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Robinson R44 Model Guide

Robinson R44 · Model Guide

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Overview

The Robinson R44 is a four-seat, single-engine piston helicopter, in production since 1993. It is FAA-certificated as a normal category rotorcraft under Type Certificate H11NM. This guide covers the limits, loading rules and maintenance items a buyer should check. The Robinson R44 family includes the R44 and R44 II.

  • Four seats, piston engine; the R44 family (R44, R44 II) is listed at up to 350 nm range and 113 kt cruise.
  • Maximum gross weight is 2400 lb. Each seat, including baggage, is limited to 300 lb.
  • Vne is 130 KIAS at 2200 lb or below, and 120 KIAS above 2200 lb.
  • R44 II fuel pumps and pressure relief valves have set replacement intervals. Check the records.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
48 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Max per seat (lb)
·
300
Max gross weight (lb)
·
2,400
Min gross weight (lb)
·
1,550
Max baggage compartment (lb)
·
50

Performance

Family max range (nm)
·
350
Autorotation vne (kt)
·
100
Vne above 2200 lbs (kt)
·
120
Family max cruise speed (kt)
·
113
Vne at or below 2200 lbs (kt)
·
130
Family max service ceiling (ft)
·
14,000
About this document
How many people can the Robinson R44 carry?

The Robinson R44 seats four. Each seat, including baggage, is limited to 300 lb, and maximum gross weight is 2400 lb. Each baggage compartment is limited to 50 lb.

What is the Vne of the Robinson R44?

On the Robinson R44, Vne is 130 KIAS at 2200 lb or below and 120 KIAS above that. It is 100 KIAS in autorotation. Vne also reduces with altitude and temperature per the placard.

What fuel system parts should I check on a Robinson R44 II?

For the Robinson R44 II with a Lycoming IO-540, check the records for the electric fuel pump (replace at 2200 hours TTIS) and the pressure relief valve (12 years or 2200 hours TTIS). Also check the servo thrust washer inspection every 500 hours.

What is the Robinson R44 Model Guide?

The Robinson R44 Model Guide is a model guide for the Robinson R44, dated 2026.

What year was the Robinson R44 Model Guide published?

The Robinson R44 Model Guide — the Robinson R44 model guide on file — is dated 2026.

How rare is it?
5,758Robinson R44 registered worldwide · 5,711 active

Common. One of the most common aircraft types we track.

Documentation completeness
7/7

Full essential library on file for the Robinson R44.

More Robinson R44manuals & documents

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In this document

Weight limits and loading

Maximum gross weight is 2400 lb (1089 kg) and minimum is 1550 lb (703 kg). The limit is 300 lb per seat including baggage, and 50 lb in any baggage compartment. Fuel burn moves the CG forward, so check loading with empty fuel as well as takeoff fuel.

Maintenance records to review

On R44 II helicopters with a Lycoming IO-540, the electric fuel pump P/N D743 must be replaced at 2200 hours TTIS. The pressure relief valve P/N D321-1 must be replaced at 12 years or before 2200 hours TTIS. The RSA-10AD1 fuel servo idle lever thrust washer needs an inspection every 500 hours, unless the terminating kit is fitted.

Equipment and modifications

Check for STC installations and their flight manual supplements. A Tyler camera mount limits Vne to 115 KIAS or the placard speed, whichever is lower. A Garmin G500H installation is limited to VFR only. Any modification means the weight and balance record must be updated.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Safety notes

  • Do not exceed 100 KIAS with any cabin door removed, or at power above maximum continuous power (MCP).
  • The FAA recommends inspecting the hydraulic flight control system. Check the self-locking nuts and attaching fittings are installed correctly.
  • Combined failure of the fuel pressure relief valve and the electric fuel pump could cause a loss of engine performance.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

Robinson R44 Model Guide The Robinson R44 is a four-seat, single-engine piston helicopter, in production since 1993. It is FAA-certificated as a normal category rotorcraft under Type Certificate H11NM. This guide covers the limits, loading rules and maintenance items a buyer should check. The Robinson R44 family includes the R44 and R44 II. • Four seats, piston engine; the R44 family (R44, R44 II) is listed at up to 350 nm range and 113 kt cruise. • Maximum gross weight is 2400 lb. Each seat, including baggage, is limited to 300 lb. • Vne is 130 KIAS at 2200 lb or below, and 120 KIAS above 2200 lb. • R44 II fuel pumps and pressure relief valves have set replacement intervals. Check the records. Weight limits and loading Maximum gross weight is 2400 lb (1089 kg) and minimum is 1550 lb (703 kg). The limit is 300 lb per seat including baggage, and 50 lb in any baggage compartment. Fuel burn moves the CG forward, so check loading with empty fuel as well as takeoff fuel. Maintenance records to review On R44 II helicopters with a Lycoming IO-540, the electric fuel pump P/N D743 must be replaced at 2200 hours TTIS. The pressure relief valve P/N D321-1 must be replaced at 12 years or before 2200 hours TTIS. The RSA-10AD1 fuel servo idle lever thrust washer needs an inspection every 500 hours, unless the terminating kit is fitted. Equipment and modifications Check for STC installations and their flight manual supplements. A Tyler camera mount limits Vne to 115 KIAS or the placard speed, whichever is lower. A Garmin G500H installation is limited to VFR only. Any modification means the weight and balance record must be updated. Safety notes: • Do not exceed 100 KIAS with any cabin door removed, or at power above maximum continuous power (MCP). • The FAA recommends inspecting the hydraulic flight control system. Check the self-locking nuts and attaching fittings are installed correctly. • Combined failure of the fuel pressure relief valve and the electric fuel pump could cause a loss of engine performance.