AD 81-18-07

final rule
Data completeness: 70%

Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear

AD Number
81-18-07
Status
final_rule
Effective Date
Product Category
appliance
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. | Volpar, Inc. 3N Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. 3NM Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. 3TM Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. C-45G Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. C-45H Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. D18C Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. D18S Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. E18S-9700 Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. G18S Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear
aircraft Textron Aviation Inc. | Volpar, Inc. H18 Airworthiness Directives; VOLPAR, INCORPORATED: Applies to Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear

Unsafe Condition

Main landing gear collapse due to bolt failure of the Walking Beam upper attach bolt P/N AN179-46A.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Visually inspect the main landing gear Walking Beam upper attach bolt P/N AN179-46A for integrity and installation per Volpar Service Bulletin 22. Replace failed bolt with a serviceable part. Remove AN179-46A bolt and install NAS 149-80 bolt within 200 hours or next annual inspection. Inspect NAS 149-80 bolt every 3,000 hours for integrity and replace if needed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Prior to further flight after the effective date of this AD for the initial inspection. The bolt replacement must be done prior to 200 additional hours' time in service or next annual inspection, whichever comes sooner. Subsequent inspections every 3,000 hours' time in service since NAS 149-80 installation.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Beech Models C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P), D18C, D18S, E18S-9700, G18S, H18, JRB-6, 3N, 3NM, and 3TM Aircraft with Volpar Tricycle Landing Gear (STC SA4-1531, SA111WE, SA1832WE or equivalent).

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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