Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale or Removal From Market.

Transcription

1 Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale or Removal From Market.

2 K i n g A i r C 9 0 S e r i a l N u m b e r LJ- 675 * N G A H I G H L I G H T S : R a i s b e c k F o u r - B l a d e P r o p s R a i s b e c k A f t S t r a k e s E n g i n e s O v e r h a u l s b y D a l l a s A i r m o t i v e E n g i n e H o t S e c t i o n s b y P r i m e T u r b i n e s G a r m i n G N S w i t h T A W S S i x Y e a r L a n d i n g G e a r I n s p./stevens N e w G o o d r i c h D e i c e B o o t s F i v e Y e a r B r a k e / P n e u m a t i c H o s e s C O N T A C T : J E T T O L B E R T P H O N E Ext.1 E M A I L JET@AMERICANAIRCRAFTSALES.COM W E B S I T E AMERICANAIRCRAFTSALES.COM N F e d e r a l H w y S u i t e B o c a R a t o n F L

3 K i n g A i r C 9 0 S e r i a l N u m b e r L J * R e g i s t r a t i o n N u m b e r N G A Airframe: TTSN 10,326.2 Hours / 9,830 Landings Engines: Props: Two PT6A-21 Right Engine: SN PCE24317 / TTSN 10,239.3 / 9,407 Cycles / 3,148 SOH / SHS Left Engine: SN PCE24315 / TTSN 10,239.3 / 9,407 Cycles / 3,148 SOH / SHS NOTE: Engines were Overhauled by Dallas Airmotive on Hot Sections done by Prime Turbine on Raisbeck Four-Blade Left and Right: Hours Total Time / Hours SOH Avionics: Audio Panel: Bendix / King KMA-24 #1 COM/NAV/GPS with TAWS: Garmin GNS-530 #2 COM/NAV: Bendix / King KX-165 Transponder: Bendix / King KT-76A Compass System: Collins PN-101 #1 VOR/LOC/GLS Indicator: Collins 331A-3G #2 VOR/LOC/GLS Indicator: Bendix / King KI-206 RMI: Bendix / King KI-266 Radar Altimeter: Terra TRI-40 DME: Bendix / King KN-64 Radar System: Bendix RDR-160 (ART 161 with IN2026A overhauled with new magneto ) ICS: PS Engineering PM1000ll Stormscope: BF Goodrich WX1000E Autopilot / Flight Director: Century IV Yaw Damper System: Century IV YK-384 ADF with KA44B Loop Antenna: Bendix / King KR-87 Clock: Davtron M811B Encoding Altimeter: IDC Maintenance: Engine Fire Extinguishers: Left & Right: Complied with: Certification Due: SQUIBES are 10 year, Complied with on: Certification Due: New Oil Filters : At Total Time : 10, Complied with on: Fuel Nozzels: At Total Time: 10, Complied with on: Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale or Removal From Market.

4 Last Phase IV: At Total Time: 10, Complied with on: Six Year Landing Gear Inspection: c/w: by Stevens Aviation at Total Time: , Cycles: New Goodrich Deice Boots: Installed on: AD : 3 Year 1000 Hour SIRM Wing Bolt Inspection: Complied with on: by Landmark Aviation at Total Time: ,000 Hour Splice Plate complied with Wing Bolts (New , Total Time: Bolts are 15,000 Hour or 15 Year Bolts Due: /15,000 HOUR). 30 Month Lub/Gear: Complied with on: All New Sprockets and Bearings 30 Month Lub Complied with at Total Time: 10, Month Lub Complied with at Total Time: 10, June 20, 2011: Removed HydroeaIre Fuel Boost Pumps and Installed Standard Overhauled Left and Right Fuel Boost Pumps,P/N: PROP GOV'S: Left : R ight: GENERATORS: Overhauled left & Right on: At Total Time: Next Due: 1000 Hours at Total Time: 10,953.5 LUB: 200, 400, 800 AND 1200 : Complied with on: At Total Time: 10, NEW EVAPORATOR FILTER: Complied with on: At Total Time: 10, NEW GILL BATTERY : ON ALTIMETER/PITOT/STATIC/TRANSPONDER INSPECTION (FAR & FAR ): C/ w: Next Due: CABIN CONTROLLER: Overhauled with New Filter on: At Total Time: INSTRUMENT FILTER : New on: At Total Time: 10, Next Due: OXYGEN BOTTLE & REGULATOR: Recertified on: Next Due: AD : Main Gear Torque Links Complied with on: At Total Time: 10, New Bushings and Bolts Next Due: 11, YEAR BRAKE HOSES: Complied with on: Next Due: YEAR PNEUMATIC HOSES: Complied with on: Next Due: HOUR POWER LEVER PIN: Complied with on: Next Due: Total Time: 11, YEAR EDGE LIGHTS: Complied with on: Next Due: NOTE: NON-ESSENTIAL SPECIAL MISSION POWER INSTALLED V IA FAA FIELD APPROVED FAA FORM 337, WITH INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ( ICA) DATED: TO INCLUDE THE FOLLOWING: SPECIAL MISSIONS POWER PANEL WITH TWO POWER CONNECTORS, 1 EACH 20 AMP MAX POWER OUTPUT, 1 EACH 10 AMP MAX POWER OUTPUT. SEVEN BNC ANTENNA FEED THRU CONNECTORS AS FOLLOWS: UHF1, UHF2,TACAN, LATR GPS (TOP), LATR ( BOTIOM), 2 EACH SNTC ANTENNAS. THE ABOVE ANTENNAS ARE FAA DER STRUCTURAL APPROVED VIA FAA FORM DATED: AIRCRAFT HAS STANDARD AND RESTRICTED AIRWORTHINESS CERTIFICATES. AIRCRAFT PART 135 FLOWN & MAINTAINED. REMOVED FROM PART 135 IN 2011 AND CURRENTLY MAINTAINED UNDER CURRENT BEECH MAINTENANCE MANUAL. Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale or Removal From Market.

5 Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale or Removal From Market.

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7 C O N T A C T : J E T T O L B E R T P H O N E Ext.1 E M A I L JET@AMERICANAIRCRAFTSALES.COM W E B S I T E AMERICANAIRCRAFTSALES.COM N F e d e r a l H w y S u i t e B o c a R a t o n F L