This 1992 Airbus AS355 N (Twin Engine) is presented alongside its 1997 counterpart as part of a package sale. While currently not airworthy, the helicopter retains substantial value in its components and presents an attractive opportunity for restoration, spares, or part-out operations. It features dual Safran Arrius 1A engines (S/N 2007 and 2048) with Engine 1 TT 1,571 h / CY NG 1,970 / CY NTL 2,550 and Engine 2 TT 2,500 h / CY NG 3,486 / CY NTL 4,627. The airframe totals 1,631 hours with 5,939 take-offs recorded. The AS355 N platform is well-known for its durable airframe, twin-engine redundancy, and versatility in utility, corporate, and surveillance roles. With proper inspection and compliance work, HK-4926 can be returned to service or leveraged for high-value component support. Highlights: Twin Safran Arrius 1A engines installed Valuable for restoration or component recovery Detailed technical status available upon request Note: This helicopter is sold exclusively as part of a package with the 1997 AS355 N (HK-4795). They will not be sold separately. Specifications last updated October 14, 2025 – Full status available upon request.

This 1997 Airbus AS355 N (Twin Engine) offers proven reliability, a spacious composite fuselage, and a lightweight design ideal for passenger, utility, or corporate missions. Equipped with dual Safran Arrius 1A engines and a total airframe time of 3,442 hours over 12,768 takeoffs, this helicopter remains in airworthy condition, maintained under professional oversight with full technical records available. The AS355 N provides a maximum take-off weight of approximately 2,600 kg, a service ceiling around 11,200 ft, and a cruise speed near 118 KT with a range of about 312 NM—delivering an excellent balance between performance, economy, and reliability. Engine 1 (SN 2195) totals 3,397 hours, while Engine 2 (SN 2198) totals 2,817 hours with respective cycle counts of CY NG 4,404 / 2,716 and CY NTL 5,302 / 4,884. Highlights: Fully airworthy condition Dual Safran Arrius 1A engines Spacious cabin and composite fuselage Maintained and ready for immediate operation Note: This helicopter is being sold as part of a package together with its 1992 counterpart (HK-4926). Individual sale is not available. Specifications last updated October 14, 2025 – Full status available upon request.

The 1979 Twin Commander 690B II is a proven high-performance turboprop renowned for its speed, reliability, and versatility. Designed for both business and personal travel, it offers excellent short-field capability, efficient operating economics, and a spacious, comfortable cabin. Equipped with powerful Honeywell TPE331 engines, the 690B II delivers impressive cruise performance, range, and climb rates, making it a standout in its class. With its rugged build quality and enduring reputation, this aircraft remains a dependable choice for operators seeking a balance of performance, comfort, and value.

General Specs Passenger Seats: 50 Configuration: Commuter – Forward Galley / Aft Lavatory Interior: New Carpet & Upholstery (Refurbished) Exterior: White Paint Scheme (Recent Application) Avionics Suite: Honeywell Maximum Certified Weights Max Takeoff Weight: 22,600 kg / 49,810 lbs Max Landing Weight: 19,800 kg / 43,639 lbs Max Zero Fuel Weight: 18,400 kg / 40,553 lbs Max Taxi Weight: 22,700 kg / 50,030 lbs Engines – Rolls-Royce AE3007A1P LEFT ENGINE (CAE-310125): TSN: 42,032.95 Hrs | CSN: 33,659 TSLSV: 2,298.75 Hrs | CSLSV: 2,049 Limiting Component: 11th Stage Compressor Wheel (4,201 FC remaining) RIGHT ENGINE (CAE-312010): TSN: 37,088.71 Hrs | CSN: 31,422 TSLSV: 2,042.59 Hrs | CSLSV: 1,833 Limiting Component: HPT Spacer (5,433 FC remaining) Avionics & Systems ADS-B Out – Honeywell (2x, PN: 7510733-623) TCAS 7.1 – Honeywell EGPWS – Honeywell FMS V6.1 – Honeywell (2x) GPS – Honeywell CVR – Allied Signal FDR – Honeywell ELT – Artex Modifications and Service Bulletins Cockpit security door installed (STC ST01409LA – January 2003) Coffee brewers installed (STC ST09858SC – July 2004) Bleed system insert installed (STC ST03994A – February 2015) MiniQAR installed (STC ST02472AT – June 2015) ADS-B Out installed (EMB SB 145-34-0118 – May 2015) FADEC upgraded to software version B9.4.1 (EMB SB 145-73-0043 – April 2016) Nose landing gear modifications for increased weight (EMB SB 145-32-0111 Rev.04 – September 2017) Structural reinforcement for increased weights (EMB SB 145-53-0068 – September 2017) Aircraft modified to meet increased MTOW and MZFW (EMB SB 145-00-0032 – September 2017) FMS upgraded from NZ 5.2 to NZ 6.1.1 (March 2025) Maintenance Status 2A Check performed at 42,176.52 hours – 208.75 hours remaining 2C Check last done at 37,496.22 hours – 5,471.55 hours remaining 30-Month Check last done at 44,931.55 hours – 1,963.78 hours remaining 3C Check due at 57,431.55 hours – 14,463.78 hours remaining 4A Check last done at 44,431.55 hours – 1,463.78 hours remaining 48-Month Check due December 2026 60-Month Check due August 2027 120-Month Check due August 2032 Landing Gear Status Nose gear last overhauled August 2024 – 20,000 flight cycle interval Left main gear last overhauled July 2019 – 20,000 flight cycle interval Right main gear overhaul data not listed Shock absorber life limited to 14,949 flight cycles or 47.5 months Features & Highlights Fresh interior upgrades completed White paint scheme in excellent condition Fully ADS-B Out compliant FMS and FADEC software upgrades completed Weight increase modifications implemented Well-maintained with full records available