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[B747] 求如何换雷达罩 所需工具 注意事项等

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发表于 2010-7-3 18:32:10 | 显示全部楼层 |阅读模式 来自: 中国福建厦门
RT 谢谢大家了
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发表于 2010-7-4 19:44:37 | 显示全部楼层 来自: 中国广东深圳
2.jpg 什么机型的呢
1.733:
TASK 53-52-00-004-001

2. Nose Radome Removal (Figure 401)

A. References

Reference
Title

34-41-11 P/B 401
WEATHER RADAR ANTENNA - REMOVAL/INSTALLATION


B. Procedure

SUBTASK 53-52-00-864-002

(1) Open all WEATHER RADAR circuit breakers on the P6 or the P18 circuit breaker panel.

NOTE: See the Weather Radar System coverage for the airplane (PAGEBLOCK 34-41-11/401).

SUBTASK 53-52-00-034-003

(2) Remove the screws that attach the aft edge of the radome to the clips on the fuselage bulkhead.

SUBTASK 53-52-00-014-045

WARNING: DO NOT OPEN THE NOSE RADOME IF THE WIND IS MORE THAN 15 KNOTS. IF YOU OPEN THE NOSE RADOME IN A WIND, THE RADOME CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.

(3) Open the radome and install the support rods in the hold open brackets on each side.

SUBTASK 53-52-00-034-005

(4) Disconnect one of the two ends of the bonding jumper at the radome hinge.

SUBTASK 53-52-00-024-006

(5) Remove the bolts that attach the hinge arms to the hinge fittings on the radome and remove the radome from the fuselage.

NOTE: When you remove the bolts, prepare to catch the shims that are installed between the hinge arms and the hinge fittings. Look at the installed positions of the shims to help the installation of the same radome.
1.jpg




TASK 53-52-00-404-007
 
 
3.  Nose Radome Installation (Figure 401)
 
 
A.   References
 
 
Reference
Title
 
20-30-11 P/B 201
ADHESIVES, CEMENTS, AND SEALERS - MAINTENANCE PRACTICES
 
20-30-31 P/B 201
CLEANERS AND POLISHES - MAINTENANCE PRACTICES
 
34-41-11 P/B 401
WEATHER RADAR ANTENNA - REMOVAL/INSTALLATION
 
51-31-00 P/B 201
SEALS AND SEALING - MAINTENANCE PRACTICES
 
 
 
B.   Tools/Equipment
 
  NOTE:  When more than one tool part number is listed under the same "Reference" number, the tools shown are alternates to each other within the same airplane series. Tool part numbers that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
 
 
Reference
Description
 
COM-614
Meter - Bonding (Non-Explosion Hazard & Fuel Vapor Areas)
(Part #: 247000, Supplier: 07239, A/P Effectivity: 737-ALL)
(Part #: 247001, Supplier: 07239, A/P Effectivity: 737-ALL)
 
 
 
C.   Consumable Materials
 
 
Reference
Description
Specification
 
A00281
Adhesive - Dow Corning 3145 RTV
MIL-A-46146 (BAC5010, Type 79)
 
B00148
Solvent - Methyl Ethyl Ketone (MEK)
ASTM D740
 
D50004
Compound - Antiseize
BMS3-28
 
 
 
D.   Location Zones
 
 
Zone
Area
 
101
Control Cabin - Left
 
 
 
E.   Prepare the radome for the installation.
 
 
SUBTASK 53-52-00-114-009 
 
  (1)  Make sure the erosion protection is in good condition.
 
 
SUBTASK 53-52-00-434-010 
 
  (2)  Install the hinge brackets, the serrated plates, and the fillers on the radome with attachment screws, and install the brackets.
 
  NOTE:  These brackets can push against the flange of the reinforcement angle.
 
 
SUBTASK 53-52-00-434-011 
 
  (3)  Tighten the bolts.
 
 
SUBTASK 53-52-00-024-012 
 
  (4)  Make sure that you open all WEATHER RADAR circuit beakers on the P6 or the P18 circuit beaker panel.
 
  NOTE:  See the Weather Radar System coverage for the airplane (PAGEBLOCK 34-41-11/401).
 
 
SUBTASK 53-52-00-864-013 
 
  (5)  Hold the radome adjacent to the fuselage bulkhead until the hinge brackets can be engaged with the hinge arms on the bulkhead.
 
 
SUBTASK 53-52-00-434-014 
 
  (6)  Install the shims, where it is necessary, between the hinge brackets and the hinge arms, and install the hinge attachment bolts.
 
 
F.   Procedure
 
 
SUBTASK 53-52-00-024-046 
 
  CAUTION:  YOU MUST BE CAREFUL WHEN YOU LOWER THE RADOME TO THE CLOSED POSITION AFTER THE INSTALLATION OF THE HINGE. IF YOU ARE NOT CAREFUL WHEN YOU LOWER THE RADOME, THE TOP AFT EDGE OF THE RADOME CAN HIT THE FUSELAGE SKIN AND CAUSE DAMAGE.
 
  (1)  Remove the radome hold open support rods and install in the storage clips on the forward pressure bulkhead.
 
 
SUBTASK 53-52-00-414-044 
 
  (2)  Lower the radome carefully to the closed position.
 
 
SUBTASK 53-52-00-214-016 
 
  (3)  Make sure that the top aft edge does not hit the fuselage skin.
 
 
SUBTASK 53-52-00-034-034 
 
  (4)  If you find an interference, do these steps:
 
  NOTE:  Do this procedure as many times as it is necessary to stop the interference between the top and the aft edge of the radome, and the fuselage skin.
 
  NOTE:  Make sure that the seal ends do not touch at the bottom of the bulkhead. There must be an opening of 8.3 to 8.7 inches at the bottom of the bulkhead to allow radome compartment drainage.
 
  (a)  Lift and hold the radome in an open position.
 
  (b)  Loosen the attachment screws of the hinge bracket.
 
  (c)  Move the brackets forward in relation to the radome and tighten the screws.
 
 
SUBTASK 53-52-00-214-036 
 
  (5)  Examine the nose radome seal for rough and damaged areas (PAGEBLOCK 20-30-11/201).
 
 
SUBTASK 53-52-00-214-017 
 
  (6)  Make sure that the seal is bonded to the bulkhead 7 inches on the two sides of the airplane centerline and 2 inches that align each end of the seal.
 
 
SUBTASK 53-52-00-034-018 
 
  (7)  Replace the seal if it is necessary as follows:
 
  NOTE:  If the seal continues to turn down, install the three seal retainers, if they are not installed (detail D) (SB 53-1112).
 
  WARNING:  DO NOT GET solvent, B00148 IN YOUR MOUTH OR EYES, OR ON YOUR SKIN. DO NOT BREATHE THE FUMES FROM SOLVENT. SOLVENTS ARE HAZARDOUS MATERIALS. REFER TO THE PRODUCT MATERIAL SAFETY DATA SHEETS (MSDS) AND LOCAL REGULATORY AGENCY FOR HANDLING PROCEDURES.
 
  (a)  Clean the mating surfaces on the bulkhead with the solvent, B00148 (PAGEBLOCK 20-30-31/201).
 
  (b)  Apply the Dow Corning 3145 RTV adhesive, A00281 to the bulkhead, 7 inches on the two sides of the airplane centerline and 2 inches that align each end of the seal.
 
  (c)  Apply the Dow Corning 3145 RTV adhesive, A00281 to the flat, align part of the seal and install with the flat surface against the bulkhead.
 
  (d)  Permit the Dow Corning 3145 RTV adhesive, A00281 to cure for 24 hours.
 
 
SUBTASK 53-52-00-214-023 
 
  (8)  Examine the attachment clips on the fuselage bulkhead.
 
  NOTE:  Carefully examine the areas adjacent to the hinges, for binding on the radome when you move the radome to closed position.
 
 
SUBTASK 53-52-00-034-022 
 
  (9)  If an adjustment is necessary, do these steps:
 
  (a)  Loosen the attachment bolts on the applicable clips and move the clips inboard.
 
  (b)  Lower the radome to the closed position and install the screws.
 
  (c)  Tighten the screws sufficiently to put the clips into contract with the inner face of the radome, and then remove the screws.
 
 
SUBTASK 53-52-00-864-035 
 
  (10)  Open the radome carefully to prevent movement of the adjusted clips.
 
  NOTE:  If the pressure sealant is moved on the clip attachment bolts, the sealant must be applied to make sure there is sufficient seal (PAGEBLOCK 51-31-00/201).
 
 
SUBTASK 53-52-00-434-024 
 
  (11)  Tighten the clip attachment bolts 100-125 pound-inches.
 
 
SUBTASK 53-52-00-214-026 
 
  (12)  Make sure that the mating surfaces are clean and bright and connect the bonding jumper to the correct attachment at one of the two sides of the radome hinge.
 
 
SUBTASK 53-52-00-764-048 
 
  (13)  Make sure that the bonding resistance between the bonding jumper and the radome is not more than 0.001 ohm. (bonding meter, COM-614)
 
  NOTE:  If a clip is not serviceable, you must remove it and install it after you clean the mating surface between the clip and the structure. You clean it to remove all the sealant or the unwanted material which causes high resistance.
 
 
SUBTASK 53-52-00-214-028 
 
  (14)  With the radome in a closed position, make sure the screw holes of the radome attachment are aligned with the holes in the attachment clips.
 
 
SUBTASK 53-52-00-434-029 
 
  (15)  If the adjustment is necessary, do these steps:
 
  (a)  Put a mandrel or equivalent tool of applicable diameter in the applicable screw holes in the radome and the clip.
 
  (b)  Apply the leverage to move the holes align.
 
  (c)  Make sure not to damage the radome or the clip by use of too much force.
 
 
SUBTASK 53-52-00-434-030 
 
  (16)  Install the screws with the compound, D50004 in the aft edge of the radome. Torque the screws to 120-150 inch-pounds.
 
 
SUBTASK 53-52-00-214-031 
 
  (17)  Make sure the seal engages correctly and the radome clearances are correct.
 
 
SUBTASK 53-52-00-864-033 
 
  (18)  Close all WEATHER RADAR circuit breakers on the P6 or the P18 circuit breaker panel.
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发表于 2010-7-5 01:36:58 | 显示全部楼层 来自: 美国
好详细啊,顶一下!!!
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发表于 2010-7-6 13:37:53 | 显示全部楼层 来自: 中国云南昆明

回 楼主(lynd7) 的帖子

其实有些东西在波音或者空客AMM手册上都可以查到了,只要是民航类的机务人员应该都有各公司的登录账号吧
LZ没有么
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 楼主| 发表于 2010-7-7 12:10:32 | 显示全部楼层 来自: 中国福建厦门
谢谢两位,我还没有账号 呵呵~
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发表于 2010-7-8 11:50:26 | 显示全部楼层 来自: 中国上海
气象雷达系统中雷达罩很重要的,一直不知道如何换的过程,只知道NG换起来比Air bus 麻烦很多,雷达罩好像要专门的地方去修才行的。
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发表于 2010-7-9 21:01:52 | 显示全部楼层 来自: 中国陕西西安
学习学习[s:203]
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发表于 2010-7-9 21:11:17 | 显示全部楼层 来自: 中国贵州六盘水
好详细啊,顶一下!!!
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