N211CC

CESSNA 680 · 2005 · Valid Registration

Registered owner: ORCHARD AVIATION LLC, MI (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
FIRST WING MANAGEMENT, LLC (F27A)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 1979-02-24 Unresolved
Swearingen SA26T None injuryoperator not yet resolved
Source: NTSB case CHI79FEE40

Maintenance disclosures

O · 2023-06-18 Matched by certificate designator
ATA 2100

DEPRESSURIZATION - EMERGENCY DESCENT. AIRCRAFT WORKED BY MANUFACTURER AND FOUND THAT AN AIR CONDITIONING SYSTEM DUCT CAME LOOSE.

Source: SDR 1JAA20230618002 · FAA SDRS
B · 2020-05-28 Matched by certificate designator
ATA 2120

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.

Source: SDR F27A2020060200001 · FAA SDRS
R · 2015-08-20 Matched by certificate designator
ATA 7321

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.

Source: SDR UG8A2015082001 · FAA SDRS
O · 2015-07-24 Matched by certificate designator
ATA 5730

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.

Source: SDR UG8A2015072401 · FAA SDRS
O · 2015-07-21 Matched by certificate designator
ATA 5512

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.

Source: SDR UG8A201507210001 · FAA SDRS