Airworthiness Directive

AD 97-11-02 R1 63 FR 1737 Active

Federal Aviation Administration · 14 CFR part 39

Requires an inspection to determine the thickness of the intercostal that attaches the third crew member seat to the floor structure in the flight compartment, and replacement, if necessary.

FR document
98-208
Amendment
39-10276
Published
1998-01-12
Effective
1998-02-17
Models covered
1

Last live check: 2026-10-04

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

97-11-02 R1

FR doc 98-208 · 63 FR 1737

AD 97-11-02 R1Published 1998-01-12Effective 1998-02-17

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 an inspection to determine the thickness of the intercostal that attaches the third crew member seat to the floor structure in the flight compartment, and replacement, if necessary.

Full official abstract

This amendment revises an existing airworthiness directive (AD), applicable to certain British Aerospace (Jetstream) Model 4101 airplanes, that currently requires an inspection to determine the thickness of the intercostal that attaches the third crew member seat to the floor structure in the flight compartment, and replacement, if necessary. That action was prompted by a report from the manufacturer indicating that intercostals have been installed that are not of sufficient thickness (and consequent strength) to support the third crew member seat during emergency landing dynamic conditions. The actions specified by that AD are intended to prevent the failure of this intercostal during an emergency landing, which could consequently result in injury to the flight crew. This amendment revises the applicability of the existing AD by removing several airplanes.

More directives for British Aerospace Jetstream 41

  1. AD 2009-16-01 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... Effective 2009-09-09
  2. AD 2009-10-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... Effective 2009-06-11
  3. AD 2009-02-07 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... Effective 2009-03-13
  4. AD 2008-18-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... Effective 2009-03-27
  5. AD 2008-17-04 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... Effective 2008-09-23

All British Aerospace Jetstream 41 directives

Applies to 1 model in our index