N14114
Registered owner: HELFRICH VINCENT, MA (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.
12 reports on file, 1996-12-09 – 2000-01-27.
Part: ANGLE — CORRODED (BS 683 - 700)
INSPECTION FOUND LAV SUPPORT ANGLE CORRODED AT STA 683-700, LBL 26. THE SUPPORT ANGLE AND MOUNT WERE REPLACED IAW BOEING DRAWING 143N5130 AND SRM 53-10-00.
Part: FLOORBEAM — CORRODED (BS 680)
INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 680 FROM LBL 24 TO RBL 15. THE CORROSION WAS REMOVRD IAW SRM 51-30-51 AND ECRA 5321-01078.
Part: INTERCOSTAL — CORRODED (BS 660-680)
INSPECTION FOUND INTERCOSTAL CORRODED AT STA 660-680, LBL 25. THE INTERCOSTAL WAS REPLACED IAW BOEING DRAWING 143N5130.
Part: BEAM — CORRODED (BS 720 - 780)
INSPECTION FOUND SEAT TRACK SUPPORT BEAM CORRODED AT STA 720-780, LBL 25. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-00-51.
Part: SUPPORT — CORRODED (BS 310 - 324)
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 310-324, RBL 41. THE FLOOR SUPPORT WAS REPLACED IAW BOEING DRAWING 141N5160.
Part: FLOORBEAM — CORRODED (BS 720)
INSPECTION FOUND TOP CAP OF FLOORBEAM CORRODED ATSTA 720, LBL 60 TO RBL 60. THE TOP CAP OF FLOORBEAM WAS REPLACED IAW TRAMCO ENGINEERING DRAWING 95-030.
Part: FLOOR PANEL — CRACKED (BS 297)
INSPECTION FOUND A .5 INCH CRACK IN FLIGHT DECK FLOOR PANEL AT ENTRYWAY AREA, STA 297, LBL17. THE FLOOR PANEL WAS REPAIRED IAW BOEING DRAWING 141N5810 AND ECRA 5321-01080.
Part: INTERCOSTAL — CORRODED (BS 680 - 700)
INSPECTION FOUND INTERCOSTALS CORRODED AT STA 680-700, RBL 54 AND RBL 15. THE INTERCOSTALS WERE REPLACED IAW BOEING DRAWINGS 143N5434 AND 143N5130.
Part: BEAM — CORRODED (BS 683)
INSPECTION FOUND SUPPORT BEAM CORRODED AT STA 683RBL 54-60 AND RBL 15-45. THE SUPPORT BEAMS WERE REPLACED IAW BOEING DRAWINGS 143N5845 AND 143N5530.
Part: SKIN — CHAFED (TE FLAP)
INSPECTION FOUND LT O/B FLAP PANEL CHAFED IN THREE PLACES ON THE UPPER PANEL AFT OF NR 3 AND NR 4 SPOILERS. THE FLAP PANEL WAS REPAIRED IAW SRM 51-70-10 AND ECRA 5731-01023.
Part: SKIN — CHAFED (TE FLAP)
INSPECTION FOUND RT O/B FLAP UPPER PANEL CHAFED BY NR 10 SPOILER BOLT. THE FLAP PANEL WAS REPAIRED IAW SRM 51-70-10 AND ECRA 5731-01023.
Part: BUS PWR CONTL — INOPERATIVE (E/E COMPT)
THE CREW RECEIVED EICAS MESSAGES, NOSE GEAR AIR GRND, RT PROBE HEAT, ANTI-SKID, RECIRC FANS AND HYD PUMPS AND EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT DC BUS SEC 1 C/B TRIPPED. THE CIRCUIT BREAKER WAS RESET AND ALL SYSTEMS CHECKED NORMAL. THE BUS POWER CONTROL UNIT WAS REPLACED. BITE CHECK SHOWED RT GCU SERIAL LINK FAULT. THE RIGHT GCU WAS REPLACED, AN ENGINE RUN WAS ACCOMPLISHED AND ALL SYSTEMS CHECKED NORMAL.