Registered owner
Geipel William Robert
Owner type
Individual
Serial number
34-7770013
Year built
1976
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 8, 1976
Certificate issued
May 20, 2024
Expires
May 31, 2031
Mode S code
A6D10F

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-360 model are included below.

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Airworthiness directives that may apply · 56

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1971In forceSuperseded2026
ADs by the year they took effect: 62 ADs
19711
19742
19753
19771
19781
19791
19802
19812
19862
19882
19911
19922
19932
19941
19952
19961
19971
19985
19992
20002
20021
20031
20055
20061
20082
20091
20103
20111
20123
20132
20222
20234
See all 69 ADs

Information bulletins that may apply · 18

Advisory, not mandatory.

See all 19 bulletins

NTSB investigations

No NTSB investigations matched to N5384FMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-34-200T aircraft

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 5

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

SDR 96ZZZX2762Impulse Coupler · cam splitMAGNETO IMPULSE COUPLER CAM SPLIT IN HALF DURING RE-INSTALLATION ON MAGNETO DURING MAGNETO 500-HOUR INSPECTION AND IMPULSE COUPLER AD 78-09-07R3.May 13, 1996 · N5384F · Piper PA34200T · Magneto/DistributorSDR 95ZZZX7035Bracket · crackedDURING INSPECTION, THE FLAP HANDLE BRACKET WAS FOUND CRACKED IN 2 PLACES ALONG GUIDE PIN TRACKS AT THE 10 DEGREE FLAP NOTCH AND AT THE 25 DEGREE FLAP NOTCH. BOTH CRACKS RADIATE FROM THE NOTCHES FORWARD TOWARD THE FORWARD EDGE OF THE BRACKET. THERE IS ALSO 1 Oct 9, 1995 · N5384F · Piper PA34200T · Trailing Edge Flap Control SystemSDR 95ZZZX6058Fitting · rivets looseFOUND 3 RIVETS WERE LOOSE ON THE LOWER AFT VERTICAL FIN-TO-FUSELAGE ATTACHMENT FITTING. THE RIVETS THAT ARE LOOSE ARE THE LOWER OUTBOARD CORNER RIVETS.Oct 8, 1995 · N5384F · Piper PA34200T · Vertical Stabilizer, Attach FittingsSDR 95ZZZX6056Turbocharger · housing crackedFOUND TURBINE HOUSING CRACKED. HOUSING IS DEFECTIVE EXACTLY AS IDENTIFIED IN AD 82-27-03, EVEN THOUGH IT IS LATEST (GOOD) PART NUMBER. THESE HOUSINGS CRACK JUST LIKE THE ORIGINAL AND ARE REALLY NOT ANY BETTER (THIS IS THE 'DN' HOUSING).Sep 25, 1995 · N5384F · Piper PA34200T · Exhaust TurbochargerSDR 95ZZZX3473Casting · crackedFOUND FORWARD CASTING OF ALTERNATOR CRACKED ADJACENT TO MOUNTING FLANGE SUPPORT BRACE. SUBMITTER KNOWS OF OTHER INSTANCES OF CRACKS IN THIS AREA ON SAME MAKE AND MODEL ALTERNATORS. FRAME IS CRACKED FROM FORWARD TO AFT ENDS ALL THE WAY THROUGH.Jun 21, 1995 · N5384F · Piper PA34200T · DC Generator-Alternator

STCs that may be installed · 320

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 320 STCs