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DornierTurboprops · England, London, UK

2018 Dornier 228-212NG In United Kingdom

Price
On request
Year
2018
Total time
3,970 hours
Location
United Kingdom
2018 Dornier 228-212NG In United Kingdom, photo 12018 Dornier 228-212NG In United Kingdom, photo 22018 Dornier 228-212NG In United Kingdom, photo 3

Specifications

General

Registration
G-ETAC
Total time
3970
Seats
21
Condition
Pre-owned
Type
Turboprop Aircraft
Sale
aircraft for sale

Description

Aircraft Manufacturer & Model
RUAG Aerospace Services GmbH Dornier 228-212NG
Serial Number / Registration
8321 / G-ETAC
Year of Manufacture
2018
Location
UK
TTAF / Landings
3,971 / 13,220 Landings at 21st December 2025
All Weather Operating Limitation
CAT. 1
Operational Status
In Service (Last ARC 12 Sep 2025)
Cabin
19 Passenger Seats / 2 Crew (Cockpit) Seats / Cockpit & Cabin Hand Fire Extinguishers / Cabin Environmental Control System (ECS)
Engine Manufacturer & Model
Honeywell TPE331-10GP-511D (TBO 5,000 Hours)
Engine S/N (Left Hand)
P-100527
TSN Hours / Cycles
5,629 Hours / 17,850 Cycles at 21st December 2025
TSO Hours / Cycles
1,106 Hours / 3,629 Cycles at 21st December 2025
Due (Limiter)
Due July 2029 approx. (3rd Stage Turbine due October 2026)
Engine S/N (Right Hand)
P-100564
TSN Hours / Cycles
3,971 Hours / 13,220 Cycles at 21st December 2025
TSO Hours / Cycles
Not Applicable
Due (Limiter)
Due November 2026 approx. (3rd Stage Turbine due February 2026)
Propeller Manufacturer & Model
MT-Propeller MTV27-1ECFR(G) (TBO 4,500 Hours / 72 Months)
Propeller S/N (Left Hand)
170496 (Hub)
TSN Days / Hours / Cycles
2,672 Days / 3,971 Hours / 13,220 Cycles
TSO Days / Hours / Cycles
663 Days / 1,106 Hours / 3,629 Cycles
Due
January 2029 approx.
Propeller S/N (Right Hand)
171365 (Hub)
Maximum Take-Off
6,400 kg. (Ref. Ops Manual Part B)
Maximum Landing
6,400 kg. (Ref. Ops Manual Part B)
Maximum Zero Fuel
5,940 kg. (Ref. Ops Manual Part B)
APS – Empty (inc. Crew & Docs)
4,180 kg. (Ref. Ops Manual Part B)
Fuel Capacity
2,417 Ltr. (Ref. POH)
EASA 2019-0307 R1 / May 2025 / Landing Gear
Carbon Brake Assembly Insp. / Replacement
SB-228-332 R0 / Feb 2020 / Wing-Fuselage Cnxn
Inspect for Possible Bearing Displacement
SB-228-345 R0 / Dec 2023 / Ind./Recording Syst.
Display Upgrade EFI-890R (SCN 1025.0.3)
KEY MAINTENANCE EVENTS STATUS (Maintenance Event
Last Done / Next Due)

Description

Introduction

Engines

Propellers

Principal operating weights

Avionics

  • 4 x Universal EFI-890R Advanced Displays
  • King KCP-299 Flight Computer
  • King KDC-298 Air Data Computer
  • CAWS 4802 Computer Unit
  • Dual Collins VHF-4000 Transceivers
  • Becker PA-3100 Amplifier
  • Becker Remote Electronic Unit (REU)
  • EM-6100 Detachable Configuration Module
  • Dual Becker ACU-6100 Audio Control Units
  • L3Harris FA2100 Solid State CVR
  • L3Harris FA2100 Solid State FDR
  • ACR/Artex C406-1 ELT (406 MHz)
  • L3Harris Underwater Locator Beacon
  • Dual Universal Radio Control Units (RCU)
  • Dual Grob-Benz Clocks
  • L3Harris F3000 FDAU
  • Dual AEE ADCU-9000 ADCU
  • Universal DCU-4300 Data Concentrator Units (DCU)
  • Dual Thommen AC-32 Air Data Computers (ADC)
  • Dual LITEF LCR-100 AHRU (28 VDC)
  • Collins ALT-4000 Radio Altimeter Transceiver
  • King ART-2000 Digital Weather Radar Transceiver
  • L3Harris ESI-1000 Standby Indicator
  • Universal TAWS (Class A) Computer (28 VDC)
  • TCAS II w/Change 7.1 Surveillance
  • Dual Collins NAV-4000 Navigation Receivers
  • Collins DME-4000 DME Transceiver (28 VDC)
  • Dual L3Harris NXT-600 Mode S Transponders
  • ADS-B (Out)
  • Universal LP/LPV Monitor (28 VDC)
  • Universal UNS-1EW FMS
  • Universal Solid State Data Transfer Unit (SSDTU)

Ad / sb / mod highlights

  • EASA 2009-0031 R2 / Mar 2024 / (ASB-228-279 R1) Eng. Controls: Throttle Box Assy Inspection
  • EASA 2013-0209 R0 / Jan 2020 / (SB-228-300 R1) Landing Gear: Inspection of MLG Axle
  • SB-228-244 R0 / Oct 2022 / FMS & LPV Monitor SCN Compatibility (ATA: 34-57-00)
  • SB-228-327 R0 / Jul 2022 / Ind./Recording Syst. ADCU Conversion in case of Misleading Indications
  • SB-228-330 R0 / Jan 2020 / Ind./Recording Syst. DCU Configuration Modification for TAWS System
  • 600 Hour: May 2025 @ 3,603 Hours / 4,803 Hours (approx. March 2026)
  • 1,200 Hour: May 2025 @ 3,603 Hours / 4,803 Hours (approx. September 2026)
  • 2,400 Hour: March 2023 @ 2,237 Hours / 4,637 Hours (approx. July 2026)
  • 4,800 Hour: – / 4,800 Hours (approx. September 2026)
  • 1,500 Cycles: May 2025 @ 11,989 Cycles / 13,489 Cycles (approx. January 2026)
  • 12 Month: May 2025 / May 2026
  • 24 Month: March 2024 / March 2026
  • 48 Month: March 2024 / March 2028
  • 72 Month: March 2024 / March 2030

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