N191FL

CONVAIR CV-440-79 · 1956 · Fixed-wing multi-engine · 2 engines · 52 seats · Valid Registration

Registered owner: IFL GROUP INC, MI (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
EDWARD A. MUELLEROperatoron 1993-10-27Operator named in NTSB report

Accident & incident history

Accident · 1993-10-27 Operator named in NTSB report
BEECH 200 No injuries Part 91EDWARD A. MUELLER

Operated by EDWARD A. MUELLER (per NTSB report)

Source: NTSB case LAX94LA030

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.

7 reports on file, 1995-01-13 – 2015-06-08.

OTHER · 2015-06-08 Matched by certificate designator
ATA 5311

Part: BELTFRAME — DENTED (FUSELAGE) · airframe 31,074 hrs · 29,170 cycles

DISCOVERED DAMAGED, DENTED, BELT FRAME AT STATION 395R FLOOR LEVEL..

Source: SDR VGCA20150608002
OTHER · 2015-06-08 Matched by certificate designator
ATA 5311

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 31,074 hrs · 29,170 cycles

DISCOVERED CRACKED BELT FRAME AT STATION 261L, FLOOR LEVEL.

Source: SDR VGCA20150608001
OTHER · 2015-06-08 Matched by certificate designator
ATA 5313

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,074 hrs · 29,170 cycles

DISCOVERED CRACKED STRINGER 22L AT STATION 210.

Source: SDR VGCA20150608003
OTHER · 2012-05-01 Matched by certificate designator
ATA 5711

Part: SPAR — CORRODED (ZONE 500) · airframe 29,676 hrs · 27,921 cycles

CORROSION LT AND RT WING, OUTER, UPPER REAR SPAR WS23-WS29.

Source: SDR VGCA201205010001
OTHER · 2011-05-17 Matched by certificate designator
ATA 5413

Part: LONGERON — CORRODED (RT NACELLE) · airframe 29,343 hrs · 27,636 cycles

RIGHT NACELLE STA 8 AND 6 LONGERON HAD SEVERE CORROSION.

Source: SDR VGCA20110517
OTHER · 2010-08-05 Matched by certificate designator
ATA 5413

Part: LONGERON — CORRODED (LT NACELLE) · airframe 29,004 hrs · 27,400 cycles

LEFT INBD UPPER NACELLE LONGERON HAD EXCESSIVE CORROSION.

Source: SDR VGCA20100805
OTHER · 1995-01-13 Unresolved
ATA 5320

Part: INTERCOSTAL — CRACKED (CABIN DOOR)

INTERCOSTAL FOUND CRACKED AT HANDRAIL SUPPORT RIVET HOLES. (2 PLACES.) CRACKS ARE SEVERE ENOUGH, CABIN DOOR HANDRAIL SUPPORT COULD COME FREE, CAUSING DOOR TO CONTACT GROUND. SUBMITTER RECOMMENDS PAYING SPECIAL ATTENTION TO THIS AREA DURING 150-HOUR INSPECTIONS.

Source: SDR 95ZZZX1032