N801SK

Cancelled 2006

Deregistered aircraft · 1994 Beech 1900D · Pratt & Whitney PT6A series

Cancelled
January 6, 2006
Exported to
South Africa
Status when cancelled
Valid registration
Serial number
UE-80
Year built
1994
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, commuter
Airworthiness date
January 21, 1994
Certificate issued
January 27, 2005
Last registry action
March 3, 2005
Mode S code
AAE72E
Owner when cancelled
General Aviation Leasing LLC
Owner type
Corporation

From the FAA registry file of October 31, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 13

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

SDR S2YA05012Gyro · inoperativeFLT 6116 - IMT-MKE - BEFORE TAKEOFF, THE CREW REPORTED THE FO DISPLAY UNIT WENT BLANK, WHEN THEY TRIED TO RESET IT THE CA DISPLAY WENT BLANK ALSO. THE CREW RETURNED TO THE GATE AND REPORT THE RED ATT AND FD FLAP ON THE FO ADI. THE AIRCRAFT WAS FERRIED BACK TFeb 5, 2005 · N801SK · Beech 1900D · Attitude and Direction Data SystemSDR S2YA04016Computer · malfunctionedDURING FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED ANNUNCIATORS ILLUMINATED INCLUDING THE FLIGHT DIRECTOR AND YAW DAMP. THE CREW MADE A PRECAUTIONARY AIR-TURN-BACK. MX INSPECTED THE SYSTEM INCLUDING REMOVAL, INSPECTION AND REINSTALL OF BOTH FYD-65 YAMay 22, 2004 · N801SK · Beech 1900D · Air Data ComputerSDR S2YA970030Switch · dirtyMKE/IND - FLT 1042 - DURING CLIMB, FLIGHT CREW NOTICED THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THEY NOTIFIED DISPATCH AND ATC OF THE PROBLEM, AND RETURNED TO MKE WITHOUT FURTHER INCIDENT. ONCE ON THE GROUND IN MKE, MAINTENANCE INSPECTED THE DOOR AND ANNUNCIASep 24, 1997 · N801SK · Beech 1900D · Door Warning SystemSDR S2YA970029Power Section · failedMKE/CVG - FLT 1026 - DURING CLIMB-OUT, CREW NOTICED THE RT ENGINE TORQUE FLUCTUATING PLUS OR MINUS 200 FEET/POUNDS AND PROPELLER SPEED WAS FLUCTUATING WITH THE TORQUE FLUCTUATIONS. THE CREW NOTIFIED ATC AND RETURNED TO MKE WITHOUT INCIDENT. THE RT AND LT PROSep 10, 1997 · N801SK · Beech 1900D · Turbine SectionSDR S2YA970028Prop Governor · malfunctionedMKE/BNA - FLT 1267 - DURING CLIMB-OUT, FLIGHT CREW SET CLIMB POWER AND FOUND LT ENGINE TORQUE FLUCTUATING APPROXIMATELY 200 FEET/POUNDS. THE CREW NOTIFIED ATC OF THE PROBLEM, DECLARED AN EMERGENCY, AND MADE AN UNEVENTFUL LANDING. MAINTENANCE GROUND RAN AIRCRSep 2, 1997 · N801SK · Beech 1900D · Propeller GovernorSDR S2YA97021Propeller Boot · debondedMKE/LSE - FLT 1093 - DURING FLIGHT, THE RT PROPELLER THREW A DEICE BOOT. THE CREW WAS ALERTED TO THE BOOT BEING FLUNG BY THE NOISE IT MADE HITTING THE SIDE OF THE FUSELAGE. THE CREW RETURNED TO MKE FOR REPAIRS. MAINTENANCE REPLACED THE PROPELLER, INSPECTED Apr 21, 1997 · N801SK · Beech 1900D · Propeller Deice Boot SectionSDR S2YA97012Actuator · malfunctionedMKE/IND - FLT 1052 - FLIGHT CREW SELECTED THE LANDING GEAR DOWN ON FINAL APPROACH. WHEN GEAR WAS EXTENDED, THE RT MAIN GEAR DOWN AND LOCKED ANNUNCIATOR DID NOT ILLUMINATE AND THE GEAR HANDLE HAD AN INTRANSIT LIGHT. THE CREW PERFORMED ALL NECESSARY CHECKS, THMar 21, 1997 · N801SK · Beech 1900D · Landing Gear ActuatorSDR 97ZZZX1792Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N801SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1788Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,Nov 1, 1996 · N801SK · Beech 1900D · Attitude and Direction Data SystemSDR 96ZZZM1052Oil Psi Gauge · malfunctionedTHE FLIGHT CREW NOTICED THE RIGHT ENGINE OIL PRESSURE INDICATION HAD DROPPED TO 27 PSI, BUT NO 'LOW PRESSURE' LIGHT. THEY TURNED BACKED TO MKE (FLT NR 1162 MKE-SBN) AND TOOK PRECAUTION TO SAVE THE ENGINE BY FEATHERING IT ON FINAL APPROACH. MX REPLACED THE RIJun 6, 1996 · N801SK · Beech 1900D · Engine Oil PressureSDR S2YA950020Rib · crackedDURING AN SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT WING CENTER MID RIB AT WS 83.00 TO HAVE A CRACK AT THE TOP APPROXIMATELY FIVE INCHES ACROSS. THE CRACK WAS LOCATED BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS AND A REPAIR WAS MADE. THE RIB REINFORAug 18, 1995 · N801SK · Beech 1900D · Wing, Rib/BulkheadSDR S2YA950003Volt/Freq Meter · knob missingTHE PUSH-TO-READ VOLT BUTTON ON THE A.C. VOLT/FREQUENCY METER EASILY BREAKS OFF OR BECOMES LOOSE AND FALLS OFF. SUBMITTER SUGGESTED THE DESIGN NEEDS TO BE IMPROVED. THREE INSTANCES OF THIS PROBLEM HAS OCCURRED ON DIFFERENT AIRCRAFT ON FLEET. (X)May 12, 1995 · N801SK · Beech 1900D · AC Generation SystemSDR 95ZZZX2478Flap Motor · inopPILOT REPORTED FLAPS COULD NOT BE SELECTED DOWN AND DURING DESCENT THEY HAD SMELL OF BURNING CARDBOARD OR SIMILAR MATERIAL. MAINTENANCE FOUND THE FLAP RELAY HOT DURING TROUBLESHOOTING. MAINTENANCE PULLED AND TY-WRAPPED BOTH FLAP MOTOR CIRCUIT BREAKERS AND MEMar 28, 1995 · N801SK · Beech 1900D · Trailing Edge Flap Control System

Other aircraft with N801SK · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N801SK is registered now to the first aircraft listed.