N822PH
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HORIZON AIR INDUSTRIES, INC. (QXEA) | Operator | on 2001-03-06 | Operator named in NTSB report |
Accident & incident history
Operated by Horizon Air Industries, Inc. (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.
90 reports on file, 1995-05-26 – 2001-03-06.
Part: BEARING — FAILED (NR 2 ENGINE) · airframe 31,854 hrs · 44,448 cycles
PDX - ON APPROACH TO PDX AN INCREASING ITT ON NR 2 ENGINE NOTED ALONG WITH VIBRATION. AFTER GEAR AND FLAP EXTENSION SMOKE SMELL NOTED. DECLARED AN EMERGENCY. AFTER LANDING TOWER ADVISED SMOKE ON NR 2 ENGINE. THE FIRE/SHUTDOWN ON GROUND CHECKLIST WAS CONDUCTED. REMOVED AND REPLACED PROP AND ENGINE. ENGINE TORN DOWN AT PWC. DISTRESS DAMAGE OBSERVED ON NR 5 BEARING. THE LIKELIHOOD OF BEARING DISTRESS WAS FROM WEAR DAMAGE ON THE BEARING FROM LOSS OF OIL PRESSURE.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 31,473 hrs · 43,964 cycles
PDX - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 1995–2000 · 88 reports
2000
Part: ROD — LACK OF LUBE (PAX DOOR) · airframe 31,122 hrs · 43,511 cycles
SEA- MAIN CABIN DOOR SOMETIMES JAMS WHEN OPEN. LEVER AT ABOUT HALFWAY POSITION. LUBED MAIN CABIN DOOR OVERCENTER RODS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: SIGN — INOPERATIVE (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LOWER EMERGENCY EXIT SIGN IN SEAT 4A IS MISSING COVER. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRAP — OUT OF ADJ (PAX DOOR) · airframe 30,560 hrs · 42,802 cycles
YKM- MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND TEFLON STRIP UNDER DOOR HINGE IMPINGING ON DOOR. ADJUSTED TEFLON STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LIGHTNING STRIKES ON AIRCRAFT SKIN. REPAIRED IAW DHC-8 SRM 5-50-31.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CRACKS AT UPPER END OF VERTICAL STIFFENERS, 4 INCHES OUTBOARD OF CENTER LINE OF AIRCRAFT LEFT AND RIGHT ON BULKHEAD AT FUSELAGE STATION X66.00. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND 51-40-11.
Part: FIREWALL — DAMAGED (LT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND NACELLE FORWARD FIREWALL INBOARD LOWER AREA HAS TWO RIVETS WITH HEADS CHAFED OFF AND AREA OF CHAFING JUST ABOVE XM107-80 AND ZM1.5-00. REPAIRED IAW RD 8-54-1333.
Part: SHIELD — CRACKED (CARGO DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- CARGO DOOR SHIELD AT CEILING IS CRACKED IN SEVERAL LOCATIONS. REPAIRED IAW DHC-8 SRM 51-70-00 PAGE 401.
Part: SKIN — GOUGED (PAX DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- MAIN CABIN DOOR OUTER SHELL HAS A GOUGE ON SEALING SURFACE OF DOOR SHELL AT LOWER FORWARD CORNER. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SKIN — GOUGED (LT WING) · airframe 30,568 hrs · 42,755 cycles
YXX- GOUGE ON LOWER WING SKIN AT FORWARD END OF LEFT HAND NR 5 FLAP TRACK, LYW373. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06, 51-20-16 PAGE 1-4 AND 51-20-36 PAGE 1-9.
Part: FIREWALL — CHAFED (NR 2 NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- CHAFE DAMAGE ON NR 2 FORWARD OUTBOARD FIREWALL WEB AT STATION YN107.18 AND ZN-10.50. REPAIRED IAW DHC-8 RD 8-54-1330, 8-54-081, AND SRM 51-00-06.
Part: DOOR FRAME — GOUGED (CARGO BAY) · airframe 30,568 hrs · 42,755 cycles
YXX- CARGO DOOR CUTOUT UPPER WEB IS GOUGED BESIDE DOOR STOPS AT FUSELAGE STATION X564.5X AND X580.5. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 7 AND HORIZON AIR EA 9-53-571.
Part: DRAG STRUT — CHAFED (LT MLG) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND MAIN LANDING GEAR DRAG STRUT FOUND WITH CHAFE MARKS. REPAIRED IAW DHC-8 RD 8-32-474, HORIZON AIR EA 9-32-102 AND CONAIR EO 2869.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE HAS A DENT BETWEEN STRINGER 19 AND 20 FORWARD OF FRAME X405.737. REPAIRED IAW DHC-8 RD 8-53-457 AND DHC-8 SRM 51-00-05, 53-00-16.
Part: STRUCTURE — LOOSE (LT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE PER DHC-8 MM.
Part: MOUNT — CHAFED (MLG ACTUATOR) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. BLENDED AREA.
Part: STRUCTURE — LOOSE (RT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE AS PER DHC-8 100 MM.
Part: SKIN — DENTED (RUDDER) · airframe 30,568 hrs · 42,755 cycles
YXX- DENT IN UPPER RIGHT HAND SIDE OF FORWARD RUDDER 4 INCHES FORWARD OF AFT SPAR AT UPPER HINGE LINE. REPAIRED IAW DHC-8 SRM 55-40-16, 55-40-28, AND 51-00-06.
Part: FIREWALL — CRACKED (LT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND NACELLE FIREWALL EXTENSION TUBE IS CRACKED AT WELD AND BOLT HOLES. REPAIRED IAW DHC-8 RD 8-54-16, AND 8-54-8.
Part: PLATE — CRACKED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND LADDER PLATE HAS A CRACK FROM DEUTCH NUT HOLE. REPAIRED IAW DHC-8 RD 8-57-876.
Part: MOUNT — CHAFED (MLG ACTUATOR) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. REPAIRED IAW DHC-8 RD 8-54-523 AND SRM 51-00-06.
Part: SKIN — LIGHTNING STRIKE (EMERGENCY EXIT) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND EMERGENCY EXIT DOOR HAS LIGHTNING STRIKES. REPAIRED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 51-20-00 PAGE 5.
Part: SKIN — DAMAGED (LT WING TIP) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND WING TIP LEADING EDGE ERRODED. REPAIRED IAW DHC-8 RD 8-57-071.
Part: SKIN — LIGHTNING STRIKE (PAX DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- MAIN CABIN DOOR OUTER SHELL EXTERIOR SKIN HAS LIGHTNING STRIKES. REPARIED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 20-34-11 PAGE 17.
Part: ANTENNA — DAMAGED (VOR) · airframe 30,568 hrs · 42,755 cycles
YXX- DAMAGE ON LEFT HAND VOR ANTENNA AND FORWARD MOUNT ON VERTICAL FIN RIB 9 AND X848. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-55-955.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- DENT AT FUSELAGE STATION X282.400 BETWEEN STRINGER 10 AND 11 JUST FORWARD OF ICE SHIELD. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06 AND 51-00-05.
Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- AIRSTAIR DOOR OUTER SKIN HAS MANY DENTS AND SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-26 PAGE 6, 51-20-11, 52-00-16 AND 51-00-06.
Part: STRUCTURE — CRACKED (NR 2 NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- CRACKED STRUCTURE ON NR 2 NACELLE BETWEEN MID DOOR''S FORWARD HINGE AND FORWARD BRACKET OF EXTENSION HANDLE. REPAIRED IAW DHC-8 RD 8-54-239 AND SRM 51-40-11 PAGES 1-4 AND 32-10-21.
Part: SKIN — GOUGED (LT WING) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND WING CENTER SECTION OF UPPER SKIN AT YW70.00 HAS GOUGE. REPAIRED IAW DHC-8 SRM 51-20-11, 57-10-16 PAGE 2 AND 51-20-00 PAGE 5.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE HAS A DENT JUST AFT OF STATION X636.00 BETWEEN STRINGER 16 AND 15. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06, 51-00-05, RD 8-53-5230 AND HORIZON AIR EO 2857.
Part: SKIN — GOUGED (LT WING) · airframe 30,568 hrs · 42,755 cycles
YXX- THREE GOUGES ON LEFT HAND UPPER WING SKIN BETWEEN YW139.000 AND YW171.000. REPAIRED IAW DHC-8 SRM 51-20-11, AND 57-10-16 PAGE 2.
Part: SKIN — CHAFED (RT WING) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND UPPER WING SKIN AFT OF NR 2 ENGINE HAS CHAFE DAMAGE FROM PANEL 422ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06 AND 51-20-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE JUST FORWARD OF MAIN CABIN DOOR THERE IS A DENT FORWARD OF STATION X545.00 BETWEEN STRINGER 22 AND 23. REPAIRED IAW DHC-8 SRM 51-20-26, 53-00-16 AND 51-00-06.
Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND NACELLE FOUND TO HAVE TWO CRACKS ABOVE ACCESS HOLES FOR MAIN LANDING GEAR RETRACT ACTUATOR ATTACH HARDWARE. REPAIRED IAW DHC-8 RD 8-54-109 PAGE 3 AND 4, SRM 54-00-00 PAGE 1 AND 20-21-18.
Part: SKIN — GOUGED (LT WING) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND UPPER WING SKIN AFT OF NR 1 ENGINE NACELLE HAS A GOUGE FROM PANEL 412ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-20-11 AND 51-20-00 PAGE 5.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE HAS DENTS BETWEEN 30 AND 31 AT STATION X151.600. REPAIRED IAW DHC-8 RD 8-53-5206, DHC-8 SRM 53-00-16 AND 51-00-05.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND FUSELAGE HAS DENT BETWEEN STRINGER 29 AND 30 AT STATION X182.00. REPAIRED IAW HORIZON AIR EA 9-53-561 AND DHC-8 SRM 51-00-05.
Part: FIREWALL — CRACKED (RT NACELLE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND NACELLE FIREWALL FOUND CRACKED ABOVE INBOARD END OF OIL COOLER. REPAIRED IAW DHC-8 SRM 51-40-11, 54-00-00 PAGE 1 AND 20-21-18.
Part: SKIN — CHAFED (PAX DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- MAIN CABIN DOOR OUTER SHELL HAS CHAFE DAMAGE ON INTERIOR LIP, 18 INCHES FROM DOOR CABLE ATTACH POINT. REPAIRED IAW DHC-8 SRM 52-00-16 AND 51-20-16 PAGE 1-5.
Part: THRESHOLD — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- SEVERAL AREAS OF PITTING AND SURFACE CORROSION ON THRESHOLD OF MAIN CABIN DOOR CUTOUT, AT FLOOR LEVEL BETWEEN FUSELAGE STATION 222.000AND X252.700. REPAIRED IAW DHC-8 SRM 51-20-00, 51-40-00 AND 20-21-21.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND OUTBOARD FORWARD SEAT TRACK HAS PITTING CORROSION WHERE SEATS ATTACH TO TRACK. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE HAS DENT AND GOUGE BETWEEN STRINGER 17 AND 19 AT FRAME 151.600. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-00-06.
Part: STRUCTURE — CHAFED (EMERGENCY EXIT) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND EMERGENCY EXIT DOOR, BOTTOM AFT CORNER OF DOOR HAS CHAFE DAMAGE TO DOOR STRUCTURE AND RIVETS. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5, 51-40-11 PAGE 1-4 AND 52-00-16 TABLE 2.
Part: INTERCOSTAL — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND FORWARD OUTBOARD SEAT TRACK INTERCOSTAL TO FRAME X356, Z102 AND Y42 HAVE CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-00 PAGE 5 AND 51-20-11.
Part: FRAME — GOUGED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- AFT FACE OF FRAME X240.50 BETWEEN STRINGER 19 AND 22 HAVE MINOR SCRATCHES AND GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16 AND 51-20-00.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION AROUND MARKER BEACON ANTENNA. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-20-00.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND INBOARD FORWARD SEAT TRACK HAS EVIDENCE OF PITTING CORROSION AT SEAT ATTACH SPOTS. REPAIRED IAW DHC-8 AD 8-53-3074 AND 8-53-1339.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 30,568 hrs · 42,755 cycles
YXX- CRACKS IN INNER RIGHT HAND STRUCTURE OF NOSE LANDING GEAR WHEEL WELL ABOVE RETRACT ACTUATOR ATTACH FITTING. ALSO, ONE SHREDDED RIVET IN AREA. REPAIRED IAW DHC-8 RD 8-53-5209, HORIZON AIR EA 9-53-562 AND DHC-8 SRM 51-00-06.
Part: SKIN — UNBONDED (RT AILERON) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND AILERON TIP TRAILING EDGE IS DISBONDING. REPAIRED IAW DHC-8 SRM 57-60-63.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND FORWARD CABIN SEAT TRACK CORRODED AT ALL SEAT TRACK ATTACHMENT POINTS. REPAIRED IAW DHC-8 AD 8-53-1342 AND DHC-8 SRM 51-40-00.
Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 30,568 hrs · 42,755 cycles
YXX- CARGO DOOR SKIN IS SCRATCHED AT X581 AND STRINGER 14L. REPAIRED IAW DHC-8 SRM 51-20-26 AND 51-20-36.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND INBOARD AFT SEAT TRACK HAS CORROSION WHERE SEATS ATTACH. REPAIRED IAW DHC-8 AD 8-53-1339 AND DHC-8 SRM 51-00-06 AND 51-20-00 PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND OUTBOARD AFT SEAT TRACK HAS PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5.
Part: SKIN — GOUGED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE EXTERIOR SKIN HAS A GOUGE BETWEEN STRINGER 16 AND 17 AT STATION X424.124. REPAIRED IAW DHC-8 SRM 53-00-16 AND 51-20-00 PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- SURFACE CORROSION ON RIGHT HAND INBOARD SEAT TRACK AT CARGO HOLD DOWN ATTACH POINT X597.500 AND 9.250. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND RD 8-53-4936.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION AROUND DME ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 7-8 AND 53-00-16 PAGE 3.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION ON FLOORBEAM AROUND RIVET AT FUSELAGE STATION X222.000 ONE FOOT INBOARD OF FORWARD EDGE OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 SRM 51-20-00 AND 53-00-16 TABLE 2.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND INBOARD AFT SEAT TRACK HAS PITTING CORROSION WHERE SEATS ATTACH TO TRACK. REPAIRED IAW DHC-8 AD 8-53-1339 AND DHC-8 SRM 51-20-00 PAGE 5.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION AT INBOARD AFT WARDROBE ATTACH BRACKET OF FUSELAGE STATION X222.00 AT LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND 53-00-16 TABLE 2.
Part: SKIN — GOUGED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE EXTERIOR SKIN HAS A GOUGE AT STRINGER 25 AND FRAME X600.000. REPAIRED IAW DHC-8 SRM 53-00-16 AND 51-20-00 PAGE 5.
Part: CLIP — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- RIGHT HAND EMERGENCY EXIT DOOR CUTOUT HAS MINOR SURFACE CORROSION ON CLIP AT FORWARD END OF INTERCOSTAL ON STRINGER 23. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND 53-00-16 TABLE 2.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION AROUND NUT FOR CROSS MEMBER ATTACHMENT TO STRINGER 31L AT FUSELAGE STATION X222.00. REMOVED CROSS MEMBER AND REPLACED WASHERS, REINSTALLED CROSS MEMBER.
Part: COVER — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- MINOR CORROSION AND SEALANT MISSING ON COVER PLATE ON BELLY OF AIRCRAFT AT FUSELAGE STATION X387.350. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND 51-30-26 PAGE 1-10.
Part: FRAME — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION ON FRAME BETWEEN STRINGER 27L AND 28L ON FRAME X151.600 OF LEFT HAND FUSELAGE. REPAIRED IAW DHC-8 SRM 51-20-00, 51-40-11 AND 53-00-16.
Part: FLOORBEAM — GOUGED (CABIN) · airframe 30,568 hrs · 42,755 cycles
YXX- UPPER CARGO DECK LEFT HAND FLOORBEAM Y9.250 HAS VARIOUS SPOTS OF CORROSION AND GOUGING BETWEEN X600.000 AND X644.897. REPAIRED IAW DHC-8 SRM 51-20-36 AND 51-20-16.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- UPPER CARGO DECK RIGHT HAND FLOORBEAM AT Y9.250 HAS VARIOUS SPOTS OF CORROSION AND GOUGING BETWEEN X600.000 AND X644.897. REPAIRED IAW DHC-8 SRM 51-20-36 AND 51-20-16.
Part: FITTING — CORRODED (AFT BULKHEAD) · airframe 30,568 hrs · 42,755 cycles
YXX- SURFACE CORROSION FOUND ON RIGHT HAND REAR BULKHEAD ATTACH FITTING X650.000 AND T23.000. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 8 FIGURE 4.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- LEFT HAND FUSELAGE HAS DENT BETWEEN STRINGER 24 AND 25 FORWARD OF FRAME X333.300. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-05 AND 51-00-06.
Part: WEB — CORRODED (CARGO BAY) · airframe 30,568 hrs · 42,755 cycles
YXX- CORROSION ON UNDER FLOOR WEB IN FORWARD CARGO AREA UNDER PANEL 144AZ. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 1-10, 51-20-00 PAGE 5 AND 51-40-11 PAGE 1-4.
Part: FRAME — GOUGED (FUSELAGE) · airframe 30,568 hrs · 42,755 cycles
YXX- FUSELAGE FRAME X424.124 HAS GOUGE AT FLOOR LEVEL JUST BELOW RIGHT HAND INBOARD TRACK SPLICE. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 9 AND 51-20-26 PAGE 6.
Part: STRUT — MALFUNCTIONED (PAX DOOR) · airframe 29,919 hrs · 41,853 cycles
BOI- MAIN CABIN DOOR WILL NOT OPEN. REMOVED AND REPLACED AFT MAIN CABIN DOOR SNUBBER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROL CABLE — OUT OF RIG (NR 2 PROPELLER)
PDX- UNABLE TO REDUCE NR 2 PROP RPM BELOW 925 RPM IN CRUISE PORTION OF FLIGHT. RETENSIONED NR 2 CONDITION CONTROL CABLES. PERFORMED ENGINE POWER AND CONDITION CONTROL RIGGING TEST, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: LIGHT — MALFUNCTIONED (CABIN)
PDX- SMELL IN CABIN SIMILAR TO FAILED LIGHTING BALLAST FROM UNKNOWN LOCATION. FOUND CENTER LIGHT FIXTURE MELTED. REMOVED AND REPLACED LIGHT FIXTURE AND BALLAST, OPERATIONAL CHECKS GOOD.
Part: POWER SUPPLY — FAILED (CABIN)
PDX - FLOOR TRACK LIGHTING FLICKERS IN FLIGHT. REMOVED AND REPLACED POWER PACKS 3352-PS1 AND 3352-PS2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — BROKEN (CABIN)
SEA - EXIT SIGN BELOW LEFT WINDOW EMERGENCY EXIT BROKEN. REMOVED AND REPLACED EXIT SIGN AT 4AB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
1999
Part: CONTROLLER — MALFUNCTIONED (CABIN)
SEA - EMERGENCY EXIT TRACK LIGHTING ILLUMINATED IN FLIGHT, CYCLED SWITH WITH NO CHANGE. MAINTENANCE REPLACED THE LIGHTING CONTROLLER. DURING OPERATIONAL CHECK THE FORWARD EXIT LOCATOR LIGHTS WENT OUT. REPAIRED A BROKEN WIRE UNDER THE FLOOR.
Part: WIRE — BROKEN (CARGO SMOKE DET)
SEA- SMOKE WARNING LIGHT CAME ON INTERMITTENTLY FOR ABOUT 5 SECONDS EACH TIME. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE OR SMOKE. FOUND 2 BROKEN WIRES AT THE CANNON PLUG ON THE NR 2 CARGO SMOKE DETECTOR. STOWED WIRES AND PLACED ON MEL.
1998
Part: BATTERY — DISCHARGED (CABIN)
TWO FORWARD FLOOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY, OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN)
PDX - FLIGHT ATTENDANT FLASHLIGHT DOES NOT TEST. REPLACED FLASHLIGHT BATTERY, OPERATIONAL CHECK GOOD.
1997
Part: ACTUATOR — REQUIRED SERVICE (ELEVATOR TRIM)
SEA - AT 20,000 FEET AUTO PILOT ENGAGED IN ICING CONDITIONS, MISTRIM NOSE DOWN ADVISORY LIGHT ILLUMINATED. DISCONNECTED AUTO PILOT AND AIRCRAFT PITCHED UP, ELIVATOR TRIM STUCK, ELEVATOR SLUGGISH. SERVICED ELEVATOR TRIM ACTUATOR. NO PARTS REPLACED, OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN)
SEA- LEFT HAND AFT EMERGENCY LIGHT AND AFT CABIN CEILING EMERGENCY LIGHT ARE INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
SEA - FORWARD TWO FLOOR EMERGENCY LIGHTS ON FLOOR STRIP INOP. REPLACED EMERGENCY POWER SUPPLY AND BATTERY ABOVE SEAT 1E. POWER SUPPLY SERIAL NUMBER 173, MANUFACTURER NUMBER 60-3844-1 TSN 25692 CSN 35543 TSR 9963, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
SEA- AFT OVRHEAD EMERGENCY EXIT LIGHT IS INOP. RELAMPED LIGHT, OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (CABIN)
EMERGENCY EXIT SIGN AT MAIN CABIN DOOR BROKEN. REPLACED EMERGENCY LIGHT HOUSING AT BOTTOM OF AIRSTAIR DOOR, OPERATIONAL CHECKS GOOD.
1996
Part: LIGHT — BROKEN (CABIN)
EMERGENCY LIGHT AT CABIN DOOR ENTRY BROKEN, REATTACHED COVER . LIGHT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROL BOX — MALFUNCTIONED (CABIN)
EMERGENCY LIGHTS WOULD NOT TURN OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND EMERGENCY LIGHTS OPS CHECKED GOOD.
1995
Part: LIGHT — MALFUNCTIONING (COCKPIT)
BOI - COCKPIT EMERGENCY FLASHLIGHT ILLUMINATES ON ITS OWN. LIGHT ASSY WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: EEL BULB — FAILED (CABIN)
SEA - ONE BULB INOP IN FORWARD RED FLOOR PROXIMITY LIGHT. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR)
SEA - GEAR SELECTED DOWN, DOORS DIDN'T OPEN AND GEAR DIDN'T EXTEND. PERFORMED ALTERNATE GEAR EXTENSION AND GEAR EXTENDED. LANDED WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. REPLACED GEAR SELECTOR VALVE AND GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE.