1990 Beechcraft KING AIR C90A

  • UP-K9001-1
  • UP-K9001-2
  • UP-K9001-1
  • UP-K9001-2


Engine Hours
TSN: 3666/7000
SOH: 548/0
TBO: 3600/3600
Propellers Hartzell 4-blade. Overhauled March 2012
SOH: 1686



Collins Single Tube 4″ EFIS
Com Dual Collins VHF 22C
Nav Dual Collins VIR 32
DME Collins DME 42
ADF Collins ADF 60A
GPS King KLN 90B
Transponders Dual Collins TDR 94
Autopilot Collins APS 65H
Radar Collins WXR 270
Stormscope WX 950
Rad Alt Collins ALT 50A
ELT Artex 406



Raisbeck dual aft body strake

Raisbeck wing lockers

Raisbeck exhaust stack fairings

Raisbeck propellers with increased gross weight

Standby horizon

Avcon camera hatch Digital aerophotographic camera Vexcel UltraCAM-X with gyro-stabilized platform SOMAG GSM-3000

Server UltraMap

AEROcontrol-II inertia navigation system (INS) of aerial pictures georeference with hardware support of planning and navigating of aerial survey CCNS WinMP and AEROoffice on CD




Overall White with Burgundy and Grey stripes




Currently equipped for aerial survey work, but available, standard 6 passenger interior in Beige leather. Aft toilet. Forward and Aft Cabin Partitions. Dual Tables. Forward RH Refreshment Centre.

Logbooks Available?
Other Logbook Info:

Logbooks available upon request

Fuel Efficiency (mpg US): 2.89
Years Aircraft Manufactured: 1971 - 1982
Serial Number Range: 502 - 1010
Seating Options: 10
Wing Loading lb/sq ft: 32.8
Power Loading lb/hp: 8.8
Noise(EPNdB): Takeoff/Sideline/Approach: 81.3
External Length (FT): 35.5
External Height (FT): 14.3
External Span (FT): 50.3
Internal Length (Overall/Net Height): 12.7
Internal Width (Max/Floor): 4.5
Internal Height: 4.8
Engine: 2 P&WC PT6A - 21
Power Output / Flat Rating: 550shp/ISA+18
Inspection Interval: 3600t
Max Ramp Weight (LBS): 10160
Max Takeoff Weight (LBS): 10100
Max Landing Weight (LBS): 9600
Zero Fuel Weight (LBS): 9389b
Empty Weight-BOW (LBS): 6780
Max Payload (LBS): 2609
Useful Load (LBS): 3380
Executive Payload (LBS): 1400
Max Fuel (LBS): 2573
Avail Payload Max Fuel (LBS): 807
Avail Fuel Max Payload (LBS): 771
Avail Fuel Exec Payload (LBS): 1980
Cabin Pressurization (PSI): 5
TO Distance (SL @ ISA) FT: 2577
TO Distance (5000 @25C) FT: 4550
Engine Out Rate (fpm): 554
Engine-Out (ft/nm): 305
Certificated Ceiling: 30000
All Eng Service Ceiling: 29800
Eng Out Service Ceiling: 14900
SL Cabin Max ALT: 11065
LRC Fuel Flow (lb/h): 316
LRC Specific Range: 0.614
HSC Specific Range: 0.417
Listing Package: No
Aircraft Category: Airplane
Class: Multi-Engine Land
Propulsion Type: Turboprop
Make: Beechcraft
Model: KING AIR C90A
Total Time: 7295
Range (NM): 219
Year: 1990
High Speed Cruise (KTAS): 247
HSC Fuel Burn (lb/h): 592
HSC Fuel Burn (In GPH): 98.50
Tail Number: UP-K9001
Serial Number: LJ1236
Engine 1 SMOH: 548
Condition: Used
Flight Rule Approval: IFR
Sale Type: Standard Sale

Fuel Efficiency Rating

  • 2.89MPG
  • N/AMPG Per Seat

Actual rating will vary based on flight conditions, aircraft features and pilot operation. Values are for informational purposes only and as such are not intended for navigation or flight planning. Please consult the POH for actual values.

All Specifications and Claims subject to Buyer’s verification.
Availability subject to prior sale and/or withdrawal from market without notice.

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