Centrair (France) Status Subject Detail Reference information TNS Contact; Societe Nouvelle Centrair, Aerodrome – 36300 LE BLANC France. +02 54 37 07 96 (It is recommended to write in French. Some staff speak a little English) DGAC, LBA and EASA Airworthiness Directives Airworthiness Directives; www.osac.aero/cn Centrair 101 - Pegase M Rudder M Tow release guide M Fuselage M Watar ballast M Controls Flight Rudder pedals cracked M Airbrake operating handle M Wheel brake control M Airbrake M Limitations M L’Hotellier connections M Battery A/B & U/C handles M Fixed undercarriages M Flying controls I Manual revisions M Control cables M Flying controls M Flying Controls M L'Hotiller couplings R Seat Harnesses R Rudder pedals R Trim Tab Top rudder hinge cracked AD 1984-113A, SB 101-4 Inspection of fittings and cable AD 1985-002A, SB 101-5 frame inspection AD 1985-021A, SB 101-6 inspection AD 1986-129A, SB 101-7 Control supports AD 1986-128A, SB 101-8 inspect "S" cable guides & tubes SB 101-11 colour fades - replace handle AD 1991-113A, SB 101-12 foul on u/c airbrake handle operated wheel brakes SB 101-15 inspection & mod of control AD 1995-261R3A, SB 101-16R4 Reduced max rough air speed (VRA) and max aerotow (VA ) AD 1993-145R1A, SB 101-17R1 annual check (BGA requires locking pins or sleeves) AD 1997-048A, SB 101-18 Reinforce mount for front battery, new factory supplied part AD 1997-149A, SB 101-19 R1 confusion avoidance fit different shaped handles (minor mod) MM 101-10 inspect for cracks AD 2003-042A, SB 101-20 Aileron hinge pin inspection AD2001-247A, SB101-22 Flight and MM revision status list Cable swaging inspections AD 2002-274A, SB101-23 Modifications to rudder pedals AD 2003-095A, SB101-24 Attachment of Airbrake plastic handle AD 2004-010A, SB101-25 Annual inspections LBA AD 93-001/3 Inspection of harness attachment SB 101-30 Inspection/reinforcement or rudder pedal adjustment tube AD 2010-0099, SB 101-29 Trim tab spring life limitation SB 101-28 12/84 04/85 10/86 04/85 06/91 & 08/96 08/91 10/92 06/94 12/97 06/97 10/98 12/99 06/01 06/01 10/01 12/01 08/03 4-2009 3-2010 2-2011 Page 1 BGA Compendium 05/14 Centrair (France) Status Subject M Inspections Detail Inspections following incidents Reference information AD 2013-0258, SB101-06 r1 Pegase In Service Reports (Advisory) Trim spring failure recurring Tailplane attachment (front) fitting un-bonded, inspect annually Elevator hinge mountings cracks Rudder travel restricted by unsecured instrument pipes & wires Rudder & hook system jam rudder pedal plastic tubes jam on winch hook with rudder adjusted fully forward Air brakes Apply simulated air loads to check paddle mount bolts for jamming Rudder travel restricted by pedal adjustment Elevator Automatic elevator connector bolt too short and nut not in safety TNS 5-2013 12/89 08/90 06/91 04/94 10/97 02/01 10/89 04/05 Centrair 201 A, B & B1-Marianne M Tail plane LE Air brake handle, lower arm M Airbrake operating handles M Aileron mass balance M Elevator control M L’Hotellier connections M Rear canopy M Service life M Flying controls I Manual revisions M Control Cables M Flying controls M Flying Controls M Controls M Controls M Fuselage M Canopy M Controls Page 2 BGA Compendium 05/14 inspect for debonding cracked & failed colour fades, replace handles not secured inspection annual check (BGA requires locking pins or sleeves) Modification required to rear jettison Kit 201BE1580 Extension of service life Aileron hinge pin inspection Flight and MM revision status list Cable swaging instructions Modifications to rudder pedals Inspection of tailplane S/N 201.002>201B072 Inspection and modification to air brake handle Inspection of Airbrake control for cracks Damage inspections to tail boom Canopy jettison mod Air brake lever AD 2002-421A R2, SB 201-06 10/88 SB 201-07 08/90 AD 1991-113, SB 201-09 08/91 AD 1992-088, SB 201-11 06/92 AD 1995-085A, SB201-13 06/95 AD 1997-048A, SB 201-15 12/97 AD 1999-055R1 (A), SB 201-16R1 04/00 AD 1995-060(A)R1, SB 201-12R2 04/01 AD2001-248A, SB201-19 06/01 06/01 AD 2002-272A, SB201-20 10/01 AD 2003-096A, SB201-21 12/01 SB201-06 R3 10/02 AD F2004-010A, SB201-23 BGA 033/11/2002 iss 1 08/03 AD F 2004-008A, SB201-24 08/03 SB201-25 10/03 AD 2003-047A, SB 201-22 AD F 2007-011A, SB 201-30 Centrair (France) Status Subject R Rudder ASW 20F & FL Detail Check correct installation of rudder control linkage Reference information SB 201-32 TNS 2-2011 M Towing Handle of the towing cable release AD 1985-001 (A) (Not available to download) M Flutter - flaps & ailerons check mass balance & backlash AD 1985-19, SB 20-6 04/85 M Structures Checking fuselage frames AD 1985-020 (A) (Not available to download) M Flying controls Flight control supports AD 1986-132R1(A) (Not available to download) M Canopy opening knobs to be painted red SB 20-7 Tow release guide fitting min slack in cable 12 mm SB 20-8 04/85 Aileron vibration correct application & maintenance of tape SB 20-11 & 12 12/87 M Airbrake operating handle colour fades - replace handle AD 1991-113, SB 20-14 08/91 M Wing extensions use suspended until wings are modified to Mod 11 AD 1992-223R1 (A), SB 20-16R1 10/93 M Limitations Reduction of max. rough air speed AD 1993-004(A), SB 20-17 01/93 M L’Hotellier connections annual check (BGA requires locking pins or sleeves) AD 1997-048A, SB 20-19 12/97 M Air brake controls in fuselage weld failure mandatory change of part & annual inspections AD 1995-260R2 (A), SB 20-18R4 04/99 M Flying controls Aileron hinge pin inspection AD2001-246A, SB20-21 06/01 M Control Cables Cable swaging instructions AD 2002-273A, SB20-22 10/01 M Flying controls Modifications to rudder pedals AD 2003-097A, SB ASW20F-23 12/01 M Flying Controls Attachment of Plastic Air brake handle AD F 2004-010, SB ASW20F-24 08/03 ASW 20 F, FL In Service Reports (Advisory) Rudder travel restricted I Manual revisions I Flaps by unsecured instrument pipes & wires Flight and MM revision status list Flap lever spring un seated unable to lock flaps 04/94 06/01 3-2008 Alliance 34 (and SF34B) M Fuselage M Fuselage Page 3 BGA Compendium 05/14 Lifting of BGA restrictions after inspection Inspection to lift flight restrictions BGA 001/05/2000 Iss2 BGA 007/08/2000 Iss 1 08/00 08/00 Status Subject I Manual revisions M Control Cables M Landing Gear M Tow release R Structure M Towing equipment M Canopy M Wings Centrair (France) Detail Flight and MM revision status list Cable swaging instructions Replacement of Wheel Axle Inspection and modification of tow release cable GRP inspections Tow hook positioning Canopy jack attachment Wing root ball joint support inspection Reference information AD 2002-271A, SB34-03 SB34-05 AD F 2004-009A, SB34-07 SB34-08 AD 2002-577A, SB 34-04 AD 2003-043A, SB 34-02 AD 2008-0057-E, SB 34-14 R1 TNS 06/01 10/01 04/03 08/03 02/04 2-2008 Page 4 BGA Compendium 05/14