[PDF] Inkraftsetzung Pilatus PC-21



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CONSIGNE DE NAVIGABILITÉ

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Inkraftsetzung Pilatus PC-21

Consigne de Navigabilité (CN) Direttive sulla Navigabilità (DN) Airworthiness Directive (AD) FOCA AD HB-2021-002R1 2/2 Rechtsgrundlage: Art 26, 51 und 51A (Verordnung über die Lufttüchtigkeit von Luftfahrzeugen: SR 748 215 1) Base juridique: Art 26, 51 et 51A (Ordonnance sur la navigabilité des aéronefs: SR 748 215 1)



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Translation of « Consigne de Navigabilité » of same number In case of difficulty, reference should be made to the French issue Direction générale de l’aviation civile France GSAC unless otherwise agreed with the Authority of the State of Registry publication No person may operate an aircraft to which an Airworthiness Directive a pplies,



Direction generale de /Aviation civile Mr Fred GUERIN

Direction technique Navigabilite et Operations Pole methodes, qua lite et competences Reference : 17-072/DSAC/NO/MQC -Paris, on the 21st of July 2017 Dear Sir, This letter aims at informing FAA how, in the context of the Agreement between the UNITED STATES OF AMERICA and the European Community on cooperation in the regulation of

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Federal Department of the Environment, Transport, Energy and

Communications DETEC

Federal Office of Civil Aviation FOCA

Safety Division - Aircraft

Lufttüchtigkeitsanweisung (LTA)

Consigne de Navigabilité (CN)

Direttive sulla Navigabilità (DN)

Airworthiness Directive (AD)

FOCA AD

HB-2021-002R1

Inkraftsetzung

Mise en vigueur

Entrata in vigore

Effective Date

23 February 2021

(same as original issue) Pilatus ± PC-21

FOCA TC/TCDS No: F 56-35

1/2

Rechtsgrundlage: Art. 26, 51 und 51A (Verordnung über die Lufttüchtigkeit von Luftfahrzeugen: SR 748.215.1)

Base juridique: Art. 26, 51 et 51A (Ordonnance sur la navigabilité des aéronefs: SR 748.215.1)

Base giuridica: Art. 26, 51 e 51A (Ordinanza concernente la navigabilità degli aeromobili: SR 748.215.1)

Legal base: Art. 26, 51 and 51A (Ordinance on the airworthiness of aircraft: SR 748.215.1)

Issue Date: 22 February 2021

ATA Chapter(s): ATA 35 ± Oxygen

ATA ± Aircraft Flight Manual

Subject: ATA ± Aircraft Flight Manual / Oxygen Overpressure at the Oxygen

Mask ± Amendment

Supersedure / Revised

AD(s):

This AD revises FOCA AD 2021-002 dated 09 February 2021.

Type Certificate

Pilatus Aircraft Ltd.

Manufacturer(s): Pilatus Aircraft Ltd.

Applicability: Model PC-21 aeroplanes, Manufacturers Serial Numbers (MSN) 101 through MSN 313. Definitions: For the purpose of this AD, the following defintions apply: The applicable Airplane Flight Manual (AFM) Temporary Revision (TR):

Pilatus Aircraft PC-21 AFM TR number: 15-TR-185

Reason: An occurrence was reported where an overpressure at the face mask of the On-Board Oxygen-Generating System on certain PC-21 aeroplanes in operation was detected. This condition, if not corrected, could result in a sudden pressure increase making it difficult or impossible to breath and may prevent the delivery of emergency oxygen. This condition can lead to higher workload and, if occurring at high altitude, exposes the aircrew to the risk of hypoxia. To address this potential unsafe condition, Pilatus issued the AFM TR to introduce a new procedure in Section 3 of the AFM and describes how to deal with an oxygen overpressure at the oxygen mask. For the reason described above, this AD requires amendment of the applicable AFM by incorporating the applicable AFM TR and operating the aeroplane accordingly. This AD is revised to clarify based on which documentation the accom- plishment of this AD has to be done. The generic (global) documentation was approved by the Federal Office of Civil Aviation of Switzerland. The approved content has been transferred by the type certification holder to the customized versions of the applicable AFM TRs.

Lufttüchtigkeitsanweisung (LTA)

Consigne de Navigabilité (CN)

Direttive sulla Navigabilità (DN)

Airworthiness Directive (AD)

FOCA AD

HB-2021-002R1

2/2

Rechtsgrundlage: Art. 26, 51 und 51A (Verordnung über die Lufttüchtigkeit von Luftfahrzeugen: SR 748.215.1)

Base juridique: Art. 26, 51 et 51A (Ordonnance sur la navigabilité des aéronefs: SR 748.215.1)

Base giuridica: Art. 26, 51 e 51A (Ordinanza concernente la navigabilità degli aeromobili: SR 748.215.1)

Legal base: Art. 26, 51 and 51A (Ordinance on the airworthiness of aircraft: SR 748.215.1)

Required Action(s)

and Compliance

Time(s):

Required as indicated below, unless already accomplished:

AFM Change:

Within 30 days after the effective date of this AD, amend the applicable AFM by incorporating the applicable AFM TR, inform all flight crews, and, thereafter, operate the aeroplane accordingly. Ref. Publication(s): Pilatus Aircraft PC-21 AFM TR number: 15-TR-185, Document:

21-A-15-00-00-85A-010A-A, original issue dated 06 November 2020.

The use of any customized versions of the above referenced documenta- tion and/or later approved revisions of this document(s) is acceptable for compliance with the requirements of this AD.

For further information

contact: from:

PILATUS AIRCRAFT LTD.

Customer Technical Support

P.O. Box 992

CH-6371 Stans, Switzerland

Tel.: +41 (0)41 619 3076

E-mail: Techsupport@pilatus-aircraft.com

For further information contact:

FEDERAL OFFICE OF CIVIL AVIATION (FOCA)

Airworthiness Engineering (STIL)

CH-3003 Bern, Switzerland

E-mail: airdir@bazl.admin.ch

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