1989 LEARJET 35A
説明
仕様
年式1989
メーカーLEARJET
モデル35A
シリアル番号650
Registration #N393SC
状態中古
FlightRulesIFR
Total Time17,076.1
Total Landings11,730
Max Takeoff Weight8,890.41 kg
AirframeFRESH 12 YEAR INSPECTION BY SPECTRA JET
Engine 1 Maintenance ProgramNone
Engine 1 Make/ModelHONEYWELL TFE731-2-2B
Engine 1 Serial NumberP-89681
Engine 1 Time16,313.8 SNEW
Engine 1 TBO4200
Engine 1 Cycles Since Overhaul11,161
Engine 1 NotesN1 DEECS
MPI DUE in 855.2
CZI DUE in 765.3
Engine 2 Make/ModelHONEYWELL TFE731-2-2B
Engine 2 Serial NumberP-89682
Engine 2 Time16,293.4 SNEW
Engine 2 TBO4200
Engine 2 Cycles Since Overhaul11,181
Engine 2 NotesN1 DEECS
MPI DUE in 855.2
CZI DUE in 773.4
APU Maintenance ProgramNone
ADS-B Equippedはい
Avionics/RadiosJET FC-530 AUTOPILOT
HONEYWELL TCAS I TPU-66A
GARMIN 1090ES TRANSPONDER
AIRCELL AST-3100 W/2 HANDSETS
DUAL COLLINS ADF-60 ADF
L3 COMMUNICATIONS A100 CVR
UNIVERSAL UNS-1E FMSW/802.X SOFTWARE
RVSM COMPLIANT
HONEYWELL MARK VIII EGPWS/TAWS
KMD-540 MFD DISPLAY
HONEYWELL KDR-510 NEXRAD WEATHER
HONEYWELL RDR-2000 RADAR
DUAL DME-42
DUAL VIR-32 NAVS
TAWS COMPLIANT
DUAL COLLINS VHF-22 COMMS
FMS RNAV 1&2 COMPLIANT
Additional EquipmentDEE HOWARD 4000 TRS
AVCON DELTA FIN STC
RAISBECK ZR LITE STC
HAWKER SECURE PLANE LEAD ACID BATTERIES
R-134A AIR CONDITIONING STC
AVCON INCREASED TAKEOFF. WEIGHT: 19,600 LBS
AVCON INCREASED ZERO FUEL WEIGHT: 14,5000 LBS
AVCON INCREASED LANDING WEIGHT: 16,000 LBS
LEARJET SB FOR LED PARKING BRAKE/ANTI-SKID LIGHTS
ROSENVIEW MOVING MAP
(3) 110V OUTLETS IN CABIN
CABIN A/V ENTERTAINMENT SYSTEM
WHELEN LED ANTI-COLLISION LIGHTING
Year Painted2015
ExteriorOVERALL IRIDIUM WHITE BASE WITH BLACK ACCENT AND RED STRIPING
Year Interior2015
Number of Seats8
Galleyはい
Galley ConfigurationMid
Lavatoryはい
Lavatory ConfigurationMid
Interior2 CREW PLUS 7 PASSENGER SEATING WITH FORWARD FLUSHABLE BELTED LAV
SEAT, (3) FOLDABLE TABLES WITH MONITORS AND A CENTER GALLEY. LIGHT TAN LEATHERS WITH CAMEL CARPETING. UPGRADED LED CABIN LIGHTING FOR BOTH READING & DOWNWASH LIGHTS.
QUICKLY CONVERT BETWEEN PAYLOAD & CHARTER.
Modifications/ConversionsSPECIAL MISSION CAPABILITIES & OPTIONS:
400 AMPS 28VDC DISTRIBUTED ON 2 PDUS
INVERTERS AND CONVERTERS A/R TO PROVIDE 11.2 KW
2 KVA CABIN INVERTER
OMNI MISSION ANTENNAS
• (2) GPS (L1/L2)
• (2) UHF/VHF/L/S-BAND
• (4) UHF/L-BAND
• (2) C/S-BAND BEACON
• L-BAND
• VHF
DIRECTIONAL MISSION ANTENNAS
• (16) EW HORNS (FWD/AFT) UP TO 40 GHZ
• LARGE FWD EW HORN UP TO 6 GHZ
• ILO WEATHER RADAR
PERFORMANCE
• UP TO 45K / .81M / 3G
• 5+ HOURS ON-STATION TIME
• 2100+ NM RANGE WITH IFR RESERVES
3200 LB PAYLOAD (IN ADDITION TO FULL FUEL AND PILOTS)
Inspection StatusPHASE A INSPECTION: C/W AUGUST 2025 @17,076.1
PHASE B INSPECTION: C/W AUGUST 2025 @17,076.1
PHASE C INSPECTION: C/W AUGUST 2025 @17,076.1
PHASE D INSPECTION: C/W AUGUST 2025 @17,076.1
3,000 CYCLE LANDING: C/W MAY 2012 @ 8,995 LANDINGS
6,000 CYCLE LANDING: C/W FEBRUARY 2005 @ 6,023 LANDINGS
12,000-HR INSPECTION: C/W AUGUST 2007 @ 11,635.6
12-YEAR AIRFRAME: C/W AUGUST 2025 @17,076.1 by SPECTRA JET
Airworthyはい