Добавил:
timofeev.9@mail.ru Опубликованный материал нарушает ваши авторские права? Сообщите нам.
Вуз: Предмет: Файл:

B737-NG-600-7-8-9-BBJ-Cockpit Guide-Compacn (19-7-10).pdf

.pdf
Скачиваний:
491
Добавлен:
05.01.2020
Размер:
71.08 Mб
Скачать

.- /

 

CFM56-7B

TRAINING MANUAL

 

 

 

 

 

 

 

ITEM

IDENTIFY THE

 

ITEM

SELECT THE PURPOSE THAT MATCHES THE

NO.

LINE, ACCESSORY OR COMPONENT

 

NO.

LINE, ACCESSORY OR COMPONENT

 

 

 

 

 

 

LPT air duct

 

 

Controls the fan air to the LPT case.

 

 

 

 

 

 

LPTCC valve

 

 

Ducts cooling air to the HPT shroud support.

 

 

 

 

 

 

LPT nozzle cooling manifold

 

 

1 of 4 tubes that cool the LPT nozzles with fourth

 

 

 

stage air.

 

 

 

 

 

 

 

 

 

 

HPT air duct

 

 

Provides the fan air path to the LPT case

 

 

 

 

 

EFFECTIVITY

GENERAL

Page 99

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

CFM56-7B

TRAINING MANUAL

 

5

1

2

4

3

CTC-189-046-00

EFFECTIVITY

GENERAL

Page 100

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

 

CFM56-7B

TRAINING MANUAL

 

 

 

 

 

 

 

ITEM

IDENTIFY THE

 

ITEM

SELECT THE PURPOSE THAT MATCHES THE

NO.

LINE, ACCESSORY OR COMPONENT

 

NO.

LINE, ACCESSORY OR COMPONENT

 

 

 

 

 

 

High Stage Bleed Air Valve

 

 

Provides cooling air to the ignition leads.

 

 

 

 

 

 

LH ignition lead

 

 

Provides 9th stage bleed air to the airplane

 

 

 

systems.

 

 

 

 

 

 

 

 

 

 

RH ignition lead

 

 

Provides the path for electricity to the LH igniter

 

 

 

plug.

 

 

 

 

 

 

 

 

 

 

Ignition lead cooling manifold

 

 

Provides the path for electricity to the RH igniter

 

 

 

plug.

 

 

 

 

 

 

 

 

 

 

T25 sensor lead

 

 

Carries HPC inlet temperature data for the control

 

 

 

logic.

 

 

 

 

 

 

 

 

 

EFFECTIVITY

GENERAL

Page 101

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

CFM56-7B

TRAINING MANUAL

 

4

2

5

 

1

3

CTC-189-047-00

EFFECTIVITY

GENERAL

Page 102

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

 

CFM56-7B

TRAINING MANUAL

 

 

 

 

 

 

 

ITEM

IDENTIFY THE

 

ITEM

SELECT THE PURPOSE THAT MATCHES THE

LINE, ACCESSORY OR COMPONENT

 

NO.

LINE, ACCESSORY OR COMPONENT

NO.

 

 

 

 

 

 

 

 

 

 

 

Transient Bleed Valve actuator

 

 

Cools the ignition leads.

 

 

 

 

 

 

Ignition lead cooling manifold

 

 

Controls 9th stage air bleed to ease engine

 

 

 

acceleration.

 

 

 

 

 

 

 

 

 

 

TBV electrical connection

 

 

Provides the electrical path to the EEC for position

 

 

 

of the TBV.

 

 

 

 

 

 

 

 

 

 

BSV

 

 

Operates the TBV butterfly.

 

 

 

 

 

 

Transient Bleed Valve

 

 

Controls the fuel flow for the staged fuel nozzles.

 

 

 

 

 

EFFECTIVITY

GENERAL

Page 103

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

CFM56-7B

TRAINING MANUAL

 

4

6

3

2

7

1

5

CTC-189-048-00

EFFECTIVITY

GENERAL

Page 104

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

 

CFM56-7B

TRAINING MANUAL

 

 

 

 

 

 

 

ITEM

IDENTIFY THE

 

ITEM

SELECT THE PURPOSE THAT MATCHES THE

NO.

LINE, ACCESSORY OR COMPONENT

 

NO.

LINE, ACCESSORY OR COMPONENT

 

 

 

 

 

 

High Stage bleed air valve

 

 

Controls 9th stage bleed air to the airplane.

 

 

 

 

 

 

5th Stage bleed air check valve

 

 

Fuel nozzle with a gold band.

 

 

 

 

 

 

(DAC) Cooling fuel nozzle

 

 

Fuel nozzle with a blue band.

 

 

 

 

 

 

(DAC) Bleed fuel nozzle

 

 

Prevents 9th stage bleed air reverse flow into the

 

 

 

HPC.

 

 

 

 

 

 

 

 

 

 

(DAC) Fuel manifolds

 

 

Provides access to the HPT rotor trailing edge.

 

 

 

 

 

 

Borescope plug

 

 

Supports the HPT shroud.

 

 

 

 

 

 

HPT Shroud support

 

 

Distributes fuel into three manifolds the pilot, main

 

 

 

1, and main 2.

 

 

 

 

 

 

 

 

 

EFFECTIVITY

GENERAL

Page 105

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

CFM56-7B

TRAINING MANUAL

 

3

4

2

1

CTC-189-049-00

EFFECTIVITY

GENERAL

Page 106

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

 

CFM56-7B

TRAINING MANUAL

 

 

 

 

 

 

 

ITEM

IDENTIFY THE

 

ITEM

SELECT THE PURPOSE THAT MATCHES THE

NO.

LINE, ACCESSORY OR COMPONENT

 

NO.

LINE, ACCESSORY OR COMPONENT

 

 

 

 

 

 

(SAC) Fuel nozzle

 

 

Sensor line for the 9th stage air called compressor

 

 

 

discharge pressure (CDP).

 

 

 

 

 

 

 

 

 

 

PS3 line (also called CDP)

 

 

Sprays the fuel into the combustor.

 

 

 

 

 

 

(SAC) Fuel supply manifolds

 

 

Prevents leakage if the B nut comes loose.

 

 

 

 

 

 

Fuel nozzle drain shroud

 

 

Distributes fuel into the staged and unstaged

 

 

 

manifolds

 

 

 

 

 

 

 

 

 

EFFECTIVITY

GENERAL

Page 107

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK

 

 

 

 

.- /

CFM56-7B

TRAINING MANUAL

 

2

1

CTC-189-050-00

EFFECTIVITY

GENERAL

Page 108

B737-600, -700, -800, -900, -BBJ/ALL

COMPONENT IDENTIFICATION Jan 99

CFMI PROPRIETARY INFORMATION

WORKBOOK