# Incident 20060704018609I: Doug DC983, Fresno, CA, July 4, 2006

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: July 4, 2006, 14:37 local time
- Place: Fresno, CA
- Airport: Fresno Yosemite International Airport
- Phase of flight: To Init Climb(1st Pwr Reduct)
- Operating rules: Air carrier (Part 121)
- Operator: AALA
- Location: 36.7766° N, 119.7188° W: Placed by OpenAirDocs at FRESNO YOSEMITE INTL (FAT), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=36.7766&lon=-119.7188&mi=10
- Aircraft: N591AA, a cancelled registration (https://openairdocs.org/deregistered/N591AA-2015-01-14) (OpenAirDocs)
- Registry model: Mcdonnell Douglas DC-9-83(MD-83) (registry code 3022083, https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (OpenAirDocs)
- Registry engine: Pratt & Whitney JT8D-219 (registry code 51694, https://openairdocs.org/engine/pratt-whitney-jt8d-219) (OpenAirDocs)
- Reported make and model: DOUG DC983
- Reported engine: PWA JT8D
- People aboard: 120
- Fatal injuries: 0
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20060704018609I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) DURING THE TAKEOFF PHASE AT LIFT-OFF, THE RIGHT ENGINE (#2) EXPERIENCED SEVERE COMPRESSOR STALLS THAT REQUIRED IMMEDIATE SHUTDOWN OF THE ENGINE. THIS TAKEOFF WAS A MAXIMUM GROSS WEIGHT TAKEOFF REQUIRING MAXIMUM POWER SETTINGS. THE AIRCRAFT RETURNED TO THE DEPARTING AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MAXIMUM BRAKING PROCEDURES WERE REQUIRED SINCE NO THRUST REVERSERS WERE UTILIZED. THE RIGHT ENGINE SHOWED DAMAGE TO THE ACOUSTICAL LINING MATERIAL INSIDE THE ENGINE NEAR THE 13TH STAGE AREA. APPARENTLY, SOME PORTIONS OF THIS ACOUSTICAL LINING MATERIAL SEPARATED DURING TAKEOFF WITH NO OTHER DAMAGE NOTED TO THE ENGINE COWLINGS. FURTHER INVESTIGATION SHOWS A BLEED AIR LEAK OCCURRED FROM A RUPTURED DUCT SEAL APPARENTLY FROM THE 13TH STAGE DUCTING MANIFOLD. NO OTHER DAMAGE WAS FOUND. ADDITIONALLY, THE LEFT ENGINE APPARENTLY EXCEEDED 610 DEGREES MOMENTARILY DUE TO THIS EMERGENCY. THE AIRCRAFT WILL UNDERGO SPECIAL INSPECTIONS FOR HEAVY WEIGHT LANDING, LEFT ENGINE INSPECTION AND HOT BRAKE INSPECTIONS.

## Other reports on N591AA (2)

Matched to the same aircraft by N-number and date.

- [Incident 20020521013129I](https://openairdocs.org/incident/20020521013129I), May 21, 2002: Doug MD83 (N591AA), Wichita, KS. (-23) American airlines flt #1061 enroute ord-phx lost oil quantity on #2 engine, with oil temp rise. Shut down #2 engine and diverted into ict. Aircraft…
- [Incident 19970306004429I](https://openairdocs.org/incident/19970306004429I), Mar 6, 1997: Doug DC983 (N591AA), Rochester, NY, Minor damage. Narrative: on March 6, 1997, an American airlines DC-9-83, N591AA, was taxiing to runway 22 at Rochester/monroe county airport (roc) for take-off. The pilot…

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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