# N190AN: Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2012-10-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 24, 2012 - Exported to: Spain - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - 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: 53190 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 22, 2000 - Certificate issued: March 30, 2012 - Last registry action: March 30, 2012 - Mode S code: A16838 - Owner when cancelled: [Awms I](https://openairdocs.org/faa-owner/AWMS%20I) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7592° N, 73.9807° W: Placed by OpenAirDocs at the center of ZIP code 10020, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N190AN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=190AN - Page: https://openairdocs.org/deregistered/N190AN-2012-10-24 From the FAA registry file of October 29, 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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ANCF200600016](https://openairdocs.org/sdr/ANCF200600016), Apr 25, 2006: TEST UNIT. DEFECTIVE. AFTER TAKEOFF THE SLAT DISAGREE LIGHT CAME ON, CHECK LIST WAS PERFORMED NOT SUCCESSFUL, RETURNED TO BOG (2 EVENTS). FIRST EVENT - ISOLATION PROCEDURE WAS ACCOMP - [SDR ANCF200400053](https://openairdocs.org/sdr/ANCF200400053), Jul 15, 2005: ENGINE. LEAKING. RIGHT ENGINE OIL QUANTITY DECREASED SLOWLY FROM 13 QTS TO 2 QTS IN FLT ( OIL PRESS AND TEMPERATURE WERE NORMAL), ENGINE SHUTDOWN 4 MIN BEFORE LANDING AS OIL REA - [SDR 2005FA0000978](https://openairdocs.org/sdr/2005FA0000978), Jun 25, 2005: NOSE COWL. DEBONDED. SKIN PANELS HAVE DELAMINATED AT FWD EDGE, COMMON TO LIP SKIN. EVIDENCE OF HIGH TEMPERATURE AS FIBERGLASS APPEARS DARKENED AND IS BRITTLE. OUTER SKINS OF BARREL - [SDR ANCF200400046](https://openairdocs.org/sdr/ANCF200400046), Apr 5, 2005: BLADE. DAMAGED. DURING OVERNIGHT SERVICE WAS ACCOMPLISHED EO 83-72-007 BORESCOPE INSPECTION FIRST AND SECOND STAGE TURBINE BLADES AND FOUND ON RT ENGINE TWO BLADES WITH CRACKS - [SDR ANCF200400045](https://openairdocs.org/sdr/ANCF200400045), Apr 5, 2005: BLADE. CRACKED. DURING OVERNIGHT SERVICE WAS ACCOMPLISHED EO 83-72-007 BORESCOPE INSPECTION FIRST AND SECOND STAGE TURBINE BLADES AND FOUND ON LT ENGINE ONE BLADE WITH CRACK ON - [SDR ANCF200400037](https://openairdocs.org/sdr/ANCF200400037), Dec 10, 2004: ENGINE. MALFUNCTIONED. DURING CLIMB AT 15000 FEET, SEVERE DAMAGE OCCURRED IN THE LT ENGINE, EMERGENCY PROCEDURE WERE PERFORMED. LT ENGINE WAS CHANGED IAW AMM 71-00-00 PAGE 401. TEST W - [SDR ANCF200400029](https://openairdocs.org/sdr/ANCF200400029), Aug 28, 2004: VALVE. FAILED. DURING INITIAL CLIMB RT ENGINE LOOP-A ILLUMINATED INTERMITTENTLY AT FIRST, THEN RT ENG FIRE HANDLE CAME (ON) WITH THE AURAL ALARM .WITH INCREASING OIL AND FUEL - [SDR ANCF200400023](https://openairdocs.org/sdr/ANCF200400023), Aug 2, 2004: ENGINE. BIRD INGESTION. A BIG BIRD WAS INGESTED THE TAKE OFF ROLL IN THE RT ENG TAKE OFF WAS CONTINUED IT OPERATED, AT ROTATION RT ENG WAS REDUCED AT 800 FT TO IDLE AIR RETURN WAS MADE - [SDR ANCF200400015](https://openairdocs.org/sdr/ANCF200400015), Jun 30, 2004: TIRE. FAILED. DURING T/O, STRONG VIBE FELT ON MLG WITH SUDDEN LOSS OF PWR ON LT ENG. PARAMETER DE & INCREASED FROM 1.3-1.8 EPR CONSTANT UNTIL 10000 FT, LT ENG STABILIZED. RET - [SDR ANCF200300024](https://openairdocs.org/sdr/ANCF200300024), Sep 4, 2003: CONTROLLER. MALFUNCTIONED. AFTER T/O WITH PACKS ON, THE FLOW LIGHT WAS PRESENTED,THE LEFT PACK DROPPED TO ZERO AND THE RIGH PACK WAS SHOWING 20 PSI. THE LEFT PACK WAS NOT POSSIBLE TO REST - [SDR ANCF200300023](https://openairdocs.org/sdr/ANCF200300023), Sep 4, 2003: STRUT. MALFUNCTIONED. DURING TAKE OFF NOSE STRUT DIDN´T WORK NORMAL, AFTER TAKE OFF WHEN GEAR HANDLE WAS SWAS UP, NOSE GEAR DIDN´T LOCK AND A STRONG NOISE WAS FELT. THE SEALS WERE RE - [SDR ANCF200300021](https://openairdocs.org/sdr/ANCF200300021), Aug 14, 2003: CONTROLLER. MALFUNCTIONED. T/O WAS PERFORMED ACCORDING TO OPTION NR 1 OF MEL 21-1 (RT PACK INOPERATIVE) AT 100FT WE SWITCHED LT A/C SYSTEM SWITCH TO AUTO & IT DIDN´T PRESSURIZE AIRCRAFT, - [SDR ANCF200300005](https://openairdocs.org/sdr/ANCF200300005), Feb 3, 2003: NUT. UNDERTORQUED. THERE WAS A VERY STRONG VIBRATION OF THE NOSE WHEELS DURING TAKE OFF ROLL. TAKE OFF WAS ABOTED BELOW 60 KTS. WAS VERIFCATED TORQUE IN NUT STRUT IAW AMM 32-21-02 - [SDR ANCF200200025](https://openairdocs.org/sdr/ANCF200200025), Nov 13, 2002: SWITCH. MALFUNCTIONED. WITH AUTO SPOILERS DISARM, AUTO BRAKES SELECTOR IN OFF AND AUTO BRAKES SWITCH IN DISARM, WHEN THROTTLES WERE ADVANCED FOR TAKE OFF, "AUTO BRAKES TAKE OFF WARNIN - [SDR ANCF200200021](https://openairdocs.org/sdr/ANCF200200021), Oct 10, 2002: ACM. DAMAGED. FIVE MINUTES AFTER TAKE OFF IT WAS FELT SMOKE SMELL FROM AIR CONDITIONING TUBES. AIRCRAFT RETURNED BACK TO BOGOTA. FLIGHT PERFORMED ON EI-CCC. AIRCRAFT WAS LEFT - [SDR ANCF200200014](https://openairdocs.org/sdr/ANCF200200014), Jul 13, 2002: VALVE. FAILED. AFTER T/O THE NLG DID NOT GO UP. PROCEDURES CHECKLIST WERE ACCOMPLISHED. AIRCRAFT WAS TURNED BACK TO BOGOTA. AIR VALVE WAS REPLACED. WAS ACCOMPLISHED SERVICE ON - [SDR ANCF200200012](https://openairdocs.org/sdr/ANCF200200012), Jun 27, 2002: PROXIMITY SENSOR. MALFUNCTIONED. DURING TAKE OFF ROLL, GEAR DOOR OPEN ANNUNTIATION CAME ON. TAKE OFF WAS ABORTED. WAS ADJUSTED AND CLEANED DOOR PROXIMITY SENSOR IAW AMM 32-60-00. WAS PERFORMED - [SDR ANCF200200001](https://openairdocs.org/sdr/ANCF200200001), Jan 11, 2002: CSD. MALFUNCTIONED. DURING CLIMB LT CSD OIL OUTLET TEMP.REACHED RED DANGER ZONE AND CONTINUED INCREASING. CSD WAS DISCONNECTED. APU WAS STARTED AT FL.260 BUT AT FL.305 APU HAD AUTO - [SDR ANCF200100009](https://openairdocs.org/sdr/ANCF200100009), May 16, 2001: AUDIO PANEL. INOPERATIVE. LT COMMUNICATIONS WAS COMPLETELY INOPERATIVE. AIR TURNBACK PROCEDURE WAS ACCOMPLISHED. LT AUDIO BOX WAS CHANGED IAW AMM 23-50-02 P 201 AND FLIGHT INTERPHONE CB - [SDR ANCF0329351](https://openairdocs.org/sdr/ANCF0329351), Feb 20, 2001: LINE. DISCONNECTED. DURING CRUISE LT ENGINE N2 STARTED TO DECREASE UNTIL REACHING 36 PERCENT (OSCILLATING BETWEEN 32 AND 40 PERCENT), THERE IS MORE THAN ONE KNOB SPLIT BETWEEN ENGI --- 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.