# N632CT: Mcdonnell Douglas MD 83, registration cancelled 2017-10-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 6, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas MD 83](https://openairdocs.org/model/mcdonnell-douglas-md-83) (registry code 3023681) - Serial number: 49632 - Type of aircraft: Fixed wing multi engine - Certificate issued: March 15, 2011 - Last registry action: March 15, 2011 - Mode S code: A8456E - Owner when cancelled: [Jet Midwest Group LLC](https://openairdocs.org/faa-owner/JET%20MIDWEST%20GROUP%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N632CT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=632CT - Page: https://openairdocs.org/deregistered/N632CT-2017-10-06 From the FAA registry file of November 7, 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 MD 83: https://openairdocs.org/model/mcdonnell-douglas-md-83.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ANCF2009061800050](https://openairdocs.org/sdr/ANCF2009061800050), Jun 18, 2009: CONTROLLER. MALFUNCTIONED. 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 DECELE - [SDR ANCF200700030](https://openairdocs.org/sdr/ANCF200700030), Dec 4, 2007: WARNING SYSTEM. FALSE ACTIVATION. 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 - [SDR ANCF200700023](https://openairdocs.org/sdr/ANCF200700023), Oct 16, 2007: PACKING. BROKEN. 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 - [SDR ANCF200700021](https://openairdocs.org/sdr/ANCF200700021), Sep 24, 2007: ELECTRICAL SYS. MULTIPLE FAIL. 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 PHA - [SDR ANCF200700012](https://openairdocs.org/sdr/ANCF200700012), Jun 2, 2007: PIN. INSTALLED. 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. N - [SDR ANCF200600019](https://openairdocs.org/sdr/ANCF200600019), May 14, 2006: CONTROL UNIT. FAILED. 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 A - [SDR ANCF200600003](https://openairdocs.org/sdr/ANCF200600003), Jan 11, 2006: PUMP. FAILED. DURING FLIGHT, CENTER TANK FAILS TO FEED. INFLIGHT ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTIING AS PER AMM 28-20-07 AND CONFIRMED THAT AFTER CENT - [SDR ANCF200400048](https://openairdocs.org/sdr/ANCF200400048), Apr 20, 2005: CSD. FAILED. 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 - [SDR ANCF200400035](https://openairdocs.org/sdr/ANCF200400035), Nov 22, 2004: TRANSDUCER. MALFUNCTIONED. 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 - [SDR ANCF200400033](https://openairdocs.org/sdr/ANCF200400033), Oct 10, 2004: LANDING GEAR. OUT OF RIG. 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 N - [SDR ANCF200400030](https://openairdocs.org/sdr/ANCF200400030), Sep 9, 2004: CSD. OVERSERVICED. 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 OI - [SDR ANCF200400027](https://openairdocs.org/sdr/ANCF200400027), Aug 12, 2004: INDICATOR. FAILED. 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), Apr 9, 2004: RADOME. BIRD STRIKE. 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 AM - [SDR ANCF173EE](https://openairdocs.org/sdr/ANCF173EE), Oct 22, 2003: CYLINDER. CRACKED. 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 - [SDR ANCF200300019](https://openairdocs.org/sdr/ANCF200300019), Jun 28, 2003: CABLE. BROKEN. 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 DIR - [SDR ANCF200200022](https://openairdocs.org/sdr/ANCF200200022), Oct 14, 2002: HOSE. LOOSE. 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), Aug 1, 2002: PIN. DAMAGED. DURING APPROACH LEFT INBOARD ANTISKID ANNUNCIATION CAME ON, ABNORMAL CHECK LIST WAS PERFORMED AND IT WAS UNSUCCESFULL.DUE TO SHORT RUNWAY IN PEREIRA CREW RETURN - [SDR ANCF200200011](https://openairdocs.org/sdr/ANCF200200011), Jun 9, 2002: COALESCER BAG. DIRTY. 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 PASS - [SDR ANCF200200005](https://openairdocs.org/sdr/ANCF200200005), Mar 10, 2002: CSD. FAILED. 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 PERFORME - [SDR ANCF200100022](https://openairdocs.org/sdr/ANCF200100022), Dec 1, 2001: ENGINE. MALFUNCTIONED. 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, - [SDR ANCF200100016](https://openairdocs.org/sdr/ANCF200100016), Oct 8, 2001: FAN. FAILED. 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 N - [SDR ANCF200100014](https://openairdocs.org/sdr/ANCF200100014), Sep 18, 2001: FLOW VALVE. FAILED. 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 AUTO --- 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.