|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
F-1982-136-014R1
|
|
1986-06-25
|
Installation of a system for holding the horizontal stabilizer flanges
|
|
1986-07-02
|
|
|
D-1986-149
|
|
1986-06-25
|
Tail Rotor Gear Box- Attachment Bolts P/N LN 9037-10040
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
1986-06-25
|
|
|
F-1986-074
|
|
1986-06-25
|
Fuselage Frame 35 Reinforcement at the level of the Baggage Compartment Floor
|
|
1986-07-02
|
|
|
ES-212-76-03R1
|
|
1986-06-20
|
Accomplish CASA SB 212-76-03 Revision 1
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1986-06-20
|
|
|
ES-212-55-06R5
|
|
1986-06-20
|
Accomplish CASA SB 212-55-06 Revision 5
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1986-06-20
|
|
|
ES-212-79-03R2
|
|
1986-06-20
|
Accomplish CASA SB 212-79-03R2
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1986-06-20
|
|
|
US-86-11-06
|
|
1986-06-04
|
SUPERSEDED BY FAA AD 2001-08-02
|
|
1986-07-14
|
|
|
G-006-06-86
|
|
1986-06-01
|
Auto Flight - To alter electrical wiring from circuit breaker No 49 and No 252.
|
|
1986-06-01
|
|
|
G-011-06-86
|
|
1986-06-01
|
Fuel - To introduce a strengthened valve spindle in 1 inch actuated ball valves fitted to fuel, hydraulic and water methanol shut-off valves.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1986-06-01
|
|
|
G-005-06-86
|
|
1986-06-01
|
Flying Controls - To introduce positive locking to aileron drive quadrant stud securing nut.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1986-06-01
|
|
|
US-86-05-02
|
|
1986-05-28
|
UNITED INSTRUMENTS, INC. - Altimeter - Test / Replacement
|
|
1986-03-01
|
|
|
F-1985-189-046R1
|
|
1986-05-28
|
Main rotor shaft (all part numbers)
|
|
1986-06-04
|
|
|
F-1986-085-002R1
|
|
1986-05-28
|
Oil cooling system
|
|
1986-05-28
|
|
|
F-1986-035-028R1
|
|
1986-05-25
|
Main rotor head - Roving sleeve beams
|
|
1986-07-16
|
|
|
ES-212-32-02R3
|
|
1986-05-05
|
Accomplish CASA SB 212-32-02 Revision 3
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1986-05-05
|
|
|
ES-212-28-11R3
|
|
1986-05-05
|
Accomplish CASA SB 212-28-11 Revision 3
|
-
AIRBUS DEFENCE & SPACE S.A.
|
1986-05-05
|
|
|
G-006-05-86
|
|
1986-05-01
|
IPECO EUROPE - Equipment/Furnishings – Pilot/Co-Pilot Seat – Inspection/ modification of the seat back disconnection mechanism.
|
-
APPLIANCES
-
ATA 25 EQUIPMENT / FURNISHINGS
|
1986-05-01
|
|
|
G-004-05-86
|
|
1986-05-01
|
DOWTY ROTOL - Landing Gear – Nose undercarriage – Inspection of forward facing section of main fitting.
|
-
APPLIANCES
-
VIKING AIR LTD
|
1986-05-01
|
|
|
G-005-05-86
|
|
1986-05-01
|
Flight Controls - To prevent incorrect installation of aileron control lever and rods.
|
|
1986-05-01
|
|
|
G-003-05-86
|
|
1986-05-01
|
CANCELLED: Flight Controls - Flaps control system - To introduce Dowty Rotol Modification 146/F/198 to flap torque limiter units 676201007, 676201008 and 676201009.
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
1986-05-01
|
|
