Airframe
Status (As of
June 18, 2008)
SERIAL NUMBER: 237
REGISTRATION NUMBER: N43QG
DATE OF MANUFACTURE: November 2003
ENTERED INTO SERVICE: April 2004
TOTAL TIME: 1817.7
LANDINGS: 1238
- Next Phase A Inspection
due at 2103.4 hrs or Dec 2008
- Next Phase B Inspection
due at 2403.4 hrs or Dec 2009
- Next Phase C Inspection
due at 2461.3 hrs or Oct 2010
- Phase D Inspection due at
2400 hrs or Apr 2012
Aircraft Parts Program:
Smart Parts
Maintenance Tracking Program: CAMP
Engine
Status
Left Engine:
- Honeywell TFE 731-20BR-1B
- Serial Number: P-116480C
- Hours: 1817.7
- Cycles: 1234
- MPI due: 2500
- CZI due: 5000
Right Engine:
- Honeywell TFE 731-20BR-1B
- Serial Number: P-116479C
- Hours: 1817.7
- Cycles: 1234
- MPI due: 2500
- CZI due: 5000
Engines and APU are covered
under the Honeywell MSP Program.
APU: Allied Signal RE 100-LJ, S/N P-175, 551 hours
Weights
- Gross Weight (Ramp):
21,750 lbs.
- Max Take Off Weight:
21,500 lbs.
- Max Landing Weight: 19,200
lbs.
- Empty Weight: 13,681 lbs.
Avionics
Honeywell Primus 1000
system, which includes:
- Engine Instrument/Crew
Alerting System (EICAS)
- Electronic Flight
Instrument System (EFIS)
- Four 8- by 7-inch Display
Tubes including dual PFD, one MFD and one EICAS display
- 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 660 Radar
- Honeywell Primus II
integrated radio system which includes:
- Dual Radio Management
Units (RMU)
- Dual RCZ-833 Integrated
Comm Units (8.33 kHz) Includes: VHF Com & Transponder
- Dual RNZ-851 Integrated
Navigation Units includes:
VHF Nav (FM Immunity), DME and single ADF
Honeywell RT-300 Radio Altimeter
- Dual Universal UNS-1E FMS
(SCN 802.4) (with GPS)
- 2-inch backup instruments
- Honeywell Cockpit Voice
Recorder (120 min)
- Bendix King TCAS 2000 TCAS
II (Change 7)
- Bendix King KHF-950 HF
with SELCAL
- Allied Signal MK-V EGPWS
(w. Windshear)
- ARTEX 406-2 ELT
- Magnastar C-2000 Digital
Airborne Telephone System
- Dual Angle of Attack
indicators
- Pedestal mounted Hobbs
meter
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Additional Equipment
- Increased MTOW to 21,500
lbs
- RVSM Compliant
- Lighted Chart Holders
- Hot Liquid container
- AIRSHOW 400
- Remote Oxygen Servicing
Provision
- Floor Emergency Escape
Path Marking
- Pulsating Recognition
Lights
- Optional Logo Lights
Interior
Original interior
completed at Learjet Inc. Tucson, Arizona; April 2004. Seats, carpet and
cabin lower side walls refurbished at Stevens Aviation, South Carolina;
May 2008.
Fireblocked, Nine (9) passenger cabin; Eight (8) place double
club configuration with four (4) foldout tables, aft lavatory is belted
for take-off and landing. Galley is forward right cabin. Headliner and
window panels are beige Ultra-Leather, the lower sidewall is a tan and
black weave fabric and the seats are Beige leather. The carpet is Fawn
wool. Cabinet exteriors are covered with a medium Walnut veneer; metal
accents are Brushed Nickel. Cabin entertainment system has forward left
10.4" cabin bulkhead monitor, Audio International DVD/CD player with a
CD changer.
Exterior
Original paint completed at
Learjet Inc. Tucson, Arizona; April 2004. The fuselage is overall
Matterhorn white with two gold vinyl accents stripes that run from nose
to tail.
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