Bell 206L, 206L-3, 206L-1, 206L-4, 407 Rotorcraft Flight Manual Supplement

Document Number
121-044-00
Page
1 of 15
Bell 206L/407 Cargo Hook Kit
Rotorcraft Flight
Manual Supplement
FAA APPROVED
ROTORCRAFT FLIGHT MANUAL
SUPPLEMENT
Bell Helicopter Models
206L, 206L-1, 206L-3, 206L-4, 407
R/N ______________ S/N _______________
Document Number
121-044-00
Page
2 of 15
Rev. 0
Bell 206L/407 Cargo Hook Kit
Rotorcraft Flight
Manual Supplement
FAA Approved
INTRODUCTION
This supplement must be attached to the appropriate Bell FAA approved Rotorcraft Flight Manual when an Onboard Systems 200-195-00 or 200-196-00 Cargo Hook Suspension Kit is installed in accordance with Supplemental Type Certificate (STC) NO. SR00418SE. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures and performance information not contained in this supplement, consult the basic Rotorcraft Flight Manual and Rotorcraft Flight Manual Supplement – Cargo Hook issued by Bell Helicopter.
The 200-195-00 and 200-196-00 Cargo Hook Suspension Kits include the cargo hook, suspension beam assembly, and pillow blocks. The suspension beam assembly supports the cargo hook and allows it to align itself with a load. The pillow blocks support each end of the suspension beam assembly and
attach to the rotorcraft’s hard points. In addition the kits
include the external manual release cable and external electrical harness. These items interface with the fixed cargo hook provisions on the rotorcraft.
The 200-196-00 kit includes a load weigh system. The load weigh system consists of a cockpit-mounted indicator, a load cell above the cargo hook, and the interconnecting wiring harness.
Document Number
121-044-00
Page
3 of 15
Rev. 0
Bell 206L/407 Cargo Hook Kit
Rotorcraft Flight
Manual Supplement
FAA Approved

1. LIMITATIONS

1-3. Types of Operation
The basic Rotorcraft Flight Manual and Rotorcraft Flight Manual Supplement – Cargo Hook issued by Bell Helicopter remain applicable. With a load attached to the cargo hook, operation shall be conducted in accordance with the respective national operational requirements. For US operators FAR Part 133 is applicable. This cargo hook is approved for non-human cargo, class B and C rotorcraft load combinations only.
The load weigh indicator (included with kit P/N 200-196-00)
shall be operated in accordance with Section 4 of Owner’s
Manual 120-055-00.
1-20 Placards
When an Onboard Systems kit P/N 200-195-00 or 200-196-00 is installed the following placards apply.
Mounted on suspension beam assembly:
Mounted on the bottom of the cargo hook:
Document Number
121-044-00
Page
4 of 15
Rev. 0
Bell 206L/407 Cargo Hook Kit
Rotorcraft Flight
Manual Supplement
FAA Approved
TURN THE WEIGHING SYSTEM OFF WHEN
NAVIGATION EQUIPMENT IS IN USE. NO AIRCRAFT
OPERATION SHOULD BE PREDICATED ON THE
READING OF THE ONBOARD WEIGHING SYSTEM.
ELECTRONIC WEIGHING SYSTEM
1-20 Placards continued
When an Onboard Systems kit P/N 200-196-00 is installed the following placards apply.
Mounted adjacent to the Onboard Systems load weigh indicator in full view of pilot or co-pilot:
Mounted adjacent to the power switch and the circuit breaker in full view of the pilot and co-pilot.
2. NORMAL PROCEDURES
2-3 Pre-flight Check
Consult the Rotorcraft Flight Manual Supplement – Cargo Hook issued by Bell Helicopters for additional procedures.
Before each Cargo Hook use perform the following procedures. If the procedures are not successful do not use the equipment until the problem has been corrected.
1. Inspect all cargo hook fasteners to ensure that they are
tight.
2. Visually inspect the electrical connector for damage and
security.
3. Operate the cargo hook keeper manually and check that it
snaps back to its normal position on the load beam.
Document Number
121-044-00
Page
5 of 15
Rev. 0
Bell 206L/407 Cargo Hook Kit
Rotorcraft Flight
Manual Supplement
FAA Approved
2. NORMAL PROCEDURES continued
2-3 Pre-flight Check continued
4. Inspect the cargo hook case and covers for cracks and
damage.
5. Inspect the cargo hook load beam for gouges and cracks.
6. Cycle the cargo hook manual release system to ensure
proper operation.
The cargo hook interfaces with the rotorcraft’s internal manual release system as supplied by Bell Helicopter. Consult the Flight Manual Supplement – Cargo Hook for operation of manual release system.
7. Cycle the cargo hook electrical release system to ensure proper operation.
The cargo hook interfaces with the rotorcraft’s internal electrical release system as supplied by Bell Helicopter. Consult the Flight Manual Supplement – Cargo Hook for operation of the electrical release system.
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