N217MC

CIRRUS DESIGN CORP SR20 · 2026 · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: CNJ AVIATION LLC, FL (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

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.

10 reports on file, 1996-06-06 – 2013-03-07.

WARNING INDICATION · 2013-03-07 Matched by certificate designator
ATA 7200

Part: ENGINE — MAKING METAL (NR 2) · airframe 13,138 hrs

CHIP LIGHT NR 2 ENGINE. REMOVED CHIP DETECTOR, DETERMINED TO BE A MINOR EVENT IAW MM. PERFORMED GROUND RUN FOR PRECAUTIONARY MEASURES, NO DEFECTS NOTED.

Source: SDR QMLA2013030713033
OTHER · 2009-04-08 Unresolved
ATA 5302

Part: FRAME — CRACKED (AFT TAILBOOM)

FOUND CRACK ON LT SIDE OF TAILBOOM AT FUSELAGE STA 9976 MM. DURING FURTHER INVESTIGATION, OTHER CRACKS WERE FOUND ON THE RT SIDE AT THE SAME FUSELAGE STATION AND INSIDE THE TAILBOOM ON THE 10L FRAME. REPAIR SCHEMES FOR THESE CRACKS WERE PROVIDED BY AEC FOR PATCHING THE SIDES AND THE DECISION WAS MADE TO COMPLETLY REPLACE THE 10L FRAME, INSIDE OF THE TAILBOOM. (K)

Source: SDR 2009FA0000459
OTHER · 2009-02-24 Unresolved
ATA 5302

Part: DOUBLER — CRACKED (TAILBOOM) · airframe 11,762 hrs · 32,292 cycles

DURING A DAILY INSP A CRACK WAS DISCOVERED IN A DOUBLER LOCATED ON THE LT SIDE OF THE TAILBOOM.

Source: SDR RMXA032520097195
OTHER · 2007-12-04 Unresolved
ATA 5302

Part: FRAME — CRACKED (TAILBOOM) · airframe 11,112 hrs

DURING A SCHEDULED INSPECTION , A CRACK WAS DISCOVERED ON THE RT SIDE OF TAILBOOM FRAME 10L. THE CRACK EXTENDS FROM THE CENTER OPENING OF FRAME 10L TO THE OMEGA CUTOUT AT THE RT OUTER EDGE OF FRAME 10L.

Source: SDR 12052007
OTHER · 2001-06-29 Unresolved
ATA 3422

Part: GYRO — DEFECTIVE (TAIL ROTOR)

SEVERE TAIL ROTOR OSCILLATION. REMOVED AND REPLACED

Source: SDR TI1R001496
INADEQUATE Q C · 2000-09-22 Unresolved
ATA 3421

Part: GYRO — MISREPAIRED (COCKPIT)

GYRO HORIZON WAS RETURNED FROM REPAIR STATION WITH 8130-3 TAG INDICATING ''REPAIRED''. AFTER INSTALLATION AND FUNCTIONAL TEST, THE UNIT WAS DETERMINED TO HAVE SAME SYMPTOMS AS ORIGINAL. THE UNIT SHOWED NO EVIDENCE THAT IT WAS EVER REPAIRED. NO ''DO NOT BREAK SEAL'' STICKER, ETC. (X)

Source: SDR 20001019SH006
OTHER · 1998-02-26 Unresolved
ATA 2312

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

TRANSCEIVER PL TONE MODULATION IS INDICATING 1.8 HKZ TO 2.1 KHZ. CHECKED SPECS - SHOULD BE AROUND .75 TO .8 KHZ. REMOVED AND REPLACED.

Source: SDR 98ZZZX1505
FLUID LOSS · 1996-11-20 Unresolved
ATA 7321

Part: FUEL CONTROL — LEAK (ENGINE)

FUEL CONTROL LEAK UNDER PX PY CAP.

Source: SDR 97ZZZX1354
OTHER · 1996-06-06 Unresolved
ATA 6410

Part: BLADE — PAINT PEEL (TAIL ROTOR)

TAIL ROTOR BLADE PAINT PEELING OFF LESS THAN 90 DAYS INSTALLED. 107.8 ACFT HRS.

Source: SDR 96ZZZX4647
OTHER · 1996-06-06 Unresolved
ATA 6410

Part: BLADE — PAINT PEEL (TAIL ROTOR)

TAIL ROTOR BLADE PAINT PEELING OFF LESS THAN 90 DAYS INSTALLED. 107.8 ACFT HRS.

Source: SDR 96ZZZX4648