£140,531
Posizione dell' Aereomobile:Winnipeg, Manitoba, Canada
Informazioni sul venditore
Visualizza le informazioni sul venditoreAircraft Canada
Contatto:Dallas Nigh
Telefono:+1 587-583-5013
Calgary, Alberta, Canada
Generale
Anno
1980
Produttore
Modello
Numero di serie
31-8052050
Registrazione #
C-GHQF
Condizione
Usati
Normative di volo
IFR
Descrizione
1980 Piper Navajo Chieftain – C-GHQF
Reliable. Versatile. Proven Performer.
Experience the perfect combination of capability and comfort with this well-equipped 1980 Piper Navajo Chieftain. C-GHQF has been meticulously maintained and upgraded, making it an ideal choice for commercial operators, charter companies, or private owners looking for a dependable multi-engine aircraft with strong performance and a comfortable cabin.
Airframe & Powerplant
Total Time: 19,829.2 Hours
Engines: Lycoming TIO-540-J2BD
Left Engine – 1,164.5 Hrs SMOH
Right Engine – 1,211.4 Hrs SMOH
Propellers: Hartzell HC-E3YR-2ATF
Both engines run strong with mid-time hours and excellent performance records — a turnkey workhorse ready to fly.
Avionics & Flight Deck
Garmin GNS 530W & GNS 430W
Garmin GMA 340 Audio Panel
King KFC-200 Flight Director / Autopilot
TAWS-B
GPS 150XL
Dual King KY 96A Comms
Artex 406 MHz ELT
A reliable IFR panel layout offering modern situational awareness and ease of navigation.
Features & Options
Factory Air Conditioning
Cargo Door
Oxygen System
Electric Prop De-Ice
Cleveland Wheels & Brakes
Cabin comfort and operational versatility make this aircraft an excellent utility platform for passenger or cargo operations.
Modifications & STCs
Boundary Layer VG Kit (Super Chief I) – SA00192SE
Landing Weight Increase Kit – SA00202SE
Wing Rib Reinforcement – SA00378SE
RG-24-20 Concorde Battery – SA01147
Performance and safety enhancements for improved handling and increased useful load.
Summary
C-GHQF represents a dependable and proven twin-engine aircraft with excellent performance pedigree. Equipped with upgraded avionics, key STCs, and mid-time engines, this Chieftain is ready for immediate service in passenger, cargo, or utility roles.
A solid investment for operators seeking performance, reliability, and value.
Struttura velivolo
Tempo totale
19,829.2
Peso massimo al decollo
3,175.15 kg
Volume della capacità del combustibile
401.25 L
Complete Logs
Si
Fusoliera
Cleveland Wheel and Brakes
Engine 1
Engine 1 Make/Model
LYCOMING TIO-540-J2BD
Motore 1 Potenza
260.99 kW
Engine 1 Time
1,164.5 SMOH
Motore 1 TBO
1800
Motore 1 Turbocompressore
Si
Engine 2
Engine 2 Make/Model
LYCOMING TIO-540-J2BD
Motore 2 cavalli vapore
260.99 kW
Engine 2 Time
1,211.4 SMOH
Motore 2 TBO
1800
Motore 2 Turbocompressore
Si
Stima
Prop 1 Fabbricante
HARTZELL
Prop 1 Modello
HC-E3YR-2ALTF
Prop 1 Tempo di revisione
1115.3 SMOH
Prop 2 Produttore
HARTZELL
Prop 2 Modello
HC-E3YR-2ATF
Prop 2 Tempo di revisione
1593.1 SMOH
Modifications/Conversions
Generatore di vortici
Si
Modifiche/Conversioni
Boundary Layer VG Kit (Super Chief I) – SA00192SE
Landing Weight Increase Kit – SA00202SE
Wing Rib Reinforcement – SA00378SE
RG-24-20 Concorde Battery – SA01147
Performance and safety enhancements for improved handling and increased useful load.
Avionica
WAAS
Si
Avionica/Radio
Garmin GNS 530W & GNS 430W
Garmin GMA 340 Audio Panel
King KFC-200 Flight Director / Autopilot
TAWS-B
GPS 150XL
Dual King KY 96A Comms
Artex 406 MHz ELT
Attrezzatura Aggiuntiva
Sistema di ossigeno
Si
Air Conditioning
Si
Attrezzature aggiuntive
DWG Known Icing
Factory Air Conditioning
Cargo Door
Oxygen System
Electric Prop De-Ice
Cleveland Wheels & Brakes
Stato Ispezione
Idoneo alla navigazione aerea
Si

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