Airworthiness Directive

AD 97-13-03 62 FR 33543 Active

Federal Aviation Administration · 14 CFR part 39

Requires revising the Airplane Flight Manual (AFM) to prohibit positioning the power levers below the flight idle stop, and to provide a statement of consequences of positioning the power levers below the flight idle stop.

FR document
97-16105
Amendment
39-10049
Published
1997-06-20
Effective
1997-07-25
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

97-13-03

FR doc 97-16105 · 62 FR 33543

AD 97-13-03Published 1997-06-20Effective 1997-07-25

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 Airplane Flight Manual (AFM) to prohibit positioning the power levers below the flight idle stop, and to provide a statement of consequences of positioning the power levers below the flight idle stop.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Gulfstream American (Frakes Aviation) Model G-73 (Mallard) series airplanes, that requires revising the Airplane Flight Manual (AFM) to prohibit positioning the power levers below the flight idle stop, and to provide a statement of consequences of positioning the power levers below the flight idle stop. This amendment is prompted by incidents and accidents involving airplanes equipped with turboprop engines in which the propeller beta was used improperly during flight. The actions specified by this AD are intended to prevent loss of airplane controllability, or engine overspeed and consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.

More directives for Gulfstream G-73 Mallard

  1. AD 2006-01-51 Airworthiness Directives; Frakes Aviation (Gulfstream American) Model G-... Effective 2006-01-17
  2. AD 99-19-07 Airworthiness Directives; Gulfstream American (Frakes Aviation) Model G-... Effective 1999-12-27
  3. AD 98-04-33 Airworthiness Directives; Gulfstream American (Frakes Aviation) Model G-... Effective 1998-03-25

All Gulfstream G-73 Mallard directives

Applies to 1 model in our index