AD 75-22-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | B-N Group Ltd. | BN2A MK. III | Airworthiness Directives; Britten Norman Ltd Model BN-2A Mark III airplanes, all series Airplanes |
| aircraft | B-N Group Ltd. | BN2A MK. III-2 | Airworthiness Directives; Britten Norman Ltd Model BN-2A Mark III airplanes, all series Airplanes |
| aircraft | B-N Group Ltd. | BN2A MK. III-3 | Airworthiness Directives; Britten Norman Ltd Model BN-2A Mark III airplanes, all series Airplanes |
Unsafe Condition
Cracks in the rudder trim jack lower mounting brackets and rudder structure could lead to possible loss of rudder trim control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the rudder trim jack lower mounting brackets and rudder structure for cracks in accordance with Service Bulletin BN-2/SB.62 before first flight each day. Replace cracked parts with same part number or FAA-approved equivalent before further flight. Modify the rudder trim jack lower mounting bracket and rudder structure per Modification Leaflet BN-2/NB/M/596 within 300 hours' time in service after AD effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the first flight of each day after the effective date of this AD; within the next 300 hours' time in service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
B-N Group Ltd. Model BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3 airplanes, all series, certificated in all categories.
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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