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Localisation d'avion:Mesa, Arizona, États-Unis
Information sur le vendeur
Voir les informations du vendeurGénéral
Année
1983
fabricant
Modèle
Numéro de série
83-23927
Inscription #
N204TM
Etat
Occasion
Description
This is not a typical Black Hawk. In 2018, it underwent the U.S. Military’s highly sought-after UH-60L Lima conversion, transforming it into one of the most capable Black Hawks available with extensive upgrades to the airframe, engines, transmission, and mission systems.
In 2026, it emerged from a three-year, ground-up modernization featuring an all-glass cockpit, Garmin G5000 advanced ACE flight deck, performance and exhaust upgrades, rotor blade enhancements, and numerous additional improvements. The result is an exceptionally rare, mission-ready Lima Black Hawk with capabilities few helicopters can match.
Contact jetAVIVA today to learn more about this extraordinary ownership opportunity.
Cellule
Temps total
6,965.3
Engine 1
Engine 1 Time
6,952 SNEW
Notes moteur 1
T700-GE-701D / GE-E-307799C
T700-GE-701D / GE-E-763826C
APU: Honeywell T62T-40-1
SN: 856225
Hours: 5,989
Engine 2
Engine 2 Time
3,281 SNEW
avionique
Équipé de l'ADS-B
Oui
Avionique / radio
VL-60 Electronic Flight Deck System
ACE DECK VL-60
Garmin G5000H upgrade - Including an integrated flight deck with app-based interface features for pilots
Engine Indicating and Crew Alerting System (EICAS) allowing a Synoptic view of the aircraft systems
COTS IFT and RNAV certified Flight Deck
Synthetic Vision
HTAWS
ADS-B in/out
Matériel supplémentaire
Crochet de chargement
Oui
Équipement additionnel
LIMA Conversion Completed in 2018 by the U.S. Military
AXNES wireless intercom system and three MP30 wireless handsets
Exterior LED lighting System
ELT ME 406HM
Upgraded Straight exhaust pipes
Upgraded Inlet Barrier Filter
Onboard Systems cargo hook with a load weight indicator
BLR Fast Fin Modification (allows an increased useful load of 600lbs and improved stability in hover)
Wires and antennas installed for future installation of a TDFM radio
Wires and control panel installed for HELITAK water tank
Refinished main rotor blade
Main rotor blade DSX coating
Extérieur
Notes extérieures
New custom paint scheme in 2025/26
Intérieur
Notes intérieures
Interior repainted in 2026
Statut d'inspection
Statut de l'inspection
Fresh PMI 1 and 2 and 48 month inspections with new paint, weight reductions, glass cockpit and coated blades
Airframe:
O/B Retention Plate (T/R): 533 hours
Complied with PMI 1, 2 and 48 month inspections
M/R Blade Cuff: 1,560 hours
Main Rotor Spindle Assembly: 2,189 hours
T/R Pitch Change Shaft: 2,229 hours
M/R Blade Cuff: 2,671 hours
Engine 1:
STG 1 FWD Cooling Plate: 1,469 hours
STG 2 AFT Cooling Plate: 1,896 hours
STG 2 FWD Cooling Plate: 2,696 hours
Compressor Impeller: 2,696 hours
STG 3 Turbine Disk: 2,696 hours
Engine 2:
STG 1 FWD Cooling Plate: 1,505 hours
STG 2 AFT Cooling Plate: 1,905 hours
STG 2 FWD Cooling Plate: 2,705 hours
Compressor Impeller: 2,754 hours
STG 3 Turbine Disk: 3,353 hours

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