N137YV

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Air Methods Corp. (QMLA)Operatoron 1992-04-04Operator named in NTSB report

Accident & incident history

Incident · 1992-04-04 Operator named in NTSB report
BEECH 1900C No injuries Part 135Air Methods Corp.

Operated by AIR MIDWEST INC. (per NTSB report)

Source: NTSB case FTW92IA104

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, 1995-03-01 – 1995-10-02.

OTHER · 1995-10-02 Unresolved
ATA 5753

Part: SKIN — CRACKED (RT TE FLAP)

RIGHT OUTBOARD FLAP CRACKED .75 INCH ON TRAILING EDGE, 35 INCHES FROM OUTBOARD END OF FLAP. STOPPED DRILLED AND INSTALLED DOUBLER. (M)

Source: SDR 95ZZZM592
OTHER · 1995-08-19 Unresolved
ATA 7120

Part: TRUSS — CRACKED (RT ENGINE)

DURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M)

Source: SDR 95ZZZM589
OTHER · 1995-08-12 Unresolved
ATA 5753

Part: FLAP — CRACKED (LT WING)

DURING ROUTINE MAINTENANCE, A .5 INCH CRACK WAS FOUND INBOARD OF ATTACH POINT. REPAIRED WITH PATCH. (M)

Source: SDR 95ZZZM479
OTHER · 1995-05-10 Unresolved
ATA 5753

Part: SKIN — CRACKED (RT TE FLAP)

DURING SCHEDULED MAINTENANCE, A 1.5 INCH CRACK WAS FOUND ON RIGHT OUTBOARD FLAP, 16 INCHES INBOARD OF END CAP AND 5 INCHES AFT OF LEADING EDGE. REPAIRED BY STOP DRILLED CRACK AND INSTALLED DOUBLER. (M)

Source: SDR 95ZZZM199
OTHER · 1995-04-27 Unresolved
ATA 5753

Part: LE SKIN — CRACKED (LT TE FLAP)

FLAP CRACKED .75 INCH ON BOTTOM LEADING EDGE, 4TH RIB INBOARD. STOP DRILLED AND INSTALLED DOUBLER, ON LT TE FLAP (P/N 35165050258). CRACK WAS FOUND DURING SCHEDULED MAINTENANCE. (M)

Source: SDR 95ZZZM17
OTHER · 1995-04-27 Unresolved
ATA 5753

Part: SKIN — CRACKED (LT TE FLAP)

FLAP IS CRACKED .5 INCH BETWEEN THIRD AND SECOND RIB FROM INBOARD END ON BOTTOM OF FLAP ON SPAR LINE AND A .75 INCH CRACK ON BOTTOM LEADING EDGE THIRD RIB FROM OUTBOARD END OF TE FLAP (P/N 35165050258). STOP DRILLED CRACKS AND INSTALLED DOUBLER CRACKS WERE FOUND DURING SCHEDULED MAINTENANCE.

Source: SDR 95ZZZM18
OTHER · 1995-03-01 Unresolved
ATA 5753

Part: FLAP — CRACKED (RT WING INBD)

DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 2 INCH CRACK IN THE BOTTOM SKIN ALONG THE TRAILING EDGE BETWEEN THE THIRD AND FOURTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER.

Source: SDR 95ZZZX1938