Registered owner
Star Marianas Air Inc
Owner type
Corporation
Serial number
32-40445
Year built
1968
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
February 12, 1968
Certificate issued
June 4, 2009
Expires
August 31, 2027
Mode S code
A4DEEB

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.

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Airworthiness directives that may apply · 92

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

1967In forceSuperseded2026
ADs by the year they took effect: 108 ADs
19672
19682
19692
19702
19713
19723
19731
19743
19754
19761
19774
19782
19793
19805
19811
19831
19841
19861
19893
19912
19922
19931
19951
19964
19972
19984
19991
20001
20023
20032
20042
20053
20066
20084
20091
20103
20112
20125
20132
20152
20173
20201
20211
20222
20231
20242
20261
See all 112 ADs

Information bulletins that may apply · 26

Advisory, not mandatory.

See all 29 bulletins

NTSB investigations · 1

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

FAA incident reports · 3

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 1SMA2021020401Spar · crackedINDICATION OF CRACK/DEFECT DETECTED WHICH EXCEEDED THE ALLOWABLE THRESHOLD ON RIGHT HAND WING OUTBOARD AFT WING SPAR BOLT HOLE DURING EDDY CURRENT INSPECTION REQUIRED BY AD 2020-26-16Feb 4, 2021 · N4127R · Piper PA32300 · Wing SparSDR 2012FA0000833Magneto · out of sequencePILOT REPORTED THAT SHORTLY AFTER TAKEOFF, FELT A SURGING, BUT DID NOT SEE ANY APPRECIABLE INDICATION ON THE RPM, MANIFOLD PRESSURE OR FUEL FLOW INDICATORS. ON DOWNWIND LEG AFTER DEPARTURE, NOTICEABLE LOSS OF POWER OCCURRED WITH A CORRESPONDING LOSS OF RPM.Dec 24, 2012 · N4127R · Piper PA32300 · Magneto/DistributorSDR 1SMA2012FA0000032Tire · defectiveWHILE SECURING ACFT AFTER FLIGHT, PILOT REPORTED RT MAIN TIRE WAS FLAT. INVESTIGATION REVEALED THAT ONE COMPLETE SECTION OF TREAD HAD DEBONDED AND COME OFF OF TIRE AND WRAPPED AROUND MAIN WHEEL FAIRING SUPPORT CAP ON AXLE END, CAUSING DAMAGE TO THE TUBE VALVEJan 18, 2012 · N4127R · Piper PA32300 · Tire TubeSDR 21200003002Alternator · fouledON APPROACH, ELECTRICAL POWER LOSS. AFTER CONTACT WITHTOWER, COMM 1 RADIO TURNED OFF, WITHIN 3-5 SEC C/B FOR ALTERNATOR OUTPUT TRIPPED & INSTRUMENT PANEL LIGHTS DIMMED, AMP GAUGE SHOW DISCHARGE OF BATTERY. TURNED OFF NON ESSENTIAL ELECTRICAL EQUIPMENT & RESEFeb 1, 2005 · N4127R · Piper PA32300 · DC Generator-AlternatorSDR 21200003001Muffler · fatiguedDURING MX CHK, MILD CORROSION IDENTIFIED ON INTERNAL AREA OF DEFECTIVE PARTS. MULTIPLE FRAGMENTS OF METAL RANGING FROM 0.25 INCH TO 1.25 INCH DIAMETERS INSIDE OF INTERNAL BAFFLE. INSP OF EXHAUST COMPONENT FAILURES. EXHAUST MUFFLER, PN 6879900, OVERHAULED OJan 2, 2005 · N4127R · Piper PA32R300 · Engine Noise Suppressor

STCs that may be installed · 357

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

See all 357 STCs