TASK 71-00-00-700-051-B00 Engine Operation Limits, Guidelines, And Special Procedures, Testing-000

DMC:V2500-A0-71-00-0000-00B-030A-B|Issue No:006.00|Issue Date:2019-08-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

All

Common Information

TASK 71-00-00-700-051-B00 Engine Operation Limits, Guidelines, And Special Procedures, Testing-000

Engine Operation Limits

Exhaust gas temperature (EGT) limits.

Take-off V2527

Duration of 5 minutes

EGT limit of 1175 deg F (635 deg C)

Take-off V2530/V2533

Duration of 5 minutes

EGT limit of 1202 deg F (650 deg C)

Maximum continuous

Duration unlimited

EGT limit of 1130 deg F (610 deg C)

Starting

Duration of 2 minutes

EGT limit of 1175 deg F (635 deg C)

Transient

Duration unlimited

EGT limit of 1175 deg F (635 deg C)

Oil pressure limits.

The main oil differential pressure must be in limits given in Figure during all stable operation. If the DMOP is below the lower limit at idle, correction for main oil temperature and HP speed can be applied during stabilized ground running at idle only using the DMOP idle correction equation. Refer to Figure for the DMOP idle correction equation.

During operation in cold weather, the scavenge oil filter clog warning is inhibited until the main oil temperature gets to approximately 90 deg F (32 deg C) in order to prevent false indication of a clogged filter due to cold oil.

Make sure at all running conditions that the No. 4 bearing compartment scavenge pressure is not more than the limits that follow:

Maximum Allowable Transient Limit:

All testing conditions: 205 psig (1413.4 kPa)

Maximum Allowable Steady-State Limit (3 Minutes Stabilization or More):

Idle and Approach Idle: 9 psig (62.1 kPa)

Band D:

Band B and C:

Band A:

17 psig (117.2 kPa)

145 psig (999.7 kPa)

Minimum: 55 psig (379.2 kPa)

Maximum: 145 psig (999.7 kPa)

If the scavenge pressure limit is exceeded at any time, you must shut down the engine as given in TASK 71-00-00-700-054-B00 (TESTING-000, CONFIG-002)

Do the checks that follow if the P4SCAV limit is exceeded:

Inspect the gasket for leaks at the interface between the No.4 bearing compartment external scavenge elbow and internal scavenge line. (This potential cause more likely will increase P4SCAV in between 130 to 160 psig (896.3 to 1103.2 kPa).

Disconnect the No. 4 bearing compartment external scavenge elbow.

Check and record signs of leaks from the gasket.

Replace the gasket. Refer to TASK 72-42-00-430-001 (ASSEMBLY, page-1001).

Do the Performance Test again to check for correct No. 4 bearing compartment scavenge pressure. Refer to TASK 71-00-00-700-010-B00 (TESTING-010, CONFIG-002).

If the scavenge pressure is still not normal, do a No. 4 Bearing Compartment Vacuum Check. Refer to TASK 72-00-43-420-001 (INSTALLATION).

If the vacuum check is more than 17 pph, disassemble, inspect and reassemble the No. 4 bearing compartment.

If the vacuum check is less than 17 pph, contact IAE Technical Services for instructions.

Oil temperature limits.

The maximum oil temperature is 311 deg F (155 deg C) (When operation is stabilized for a minimum of three minutes). If the oil temperature is higher than 311 deg F (155 deg C), find the cause of the high temperature as soon as possible. Refer to the fault isolation TASK 71-00-00-810-015 (FAULT ISOLATION-015).

The maximum transient temperature is 329 deg F (165 deg C) for 15 minutes after any high power operation. If the temperature is higher than 329 deg F (165 deg C), shut down the engine and find the cause of the high temperature. Refer to the fault isolation TASK 71-00-00-810-015 (FAULT ISOLATION-015).

Minimum Oil Temperatures are shown in the table below:

Oil Temperature - °C

V2500 - A1

All other A5 models

V2530 - A5

V2533 - A5

Minimum starting

-40

-40

-40

-40

Minimum prior to exceeding idle

-10

-10

-10

-10

Prior to takeoff

FSII not used

IDG engaged

OAT>-45°C

50

50

50

50

-54°C<OAT<-45°C

Not allowed

50

50

50

IDG disconnected (no heat addition from IDG)

OAT>-40°C

50

50

50

50

-40°C>OAT>-45°C

50

50

50

60*

-54°C<OAT<-45°C

Not allowed

50

63**

Not allowed

FSII used

Whatever IDG condition (engaged or disconnected)

OAT>-45°C

50

50

50

50

-54°C<OAT<-45°C

Not allowed

50

50

50

Maximum Continuous

155

155

155

155

Maximum Transient (15 Minutes)

165

165

165

165

NOTE

Use of approved Fuel System Icing Inhibitor (FSII) of 0.1% or greater.
OAT - Outside Air Temperature.
Prior to take-off, minimum oil temperatures for fuel inlet temperature of -45°C except as noted below.
* 60°C for fuel temperature of -45°C, 50°C for fuel temperature -40°C and above.
** 63°C at N2=8781 rpm (8% MTO part power) for fuel temperature of -45°C.

Rotor operation speed limits.

The maximum N1 is 5,650 RPM/100%.

The maximum N2 is 14,950 RPM/100%.

Vibration limits

Fan case (VFAVM-1) (SEE NOTE)

Overall - 1.0 IPS (21 to 400 Hz at 3dB)

N1 (Peak) - 0.6 IPS

N2 (Peak) - 0.6 IPS

Fan case (VFAVM-2) (SEE NOTE)

Overall - 1.0 IPS (21 to 400 Hz at 3dB)

N1 (Peak) - 0.6 IPS

N2 (Peak) - 0.6 IPS

Overtemperature limit.

Refer to Procedure After Engine Overtemperature (No Surge or Stall) (Refer to TASK 71-00-00-700-056-B00) (TESTING-000, CONFIG-002) or Procedure After Engine Overtemperature (with Surge or Stall) (Refer to TASK 71-00-00-700-057-B00) (TESTING-000, CONFIG-002).

Nacelle temperature limit.

The maximum temperature is 500 deg F (260 deg C).

Fuel pressure limit.

The fuel inlet pressure supplied to the engine must be 5 to 70 psig (34.5 to 482.6 kPa).

Engine Operation Guidelines

Oil consumption guidelines.

Oil consumption is acceptable if the consumption is not more than 0.6 pints (0.5 Imperial pint, 0.285 liters, 0.3 quarts) each hour.

If it is found that the oil level has increased by 0.42 US pints (200 cc, 0.21 quarts) or more compared to before, obtain an oil sample and send it to the laboratory for fuel contamination check.

The minimum time of operation for a check of oil consumption is 30 minutes. The engine must have operated at high and low thrust lever positions.

Starter operation guideline.

Usual starter operation time must not be more than two minutes.

Do the starter procedure that follows:

Do three consecutive cycles (two cycles of two minutes and one cycle of one minute).

Stop for 15 seconds between cycles to let the starter rotor lubricate again.

After three cycles, stop for 30 minutes to let the starter become cool.

Do not engage the starter again with the engine motoring above 1490 RPM (10 percent N2)

Starter operating pressure is 30 to 40 psig (206.8 to 275.8 kPa).

Idle thrust guidelines.

The minimum idle corrected fuel flow, approach and minimum idle corrected net thrust must not be more than the value given below:

APPROACH IDLE

THRUST (lbs)

MINIMUM IDLE

THRUST (lbs)

MINIMUM IDLE CORRECTED

FUEL FLOW (lbs/hr)

1925

1205

850

Running with the Reduced Ground Idle is projected to reduce Minimum Idle Thrust and Fuel Flow by 19% and 9.1% respectively above 0 deg C ambient temperature.

Calculate the EPR modifier number and select the thrust/EPR value that is given below in Test No.10, TASK 71-00-00-700-010-B00 (TESTING-010, CONFIG-002).

Engine limits of new overhauled engines are in Test No.10, TASK 71-00-00-700-010-B00 (TESTING-010, CONFIG-002). Refer to Test No.12, TASK 71-00-00-700-012-B00 (TESTING-012, CONFIG-002) for limits on an in-service engine when you remove a module or section and install it again without overhaul, rework, repair or replacement.

The engine dry weight is 5300 pounds. The maximum engine weight which includes the engine build-up unit (EBU) is 5550 pounds.

Engine Operation Special Procedures

Procedure for the inspection of magnetic chip detectors (MCD) after test.

Refer to INSPECTION/CHECK-08 TASK 72-00-00-200-008 (INSPECTION/CHECK-008).

NOTE

To identify the consumable materials refer to the PCI.

NOTE

The starter operation guideline provides more data on the starter operation, refer to paragraph 7.

NOTE

Refer to Fault Isolation TASK 71-00-00-810-018 (FAULT ISOLATION-018) if N1 is more than the limit. Refer to Fault Isolation TASK 71-00-00-810-019 (FAULT ISOLATION-019) if N2 is more than the limit.

NOTE

The maximum spread that is allowed between VFAVM-1 and VFAVM-2 is 0.25 IPS. If the spread is out of limits, refer to Fault Isolation TASK 71-00-00-810-024 (FAULT ISOLATION-024). 1.5 IPS = 5.0 Aircraft units.

NOTE

If you see oil wetness from the No. 4 bearing compartment weep tube exit at the bottom of the turbine exhaust case and you see the wetness after consecutive starting cycles, do the dry out procedure that follows before you advance the TLA above idle power.

NOTE

Run the engine at Approach Idle for 20 minutes. Inspect the No. 4 bearing compartment weep tube exit at the bottom of the turbine exhaust case for signs of oil. If you see wetness, contact IAE for instructions.

NOTE

Use the idle thrust guideline values for new engines. Do not use these guidelines for repaired engines.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-277 KEROSINELOCALCoMat 01-277

Spares

NONE

Safety Requirements

NONE

Procedure

  1. Figure: Delta Main Oil Pressure (DMOP) Limits

    Delta Main Oil Pressure (DMOP) Limits

    Figure: Delta Main Oil Pressure (DMOP) Idle Correction Equation

    Delta Main Oil Pressure (DMOP) Idle Correction Equation

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Updated oil presure limits statement (18VC424A) (CAS-44506-V1Y6X2)

Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-277
Type:sp01
Supply Short Name:CoMat 01-277 KEROSINE
Supply Name:CoMat 01-277 KEROSINE
Specification Groups:
Doc NumberType
OMAT: 101COMMERCIAL GRADE D.ENG.RD2494 MIL-T-5624 TYPE JP5
Suppliers:
ManufacturerRemarks
LOCAL
IE108