Airframe
Status (As of January 15,
2009)
SERIAL NUMBER: 016
REGISTRATION NUMBER: N74SG
DATE OF MANUFACTURE: January 1999
ENTERED INTO SERVICE: January 1999
TOTAL TIME: 5228
LANDINGS: 5185
- Phase A Inspection due at 5387 hrs or
May 2009
- Phase B Inspection due at 5397 hrs or
December 2009
- Phase C Inspection due at 5997 hrs or
December 2012
- Phase D Inspection due at 7197 hrs or
December 2016
- Eligible for Smart Parts Program.
- Maintenance Tracking Program: CAMP
Engine
Status
Left Engine:
- Honeywell TFE 731-20BR-1B
- Serial Number: P-111144
- Hours: 5228
- Cycles: 5185
- MPI due: 5539.4
- CZI due: 6000
Right Engine:
- Honeywell TFE 731-20BR-1B
- Serial Number: P-111145
- Hours: 5228
- Cycles: 5185
- MPI due: 5539.4
- CZI due: 6000
APU: Allied Signal RE 100-LJ, S/N P-164,
1512.3 hours.
Weights
- Gross Weight (Ramp): 21,750 lbs.
- Max Take Off Weight: 21,500 lbs.
- Max Landing Weight: 19,200 lbs.
- Empty Weight: 13,549 lbs.
Interior
Completed at Learjet Inc. Wichita, KS
January 1999. Soft goods and hard goods refurbished November 2008 by BAS
Tucson.
Fireblocked, Nine (9) passenger cabin: Eight, (8) place Standard
Floorplan (Option #1) configuration with four (4) single foldout tables and
two (2) double foldout tables. Aft lavatory is belted for take-off and
landing. Galley is forward right cabin. Headliner and window panels are
off-white Ultra-leather, seats and lower sidewall is beige leather. Cabinet
exteriors are covered with a medium Walnut veneer and Metal Accents are
Chrome.
Avionics
Honeywell Primus 1000 system, which
includes:
- Four 8- by 7-inch Display Tubes
including dual PFD, one MFD and one EICAS display
- Engine Instrument/Crew Alerting System
(EICAS)
- Electronic Flight Instrument System (EFIS)
- Dual IC-600 integrated Avionics
Computers
- Dual DA-800 Dual-channel Data
Acquisition Units
- Dual AZ-850 solid-state Micro Air Data
Computers
- Dual Honeywell AHZ-800 AHRS
- Honeywell Primus 650 Radar with
Turbulence Detection
Honeywell Primus II integrated radio system which includes:
- Dual Radio Management Units (RMU)
- Dual RCZ-833 VHF Integrated Comm Units
(8.33 kHz) Includes: Mode S Diversity Transponders
- Dual RNZ-850 Integrated Navigation
Units:
Includes: (FM Immunity), DME & single ADF
- Honeywell RT-300 Radio Altimeter
- Dual Universal UNS-1C FMS (SCN 604) (has
Internal GPS)
- Bendix King CAS 67 ACAS II / TCAS II
(Change 7)
- Allied Signal KHF-950 HF with SELCAL
- 2-inch backup instruments
- Dual Angle of Attack indicators
- Pedestal mounted Hobbs meter
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Additional Equipment
- Honeywell Cockpit Voice Recorder (30
min)
- Allied Signal MK-V EGPWS (w. Windshear)
- ARTEX 406 ELT with Nav interface
- RVSM Equipped
- Lighted Chart Holders
- Hot Liquid container
- Magnastar C-2000
- Remote Oxygen Servicing Provision
- Floor Emergency Escape Path Marking
Exterior
Repainted by BAS Tucson November 2008. The
fuselage is painted overall Matterhorn white; accent stripes TBD by
purchaser. |
