN ENGINE NUMBER TWO AND THE THROAT EPR NR 2 WAS OUT OF SERVICE. THE EPR TX ASSY NUMBER TWO WAS - [SDR MEX2002263](https://openairdocs.org/sdr/MEX2002263), Dec 8, 2001: WIRE. BROKEN. DURING TAXI CAPTAIN INFORMED THAT THE LIGHT OF RUDDER TRAVEL UNRESTRICTED DID NOT TURN ON. PROXIMITY SWITCH WAS VERIFIED AND FOUND A FAILURE IN THE CARD 706. PR ## Other aircraft with N505MD - [Registered now](https://openairdocs.org/aircraft/N505MD): Bell Textron Canada 505, S/N 65405, built 2022 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.