# Service difficulty reports: N190AN, cancelled Oct 24, 2012

A list on [N190AN, cancelled Oct 24, 2012](https://openairdocs.org/deregistered/N190AN-2012-10-24.md).

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

- [SDR ANCF200600016](https://openairdocs.org/sdr/ANCF200600016.md): Test Unit · defective · Apr 25, 2006 · N190AN · Doug DC983 · Leading Edge Slat Control System
  > AFTER TAKEOFF THE SLAT DISAGREE LIGHT CAME ON, CHECK LIST WAS PERFORMED NOT SUCCESSFUL, RETURNED TO BOG (2 EVENTS). FIRST EVENT - ISOLATION PROCEDURE WAS ACCOMPLISHED POSITION OF SENSORS WERE TESTED SATISFACTORY AS PER AMM27-80-00 PAGE 106 TO 106. SECOND EVE
- [SDR ANCF200400053](https://openairdocs.org/sdr/ANCF200400053.md): Engine · leaking · Jul 15, 2005 · N190AN · Doug MD83 · Turbine Engine Oil System
  > 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 REACHED 2 QTS & OIL TEMP STARTED TO INCREASED. ENGINE INITIALLY OPERATED IN IDLE THRUST FOR ABOUT 15 M
- [SDR 2005FA0000978](https://openairdocs.org/sdr/2005FA0000978.md): Nose Cowl · debonded · Jun 25, 2005 · N190AN · Doug DC983 · Engine Air Intake System
  > 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 ARE DEBONDED AND DISCOLORED BY HIGH TEMPERATURE. PROBABLE CAUSE: ANTI-ICE LEFT OPERATING FOR LON
- [SDR ANCF200400046](https://openairdocs.org/sdr/ANCF200400046.md): Blade · damaged · Apr 5, 2005 · N190AN · Doug DC983 · Engine (Turbine/Turboprop)
  > 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 ON TRAILING EDGE CONCAVE SIDE OF FIRST STAGE TURBINE. THE ENGINE HAS BEEN REMOVED IAW AMM 72-00-00,
- [SDR ANCF200400045](https://openairdocs.org/sdr/ANCF200400045.md): Blade · cracked · Apr 5, 2005 · N190AN · Doug DC983 · Turbine Engine Compressor Section
  > 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 TRAILING EDGE CONCAVE SIDE OF FIRST STAGE TURBINE. THE ENGINE HAS BEEN REMOVED IAW AMM 72-00-00, 7
- [SDR ANCF200400037](https://openairdocs.org/sdr/ANCF200400037.md): Engine · malfunctioned · Dec 10, 2004 · N190AN · Doug DC983 · Engine (Turbine/Turboprop)
  > 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 WITH ENGINE RUN UP WERE PERFORMED IAW AMM 71-00-00 PAGE BLOCK 501 WITH SATISFACTORY RESULTS. BOROSC
- [SDR ANCF200400029](https://openairdocs.org/sdr/ANCF200400029.md): Valve · failed · Aug 28, 2004 · N190AN · Doug MD83 · Ice/Rain Protection System
  > 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 TEMPERATURE WITH EOAP ANNUNCIATION OF RT ENG VALVE AND RT ANTI-ICE (ON). PROCEDURE WAS ACCOMPLISH.
- [SDR ANCF200400023](https://openairdocs.org/sdr/ANCF200400023.md): Engine · bird ingestion · Aug 2, 2004 · N190AN · Doug MD83 · Engine (Turbine/Turboprop)
  > 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 AFTER THE SURGE CHECKLIST WAS ACCOMPLISHED REDUCED TAKEOFF FLEX WAS 1.84 AFTER IMPACT IT WENT DOWN
- [SDR ANCF200400015](https://openairdocs.org/sdr/ANCF200400015.md): Tire · failed · Jun 30, 2004 · N190AN · Doug DC983 · Tire
  > 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. RETURNED TO DEPART. NORM LANDING. LT MLG RED LIGHT CAME ON CONSTANT. LT MLG IB WHEEL, TREAD SEPARATIO
- [SDR ANCF200300024](https://openairdocs.org/sdr/ANCF200300024.md): Controller · malfunctioned · Sep 4, 2003 · N190AN · Doug DC983 · Cabin Pressure Controller
  > 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 RESTORE SO WE PROCEED TO PRESSURIZE MANUALLY,WHICH WAS ALSO IMPOSSIBLE.ON FINAL THE LT PACK WAS RESTORED
- [SDR ANCF200300023](https://openairdocs.org/sdr/ANCF200300023.md): Strut · malfunctioned · Sep 4, 2003 · N190AN · Doug DC983 · Nose/Tail Landing Gear
  > 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 REPLACED ON NOSE GEAR STRUT. SERVICE OLEO NEUMATIC WAS ACCOMPLISHED IAW AMM 32-21-02 PAG 801 AND AM
- [SDR ANCF200300021](https://openairdocs.org/sdr/ANCF200300021.md): Controller · malfunctioned · Aug 14, 2003 · N190AN · Doug DC983 · Cabin Pressure Controller
  > 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, SUPPLY PRESSURE DROPS TO ZERO CHECK LIST WAS PERFORMED & WAS UNSUCCESFULL THE WE SWITCHED THE PRESSU
- [SDR ANCF200300005](https://openairdocs.org/sdr/ANCF200300005.md): Nut · undertorqued · Feb 3, 2003 · N190AN · Doug MD83 · Nose/Tail Landing Gear
  > 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 PAG 404 WAS ADJUSTED DEFLECTOR IAW AMM 32-20-02 PAG 202 AND NOSE WHEELS WERE REPLACED IAW AMM 32-
- [SDR ANCF200200025](https://openairdocs.org/sdr/ANCF200200025.md): Switch · malfunctioned · Nov 13, 2002 · N190AN · Doug MD83 · Drag Control System
  > 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 WARNING" CONFIGURATION CAME ON. TAKE OFF WAS ABORTED. REJECTED TAKE OFF SWITCHES WERE ADJUSTED PROPERLY I
- [SDR ANCF200200021](https://openairdocs.org/sdr/ANCF200200021.md): Acm · damaged · Oct 10, 2002 · N190AN · Doug MD83 · Cabin Cooling System
  > 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 ON GROUND FOR WORKING ON IT AT NIGHT. THE RIGHT PACK AIR CYCLE MACHINE WAS FOUND BINDING. THE AI
- [SDR ANCF200200014](https://openairdocs.org/sdr/ANCF200200014.md): Valve · failed · Jul 13, 2002 · N190AN · Doug MD83 · Landing Gear Retraction/Extension System
  > 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 SHOCKSTRUT AND PERFORMED RETRACTION TEST IAW AMM 32-30-00 PAG 1. RESULTS SATISFACTORY.
- [SDR ANCF200200012](https://openairdocs.org/sdr/ANCF200200012.md): Proximity Sensor · malfunctioned · Jun 27, 2002 · N190AN · Doug MD83 · Landing Gear Position and Warning
  > 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 BITE ON PSEU IAW AMM 32-60-04 PARAGRAPH 1C, PAGE 201. RESULTS SATISFACTORY.
- [SDR ANCF200200001](https://openairdocs.org/sdr/ANCF200200001.md): Csd · malfunctioned · Jan 11, 2002 · N190AN · Doug DC983 · Alternator-Generator Drive
  > 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 SHUT DOWN. DESCENT WAS DOWN TO FL.290 WE TRIED TO START APU AGAIN BUT START WAS UNSUCCESSFUL. CREW
- [SDR ANCF200100009](https://openairdocs.org/sdr/ANCF200100009.md): Audio Panel · inoperative · May 16, 2001 · N190AN · Doug DC983 · Communications System
  > 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 A-10 WAS RESEATED. SYSTEM OPERATION WAS CHECKED IAW AMM 23-00-00 PG 1. CHECKED OK.
- [SDR ANCF0329351](https://openairdocs.org/sdr/ANCF0329351.md): Line · disconnected · Feb 20, 2001 · N190AN · Doug DC983 · Engine RPM Indicating System
  > 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 ENGINES TO KEEP SAME EPR. FLIGHT DIVERTED TO PTY. MOISTURE TRAP WAS CHECK FOR CONDITION AND BURNER PRE

## 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 = 'N190AN' AND deregistration_id = 'N190AN-2012-10-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N190AN-2012-10-24/reports

---
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.