Airworthiness Directive

AD 2001-11-02 66 FR 30300 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-13580
Amendment
39-12243
Published
2001-06-06
Effective
2001-07-23
Models covered
1
Last live check
2026-10-01
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

2001-11-02

FR doc 01-13580 · 66 FR 30300

AD 2001-11-02Published 2001-06-06Effective 2001-07-23

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 modifying the generator 2 excitation by removing certain diodes and installing a new 5-amp circuit breaker and suppression filter on certain Pilatus Aircraft Ltd.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 99-17- 08, which currently requires modifying the generator 2 excitation by removing certain diodes and installing a new 5-amp circuit breaker and suppression filter on certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD is the result of the Federal Aviation Administration's determination that the A250 voltage spike suppression filter in the modification kit can cause the circuit breaker 235 to trip because of overload. In extreme circumstances, this can lead to overheating of wiring. This AD requires you to modify the generator 2 excitation by removing certain diodes and installing a new 5-amp circuit breaker and suppression filter of improved design in accordance with revised procedures. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent damage to electrical components if generator 2 is not switched off before engine shutdown and it overheats. This could result in loss of electrical power to certain critical airplane components.

More directives for Pilatus PC-12

  1. AD 2026-15-12 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-08-28
  2. AD 2026-15-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-07-30
  3. AD 2026-12-01 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-06-09
  4. AD 2024-08-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2024-04-29
  5. AD 2023-12-17 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2023-07-03

All Pilatus PC-12 directives

Applies to 1 model in our index