(2)
Do an inspection of the component interface and/or the adjacent area.
EFF : ALL
53-35-11Page 433
(3) Examine the fuselage seal profiles (4), the wing seal profiles (5) and/or the seals type 'P' (10), as applicable, for damage.
NOTE : Make sure that you replace the damaged pre-mod seals with the
____ applicable post-mod seals (Ref. SIL 51-008). If a Service Bulletin (SB) is referred to, you must fully embody the applicable SB, before you install the post-mod seal.
(4)
If you must install a new wing seal profile
(Ref. Fig. 410/TASK 53-35-11-991-004)
(a)
Put the wing seal profile (5) and the seal retainer (7) in position at the panel (3).
(b)
Install the screws (9), the washers (8) and the nuts (6).
(5)
Do an inspection of the bonded seals of the panels 191BT (192BT) and 191CT (192CT) for condition. If a seal is defective, do the subsequent repair procedure.
R **ON A/C 003-049, 053-057, 101-101,
Subtask 53-35-11-560-050-B
A. Preparation for Installation:
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Examine the fuselage seal profiles (4), the wing seal profiles (5) and/or the seals type 'P' (10), as applicable, for damage.
NOTE : Make sure that you replace the damaged pre-mod seals with the
____ applicable post-mod seals (Ref. SIL 51-008). If a Service Bulletin (SB) is referred to, you must fully embody the applicable SB, before you install the post-mod seal.
(4) Prepare the panels 191DT (192DT)
(Ref. Fig. 414/TASK 53-35-11-991-005-A)
NOTE : The procedure step (5) is only applicable for the first
____ installation of the panels 191DT (192DT).
(a)
Prepare the foam shim. See view 'B'.
(b)
Apply BONDING COMPOUND PQ10054.040 (Caf.4) to the faces bonded to the seal.
(c)
Install the foam shim in the area between the double lip seal and the seal type 'P'.
(d)
Press the double lip seal together and attach it with tape.
(e)
Let it dry for a half hour.
(f)
Remove the tape.
Panels 191DT and 192DT - Seal Profile Figure 414/TASK 53-35-11-991-005-A
R EFF : 003-049, 053-057, 101-101, 53-35-11 Page 435 May 01/05
CES
(5)
If you must install a new wing seal profile:
(Ref. Fig. 410/TASK 53-35-11-991-004)
(a)
Put the wing seal profile (5) and the seal retainer (7) in position at the panel (3).
(b)
Install the screws (9), the washers (8) and the nuts (6).
(6)
Do an inspection of the bonded seals of the panels 191BT (192BT) and 191CT (192CT) for condition. If a seal is defective, do the subsequent repair procedure.
R **ON A/C 058-099, 102-149, 151-199, 201-299, 301-399, 401-499,
Subtask 53-35-11-560-050-A
A. Preparation for Installation: WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
R EFF : 003-049, 053-099, 101-149, 151-199, 53-35-11Page 436 201-299, 301-399, 401-499, Aug 01/05
CES
(3) Examine the fuselage seal profiles (4), the wing seal profiles (5) and the seals type 'P' (10), as applicable, for damage.
NOTE : Make sure that you replace the damaged pre-mod seals with the
____ applicable post-mod seals (Ref. SIL 51-008). If a Service Bulletin (SB) is referred to, you must fully embody the applicable SB, before you install the post-mod seal.
(4) Prepare the panels 191DT (192DT) (Ref. Fig. 414A/TASK 53-35-11-991-005)
NOTE : The procedure step (5) is only applicable if you install a new
____ panel 191DT (192DT). The procedure is the same for the panels 191DT and 192DT.
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