N575U
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ERA AVIATION INC | Operator | on 2013-10-23 | Operator named in NTSB report |
Accident & incident history
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.
4 reports on file, 2010-06-14 – 2012-01-22.
Part: SWITCH — OUT OF ADJUST (CABIN DOOR) · airframe 27,800 hrs · 35,000 cycles
CABIN WARNING DOOR LIGHT CAME ON. ADJUSTED CABIN DOOR SILL SWITCH, REFERENCE BEECH 1900C MAINTENANCE MANUAL 52-70-00. OPS CHECK GOOD.
Part: DOOR FRAME — CRACKED (FS 458.3)
DURING THE 3RD, 200 HR INTERVAL, DETAILED INSP, A CRACK WAS DISCOVERED IN THE UPPER FWD CORNER OF THE AFT CARGO DOOR FRAME. THE CRACK WAS LOCATED IN THE UPPER LEG OF THE DOOR FRAME STARTING AT FS 458.3 AND EXTENDED AFT HORIZONTALLY ABOUT 4". THE CRACK WAS JUST UNDER THE EDGE OF THE FUSELAGE SKIN LAP AND VISIBLE ONLY FROM THE INSIDE.
Part: SPAR CAP — CORRODED (HORIZONTAL STAB)
HORIZONTAL STABILIZER REAR SPAR, RT LOWER CAP, FOUND CORRODED INBD AND OTBD OF THE HSS 66.0 CENTER ELEVATOR HINGE LOCATION.
Part: CHANNEL — CRACKED (ZONE 100) · airframe 26,160 hrs · 33,308 cycles
DURING NR 3 PHASE INSP THE LOWER DOOR FRAME CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL, PN 114-420041-41, RUNS FROM FUSELAGE STA 150.60 TO STA 177.35 ACROSS THE BOTTOM OF THE DOOR OPENING. THE CRACK WAS LOCATED IN THE BEND RADIUS OF THE OTBD SUPPORT FLANGE AND EXTENDED APPROX 3.25 AFT FROM THE CTR CUTOUT. REPLACED THE CRACKED CHANNEL WITH NEW IAW SRM, CHAP 51-00-00.