N355UA
Registered owner: LOPEZ FABIO A, NC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CENTURY AVIATION INC (LDIA) | Certificate holder | — | Matched by certificate designator |
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.
20 reports on file, 1997-03-20 – 2003-01-07.
Part: FRAME — DENTED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
AFT PIT RIGHT FRAME STATION 727C DENTED AT RBL 28. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CORROSION ON RIGHT CREASE BEAM INBOARD CHORD FROM BS 294 TO BS 334. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STRINGER CLIP CRACKED BS 270 STRINGER 15R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CREASE BEAM WEB BELOW FORWARD GALLEY DOOR STA 297 - STA 327 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CRACK IN UPPER FLANGE OF CABIN FLOOR INTERCOSTAL AT BS 346 FLOORBEAM BL0 SEEN FROM LOWER SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.
Earlier reports · 1997–2002 · 15 reports
2002
Part: SKIN — DENTED (HORIZ STAB) · airframe 41,461 hrs · 23,918 cycles
DENT IN LEADING EDGE OF RIGHT HAND HORIZONTAL STABILIZER, 8 INCHES INBOARD OF TIP. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.
Part: CLIP — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
BODY STATION 178 LOWER CHORD RBL20, WL188, Z CLIP TO INTERCOSTAL IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED Z CLIP.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
FORWARD CABIN FRAME AT STATION 400 IS CRACKED STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STATION 807 FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STATION 867 FRAME CRACKED JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STATION 847 FRAME IS CRACKED AT FASTENER JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
AFT CABIN FRAME IS CRACKED STATION 767 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED DOUBLER REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STA 827 FRAME CRACKED AT FASTENER ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR .
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN STATION 807 FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
FUSELAGE FRAME, STATION 188, LEFT OUTBOARD CHORD CRACKED AT STRINGER 17 WL 207. MAJOR REPAIR ACCOMPLISHED. CHORD AND WEB REPAIR INSTALLED.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
FUSELAGE FRAME, STATION 188, RIGHT SIDE IS CRACKED IN OUTBOARD CHORD AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR.
Part: WEB — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
FUSELAGE WEB STA 188-199 AT WL 207 ON LEFT SIDE CRACKED IN CUTOUT RADIUS FOR FRAME FLANGE. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,461 hrs · 23,918 cycles
CABIN FUSELAGE FRAME STATION 747 IS CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,318 hrs · 23,159 cycles
RETURNED TO FIELD DUE TO WING BODY OVERHEAT INDICATION.
1997
Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN)
FLIGHT RETURNED TO DENVER DUE TO CABIN PRESSURE PROBLEMS. LANDING WAS NORMAL. *S/D* AIRCRAFT WOULD NOT PRESSURIZE, RT PACK HI, OUTFLOW VALVE CLOSED, IN AUTO OR STANDBY, BOTH BLEEDS ON. USING APU BLEED, NO HELP. REPLACED FORWARD AND AFT OUTFLOW VALVES, OPS CHECK GOOD.