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N75340

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1976 Piper PA-28R-200 · Lycoming I0360 series

Open in FAA registry

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Registered owner
High Point Aviation LLC
Location
Spencerport, NY
Owner type
LLC
Serial number
28R-7635292
Year built
1976
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
May 17, 1976
Certificate issued
March 8, 2016
Expires
March 31, 2029
Mode S code
AA282B
Piper PA-28R-200Airframe model · 4 seats · 1 engine · 1,223 registeredTCDS 2A13Airframe · Piper PA-28R-200TCDS 1E10Engine · Lycoming I0360 series

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
See all 91 ADs

Information bulletins that may apply · 28

Advisory, not mandatory.

See all 32 bulletins

NTSB investigations

No NTSB investigations matched to N75340Matched 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

No FAA accident or incident reports matched to N75340Matched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piper PA-28R-200 aircraft

Service difficulty reports · 8

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

SDR 2005FA0001360Skin · crackedAT CABIN ENTRANCE, WING WALK, FOUND SUPPORT PANEL UNDER WING WALK CRACKED. FAILURE DUE TO REPEATED WALKING ON. IF FACTORY STAMPED SUPPORT OUT OF HEAVIER, THICKER PANEL, MAY HELP PROLONG FAILURE. (EA21200507814) (K)Sep 14, 2005 · N75340 · Piper PA28R200 · Fuselage Main, Plate/SkinSDR 96ZZZX5029Hinge Pin · failedDURING PRE-FLIGHT RUN UP, POWER WAS LIMITED TO 1,900 RPM. THE ALTERNATE AIR DOOR WAS FOUND IN THE FUEL METERING UNIT, THE HINGE PIN HAD WORN COMPLETELY THROUGH IN 600 HOURS OF OPERATION. (ONE YEAR AT FLIGHT SCHOOL). SUBMITTER RECOMMENDATION, A TAB ON THE ALSep 2, 1996 · N75340 · Piper PA28R200 · Engine Air Intake SystemSDR 96ZZZX5030Trim Tab · crackedDURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND TO BE CRACKED: UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS., ON BOTH LT AND RT TRIM Jul 1, 1996 · N75340 · Piper PA28R200 · Elevator, Tab StructureSDR 96ZZZX3543Trim Tab · crackedDURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIMJun 19, 1996 · N75340 · Piper PA28R200 · Horizontal Stabilizer, Tab StructureSDR 96ZZZX3542Trim Tab · crackedDURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIMJun 19, 1996 · N75340 · Piper PA28R200 · Horizontal Stabilizer, Tab StructureSDR 96ZZZX3529Crankcase · crackedDURING 100-HOUR INSPECTION, THE CRANKCASE WAS FOUND CRACKED (2 INCHES). THIS WAS THE SAME CRACK THAT WAS FOUND 2 YEARS AGO WHEN THE ENGINE HAD 1,500 HOURS TSMO. THE CASE HALVES WERE REPLACED AND NOW 1,000 HOURS LATER, THE SIMILAR CRACK HAS RE-APPEARED. SUSPJun 19, 1996 · N75340 · Piper PA28R200 · Reciprocating Engine Power SectionSDR 96ZZZX2468Power Pack · defectiveAFTER OPERATING FOR 500 HOURS, THE HYDRAULIC POWER PACK BEGAN TO CAVITATE EITHER BECAUSE OF AIR OR CONTAMINATION. THE SM INSTRUCTIONS CLEARLY STATE 'OPERATE PUMP TO PURGE AIR FROM SYSTEM' WHENEVER REPLACING THE PUMP, A CYLINDER, OR A LINE. UNFORTUNATELY, THEApr 3, 1996 · N75340 · Piper PA28R200 · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX2119Mount · crackedFLIGHT CREW MEMBER IDENTIFIED CRACK ON ENGINE MOUNT RING TUBE ADJACENT TO DIP STICK. INTERESTINGLY, THIS CRACK IS IDENTICAL TO THOSE FOUND ON AIRCRAFT AFFECTED BY PIPER SL 568. SUBMITTER RECOMMENDS A REVIEW/EXPANSION OF THIS SL AND THE ADDITION OF REINFORCEMApr 4, 1995 · N75340 · Piper PA28R200 · Engine Mount Section

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