N824RW
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.
4 reports on file, 2021-11-29 – 2021-12-01.
Part: RIB — CRACKED (ZONE 300) · airframe 38,244 hrs · 25,580 cycles
DURING HEAVY CHECK MAINTENANCE FOUND RH HORIZONTAL STABILIZER LEADING EDGE RIB 4 IS CRACKED. RH HORIZONTAL STAB LEADING EDGE RIB 4 REMOVED AND REPLACED IAW EMB SRM 51-41-02.
Part: RIB — CRACKED (ZONE 100) · airframe 38,244 hrs · 25,580 cycles
DURING HEAVY CHECK MAINTENANCE FOUND LH HORIZONTAL STAB LEADING EDGE RIB 4 IS CRACKED. LH HORIZONTAL STAB LEADING EDGE RIB 4 REMOVED AND REPLACED WITH NEW IAW EMB SRM 51-41-02.
Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,244 hrs · 25,580 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE, CORROSION FOUND ON GUSSET PLATE AT FR 90 AT BL 0. CORRODED GUSSET PLATE AT FR90, BL 0 REPLACED WITH NEW IAW EMB SRM 51-43-03.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,244 hrs · 25,580 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CFIII FLOOR STRUCTURE, CORROSION FOUND ON PREVIOUS REPAIR AT LH UPPER BEAM BETWEEN FR87-89. CORRODED PREVIOUS REPAIR AT LH UPPER BEAM BETWEEN FR87-89, REPLACED IAW EMB 170 SRM 53-23-10 AND 51-43-04.