N824PH
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.
113 reports on file, 1995-12-18 – 2001-08-22.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,730 hrs · 42,987 cycles
PDX - ONE LAMP INOPERABLE ON FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING, AT ROW ONE. RESPLICED ENVIRONMENTAL SPLICES AND REATTACHED LIGHT SOCKET. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 29,319 hrs · 41,021 cycles
SEA- FORWARD 2 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT PS-2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — MISREPAIRED (TE FLAP) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD FLAP FAILED CLEARANCE CHECK AT REPAIR DOUBLER ON TOP SKIN AT STATION YW 391.5 TO 405. REPAIRED IAW HORIZON AIR EA 9-57-551.
Part: SKIN — MISREPAIRED (TE FLAP) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD FLAP FAILED CLEARANCE CHECK AT REPAIR DOUBLER ON TOP OF SKIN. REPAIRED IAW DHC-8 MRD8-57-1908.
Part: SKIN — TORN (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND NACELLE SKIN TORN LEFT HAND SIDE AT STATION XN137.35, ADJACENT TO MAIN LANDING GEAR FORWARD DOOR CUTOUT. REPAIRED IAW DHC-8 RD8-54-729.
Part: SKIN — DENTED (RT ENG NACELLE) · airframe 29,271 hrs · 40,956 cycles
PDX- ENGINE NACELLE RIGHT HAND SIDE, BOTTOM INBOARD SIDE IS A DENT IN SKIN, INBOARD OF OIL COOLER. REPAIRED IAW DHC-854-30-21 AND HORIZON AIR EA 9-54-266.
Part: ANGLE — CUT (NR 2 ENG FIREWAL) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND ENGINE FIREWALL AFT SIDE OUTBOARD ANGLE IS CUT INTO BY TGT HARNESS. REPAIRED IAW DHC-8 RD8-54-991.
Part: SEAL — TORN (LT WING) · airframe 29,271 hrs · 40,956 cycles
PDX- SEAL IS TORN AND LEFT WING LOWER SURFACE TRAILING EDGE IS DAMAGED AT STATION YW139-00. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 9-57-549.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND INBOARD SEAT TRACK HAS PAINT MISSING THROUGH OUT THE TRACK. REPAIRED IAW HORIZON AIR EA 9-53-592 AND DHC-8 SRM 51-20-16, PAGES 1-4.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND INBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X424.124. REPAIRED IAW HORIZON AIR EA 9-53-592, AND DHC-8 RD8-53-1339, AND SRM 51-20-13, PAGES 1-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND INBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP AREA AT STATION X456.500. REPAIRED IAW HORIZON AIR EA 9-53-592 AND DHC-8 RD8-53-1339, AND SRM 51-20-16, PAGE 1-4.
Part: ANGLE — CHAFED (LT ENG FIREWALL) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND ENGINE FIREWALL APERTURE ANGLE IS CHAFED ON FRONT FLANGE RADIUS AND EDGE OF ANGLE NEAR TGT HARNESS AREA. REPAIRED IAW DHC-8 RD8-54-991.
Part: FIREWALL — CRACKED (NR 2 ENGINE BAY) · airframe 29,271 hrs · 40,956 cycles
PDX- NR 2 FIREWALL CRACKED AT INBOARD SIDE AT CORNER OF CUTOUT ON CLOSING MEMBER. REPAIRED IAW DHC-8 RD8-54-109, PAGE 3.
Part: SPAR — CORRODED (LT WING) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT WING FRONT SPAR LOWER SURFACE HAS FRETTING CORROSION AT STATION YW210-220. REPAIRED IAW HORIZON AIR EA 9-57-548.
Part: SPAR — CORRODED (LT WING) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT WING FRONT SPAR, UPPER SURFACE HAS FRETTING CORROSION AROUND ATTACH HOLES FOR PANEL 511AL. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-2011, AND HORIZON AIR EA 9-57-546.
Part: ARM — GOUGED (NLG) · airframe 29,271 hrs · 40,956 cycles
PDX- NOSE LANDING GEAR TRAILING ARM HAS A GOUGE WITH RAISED METAL. REPAIRED IAW DHC-8RD 8-32-289.
Part: SKIN — DENTED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND SIDE OF FUSELAGE THERE IS A DENT JUST FORWARD OF AFT CARGO DOOR, BELOW FLOOR LEVEL. REPAIRED IAW HORIZON AIR EA 9-53-590.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS MISSING MATERIAL AND GOUGED UPAT STATION X434.500. REPAIRED IAW DHC-8 RD8-53-1339.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X434.500. REPAIRED IAW DHC-8 RD8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK AT STATION X257 HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 9-53-589 AND DHC-8 RD8-53-1339.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X405.737. REPAIRED IAW DHC-8 RD8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X376.110. REPAIRED IAW DHC-8 RD8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND INBOARD SEAT TRACK HAS LIGHT PITTING ON TOP AT STATION X282.400. REPAIRED IAW DHC-8 RD8-53-1339.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS SOME SMALL PITTING AT STATION X307.400. REPAIRED IAW DHC-8 SRM 51-40-00, PAGES 1-4 AND RD8-51-102 AND RD8-53-1339.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP SIDE AT STATION X280.400. REPAIRED IAW HORIZON AIR EA 9-53-587 AND DHC-8 RD8-53-1342 AND SRM 51-20-13.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X264.100. REPAIRED IAW DHC-8 RD8-53-1342 AND SRM 51-20-16, AND HORIZON AIR EA 9-53-587.
Part: CLIP — CRACKED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- CLIP CRACKED BELOW LEFT HAND EMERGENCY EXIT. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X280.400. REPAIRED IAW HORIZON AIR EA 9-53-587 AND DHC-8 RD8-53-1342, AND SRM 51-20-16.
Part: CLIP — CRACKED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- CLIP CRACKED AT FRAME 333 OUTBOARD OF LEFT HAND OUTBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS RAISED MATERIAL AT STATION X361.050. REPAIRED IAW HORIZON AIR EA 9-53-587 AND DHC-8 RD8-53-1342 AND SRM 51-20-13.
Part: FLANGE — TOOL DAMAGE (VERTICAL STAB) · airframe 29,271 hrs · 40,956 cycles
PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON LEFT HAND FLANGE. REPAIRED IAW DHC-8 51-10-00 AND SRM 51-20-16.
Part: FLANGE — TOOL DAMAGE (VERTICAL STAB) · airframe 29,271 hrs · 40,956 cycles
PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING GOUGES. REPAIRED IAW DHC-8 SRM 51-10-00 AND SRM 51-20-16.
Part: FLANGE — TOOL DAMAGE (VERTICAL STAB) · airframe 29,271 hrs · 40,956 cycles
PDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON RIGHT HAND FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-10-00.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTED AREA AT STATION X519.000. REPAIRED IAW HORIZON AIR EA 9-53-588 AND DHC-8 RD8-53-1339.
Part: SPAR — CORRODED (LT WING) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT WING FRONT SPAR, LOWER SURFACE HAS FRETTING CORROSION AT STATION YW 48-82. REPAIRED IAW DHC-8 RD8-57-811 AND RD8-57-1150.
Part: FAIRING — CORRODED (LT WING ROOT) · airframe 29,271 hrs · 40,956 cycles
PDX- TWO AREAS OF CORROSION AT FORWARD END OF LEFT WING ROOT FAIRING BETWEEN STA X312 AND X333 AND IN LINE WITH Z168. REPAIRED IAW DHC-8 SRM 51-10-00 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X300.400. REPAIRED IAW DHC-8 RD8-53-1339 AND HORIZON AIR EA 9-53-588.
Part: PLATE — CORRODED (WING) · airframe 29,271 hrs · 40,956 cycles
PDX- LADDER PLATE HAS PITTING, PANEL 524BT, AFT INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD8-57-633, PAGE 3.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- CORROSION UNDER BOLTHEAD ON STRAP ON INBOARD SIDE OF SEAT TRACK AT STATION X597.5 AND STRINGER 31L. REPAIRED IAW DHC-8 20-14-01 AND SRM 51-20-16, AND SRM 51-20-26.
Part: PLATE — SCRATCHED (LADDER) · airframe 29,271 hrs · 40,956 cycles
PDX- LADDER PLATE SCRATCHED, PANEL 524BT CENTER AFT LADDER PLATE. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD8-57-633.
Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,271 hrs · 40,956 cycles
PDX- LEFT WING OUTBOARD FLAP CHAFED ON UPPER SURFACE. REPAIRED IAW DHC-8 SRM 51-20-50 AND SRM 51-20-11, PAGE 6.
Part: FLOOR PANEL — CORRODED (CABIN) · airframe 29,271 hrs · 40,956 cycles
PDX- MAIN CABIN DOORWAY FLOOR PANEL APERTURE FOR PANEL 131DZ HAS CORROSION ON 5 NUT PLATES AND SUROUNDING AREAS OF EACH NUT PLATE. REPAIRED IAW DHC-8 SRM 51-20-16.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- LIGHT CORROSION ON FRAME X510.000 BETWEEN STRINGER 31 AND 30. LOCATED ON FRAME FLANGE AROUND FUSELAGE RIVETS. REPAIRED IAW DHC-8 SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X264.100. REPAIRED IAW DHC-8 RD8-53-1339.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING AT STATION X310.350. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342.
Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS A SCRATCH AT STATION X501.000. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,271 hrs · 40,956 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS PITTING AT STATION X490.500. REPAIRED IAW DHC-8 SRM 51-20-41 AND RD8-53-1342.
Earlier reports · 1995–2000 · 66 reports
2000
Part: SKIN — SCRATCHED (LT WING) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND INBOARD WING SKIN AT LOWER FORWARD SPAR X384.5 BETWEEN STATIONS YW42 AND YW 139 HAS SCRATCHES TO SKIN. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, AND SRM 51-00-06, AND RD8-57-1785.
Part: STRUCTURE — DAMAGED (LT AILERON) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND AILERON COMPOSITE TIP DAMAGED. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: WEB — GOUGED (CABIN DOOR SILL) · airframe 28,524 hrs · 39,949 cycles
YXX- UPPER DOOR SILL WEB GOUGED AT X564.5 AND X580.5. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 51-00-06, AND SRM 51-20-00, PAGE 5.
Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- LIGHTNING STRIKE DAMAGE IN VARIOUS SPOTS ON EXTERIOR FUSELAGE. REPARIED IAW DHC-8 MM 5-50-31.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- DENT IN RIGHT HAND FUSELAGE EXTERIOR SKIN AT STATION X202.75 AND STRINGER 26R, FORWARD OF LAVATORY SERVICE DOOR. REPAIRED IAW DHC-8 SRM 51-00-05 AND 20-34-11 PAGE 14-15.
Part: SKIN — CHAFED (TE FLAP) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND OUTBOARD FLAP ASSEMBLY UPPER SKIN IS CHAFED. REPAIRED IAW DHC-8 SRM 51-00-06, AND RD8-57-1786.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FUSELAGE SKIN AT STATION 242 AND STRINGER 95 TO 10 HAS A GAP UNDER RIVET INTO COUNTER SINKS. REPAIRED IAW DHC-8 SRM 51-20-26, 51-00-05, 51-00-06 AND DHC-8 RD 8-53-5299.
Part: STRUCTURE — DAMAGED (LT AILERON) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND AILERON TIP, UNDERLYING STRUCTURE FOR COMPOSITE TIP HAS DAMAGE TO MOUNTING FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-22-00, PAGE 5.
Part: ANGLE — CHAFED (PYLON) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND HORSE COLLAR HAS CHAFE DAMAGE AT LOWER FORWARD ANGLE AT STATION XN60.00 AND YW 164.00. REPAIRED IAW DHC-8 SRM 51-20-11, AND EA 9-54-257, AND RD8-54-1346.
Part: SKIN — SCRATCHED (LT WING) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND WING LOWER SKIN AT YW139 AND X384.5 TO X426.9 HAS SCRATCHED SKIN EXTERIOR SURFACE. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, AND SRM 51-13-01, PAGE 1-15.
Part: ANGLE — DAMAGED (FUEL DOOR) · airframe 28,524 hrs · 39,949 cycles
YXX- REPLACED RIGHT HAND FUEL CLOSING ANGLE. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1-5, AND SRM 51-40-11.
Part: SKIN — CHAFED (TE FLAP) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND OUTBOARD FLAP ASSEMBLY CHAFED AT REAR SPAR, TOP SKIN. REPAIRED IAW DHC-8 SRM 51-20-11, AND RD8-57-1777, AND HORIZON AIR EA 9-57-517.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FUSELAGE EXTERIOR SKIN IS DENTED AT STATION X332 AND STRINGER 14P. REPAIRED IAW DHC-8 SRM 53-00-16, DHC-8 RD 8-53-5298, HORIZON AIR EO 2882, EA 9-53-576 AND HORIZON AIR GMM 5-5-0.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- EXTERIOR FUSELAGE SKIN IS DENTED AT STATION X290 AND STRINGER 19P AND 20P. REPAIRED IAW DHC-8 53-00-16, 51-00-06, 51-00-05, HORIZON AIR EO 2880 AND EA 9-53-577.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FUSELAGE EXTERIOR SKIN IS DENTED IN TWO PLACES AT STATION X330 AND STRINGER 13P. REPAIRED IAW DHC-8 SRM 53-00-16 PAGE 1-6, 53-10-11 PAGE 1-10, 51-00-06, 51-00-05, DHC-8 RD 8-53-5297 AND HORIZON AIR EO 2883 AND EA 9-53-5751.
Part: ANGLE — DAMAGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- REPLACED LEFT HAND FORWARD CLOSING ANGLE. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1-4, SRM 51-40-00, PAGE 1-5.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND FUSELAGE HAS A GOUGE AND DENT 5.5 INCHES FORWARD OF FRAME X636.000 BETWEEN STRINGER 15 AND 16. REPAIRED IAW DHC-8 SRM 51-13-01 PAGE 1-15, 51-20-26 PAGE 6, 51-00-05, 51-20-11 PAGE 5 AND DHC-8 RD 8-53-5302.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- GOUGE 8 INCHES FORWARD OF FUSELAGE STATION X564.500 BETWEEN STRINGER 3L AND 4L. REPAIRED IAW DHC-8 SRM 53-00-16 PAGE 3, 51-20-00 PAGE 5,51-00-06, 51-00-05, 20-34-11 PAGE 17, DHC-8 RD 8-53-5300, HORIZON AIR EO 2884 AND EA 9-53-574.
Part: ANGLE — DAMAGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- REPLACED LEFT HAND AFT CLOSING ANGLE. REPAIRED IAW DHC-8 SRM 51-20-00, PAGE 5.
Part: PRESSURE PANEL — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- SCRATCH AT STATION Z135.0 AND Y50.0 ON INSIDE FACE OF REAR PRESSURE DOME. REPAIRED IAW DHC-8 SRM 51-20-26, PAGE 6, SRM 51-13-01, PAGE 1-15, SRM 51-20-11, PAGE 1-10, SRM 51-20-16, PAGE 1-5 AND RD8-53-5301 AND EA 9-53-573.
Part: PRESSURE PANEL — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- SCRATCH AT STATION Z104.0 AND Y40.95 ON INSIDE OF REAR PRESSURE DOME. REPAIRED IAW DHC-8 SRM 51-20-26, PAGE 6, SRM 51-13-01, PAGE 1-15, SRM 51-20-11, PAGE 1-10, SRM 51-20-16, PAGE 1-5 EA 9-53-573.
Part: ANGLE — CORRODED (CARGO DOORWAY) · airframe 28,524 hrs · 39,949 cycles
YXX- BAGGAGE DOOR CUTOUT X597 297 X30 LEFT HAND ANGLE FROM FRAME TO DOOR SILL IS CORRODED. REPAIRED IAW DHC-8 SRM 51-20-00, PAGE 5, AND SRM 53-00-16, PAGE 4.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FRAME X387 AT STRINGER 75 HAS ENLARGED RIVET HOLE. REPAIRED IAW DHC-8 SRM 51-10-36, AND SRM 51-20-16, PAGE 1-5, AND SRM 53-20-21.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- STRINGER 29 CORRODED AT METAL STANDOFF OF STATION X175. REPAIRED IAW DHC-8 SRM 51-20-11.
Part: ANGLE — DAMAGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- REPLACED RIGHT HAND CLOSING ANGLE. REPAIRED IAW DHC-8 SRM 51-20-00, PAGE 5, AND SRM 51-40-00, PAGE 1-5.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 28,524 hrs · 39,949 cycles
YXX- FLOOR PANEL SUPPORT ANGLE ON LEFT HAND SIDE OF LOWER BAGGAGE PIT AT STATION X597.5 HAS SURFACE CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, SRM 51-20-00, PAGE 5.
Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FORWARD PRESSURE BULKHEAD, FORWARD FACE AT STATION Y9.0 AND Z95.0 HAVE CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16 AND 51-20-00 PAGE 5.
Part: STRAP — LIGHTNING STRIKE (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- LONGITUDINAL JOINT STRAP HAS A LIGHTNING STRIKE ON RIVET AT STATION X151 AND STRINGER 22P. REPAIRED IAW DHC-8 SRM 51-40-00 PAGE 1-6 AND 51-40-11 PAGE 1-4.
Part: THRESHOLD — TOOL DAMAGE (CARGO BAY) · airframe 28,524 hrs · 39,949 cycles
YXX- BAGGAGE DOOR CUTOUT UPPER SILL HAS TOOLING DAMAGE AROUND RIVET HEAD AT X567 Z160. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1-4, AND SRM 53-00-16.
Part: SKIN — GOUGED (CARGO DOOR) · airframe 28,524 hrs · 39,949 cycles
YXX- UPPER EDGE OF BAGGAGE DOOR OUTER SKIN GOUGED AT X564.5. REPAIRED IAW RD8-52-025.
Part: FRAME — CHAFED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FORWARD SPAR FRAME AT X387.35 CHAFED AT GROUND STRAP ATTACH POINT STRINGER 7L. REPAIRED IAW DHC-8 SRM 53-00-16, SRM 51-20-11, AND SRM 51-20-00, PAGE 5.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 28,524 hrs · 39,949 cycles
YXX- CRACKS FOUND ON LEFT HAND NOSE LANDING GEAR BOX STATION X97.0, Y12.5 AND Z110.0. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5, 51-30-21, AND DHC-8 RD 8-53-1676.
Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 28,524 hrs · 39,949 cycles
YXX- RIGHT HAND EMERGENCY EXIT LOWER SILL STRUCTURE AT STAION X370 HAS CORROSION ON INTERNAL FRAME. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, AND SRM 51-20-00, PAGE 5.
Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND EMERGENCY EXIT LOWER SILL STRUCTURE AT STATION X366.0 HAS CORROSION ON INTERNAL FRAMES. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, AND SRM 51-20-00, PAGE 5.
Part: FRAME — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- GOUGE ON FORWARD FRAME OF STATION X222 OF CUTOUT FOR AIRSTAIR DOOR ABOVE FORWARD LOWER DOOR STOP. REPAIRED IAW DHC-8 SRM 53-00-16 AND 51-20-00 PAGE 5.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- GOUGE 5 INCHES AFT OF BAG DOOR CUTOUT AT STRINGER 18L. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 53-00-16 PAGE 2, 51-20-00 PAGE 5 AND 20-34-11 PAGE 12.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- SCRATCH ON RIGHT HAND FUSELAGE SKIN AT X188 STRINGER 14R. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, SRM 51-20-16, PAGE 1-6, SRM 51-20-46, PAGE 1-4, AND SRM 53-00-16.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FUSELAGE SKIN IS SCRATCHED AT STATION X259 AND STRINGER 19P AND 20P. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 51-20-16 PAGE 1-6, 51-20-46 PAGE 1-4, 53-00-16, AND 20-34-11 PAGE 17.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- RIGHT HAND FUSELAGE HAS A GOUGE 12 INCHES FORWARD OF REAR PRESSURE BULKHEAD BETWEEN STRINGER 13 AND 14. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 53-00-16 PAGE 2 AND 51-20-00 PAGE 5.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- EXTERIOR FUSELAGE SKIN IS SCRATCHED AT STATION X345 AND STRINGER 16P. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 51-20-16 PAGE 1-6, 51-20-46 PAGE 1-4, 53-00-16, AND 20-34-11 PAGE 17.
Part: FRAME — SCRATCHED (COCKPIT WINDOW) · airframe 28,524 hrs · 39,949 cycles
YXX- SCRATCH ON PILOTS WINDSCREEN FRAME LOWER MOUNTING SURFACE AT X118 AND 47.0. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 53-00-16, 51-20-16 AND 51-20-36 PAGE 1-8.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- FUSELAGE EXTERIOR SKIN IS SCRATCHED AT STATION X356 AND STRINGERS 17P AND 18P. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 51-20-16 PAGE 1-6, 51-20-46 PAGE 1-4, 53-00-16 PAGE 2 AND 20-34-11 PAGE 17.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- LEFT HAND FUSELAGE HAS A GOUGE 9 INCHES FORWARD OF REAR PRESSURE BULKHEAD AT STRINGER 19. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 53-00-16 PAGE 2, 51-20-00 PAGE 5 AND 20-34-11 PAGE 17.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- STATION X210 HAS SCRATCHES IN SKIN. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-00 AND 20-34-11 PAGE 12.
Part: SKIN — GOUGED (FUSELAGE) · airframe 28,524 hrs · 39,949 cycles
YXX- GOUGE 9 INCHES OF FORWARD FUSELAGE STATION X618.000 AND STRINGER 26R. REPAIRED IAW DHC-8 51-20-11 PAGE 1-10, 53-00-16 PAGE 2 AND 51-20-00 PAGE 5.
1999
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
SEA- MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED DOOR STOP/RAMPS, OPERATIONAL CHECKS OK. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
SEA- MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED DOOR ROLLERS, TRACKS AND STOPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR MECHANISM. FLIGHT ATTENDANT OPERATED DOOR, NO EXCESSIVE EFFORT REQUIRED TO OPEN DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: LIGHT — INOPERATIVE (COCKPIT)
PDX- COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. MAINTENANCE REPLACED THE OVERHEAD LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD.
Part: LIGHT — INOPERATIVE (COCKPIT)
SEA- COCKPIT OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE COCKPIT OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD.
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
SEA- THE MAIN CABIN DOOR LEVER IS VERY HARD TO OPEN FROM THE INSIDE. MAINTENANCE CLEANED AND LUBRICATED THE DOOR STOPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: HANDLE — DIRTY (PAX DOOR)
PDX- MAIN CABIN DOOR HANDLE IN CABIN IS HARD TO OPERATE. MAINTENANCE CLEANED THE SEAL CONTACT AREA FOR THE TOP OF THE MAIN CABIN DOOR. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.
1998
Part: BATTERY — DISCHARGED (CABIN)
EMERGENCY FLASHLIGHT BELOW FLIGHT ATTENDANT SEAT NOT FLASHING. REPLACED BATTERY PACK FOR THE EMERGENCY FLASHLIGHT, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
TWO FLOOR EMERGENCY LIGHTS INOP. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTION (NR 2 ENGINE)
SEA - WHILE TAXIING TO PARKING, THE NR 2 ENGINE FEATHERED, THEN CAME OUT OF FEATHER WITHOUT ANY INPUT FROM THE CREW. THE POWER LEVER WAS SLIGHTLY AFT OF THE FLIGHT IDLE GATE. THE CONDITION LEVER WAS AT MIN. REPLACED NR 2 PROPELLER CONTROL UNIT (PCU). RIGGED PCU AND PERFORMED ENGINE RUN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHTS — INOPERATIVE (CABIN)
TWO FORWARD EMERGENCY ESCAPE FLOOR PATH LIGHTS ARE INOP. RESTORED WIRING TO ORIGINAL CONDITION IAW DHC MAINTENANCE MANUAL. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
FORWARD 2 EMERGENGY FLOOR LIGHTS INOP. THE POWER SUPPLY AT 3352 PS 2 WAS REMOVED AND REPLACED, OPERATIONAL CHECK IS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
FIRST 2 FLOOR PROXIMITY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - FORWARD TWO FLOOR PROXIMITY EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED RIGHT FORWARD POWER SUPPLY (3352-P2), OPERATIONAL TEST IS GOOD.
1997
Part: SWITCHES — DIRTY (COCKPIT)
BLI - ROLL SPOILER INBOARD/OUTBOARD CAUTION LIGHTS AND ADVISORY LIGHTS ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. CLEANED AND LUBRICATED SWITCHES ON QUADRANT. OPERATIONAL CHECK IS GOOD, NO COMPONENTS WERE REPLACED.
Part: SWITCHES — DIRTY (GROUND SPOILERS)
BZN - ABORTED TAKEOFF ROLL, INBOARD/GROUND OUTBOARD SPOILER CAUTION LIGHTS ON. CLEANED PEDESTAL SWITCHES WITH CLEANER. NO PARTS REPLACED. GROUND RAN AT TAKEOFF POWER WITH NO FURTHER DEFECTS NOTED.
Part: LAMP — FAILED (CARGO COMP)
NR 1 BAGGAGE SMOKE DETECTOR WARNING TEST FAILS. RELAMPED BEACON AND TEST LAMPS, OPERATIONAL CHECKS GOOD.
Part: CAUTION LIGHT — ILLUMINATED (LT/RT SPOILERS)
SEA - ON TAKEOFF MASTER CAUTION ROLL SPOILER INBOARD AND OUTBOARD HYDRAULIC LIGHTS CONTINUOUSLY ILLUMINATED. ABORTED TAKEOFF. CLEANED AND INSPECTED BOTH LEFT AND RIGHT LIFT DUMPERS SOLENOID VALVE C-PLUGS AND WIRING. RERACKED ADVISORY LIGHT CONTROL BOX. NO PARTS REPLACED. GROUND RAN HIGH SPEED TAXI. COULD NOT DUPLICATE.
Part: PROP CNTRL UNIT — MALFUNCTION (NR 2 ENGINE)
LWS - NR 2 PROP WOULD NOT COME OUT OF FEATHER DURING START. REPLACED NR 2 PROP CONTROL UNIT. OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
AFT LEFT OUTSIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.
1995
Part: PROX SENSOR — INOPERATIVE (DRAG STRUT)
IDA - THE NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH DURING RETRACTION OR FURTHER EXTENSION. ALTERNATE INDICATOR SHOWED DOWN AND LOCKED. AIRCRAFT WAS INSPECTED AND FERRIED TO PDX FOR REPAIR. REMOVED AND REPLACED THE DRAG STRUT PROX SENDOR IAW 32-20-16. ADJUSTED SENSOR IAW 32-20-11. GEAR SWINGS COMPLIED WITH, OPERATIONAL CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.