AIRWORTHINESS DIRECTIVE - Civil Aviation Safety Authority
Translation of ‘ Consigne de Navigabilité’ ref : 2003-106(B) R1 In case of any difficulty, reference should be made to the French original issue April 16, 2003 ATR ATR 42 and ATR 72 aircraft 2003-106(B) R1 GSAC ATR ATR 42 and ATR 72 aircraft Flight controls - Stand by pitch trim switch (ATA 92) 1 APPLICABILITY:
Bundesamt für Zivilluftfahrt (BAZL) FOCA AD Office fédéral de
Consigne de Navigabilité (CN) Prescrizione di Aeronavigabilità (PA) Airworthiness Directive (AD) Inkraftsetzung Mise en vigueur Entrata in vigore Effective Date 17 February 2003 PILATUS - PC-6 FOCA TC/TCDS No : F 56-10 ATA 57 FOCA AD HB 2003-092 TITLE: PILATUS AIRCRAFT LTD – PC-6 INTEGRAL FUEL TANK RIB ASSEMBLIES - Inspection/Repair
FOCA AD Lufttüchtigkeitsanweisung (LTA) Consigne de
Consigne de Navigabilité (CN) Prescrizione di Aeronavigabilità (PA) Airworthiness Directive (AD) HB Inkraftsetzung Mise en vigueur Entrata in vigore Effective Date 15 September 2003 PILATUS - PC-7 FOCA TC/TCDS No : F 56-20 ATA 28 FOCA AD 2003-392 Supersedes HB 2001-505 TITLE: PILATUS AIRCRAFT LTD – PC-7
AIRWORTHINESS DIRECTIVE
December 10, 2003 Page : 1/7 This Airworthiness Directive is published by the DGAC : générale X on behalf of EASA, the Primary Airworthiness Authority for the affected product as the Registration Airworthiness Authority for the affected aircraft Direction de l’aviation civile France Translation of « Consigne de Navigabilité » of same
SERVICE DIFFICULTY ALERT DIFFICULTÉS EN SERVICE
La consigne de navigabilité 89-25-10 de la FAA et la consigne CF-1981-25R6 de Transports Canada exigent de porter une attention particulière à cette région pour un nombre limité d’avions dont le numéro de série figure dans les consignes Cette cirque s’est produite sur un avion qui n’était pas visé par ces consignes
(LDP)
25-09-2003 00:59 GSAG: 0146904840 Page 003/003 Further to observations on the involved aircraft, revision 1 of this AD (ref 2001-616(A) R1) enforced new detailed inspections (upper spar flange, lower spar flange and landing gear attachment blocks)
AIRWORTHINESS DIRECTIVE Issue date
3 1 A300B4-600 and A300C4-600 aircraft without trim tanks (repeat of AD 2003-085) 3 1 1 Integrity inspection and detailed visual inspection program: Within 15 days following February 20th, 2003 (effective date of AIRBUS AOT A300-600-28A6075), check the integrity of the center fuel tank pump canisters and bodies and perform a detailed
LUFTDYKTIGHETSPABUD 1111r:::::;::::::;:::::::
2003-069 UTSKIFTING AV GLIDER OG STYRELINER Påbudet gjelder: Alle Paraehutes de Prance SA (PDP) TECHNO 240, PIN ROl-240-0 nødfallskjermer som beskrevet i vedlagte kopi av DGAC AD 2003-301(A) Påbudet omfatter: Utfør tiltak som beskrevet i vedlagte kopi av DGAC AD 2003-301 (A) Anm : Denne LDP erstatter og opphever LDP 2003-055 Tid for
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