Airworthiness Directive

AD 98-20-34 63 FR 51520 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-25774
Amendment
39-10801
Published
1998-09-28
Effective
1998-11-03
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

98-20-34

FR doc 98-25774 · 63 FR 51520

AD 98-20-34Published 1998-09-28Effective 1998-11-03

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 revising the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for, and procedures for exiting from, severe icing conditions.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Twin Commander Aircraft Corporation Models 500, 500-A, 500- B, 500-S, 500-U, 520, 560, 560-A, 560-E, 560-F, 680, 680-E, 680FL(P), 680T, 680V, 680W, 681, 685, 690, 690A, 690B, 690C, 690D, 695, 695A, 695B, and 720 airplanes. This action requires revising the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for, and procedures for exiting from, severe icing conditions. This AD is prompted by the results of a review of the requirements for certification of these airplanes in icing conditions, new information on the icing environment, and icing data provided currently to the flight crew. The actions specified by this AD are intended to minimize the potential hazards associated with operating these airplanes in severe icing conditions by providing more clearly defined procedures and limitations associated with such conditions.

More directives for Twin Commander (Aero Commander)

  1. AD 2013-09-05 Airworthiness Directives; Twin Commander Aircraft LLC Airplanes Effective 2013-05-29
  2. AD 2009-25-02 Airworthiness Directives; Twin Commander Aircraft LLC Models 690, 690A, ... Effective 2010-01-08
  3. AD 2006-15-01 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... Effective 2006-08-21
  4. AD 2003-07-03 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... Effective 2003-05-16
  5. AD 2000-02-30 Airworthiness Directives; Twin Commander Aircraft Corporation 600 Series... Effective 2000-03-24

All Twin Commander (Aero Commander) directives

Applies to 1 model in our index