Airworthiness Directive

AD 2005-01-11 70 FR 1329 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-185
Amendment
39-13935
Published
2005-01-07
Effective
2005-02-22
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

2005-01-11

FR doc 05-185 · 70 FR 1329

AD 2005-01-11Published 2005-01-07Effective 2005-02-22

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 you to check the airplane logbook to determine whether any main landing gear (MLG) actuator (part number (P/N) 960.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD requires you to check the airplane logbook to determine whether any main landing gear (MLG) actuator (part number (P/N) 960.30.01.103) with serial numbers (SNs) 830E through 881E is installed. If any MLG actuator with one of these SNs is installed, you are required to replace the MLG actuator with a P/N 960.30.01.103 actuator that has a SN other than 830E through 881E. The pilot is allowed to do the logbook check. If the pilot can positively determine that no MLG actuator with one of these SNs is installed, then no further action is required. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to prevent failure of the MLG actuator caused by an incorrect heat treating process, which could result in loss of hydraulic extension/retraction of the MLG. This failure could lead to loss of control during ground operations.

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