# Service difficulty reports: N632CT, cancelled Oct 6, 2017

A list on [N632CT, cancelled Oct 6, 2017](https://openairdocs.org/deregistered/N632CT-2017-10-06.md).

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

- [SDR ANCF2009061800050](https://openairdocs.org/sdr/ANCF2009061800050.md): Controller · malfunctioned · Jun 18, 2009 · N632CT · Doug MD83 · Compressor Bleed Valve
  > THRUST SET FOR TAKEOFF, LT AND RT ENGINE EPR 2.08 LT ENG N1 98 PERCENT RT ENG N1 98.7 PERCENT, LT AND RT ENGINE EGT WITHIN LIMITS. ABOUT 100 KTS A STRONG DECELERATION WAS FELT, RT ENGINE EPR DROPPED TO 1.78, AFT CREW REPORTED A LOUD BANG FROM RT ENGINE. AMM
- [SDR ANCF200700030](https://openairdocs.org/sdr/ANCF200700030.md): Warning System · false activation · Dec 4, 2007 · N632CT · Doug MD83 · Central Warning
  > DURING ROLL T/O FLAPS CONFIGURATION ALARM SOUNDS WITH THE FLAPS T/O SELECTOR IN TO POSITION AT 60 KTS. IAW AMM 27-53-01 PAG 201. FLAPS WARNING SWITCH CHECK AND TEST WERE EFECTUATED. FAULT NOT DUPLICATED.
- [SDR ANCF200700023](https://openairdocs.org/sdr/ANCF200700023.md): Packing · broken · Oct 16, 2007 · N632CT · Doug MD83 · Hydraulic System, Main
  > DURING APP AT BOG, R HYD QTY DROPPED TO 1 QT WITH THE SYSTEMS PRESSURIZED. THERE WAS NOT R HYD QTY ANNU ON THE EOAP. (THIS CAUSES EMERGENCY LANDING) SEVERE HYD LEAK FOUND AT FWD OUTLET LINE FITTING OF MOTOR OPERATED DUAL SHUTOFF VALVE. DURING INSPECTION FITT
- [SDR ANCF200700021](https://openairdocs.org/sdr/ANCF200700021.md): Electrical Sys · multiple fail · Sep 24, 2007 · N632CT · Doug MD83 · Electrical Power System
  > DURING TAKEOFF ROLL, HAD AN ELECTRICAL FAILURE: TAKEOFF WAS ABBORTED AT 90 KNOTS. THE FLIGHT GUIDANCE STATUS AND MAINT PNL C/B G 25 WAS TRIPPED. THE AC BUSS PHASE B C/B WAS ALSO TRIPPED. ART WAS ACCURATED. IAW AMM 24-20-00/201 GCU`S WERE CHECKED AND RESET
- [SDR ANCF200700012](https://openairdocs.org/sdr/ANCF200700012.md): Pin · installed · Jun 2, 2007 · N632CT · Doug MD83 · Main Landing Gear
  > AFTER TAKEOFF LEFT AND RIGHT AND GEAR DOOR OPEN LIGHTS REMAIN ON. ABNORMAL CHECK LIST CARRIED OUT AND RETURNED. LANDING EXTEND AND ALL INDICATION WERE NORMAL. NORMAL LANDING CARRIED OUT SKBO. GEAR LOCK PINS WERE FOUND INSTALLED ON BOTH MAIN LANDING GEAR.
- [SDR ANCF200600019](https://openairdocs.org/sdr/ANCF200600019.md): Control Unit · failed · May 14, 2006 · N632CT · Doug MD83 · AC Power Distribution System
  > DURING CLIMB AT FLIGHT LEVEL 210 AC CROSS DURING CLIMB AT FLIGHT LEVEL 210 AC CROSS TIE LOCK OUT LIGHT TURNED ON WITH NO ADDITIONAL LIGHTS IN THE EOAP. FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR. FOUND BURNT GCU APU IN ACCORDANCE TO AMM 24-20-07 PAG 4
- [SDR ANCF200600003](https://openairdocs.org/sdr/ANCF200600003.md): Pump · failed · Jan 11, 2006 · N632CT · Doug MD83 · Fuel Boost Pump
  > DURING FLIGHT, CENTER TANK FAILS TO FEED. INFLIGHT ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTIING AS PER AMM 28-20-07 AND CONFIRMED THAT AFTER CENTRAL FUEL TANK AC PUMP IS FAULT. TRANSFERED TO DMI 648 AS PER MEL 28-2 CATEGORY C. MAINTENACE PRO
- [SDR ANCF200400048](https://openairdocs.org/sdr/ANCF200400048.md): Csd · failed · Apr 20, 2005 · N632CT · Doug MD83 · Alternator-Generator Drive
  > DURING RT ENG START, RT GEN FREQ 396 CPS & GEN CAME ON LINE AT 50 PERCENT N2. REPORTED TO TECH. DURING TAKEOFF ROLL, RT GEN TRIPPED, RESET UNSUCCESFULL. RT CSD OIL TEMP BEGAN RISING UNTIL OFF SCALE, WITH GEN OFF, FOLLOWED CHKLST, CSD DISCONNECTED. THROUGH
- [SDR ANCF200400035](https://openairdocs.org/sdr/ANCF200400035.md): Transducer · malfunctioned · Nov 22, 2004 · N632CT · Doug MD83 · Landing Gear Position and Warning
  > TWO REJECTED TAKEOFF WAS PERFORMED DUE WHEEL NOT TURNING COMES ON APPROX 90 KNOTS. REPLACED TRANSDUCER IN MLG RT POSITION NR 3 AND NR 4 IAW AMM:32-43-02 PAG 201 PN OFF:4062575, S/N:OFF:627, S/N ON:5325A POS NR 3.
- [SDR ANCF200400033](https://openairdocs.org/sdr/ANCF200400033.md): Landing Gear · out of rig · Oct 10, 2004 · N632CT · Doug MD83 · Nose/Tail Landing Gear
  > TAKE-OFF WAS ABORTED DUE TO STRONG VIBRATION OA THE NOSE GEAR, IT HAPPENED ABOVE 100 KTS. IAW AMM 32-21-03 PAGE 403. IN NLG WAS PERFORMED CHECK AND RIGGING IN NOSE GEAR UPPER LINKAGE TORQUE TUBE.
- [SDR ANCF200400030](https://openairdocs.org/sdr/ANCF200400030.md): Csd · overserviced · Sep 9, 2004 · N632CT · Doug MD83 · Alternator-Generator Drive
  > RT CSD OIL TEMPERATURE REACHED THE RED ZONE. ABNORMAL PROCEDURE WAS ACCOMPLISHED SWITCHING RT GENERATOR OFF, RT CSD OIL TEMPERATURE STARTED TO COOL DOWN. THE OIL LEVEL WAS FOUND OVERFILL, IT WAS DRAINED AND PERFORMED FLUSHING CHECK POP OUTS MAGNETIC CHIP DET
- [SDR ANCF200400027](https://openairdocs.org/sdr/ANCF200400027.md): Indicator · failed · Aug 12, 2004 · N632CT · Doug MD83 · Rate of Climb Indicator
  > AFTER T/O THE LT RATE OF CLIMB IND FAIL. IAW AMM 34-14-01/201 THE VERTICAL SPEED INDICATOR LT POS. WAS REMOVED AND REPLACED. OPS CHECKED ON GROUND, SATISFACTORY.
- [SDR ANCF200400006](https://openairdocs.org/sdr/ANCF200400006.md): Radome · bird strike · Apr 9, 2004 · N632CT · Doug MD83 · Aerodynamic Fairings
  > BIRD STRIKE AT AIRPLANE'S DOME, THE AIRCRAFT DID NOT SHOW ANY ABNORMAL INDICATION, RADAR WAS TURN OFF AS A PRECAUTIONARY MEASURE. THE RADOME WAS REPLACED IAW AMM 53-51-00 PAG 401 AND ANTENNA TILT POSITION WAS CHECKED AND PERFORMED TEST IAW AMM 34-41-00 PAG 20
- [SDR ANCF173EE](https://openairdocs.org/sdr/ANCF173EE.md): Cylinder · cracked · Oct 22, 2003 · N632CT · Doug MD83 · Main Landing Gear Strut/Axle/Truck
  > AS RESULT OF MAGNETIC PARTICLE INSPECTION AS REQUIRED BY AVIANCA ENGINEERING ORDER 83-32-031 R4 REFERING SB MD80-32A286R3 WAS FOUND THE SHOCK STRUT CYLINDER AT LT MLG WITH CRACKS
- [SDR ANCF200300019](https://openairdocs.org/sdr/ANCF200300019.md): Cable · broken · Jun 28, 2003 · N632CT · Doug MD83 · Landing Gear Steering System
  > WHILE TURNING TO POSITION ON THE RUNWAY FOR TAKE OFF,THE NOSE WHEEL STEERING SYSTEM BROKE DOWN. LOOSING ALL CONTROL. C/A: ACCOMPLISHED REPLACE OF THE SYSTEM DIRECTIONAL CABLES,WAS VERIFICATED RIGGING OF SYSTEM IAW AMM 32-50-00 PAG 201-205 TEST ON GROUND SATI
- [SDR ANCF200200022](https://openairdocs.org/sdr/ANCF200200022.md): Hose · loose · Oct 14, 2002 · N632CT · Doug MD83 · Airspeed/Mach Indicator
  > RT AIRSPEED INDICATOR INOPERATIVE. IT WAS FOUND LOOSEN HOSE IN CADC. IT WAS ADJUSTED PROPERLY AND PERFORMED TEST IAW AMM.
- [SDR ANCF200200016](https://openairdocs.org/sdr/ANCF200200016.md): Pin · damaged · Aug 1, 2002 · N632CT · Doug MD83 · Tire Tube
  > DURING APPROACH LEFT INBOARD ANTISKID ANNUNCIATION CAME ON, ABNORMAL CHECK LIST WAS PERFORMED AND IT WAS UNSUCCESFULL.DUE TO SHORT RUNWAY IN PEREIRA CREW RETURNED TO BOGOTA. ANTI-SKID CCONTROL TEST AND ANTI-SKID CONTROL BOX BITE WERE PERFORMED IAW AMM 32-43-00
- [SDR ANCF200200011](https://openairdocs.org/sdr/ANCF200200011.md): Coalescer Bag · dirty · Jun 9, 2002 · N632CT · Doug MD83 · Humidity Control System
  > AFTER TAKE OFF A STRONG SMOKE SMELL WAS PRESENTED IN THE COCKPIT, INMEDIATELY, THE CABIN SUPPERVISOR INFORMED THAT THERE WAS A STRONG SMOKE SMELL ALONG THE PASSENGER CABIN, SPECIALLY IN THE REAR SECTION. THERE WAS NOT FUMES NOR FIRE VISIBLE AT ANY MOMENT. WE R
- [SDR ANCF200200005](https://openairdocs.org/sdr/ANCF200200005.md): Csd · failed · Mar 10, 2002 · N632CT · Doug MD83 · AC Generation System
  > AFTER TAKE OFF ROLL DURING CLIMB. PRIOR TO CLIMB THRUST REDUCTION IN ANNUNCIATOR PANEL, RIGHT CSD OIL PRESSURE LOW AND RIGHT GENERATOR OFF APPEARS. WAS PERFORMED THE RESPECTED MALFUNCTIONS PROCEDURE AND CHECK LIST. THE CREW RETURNED TO EDR. THE RIGHT CSD WAS
- [SDR ANCF200100022](https://openairdocs.org/sdr/ANCF200100022.md): Engine · malfunctioned · Dec 1, 2001 · N632CT · Doug DC983 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, LT ENGINE WAS REDUCED DUE TO IMPENDING HIGH EGT (576°C), THE BEHAVIOR OF THE LEFT ENGINE WAS NORMAL UNTIL CLIMBING, THROUGH APPROXIMATELY FL 280, A STRONG STALL NOISE WAS FELT WITH AIRCRAFT YAWING. LT ENGINE EPR WAS DECREASED AND EGT ROSE UP.
- [SDR ANCF200100016](https://openairdocs.org/sdr/ANCF200100016.md): Fan · failed · Oct 8, 2001 · N632CT · Doug DC983 · Air Distribution Fan
  > DURING CLIMB STRONG NOISE WAS HEARD CLOSE TO THE RT AFT WINDOW IN THE COCKPIT AND BETWEEN 15 & 16 ROW CEILING IN THE CABIN. WHEN LEVELED OFF AT FL310 THE AHRS NR 2 WAS LOST, CONTINUING THE FLIGHT WITH TRANSFER BOTH ON 1. RETURNED TO BOGOTA. CIRCUIT BREAKER
- [SDR ANCF200100014](https://openairdocs.org/sdr/ANCF200100014.md): Flow Valve · failed · Sep 18, 2001 · N632CT · Doug DC983 · Cabin Cooling System
  > AFTER TAKEOFF WITH LT PACK INOPERATIVE, THE FLOW LIGHT CAME ON. CHECK LIST WAS PERFORMED UNSUCCESSFULLY, OUT FLOW VALVE WAS FULLY CLOSE ALL THE TIME. CABIN AUTOMATIC PRESSURE CONTROLLER DEFERRED TO CARRY OVER 090 MEL 21-24 CAT-C. FLOW CONTROL VALVE WAS CHAN

## 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 = 'N632CT' AND deregistration_id = 'N632CT-2017-10-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N632CT-2017-10-06/reports

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