N746CC
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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, 2011-07-29 – 2026-07-16.
Part: SKIN — GOUGED (ZONE 100) · airframe 48,858 hrs · 37,246 cycles
DURING REMOVAL OF TCAS ANTENNA DOUBLER, FUSELAGE SKIN WAS GOUGED UNDER DOUBLER BETWEEN FR18 AND FR19. (MAJOR REPAIR). REPAIRED IAW ERS-EJ-53MR-5470.
Part: SKIN — CRACKED (ZONE 500) · airframe 48,858 hrs · 37,246 cycles
SKIN ON BOTTOM OF LT WING AT RIB 7, ABOUT 1 FOOT FWD OF TRAILING EDGE HAS CRACKS FROM EDGE OF 2 EA. FASTENER HOLES. REPAIRED IAW ERS-EJ-57MR-1797.
Part: RIB — CRACKED (ZONE 300) · airframe 48,858 hrs · 37,246 cycles
RIGHT HOR STAB RIB 11A IS CRACKED BETWEEN FWD AND MID SPARS. (MAJOR REPAIR) REPLACED RIB 11A IAW SRM 51-41-01, 51-42-02 AND EO EJ-5500-006.
Part: SKIN — DAMAGED (NOT REPORTED) · airframe 48,858 hrs · 37,246 cycles
FUSELAGE SKIN REPAIR (MAJOR REPAIR). COMPLIED WITH ERS-EJ-53MR-5470 FUSELAGE SKIN REPAIR
Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 48,311 hrs · 36,729 cycles
DOOR PAX FWD OPEN EICAS WARNING ON TAKEOFF ROLL. REJECTED AT APPROX 40 KTS. DOOR INDICATIONS WERE ALL GREEN BEFORE PUSHBACK AND TAXI. AFTER REJECTED TAKEOFF, ASKED FA1 WHAT DOOR INDICATIONS WERE. SHE STATED ALL NORMAL INDICATIONS EXCEPT DOOR ARMED WENT RED. RETURNED TO GATE. PERFORMED GVI OF L1 DOOR IAW AMM 05-25-00-211-802A / 05-25-00-211-801A. NO DEFECTS NOTED. LUBED ALL ARTICULATING JOINTS IN VENT FLAP MECHANISM. MEL RESTORED.
Part: PACKBOARD — DAMAGED (ZONE 800 SLIDE) · airframe 47,988 hrs · 36,422 cycles
FOUND L1 DOOR EMERGENCY SLIDE PACKBOARD UPPER TAB BROKEN OFF. IAW AMM 25-65-01/400 FIGURE 402 ITEM G. PAGE 13/37 R & R L1 DOOR EMERGENCY SLIDE IAW AMM 25-65-01. NO DEFECTS NOTED.
Part: TIRE — FAILED (ZONE 700) · airframe 47,414 hrs · 35,885 cycles
TIRE TREAD SEPARATION ON LANDING RESULTING IN FLAP DAMAGE. UPON LANDING GROUND SPOILERS FAIL, FLT CTRL NO DISPATCH, LG NO DISPATCH, HYD 2 LO QTY (2%) POSTED. DURING POST FLIGHT FOUND SIGNIFICANT DAMAGE DUE TO TIRE RETREAD DEPARTING TIRE. RAR #3 WHEEL ASSY IAW EA32-49-05-801.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,454 hrs · 34,182 cycles
SHEAR CLIP AT FR 88 BETWEEN STR 27R AND 28R IS CORRODED (LEVEL 2 CORROSION). REMOVED AND REPLACE SHEAR AT FRAME 88 BETWEEN STRINGER 27-28R IAW SRM 51-40-08.
Part: PITOT SYSTEM — FAILED · airframe 44,879 hrs · 33,720 cycles
IAS FLAGGED IN BOTH PFDS RIGHT BEFORE ROTATION DURING TAKE OFF. RETURNED TO CMI ADS PROBE 1 FAIL AFTER LANDING UNDER MAX LANDING WEIGHT. "TRANSFERRED TO NRWC 746-CMI-00862" AIR SPEED INDICATOR. NO EMERGENCY DECLARED. T/S IAW FIM 34-15-00-810-864-A. RAR ADS PROBE 1 IAW ERJ 170 AMM 34-13-01 OPS CHK GOOD NO FURTHER DEFECTS NOTED
Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,469 hrs · 22,201 cycles
TWO AFT CEILING EMERGENCY LIGHTS ON UPPER DECK INOP.