N138DM
Registered owner: MLD 605 LEASING LLC, IN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Image Air Charter LLC (BLUA) | Certificate holder | — | Matched by certificate designator |
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.
8 reports on file, 2018-01-11 – 2023-02-03.
Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 5,470 hrs · 3,148 cycles
LEFT AND RIGHT WING FUEL TANK ACCESS PANELS 510CB, 540AB, 610AB, 640AB, 640BB LIGHT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-57-25-1062.
Part: SKIN — CORRODED (ZONE 100) · airframe 5,470 hrs · 3,148 cycles
LEFT AND RIGHT LOWER FUSELAGE SKIN AT FORWARD BELLY FAIRING ATTACHMENTS LIGHT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-53-21-420.
Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 5,470 hrs · 3,148 cycles
LEFT AND RIGHT WING FUEL ACCESS OPENINGS, 510AB,540AB & 610AB LIGHT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-57-25-1060
Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 5,470 hrs · 3,148 cycles
LEFT AND RIGHT FUEL PANELS 540AB & 610AB CORROSION ON CLAMPING RINGS. REPAIRED UNDER BOMBARDIER REO 604-57-25-1061.
Part: SPAR CAP — CORRODED (ZONE 500) · airframe 5,470 hrs · 3,148 cycles
LEFT WING FRONT SPAR CAP LIGHT CORROSION AT STATION BL 45. REPAIRED UNDER BOMBARDIER REO 604-57-22-108.
Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 5,470 hrs · 3,148 cycles
RIGHT WING LOWER PLANK ACCESS PANELS 640AB & 640BB LIGHT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-57-25-1057.
Part: SKIN — CORRODED (ZONE 200) · airframe 5,470 hrs · 3,148 cycles
AFT FUSELAGE SKIN AT APU EXHAUST CUTOUT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-53-42-490
Part: TUBE — CHAFED (HYD SYSTEM) · airframe 2,959 hrs · 1,552 cycles
TUBE WAS CHAFED AT TWO LOCATIONS UNDER ADEL CLAMPS USED FOR ROUTING THE STAINLESS STEEL TUBE. WEAR WAS NOT TO THE POINT OF CAUSING ANY LEAKAGE IN THIS 3000 PSI PRESSURE LINE. THESE WERE BOTH LOCATIONS REQUIRED FOR INSPECTION WHEN PERFORMING SB 605-29-008. CONDITION WAS FOUND DURING COMPLIANCE WITH THIS SB.