N422FL
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ROBERT S. GOLABEK | Operator | on 1996-09-07 | Operator named in NTSB report |
Accident & incident history
Operated by ROBERT S. GOLABEK (per NTSB report)
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.
14 reports on file, 2009-12-07 – 2015-05-28.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,601 hrs · 7,195 cycles
DURING LANDING, CREW COULD NOT GET A LANDING NOSE GEAR DOWN GREEN LIGHT. TEST WOULD NOT LIGHT BULB EITHER. DECLARED EMER & CONDUCTED FLY-BY OF TOWER, FOR VISUAL CONFIRMATION OF GEAR DOWN. UPON LANDING THE NOSE GEAR LIGHT ILLUMINATED. LANDING & TAXI WITHOUT INCIDENT. CHECKED ALL SWITCHES FOR RIGGING, WIRING FOR DAMAGE & PERFORMED SEVERAL GEAR SWINGS. ALL CHECKS & RIGGING SATISFACTORY, NO WIRE DAMAGE NOTED. WORK PERFORMED IAW AMM 32-30-00.
Part: DOOR SEAL — FAILED (MAIN DOOR) · airframe 8,599 hrs · 7,193 cycles
THE MAIN DOOR SEAL FAILED IN FLIGHT & THE PAX OXYGEN MASKS DROPPED. PAXS DONNED OXYGEN MASKS WHILE CREW PROCEEDED TO DIVERT FLIGHT & DESCEND BELOW FL 120. AN EMER LANDING WAS DECLARED & THE ACFT LANDED WITHOUT FURTHER INCIDENT. R & R THE DOOR SEAL. LEAKS & OPERATION CHECKS WERE GOOD & THE ACFT RETURNED TO SERVICE.
Earlier reports · 2009–2013 · 12 reports
2013
Part: UNKNOWN — ODOR (AFT) · airframe 7,528 hrs · 6,374 cycles
BURNING ELECTRICAL ODOR IN THE AFT AREA OF THE BAGGAGE COMPARTMENT. MX INSPECTED THE AREA WITH ENGINES AND AIR CONDITONER RUNNING BUT COULD NOT DUPLICATE THE DISCREPANCY, NO REPEATS TO DATE.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,407 hrs · 6,281 cycles
REMOVED LT HORIZONTAL STAB RIB L2M, INSTALLED HORIZONTAL STAB RIB L2M.
Part: RIB — CRACKED (ZONE 300) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED IAW MFG 128-6200-001.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RIGHT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB WAS FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
Part: RIB — CRACKED (ZONE 300) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LEFT HORIZONTAL STAB CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
Part: RIB — CRACKED (ZONE 300) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM FASTENER HOLE. RIB REPLACED IAW MFG KIT 128-6200-001.
Part: RIB — CRACKED (ZONE 300) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,407 hrs · 6,281 cycles
DURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 62.20, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED IAW 128-6200-001.
2010
Part: SEAL — LOOSE (PAX DOOR)
DURING CLIMB, CREW NOTED A LOUD SQUEAL FOLLOWED BY A POP AND A STEADY LOSS OF CABIN PRESSURE (ABOUT 2000 FPM). EMERGENCY PROCEDURES WERE EXECUTED AND EMERGENCY WAS DECLARED. ACFT LANDED SAFELY. MX INSPECTED THE ACFT AND FOUND THE MAIN ENTRY DOOR SEAL HAD COME LOOSE. THE DOOR SEAL WAS REATTACHED.
2009
Part: COALESCER BAG — FROZEN · airframe 5,018 hrs · 4,408 cycles
ON CLIMB OUT, AFTER TAKEOFF, CREW REPORTED VIBRATION FELT THROUGHOUT THE ACFT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MX PERFORMED ENG RUNS AND ENG OPS CHECKS, CHECKED ALL FLIGHT CONTROL RIGGING, AND PERFORMED LANDING GEAR OPS AND VISUAL CHECKS BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY ON THE GROUND. HOWEVER, MX VERIFICATION FLIGHT CONFIRMED THE EXISTANCE OF THE VIBRATION. MX FOUND THE COALESCER SOCK FROZEN. UPON REPLACEMENT OF THE SOCK AND SUBSEQUENT MX VERIFICATION FLIGHT, THE NOISE WENT AWAY.