Airworthiness Directive

AD 2002-21-05 67 FR 64039 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the upper and lower wing spar doublers and angles for cracks at a certain time after the incorporation of Modification Kit B-79 or FAA-approved equivalent, replace any cracked wing spar doubler or angle…

FR document
02-26371
Amendment
39-12911
Published
2002-10-17
Effective
2002-10-23
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2002-21-05

FR doc 02-26371 · 67 FR 64039

AD 2002-21-05Published 2002-10-17Effective 2002-10-23

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to inspect the upper and lower wing spar doublers and angles for cracks at a certain time after the incorporation of Modification Kit B-79 or FAA-approved equivalent, replace any cracked wing spar doubler or angle, and report the results of the inspection to the Federal Aviation Administration (FAA).

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain REVO, Incorporated (REVO) Models Lake LA-4, Lake LA- 4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 airplanes. This AD requires you to inspect the upper and lower wing spar doublers and angles for cracks at a certain time after the incorporation of Modification Kit B-79 or FAA-approved equivalent, replace any cracked wing spar doubler or angle, and report the results of the inspection to the Federal Aviation Administration (FAA). The kit modification consists of installing a doubler kit to give the spar an adequate fatigue life. This AD is the result of an incident of a crack found at the most outboard wing attachment fitting hole on one of the affected airplanes with the modification incorporated. The actions specified by this AD are intended to prevent wing spar failure caused by cracks in the wing spar doublers or angles, which could result in the wing separating from the airplane with consequent loss of control.

More directives for Lake LA-4

  1. AD 2013-08-14 Airworthiness Directives; Revo, Incorporated Airplanes Effective 2013-06-13
  2. AD 2005-12-02 Airworthiness Directives; Revo, Incorporated Models Colonial C-2, Lake L... Effective 2005-07-08
  3. AD 2000-10-22 Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4... Effective 2000-06-20
  4. AD 98-10-12 Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake L... Effective 1998-06-08

All Lake LA-4 directives

Applies to 1 model in our index