A. Aircraft Maintenance Configuration
(1)
Make sure that the flaps and slats are retracted (Ref. TASK 27-50-00-866-009) (Ref. TASK 27-80-00-866-005).
(2)
Before the installation of the SAFETY ROPE - WING (98D57004022000) make sure that:
(a)
The shackle (12) and the rope (6) are attached to the bracket.
(b)
The bolts (9) and the washers (10) are installed on the bracket (11).
(c)
The snap shackle (5) is attached to the rope (6) and the latching ratchet (4).
(d) The shackle (2) is attached to the anchorage-plate (3).
Subtask 12-00-00-941-058
B. Safety Precautions
(1) Put a warning notice in the cockpit, to tell persons not to operate the flap and slat
Subtask 12-00-00-010-050
C. Get Access
(1) Put the ajustable access platform in position at the wing.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 201/TASK 12-00-00-991-001-A) R **ON A/C 151-199, 401-499,
(Ref. Fig. 201A/TASK 12-00-00-991-001-B)
**ON A/C 301-399,
(Ref. Fig. 201B/TASK 12-00-00-991-001-C)
**ON A/C ALL
Subtask 12-00-00-210-052
A. Preparation for Installation
(1) Make sure that the SAFETY ROPE - WING (98D57004022000) is serviceable.
Subtask 12-00-00-481-050-A
B. Installation of the Safety Rope
(1)
Put the SAFETY ROPE - WING (98D57004022000) in position along the wing surface so that:
-
The anchor shackle (2) is on the fuselage side.
-
The bracket (11) is on the wing tip side.
(2)
At the wing tip joint, remove and retain the four aircraft screws.
(3)
Remove the bolts (9) and the washers(10) from the bracket (11).
(4)
Install the bracket (11) with the bolts (9) and the washers (10) at the position of the removed aircraft screws.
(5)
Stow the removed aircraft screws on the bracket (11).
(6)
Remove and discard the self adhesive patch from the fuselage.
(7)
Remove and retain the aircraft plastic plug from the fuselage.
(8)
Install the hoisting lug (1) on the fuselage.
(9)
Attach the anchor shackle (2) to the eye of the hoisting lug (1).
(10) Operate the lever of the latching ratchet (4) to adjust the tension of the rope.
NOTE : There is a risk of damage to the aircraft if the rope is loose
____
or the tension too high.
(11)
Connect the lanyard (8) to the rope (6) and the body harness (7).
(12)
Make sure that:
(a)
The snap shackles on the lanyard (8) are closed.
(b)
When the wing SAFETY ROPE - WING (98D57004022000) is used for long periods, examine the rope tension regularly:
-A loose rope is dangerous.
REPLENISHING - DESCRIPTION AND OPERATION
________________________________________
1. General
_______ This section provides all data for accomplishment of replenishing operations. It is divided as follows:
-FUEL SYSTEM (Ref. ATA 12-11),
-HYDRAULIC FLUIDS (Ref. ATA 12-12),
-OIL (Ref. ATA 12-13),
-GAS (Ref. ATA 12-14),
-WATER (Ref. ATA 12-15),
-TOILET SANITARY FLUID (Ref. ATA 12-16),
-RAIN REPELLENT (Ref. ATA 12-17).
FUEL - DESCRIPTION AND OPERATION
________________________________
1. General
_______
Refer to (Ref. 20-31-00) for data on the types of fuel that can be used.
FUEL SYSTEM - SERVICING
_______________________ TASK 12-11-28-650-001 General Refuel/Defuel Safety Procedures WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON
_______
ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES.
1. Reason for the Job
__________________
The procedure that follows contains information as specified in the IATA Guidance Material on Standard Into-Plane Fuelling Procedures
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-34-24-869-001 Aircraft Grounding for the Refuel/Defuel Operations 28-00-00-910-001 Fuel Safety Procedures 29-10-00-863-002 Pressurize the Yellow Hydraulic System FM 2.04.00 12-11-28-991-001 Fig. 301
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