N37127

CESSNA 404 · 1977 · Fixed-wing multi-engine · 2 engines · 8 seats · Valid Registration

Registered owner: RICHLAND AVIATION INC, MT (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Richland Aviation, Inc. (HTKA)Certificate holderMatched by certificate designator
Key Lime Air Corporation (KY7A)Operatoron 2009-06-05Operator named in NTSB report

Accident & incident history

Accident · 2009-06-05 Operator named in NTSB report
CESSNA 404 No injuries Part 135Key Lime Air Corporation

Operated by KEY LIME AIR CORPORATION (per NTSB report)

Source: NTSB case CEN09CA343

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, 2009-06-05 – 2019-10-28.

OTHER · 2019-10-28 Matched by certificate designator
ATA 8500

Part: ENGINE — MALFUNCTIONED

ENGINE DEVELOPED LOW OIL PRESSURE IN FLIGHT APPROX 20 PSI. REMOVED AND CLEANED OIL PRESSURE RELIEF PLUNGER. FOUND CARBON BITS IN OIL FROM CAVITY. ABOUT 20 HOURS LATER THE LOW OIL PRESSURE RETURNED. REMOVED OIL PRESSURE RELIEF PLUNGER. MORE CARBON BITS FOUND IN OIL FROM THE CAVITY. CLEANED CAVITY AND INSTALLED NEW PLUNGER, SPRINGER AND SEAT. OIL AND FILTER CHANGED. 1.1 HOURS LATER LOW OIL PRESSURE. THIS TIME THE NEW PLUNGER IS BADLY PITTED FROM DEBRIS AND FLAKES OF METAL ARE FOUND IN THE OIL FROM THE CAVITY. ENGINE REMOVED FROM SERVICE UNTIL THE SOURCE OF THE MATERIAL CAN BE DETERMINED. SENT OIL PUMP TO CONTINENETAL FOR EVALUATION. THE ENGINE HAS BEEN IN SERVICE SINCE 05/2018. IT IS FACTORY REBUILT ENGINE.

Source: SDR 2020FA0000006
WARNING INDICATION · 2013-06-19 Matched by certificate designator
ATA 3231

Part: DOOR — BINDING (NLG) · airframe 17,921 hrs

NOSE GEAR FAILED TO EXTEND ON APPROACH. PILOT ABORTED APPROACH AND CONDUCTED TROUBLESHOOTING AND EMERGENCY EXTENSION PROCEDURES WITH NO EFFECT ON NOSE GEAR. PILOT DIVERTED AND CONDUCTED LANDING WITH NOSE GEAR RETRACTED. MX RECOVERED ACFT AND FOUND NOSE GEAR DOORS WERE JAMMED CLOSED; ONCE FREED THE NOSE GEAR EXTENDED NORMALLY. FURTHER MX TROUBLESHOOTING FOUND THAT THE NOSE GEAR HAD OVER-RETRACTED, CAUSING NOSE GEAR DOORS TO JAM CLOSED. RIGGING OF NOSE GEAR, UPLOCKS, AND DOORS ALL APPEARED NORMAL DURING MX TROUBLESHOOTING. MX PERSONNEL WERE ABLE TO DUPLICATE MALFUNCTION BY APPLYING MODERATE UPWARD PRESSURE TO THE NOSE GEAR DURING RETRACTION. MX SUSPECTS THAT TURBULENCE COULD HAVE CAUSED THE OVER-RETRACTION; THE PILOT REPORTED THAT THERE WAS SIGNIFICANT TURBILENCE ON THE INCIDENT NIGHT.

Source: SDR KY7A20130624001
OTHER · 2012-05-25 Matched by certificate designator
ATA 5280

Part: HINGE — CRACKED (NLG DOOR) · airframe 17,450 hrs

NLG FAILED TO EXTEND DURING NORMAL OPERATIONS DURING TRAINING FLIGHT. FLIGHT CREW PERFORMED EMERGENCY LANDING GEAR EXTENSION PROCEDURES; NOSE GEAR EXTENDED AND LOCKED. FLIGHT CREW PERFORMED NORMAL LANDING WITH NO FURTHER DIFFICULTY. MX PERSONNEL INSPECTED ACFT AND FUNCTIONALLY CHECKED LANDING GEAR RETRACTION/EXTENSION SYS. MX FOUND CRACKED HINGE ON 1 NOSE GEAR DOOR WHICH CAUSED THE DOORS TO JAM IN THE CLOSED POSITION.

Source: SDR KY7A12052501
FLUID LOSS; WARNING INDICATION · 2009-06-05 Matched by certificate designator
ATA 2910

Part: LINE — FAILED (HYD SYSTEM) · airframe 17,139 hrs

HYDRAULIC LINE FAILURE CAUSED TOTAL LOSS OF FLUID PREVENTING NORMAL GEAR EXTENSION. EMERGENCY BLOWDOWN FAILED DUE TO FAILURE OF PNEUMATIC LINE FAILURE AT BLOWDOWN BOTTLE.

Source: SDR KY7A14634
FLUID LOSS · 2009-06-05 Matched by certificate designator
ATA 2910

Part: LINE — FRACTURED (HYD SYSTEM) · airframe 17,139 hrs

HYDRAULIC PRESSURE LINE FAILURE IN RIGHT WING LEADING EDGE BETWEEN FLOW VALVE AND FILTER HOUSING OCCURRED IN 90° BEND.

Source: SDR KY7A14634A