Epstein Files Search

EFTA01105909Set 9

22p6,179w

purpose of the pneumatics system is to provide a common manifold, known as the bleed air manifold, with hot compressed air for use by other systems. Therefore, this section describes ... sources of air for the bleed air manifold, their controls and the indications they provide to the flight crew. The airplane systems which use air from the bleed air manifold ... appropriate sections of this chapter. The pneumatics system uses the following types of bleed air: • Low pressure (LP) bleed air from the engines • High pressure (HP) bleed air from

https://www.justice.gov/epstein/files/DataSet%209/EFTA01105909.pdf

EFTA01105877Set 9

32p10,243w

controller in the normal operating mode, but can be controlled manually. • Select and control bleed air entering and exiting two environmental control system refrigeration pack assemblies, referred ... Right ECS Packs. Source air into the ECS Packs is provided to a bleed air manifold by either external air or APU air (while on the ground ... ground or in flight). Through use of an isolation valve. air from the bleed air manifold can be directed to either ECS Pack. This results in a constant mass

https://www.justice.gov/epstein/files/DataSet%209/EFTA01105877.pdf

EFTA01735529Set 10

11p3,734w

enve- lope of the aircraft. The normal source of air for air conditioning is bleed air from the engines. The APU is an alternate source and provides heating and cooling ... MANUAC During normal in-flight operation. hot com- pressed air is supplied from the bleed-air man- ifold (Figure I - 1 ). This air, which is temperature and pressure-controlled, obtained ... air machine, which are capable of reducing the temperature of the air from the bleed-air man- ifold to values above freezing. Humidity re- duction is accomplished by a mechanical

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01735529.pdf

EFTA01119971Set 9

11p3,688w

enve- lope of the aircraft. The normal source of air for air conditioning is bleed air from the engines. The APU is an alternate source and provides heating and cooling ... During normal in-flight operation, hot com- temperature of the air from the bleed-air man. pressed air is supplied from the bleed-air man- ifold to values above freezing ... PUMA ow MA Figure 11-1. Bleed-Air Manifold FOR TRAINING PURPOSES ONLY 11-2 EFTA01119972 REAR PRESSURE TEMPERATURE CONTROL BULKHEAD VALVE TORQUE MOTOR TEMPERATURE COCKPIT MANUAL CONTROL VALVE TEMPERATURE

https://www.justice.gov/epstein/files/DataSet%209/EFTA01119971.pdf

EFTA01186744Set 9

22p6,179w

purpose of the pneumatics system is to provide a common manifold, known as the bleed air manifold, with hot compressed air for use by other systems. Therefore, this section describes ... sources of air for the bleed air manifold, their controls and the indications they provide to the flight crew. The airplane systems which use air from the bleed air manifold ... appropriate sections of this chapter. The pneumatics system uses the following types of bleed air: • Low pressure (LP) bleed air from the engines • High pressure (HP) bleed air from

https://www.justice.gov/epstein/files/DataSet%209/EFTA01186744.pdf

EFTA00590661Set 9

6p1,251w

FROM LEI SERVO CONTROL SYSTEM LEGEND WARM AIR ▪ ▪ ▪ COLD AIR MM AIR HOT BLEED AIR CONDITIONED AIR CI PRIMARY HEAT EXCHANGER 0 SECONDARY HEAT EXCHANGER Figure 11-5. Refrigeration Unit ... reducing cycle the GENERAL operation, hot com- temperature of the air from the bleed-air man. During normal in-flight the le air man- ifold to values above freezing. Humidity ... LEGEND PRESSURE ■ NOT LA REGULATOR ▪ WARN Asa FAN RR APU GIN MR Figure 11.1, Bleed-Air Manifold 11-2 FOR TRAINING PURPOSES ONLY EFTA00590663 Fightketv eutricoons1400 PILOT TRAINING MANUAL

https://www.justice.gov/epstein/files/DataSet%209/EFTA00590661.pdf

EFTA02705525Set 11

22p6,232w

purpose of the pneumatics system is to provide a common manifold, known as the bleed air manifold. with hot compressed air for use by other systems. Therefore, this section describes ... sources of air for the bleed air manifold. their controls and the indications they provide to the flight crew. The airplane systems which use air from the bleed air manifold ... appropriate sections of this chapter. The pneumatics system uses the following types of bleed air • Low pressure (LP) bleed air from the engines • High pressure (HP) bleed air from

https://www.justice.gov/epstein/files/DataSet%2011/EFTA02705525.pdf

EFTA00609974Set 9

24p9,270w

warning devices. During normal in-flight operation, hot compressed air is supplied from the bleed air manifold. This is High Pressure (HP) bleed air which is temperature and pressure controlled ... cycle machine which are capable of reducing the temperature of the air from the bleed air manifold to values below ambient. Humidity reduction is accomplished by a mechanical water separator ... Temperature control of the occupied areas is accomplished by varying the amounts of hot bleed air manifold air which bypasses the cooling equipment. Separate temperature control is provided

https://www.justice.gov/epstein/files/DataSet%209/EFTA00609974.pdf

EFTA01122646Set 9

78p28,263w

reduced as a result of this bypassing, reducing the need for high- pressure bleed air. Reducing the need for high stage bleed air improves engine efficiency, reducing the amount ... turbine exhaust temperature in degrees C. The temperature will vary widely depending on bleed air loads. The green band is the normal operating range, and the red radial ... directly. This generator can supply electrical power to all airplane systems for ground operation. Bleed air is extracted from the APU compressor to be used for airplane air conditioning

https://www.justice.gov/epstein/files/DataSet%209/EFTA01122646.pdf

EFTA01119984Set 9

3p421w

STAGE BLEED-AIR CHECK VALVE 2. 12 STAGE BLEED AIR AND SOV 3. BLEED-AIR PRESSURE REGULATOR SOV 4. BLEED-AIR ISOLATION SHUTOFF VALVE 5. AIR- CONDITIONING SYSTEM ... OVERBOARD t ick O LEGEND • COLD AIR RAM AIR TO OVERTEMPERATURE - TJ • HOT BLEED AIR LIGHT (ON AT 450 F) LIGHT ON (OPEN) SWITCH -,•-• - - COMPRESSOR TO VALVE • DISCHARGE OPEWCLOSE SWITCH ... System EFTA01119984 G-IV MAINTENANCE SCHEMATIC MANUAL 1. 7TH-STAGE 2 12 STAGE 3. BLEED-AIR 4. BLEED-AIR I S. AIRCONDI 6. CABIN/COC REFRIGERA a. PRIMARY b. AIR CYCL

https://www.justice.gov/epstein/files/DataSet%209/EFTA01119984.pdf

EFTA01126916Set 9

2016-03-10123p31,377w

DATED MAR 18, 2016. WORK DONE IAW WESTERN COMMANDER , INC. WIRING DIAGRAM NO. 08030131 - BLEED AIR CONTROL MONITOR. DATED 2/10/89. Step: 6.8.2 Open NEED OPERATIONAL TEST Discrepancy: 6.9 DURING AIRCRAFT

https://www.justice.gov/epstein/files/DataSet%209/EFTA01126916.pdf

EFTA00590796Set 9

2016-03-10123p21,314w

DATED MAR 18.2016. WORK DONE IAW WESTERN COMMANDER , INC. WIRING DIAGRAM NO. 08030131 - BLEED AIR CONTROL MONITOR. DATED 2/10189. Step: 6.8.2 Open NEED OPERATIONAL TEST Discrepancy: 6.9 DURING AIRCRAFT POWER

https://www.justice.gov/epstein/files/DataSet%209/EFTA00590796.pdf

EFTA01097323Set 9

2012-11-0823p7,208w

ENGINE GENERATOR/ALTERNATOR (LEFT)- TRIP POINT CHECK; 264617/18• ENGINE GENERATOR/ALTERNATOR (LEFT)- TRIP POINT CHECK; 265020/25• BLEED AIR OVERHEAT SWITCH (LEFT/RIGHT). TRIP POINT CHECK; 268651/56• COMBINED/FLIGHT HYDRAULIC SYSTEM OVERHEAT SWITCH- TRIP POINT ... ENGINE GENERATOR/ALTERNATOR (LEFT). TRIP POINT CHECK; 264617/18- ENGINE GENERATOR/ALTERNATOR (LEFT)- TRIP POINT CHECK; 265020/25• BLEED AIR OVERHEAT SWITCH (LEFT/RIGHT). TRIP POINT CHECK; 268651/56• COMBINED/FLIGHT HYDRAULIC SYSTEM OVERHEAT SWITCH- TRIP POINT ... Discrepancy Hours Subtotal 361010/15• HIGH PRESSURE REGULATING VALVE (LEFT/RIGHT)- OPERATIONAL TEST; Flat 825.00 361030- BLEED AIR MANIFOLD PRESSURE INDICATION- FUNCTIONAL TEST; 362036/2536- PRECOOLER LOW PRESSURE INLINE FILTER (LEFT/RIGHT)- INSPECTION

https://www.justice.gov/epstein/files/DataSet%209/EFTA01097323.pdf

EFTA01117570Set 9

2009-08-0352p14,503w

MAINTENANCE. P2294 PIN ASSY. MLG CABIN COMFORT SYSTEM PIN ASSY. NLG Cockpit and cabin bleed air heating (25000 BTU) SHIELD ASSY, ENGINE INLET, R/H w/windshield defogging system SHIELD ASSY, ENGINE ... Environmental System Cabin Cockpit Climate Control, C4 System, exchange for standard bleed air heating system, provides one button set-and-forget control of the cabin temperature. System includes: Master Control ... overhead above inboard pilots seat: System Controller (computer): Primary and Secondary Distribution Ducts; Bleed-Air Heat Outlets - Cockpit Footwarmer (pilot and copilot bleed-air floods located between rudder pedals), Cabin

https://www.justice.gov/epstein/files/DataSet%209/EFTA01117570.pdf

EFTA00807159Set 9

2017-04-212p401w

SELECTOR TEMP $6,070 Air Cycle & Air Source Systems 1151582-6-2 CONTROL BLEED AIR $19,400 Airframe Valves 129740-1-1 THERMOSTAT, INLET AIR, $7,850 Cabin Pressure Controls ... Water Extractor $27,174 Air Cycle & Air Source Systems 2341172-1 PRECOOLER BLEED AIR $187,117 Air Cycle & Air Source Systems 2341172-2 PRECOOLER BLEED AIR $236,515 Air Cycle

https://www.justice.gov/epstein/files/DataSet%209/EFTA00807159.pdf

EFTA00807438Set 9

17p6,451w

SELECTOR TEMP $6,070 Air Cycle & Air Source Systems 1151582-6-2 CONTROL BLEED AIR $19,400 Airframe Valves 12974O-1-1 THERMOSTAT, INLET AIR, $7,85O Cabin Pressure Controls ... Water Extractor $27,174 Air Cycle & Air Source Systems 2341172-1 PRECOOLER BLEED AIR $187,117 Air Cycle & Air Source Systems 2341172-2 PRECOOLER BLEED AIR $236,515 Air Cycle

https://www.justice.gov/epstein/files/DataSet%209/EFTA00807438.pdf

EFTA00612414Set 9

17p6,453w

SELECTOR TEMP $6,070 Air Cycle & Air Source Systems 1151582-6-2 CONTROL BLEED AIR $19,400 Airframe Valves 12974O-1-1 THERMOSTAT, INLET AIR, $7,85O Cabin Pressure Controls ... Water Extractor $27,174 Air Cycle & Air Source Systems 2341172-1 PRECOOLER BLEED AIR $187,117 Air Cycle & Air Source Systems 2341172-2 PRECOOLER BLEED AIR $236,515 Air Cycle

https://www.justice.gov/epstein/files/DataSet%209/EFTA00612414.pdf

EFTA00796097Set 9

2017-12-1816p8,019w

Overheat Switch -Trip Point Check 261060 Flight Hydraulic System Overheat Switch - Removal/ Installation 261235 Bleed Air Manifold Overheat Switch (Left) - Trip Point Check 261225 Bleed Air Manifold Overheat Switch (Left ... Removal/ Installation 261236 Bleed Air Manifold Overheat Switch (Right) -Trip Point Check 261230 Bleed Air Manifold Overheat Switch (Right) - Removal / Installation 261440 APU Overheat Switch - Trip Point Check ... Computer No. 3 - Battery Pack Replacement X 352005 Passenger Oxygen System - Operational Test 361007 Bleed Air System (Left) - Operational Test 362005 Bleed Air Manifold Pressure Indication - Functional Test 520306 Main

https://www.justice.gov/epstein/files/DataSet%209/EFTA00796097.pdf

EFTA01117750Set 9

2015-08-1923p5,821w

Bearings (Right O/B #4) - Insp / Pack (ABS) Resolution: No action taken. Discrepancy: 8.8 Evaluate bleed air isolation valve for sticking. Resolution: Removed bleed air isolation/ shut off valve ... Description Quantity Sell price USD Extended USD 8.8 #3 398896-3-1 VALVE, ISOLATION, BLEED AIR 1 $23,530.00 $23,530.00 Step: 8.8.1 Completed Perfomed ops check of valve ... Material ST 5.50 @ $127.00 $698.50 Total USD: $698.50 Discrepancy: 8.12 CMP GIV 361065 Bleed Air Isolation Shutoff Valve - Removal / Installation Resolution: COMPLIED WITH CMP GIV 361065 Bleed Air Isolation Shutoff

https://www.justice.gov/epstein/files/DataSet%209/EFTA01117750.pdf

EFTA01112828Set 9

2015-08-1418p4,416w

Bearings (Right O/B #4) - Insp / Pack (ABS) Resolution: No action taken. Discrepancy: tit Evaluate bleed air isolation valve for sticking. Resolution: Removed bleed air isolation/ shut off valve ... Description Quantity Sell price USD Extended USD 8.8 #3 398896-3-1 VALVE, ISOLATION, BLEED AIR 1 $23,530.00 $23,530.00 Step: 8.8.1 Completed Perfomed ops check of valve ... Material ST 5.50 @ $127.00 $698.50 Total USD: $698.50 Discrepancy: 8.12 CMP GIV 361065 Bleed Air Isolation Shutoff Valve - Removal / Installation Resolution: COMPLIED WITH CMP GIV 361065 Bleed Air Isolation Shutoff

https://www.justice.gov/epstein/files/DataSet%209/EFTA01112828.pdf