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BELL 47G-3B-1 Model Guide

BELL 47G-3B-1 · Model Guide

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Overview

BELL 47G-3B-1 is a single-engine piston helicopter in the Bell 47 family. The registry has no variant-specific specs or performance for it, so this guide relies on the service documents. Across the whole family, variants carry up to 4 passengers at up to 2700 kg max takeoff weight. Those are family maximums, not figures for this variant.

  • The BELL 47G-3B-1 airworthiness life limits are in Table 6 of Information Letter 47-00-7 (shared with the 47G-3B).
  • Main rotor blades, pitch horn, steel yoke, collective sleeve and scissors assembly are listed at 5000 hrs.
  • Fan belts are 600 hrs (900 hrs or 5-year shelf life for the -9 set). Main rotor grips are 1200 or 300 hrs.
  • Check the throttle linkage-to-carburetor joint and its safety wire; separation has caused accidents.

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.

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Source

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
47 KB
Copy found at
·
sprinkle.com
About this document
How many people does the BELL 47G-3B-1 carry?

The registry has no seat count for the BELL 47G-3B-1. The Bell 47 family as a whole is listed at up to 4 passengers, which is a family maximum. Confirm the seating in this aircraft's flight manual.

Where are the BELL 47G-3B-1 life limits listed?

The BELL 47G-3B-1 is covered with the 47G-3B in Table 6 of Bell Information Letter 47-00-7 (August 11, 2000). It lists the part numbers and hour lives, with footnotes for some parts. Check that the aircraft records match the current limits.

What should I check on the BELL 47G-3B-1 throttle linkage?

On the BELL 47G-3B-1, check for looseness or axial movement between the carburetor stop arm and the linkage adapter. Also check for clamp screws that are secure and safety wired, and for intact anti-sabotage lacquer. Review the records for ASB 47-15-27 compliance.

What is the BELL 47G-3B-1 Model Guide?

The BELL 47G-3B-1 Model Guide is a model guide for the BELL 47G-3B-1, dated 2026.

What year was the BELL 47G-3B-1 Model Guide published?

The BELL 47G-3B-1 Model Guide — the BELL 47G-3B-1 model guide on file — is dated 2026.

How rare is it?
843BELL 47G-3B-1 registered worldwide · 837 active

Common. More common than 95% of the aircraft models we track.

Documentation completeness
3/7

Most owners only have the POH. Here's the essential set for the BELL 47G-3B-1.

More BELL 47G-3B-1manuals & documents

In this document

Life-limited parts (Table 6)

Listed lives for the 47G-3B-1: main rotor blades 5000 hrs, drag brace 2500 hrs, pitch horn 5000 hrs, gimbal ring -23 4800 hrs, steel yoke 5000 hrs, collective sleeve 5000 hrs, scissors assembly 5000 hrs, engine mount 2500 hrs, shear screw -485-9 1200 hrs. Ask for logbook proof of each part's time in service.

Wear items to price in

Main rotor grips 47-120-252-1, -7 and -11 are listed at 1200 hrs; grip -252-5 is 300 hrs. Tail rotor yoke -126-5 and blades -117-1 and -105 are 2500 hrs. Fan belts 47-661-041-1 through -7 are 600 hrs; the -9 belt is 900 hrs with a 5-year shelf life. Several parts are listed only as on condition or with footnotes, so check each footnote.

Throttle linkage service bulletin

ASB 47-15-27 applies to Scott's Bell 47 helicopters with listed Marvel Schebler carburetors. It follows seven incident/accidents over forty two years from the throttle linkage separating from the carburetor stop arm. It calls for a check of the linkage, clamp screws and 0.032 inch safety wire, then a ground run and flight test after any rework. Confirm in the records that Parts I and II were done.

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

  • Without correct safety wire, the throttle linkage can separate from the serrated shaft and cause loss of throttle control (47G-3 M&O TR 47-16-3).
  • If anti-sabotage lacquer on the throttle joint is found fractured, find the cause and correct it before further flight.
  • The throttle joint splines must be assembled with no lubricant or anti-seize.

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

BELL 47G-3B-1 Model Guide BELL 47G-3B-1 is a single-engine piston helicopter in the Bell 47 family. The registry has no variant-specific specs or performance for it, so this guide relies on the service documents. Across the whole family, variants carry up to 4 passengers at up to 2700 kg max takeoff weight. Those are family maximums, not figures for this variant. • The BELL 47G-3B-1 airworthiness life limits are in Table 6 of Information Letter 47-00-7 (shared with the 47G-3B). • Main rotor blades, pitch horn, steel yoke, collective sleeve and scissors assembly are listed at 5000 hrs. • Fan belts are 600 hrs (900 hrs or 5-year shelf life for the -9 set). Main rotor grips are 1200 or 300 hrs. • Check the throttle linkage-to-carburetor joint and its safety wire; separation has caused accidents. Life-limited parts (Table 6) Listed lives for the 47G-3B-1: main rotor blades 5000 hrs, drag brace 2500 hrs, pitch horn 5000 hrs, gimbal ring -23 4800 hrs, steel yoke 5000 hrs, collective sleeve 5000 hrs, scissors assembly 5000 hrs, engine mount 2500 hrs, shear screw -485-9 1200 hrs. Ask for logbook proof of each part's time in service. Wear items to price in Main rotor grips 47-120-252-1, -7 and -11 are listed at 1200 hrs; grip -252-5 is 300 hrs. Tail rotor yoke -126-5 and blades -117-1 and -105 are 2500 hrs. Fan belts 47-661-041-1 through -7 are 600 hrs; the -9 belt is 900 hrs with a 5-year shelf life. Several parts are listed only as on condition or with footnotes, so check each footnote. Throttle linkage service bulletin ASB 47-15-27 applies to Scott's Bell 47 helicopters with listed Marvel Schebler carburetors. It follows seven incident/accidents over forty two years from the throttle linkage separating from the carburetor stop arm. It calls for a check of the linkage, clamp screws and 0.032 inch safety wire, then a ground run and flight test after any rework. Confirm in the records that Parts I and II were done. Safety notes: • Without correct safety wire, the throttle linkage can separate from the serrated shaft and cause loss of throttle control (47G-3 M&O TR 47-16-3). • If anti-sabotage lacquer on the throttle joint is found fractured, find the cause and correct it before further flight. • The throttle joint splines must be assembled with no lubricant or anti-seize.