N483AA
Registered owner: AERIAL ACRES LLC, IN (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.
11 reports on file, 2002-11-06 – 2017-01-19.
Part: COVER — OUT OF POSITION (R1 DOOR SLIDE) · airframe 79,577 hrs · 42,325 cycles
R1 DOOR EMERGENCY EVACUATION SLIDE COVER IS NOT IN THE PROPER POSITION. INSTALLED LOCK. OPERATIONAL CHECKED GOOD.
Part: O-RING — LEAKING (APU) · airframe 78,812 hrs · 41,844 cycles
MAINTENANCE REPORTED FUMES IN CABIN. INVESTICATION FOUND OIL IN THE APU INLET. OIL DETERMINED TO BE FROM OIL DRAIN PLUG LEAK. REMOVED AND REPLACED DRAIN PLUG O-RING IAW AMM 49-90-12. SYSTEM CHECKS NORMAL. AIRCRAFT WAS GROUNDED.
Part: FUEL SYS — LEAKING (APU) · airframe 78,524 hrs · 41,666 cycles
RAW FUEL ODOR IN CABIN DURING APU OPERATION. AIRCRAFT GROUNDED. ACCOMPLISHED MCM 21-96-01 AND VERIFIED FUEL ODOR IN CABIN. LEAK CHECKED AND FOUND FUEL AT APU DOOR DRAIN. REMOVED AND REPLACED APU IAW MCM 49-96-82. SYSTEM CHECK NORMAL. (OPEN)
Part: O-RING — LEAKING (APU FUEL) · airframe 78,510 hrs · 41,660 cycles
RAW FUEL ODOR IN CABIN REPORTED DURING APU USAGE. AIRCRAFT GROUNDED. MAINTENANCE FOUND FUEL LEAKING FROM THE APU FUEL INLET LINE ADAPTER. REMOVED AND REPLACED ADAPTER O-RING IAW AMM 49-30-01. OPS AND LEAK CHECKED NORMAL.
Part: FUEL CONTROL — LEAKING (APU) · airframe 78,502 hrs · 41,656 cycles
DURING TAXI IN A STRONG ODOR OF FUEL WAS REPORTED IN THE CABIN AND COCKPIT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND FUEL LEAKING FROM THE APU FUEL CONTROL DRAIN LINE. REMOVED AND REPLACED THE APU FUEL CONTROL IAW AMM 49-30-01. OPS AND LEAK CHECKED NORMAL.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,932 hrs · 41,321 cycles
AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED, AT STATION 1474 ON RT SIDE, BETWEEN THE 12TH & 13TH RIVETS UP FROM THE LOWER SEAM. ACCOMPLISHED SKIN REPAIR IAW AARD 53-30-00-4. REPAIRED SKIN IAW SRM 53-01-00-001.
Part: SKIN — DAMAGED (RT WING) · airframe 62,199 hrs · 32,324 cycles
DURING AUTO LAND RIGHT WING CONTACTED RUNWAY. AIRCRAFT OUT OF SERVICE FOR INSPECTION AND REPAIR. REPLACED NUMBER 5 SLAT AND CENTER SECTION RETRACT CABLE. REPLACED NUMBER 15 SLAT TRACK AND RIGHT OUTBOARD FLAP WEDGE. REPLACED NUMBER 1 AND 2 MAIN LANDING GEAR TIRES. REPLACED RIGHT WING TIP. INTERIM REPAIRS MADE AND AIRCRAFT FERRIED TO MCI FOR EVALUATION AND REPAIRS.
Part: DOOR FRAME — CORRODED (FUSELAGE)
TUL - FOUND FORWARD CARGO LOWER FRAME HORIZONTAL FLANGE CORRODED AT MAIN DOOR CUTOUT. REMOVED CORROSION. CUT OUT DAMAGED AREA. INSTALLED FILLER AND INTERIM REPAIR DOUBLER PER ESO 80559, DATED 11-07-02. (M)
Part: ATTACH ANGLE — CRACKED (FUSELAGE)
TUL - FOUND VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE CRACKED, AT AFT END. CUT OUT DAMAGED SECTION OF SKATE ANGLE. INSTALLED FILLER AN DOUBLER REPAIR PER AARD 53-10-00-2. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND LEFT AFT FUSELAGE SKIN CRACKED AT FASTENER HOLE, STATION 1380, LONGERON 12L. DAMAGE REMOVED, DOUBLER INSTALLED PER AARD 53-30-00-02. (M)
Part: STRUCTURE — CRACKED (FUSELAGE)
TUL - FOUND .25 INCH CRACK IN OUTBOARD END OF RIGHT WHEEL WELL AFT LANDING. ROUTED OUT DAMAGE AND INSTALLED REPAIR ANGLES PER SRM 53-01-00 FIG 2. AREA DYE-CHECKED, NO INDICATION OF CRACK FOUND. (M)