• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 16:55来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 radial and 0.59 in. (15 mm) axial
 (4) Nicks, dents, scratches for area E: any  50 cycles/75 hours
 number, less than 0.059 in. (1.5 mm) in
 diameter, protrusion acceptable, not thru
 (5) Nicks, dents, scratches for airfoil out of  50 cycles/75 hours
 area E, not L/E and T/E: any number, less
 than 0.236 in. (6 mm) in diameter, protrusion
 acceptable
 (6) Nicks, dents, scratches out of area E on L/E  50 cycles/75 hours
 and T/E: maximum axial length less than 0.059
 in. (1.49 mm)
 (7) Distorted L/E and T/E, out of area E maximum  50 cycles/75 hours
 circumference equals 0.275 in. (6.98 mm)
 radial length equals 0.708 in. (17.98 mm)
 E. Booster vanes (stage 1 only) for:
 (1) Piece missing:  50 cycles/75 hours
 maximum 20 blades more than 0.256 in. (6.5
 mm) axial, 0.728 in. (18.49 mm) radial, no
 cracks starting from damage area allowed in
 areas A and B
 (2) Cracks and tears in area C, any number, more  10 cycles/15 hours
 than 0.256 in. (6.5 mm) radial and 0.078 in.
 (1.98 mm) axial. In areas A and B, any number

 F 『 EEFF : ALL E Page 67572-00-00
 E E Aug 01/05 ERE
ECES E -------------------------------------------------------------------------------CONDITION MAX EXTENSION -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


more than 0.128 in. (3.25 mm) radial and
 0.039 in. (0.99 mm) axial
 (3) Distortion of T/E and L/E: any number, if the length L is no more than 1 in. (25.4mm) and the maximum dimension X along the chord width is not more than 0.492 in. (12.5mm)

 (4) Nicks, dents, scratches for areas A and B ; any number, less than 0.157 in. (3.99 mm) in diameter, protrusion permitted

 (5) Nicks, dents, scratches for area C: any number, less than 0.295 in. (7.49 mm) in diameter, protrusion permitted

 (6) Nicks, dents, scratches L/E and T/E maximum axial length less than 0.118 in. (2.99 mm) in diameter

 (7) Cracked inner shroud: Maximum of 4 cracks extending from the L/E to the T/E of the inner shroud (passing through a recess) are permitted if there is a minimum separation of 3 non-cracked vane recesses between 2 cracked recesses.


 A sound check (see note below) done on the vanes at, and adjacent to the cracked inner shroud area, must demonstrate no difference in tonality.
50 cycles/75 hours
10 cycles/15 hours
50 cycles/75 hours
20 cycles/30 hours
3000 hours/"C"check
This extension maybe used againindefinitely inintervals of 3000 hours as long as there is no further deterioration of these conditions.
 NOTE : Sound
____ Tonality Check Recommendati A sound tonality check must be done to
 F 『 EEFF : ALL E Page 67672-00-00
 E E Aug 01/05 ERE
ECES E -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


CONDITION MAX EXTENSION
 -------------------------------------------------------------------------------
detect if the abradable material inside the inner shroud is still in contact with the root of the vane. Use a smooth-ended cylindrical tool made of steel with diameter of approximatel
 0.5 in. (12.6999 mm). (For example, a ratchet wrench extension bar). Tools made of aluminium, plastic or wood do not permit the detection of significant variation in the sound tone from one vane to the next. Removal of 2 or 3 fan blades gives a better accessibilit to do the check.
 F 『 EEFF : ALL E Page 67772-00-00
 E E Aug 01/05 E
RE ECES E -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


CONDITION MAX EXTENSION
 -------------------------------------------------------------------------------
Be careful to not use a tool or excessive force during the check. This would damage the vanes.
 Do the check on an area including 3 or 4 vanes on each side of the vane where the cracked inner shroud is located. Place the tool on the leading edge mid-span of the couterclockw most vane. Lightly stroke the vane and subsequent vanes in the clockwise direction using a constant speed. Note any variations in the sound tone from one vane to the next. If there is a
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM ENGINE 发动机 1(56)