AIRWORTHINESS
DIRECTIVE
CAA-AD-059/2000R2
Supersedes CAA-AD-059/2000R1
Date of issue: March
20, 2002
APPLIANCE - PASSENGER SEATS (ATA 25) - INSPECTION
Applicability: SICMA
AERO SEAT seats P/N 9lxx, 93xx, 95xx, 96xx, 97xx, 98xx, 99xx, 9Axx, 9Bxx, 9Cxx
equipped with seat belt shackle P/N 95-000500-350-0, 95-000501-350-0,
95-000505-350-0, 61-000502-300-0 or 75-000500-500-0 manufactured before May 31,
2000.
Date
of manufacture can be found on placard P/N 00-5007.
An indicative P/N list is given by Annex
1 to Service Bulletin SICMA AERO SEAT 91-25-032 Revision 2. This list was
updated on July 15, 2000.
These
seats are installed on but not limited to the following aircraft: Airbus
Industrie, ATR, Boeing, Boeing (formerly McDonnell Douglas), Fokker, Let,
Bombardier, Tupolev.
Seats which have already been modified as
per original issue or Revision 1 of Service Bulletin SICMA AERO SEAT 91-25-032
are not affected by Revision 2 of this Airworthiness Directive.
Effective date: May 16, 2002
Compliance: Required as indicated in DGAC AD
2000-214(AB)R2.
Remarks: The compliance of this AD must be recorded
in Aircraft Logbook, where applicable the requirements of this AD must be integrated
into Aircraft Technical Documentation. Address inquiries concerning this AD to:
Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague
6, Czech Republic, tel.: 420 2 33320922, fax: 420 2 20562270.
Ing. Pavel MATOUŠEK
Director of Airworthiness Division
CAA CZ
DGAC AD ref.: 2000-214(AB) R2
SICMA AERO SEAT
Equipment:
passenger seats
Seat belt
attachment fitting (ATA 25)
APPLICABILITY:
SICMA AERO SEAT seats P/N 9lxx, 93xx,
95xx, 96xx, 97xx, 98xx, 99xx, 9Axx, 9Bxx, 9Cxx equipped with seat belt shackle
P/N 95-000500-350-0, 95-000501-350-0, 95-000505-350-0, 61-000502-300-0 or
75-000500-500-0 manufactured before May 31, 2000.
Date
of manufacture can be found on placard P/N 00-5007.
An indicative P/N list is given by Annex
1 to Service Bulletin SICMA AERO SEAT 91-25-032 Revision 2. This list was
updated on July 15, 2000.
These
seats are installed on but not limited to the following aircraft: Airbus
Industrie, ATR, Boeing, Boeing (formerly McDonnell Douglas), Fokker, Let,
Bombardier, Tupolev.
Seats which have already been modified as
per original issue or Revision 1 of Service Bulletin SICMA AERO SEAT 91-25-032
are not affected by Revision 2 of this Airworthiness Directive.
REASONS:
The
fixing bolt of seat belt attachment on several aisle and window side seats has
become loose and later lost and so the seat belt was no more attached to the
seat.
Revision
1 of this Airworthiness Directive introduces precision on the list of affected
seats.
Revision 2 of this Airworthiness
Directive cancels seats in Applicability paragraph.
COMPLIANCE:
1.
Seats manufactured between March 01, 2000 and May 31, 2000.
These
seats have been modified while being manufactured by SICMA. However, indication
of this modification has not been recorded on the seat itself.
On
these seats, before December 31, 2003, stick a placard P/N 00-5179, and record
on it application of Service Bulletin SICMA AERO SEAT 91-25-032.
2.
Seats manufactured before March 01, 2000.
2.1.
Upon effective date of this Airworthiness Directive, if not already
accomplished, within 650 flight hours, check tightening of the affected bolt
onto the seat belt attachment by using a torque wrench as per instructions
given in part one of SICMA AERO SEAT Service Bulletin 97-25-032, Revision 2.
2.2.
Repeat this inspection at intervals not exceeding 650 flight hours.
2.3. Before December 31, 2003, modify
seats as per instructions given in Part two of SICMA AERO SEAT Service Bulletin
91-25-032 Revision 2. This application cancels requirement of repetitive
inspections as per paragraph 2.2. above mentioned.
REF.:
SICMA AERO SEAT Service Bulletin 91-25-032 Revision 2 dated July 06, 2000 (or
further approved revisions).
This Revision 2 replaces AD
2000-214(AB) R1 dated September 20,
2000.
EFFECTIVE DATES:
Original
AD: JUNE 10, 2000
Revision
1: SEPTEMBER 30, 2000
Revision 2: MARCH 16, 2002