N211CC
Registered owner: ORCHARD AVIATION LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| First Wing Management, LLC (F27A) | Certificate holder | — | Matched by certificate designator |
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.
5 reports on file, 2015-07-21 – 2023-06-18.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 4,964 hrs · 3,577 cycles
DEPRESSURIZATION - EMERGENCY DESCENT. AIRCRAFT WORKED BY MANUFACTURER AND FOUND THAT AN AIR CONDITIONING SYSTEM DUCT CAME LOOSE.
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 3,788 hrs · 2,889 cycles
DURING CLIMB OUT CREW NOTICES AN OIL SMELL AND HAZE IN COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND LANDED AT KOKK. DISPATCHED MAINTENANCE TO THE AIRCRAFT, COULD NOT DUPLICATE DISCREPANCY ON THE GROUND. RETURNED AIRCRAFT TO KEYE FOR FURTHER TROUBLESHOOTING OF DISCREPANCY.
Part: FUEL CONTROL — CLOGGED (ENGINE) · airframe 3,012 hrs · 2,378 cycles
UPON CROSS FLOW, RT TANK TO LT ENG, CAUSES ENG FLUCTUATIONS. INSTALLED IN-LINE FUEL STRAINERS IN THE PROPER POSITION. ACFT WAS FLOWN & FOUND TO BE WITHOUT DEFECTS.
Part: SKIN — CORRODED (RT WING) · airframe 3,010 hrs · 2,377 cycles
DURING INSPECTION OF RT UPPER WING SKIN ASSEMBLIES AT WS 37.00, CORROSION WAS FOUND AT 3 LOCATIONS. DAMAGE AREA A , BETWEEN CTR SPAR & AFT SPAR INBD OF WS 37. DAMAGE AREA B, BETWEEN CTR SPAR & AFT SPAR OTBD OF WS 37. DAMAGE AREA C, BETWEEN FWD SPAR & CTR SPAR OTBD OF WS 37. BLENDED 3 LOCATIONS OF CORROSION AT WS 37 IAW REPORT S-0-0034 04RD. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS IAW THE MODEL 680 NON-DESTRUCTIVE TESTING MANUAL, PART 6 EDDY CURRENT, CHAPTER 20-00-02, EDDY CURRENT SURFACE TECHNIQUES GENERAL. DETERMINED MATERIAL THICKNESS REMAINING IS WITHIN THE LIMITS SHOWN IN TABLE 2 0-1 OF REPORT S-680-0034 04RD. CLEANED, TREATED & PRIMED THE BLENDED AREAS IAW SRM, CHAPTER 51-20-01. PROTECTIVE TREATMENT OF METAL. RE-INSTALLED EXISTING TYPE & SIZE FASTENERS OF SUITABLE LENGTHS IAW THE SRM CHAPTER 51-40-03.
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 3,010 hrs · 2,377 cycles
FOUND SEVERAL AREAS OF CORROSION ON THE UPPER & LOWER SIDES OF PANELS 351AC & 52AC, JUST INBD OF HORIZONTAL STABILIZER REAR SPARS. BLENDED & REMOVED CORROSION IN AFFECTED AREAS, NDT FINDINGS SHOW REMAINING THICKNESS TO BE BEYOND ALLOWABLE LIMITS IAW SRM 51-10-01. DAMAGES WERE SUBMITTED FOR EVALUATION. COMPLIED WITH REPAIR S-680-0034 03RD REV DATED 6 23 15.