2002 ROBINSON R44 RAVEN I

2002

2148

D-HALZ

Used

Important Notice Regarding Current Status & Operational Potential: The comprehensive maintenance and servicing work on this helicopter has been fully completed. The aircraft is finished, fully airworthy, and has 240 remaining hours available until its next major overhaul. As part of the recent maintenance, key components including the fanwheel assembly were replaced with new parts. Additionally, main rotor blades with an extended remaining calendar life have been installed. This allows the helicopter to be operated privately for up to six more years within its remaining hours before the overhaul is due. Overview & Key Specifications: Aircraft Make / Model: Robinson R44 Raven I Registration: D-HALZ Serial Number: 2148 Price: Excl. 19% German VAT Contact & Viewing > The helicopter is ready for immediate inspection and test flights. Complete maintenance history, logbooks, and all EASA Form 1 / FAA Form 8130-3 documents are available.

4,160

Aircraft Total Time (ACTT): approx. 4,160 h (4,159:58 h as of Oct 22, 2026) Remaining Time: 240 operating hours until overhaul Operational Potential: Up to 6 years of private operation within remaining hours

Rotor Blades: Installed blades feature extended calendar life Status: Fully maintained, ready for immediate service, and released under a Certificate of Release to Service (CRS) Rotor & Control Systems Main Rotor Blades: Blades with extended calendar life installed; removed, inspected, and serviced per RHC MM § 28-10, 28-12. Rotor Special Inspection: Completed per Robinson MM § 2.540 Part A. Main Rotor Track & Balance: Flight test completed per RHC § 10.230 (Results: Hover 0.10 IPS; in-flight track within 3/8 inch across all speeds). Swashplate: Cleaned, adjusted, retorqued (friction value: 3.5 lbs), and lubricated per RHC MM § 2.640. Main Rotor Hub: Friction adjusted per RHC MM § 28-32 Part A to 10.5 ft-lb. Control Forks: Upper and lower forks cleaned and friction checked per RHC MM § 2.410 Part 11.

Engine & Ignition System Retard Magneto: Replaced with overhauled unit (P/N 10-600616-3, S/N G-03368) supported by EASA Form 1 (Document M26-0274). Tachometer Magneto: Replaced with overhauled unit (P/N 10-600646-201, S/N E07FA193) supported by FAA Form 8130-3. Engine Inspection: Special inspection performed in accordance with Lycoming SB 369 S. Cylinder Compression Test Cylinder #1: 76/80 Cylinder #2: 79/80 Cylinder #3: 77/80 Cylinder #4: 74/80 Cylinder #5: 77/80 Cylinder #6: 75/80 Valve & Tappet Clearance: Inspections accomplished per Lycoming SB 388C and SB 480F. Oil Analysis: Spectrographic analysis by Spectro Jet-Care from Oct 26, 2026 confirmed normal condition ("NORMAL").

Detailed Breakdown of Maintenance & Work Performed (October 2026) Drive & Cooling System (New Parts) Fanwheel Assembly: Installed new fanwheel (P/N D174-2, REV. P, Lot 776) and dynamically balanced per RHC MM § 6.240 (Result: 0.09 IPS @ 122°). Fanshaft & Bearings: Installed new fanshaft assembly (P/N C007-5, S/N 14035) including new bearing (P/N C181-3 Rev. j). Documentation: All new parts accompanied by FAA Form 8130-3. Additional Maintenance Items Cylinder #4: Installed 2 new thrust buttons on rocker shaft. Ventilation & ELT: Intake hose (P/N A785-11) and ELT antenna connections inspected for security and recorded on Form STH-GMD-004. Foreign Object Debris (FOD): Full inspection performed to clear tools and loose items, and panels secured.

Yes