N4167G

CESSNA 402B · 1976 · Valid Registration

Registered owner: W J MEDICAL CONSULTING, PR (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
W J MEDICAL CONSULTINGOperatoron 2024-07-11Operator named in NTSB report

Accident & incident history

Acc · 2024-07-11 Operator named in NTSB report
CESSNA 402B Fatal injury Part 91W J MEDICAL CONSULTING
Source: NTSB case ERA24FA301
Accident · 1978-07-28 Unresolved
Cessna 402B Serious injuryoperator not yet resolved
Source: NTSB case CHI78FEX27

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

1 report on file, 2004-04-05.

OTHER · 2004-04-05 Unresolved
ATA 5712

Part: RIB — CRACKED (LT WING) · airframe 11,745 hrs

RAMP INSP FOUND OIL CANNING IN LT WING OF HIGH TIME. WING WAS INSPECTED AND ONLY DEFECT FOUND WAS LWR FLANGE ON 4 OF INTERSPAR RIBS WERE CRACKED AT STRINGER PASS-THROUGH. CRACK WAS .5-.75 INCHES LONG AND USUALLY EXTENDED PAST FIRST RIVET. AFTER REPAIRING IAW SRM THE OIL CANNING WAS STILL EVIDENT. CONCLUSION THAT OIL CANNING SKIN IS NOT RESULT OF RIB CRACKS BUT CRACKS ARE DIRECT RESULT OF OIL CANNING SKIN. OIL CANNING WHEN A GENTLE LIFTING FORCE IS PLACED ON AFT END OF TIP TANK (CAUSE OF DAMAGE) AND POSSIBLY SOME LOOSE OR SMOKING RIVETS ON RIB LINE (RESULT OF THE DAMAGE) IF RIVETS ARE LOOSE OR SMOKING BE SURE TO INSPECT INNER STRUCTURE BEFORE PUTTING A BLIND FASTENER IN.

Source: SDR 2004FA0000391