""Combustion Chambers"" — Epstein Files Search

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13 results for “"Combustion Chambers"”

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EFTA01134615Set 9

2014-02-1750p8,541w

JT8D Engines ADs AD 1986-09-02R2 (Amdt 39-9385) Inspection of Combustion Chambers for Cracking and Misalignment 11/17/1995 Not Applicable by Engine Model JT8D-219 (ASB 5639R10) CAMMS ... JT8D Engines ADs AD 1994-25-07 (Amdt 39-9091) Inspection of Certain Combustion Chamber Outer Cases 03/30/1995 Not Applicable by Engine Model JT8D-219 (ASB 5842R3) CAMMS / Centurion Aircraft ... JT8D Engines ADs AD 1996-23-14 (Amdt 39-9820) Inspection of Certain Combustion Chamber Outer Cases 01/02/1997 Not Applicable by Engine Model JT8D-219 (ASB A6202R1 & ASB A6228) N908JE

https://www.justice.gov/epstein/files/DataSet%209/EFTA01134615.pdf

EFTA01100499Set 9

2014-02-267p2,380w

level of inspection. Visually inspect first stage NGVs in-situ. Visually inspect combustion chambers Visually inspect combustion chamber outlet duct assembly. Shop Inspect OCC. 6 High Pressure Turbine Inspect

https://www.justice.gov/epstein/files/DataSet%209/EFTA01100499.pdf

EFTA00301420Set 9

2012-05-2964p20,366w

combustion to the outside while the outer liner draws outside combustion air into the combustion chamber thereby eliminating theneed louse heatedroom air for combustion and losing warm room air upthechimney

https://www.justice.gov/epstein/files/DataSet%209/EFTA00301420.pdf

EFTA01086751Set 9

2013-02-063p696w

overhauled condition c) TI outer air seal to be installed in serviceable condition d) Combustion Chamber Support assembly will be visually inspected. e) Install serviceable Combustion Chambers

https://www.justice.gov/epstein/files/DataSet%209/EFTA01086751.pdf

EFTA01189539Set 9

2013-02-063p693w

overhauled condition c) TI outer air seal to be installed in serviceable condition d) Combustion Chamber Support assembly will be visually inspected. e) Install serviceable Combustion Chambers

https://www.justice.gov/epstein/files/DataSet%209/EFTA01189539.pdf

EFTA02708135Set 11

2013-02-063p697w

overhauled condition c) TI outer air seal to be installed in serviceable condition d) Combustion Chamber Support assembly will be visually inspected. e) Install serviceable Combustion Chambers

https://www.justice.gov/epstein/files/DataSet%2011/EFTA02708135.pdf

EFTA01902083Set 10

2013-02-063p695w

overhauled condition c) TI outer air seal to be installed in serviceable condition d) Combustion Chamber Support assembly will be visually inspected. e) Install serviceable Combustion Chambers

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01902083.pdf

EFTA00798623Set 9

2016-12-12126p40,656w

Maintenance 1999M.1B.80-14 5094049 12/12/2016 08/10/2017 08/10/2017 Description: 72-180-01: NO. 1 ENGINE - BORESCOPE COMBUSTION CHAMBER 80-15-Maintenance 1999M.1B.80-15 5094050 12/12/2016 08/10/2017 10/19/2017 Description ... ENGINE - BORESCOPE COMBUSTION CHAMBER 80-16-Maintenance 1999M.18.80-16 5094051 12/12/2016 07/29/2017 07/29/2017 Description: 72-200-01: NO. 1 ENGINE - BORESCOPE HIGH PRESSURE TURBINE NOZZLE 80-17-Maintenance 1999M.18.80-17 5094052 12/12/2016

https://www.justice.gov/epstein/files/DataSet%209/EFTA00798623.pdf

EFTA00283811Set 9

weeks, or as needed during operation. There are visible fractures on the furnace's combustion chamber liner. If any of these cracks extend through the fire lining and excessive heat ... smoke pipe of the heating plant. This device controls the draft at the combustion chamber. A proper operating draft control will result in fuel economy therefore a draft control should

https://www.justice.gov/epstein/files/DataSet%209/EFTA00283811.pdf

EFTA00691518Set 9

2017-03-014p1,888w

language! Challenge 8 seems to be designed by a rocket scientist who specializes in combustion chambers and leaves all other parts of getting the rocket to fly as an exercise

https://www.justice.gov/epstein/files/DataSet%209/EFTA00691518.pdf

EFTA02385630Set 11

2017-03-014p1,922w

language! Challenge 8 seems to be designed =y a rocket scientist who specializes in combustion chambers and leaves =11 other parts of getting the rocket to fly as an exercise

https://www.justice.gov/epstein/files/DataSet%2011/EFTA02385630.pdf

EFTA00605232Set 9

2016-03-2363p15,373w

centrifugal compressor TURBINE STAGES: 1 stage high pressure turbine, 3 stage low pressure turbine COMBUSTION CHAMBER: annular reverse flow combustor DIMENSIONS & WEIGHTS: Max Envelope Diameter: 39.4 in. Max Envelope Length

https://www.justice.gov/epstein/files/DataSet%209/EFTA00605232.pdf

EFTA01052854Set 9

2017-03-014p1,987w

language! Challenge 8 seems to be designed by a rocket scientist who specializes in combustion chambers and leaves all other parts of getting the rocket to fly as an exercise

https://www.justice.gov/epstein/files/DataSet%209/EFTA01052854.pdf

Corpus: 1990-03-17 – 2025-12-01

February 2014

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Results by Dataset13 total

Set 9

10

Set 10

1

Set 11

2