42 lines
13 KiB
Markdown
42 lines
13 KiB
Markdown
## PW11
|
||
### 80-11-00 Starting
|
||
80-11-00-03
|
||
Fill Starter with Oil 80-11-00-600-801-A
|
||
Fill 473ml - 591ml (16fl.oz. - 20fl.oz.)
|
||
|
||
80-11-01 Starter
|
||
80-11-02 MagPlug
|
||
80-11-03 Start Valve
|
||
80-11-04 Speed Sensor
|
||
### 80-11-49 Starter Duct
|
||
#### Inspection GVI LWR STARTER DUCT
|
||
Ref. AMM 80-11-00-210-801-A
|
||
[TASK](https://airnavx.lht.ham.dlh.de/airnavx/document/635628_SGML_C/toc?itemId=635628_SGML_C_EN80114900080200&itemType=DATAMODULE&wc=actype:A318;actype:A319;actype:A320;actype:A321;customization:DLH;doctype:AMM;tailNumber:N10304)
|
||
|
||
![[lwr_starter_duct.png]]
|
||
|
||
| | | |
|
||
| --------------------------------------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||
| Lower duct cracks around the clevis weld seam | If the total crack length is equal to 1.50 in. (38.10 mm) or less. Do an inspection of the crack every 1000 flight cycles to measure the crack length | Permitted (continue in service). |
|
||
| | If the total crack length is equal to 2.30 in. (58.42 mm) or less but more than 1.50 in. (38.10 mm), continue in service. Do an inspection of the crack every 500 flight cycles to measure the crack length | Permitted (continue in service). |
|
||
| | If the total crack length is equal to 3.00 in. (76.20 mm) or less but more than 2.30 in. (58.42 mm), continue in service. Do an inspection of the crack every 100 flight cycles to measure the crack length | Permitted (continue in service). |
|
||
| | If the total crack length is more than 3.00 in. (76.20 mm)<br><br>Ref. Fig. Total Crack Permitted | Not permitted (Remove the duct from service within ten flight cycles) [Ref. AMM TASK 80-11-49-000-802](https://airnavx.lht.ham.dlh.de/airnavx/document/635628_SGML_C/toc?itemId=635628_SGML_C_EN80114900080200&itemType=DATAMODULE&wc=actype:A318;actype:A319;actype:A320;actype:A321;customization:DLH;doctype:AMM;tailNumber:N10304) and Ref. AMM TASK 80-11-49-400-802. |
|
||
|
||
| | | |
|
||
| ------------------ | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
|
||
| Round bottom dents | Dents in zone 1 that are less than 0.100 in. (2.540 mm) in depth and 3.000 in. (76.200 mm) or more to the nearest edge of a different dent are permitted | Permitted. |
|
||
| | Dents in zone 1 that are 0.100 in. (2.540 mm) in depth and less than 0.250 in. (6.350 mm), and more than ten times the depth across, and 3.00 in. (76.200 mm) or more to the nearest edge of a different dent are permitted with a 1000 flight cycle reinspection | Not permitted. Replace the duct Ref. AMM TASK 80-11-49-000-802 and [Ref. AMM TASK 80-11-49-400-802](https://airnavx.lht.ham.dlh.de/airnavx/document/635628_SGML_C/toc?itemId=635628_SGML_C_EN80114940080200&itemType=DATAMODULE&wc=actype:A318;actype:A319;actype:A320;actype:A321;customization:DLH;doctype:AMM;tailNumber:N10304). |
|
||
| | Dents in zone 2 that are 0.250 in. (6.350 mm) in depth or less and more than ten times the depth across, and 3.00 in. (76.200 mm) or more to the nearest edge of a different dent are permitted | |
|
||
| | Dents in zone 1 and zone 2 that are more than 0.250 in. (6.350 mm) or less than ten times the depth across are not permitted<br><br>Ref. Fig. GVI of the Engine Starting System | |
|
||
| Nicks or scratches | Up to 0.025 in. (0.63 mm) depth or less | Permitted. |
|
||
|
||
|
||
| EXAMINE | DAMAGE | DISPOSITION |
|
||
| ---------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||
| The starter ducts (upper and lower) for: | | |
|
||
| Looseness or incorrect assembly | Any amount | Not permitted. Tighten or reassemble as necessary [Ref. AMM TASK 80-11-49-400-802](https://airnavx2.lht.ham.dlh.de/airnavx/document/658069_SGML_C/toc?itemId=658069_SGML_C_EN80114940080200&itemType=DATAMODULE&wc=actype:A318;actype:A319;actype:A320;actype:A321;customization:DLH;doctype:AMM). |
|
||
| Round bottom dents | Dents in zone 1 that are less than 0.100 in. (2.540 mm) in depth and 3.000 in. (76.200 mm) or more to the nearest edge of a different dent | Permitted. |
|
||
| | Dents in zone 1 that are 0.100 in. (2.540 mm) in depth and less than 0.250 in. (6.350 mm) and more than ten times the depth across, and 3.00 in. (76.200 mm) or more to the nearest edge of a different dent | Permitted with a re-inspection interval of 1000 flight cycles. |
|
||
| | Dents in zone 2 that are 0.250 in. (6.350 mm) in depth or less and more than ten times the depth across, and 3.00 in. (76.200 mm) or more to the nearest edge of a different dent | Permitted. |
|
||
| | Dents in zone 1 and zone 2 that are more than 0.250 in. (6.350 mm) or less than ten times the depth across<br><br>Ref. Fig. GVI of the Engine Starting System | Not permitted. Replace the duct [Ref. AMM TASK 80-11-49-000-802](https://airnavx2.lht.ham.dlh.de/airnavx/document/658069_SGML_C/toc?itemId=658069_SGML_C_EN80114900080200&itemType=DATAMODULE&wc=actype:A318;actype:A319;actype:A320;actype:A321;customization:DLH;doctype:AMM) and |
|