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MD HELICOPTERS 600N Model Guide

MD HELICOPTERS 600N · Model Guide

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Overview

MD HELICOPTERS 600N is covered here by float, cargo hook and service bulletin documents. No variant-specific spec sheet was supplied. Family-level registry data lists turboshaft power and up to 8 passengers, up to 380 nm range, up to 134 kt cruise and up to 20000 ft ceiling. Library data says piston, which conflicts, so confirm the engine type from the aircraft records.

  • Family-level figures are only 'up to' values: 380 nm range, 134 kt cruise, 8 passengers. They are not confirmed for a specific aircraft.
  • With Apical emergency floats fitted, maximum gross weight is 4100 pounds and water landings have not been demonstrated.
  • Several mandatory service bulletins apply to the 600N: rotor blade root, lead-lag bolts and the tail rotor torque tube.
  • Ask for proof of compliance with each bulletin in the Rotorcraft Log Book compliance record.

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

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Document details

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

Specifications & performance

Extracted from this document.

Specifications

Propulsion class
·
turboshaft
Family max passengers
·
8

Performance

Family max range (nm)
·
380
Family max cruise speed (kt)
·
134
Family max service ceiling (ft)
·
20,000
Max float inflation altitude (ft)
·
6,600

V-speeds

MAX_FLOAT_INFLATION_SPEED_KTS
·
85
MAX_SPEED_FLOATS_INFLATED_KTS
·
100
FERRY_SPEED_FLOATS_INFLATED_KTS
·
100

Weight & balance

Max gross weight floats installed (lb)
·
4,100
About this document
What range and speed does the MD HELICOPTERS 600N have?

The documents give no variant-specific figures. Family-level registry data for the MD HELICOPTERS 600N lists up to 380 nm range, up to 134 kt cruise and up to 20000 ft service ceiling. Verify against the flight manual.

What are the float limits on the MD HELICOPTERS 600N?

With the Apical floats, the MD HELICOPTERS 600N has an 85 KIAS maximum inflation speed, 100 KIAS maximum with floats inflated, and 4100 pounds maximum gross weight. Water landings have not been demonstrated.

Which bulletins should I check on an MD HELICOPTERS 600N?

For the MD HELICOPTERS 600N, check SB600N-071R1 (rotor blade root, every 100 hours), SB600N-073 (lead-lag bolts) and SB600N-080R2 (tail rotor torque tube, 300-hour borescope). Ask for the compliance records.

What is the MD HELICOPTERS 600N Model Guide?

The MD HELICOPTERS 600N Model Guide is a model guide for the MD HELICOPTERS 600N, dated 2026.

What year was the MD HELICOPTERS 600N Model Guide published?

The MD HELICOPTERS 600N Model Guide — the MD HELICOPTERS 600N model guide on file — is dated 2026.

How rare is it?
31MD HELICOPTERS 600N registered worldwide

Common. More common than 56% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the MD HELICOPTERS 600N.

More MD HELICOPTERS 600Nmanuals & documents

In this document

Emergency floats (Apical STC SR00471LA)

Floats are stowed on top of each skid and inflate from a nitrogen vessel when the cyclic handle is pulled. They are for emergency landings only. Maximum inflation speed is 85 KIAS and maximum inflation altitude is 6,600 ft above the landing surface. Over-water operating temperature range is -4° F to +125° F. Takeoff after a water ditching is prohibited.

Cargo hook options

The Onboard Systems dual cargo hook system (STC SR02693LA) is documented for the 600N. Kit P/Ns 200-448-01 and 200-383-01 were added for this model in Revision 3 (08/17/2021). Its Instructions for Continued Airworthiness cover inspection, overhaul schedules and servicing. Check which hook and load-weigh kit is fitted and whether its inspections are current.

Mandatory service bulletins to verify

SB600N-071R1 requires an enhanced 100-hour inspection of the main rotor blade root fittings. SB600N-073 covers main rotor lead-lag bolts P/N 369D21220 with unauthorized plating repairs. SB600N-080R2 requires torque tube inspection, then a borescope check at every 300-hour inspection. Confirm serial numbers and compliance entries.

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

  • Tail rotor torque tube cracking has reduced pedal authority in service. Above 600 flight hours, SB600N-080R2 requires inspection within 5 flight hours.
  • Night flight over water beyond autorotational capability to the ground is prohibited unless the Float Lamp Assembly is installed.
  • After a water landing, inspect the electrical and mechanical components in the lower fuselage and the pitot static system.

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

MD HELICOPTERS 600N Model Guide MD HELICOPTERS 600N is covered here by float, cargo hook and service bulletin documents. No variant-specific spec sheet was supplied. Family-level registry data lists turboshaft power and up to 8 passengers, up to 380 nm range, up to 134 kt cruise and up to 20000 ft ceiling. Library data says piston, which conflicts, so confirm the engine type from the aircraft records. • Family-level figures are only 'up to' values: 380 nm range, 134 kt cruise, 8 passengers. They are not confirmed for a specific aircraft. • With Apical emergency floats fitted, maximum gross weight is 4100 pounds and water landings have not been demonstrated. • Several mandatory service bulletins apply to the 600N: rotor blade root, lead-lag bolts and the tail rotor torque tube. • Ask for proof of compliance with each bulletin in the Rotorcraft Log Book compliance record. Emergency floats (Apical STC SR00471LA) Floats are stowed on top of each skid and inflate from a nitrogen vessel when the cyclic handle is pulled. They are for emergency landings only. Maximum inflation speed is 85 KIAS and maximum inflation altitude is 6,600 ft above the landing surface. Over-water operating temperature range is -4° F to +125° F. Takeoff after a water ditching is prohibited. Cargo hook options The Onboard Systems dual cargo hook system (STC SR02693LA) is documented for the 600N. Kit P/Ns 200-448-01 and 200-383-01 were added for this model in Revision 3 (08/17/2021). Its Instructions for Continued Airworthiness cover inspection, overhaul schedules and servicing. Check which hook and load-weigh kit is fitted and whether its inspections are current. Mandatory service bulletins to verify SB600N-071R1 requires an enhanced 100-hour inspection of the main rotor blade root fittings. SB600N-073 covers main rotor lead-lag bolts P/N 369D21220 with unauthorized plating repairs. SB600N-080R2 requires torque tube inspection, then a borescope check at every 300-hour inspection. Confirm serial numbers and compliance entries. Safety notes: • Tail rotor torque tube cracking has reduced pedal authority in service. Above 600 flight hours, SB600N-080R2 requires inspection within 5 flight hours. • Night flight over water beyond autorotational capability to the ground is prohibited unless the Float Lamp Assembly is installed. • After a water landing, inspect the electrical and mechanical components in the lower fuselage and the pitot static system.