# N8407C: 1976 Piper PA-34-200T, registration cancelled 2005-04-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 13, 2005
- Status when cancelled: Triennial form not returned
- Airframe: [Piper PA-34-200T](https://openairdocs.org/model/piper-pa-34-200t) (registry code 7103406)
- Engine: [Continental TSIO-360 series](https://openairdocs.org/engine/continental-tsio-360-series) (registry code 17019)
- Data sheets: [TCDS A7SO](https://openairdocs.org/tcds/A7SO), [TCDS E9CE](https://openairdocs.org/tcds/E9CE) (OpenAirDocs)
- Serial number: 34-7670137
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: January 22, 1976
- Certificate issued: October 2, 1980
- Last registry action: March 15, 2005
- Mode S code: AB8329
- Owner when cancelled: [Airpac Airlines Inc](https://openairdocs.org/faa-owner/AIRPAC%20AIRLINES%20INC)
- Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)
- Owner type: Corporation
- Owner's area on the map: 47.5351° N, 122.3059° W: Placed by OpenAirDocs at the center of ZIP code 98108, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8407C
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8407C
- Page: https://openairdocs.org/deregistered/N8407C-2005-04-13

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Piper PA-34-200T: https://openairdocs.org/model/piper-pa-34-200t.md

## Service difficulty reports (11)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 97ZZZX3713](https://openairdocs.org/sdr/97ZZZX3713), Jul 29, 1997: STABILIZER. RIVETS SHEARED. EIGHT RIVETS WERE SHEARED ON BOTH SIDES OF VERTICAL STABILIZER (WHERE VERTICAL STABILIZER ATTACHED TO EMPENNAGE). SUBMITTER STATED THIS MAKES SIX AIRPLANES IN F
- [SDR 97ZZZX3169](https://openairdocs.org/sdr/97ZZZX3169), Jun 26, 1997: ALTERNATOR. DEFECTIVE. AFTER ONLY 109 HOURS ON THE OVERHAULED ALTERNATOR, IT WOULD NOT FUNCTION PROPERLY (I.E., PARALLEL, SHARE THE LOAD, REMAIN ON-LINE). UPON REMOVAL OF THE BRUSHES,
- [SDR 96ZZZX6106](https://openairdocs.org/sdr/96ZZZX6106), Nov 20, 1996: ALTERNATOR. CASE CRACKED. ALTERNATOR REMOVED DUE TO DEFECTIVE DIODES, BUT ALSO FOUND CRACK IN CASE AT DRIVE END.
- [SDR 96ZZZX6105](https://openairdocs.org/sdr/96ZZZX6105), Nov 19, 1996: NOSE GEAR. FROZEN. AIRCRAFT DEPARTED BOEING FIELD WITH SNOW ON TAXIWAY AND RUNWAY. SNOW SLUSH ENTERED NOSE WHEEL WELL AND FROZE GEAR IN 'UP' POSITION. AIRCRAFT LANDED ON RUNWAY WI
- [SDR 96ZZZX5713](https://openairdocs.org/sdr/96ZZZX5713), Oct 30, 1996: PUMP. FAILED. ENGINE DRIVEN FUEL PUMP DEVELOPED EXCESSIVE OUTPUT. (HIGH PRESSURE) FOUND FUEL IN DECK REFERENCE LINE, INDICATING INTERNAL LEAKAGE.
- [SDR 96ZZZX5712](https://openairdocs.org/sdr/96ZZZX5712), Oct 24, 1996: BRACKET. CRACKED. RIGHT MAIN GEAR 'UP' LIGHT SWITCH MOUNTING BRACKET CRACKED ALLOWING SWITCH TO FLEX AWAY FROM TRUNNION ON RETRACTION. THIS CAUSED RED 'UNSAFE' LIGHT TO STAY 'ON'
- [SDR 96ZZZX5711](https://openairdocs.org/sdr/96ZZZX5711), Oct 15, 1996: CENTERING SPRING. SHAFT BROKEN. CENTER SHAFT OF NOSE GEAR CENTERING SPRING FOUND SHEARED AT ROD END FITTING. VISUAL INSPECTION INDICATED SHAFT HAD BEEN CRACKED VERTICALLY ON BOTH SIDES OF CENT
- [SDR 96ZZZX5710](https://openairdocs.org/sdr/96ZZZX5710), Oct 15, 1996: HSI. FAILED. HEADING FUNCTION OF HSI FAILED JUST PRIOR TO ENTERING IMC. MOTOR INSIDE INSTRUMENT BURNED OUT. SUBMITTER STATED OPERATOR'S FLEET HAS MANY, MANY FAILURES OF NSD-
- [SDR 96ZZZX5727](https://openairdocs.org/sdr/96ZZZX5727), Oct 14, 1996: TERMINAL STRAP. BURNED. BRAIDED-WIRE-TYPE BATTERY TERMINAL STRAP BECAME LOOSE AT NEGATIVE TERMINAL CAUSING HIGH RESISTANCE, HEAT, AND ARCING, AND TOTAL ELECTRICAL SYSTEM FAILURE (INTER
- [SDR 96ZZZX2510](https://openairdocs.org/sdr/96ZZZX2510), Apr 23, 1996: CRANKCASE. CRACKED. SMALL CRACK FOUND IN RIGHT SIDE OF CRANKCASE NEXT TO THROUGH-BOLT JUST FORWARD OF CYLINDER NR 5. CONSIDERED NON-CRITICAL AREA PER SB M90-17.
- [SDR 95ZZZX7028](https://openairdocs.org/sdr/95ZZZX7028), Oct 24, 1995: BRACKET. CRACKED. FLAP HANDLE BRACKET IS CRACKED AT BOTH LOWER FORWARD BEND RADIUS NEXT TO ATTACH POINTS TO AIRFRAME. SECOND UNIT IN FLEET IN SAME CONDITION.

## FAA accident and incident reports (2)

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.

- [Incident 19890928053389I](https://openairdocs.org/incident/19890928053389I), Sep 28, 1989: Piper PA34200T (N8407C), Portland, OR. Left engine lost power. Returned. Landed safely. Found throttle extension fitting had broken.
- [Incident 19810511030509I](https://openairdocs.org/incident/19810511030509I), May 11, 1981: Piper PA34200T (N8407C), Spokane, WA, Minor damage. Right wingtip struck fence on taxiway. Minor damage to aircraft and fence.

## Other aircraft with N8407C

- [Cancelled 1950-04-13](https://openairdocs.org/deregistered/N8407C-1950-04-13): Curtiss Wright C-46D, S/N 22218. Owner: [C.A.T. Inc](https://openairdocs.org/faa-owner/C.A.T.%20INC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)

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