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Fuel Tank Safety

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Fuel Tank Safety Mike Kaszycki, FAA Dave Gibbons, JAA Fuel Tank Safety Harmonization of Unsafe Condition Criteria Fuel Tank Safety Reviews Implementation of Unsafe ... – PowerPoint PPT presentation

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Title: Fuel Tank Safety


1
Fuel Tank Safety
  • Mike Kaszycki, FAA
  • Dave Gibbons, JAA

2
Fuel Tank Safety
  • Harmonization of Unsafe Condition Criteria
  • Fuel Tank Safety Reviews
  • Implementation of Unsafe Condition Criteria
  • Continued Operational Safety/Maintenance
  • Fuel Tank Inerting
  • Summary

3
Harmonization of Unsafe Condition Criteria
  • FAA and JAA fuel tank safety review requirements
    reference different regulations
  • FAA FAR 25.901 25.981(a) (b), amendment
    25-102
  • JAA JAR 25.1309
  • FAA and JAA developed harmonized policy
  • Includes unsafe condition criteria for
    determining mandatory action from SFAR 88 JAA
    fuel tank safety reviews.
  • JAA issued policy letter on February 3, 2003
  • FAA issued policy memorandum on February 25, 2003
  • Expectation is to have common solution set.

4
Unsafe Condition Criteria
  • Four-Element Unsafe Condition Evaluation Criteria
  • Element 1. Single Failures all tanks
  • Element 2. Combination of failures
  • a) Fuel tanks with low flammability exposure
    time Known combinations of failures are
    considered an unsafe condition.
  • b) Fuel tanks with high flammability exposure
    time Non-compliant design features and
    associated maintenance actions identified by the
    system safety analysis will be used for
    establishing unsafe condition.
  • Element 3. Unacceptable service experience all
    tanks
  • Element 4.  Determination of the flammability
    exposure time of each fuel tank
  • Heated CWT High flammability exposure
  • Other tanks Low flammability exposure

5
Fuel Tank Safety Reviews
  • FAA/JAA are participating in joint SFAR 88
    reviews of several type certificate holders,
    together with certifying authorities
  • Airbus (Toulouse) March 19 - 20
  • Boeing (Seattle) April 22 - 25
  • Embraer (Ft. Lauderdale, FL) April 29 May 1
  • Bombardier (Montreal) May 6 8
  • Other TC holder reviews may only have the
    certifying authority participation, depending on
    the results of the above reviews (JAA will
    provided standardization of European NAA reviews).

6
Implementation of Unsafe Condition Criteria
  • OEM review identified harmonization issues with
    implementation of the unsafe condition criteria.
  • Authorities differed in interpretation of
    portions of the unsafe condition criteria.
  • We are committed to jointly resolving open issues
    from SFAR 88 review.

7
Continued Operational Safety/Maintenance
  • SFAR 88 requires identification of additional or
    enhanced maintenance and inspection procedures,
    in addition to possible design changes.
  • When SFAR 88 was issued, FAA believed the most
    practical method to incorporate necessary
    maintenance and inspection instructions would be
    by operating rules.
  • After rule was issued, several aviation
    authorities and industry groups indicated
    mandating by airworthiness directives would be
    preferred.
  • As part of the harmonization program, the FAA
    agreed that airworthiness directives would be
    used to mandate any maintenance and inspection
    procedures required to address unsafe conditions.

8
Continued Operational Safety/Maintenance
  • FAA will change the operating rules back to their
    pre-SFAR 88 wording.
  • FAR sections 91.410(b), 121.370(b), 125.248(b)
    and 129.32(b).
  • ADs will be issued to require maintenance actions
    necessary to address unsafe conditions.
  • Maintenance and inspection instructions not
    required to address unsafe conditions will be
    evaluated under existing standard maintenance
    review processes.(e.g., MRB)
  • If practical, ADs will use the December 6, 2004,
    compliance date to be harmonized with JAA policy
    letter.
  • Any change to this target date will be harmonized
  • Requirement deleted for U.S. operators to perform
    a design reviews for STC holders who did not
    complete SFAR 88 reviews.

9
Fuel Tank Inerting
  • Boeing applied to FAA for certification of
    Flammability Reduction System (FRS) for 737 and
    747 airplane models.
  • FRS is based on using fuel tank inerting system
    to reduce center wing tank flammability
  • Boeing applied to JAA for 737 Next Generation
    models to formalize harmonization process.
  • FAA and JAA have developed harmonized
    certification requirements.
  • FAA 737 issue paper P-1 contains proposed FAA
    special conditions
  • JAA CRI PTC E-10 contains proposed JAA special
    conditions
  • Plan is to publish both FAA and JAA proposed
    special conditions for comment concurrently in
    June 2003 with 60 day comment period.

10
Fuel Tank Safety Summary
  • Harmonization of implementation of the unsafe
    criteria continues to support common solution
    set.
  • Fuel tank safety reviews are taking place to
    support mandatory action decisions by June 2003.
  • FAA and JAA have harmonized certification
    requirements for fuel tank inerting.
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