Owner type
Co-owned
Serial number
28R-7335072
Year built
1972
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
November 14, 1972
Certificate issued
April 1, 2014
Expires
April 30, 2027
Mode S code
A0E075

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.

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Airworthiness directives that may apply · 76

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

1964In forceSuperseded2026
ADs by the year they took effect: 89 ADs
19641
19661
19672
19693
19712
19724
19732
19741
19753
19761
19774
19781
19792
19802
19811
19822
19861
19892
19911
19921
19931
19941
19951
19965
19971
19984
20001
20011
20021
20032
20041
20052
20066
20071
20083
20091
20103
20111
20123
20131
20151
20172
20182
20212
20222
20242
20261
See all 91 ADs

Information bulletins that may apply · 28

Advisory, not mandatory.

See all 32 bulletins

NTSB investigations

No NTSB investigations matched to N15597Matched 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-28R-200 aircraft

FAA incident reports · 1

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 · 6

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

SDR 97ZZZX1699Filler Neck · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION. FOUND THE FUEL TANK FILLER NECK CORRODED THROUGH INTO THE FUEL Mar 27, 1997 · N15597 · Piper PA28R200 · Fuel StorageSDR 97ZZZX1698Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.Mar 27, 1997 · N15597 · Piper PA28R200 · Wing, Fuselage Attach FittingsSDR 97ZZZX1697Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.Mar 27, 1997 · N15597 · Piper PA28R200 · Wing, Fuselage Attach FittingsSDR 97ZZZX1702Mount · crackedMOST OF THE TUBES ON THIS ENGINE/LANDING GEAR MOUNT HAD TO BE REPLACED DUE TO CORROSION, CRACKS, OR CHAFING. THE CHAFING WAS FROM OLD LOOP-TYPE (ADEL) CLAMPS THAT HAD NOT BEEN REPLACED WHEN THE RUBBER CUSHIONS DRIED OUT. THE AIRCRAFT HAD BEEN IN AN ACCIDENT Mar 26, 1997 · N15597 · Piper PA28R200 · Engine Mount SectionSDR 97ZZZX1701Pitot Head · corrodedTHE PITOT MAST WAS SO CORRODED THE AIR INLET HOLES WERE CLOSED APPROXIMATELY ONE-FOURTH DUE TO THE BUILD-UP OF THE CORROSION. SUBMITTER STATED THE AIRCRAFT HAD BEEN BASED IN A CORROSIVE ENVIRONMENT (FLORIDA).Mar 26, 1997 · N15597 · Piper PA28R200 · Pitot/Static SystemSDR 97ZZZX1700Belt · failedA COMMON PROBLEM THAT SUBMITTER HAS FOUND OVER THE YEARS, WITH PIPER PRODUCTS ESPECIALLY, IS THE USE OF AUTOMOTIVE OR UNAPPROVED ALTERNATOR DRIVE BELTS. IN THIS CASE, A NAPA AUTOMOTIVE BELT WAS INSTALLED.Mar 26, 1997 · N15597 · Piper PA28R200 · Alternator-Generator Drive

STCs that may be installed · 398

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

See all 398 STCs