N102AV
Registered owner: VAN NICE ANDREW, IA (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
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.
44 reports on file, 1995-01-16 – 1998-12-29.
Part: LIGHT — INOP (COCKPIT)
HANDHELD EMERGENCY LIGHT IN THE COCKPIT OVERHEAD IS INOP. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECKS GOOD.
Part: HINGE — DAMAGED (RUDDER)
FORE RUDDER TRAILING TOP HINGE FITTING HAS MECHANICAL DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-36.
Part: HINGE — DAMAGED (RUDDER)
FORE RUDDER TRAILING HINGE, BOTTOM FITTING HAS MECHANICAL DAMAGE. REPAIRED IAW DHC -8 SRM 51-20-16 AND 51-20-36.
Part: SKIN — DENTED (BS 21 & 498)
DENT BEYOND LIMITS AT X498.737 AND .5 BELOW STATION 21. REPAIRED IAW RD 8-53-3961.
Part: SKIN — DENTED (NR 2 NACELLE)
DENTS FOUND IN OUTER SKIN OF INBOARD NR 2 ENGINE PANEL 425AL. REPAIRED IAW DHC-8 RD 8-71-139.
Part: SUPPORT — CORRODED (BS 424-488.5)
FRETTING CORROSION FOUND ON LEFT SUPPORT FOR PANELS 143AZ AND 143BZ BETWEEN FUSELAGE STATION X424.124 AND X488.500. REPAIRED IAW DHC-8 RD 8-53-3960.
Part: DOOR — DAMAGED (CARGO COMPT)
MECHANICAL DAMAGE ON CARGO DOOR UNDER MOUNTING AREA FOR UPPER MOST OF REAR VERTICAL EDGE. REPAIRED IAW RD 8-52-368.
Part: DOOR — CRACKED (NR 2 ENG COWL)
NR 1 ENGINE COWL DOOR 416AR HAD CRACK. REPAIRED IAW DHC-8 RD 71-142.
Part: FITTING — WORN (VERT STAB)
LOWER LUG OF MIDDLE LOWER RUDDER FITTING ON VERTICAL STABILIZER IS WORN WHERE THE BEARING SITS. REPAIRED IAW RD 55-350.
Part: ACTUATOR — CHAFED (LT MLG)
LEFT MAIN LANDING GEAR STANDBY ACTUATOR FOUND TO BE CHAFING ON ATTACH POINT FITTING. REPAIRED IAW DHC-8 MM 32-30-16, PAGE 202, PARAGRAPH B.
Part: ACTUATOR — CHAFED (NR 2 MLG)
NR 2 MAIN GEAR STANDBY ACTUATOR CHAFING AT ATTACH POINT. REPAIRED IAW RD 8-54-1001 AND DHC -8 MM 32-30-16, PAGE 202, PARAGRAPH B.
Part: SUPPORT — GOUGED (NR 1 ENGINE)
NR 1 ENGINE OUTBOARD SUPPORT STRUT HAS GOUGES FROM FIRE DETECTION WIRES IN TWO PLACES. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-36.
Part: FITTING — CHAFED (RUDDER)
MINOR CHAFE DAMAGE ON UPPER AND LOWER FORE RUDDER ACTUATOR FITTINGS. REPAIRED IAW RD 8-55-128.
Part: FITTING — CHAFED (RUDDER)
MINOR CHAFE DAMAGE ON FORE RUDDER HYDRAULIC DAMPER FITTING. REPAIRED IAW RD 8-55-128.
Part: BUSHING — WORN (MLG DOOR)
GEAR DOOR ON NR 1 SIDE WAS HANGING DOWN IN-FLIGHT, 10 TO 12 BOLT FOUND TO BE LOOSE ON GEAR DOOR. SECURED ROD END BOLT TO DOOR BRACKET PIVOT POINT WITH .032 STAINLESS SAFETY WIRE. FERRIED AIRCRAFT TO PDX. AT PDX, INSPECTED DOOR AREA FOR DAMAGE, NO DAMAGE FOUND. INSTALLED FORWARD GEAR DOOR ROD TO DOOR. REPLACED THREADED BUSHING.
Earlier reports · 1995–1997 · 29 reports
1997
Part: BULB — FAILED (CABIN)
PDX- FORWARD EMERGENCY EXIT LIGHT AT THE FORWARD EMERGENCY DOOR IS INOP. REPLACED LAMP, OPERATIONAL CHECKS GOOD.
Part: CONECTOR — DIRTY (CABIN)
PDX- LEFT HAND OVERHEAD EMERGENCY LIGHTS ARE INOP. CLEANED TERMINALS ON THE PS1 POWER SUPPLY, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA- FORWARD TWO FLOOR PROXIMITY LIGHTS INOP. REPLACED POWER SUPPLY AT 1DE, OPERATIONAL CHECK GOOD.
Part: HMU — MALFUNCTIONED (NR 2 ENGINE)
SEA - NR 2 ENGINE FLAMED OUT AT 300 FEET ALG ON APPROACH. REPLACED HMU FUEL PUMP AND LP FUEL FILTER, NO DEFECTS NOTED. LEAK CHECKED, OPERATIONAL CHECK GOOD.
Part: PLATE — CORRODED (WING)
PDX- LADDER PLATE UNDER PANEL 522AT HAS AREAS OF CORROSION AND PITTING. REPAIRED CORROSION AND PITTING PER EA 957-283.
Part: STRAP — CHAFED (BS 240/264)
PDX- FRAME STRAPS AT STATION X240.5 AND X264.1 AT Z155.550 APPROX ARE CHAFFED. REPAIRED FRAME STRAPS PER EA 9-53-316.
Part: FITTING — CHAFED (LEFT)
PDX- LEFT HAND NR 3 BATHTUB FITTING CHAFED BY THE FLAP SECONDARY DRIVE HOUSING. REPAIRED PER EA 9-53-312.
Part: FITTING — CHAFED (RIGHT)
PDX- RIGHT HAND NR 3 BATHTUB FITTING CHAFED BY FLAP SECONDARY DRIVE HOUSING. REPAIRED PER EA 9-53-311.
Part: SKIN — DENTED (WS 736)
PDX- RIGHT HAND AFT FUSELAGE AT STATION X 736.096 Z 150.000 THERE IS A PAINTED DENT .5 INCH FROM THE EDGE OF THE STRINGER. DENT IS 2.5 INCHES LONG, 0.8 INCHES WIDE, AND .019 INCHES DEEP. REPAIRED PER EA 9-53-310.
Part: SKIN — DENTED (RT TE FLAP)
PDX- RIGHT OUTBOARD FLAP TOP SKIN IS DENTED IN TORSION BOX AT STATION YW 189, .040 INCHES DEEP AND 3 INCHES LONG. FABRICATED AND INSTALLED PATCH PER EA 9-57-282.
Part: INTERCOSTAL — CRACKED (WING)
PDX- INTERCOSTAL AT OUTBOARD OIL COOLER HINGE IS CRACKED. REPAIRED PER EA 9-54-135.
Part: RIB — CRACKED (LT WING)
PDX- LEFT HAND OIL COOLER DOOR INBOARD ATTACH RIB IS CRACKED AT THE MOUNTING BOLT. REPAIRED PER EA 9-54-133.
Part: BOLT — MISSING (RT MLG DOOR)
AFTER TAKEOFF ON LANDING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR FORWARD DOOR REMAINED IN THE OPEN POSITION. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. INSPECTED AND FOUND SAFE FOR FERRY FLIGHT FROM SEA TO PDX. IN PDX, FOUND MISSING BOLT AND BUSHING ON GEAR DOOR ACTUATOR ROD. REPLACED BOLT AND BUSHING. PERFORMED RIGGING AND OPERATIONAL CHECK OF SYSTEM, CHECKS GOOD.
1996
Part: LIGHT — INOPERATIVE (COCKPIT)
COCKPIT EMERGENCY LIGHT WAS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
SEA - LAV SMOKE DETECTOR CAME ON IN FLIGHT, NO SMOKE WAS OBSERVED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. LAV SMOKE DETECTOR REPLACED AND DETECTOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: AIR DISTR — ODOR (CABIN)
BOI - OIL SMELL IN CABIN ON DESCENT. AIRCRAFT LANDED IN BOI WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. NR 1 ENGINE REPLACED IAW MAINT MANUAL. ENGINE AND BLEED AIR OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. AWAITING ENGINE TEARDOWN FOR CAUSE.
Part: BLEED VALVE — DEFECTIVE (NR 1 ENGINE)
BOI - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. NR 1 ENGINE P2.5-3 VALVE REPLACED AND BLEED AIR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
1995
Part: SEAT TRACK — CORRODED (CABIN)
PDX - SEAT TRACKS P/N 85320701-125 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (CABIN)
PDX - SEAT TRACK P/N 85330507-107 FOUND CORRODED BEYOND MANFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (CABIN)
PDX - DURING C-CHECK, FOUND SEAT TRACK P/N 85320701-123 IS CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (CABIN)
PDX - SEAT TRACK P/N 85331040-109 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (CABIN)
PDX - SEAT TRACK P/N 85330469-001 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (CABIN)
PDX - SEAT TRACK P/N 85330217-001 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR)
SEA - GEAR INTRANSIT LIGHTS CAME ON, BUT GEAR DID NOT EXTEND AFTER SELECTING GEAR DOWN. GEAR HANDLE CYCLED UP AND RED LIGHTS WENT OUT. ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. LANDING GEAR SELECTOR VALVE REPLACED I/A/W MAINT. MANUAL. VALVE OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - EMERGENCY LIGHTS ARE INOP. ALL BATTERY PACKS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN FLASHLIGHT)
DURING PREFLIGHT, FOUND FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT INOP. BATTERY REPLACED AND LIGHT FUNCTION TESTED GOOD. AIRCRAFT RELEASED FOR SERVICE.
Part: BATTERY — DISCHARGED (COCKPIT LIGHT)
DURING MAINTENANCE COCKPIT EMERGENCY FLASHLIGHT WAS FOUND TO HAVE DEPLETED BATTERIES. BATTERIES REPLACED AND AIRCRAFT RELEASED FOR SERVICE.
Part: EEL LENS — MISSING (CABIN)
PDX - THE EMERGENCY LIGHT AT THE MAIN CABIN DOOR IS MISSING A LENS. INSTALLED A REPLACEMENT LENS COVER. AIRCRAFT RETURNED TO SERVICE.
Part: RETRACT MECH — OBSTRUCTED (RT MLG DOOR)
PDX - THE RT YELLOW MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED THE GEAR HANDLE DOWN LEFT MAIN AND NOSE GEAR WENT DOWN AND LOCKED. RT MAIN RED UNSAFE LIGHT REMAINED ILLUMINATED WITH NO GREEN DOWN AND LOCKED AND INDICATED UNSAFE BY ALTERNATE MEANS. REMOVED OBSTRUCTION FROM RT FORWARD GEAR DOOR HINGE ARM PATH. GEAR OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.