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时间:2011-04-16 10:09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

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
INLET COWL 2. PT2/TT2 PROBE ACCESS DOOR
1. SCREW (8 PLACES)
SEE A
SEE B
A FWD
5. ELECTRICAL CONNECTOR DT867B
4. BOLT
6. ELECTRICAL CONNECTOR3. WASHER DT867A
7. NUT JUMPER 14. BONDING (6 PLACES)
8. WASHER
3. WASHER (6 PLACES)
13. NUT
PT2 SENSE
PT2 SENSE

TUBE
FITTING

12.
9. EEC INLET TOTAL TEMPERATURE/PRESSURE (PT2/TT2) PROBE T867
11. REDUCER
10. PACKING
STUD (6 PLACES)
FWD INLET COWL
B
EEC Inlet Total Temperature/Pressure (PT2/TT2) Probe Installation Figure 401
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 73-21-03
 ALL  ú ú N01 Page 402 ú Dec 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
4) 6G16 SCU ALT PWR ENG 2 5) 6G24 ENG SCU 2 6) 6H21 PROBE HEAT ENG 2 7) 6G17 SCU ALT PWR ENG 3 8) 6G25 ENG SCU 3 9) 6H23 PROBE HEAT ENG 3 10) 6G18 SCU ALT PWR ENG 4 11) 6G26 ENG SCU 4 12) 6H25 PROBE HEAT ENG 4
 (2)  S 864-003-N00Install the DO-NOT-OPERATE tag on the applicable FUEL CONTROL switch.
 (3)  S 014-004-N00Remove the access panel (2) for the PT2/TT2 probe. (a) Remove the screws (1) which attach the access panel (2) to the inlet cowl. (b) Remove the access panel (2) from the inlet cowl.
 (4)  S 034-005-N00Disconnect the electrical connectors DT867B (5) and DT867A (6) from the PT2/TT2 probe (9). (a) Install the caps on the open ends of the electrical connectors.
 (5)  S 034-006-N00Remove the bolt (4), nut (13), and washers (3) which attach the bonding jumper (14) to the PT2/TT2 probe (9).
 (6)  S 034-007-N00Disconnect the PT2 sense tube (12) from the PT2/TT2 probe (9). (a) Install the cap on the open end of the PT2 sense tube (12).
 (7)  S 034-008-N00Remove the nuts (7) and washers (8) which attach the PT2/TT2 probe (9) to the inlet cowl.
 (8)  S 024-009-N00Remove the PT2/TT2 probe (9) from the inlet cowl.
 (9)  S 034-010-N00If you will replace the PT2/TT2 probe (9), do the steps that follow: (a) Remove the reducer (11) from the PT2 sense fitting on the PT2/TT2 probe (9).

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 73-21-03
 ALL  ú ú N03 Page 403 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(b) Discard the packing (10).
 S 034-011-N00
 (10) Install the cap on the PT2 sense fitting on the PT2/TT2 probe (9).
 TASK 73-21-03-404-012-N00
 3. Install the EEC Inlet Total Pressure/Temperature (PT2/TT2) Probe (Fig. 401)
________________________________________________________________
 A. Standard Tools and Equipment
 (1)
Bonding Meter (AMM 20-22-01/601)

 (2)  
Mats - Protection, Rubber Manufacturers Association Grade SC43, Neoprene Sponge, 1 inch (25 mm) thick, approximately 3 X 4 feet (90 X 120 cm) with warning streamers attached (three are ncessary)

 B.
Consumable Materials

 (1)
A00247 Sealant - BMS 5-95 Class B-1/2

 (2)  
A00247 Sealant - Chromate, BMS 5-95, Class B-1/2 (optional to the BMS 5-79)

 (3)
B00148 Solvent - Methyl Ethyl Ketone (MEK), TT-M-261

 (4)  
B00448 Solvent - 1,1,1-Trichloroethane Inhibited, MIL-T-81533 (optional to the MEK)

 C.
Parts


 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 9 | PT2/TT2 Probe | 71-11-01 | 01 | 25 | | | 10 | Packing | | | 245 | 2.....….........…...................................…..........…......…........1
 D. References
 (1)
20-11-15/401, Bonding Jumpers and Ground Leads

 (2)
20-22-01/601, Electrical Bonding
 
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