Prescrizione di Aeronavigabilità

Rif. N.
2014-50 del
07/feb/14
Prescrizione di Aeronavigabilità
Airworthiness Directive
Si allega la Prescrizione di Aeronavigabilità emessa dalla:
Attached the Airworthiness Directive issued by:
Agenzia Europea per la Sicurezza Aerea
European Aviation Safety Agency
Autorità Primaria di Certificazione
Primary Certification Authority
RIFERIMENTO AD
AD Reference
EASA N. 2014-0027R1
COSTRUTTORE
Manufacturer
Dassault Aviation
SOGGETTO
Applicability
Falcon 2000 and Falcon F2000EX aeroplanes
OGGETTO
Subject
Equipment/Furnishings - Tie-downs in forward servicing
compartment - inspection/removal
NOTE
Remark
Cancella la INFO ENAC 2014-46 del 05 febbraio 2014
Nota 1
Il Certificato di Navigabilità dell'aeromobile sulle cui strutture od impianti deve essere applicata la Prescrizione
di Aeronavigabilità a riferimento, scade di validità qualora essa non venga attuata nei termini prefissati.
The Certificate of Airworthiness of the aircraft to which structures and/or systems the referenced Airworthiness
Directive shall be applied expires if the AD is not embodied within specified terms.
Nota 2
Per ulteriori informazioni contattare ENAC Direzione Regolazione Navigabilità e Operazioni
For further information contact ENAC Airworthiness and Operations Regulation Division
email : [email protected]
fax :+390644596731
EASA AD No : 2014-0027R1
EASA
AIRWORTHINESS DIRECTIVE
AD No.: 2014-0027R1
Date : 05 February 2014
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with
Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of
the European third countries that participate in the activities of EASA under Article 66 of that
Regulation.
In accordance with the EASA Continuing Airworthiness Procedures, the Executive Director is proposing the issuance of an EASA
Airworthiness Directive (AD), applicable to the aeronautical product(s) identified below.
All interested persons may send their comments, referencing the PAD Number above, to the e-mail address specified in the ‘Remarks’
section, prior to the consultation closing date indicated.
Design Approval Holder’s Name:
Type/Model designation(s):
DASSAULT AVIATION
Falcon 2000 and F2000EX aeroplanes
TCDS Number :
EASA.A.008
Foreign AD :
Not applicable
Revision :
This AD revises EASA AD 2014-0027 dated 04 February 2014.
ATA 25
Equipment / Furnishings – Tie-Downs in Forward Servicing
Compartment – Inspection / Removal
Manufacturer(s):
DASSAULT AVIATION
Applicability:
Falcon 2000 aeroplanes, serial numbers (s/n) from 1 to 231 inclusive and,
Falcon F2000EX aeroplanes, s/n from 1 to 262 inclusive and s/n from 601 to
604 inclusive.
Reason:
The Forward Servicing Compartment (FSC) of the Falcon 2000 is an
unpressurized service compartment located between fuselage frames 26 and
33. This compartment is accessible from a lockable external door located in
the lower aft fuselage.
A design review has brought to light that the compartment is configured with
tie-down points, which were used by operators to fix loads (e.g. ski or golf
bags) in that compartment. However, the FSC has not been designed and
consequently demonstrated as being compliant with cargo compartment
airworthiness requirements.
This condition, if not corrected, could lead to inadvertent use of the FSC as
cargo compartment, which could result in damage to the structure of the
aeroplane or potential risk of fire.
To address this potential unsafe condition, Dassault Aviation issued Service
Bulletin (SB) F2000-407 and SB F2000EX-289, as applicable, which provide
instructions for removal of the tie-down points.
For the reasons described above, this AD requires removal of the tie-down
points from the FSC.
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
1/2
EASA AD No : 2014-0027R1
Note: Operators are also reminded about the intended function of the FSC.
This AD is revised to clarify the AD Applicability and to correct the TCDS
Number.
Effective Date:
Revision 1 (same as original issue): 18 February 2014
Required Action(s)
and Compliance
Time(s):
Required as indicated, unless accomplished previously:
Ref. Publications:
Dassault Aviation SB F2000-407, initial issue, dated 17 December 2013.
Within 440 flight hours or 9 months, whichever occurs first after the effective
date of the AD, inspect the FSC and, if tie-down points are installed, remove
the tie-down points from the FSC in accordance with the instructions of
Dassault Aviation SB F2000-407 or SB F2000EX-289, as applicable,
depending on aeroplane model.
Dassault Aviation SB F2000EX-289, initial issue, dated 17 December 2013.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
Remarks :
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 19 December 2013 as PAD
13-187 for consultation until 16 January 2014. No comments were
received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Executive Directorate, EASA. E-mail [email protected].
4. For any question concerning the technical content of the requirements in
this AD, please contact your Dassault Falcon Technical Assistance:

For Europe, Middle East and Africa based operators:
Hot Line: (33) 1 47 11 37 37

For USA, Canada and Mexico based operators:
Help Desk: (1) 800-2FALCON (2325266)

All other areas:
Help Desk: (1) 201 541 4747
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
2/2