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Translation of ‘Consigne de Navigabilité’ ref : 2001-615-062(B) In case of any difficulty, reference should be made to the French original issue December 26, 2001 ATR ATR 72 aircraft 2001-615-062(B) GSAC ATR ATR 72 aircraft Main Landing Gear - Swinging lever spacer (ATA 32) 1 APPLICABILITY:

AIRWORTHINESS DIRECTIVE - Civil Aviation Safety Authority

Translation of ‘Consigne de Navigabilité’ ref : 2001-388-058(B) In case of any difficulty, reference should be made to the French original issue September 05, 2001 ATR ATR 72 aircraft 2001-388-058(B) GSAC ATR ATR 72 aircraft Flight controls - Normal pitch trim switches (ATA 27) 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 05 11 2001 PILATUS - PC-12 FOCA TC/TCDS No : F 56-30 ATA 32 FOCA AD HB 2001-603 TITLE: PILATUS AIRCRAFT LTD – PC-12 MAIN LANDING GEAR – SPECIAL BOLTS - Replacement

20401 HB 2002-546 DGAC Airbus A330

Translation of ‘Consigne de Navigabilité’ ref : 2001-528(B) R1 In case of any difficulty, reference should be made to the French original issue August 21, 2002 AIRBUS A330 aircraft 2001-528(B) R1 GSAC AIRBUS A330 aircraft Thrust reversers - C-Ducts (ROLLS-ROYCE TRENT 700 Engines) (ATA 78) 1 APPLICABILITY:

Bundesamt für Zivilluftfahrt (BAZL) Lufttüchtigkeitsanweisung

Consigne de Navigabilité (CN) Prescrizione di Aeronavigabilità (PA) Airworthiness Directive (AD) Inkraftsetzung Mise en vigueur Entrata in vigore Effective Date 20 08 2001 PILATUS - PC-7 FOCA TC/TCDS No : F 56-20 ATA 32 FOCA AD HB 2001-483 TITLE: PILATUS AIRCRAFT LTD – PC-7 LANDING GEAR EMERGENCY-EXTENSION SELECTOR CABLE APPLICABILITY

Aging Aircraft Program - mitrecaasdorg

Consigne de Navigabilité Atsrac phase 2 (2001-2002) - On-going Aging Aircraft - Systems & Wiring - General 23 SEE5a 956 0503/01 Nov 01 Phase 2 - Conclusion

I +1

AV-2001-06 2/2 This particular rotorcraft was fitted with an electrical ftiel/fiael pressure gauge that was located in the lower left side of the instrument panel The fuel normally indicates 10 to 20 per cent electrical load in flight, wich the indicator needle positioned approximately one needle width above the zero position indication

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The present AD replaces AD 2001-616(A) R1 which will be canceled by its revision 2 REF : New CAP 10B maintenance schedule (issue 1 dated March 01, 2002) GAP 1 OB Service Bulletin N° 16 (CAP 1 OB-57 -004) CONTACTS: Type Gertificate holder: APEX AIRGRAFT, 1 route de Troyes, 21121 DAROIS Fax: +33 3 80 35 65 15, e-mai: airworthineSS(fapex

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