PC-24

ADs applicable to Swiss registred aeronautical products designed by
PILATUS AIRCRAFT Ltd.

Pertaining to Model: PC-24
TCDS: EASA.A.594
Last update: 12 November 2020

EASA AD	Superseded by	Subject	SB Ref.
EASA 2020-0252 (PDF, 560 kB, 12.11.2020)		Fuel Drain System	28-003R1 (PDF, 2 MB, 23.01.2020)
EASA 2020-0202 (PDF, 597 kB, 22.09.2020)		Airworthiness Limitations Section	refer to Pilatus electronic publication
EASA 2020-0200 (PDF, 563 kB, 21.09.2020)		Integrated Modular Avionics - Utility Management System	42-010 (PDF, 2 MB, 21.01.2020)
EASA 2020-0194 (PDF, 565 kB, 08.09.2020)		Engine Attachment Hardware	71-001 (PDF, 1 MB, 30.06.2020)
EASA 2020-0160 (PDF, 563 kB, 16.07.2020)		Cockpit and Cabin Evaporator Filters	21-006 (PDF, 1 MB, 03.04.2020)
EASA 2020-0158 (PDF, 564 kB, 16.07.2020)		Electrical Harness Installation	91-001 (PDF, 10 MB, 07.04.2020)
EASA 2020-0096 (PDF, 561 kB, 29.04.2020)		Electronic Circuit Breaker	AFM TR No. 02371-016 (PDF, 281 kB, 01.11.2019)
EASA 2020-0074 (PDF, 1 MB, 27.03.2020)	EASA 2020-0202	Airworthiness Limitations Section	refer to Pilatus electronic publication
EASA 2019-0293 (PDF, 496 kB, 04.12.2019)		Emergency Exits / Grommets	25-005 (PDF, 247 kB, 12.08.2019)
EASA 2019-0240 (PDF, 568 kB, 25.09.2019)		Saddle Clamps & Motive-Flow Fuel Pipes	28-002 (PDF, 1 MB, 03.05.2019)
EASA 2019-0166 (PDF, 497 kB, 15.07.2019)		Pitot and Static Electrical Wiring Splices	30-002 (PDF, 287 kB, 03.04.2019)