SAIB ANE-99-26

SPECIAL

AIRWORTHINESS

INFORMATION

BULLETIN

REGULATORY SUPPORT DIVISION P.O. BOX 26460 OKLAHOMA CITY, OKLAHOMA 73125- 0460

U.S. Department of Transportation Federal Aviation Administration

No. ANE-99-26 July 12, 1999

SAIB’s are posted on the internet at http://av-info.faa.gov This is issued for informational purposes only and any recommendation for corrective action is not mandatory.

Introduction:

The purpose of this Special Airworthiness Information Bulletin (SAIB)is to alert repair stations, mechanics holding Inspection Authorization (IA), Principal Maintenance Inspectors (PMI) in the FAA Flight Standards District Offices (FSDO), and the Suspected Unapproved Parts Program Office ( AVR-20) of service difficulties and safety issues with overhauled or repaired AlliedSignal (previously Garrett or AiResearch) turbochargers installed on general aviation reciprocating engines. This bulletin is a follow-up to SAIB ANE-97-02 issued March 6, 1997.

Background:

A letter from the National Transportation Safety Board (N TSB) Washington, DC dated November 14, 1996, and a memorandum from the FAA Fresno FSDO dated August 20, 1996, both expressed the following concerns:

1. In-flight failure of overhauled and repaired AlliedSignal turbochargers.

2. Lack of part marking to differentiate FAA approved aircraft engine turbocharger components from automotive turbocharger components.

3. FAA approved repairs on turbocharger components whic h are beyond the scope of the AlliedSignal “Overhaul Manual for Aircraft System Turbochargers” TP20-0128, dated August 15, 1985.

An FAA technical team was formed to review all the acci dents and incidents in the FAA database related to the turbocharger system since 1974, to inves tigate major turbocharger repair facilitie s, to investigate FAA approved repairs beyond the AlliedSignal overhaul manual and to review AlliedSignal production drawings and processes.

Information:

FAA Team Findings and Action:

1. The review of accident/incident data indicates that the principal causes of the turbocharger system failures have been related to maintenance and installation issues i.e., exhaust clamp, air inlet duct, oil lines, lack of lubrication, etc. However, potential for catastrophic failure exists from performing unapproved repa irs or installing unapproved components in aircraft turbochargers i.e., turbocharger shaft fa ilure, engine oil contamination, engine fire, loss of engine power, etc.

2. Since welding repairs may affect the integrity of the turbocharger shaft, the previously approved welding repair to the shaft seal groove was rescinded by the FAA on March 6, 1998.

3. Chrome plating or plasma coating of the turbine shaft at overhaul is not approved by AlliedSignal nor the FAA because the process, if not properly accomplished, may weaken th e shaft below its struct ural integrity, and the coating/plating may flake away and contaminate the oil system. In addition, these repairs may extend the in-service time of the shaft beyond its intended structural integrity, and the in-service time of the turbine wheel beyond its creep growth limit.

4. Since AlliedSignal manufactures turbochargers and components for both the aviation and the automotive industries, there are physical similaritie s in design between the two lines of tu rbochargers and components. Also, in some instances, the same components are used for both applications. However, in most instances, there are differences in material, process and quality control a pplied during manufacturing of component s for aircraft a pplication versus automotive application.

The availability and lower cost of automotive turbocharger component s have enhanced the potential of unapproved automotive components being in stalled inplace of FAA a pproved aircraft component s during turbocharger repair or overhaul. The components of most concern are: turbine wheel/shaft assemblies, bearings, center housings and

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turbine housings. The criticality of inst allation of unapproved automotive parts is further enhanced by the difference in the type of operations between aircraft and automotive, i.e ., higher turbine temperature a nd rpm for aircraft, high cycle for automotive, etc.

5. Major turbocharger components appr oved for aircraft and manufactured by AlliedSignal after December 1, 1997, are now permanently identified with a part number (i.e., xxxxxxAxxxx or xxxxxx-xxxxA). The part number location is depicted in the figure of this bulletin. For small components, the part number is identified on the packaging

i.e., bag and tag, reference 14 CFR part 45.15.

6. It is the intent of the FAA that most turbocharger components, which are currently unmarked and installed in aircraft, will eventually be purged out of the system.

7. AlliedSignal Overhaul Manual TP 20-0128 is being updated a nd revision should be av ailable to the FAA approved repair stations early in the year 2000.

Recommendations:

1. Use only FAA approved repair, overhaul and service data when servicing or working on AlliedSignal aircraft turbochargers.

2. Use only FAA approved replacement co mponents for aircraft turbocharg ers. These components are now permanently identified with an AlliedSignal part number a nd an “A” for aircraft (see figure for marking location and AlliedSignal Overhaul Manual TP20-0128 for FAA approved part listing).

3. At turbocharger overhaul or when a turbocharger is taken apart for repair, all serviceable components should be examined on an individual basis. If their configuration or origin is questionable or if unauthorized repairs are found, the components should be replaced with FAA approved components per AlliedS ignal Overhaul Manual TP20-0128 part list and with a permanent part number marking (see figure for component markings and locations).

Examples of unauthorized repairs:

- welding of housings, flanges, shaft, turbine wheel

- plasma coating of wear surfaces such as seal grove

- chrome plating of turbine shaft

4. Carefully review and inspect the pa perwork that accompanies any replacement parts to verify that the parts are FAA approved parts, produced under an a pproved FAA quality system, and that th e paperwork includes the appropriate airworthiness tags/certificates for AlliedSignal aircraft turbocharger installation.

5. Repair stations should maintain onl y aircraft approved parts in their ai rcraft turbocharger overhaul facility area.

6. Report any suspected unapproved parts to the local Flight Standards District Office (FSDO) or Manufacturing Inspection District Office (MIDO).

For Further Information Contact:

Rejean Chartier Los Angeles Aircraft Certificati on Office, 3960 Paramount Blvd., Lakewood, CA 90712-4137;

telephone: (562) 627-5240; fax: (562) 627-5210; email: rejean.chartier@faa.gov. Others include: Guy Dalla Riva (LAACO), (562) 627-5248; Mark Rumizen, Engine & Propeller Directorate (781) 238-7113; Peter Hakala, Southwest Special Certification Office (817) 222-5145; Jim Connelly, Los Angeles MIDO (562) 627-5290.

ANE-99-26 3

TURBOCHARGER COMPONENT PART NUMBER LOCATION (xxxxxxxxxx or xxxxxx-xxxxA) Back Plate Front Side (visible when compressor housing is removed) Compressor Wheel Back Disk (not visible when assembled) Turbine Wheel/Shaft Assy. Center Compressor Housing Inside (visible thru center housing (not visible when assembled) oil port when assembled) Center Housing Oil Port Mating Surface (visible when oil fitting is removed) Bearing Side (not visible when assembled) (last 4 digits of p/n and dash number) Turbine Housing Mating Surface (not visible when turbocharger is installed) Figure 1. ANE-99-26