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Airworthiness Directive

AD 98-19-15 R1 65 FR 1540 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc.

Superseded by AD 2007-16-03Federal Register (opens in a new tab)

FR document
00-537
Amendment
39-11507
Published
2000-01-11
Effective
2000-03-03
Models covered
1

Last live check: 2026-10-04

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AD

98-19-15 R1

FR doc 00-537 · 65 FR 1540

AD 98-19-15 R1Published 2000-01-11Effective 2000-03-03

Superseded by 2007-16-03 Revises 98-19-15

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc.

Full official abstract

This amendment revises Airworthiness Directive (AD) 98-19-15, which currently requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes equipped with Barber- Colman pitch trim actuators, part number (P/N) 27-19008-001/-004 or P/N 27-19008-002/-005. Since AD 98-19-15 became effective, improved design pitch trim actuators have been developed that, when installed, will eliminate the speed restriction and minimum pilot requirements of the current AD. This AD requires incorporating these installations as a method of complying with the current AD. The actions specified by this AD are intended to lessen the possibility of airplane pitch up caused by mechanical failure of the pitch trim actuator, which could result in a pitch upset and structural failure of the airplane.

More directives for Fairchild SA226/SA227 Metro

  1. AD 2021-01-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2021-02-26
  2. AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes Effective 2017-05-05
  3. AD 2016-25-12 Airworthiness Directives; M7 Aerospace LLC Effective 2017-01-12
  4. AD 2016-15-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-08-26
  5. AD 2016-10-01 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-06-15

All Fairchild SA226/SA227 Metro directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 98-19-15 R1 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index