N121CZ
Registered owner: N121CZ LLC, WI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FREIGHT RUNNERS EXPRESS, INC. (KCQA) | Certificate holder | — | Matched by certificate designator |
| FREIGHT RUNNERS EXPRESS, INC. (KCQA) | Operator | 2017-09-12 – 2017-09-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
THE FOLLOWING CORRODED PARTS WERE REMOVED AND REPLACED: (1) FRAME 16, RH T-CHANNEL CORRODED. REMOVED AND REPLACED T-CHANNEL PER SRM 51-40-02 PN 120-08896-001 SN NSN. (2) RH CENTER âTâ PROFILE AT FRAME 40 CORRODED. REMOVED AND REPLACED AFT RH âTâ PROFILE PER SRM 51-40-02 PN 120-04449-001 SN NSN. (3) LH BEAM PLATE CORRODED FROM STATION 13056.0 â 15050.0. REMOVED AND REPLACED LH BEAM PLATE (BUTT STRAP) PN 120-06158-001 SN NSN IAW SRM 51-40-02. (4) RH BEAM PLATE CORRODED FROM STATION 11430.0 â 13056.0. REMOVED AND REPLACED RH BEAM PLATE (BUTT STRAP) PN 120-46163-001 IAW CPM 53-20-01 AND SRM 51-40-02. (5) RH BEAM PLATE CORRODED FROM APPROXIMATELY STATION 13056.0 â 15050.0. REMOVED AND REPLACED RH BEAM PLATE PN 120-06158-001 SN NSN IAW CPM 53-20-01 AND SRM 51-40-02. (6) LH FLOOR SILL CORRODED FROM STATION 4992.0 â 6653.1. REMOVED AND REPLACED SILL PN 120-05802-001 SN FLL0116097 PER SRM 51-40-02. (7) LH FLOOR SILL CORRODED FROM APPROXIMATELY STATION 15050.0 â 16144.9. REMOVED AND REPLACED LH FLOOR SILL IAW SRM 51-40-00 PN 120-06157-005 SN NSN (QTY 2). (8) RH FLOOR SILL CORRODED FROM STATION 13056.0 â 15050.0. REMOVED AND REPLACED RH FLOOR SILL PN 120-06159-01 SN NSN IAW SRM 51-40-02. (9) RH FLOOR SILL CORRODED FROM APPROXIMATELY STATION 11430.0 â 13056.0. REMOVED AND REPLACED RH FLOOR SILL PN 120-04171-002 SN NSN IAW SRM 51-40-02 (QTY 2). (10) LH AND RH FLOOR BUTT STRAP CORRODED, BETWEEN FRAMES 13A â 20. REMOVED AND REPLACED LH AND RH FLOOR BUTT STRAPS WITH FABRICATED BUTT STRAPS PN 120-46156-601 SN NSN USING THE ORIGINAL PART DIMENSIONS IAW EMB DRAWING 120-46156 AND EMB SRM 51-30-01, INSTALLED IAW SRM 51-40-02 PN (QTY 4).
DURING FLIGHT RH ENGINE EEC FAILURE ANNUNCIATED WITH POWER REDUCTION TO ZERO PERCENT TORQUE. CREW PERFORMED QRH PROCEDURE, UNABLE TO RESTORE POWER ABOVE FLT IDLE. AIRCRAFT DIVERTED TO SUITABLE AIRPORT WITH PROPELLER IN FEATHER. AFTER LANDING ENGINE POWER AND EEC SYSTEM CHECKED, COULD NOT DUPLICATE, EEC AND ENGINE OPERATION WAS NORMAL.