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31 Cards in this Set

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What powers the P8?

Two General Electric CFM56-7B27AEAE turbo-fan engines.


Rated at 27,000 pounds thrust each.

Engines

When should the initial AIDR be submitted via JDRS?

Within five calendar days after completing the Acceptance Inspection.

If needed, when must a supplemental AIDR be submitted?

Within 30 calendar days of completion of the initial AIDR.

What is required of all Life Rafts upon acceptance of a new aircraft?

A Place in Service (PIS) inspection conducted by local FRC.

Upon acceptance of an aircraft, what must be done with the Wire Diagram Manuals?

Turned in to the local FST for safekeeping/technical reference.

What is the height of the P8?

Tail height=42 feet 2 inches.

What is the wingspan of the P8?

123 feet 6 inches.

NAVAIR directives, engineering directives, maintenance instructions or SMP. Which takes precedence when a conflict exists?

SMP. Maintenance activities shall contact the applicable FST, and CC Cognizant Wing, for immediate resolution of the conflict.

Can a squadron rebase P8 inspections? Why/Why not?

Squadrons SHALL NOT rebase inspections due to the impact to the planned Depot induction schedule.

How long shall completed MAF data be stored?

Six months from completion date or one complete inspection cycle or six months (whichever is greater) for phased or special inspections.

What is the P8's Depot level maintenance interval?

D-Check-


72 months initial/48 month repeat


30 day duration

What shall the flight crew ensure/verify prior to Depot level induction?

The latest version of the Nav Data Base is loaded into the Flight Management computer system.

When shall the P8 be delivered to the Depot facility for induction?

No later than 1200 hours on the day prior to the scheduled induction date or as directed by TYCOM.

What may squadron maintenance perform on P8 engines (CFM56-7B)?

Limited to testing, troubleshooting, and removal/replacement of EXTERNAL engine components.


Complete engine assembly R&R performed by contractor field team.

When SHALL hydraulic contamination fluid analysis be completed?

  • Acceptance of aircraft.
  • Any time system is subject to excessive temperature (225*F).
  • Not required after R&R of a component or system has been opened.

Where are P8 tire and wheel assembly inspection criteria and wear limits located?

AMM.

What conditions must be met to transport main wheel and brake assemblies onboard the P8?

  • Must be stored in organic storage area utilizing wheeled pallet assembly.
  • Deflated to 55 psi or 25% of operating pressure.

What conditions must be met to transport nose wheel assemblies onboard the P8?

  • Stored inside ANY organic stowage container.
  • Deflated to 53 psi or 25% of operating pressure.

What must be ensured of all engine ground turn data and flight data from the PCMCIA Card?

Uploaded daily to AHM Web and Delta.

What must be done with any corrupted/non-functioning PCMCIA Card?

Destroy, discard, and order a new PCMCIA Card through normal supply channels.

What is the hydrostatic test requirements for:


  • Engine/APU Fire Bottles?
  • FE-25/FE-36 Suppressors?
  • Monnex Suppressors?
  • 5 years.
  • 10 years.
  • No requirement.

What Ordnance Qual/Cert level(s) is/are required for removal/replacement of engine/APU fire bottles or Dry Bay Fire Suppression System Suppressors?

Not required provided the cartridges remain installed as part of the assembly.

When are oxygen systems required to be purged?

P8 aircraft do not require oxygen system purging.

What is the preferred passenger life vest?

The LPU-32/P; available for all passengers.

When are the Commercial Life Vests used?

IN CASE OF EMERGENCY ONLY.


Inspected on the Daily.

What is the inspection/replacement cycle of the Commercial Life Vest?

Discarded/Replaced at 10 years or if opened.

How much data can the PCMCIA Card hold?

Up to 8 GB for a typical 20 hour flight. A typical P-8 mission will only generate 2GB of data.

When is standby (wet) compass calibration required?

Only when the standby magnetic compass is replaced or following any flight when errors of +/-5* exist in any A/C compass system.

When is the aircraft required to be moored?

With wind speeds at or above the ones identified by the tool created to assist in interpreting AMM Task 10-11-03-580-801Fig 201.

What is the maximum water pressure for using the "bird bath"?


Minimum OAT?

80 PSI.


40*F.

When is use of taxi-through rinse facilities (bird bath) required?

After low-level flight (below 3000' AGI) when operating near sea water.