Accident Piper PA-32R-300 N6209J,
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ASN Wikibase Occurrence # 294531
 
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Date:Thursday 9 September 2004
Time:06:14 LT
Type:Silhouette image of generic P32R model; specific model in this crash may look slightly different    
Piper PA-32R-300
Owner/operator:San Antonio Piper Inc.
Registration: N6209J
MSN: 32R-7680332
Year of manufacture:1976
Total airframe hrs:8411 hours
Engine model:Lycoming IO-540-K1G5D
Fatalities:Fatalities: / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:Rachel, Texas -   United States of America
Phase: Unknown
Nature:Unknown
Departure airport:San Antonio-Stinson Municipal Airport, TX (SSF/KSSF)
Destination airport:McAllen-Miller International Airport, TX (MFE/KMFE)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
A single-engine airplane, operating in dark night instrument meteorological conditions as a Part 135 mail cargo flight, impacted terrain after an in-flight break up. Several minutes before the impact, the pilot reported to air traffic control that he had lost his vacuum pump. An on-site examination of the wreckage revealed that the vacuum pump the drive was separated from the engine and the flex coupling displayed a torsion-type separation with coupling wear consistent with engine operation after the separation. Disassembly of the model 211CC vacuum pump revealed the following. A number was assigned to each of the rotor segments and the corresponding vanes were marked and removed from their respective slots. Five of the six vanes were intact, and vane #4 was broken. Four pieces were reassembled to recreate approximately 80 percent of vane #4. Three of the four pieces were found in the mounting flange, and one piece was found in the back flange. The rotor segments were marked such that vane slot #4 is between segment 4 and segment 5. Upon examination of the walls of vane slot 4, a groove approximately .450 inches by .120 inches by .020 inches deep was found on both sides of the vane slot. These grooves corresponded in dimension and position to the portion of the vane that was missing. Three carbon pieces were found, which exhibited extensive wear, which, in two cases, were smooth and round like a "BB." The rear fracture surface of vane #4 exhibited a smooth, polished, spherical wear mark corresponding with the carbon pieces found. The pump housing had severe wear such that there were washboard marks around its entire circumference. At the bottom of the bore, a burr was found on the edge of one of the back flange discharge ports. Corresponding rotational marks were found on the pump's rotor. According to Parker Hannifin, the rule of thumb for vane wear versus service life is: .025-inches of wear for every 100 hours of operation. Using Parker's original new vane length of .845 inches, the estimated time of operation of the vanes of the accident pump was approximately 1,380 hours. According to Parker the vacuum pump had been overhauled. Parker's service letters require replacement of model 211CC vacuum pumps after 500 hours of operation or 6 years from the date of manufacture, which ever occurs first. Examination of the directional gyro revealed that the housing was intact and the gyro was free to move. No rotational marks were found on the gyro or inside the housing. The turn coordinator gyro was examined and no rotational scoring was found when removed from the housing. A small portion of the housing was fractured and missing. The attitude indicator gyro was free to move within its housing and the housing was intact. No rotational scoring was noted when the gyro was removed from the housing. The filament of the vacuum enunciator bulb # PL33[0] exhibited stretching.

Probable Cause: The total failure of the vacuum pump that resulted in an inoperative attitude gyro and spatial disorientation and a subsequent loss of aircraft control by the pilot. Factors were; the prevailing instrument meteorological conditions, and the dark night light condition.

Accident investigation:
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Investigating agency: NTSB
Report number: FTW04FA235
Status: Investigation completed
Duration: 10 months
Download report: Final report

Sources:

NTSB FTW04FA235

Revision history:

Date/timeContributorUpdates
11-Oct-2022 19:16 ASN Update Bot Added

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