Southwest Airlines has added a news release to its Investor Relations website.
Title: Former NTSB Investigator in Charge Offers Safety of Flight Assessment on Behalf of Southwest Airlines
Date: 3/7/2008 4:55:00 PM
For a complete listing of our news releases, please click here
DALLAS, March 7 /PRNewswire-FirstCall/ -- The following is a statement by
Gregory A. Feith:
I was requested by Southwest Airlines (SWA) to review and assess the
potential safety of flight risk that could have resulted from the continued
in-service operation of 46 of their Classic 737 airplanes in March 2007 as
they progressively inspected a small area (under 0.6%) of the fuselage skin as
required by FAA Airworthiness Directive 2004-18-06. The assessment involved
the review of technical documents associated with both mandatory and
non-mandatory inspections, pertinent service/maintenance history for the
46 airplanes, a technical briefing by the Southwest Airlines Engineering
Department and technical data/analysis provided by Boeing (the airplane
manufacturer) related to structural integrity of fuselage skin cracks that
were found on five of the 46 SWA airplanes. The scope of the assessment was
confined to the safety of flight issues only.
Based on the information I have reviewed, it is apparent that on March 15,
2007, SWA initiated re-inspection of the affected airplanes to accomplish the
inadvertently missed portion of FAA Airworthiness Directive (AD) 2004-18-06.
A review of the historical information that led to the issuance of the AD
indicates that a progressive inspection for fuselage skin cracking was
initially distributed to operators in the form of a "non-mandatory" Service
Bulletin (SB) that provided "risk mitigation" actions that operators were
encouraged to incorporate into their maintenance program. This Service
Bulletin was based, in large part, on an inspection program developed by
Southwest Airlines. The issuance of the AD was a continued effort to ensure
that cracks in the fuselage skin on the Boeing 737 airplanes were identified
and mitigated well before they could pose a safety of flight issue. It is
evident from the 4500 hour initial inspection requirement (regardless of
aircraft age (i.e. flight cycles)) that the FAA did not regard the skin
cracking as an "immediate threat" to the safety of flight of the airplane.
Thus, the FAA Airworthiness Directive permitted aircraft to remain in-service
for approximately 1 1/2 years, until a normally scheduled heavy maintenance
visit occurred, before the first inspection was required.
In addition, it is evident from the analysis and testing data developed by
Boeing that cracks up to 6 inches in the fuselage skin do not compromise the
structural integrity or pose a safety of flight issue. This is further
supported by the design of the fuselage structure which incorporates "internal
reinforcing doublers in the skin assembly" and "tearstraps," both of which are
intended to provide strength, and slow or abate the growth rate of a crack
under normal operating aerodynamic loads.
Based on the available data and information reviewed, it is apparent that
there was no risk to the flying public in March 2007 while Southwest Airlines
performed their program to re-inspect the small area of aircraft fuselages
identified in the AD inspection that was inadvertently missed.
Gregory A. Feith
International Aviation Safety & Security Consultant
Title: Former NTSB Investigator in Charge Offers Safety of Flight Assessment on Behalf of Southwest Airlines
Date: 3/7/2008 4:55:00 PM
For a complete listing of our news releases, please click here
DALLAS, March 7 /PRNewswire-FirstCall/ -- The following is a statement by
Gregory A. Feith:
I was requested by Southwest Airlines (SWA) to review and assess the
potential safety of flight risk that could have resulted from the continued
in-service operation of 46 of their Classic 737 airplanes in March 2007 as
they progressively inspected a small area (under 0.6%) of the fuselage skin as
required by FAA Airworthiness Directive 2004-18-06. The assessment involved
the review of technical documents associated with both mandatory and
non-mandatory inspections, pertinent service/maintenance history for the
46 airplanes, a technical briefing by the Southwest Airlines Engineering
Department and technical data/analysis provided by Boeing (the airplane
manufacturer) related to structural integrity of fuselage skin cracks that
were found on five of the 46 SWA airplanes. The scope of the assessment was
confined to the safety of flight issues only.
Based on the information I have reviewed, it is apparent that on March 15,
2007, SWA initiated re-inspection of the affected airplanes to accomplish the
inadvertently missed portion of FAA Airworthiness Directive (AD) 2004-18-06.
A review of the historical information that led to the issuance of the AD
indicates that a progressive inspection for fuselage skin cracking was
initially distributed to operators in the form of a "non-mandatory" Service
Bulletin (SB) that provided "risk mitigation" actions that operators were
encouraged to incorporate into their maintenance program. This Service
Bulletin was based, in large part, on an inspection program developed by
Southwest Airlines. The issuance of the AD was a continued effort to ensure
that cracks in the fuselage skin on the Boeing 737 airplanes were identified
and mitigated well before they could pose a safety of flight issue. It is
evident from the 4500 hour initial inspection requirement (regardless of
aircraft age (i.e. flight cycles)) that the FAA did not regard the skin
cracking as an "immediate threat" to the safety of flight of the airplane.
Thus, the FAA Airworthiness Directive permitted aircraft to remain in-service
for approximately 1 1/2 years, until a normally scheduled heavy maintenance
visit occurred, before the first inspection was required.
In addition, it is evident from the analysis and testing data developed by
Boeing that cracks up to 6 inches in the fuselage skin do not compromise the
structural integrity or pose a safety of flight issue. This is further
supported by the design of the fuselage structure which incorporates "internal
reinforcing doublers in the skin assembly" and "tearstraps," both of which are
intended to provide strength, and slow or abate the growth rate of a crack
under normal operating aerodynamic loads.
Based on the available data and information reviewed, it is apparent that
there was no risk to the flying public in March 2007 while Southwest Airlines
performed their program to re-inspect the small area of aircraft fuselages
identified in the AD inspection that was inadvertently missed.
Gregory A. Feith
International Aviation Safety & Security Consultant