N821PH
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.
47 reports on file, 1995-01-15 – 1999-07-28.
Part: FRAME — CORRODED (NACELLE)
PDX - NACELLE FRAME UNDER MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION. REPAIRED IAW HORIZON AIR EA 9-54-203.
Part: ANGLE — CRACKED (LT WING /FUS)
PDX - LEFT FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 4, TABLE 4.
Part: SEAT TRACK — GOUGED (BS 268)
PDX - LEFT INBOARD SEAT TRACK HAS TWO GAUGES AT X268. REPAIRED IAW DHC-8 SRM 51-26-26.
Part: SEAT TRACK — CORRODED (BS 364)
PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X364. REPAIRED IAW RD 8-53-1342.
Part: SEAT TRACK — CORRODED (BS 374)
PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X374. REPAIRED IAW RD 8-53-1342.
Part: SEAT TRACK — CORRODED (BS 312)
PDX - RIGHT OUTBOARD SEAT TRACK AT X312 HAS CORROSION PITS. REPAIRED IAW RD 8-53-1342.
Part: SEAT TRACK — CORRODED (BS 342)
PDX - LEFT OUTBOARD SEAT TRACK AT STATION 342 THERE IS CORROSION PITS. REPAIRED IAW RD 8-53-1342.
Part: SEAT TRACK — CORRODED (BS 327)
PDX - RIGHT OUTBOARD SEAT TRACK AT X327 HAS DEEP CORROSION PITS. REPAIRED IAW DHC8 SRM 51-26-26.
Part: HOUSING — CHAFED (LT TE FLAP)
PDX - LEFT NR 5 FLAP CARRIAGE HOUSING ASSEMBLY IS CHAFED ON INBOARD SIDE WHERE FAIL/SAFE STRAP MOUNTS. REPAIRED IAW HORIZON AIR EA 9-57-437.
Part: FLAP TRACK — OUT OF POSITION (LT TE FLAP)
PDX - LEFT NR 5 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURER SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436.
Part: FLAP TRACK — OUT OF ADJUST (LT TE FLAP)
PDX - LEFT NR 4 FLAP TRACK ASSEMBLY TO CHECK GAPS. REPAIRED IAW HORIZON AIR EA 9-57-436.
Part: FLAP TRACK — OUT OF ADJUST (RT TE FLAP)
PDX - RIGHT NR 4 FLAP TRACK AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436.
Part: MOUNT — OUT OF ADJUST (RT TE FLAP)
PDX - RIGHT NR 4 FLAP AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436.
Part: FLAP TRACK — OUT OF POSITION (LT TE FLAP)
PDX- LEFT NR 4 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURERS SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436.
Part: ANGLE — CRACKED (RT WING/FUS)
PDX - RIGHT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11.
Part: SKIN — DAMAGED (LT TE FLAP)
PDX - LEFT OUTBOARD FLAP ASSEMBLY INBOARD SIDE HAS COMPOSITE DAMAGE. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 201, FIGURE 2.
Part: ANGLE — CRACKED (LT WING/FUS)
PDX - LEFT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11.
Part: HINGE — CORRODED (RUDDER)
PDX - FORE RUDDER BOTTOM SAFETY HINGE LUG IS CHAFFED AND HAS FRETTING CORROSION ACROSS ENTIRE LUG TOP SURFACE. REPAIRED IAW RD 8-55-537.
Part: SKIN — CRACKED (LT NACELLE)
PDX - LEFT NACELLE LOWER INBOARD FORWARD CORNER CUTOUT IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-724.
Part: SPAR — SCRATCHED (RT WING)
PDX - THERE IS A 3.5 INCH SCRATCH IN REAR SPAR AT YW RIGHT. REPAIRED IAW DHC8 SRM 51-20-11.
Part: SEAT TRACK — GOUGED (BS 346)
PDX - RIGHT OUTBOARD SEAT TRACK AT X346 HAS A GOUGE. REPAIRED IAW DHC8 SRM 51-20-16.
Part: PLATE — CORRODED (WING)
PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624BT. REPAIRED IAW RD 8-57-633.
Part: PANEL — CHAFED (WING)
PDX - FUEL PANEL 524CT IS CHAFED AT INBOARD EDGE. REPAIRED IAW RD 8-57-320.
Part: PLATE — CORRODED (WING)
PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624AT. REPAIRED IAW RD 8-57-611 AND DHC8 SRM 51-20-16.
Part: SEAT TRACK — CORRODED (BS 406)
PDX - RIGHT OUTBOARD SEAT TRACK HAS PITS IN THE HAT CHANNEL AT X406. REPAIRED IAW DHC8 SRM 51-20-16.
Part: SKIN — CHAFED (RT TE FLAP)
PDX - RIGHT OUTBOARD FLAP HAS A SMALL CHAFED AREA ON OUTBOARD END OF TOP SURFACE. REPAIRED IAW 57-20-11.
Earlier reports · 1995–1998 · 21 reports
1998
Part: WIRE — BROKEN (NR 2 SMOKE DET)
SEA - FOUND BROKEN WIRE ON NR 2 SMOKE DETECTOR CANNON PLUG. MAINTENANCE SOLDERED WIRE TO CANNON PLUG. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: BATTERY — DISCHARGED (COCKPIT)
COCKPIT EMERGENCY FLASHLIGHT IS NOT BLINKING. REPLACED BATTERY IN FLASHLIGHT, OPERATIONAL CHECKS GOOD.
Part: WHEEL — CRACKED (RT MLG)
NR 4 MAIN WHEEL BROKEN. THE OUTER RIM FAILED AT THE BEAD SEAT. THE CRACK RUNS APPROXIMATELY HALF OF THE WAY AROUND THE BEAD SEAT AREA. REPLACED THE NR 4 WHEEL ASSEMBLY.
Part: ACTUATOR — MALFUNCTION (LT MLG)
LEFT MAIN GEAR DOOR HANGS OPEN ABOUT 2 INCHES DURING FLIGHT. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX REPLACED UPLOCK ACTUATOR, OPERATIONAL CHECK GOOD.
Part: ENGINE — FAILED (NR 1)
BOI- NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. AWAITING TEARDOWN RESULTS OF ENGINE.
Part: ENGINE — MALFUNCTION (NR 1)
NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. TEARDOWN RESULTS OF ENGINE SHOW A FAILURE OF AN LP BLADE DUE TO A FRACTURE JUST ABOVE THE ROOT, WHICH CAUSED THE BALDE TO TRAVEL THROUGH THE GAS PATH. AN OUT OF BALANCE CONDITION RESULTED CAUSING ADDITIONAL ENGINE COMPONENT FAILURES.
Part: LIGHT — BROKEN (CABIN)
THRESHOLD EXIT SIGN BROKEN AT THE RIGHT UNDERWING EXIT DOOR. INSTALLED NEW SIGN AT THE RIGHT UNDERWING EXIT, OPERATIONAL CHECKS GOOD.
Part: BRACKET — CHAFED (NACELLE)
NACELLE AFT WALL GRAVEL GUARD MOUNT BRACKETS CHAFED. REPAIRED IAW HORIZON EA 9-54-154.
Part: BRACKET — CHAFED (LT MLG)
FIVE BRACKETS THAT RETAIN LEFT HAND MAIN LANDING GEAR GRAVEL GUARD ARE SEVERLY CHAFED. INSTALLED BRACKETS IAW DHC-8 SRM 51-40-00. INSTALLED CAM LOC RECEPTICALS IAW DHC-8 SRM 51-40-00.
1997
Part: CONTROL VALVE — MALFUNCTION (NR 1 MAIN BRAKE)
PDX - NR 1 MAIN BRAKE IS INEFFECTIVE. REPLACED NR 1 DUAL SKID CONTROL VALVE, OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — NO TEST (NR 2)
PDX - NUMBER 2 SMOKE DETECTOR WILL NOT TEST. PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
PDX- FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH INOP. RELAMPED, OPERATION CHECK GOOD.
Part: LAMP — FAILED (CARGO COMPT)
SEA- BAGGAGE SMOKE DETECTOR WILL NOT TEST IN POSITION NR 1. RELAMPED INTERNAL SMOKE DETECTOR LIGHT, OPERATIONAL CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA- TWO FORWARD RED EGRESS LIGHTS ARE INOP. REPLACED BATTERY PACK AT 1ED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (COCKPIT)
COCKPIT EMERGENCY FLASHLIGHT HAS A LOW BATTERY. REPLACED BATTERY PACK FOR FLASHLIGHT, OPERATIONAL CHECKS NORMAL.
Part: BRACKET — FRETTING (NACELLE)
FRETTING CORROSION IN NACELLE WHERE MAIN LANDING GEAR ACTUATOR BRACKET ATTACHES TO NACELLE. REPAIRED IAW HORIZON EA 9-54-155.
1996
Part: LIGHT — INOPERATIVE (COCKPIT)
COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
1995
Part: DETECTOR — MALFUNCTIONED (CARGO COMPT)
PDX - NR 1 CARGO SMOKE WARNING LIGHT INTERMITTENTLY ILLUMINATES. VERIFIED THAT THERE WAS NO SMOKE IN CARGO COMPARTMENT. NR 1 SMOKE DETECTOR WAS REPLACED AND TESTED NORMAL. AIRCRAFT RETURNED TO SERVICE.
Part: LAMP — FAILED (AFT CARGO COMPT)
MFR - DURING PREFLIGHT TEST, FOUND NR 1 SMOKE DETECTOR INOP. PLACED ON MEL AND CONTINUED TO PDX. AT PDX FOUND REFERENCE LAMP BURNED OUT, REPLACED BOTH LAMPS, TESTED. AIRCRAFT RETURNED TO SERVICE.
Part: EEL SIGN — BROKEN (CABIN)
SEA - EXIT SIGN AT 4A BROKEN. REPLACED SIGN AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PSEU — DEFECTIVE (LANDING GEAR)
PDX - THE LANDING GEAR INOP CAUTION LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED PSEU IAW, DEHAVILLAND -8 M.M. 32-61-50, PG. 201. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.