N55NW

CIRRUS DESIGN CORP SR22T · 2023 · Fixed-wing single-engine · 1 engine · 5 seats · Valid Registration

Registered owner: LR AVIATION LLC, TX (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
CJ Systems Aviation GroupOperatoron 2002-01-20Operator named in NTSB report

Accident & incident history

Accident · 2002-01-20 Operator named in NTSB report
Agusta A109A II Serious injury Part 91CJ Systems Aviation Group

Operated by CJ Systems Aviation Group (per NTSB report)

Source: NTSB case SEA02FA030

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, 1996-03-30 – 2001-08-17.

ENGINE FLAMEOUT; WARNING INDICATION · 2001-08-17 Unresolved
ATA 7230

Part: SPLINE ADAPTER — FAILED (COMPRESSOR ASSY)

ENGINE SHUTDOWN DURING FLIGHT DUE TO FLAMEOUT. CAUSE: FAILURE OF SPLINED ADAPTER IN COMPRESSOR ASSEMBLY.

Source: SDR 2001FA0000330
OTHER · 2000-04-04 Unresolved
ATA 6220

Part: SCISSORS — CRACKED (MAIN ROTOR)

DURING INSPECTION OVERHAUL, THE END OF THE LEVER ASSY (ROTATING SCISSORS ASSY) WAS FOUND TO HAVE A CRACK AT THE BUSHING BOSS END APPROXIMATELY 1 INCH LONG. MATERIAL IS 2 INCHES THICK. (X)

Source: SDR 20000502SH020
FLUID LOSS; WARNING INDICATION · 1999-02-12 Unresolved
ATA 2910

Part: LINE — RUPTURED (HYDRAULIC SYSTEM)

DURING FLIGHT, PILOT EXPERIENCED LOSS OF NR 2 HYDRAULIC PRESSURE, NR 2 HYDRAULIC SERVO CAUTION LIGHT, THEN LOSS OF PRESSURE TO THE UTILITY HYDRAULIC SYSTEM. AIRCRAFT WAS LANDED AT BOEING FIELD WITHOUT INCIDENT AT 23:15 HOURS. CAUSE OF FAILURE WAS DETERMINED TO BE A RUPTURED HOSE ASSEMBLY SUPPLYING PRESSURE TO THE NR 2 FLIGHT CONTROL SYSTEM. HOSE WAS REPLACED WITH A SERVICEABLE PART.

Source: SDR 99ZZZX1472
OTHER · 1996-05-31 Unresolved
ATA 3230

Part: BRACE — CRACKED (MLG)

MAIN LANDING GEAR BRACE HAS CRACK LOCATED AT OUTBOARD BEARING BORE. SUBMITTER STATED DIFFICULT TO SEE UNLESS UNIT IS REMOVED.

Source: SDR 96ZZZX3159
OTHER · 1996-03-30 Unresolved
ATA 5520

Part: ELEVATOR — CRACKED (RT SYNC ELEV)

RIGHT SYNC ELEVATOR CRACKS SHOWED ALONG EDGE OF INBOARD RIB. RIB PN 109-8200-02-59 AND PN 109-0200-04-7. FURTHER DISASSEMBLY REVEALED CRACKS IN FORWARD SPAR AND SPAR DOUBLER PN 109-0200-02-49 AND AFT SPAR AND DOUBLER PN 109-0200-02-33. CRACKING APPEARS TO DEVELOP FROM LOOSENING OF THE ATTACH ANGLES LOCATED ON THE SPARS AND ATTACHED TO THE INBOARD RIB.

Source: SDR 96ZZZX1982