N187AL

BEECH C90 · Fixed-wing multi-engine · 2 engines · 9 seats · Valid Registration

Registered owner: ALM HOLDINGS DELAWARE 2 LLC, DE (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

6 reports on file, 1995-12-01 – 2005-11-20.

OTHER · 2005-11-20 Matched by certificate designator
ATA 2435

Part: STARTER GEN — FAILED

DURING FLIGHT, AIRCRAFT GENERATOR FAILED. REPLACED STARTER/GENERATOR. (K)

Source: SDR ALG2005F00109
VIBRATION/BUFFET; WARNING INDICATION · 2005-08-24 Matched by certificate designator
ATA 7200

Part: ENGINE — VIBRATION

ON REPOSITION TO THE FLY AWAY, A LOUD BANG WAS HEARD FOLLOWED BY A NOTICEABLE CHANGE AND A VIBRATION IN THE AIRCRAFT. AC FELT UNSTABLE AND WAS SET DOWN. DURING COAST DOWN/ SHUTDOWN AC CONTINUED TO HAVE ODD VIBRATION/ OSCILLATION. MAINTENANCE NOTIFIED. REMOVED AND REPLACED ENGINE ASSY IAW MM AND THE APPLICABLE STC. WORK ACCOMPLISHED 8/28/2005. COMP, GRIND NOISE, OIL PUMP. (K)

Source: SDR ALG2005F00075
OTHER · 2001-06-14 Matched by certificate designator
ATA 6210

Part: SKIN — CORRODED (M/R BLADE)

DISCOVERED DURING ROUTINE AIRFRAME INSPECTION, FOUND CORROSION BENEATH OUTBOARD TRIM TAB, T/E EXTRUSION AND BLADE SKIN CORRODED BEYOND REPAIRABLE LIMITS.

Source: SDR ALG2001F00022
OTHER · 1998-03-12 Unresolved
ATA 5320

Part: BEAM — CRACKED (FUSELAGE)

ON DAILY INSPECTION FOUND CRACK NEAR AFT LEFT SIDE NODAL BEAM SUPPORT APPROXIMATELY .3 INCH OUTBOARD OF NODAL BEAM SUPPORT NEAR A RIVET HEAD .

Source: SDR 99ZZZX207
OTHER · 1996-09-03 Unresolved
ATA 6230

Part: LEVER ASSY — WORN (PYLON)

DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. SUBMITTER STATED NORMAL USE CAUSED PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 363.9.

Source: SDR 96ZZZX5514
OTHER · 1995-12-01 Unresolved
ATA 7810

Part: EXH COLLECTOR — CRACKED (PT SECTION)

PRE-FLIGHT OF AIRCRAFT, FOUND EXHAUST COLLECTOR CRACKED SHEET METAL; 2 PLACES, 3 O'CLOCK AND 9 O'CLOCK POSITIONS.

Source: SDR 96ZZZX108