BELL 204B Model Guide
BELL 204B · Model Guide
Overview
BELL 204B is the 204B variant in Bell's 204 family. Registry data for the whole family lists turboshaft power, up to 16 passengers, up to 4700 kg MTOW, up to 117 kt cruise, up to 300 nm range and a 14000 ft service ceiling. These are family maxima, not BELL 204B figures. No 204B-specific flight manual or performance data was supplied, so confirm the figures against the aircraft's own documents.
- Family-level maxima only (up to 16 passengers, 4700 kg MTOW, 117 kt, 300 nm). No 204B-specific performance was supplied.
- Main rotor blade P/N 204P2100-101 (all serial numbers) needs periodic root-end inspections under AD 2016-23-09.
- The optional Anti-Torque System for external-load cargo hooks is not approved for the Bell 204B.
- The library row says piston but the family data says turboshaft. Verify the actual engine and records.
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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.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 46 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Cargo hook system design load (lb) ·
- 5,000
- Cargo hook mechanical release force (lb) ·
- 18
- Cargo hook system ultimate strength (lb) ·
- 18,750
- Cargo hook electrical release capacity (lb) ·
- 15,000
- Cargo hook mechanical release capacity (lb) ·
- 15,000
What performance can I expect from the BELL 204B?
No BELL 204B-specific performance was supplied. The 204 family shows up to 117 kt cruise, 300 nm range and a 14000 ft service ceiling, as maxima across variants. Use the aircraft's flight manual for real figures.
Is there an airworthiness item on the BELL 204B rotor blades?
Yes. Notice 204-2100-1R3 covers main rotor blade P/N 204P2100-101, all serial numbers, and lists the BELL 204B. It requires inspections per AD 2016-23-09 at the interval specified, recorded in the log book.
Can a BELL 204B use the Anti-Torque System with its cargo hook?
No. The Onboard Systems owner's manual states the Anti-Torque System is not approved for the Bell 204B. It is recommended for spreader-bar loads on approved models, so ask about the intended external-load work.
How is the load released on a BELL 204B cargo hook?
The pilot uses the cyclic release switch. If the electrical system fails, a manual release lever, typically foot operated, is used. Ground crew can also release the load with a lever on the side of the hook.
What is the BELL 204B Model Guide?
The BELL 204B Model Guide is a model guide for the BELL 204B, dated 2026.
What year was the BELL 204B Model Guide published?
The BELL 204B Model Guide — the BELL 204B model guide on file — is dated 2026.
Common. More common than 53% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the BELL 204B.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Main rotor blade root-end inspections
Notice 204-2100-1R3 (12 December 2017) lists the 204B among the models affected. It requires cleaning and visual inspection of the main rotor blades, then repair or replacement depending on findings. It followed a blade found with fatigue cracking around the retention bolt hole. Compliance must be recorded in the Rotorcraft Log Book.
External load and cargo hook
An Onboard Systems non-rotating cargo hook suspension system (STC SR00713SE) is listed for the Bell 204B. Kit design load is 5,000 lb and ultimate strength is 18,750 lb. Release is by cyclic switch, a manual foot lever, or a ground-crew lever on the hook. The optional Anti-Torque System is not approved for the 204B.
What to check before buying
Confirm the engine type and the actual weights and performance from the aircraft's own flight manual, since the supplied data is family-level only. Review the logbook for AD 2016-23-09 blade inspections. If a cargo hook is fitted, check the STC paperwork, the release cable settings and any twist or cracks in the torsion/tension straps.
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Safety notes
- Failure to comply with the blade inspection requirements may result in loss of a main rotor blade in operation and loss of helicopter control.
- Do not use the cargo hook suspension for side pulling such as wire-stringing. The load must be lifted free of land or water.
- A Surefire hook needs the release switch held more than 1/2 second. For an immediate release, use the manual release.
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 204B Model Guide BELL 204B is the 204B variant in Bell's 204 family. Registry data for the whole family lists turboshaft power, up to 16 passengers, up to 4700 kg MTOW, up to 117 kt cruise, up to 300 nm range and a 14000 ft service ceiling. These are family maxima, not BELL 204B figures. No 204B-specific flight manual or performance data was supplied, so confirm the figures against the aircraft's own documents. • Family-level maxima only (up to 16 passengers, 4700 kg MTOW, 117 kt, 300 nm). No 204B-specific performance was supplied. • Main rotor blade P/N 204P2100-101 (all serial numbers) needs periodic root-end inspections under AD 2016-23-09. • The optional Anti-Torque System for external-load cargo hooks is not approved for the Bell 204B. • The library row says piston but the family data says turboshaft. Verify the actual engine and records. Main rotor blade root-end inspections Notice 204-2100-1R3 (12 December 2017) lists the 204B among the models affected. It requires cleaning and visual inspection of the main rotor blades, then repair or replacement depending on findings. It followed a blade found with fatigue cracking around the retention bolt hole. Compliance must be recorded in the Rotorcraft Log Book. External load and cargo hook An Onboard Systems non-rotating cargo hook suspension system (STC SR00713SE) is listed for the Bell 204B. Kit design load is 5,000 lb and ultimate strength is 18,750 lb. Release is by cyclic switch, a manual foot lever, or a ground-crew lever on the hook. The optional Anti-Torque System is not approved for the 204B. What to check before buying Confirm the engine type and the actual weights and performance from the aircraft's own flight manual, since the supplied data is family-level only. Review the logbook for AD 2016-23-09 blade inspections. If a cargo hook is fitted, check the STC paperwork, the release cable settings and any twist or cracks in the torsion/tension straps. Safety notes: • Failure to comply with the blade inspection requirements may result in loss of a main rotor blade in operation and loss of helicopter control. • Do not use the cargo hook suspension for side pulling such as wire-stringing. The load must be lifted free of land or water. • A Surefire hook needs the release switch held more than 1/2 second. For an immediate release, use the manual release.