N360PH

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 37,875 hrs · 50,273 cycles

FOUND DAMAGE ON FORE RUDDER AND TRAILING RUDDER. PERMANENT REPAIR OF RUDDER IAW EA 38-2017-116.

Part: PROXIMITY SWITCH — INOPERATIVE (LEFT MLG) · airframe 37,705 hrs · 50,060 cycles

LEFT MAIN GEAR UNSAFE AND LEFT DOOR ADVISORY ILLUMINATED DURING TAXI. R & R THE PSEU IAW AMM 32-61-00. OPS CHECKED GOOD. GEAR SWINGS PERFORMED MULTIPLE TIMES IAW AMM 32-30-00. OPS CHECKED GOOD. NO DEFECTS NOTED. PERFORMED WIRING CHECK OF ALL LANDING GEARS, ALL VALVES FOUND TO BE WITHIN LIMITS. NO DEFECTS NOTED. CHECKED PSEU BOX FOR FAULT CODES. NO CODES FOUND. INSPECTED GAPS ON THE WOW SWITCHES IAW AMM 32-11-11. NO DEFECTS NOTED. PERFORMED LANDING SYSTEM CHECKED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 37,682 hrs · 50,033 cycles

LT DOOR LIGHT ON GEAR PANEL REMAIN ILLUMINATED AFTER TAKEOFF AND GEAR UP. FOUND A LEAK ON THE NOSE GEAR DOWN RIDGE LINE, WHICH CAUSED AIR TO BE INTRODUCED INTO HYDRAULIC SYSTEM. R & R THE LINE. LEAK CHECKED GOOD. JACKED AIRCRAFT AND PERFORMED TOTAL OF 1Z GEAR SWINGS AFTER BLEEDING HYDRAULIC SYSTEM. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE · airframe 37,586 hrs · 49,913 cycles

EMERGENCY LIGHTS INOPERATIVE. R&R EMERGENCY LIGHT SWITCH OPS CHECK SAT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 37,589 hrs · 49,916 cycles

MAIN CABIN DOOR EMERGENCY EXIT SIGN INOPERATIVE. FOUND CONNECTOR BEHIND EMERGENCY EXIT SIGN NOT SECURE. SECURED CONNECTOR OPS CHECKED SAT.

Part: SKIN — DENTED (BS 270-291) · airframe 37,583 hrs · 49,910 cycles

DENT LOCATED ON LT FUSELAGE SKIN BETWEEN BS 270.5 - 291, STRINGERS 9 - 10P. REPAIRED IAW RD 8-53-15173.

Part: STRUCTURE — DAMAGED (ACCESS PANEL) · airframe 37,583 hrs · 49,910 cycles

LADDER PLATE UNDER FUEL PANEL 624AT DAMAGED. REPAIRED IAW RD 8-57-7814.

Part: DECK PLATE — CHAFED (LT NACELLE) · airframe 37,583 hrs · 49,910 cycles

UPPER DECK ON LT NACELLE CHAFED THROUGH BY FINGERNAIL. DAMAGE CUT OUT.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

CENTER WING, RT T-DUCT SUPPORT BRACKET CRACKED. REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

RT FLOOR SUPPORT CRACKED UNDER FLIGHT DECK FLOOR UNDER CONTROL COLUMN. REPLACED RT FLOOR SUPPORT.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 37,583 hrs · 49,910 cycles

BAGGAGE DOOR COUNTERBALANCE CABLE AFT PULLEY BRACKET IS CRACKED. COUNTERBALANCE AFT CABLE REPLACED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

AFT RT KEEL STRINGER TENSION FITTING CORRODED. FITTING REPLACED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

CENTER WING, FD OF BLEED AIR T-DUCT, STIFFENER CRACKED. REPLACED, TREATED AND PRIMED.

Part: SKIN — DENTED (PAX DOOR) · airframe 37,583 hrs · 49,910 cycles

SMALL CRACK FOUND ON FWD SIDE OF BOTTOM BEAM OF PASSENGER DOOR SHELL. REMOVED CRACKED BEAM ASSEMBLY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

MINOR CORROSION FOUND ON BOTH FWD AND AFT OB LT SEAT RAILS. CORROSION REMOVED IAW RD 8-53-1342.

Part: STRUCTURE — CORRODED (BS 222) · airframe 37,583 hrs · 49,910 cycles

CORROSION FOUND ON UNDER FLOOR STRUCTURE LOCATED AT BS 222, RH31. WORK CARRIED OUT IN REFERENCE TO SRM 51-20-11 AND 51-20-36.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 37,583 hrs · 49,910 cycles

CORROSION FOUND IN CABIN UNDER FLOOR LOCATIONS RT 31 X270.5 X291.4 X312.35 X333.3. WORK CARRIED OUT IN REFERENCE TO SRM 51-20-11 AND SRM 51-20-36.

Part: BRACKET — DAMAGED (PAX DOOR STEP) · airframe 37,583 hrs · 49,910 cycles

SMALL AREA OF SURFACE CORROSION FOUND ON FWD AND AFT PASSENGER DOOR STEP LOWER ANGLES AND UPPER AFT SUPPORT BRACKET. BRACKETS FOUND TO BE DAMAGED. BRACKETS REPLACED AND CORROSION BLENDED.

Part: FRAME — CORRODED (BS 201) · airframe 37,583 hrs · 49,910 cycles

SKIN DEFECT AT STRINGER 31S AND BS 201.150. POSSIBLE CORROSION BETWEEN SKIN AND STRINGER. THE FRAME WAS CORRODED BEYOND LIMITS.

Part: PANEL — DAMAGED (RT WING) · airframe 37,583 hrs · 49,910 cycles

RT WING FUEL PANEL 624AT (IB PANEL) HAS 2 SCREW HOLES DAMAGED, DAMAGE ALSO CARRIED THROUGH TO THE LADDER PLATE. REPAIRED RD8-57-2673.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT)

EMERGENCY EXIT DOOR AT 2CD HAS A GAP. ADJUSTED DOOR PANEL AND RESET DOOR. NO DEFECTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,035 hrs · 49,297 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,035 hrs · 49,297 cycles

EMERGENCY LIGHT ABOVE MAIN CABIN DOOR INOPERATIVE. R & R THE POWER SUPPLY.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 36,931 hrs · 49,173 cycles

AUTOFEATHER DID NOT ARM DEPARTURE ROLL. PERFORMED OPERATIONAL CHECK ON AUTOFEATHER SYSTEM. OPS CHECKED GOOD.

Part: SWITCH — DIRTY (EMERGENCY LIGHT) · airframe 36,873 hrs · 49,105 cycles

EMERGENCY LIGHTS WILL NOT EXTINGUISH BY FA PANEL WHEN ARMED. CLEANED EMERGENCY LIGHT SWITCH. OPS CHECK SAT. NO DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,729 hrs · 48,937 cycles

DURING L CHECK, EMERGENCY LIGHTS FOUND INOPERATIVE. R & R EMERGENCY BATTERIES, OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,561 hrs · 48,716 cycles

EMERGENCY LIGHT OVER MAIN CABIN DOOR NOT ILLUMINATING. R & R EMERGENCY BATTERIES OPS CK SAT NO DEFECTS NOTED AT THIS TIME. ADDITIONAL BATTERIES REMOVED PN 61-0478-9, SN L-121, T/T 7033.75 T/C 8196; PN 61-0478-11, SN H133, T/T 40044.73, T/C 53849, 9802262 T/T 1074.45, T/C 1191, H129 T/T 41947.37, T/C 56964.

Part: ENGINE — SMOKE (NR 2) · airframe 36,312 hrs · 48,437 cycles

SMOKE IN THE FLT DECK AFTER ENGINE START. R & R ACM, OPS CHECK FAILED. BORESCOPE INSPECTION-1 AREA WAS MOIST WITH OIL RESIDUE BUT NOT COLLECTIBLE AS A QUANTITY. FOUND A DIFFUSER DUCT BOLT CLOGGING DRAIN, REMOVED BOLT, R & R NL PROBE O-RINGS. NOTE THAT ENGINE STILL SMOKES WHEN BLEED IS SELECTED. R & R NR 2 ENGINE. OPS AND LEAK CHECK SATISFACTORY.

Part: SWITCH — OUT OF ADJUST (CABIN) · airframe 36,166 hrs · 48,267 cycles

EMERGENCY LIGHTS WON'T EXTINGUISH USING FLIGHT ATTENDANT BUTTON. ADJUSTED FLIGHT ATTENDANT BUTTON BY ADJUSTING TWO SCREWS FOR THE SWITCH.

Part: INVERTER — INOPERATIVE (ELECTRICAL SYS) · airframe 36,043 hrs · 48,132 cycles

PRIMARY INVERTER FAIL WITH SMOKE ODOR. R & R PRIMARY INVERTER.

Part: HYDRAULIC LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 35,748 hrs · 47,806 cycles

NUMBER 1 ENG HYD PUMP, CAUTION FLICKERING, FOLLOWED BY NR 1 HYD QTY, LOSING ALL PRESS DURING FLIGHT. R & R NR 1 ENG HYD RESERVOIR FILLER LINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,672 hrs · 47,714 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R ALL EMER LIGHT BATTERY PACKS.

Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 35,572 hrs · 47,600 cycles

ON LANDING ROLLOUT WITH NR 2 ENG POWER LEVER AT DISK, THE TORQUE & RPM ADVANCED TO TAKEOFF POWER UN-COMMANDED. PERFORMED BETA BACKUP, OVERSPEED GOVERNOR, MINIMUM GOVERNOR & MAXIMUM GOVERNOR SPEED TEST, RUNS WERE SATISFACTORY WITH NO SIGNS OF TORQUE OR RPM SURGES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,509 hrs · 47,528 cycles

WITH LG DOWN & LOCKED, RECEIVED GEAR UNSAFE HORN AS WELL AS BOTH AMBER & RED GEAR UNSAFE LIGHTS, WHICH WERE ILLUMINATED. GEAR UNSAFE LIGHTS CYCLED 6 TIMES FROM AMBER TO RED WHILE PROCEEDING TO GO AROUND IN LEVEL FLIGHT. ALTERNATE EXTENSION PROCEDURES WERE EXECUTED TO ENSURE GEAR WAS DOWN & LOCKED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,265 hrs · 47,242 cycles

EMERGENCY LIGHTS FLICKER ON WHEN SELECTED, THEN GO OUT. R & R EMER BATTERY PS-2.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,090 hrs · 47,040 cycles

LOWER EMER LIGHTS IN THE CABIN ARE INOPERATIVE. R & R LIGHT POWER SUPPLY UNIT AT PS4. R & R EMER LIGHT SWITCH.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,085 hrs · 47,034 cycles

EMERGENCY LIGHTS WILL NOT OPERATE FROM THE FLIGHT ATTENDANT STATION. R & R EMER BATTERIES PS-1, PS-2 & PS-6.

Part: RELAY — FAILED (CABIN) · airframe 35,052 hrs · 47,000 cycles

FOUR EMER LIGHTS ARE INOPERATIVE. R & R 3351 K2 RELAY.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 35,049 hrs · 46,996 cycles

FOUR EMER EXIT LIGHTS IN CABIN AREA ARE NOT ILLUMINATED. RE-PINNED WIRE ON FLIGHT ATTENDANT SWITCH.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,870 hrs · 46,789 cycles

CABIN EMER LIGHTS WILL NOT ILLUMINATE. R & R ELEC POWER SUPPLY AT PS2.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,812 hrs · 46,718 cycles

EMERGENCY LIGHTS NOT OPERATING PROPERLY. RACKED BATTERY PACK PS4.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2 ENGINE) · airframe 34,386 hrs · 46,212 cycles

NUMBER 2 ENG SHUTDOWN AT 500 FEET. AFTER NR 2 ENG SHUTDOWN PILOT HEARD PROP FEATHER ON ITS OWN. AUTO FEATHER WAS ARMED & UP TRIM LIGHT ILLUMINATED. NO FIRE INDICATIONS, CAUTION LIGHTS CAME ON AS NORMAL WHEN NR 2 ENG SHUT OFF. TORQUE WAS AT 97 JUST BEFORE PROP FEATHERED & NOTICED NO REDUCTION OF POWER. R&R BOTH ENGINE TSCU'S.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,348 hrs · 46,168 cycles

CABIN DOOR EXIT SIGN DOES NOT STAY ILLUMINATED WHEN TESTED. R & R POSITION ONE EMER LIGHT BATTERY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,346 hrs · 46,166 cycles

CEILING & UPPER SIDEWALL EMER LIGHTS INOPERABLE. R & R EMER LIGHT BATTERIES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,194 hrs · 45,980 cycles

EMERGENCY LIGHTS INOPERABLE. R & R EMER BATTERIES.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,184 hrs · 45,971 cycles

LOWER MAIN CABIN DOOR EMER LIGHT WILL NOT ILLUMINATE WITH FLIGHT ATTENDANT SWITCH. R & R PS 3.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 34,041 hrs · 45,799 cycles

PASSENGER DOOR SILL HAS SUSPECTED CORROSION ON BOTTOM SURFACE. REPAIRED & INSTALLED NEW THRESHOLD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 34,041 hrs · 45,799 cycles

PASSENGER DOOR SILL HAS SUSPECTED CORROSION ON BOTTOM SERVICE. REPAIRED & INSTALLED NEW THRESHOLD. UPDATE CONTROL NR TO CORRECT DATE.

Part: RELAY — DEFECTIVE (CABIN) · airframe 33,894 hrs · 45,632 cycles

VERTICAL EMER EXIT LIGHT ABOVE FLIGHT ATTENDANT SEAT INOPERABLE. R & R RELAYS K3 & K4.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,807 hrs · 45,532 cycles

TWO EMER LIGHTS & THE MCD EXIT SIGN LIGHT ARE INOPERABLE. R & R POWER SUPPLY.

Part: LIGHT — LOOSE (CABIN) · airframe 33,790 hrs · 45,512 cycles

OVERHEAD EMER LIGHT INOPERABLE OVER ROW 21. SECURED BULB.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,772 hrs · 45,490 cycles

FLIGHT ATTENDANT EMER LIGHT SWITCH ONLY TURNS ON TWO OF THE FOUR OVERHEAD CABIN LIGHTS. R & R EMER LIGHT POWER SUPPLY UNIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,666 hrs · 45,365 cycles

TWO EMER LIGHTS OUT IN THE CEILING. PERFORMED AN ELEC RESET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,660 hrs · 45,360 cycles

TWO EMER LIGHTS OUT IN THE CEILING. PERFORMED AN ELEC RESET.

Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 33,650 hrs · 45,349 cycles

NUMBER 2 ENG TORQUE WENT TO 160% TORQUE ON CLIMB.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,599 hrs · 45,292 cycles

EMERGENCY LIGHTS IN CABIN INOPERABLE. CHARGED EMERGENCY LIGHT BATTERIES.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 33,566 hrs · 45,259 cycles

NUMBER 1 & NR 3 CEILING EMERGENCY LIGHTS INOPERABLE. CHARGED POWER SUPPLIES. OPERATIONS CHECKED SATISFACTORY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 3,356 hrs · 45,250 cycles

TWO CEILING EMER LIGHTS WILL NOT ILLUMINATE. CHARGED EMER LIGHT BATTERIES.

Part: BATTERY — NOT SEATED (CABIN) · airframe 33,503 hrs · 45,187 cycles

TWO OVERHEAD EMERGENCY LIGHTS WILL NOT TEST PROPERLY. REMOVED & RESEATED BATTERIES.

Part: LIGHT — BROKEN (CABIN) · airframe 33,487 hrs · 45,171 cycles

NR 3 EMERGENCY LIGHT FIXTURE BROKEN. R & R NR 3 EMERGENCY LIGHT FIXTURE. OPERATIONS CHECKED SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,487 hrs · 45,171 cycles

NR 1 & NR 3 OVERHEAD EMERGENCY LIGHTS INOPERABLE. R & R NR 2, NR 5 POWER SUPPLY UNITS & BATTERIES. OPERATIONS CHECKED SATISFACTORY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 33,487 hrs · 45,171 cycles

NR 1 & NR 3 OVERHEAD EMERGENCY LIGHTS INOPERABLE. FOUND LOOSE CONNECTOR ON PS1 BATTERY, CONNECT CONNECTOR. OPERATIONAL CHECK SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,423 hrs · 45,097 cycles

TWO EMERGENCY CEILING LIGHTS INOPERABLE. R & R PS3, OPERATIONS CHECKED SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,414 hrs · 45,089 cycles

MAIN CABIN DOOR EMERGENCY LIGHTS NOT ILLUMINATING. R & R ALL SIX EMERGENCY BATTERY POWER SUPPLIES. NO DEFECTS NOTED. OPERATIONS CHECKED SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,302 hrs · 44,958 cycles

EMERGENCY LIGHT BELOW FLIGHT ATTENDANT PANEL INOPERABLE. PERFORMED OPERATIONAL CHECK & FOUND TO BE SATISFACTORY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 32,974 hrs · 44,562 cycles

SMOKE WARNING LIGHT MOMENTARILY ILLUMINATED ON CLIMB OUT. CLEANED, INSPECTED & PERFORMED OPERATIONAL CHECK OF BAGGAGE SMOKE DETECTION, OPERATIONAL CHECKED SATISFACTORY, REQUIRES & OCF.

Part: SEAL — DAMAGED (NR 1 ENGINE) · airframe 32,918 hrs · 44,489 cycles

NR 1 ENG OIL PRESS ILLUMINATED IN FLIGHT. OIL PRESS DIPPED TO 40 PSI & NR 1 ENG WAS SHUT DOWN. REMOVED PCU & CHANGED SEALS.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 32,656 hrs · 44,182 cycles

TOP LIGHT ON EMERGENCY LIGHT SWITCH WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT SWITCH, OPERATIONS CHECKED SATISFACTORY IRW DH8 Q200 AMM 33-51-00. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (CABIN) · airframe 32,638 hrs · 44,162 cycles

SMOKE COMING FROM COMPARTMENT ABOVE CLOSET. REMOVED DUST FROM COMPARTMENT ABOVE CLOSET. INSPECTED WIRING & EQUIPMENT IN WARDROBE AREA, NO DEFECTS FOUND.

Part: PUMP — INOPERATIVE (NR 2 ENGINE) · airframe 32,179 hrs · 43,585 cycles

DURING CLIMB, NR 2 ENGINE POWER LEVER NOT RESPONSIVE. R & R NR 2 ENGINE MFC AND FUEL PUMP AND RIGGED.

Part: LIGHT — INOPERATIVE · airframe 31,983 hrs · 43,339 cycles

EMERGENCY LIGHTS OVER ROW 9 INOPERATIVE. CYCLED EMERGENCY LIGHTS, OPS CHECK SATISFACTORY.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,525 hrs · 42,787 cycles

THE EMERGENCY LIGHT POWER SUPPLY AT PS3 WAS FOUND INOPERATIVE. THE POWER SUPPLY WAS REPLACED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,470 hrs · 42,717 cycles

CREW REPORTED THAT THE FIRST AND 3RD EMERGENCY LIGHT IN THE CEILING WAS INOPERATIVE. MX ALLOWED THE BATTERIES TO CHARGE. ONCE THEY WERE CHARGED ALL TEST WERE SATISFACTORY.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,453 hrs · 42,699 cycles

CREW REPORTED THAT THE 1ST AND 3RD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX CHARGED THE POWER SUPPLY.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 31,439 hrs · 42,679 cycles

CREW REPORTED THAT THE NLG CYCLED TWICE IN FLIGHT. MX REPLACED THE NLG DRAG STRUT SENSOR.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,433 hrs · 42,673 cycles

DURING PRE-FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 1 WAS INOPERATIVE. MX REPLACED THE BULB FOR THE EMERGENCY LIGHT.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 31,418 hrs · 42,653 cycles

DURING GEAR RETRACTION, THE CREW REPORTED THE NOSE GEAR DOOR CYCLED AND GEAR RETRACTION WAS SLOW TO COME UP. MX CREW REPLACED A HYD FLUID LINE IN THE NOSE WHEEL WELL.

Part: LIGHT — UNKNOWN · airframe 31,400 hrs · 42,627 cycles

DURING PREFLIGHT, CREW OBSERVED 2 CEILING EMERGENCY LIGHT WERE NOT TESTING. MX WAS UNABLE TO DUPLICATE.

Part: COVER — BURNED (LIGHT) · airframe 31,246 hrs · 42,444 cycles

CREW REPORTED A STRONG ODOR OF BURNING RUBBER OR PLASTIC IN FLIGHT DECK. MX R & R THE TOP AIR STAIR DOOR LIGHT COVER.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,101 hrs · 42,271 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CEILING WERE NOT FUNCTIONING. GROUND MX CREW R & R THE EMERGENCY LIGHT BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,990 hrs · 42,134 cycles

DURING PRE-FLIGHT THE CREW REPORTED THAT THE FIRST AND THIRD EMERGENCY LIGHTS WERE NOT ILLUMINATING DURING TESTING. GROUND MX CREW OPERATIONALLY CHECKED THE EMERGENCY LIGHTS AND OBSERVED THAT ALL EMERGENCY LIGHTS WERE OPERATING NORMALLY AND NONE APPEARED TO BE NON OPERATIONAL. THE GROUND MX CREW WAS UNABLE TO DUPLICATE THE ISSUE REPORTED. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,982 hrs · 42,123 cycles

DURING A SERVICE CHECK, THE TECH OBSERVED THE LT SIDE AFT EMERGENCY LIGHT WAS NOT ILLUMINATING. THE TECH R & R THE LAMP. ALL OPS CHECKS WERE SATISFACTORY.

Part: HYDRAULIC SYSTEM — CONTAMINATED (HYD SYSTEM) · airframe 30,950 hrs · 42,080 cycles

DURING CLIMB, CREW REPORTED THE LEFT NOSE DOOR WOULD NOT CLOSE AND THAT THE NR 2 ENGINE HYD PUMP LIGHTS ILLUMINATED, AND THE ROLL SPOILER HYD CAUTION LIGHT ILLUMINATED. GROUND MX CREW BLED AIR FROM THE HYD SYSTEMS. THE GROUND MX CREW PERFORMED A RETRACTION CHECK OF THE LANDING GEAR SYSTEM. ALL OPS AND LEAK CHECKS PRODUCED SATISFACTORY RESULTS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 30,945 hrs · 42,074 cycles

DURING PREFLIGHT IT WAS REPORTED THAT SEVERAL INTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TESTING. GROUND MX CREW FOUND A RECESSED PIN IN A CONNECTOR PLUG. THE PIN WAS REPAIRED AND ALL OPS CHECKS PRODUCED SATISFACTORY RESULTS.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 30,950 hrs · 42,079 cycles

DURING FLIGHT, CREW REPORTED THAT THE AMBER NOSE GEAR LIGHT AND THE RED NOSE GEAR LIGHT ILLUMINATED BRIEFLY AND BOTH OF THEM THEM EXTINGUISHED. GROUND MX CREW R & R THE NLG SENSOR. ALL OPS CHECKS PRODUCED SATISFACTORY RESULTS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,863 hrs · 41,984 cycles

DURING A LINE CHECK INSPECTION, NOTICED THE LT AFT EMERGENCY EXIT LIGHT WAS NOT ILLUMINATING DURING TESTING. REPLACED THE EMERGENCY LIGHT BATTERY AND CONDUCTED AN OPS TEST WHICH PRODUCED SATISFACTORY RESULTS.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,219 hrs · 39,920 cycles

DURING PRE-FLIGHT INSPECTION, CREW NOTICED THE EMERGENCY LIGHT OVER THE CABIN DOOR WAS INOPERATIVE. THE GROUND CREW RETESTED IAW MX CONTROLS AND EMERGENCY LIGHT TESTED SATISFACTORY ON THE SECOND ATTEMPT. THE ACFT WAS RELEASED TO FLIGHT STATUS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,115 hrs · 39,794 cycles

DURING PRE-FLIGHT INSPECTION, FLIGHT CREW NOTICED THAT THE EMERGENCY LIGHT ABOVE THE MAIN CABIN DOOR WAS INOPERATIVE. GROUND MX CREW ALLOWED THE EMERGENCY LIGHT BATTERIES TO CHARGE, AND PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHTING SYS. OPS CHECKED SATISFACTORY. ACFT RELEASED TO FLIGHT STATUS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,070 hrs · 39,733 cycles

FLIGHT CREW DISCOVERED CEILING EMERGENCY LIGHT 1 AND 3 INOPERATIVE DURING GROUND INSPECTION. CHARGED BATTERIES AND ALLOW ACFT TO WARM. OPS CHECKED SATISFACTORY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 29,050 hrs · 39,702 cycles

DURING PRE-FLIGHT INSPECTION, FLIGHT CREW NOTICED THAT AN EMERGENCY LIGHT FLOOR STRIP WAS INOPERATIVE. GROUND MX CREW RESECURED EMERGENCY LIGHT STRIP ELECTRICAL CONNECTOR. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYS, OPS CHECKS WERE SATISFACTORY. ACFT RELEASED TO FLIGHT STATUS.

Part: LIGHT — BROKEN (CABIN) · airframe 28,942 hrs · 39,560 cycles

FLIGHT CREW REPORTED THAT THE ISLE EMERGENCY LIGHT BROKEN. MX CREW R &R LIGHT LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,781 hrs · 39,356 cycles

CEILING EMERGENCY LIGHTS ARE NOT WORKING. MX CREW R & R THE BATTERY SUPPLY PERFORMED. OPS CHECK SATISFACTORY.

Part: OIL SYSTEM — OVERSERVICED (ENGINES) · airframe 28,156 hrs · 38,556 cycles

FLIGHT CREW REPORTED SMOKE IN COCKPIT ON START. MX CREW FOUND BOTH ENGINES OVERSERVICED WITH OIL. PERFORMED GROUND RUNS AND ODOR/SMOKE WAS GONE. ACFT WAS RETURNED TO FLIGHT STATUS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,023 hrs · 38,391 cycles

FLIGHT CREW REPORTED OVERHEAD EMERGENCY OVERHEAD LIGHTS NOT ILLUMINATED IN ROW 1 AND 7. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IN POSITION PS3. PERFORMED OPS CHECK SATISFACTORY.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 27,920 hrs · 38,259 cycles

DURING PREFLIGHT INSP AIRCREW NOTICED THE EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROW 1. GROUND MX CREW REPLACED THE FLOOR STRIP AT ROW 1. OPS CHECK WAS PERFORMED ON THE EMERGENCY LIGHTS SYS. OPS CHECKED SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,744 hrs · 38,046 cycles

DURING PREFLIGHT INSP, AIRCREW REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY LIT WHEN TESTED FROM FA STATION. AIRCREW SHUT SYS DOWN AND ALLOWED TO RECHARGE. PERFORMED SYS CHECK AND OPS CHECKED SATISFACTORY. ACFT RETURNED TO FLIGHT STATUS.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 22,115 hrs · 31,143 cycles

MECH WAS TRYING TO EASY-OUT A SCREW FROM LEFT LADDER PLATE (STATION 5711069, BETWEEN YW74.4 AND YW90.6 ON STRINGER 6) DRILLED A HOLE INTO THE LADDER PLATE. PERMANENT REPAIR (RD 8-57-93) WAS COMPLIED WITH ON 23 FEB 2008, BY DOING A BUSHING REPAIR FOR THE DAMAGED HOLE. TO BE REINSPECTED BY STANDARD HIGH FREQUENCY EDDY CURRENT AT INTERVALS OF 8160 FLIGHTS.

Part: BRAKE ASSY — MALFUNCTIONED (NLG) · airframe 20,498 hrs · 29,573 cycles

SEA FLIGHT NR 2070, NOSE LANDING GEAR VIBRATION WHEN BRAKES ARE APPLIED. MAINTENANCE REPLACED BOTH BRAKE ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 20,460 hrs · 29,511 cycles

SEA FLIGHT NR 2234, LOUD NOISE FROM NOSE WHEEL STEEERING, NOSE WHEEL STEERING INOP. MAINTENANCE PLACED ON MEL

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 19,941 hrs · 28,767 cycles

SEA - ON FLIGHT 2076, EMERGENCY LIGHTS FLICKERED DURING CLIMB IN SMOOTH AIR. MAINTENANCE REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 19,934 hrs · 28,758 cycles

PDX - ON FLIGHT 2034, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. RESET AS PER CHECKLIST STAYED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 19,725 hrs · 28,476 cycles

SEA FLIGHT NR 2006 AT THE END OF THE RUNWAY, THE RIGHT WINDSHIELD HOT CAUTION ILLUMINATED AS PER CHECKLIST WITH WINDSHIELD HEAT IN WARM-UP THE CAUTION LIGHT EXTINGUISHED. AFTER TURNED THE HEAT BAD TO NORM AFTER FOUR MINUTES LEFT AND RIGHT WINDSHIELD HOT CAUTION LIGHTS ILLUMINATED. BOTH EXTINGUISHED IN WARM-UP. MAINTENANCE REPLACED CO-PILOT WINDSHIELD HEAT CONTROLLER. PERFORMED OPERATIONAL TEST OF PILOT AND CO-PILOTS WINDSHIELD HEATING SYSTEM IAW Q200 AM TASK 30-41-0-710-801. OPERATIONAL CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - FUSELAGE INTERIOR BAGGAGE PIT UNDER FLOOR SHEAR WEB UNDERSIDE TRANSVERSE ATTACH ANGLE AT STATION X580 LBL25 IS CRACKED IN THE RADIUS. REPAIRED IAW SRM 51-40-11 AND EA 2-53-784.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 19,420 hrs · 28,048 cycles

LT UPPER WING ACCESS PANEL CUTOUT, TOP SURFACE OF LADDER PLATE HAS CHAFE DAMAGES. REPAIRED IAW RD8-57-3486.

Part: BRACKET — CORRODED (BS 600 S24) · airframe 19,420 hrs · 28,048 cycles

C4 YYC-LT INTERIOR FUSELAGE STATION 600 AT STRINGER 24 HAS CORROSION ON MACHINED BRACKET. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-26.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - VERTICAL STAB RIGHT SKIN HAS A 2" SCRATCH IN IT, RIB 8 BETWEEN MID SPAR AND AFT SPAR. REPAIRED IAW RD8-55-1758.

Part: PANEL — FOD (RT WING) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - RIGHT WING UPPER TANK PANEL 622AT BOTTOM EDGE OF PANEL DAMAGED BY FOREIGN OBJECT AT YN52 AND REBATE ON WING ALSO DAMAGE AT SAME LOCATION. REPAIRED IAW RD8-57-3485.

Part: PLATE — GOUGED (LT WING TANK) · airframe 19,420 hrs · 28,048 cycles

LT WING INNER FUEL TANK 526AT LADDER PLATE HAS MECHANICAL GOUGE. REPAIRED IAW RD8-57-611.

Part: CHANNEL — CHAFED (RT NACELLE) · airframe 19,420 hrs · 28,048 cycles

RT NACELLE STATION XN121 FIREWALL SEAL CHANNEL WORN THROUGH ABOVE OIL COOLER. REPAIRED IAW SRM 51-40-11.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 19,420 hrs · 28,048 cycles

LT WING UPPER ACCESS PANEL 523AT HAS CHAFE DAMAGE ON MATING SURFACE. REPAIRED IAW RD8-57-684.

Part: SILL — CORRODED (THRESHOLD) · airframe 19,420 hrs · 28,048 cycles

AIRSTAIRS DOOR CUTOUT LOWER SILL MEMBER HAS MULTIPLE AREAS OF CORROSION ON THE SURFACE. REPAIRED IAW SRM 51-20-11 AND SRM 51-20-36, SRM 51-40-11.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - LEFT ELEVATOR UPPER SKIN ON HORN HAS MANY SMOKING AND LOOSE RIVETS AND HAS SKIN DAMAGE. REPAIRED IAW RD8-55-324.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 19,420 hrs · 28,048 cycles

BAGGAGE COMPARTMENT LT SIDE FLOOR WEB HAS CORROSION AT (B) ANCHOR NUT LOCATIONS BETWEEN STATION X547 AND X600. REPAIRED IAW SRM 51-40-11, 51-20-11, 51-20-36, AND 51-20-51.

Part: PANEL — CORRODED (PAX DOOR) · airframe 19,420 hrs · 28,048 cycles

DOOR SHELL PANEL HAS CORROSION UNDER AL NUT AT FORWARD LOWER CORNER. REPAIRED IAW RD8-52-647 AND SRM 51-40-11.

Part: PANEL — DAMAGED (NR 2 NACELLE) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - NR 2 NACELLE TOP STRUCTURE INBOARD AND OUTBOARD FILLET PANELS BETWEEN XN110 AND XN127 HAS 7 LOOSE RIVETS. REPAIRED IAW SRM 51-40-00.

Part: WEB — CORRODED (FUSELAGE) · airframe 19,420 hrs · 28,048 cycles

BAGGAGE COMPARTMENT THRESHOLD TROUGH WEB HAS CORROSION ON TOP SURFACE BETWEEN STATION X571 AND X600. REPAIRED IAW SRM 51-20-11, 51-20-36, AND 51-20-51.

Part: WEB — CORRODED (FUSELAGE) · airframe 19,420 hrs · 28,048 cycles

BAGGAGE COMPARTMENT LT SIDE FLOOR WEB LIGHTNING HOLE AT STATION X573 LBL12.0 HAS CORROSION ON UNDERSIDE OF FLANGE. REPAIRED IAW SRM 51-20-11, 51-20-36, AND SRM 51-2051.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 19,420 hrs · 28,048 cycles

C4 YYC - NR 2 NACELLE HORSE COLLAR EXTERIOR SKIN PANEL HAS LOOSE RIVETS AT TOP ENGINE MOUNT AREA. REPAIRED IAW SRM 51-40-00.

Part: PRESSURE SWITCH — FAILED (RUDDER) · airframe 18,896 hrs · 27,240 cycles

YVR FLIGHT 2233 (SEA) RUDDER FULL PRESSURE ON TAKEOFF. MAINTENANCE REPLACED FULL PRESSURE SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RUDDER — OUT OF LIMITS · airframe 18,457 hrs · 26,576 cycles

SEA FLIGHT NR 2070, RUDDER TRAVEL CHECK FAILED ON THE LEFT SIDE DURING AFTER START FLOW. RUDDER TRAVEL CHECK WORKED ON PROPERLY TO RIGHT SIDE. MAINTENANCE COMPLIED WITH RUDDER TRAVEL CHECK IAW MTC 972002 TRAVEL FOUND TO BE OUT OF LIMITS. COMPLIED WITH RIGGING CHECK IAW MTC 9272004 TRAVEL CHECK GOOD. AIRCRAFT OK TO CONTINUE SERVICE.

Part: STARTER GEN — MALFUNCTIONED (ENGINE) · airframe 17,827 hrs · 25,657 cycles

SEA FLIGHT NR 2062, DURING CLIMB-OUT NR 1 DC GENERATOR HOT CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST ITEMS FOR THAT CAUTION LIGHT. MAINTENANCE REPLACED NR 1 DC STARTER/GENERATOR IAW MTC 9801001. OPERATIONAL CHECK OF DC GENERATORS GOOD PER DHC 8 MM 24-31-00, PAGE 501-504.

Part: CONNECTOR — DIRTY (NR 1 ENG TORQUE) · airframe 17,731 hrs · 25,523 cycles

SEA FLIGHT NR 2004, NR 1 ENGINE TORQUE WENT TO 108 PERCENT FOR LESS THAN A SECOND THEN RETURNED TO NORMAL TORQUE WITH POWER LEVER BEING SLIGHTLY ADVANCED FROM DISC SETTING WHILE BEGINNING TO TAXI NO OTHER ABNORMAL INDICATIONS. MAINTENANCE PERFORMED A DATA DOWNLOAD OF THE FDR AND FOUND TORQUE DID NOT EXCEED 91.6 PERCENT. CLEANED CONNECTORS AT THE PCU, MFC AND ECU. ALSO PERFORMED A RIGGING CHECK OF THE NR 1 ENGINE IAW QX MTC 9761002. NO DEFECT NOTED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LOOSE (CARGO) · airframe 17,644 hrs · 25,396 cycles

GEG FLIGHT NR 2207 AT FL220 TOTAL PRESSURIZATION FAILURE. DESCENDED TO 80. LANDED WITHOUT INCIDENCE. MAINTENANCE REMOVED AFT BAG DOOR AND PERFORMED BENCH RIGGING. RE-INSTALLED AFT CARGO DOOR IAW AMM TASK 52-30-00-400-801 COMPLIED WITH ADJUSTMENT OF BAGGAGE DOOR ON AIRCRAFT IAW AMM TASK 52-30-00-820-801. OPERATIONAL TEST GOOD. PRESSURIZED AIRCRAFT AND CHECKED DOOR IAW TASK 52-30-00-820-801. NO LEAKS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: STARTER GEN — MALFUNCTIONED (NR 2) · airframe 17,421 hrs · 25,077 cycles

SEA FLIGHT NR 2220, ON CLIMB-OUT NR 2 DC GENERATOR CAUTION LIGHT, RAN CHECKLIST, NR 2 DC GENERATOR CAUTION LIGHT REMAINS ILLUMINATED. MAINTENANCE REPLACED THE STARTER/GENERATOR AND CONTROL UNIT. CONTROL UNIT PART NUMBER 51539-008C, SERIAL NUMBER 3730, TSN 27436, CSN 38720, TSR 10787. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 17,219 hrs · 24,784 cycles

PDX FLIGHT 2289 RIGHT WINDSHIELD HOT CAUTION LIGHT ON TOP OF DESCENT. WINDSHIELD FELT HOT, OAT WAS +1 DEGREE CELCIUS. RAN CHECKLIST AND THEN LIGHT WENT OUT. MAINTENANCE REPLACED RIGHT WINDSHIELD HEAT CONTROLLER IAW ANN TASK 30-41-00-710-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — CONTAMINATED (MLG) · airframe 17,060 hrs · 24,553 cycles

ON FLIGHT 2219, PASSENGERS AND FUELER REPORTED MODERATE SMOKE COMING FROM RIGHT (FO SIDE) OUTBOARD BRAKE ASSEMBLY. INSPECTED NR 3 AND NR 4 BRAKES. NO LEAKS NOTED. FOUND RESIDUAL HYDRAULIC FLUID FROM ANTI-SKID TEST DONE BEFORE PREVIOUS FLIGHT. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 16,577 hrs · 23,811 cycles

RT FORWARD EMERGENCY EXIT SIGN AND EXIT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER SUPPLY UNIT 3351 PS2 AND BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 15,998 hrs · 22,928 cycles

PSC - ON FLIGHT NUMBER 2096, SMOKE WARNING AND MASTER WARNING ILLUMINATED INTERMITTENTLY. NO AUDIBLE OR VISUAL INDICATION AND NO SMOKE NOTICED. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE, C/W OPERATIONAL TEST OF BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM. OPERATIONAL TESTS GOOD. REMOVED AND REPLACED SMOKE DETECTOR AS PRECAUTIONARY MEASURES. AIRCRAFT RETURNED TO SERVICE.

Part: STOP — OUT OF ADJUST (MAIN CABIN DOOR) · airframe 7,575 hrs · 8,179 cycles

CREW REPORTS THE MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND FOUND THE FORCE REQUIRED TO OPEN THE DOOR WAS 35 LBS. THE DOWN LIMIT STOP WAS ADJUSTED IAW THE AMM AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: REGULATOR — FAILED (RUDDER) · airframe 15,169 hrs · 21,700 cycles

PDX - FLIGHT 2048 - AIRCRAFT RETURNED TO FIELD AFTER THE RUDDER PRESSURE CAUTION LIGHTS CAME ON DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED RUDDER DUAL PRESSURE REGULATOR AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS WERE GOOD, NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FAILED (AFT CARGO) · airframe 14,977 hrs · 21,426 cycles

SEA - FLIGHT 2071 - THE CREW REPORTED AN INTERMITTENT SMOKE WARNING IN CRUISE FLIGHT. THERE WAS NO EVIDENCE OF SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 AFT CARGO PIT FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (FLT GUIDANCE) · airframe 14,964 hrs · 21,405 cycles

RDM- AFTER TOUCHDOWN, BOTH MAIN GEAR ON THE GROUND, NOSE IN THE AIR, RT AILERON APPLIED FOR CROSSWINDS, CONTROL COLUMN FROZE IN PLACE AND HAD TO BE OVERPOWERED. BOTH PITCH AND ROLL STUCK IN PLACE. AIRCRAFT ACCOMPLISHED AN UNEVENTFUL TAXI TO THE GATE. FIRST OPERATION CHECK FLIGHT FAILED. MAINTENANCE REPLACED BOTH FLIGHT GUIDANCE COMPUTERS, AND THE AFCS CONTROL PANEL. SECOND OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. AFCS CONTROL PANEL S/N 90101208 (6778 TSR), NR 2 FLIGHT GUIDANCE COMPUTER S/N 96064529 (3317 TSR).

Part: WIRE — BROKEN (ZONE 200) · airframe 14,458 hrs · 20,644 cycles

CARGO BAY FORWARD SMOKE DETECTOR WIRES ARE BROKEN. REMOVED AND REPLACED WIRE 2612-1J3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRAP — GOUGED (ZONE 200) · airframe 14,466 hrs · 20,656 cycles

PDX - GOUGE IN SPLINE STRAP, X264.10 NEXT TO RIGHT HAND FORWARD EMERGENCY EXIT DOOR, Z155.55, .022 DEEP .175 DIAMETER. REPAIRED IAW HORIZON AIR EA 2-53-565.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 14,457 hrs · 20,640 cycles

CRACKED BRACKET AT MAIN CABIN DOOR APERTURE FLOOR LEVEL STATION 240.500. REPAIRED IAW DHC-8-200 SRM 51-40-11.

Part: BRACKET — CRACKED (ZONE 500) · airframe 14,457 hrs · 20,640 cycles

LT WING FORWARD SPAR Z BRACKET IS CRACKED AT APPROXIMATELY STATION YW48.000. REPAIRED IAW SRM 51-40-11 AND EA 2-57-267.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,457 hrs · 20,640 cycles

PDX - RT OB TRACK NR 12 SEAT ATTACH AREA CORROSION, BARE METAL APPROXIMATELY X518.00. REPAIRED IAW SRM 51-40-00.

Part: BRACKET — CRACKED (ZONE 600) · airframe 14,457 hrs · 20,640 cycles

RT WING LEADING EDGE HAS A CRACKED BLEED AIR ZEE BRACKET AT YW48. REPAIRED IAW 8-200 SRM 51-40-11 AND EA 2-57-267.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 14,466 hrs · 20,656 cycles

PDX - INBOARD FORWARD SEAT TRACK NR 4 HAS AREAS OF HEAVY CORROSION FROM STATION 201.000 TO 359.400. REPAIRED IAW RD 8-53-4473 AND RD 8-53-1102.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,457 hrs · 20,640 cycles

RT OB TRACK NR 11 SEAT ATTACH AREA CORROSION APPROXIMATELY X 500.00. REPAIRED IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,457 hrs · 20,640 cycles

PDX - RT OB TRACK NR 10 SEAT ATTACH AREA CORROSION APPROXIMATELY X424.00. REPAIRED IAW SRM 51-40-11.

Part: PRESSURE SWITCH — INOPERATIVE (ZONE 300) · airframe 14,261 hrs · 20,357 cycles

PDX - ON FLIGHT NUMBER 2092, ON TAKEOFF ROLL AFTER POWER WAS APPLIED AT ABOUT 50 KIAS, THE RUD FULL PRESSURE CAUTION LIGHT ILLUMINATED. THE LIGHT HAD EXTINGUISHED WHEN THE TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 2 RUD FULL PRESSURE SWITCH ON THE RUDDER DUAL PRESSURE REGULATOR. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — LOOSE (CARGO DOOR) · airframe 14,192 hrs · 20,239 cycles

PDX-AFT CARGO DOOR SKIN HAS NUMEROUS RIVETS SHOWING WORK TRAILS AND MISSING PAINT INDICATING RIVET MOVEMENT. REPAIRED IAW D-8 200 SRM 51-40-11.

Part: NUT PLATE — DAMAGED (FUSELAGE) · airframe 14,161 hrs · 20,189 cycles

PDX- PANEL 121BL HAS A BAD NUTPLATE ON LOWER ROW. DOME SEALED NUT PLATE IAW DHC-8 SRM 51-23-00.

Part: NUT PLATE — DAMAGED (FUSELAGE) · airframe 14,161 hrs · 20,189 cycles

PDX- RT FORWARD FUSELAGE PANEL 122AR HAS TWO BAD NUTPLATES. DOME SEALED NUTPLATES IAW DHC-8 SRM 51-23-00.

Part: DOOR — BINDING (MAIN CABIN) · airframe 14,094 hrs · 20,095 cycles

THE MAIN CABIN DOOR BINDS DURING OPENING. DOOR MUST BE MANUALLY MOVED TO THE OPEN POSITION. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR HINGES AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — FAILED (ZONE 200) · airframe 13,994 hrs · 19,939 cycles

ON FLIGHT 2193 FORWARD EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED FORWARD SECTION OF AISLE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT REUTNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 13,661 hrs · 19,420 cycles

PDX - AFT UPPER EMERGENCY LIGHT AND AFT RIGHT HAND SIDE EGRESS LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED PS4 AND PS6 POWER SUPPLY.

Part: NUT PLATE — BROKEN (PANEL) · airframe 13,616 hrs · 19,353 cycles

PDX - MAINTENANCE FOUND SEVERAL NUT PLATES BROKEN ON PANEL 122BR. REMOVED AND REPLACED BROKEN NUT PLATES IAW SRM 51-40-11.

Part: STARTER GEN — MALFUNCTIONED (NR 2) · airframe 13,601 hrs · 19,335 cycles

SEA - ON FLIGHT 2108 UPON DC POWER APPLICATION, SMOKE CAME OUT OF NR 2 STARTER GENERATOR. REMOVED AND REPLACED STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 12,574 hrs · 17,839 cycles

SEA- ON FLIGHT 2176 RETURNED TO FIELD DUE TO, AFTER DEPARTURE RECIEVED AN INTERMITTENT SMOKE WARNING INDICATION. REMOVED AND REPLACED AFT BAGGAGE COMPARTMENT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — TORN (EMERGENCY AIR) · airframe 12,291 hrs · 17,409 cycles

SEA-FOUND TORN DUCT HOSE ON EMERGENCY AIR SUPPLY LOCATED ABOVE AIRCRAFT CONDENSOR. REMOVED AND REPLACED EMERGENCY AIR SUPPLY DUCT HOSE. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ZONE 200) · airframe 11,674 hrs · 16,498 cycles

SEA-ON FLIGHT NUMBER 2002, ON PUSHBACK, MASTER WARNING SMOKE LIGHT CAME ON FOR ABOUT 15 SECONDS, THEN WENT OUT. INVESTIGATED BOTH SMOKE DETECTORS IN AFT CARGO BAY, NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK, OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (ZONE 200) · airframe 11,640 hrs · 16,446 cycles

PSC- EMERGENCY FLOOR STRIP LIGHTING HAS TWO MISSING RED LIGHTS ON SECOND STRIP FOR FORWARD EMERGENCY EXIT. REMOVED AND REPLACED FLOOR STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — INTERMITTENT (ZONE 200) · airframe 11,386 hrs · 16,069 cycles

PDX- EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANTS POSITION INTERMITTANT. REPLACED FLIGHT ATTENDANT'S EMERGENCY LIGHT SWITCH 3351-S2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BUSHING — BACKED OUT (PAX DOOR) · airframe 11,083 hrs · 15,631 cycles

BOI- MAIN CABIN DOOR WILL NOT OPEN. FOUND AFT HANDRAIL EXTENSION PIVOT BUSHING BACKED OUT. RESECURED BUSHING. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CABIN) · airframe 10,986 hrs · 15,495 cycles

BOI ON FLIGHT 2201- SMOKE WARNING CAME ON INTERMITTENTLY DURING FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FORWARD SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BOLT — BACKED OUT (PAX DOOR) · airframe 10,849 hrs · 15,300 cycles

PDX-MAIN CABIN DOOR VERY DIFFICULT TO OPEN, GRINDING AND IT POPS HARD. FOUND AFT HANDRAIL OVER CENTER ROD CONNECTING BOLT BACKED OUT. RETIGHTENED BOLT. MAIN CABIN DOOR OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HYDRAULIC LINE — BROKEN (HYD SYSTEM) · airframe 10,783 hrs · 15,207 cycles

PDX- RETURNED TO FIELD DUE TO NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT IS ILLUMINATED. NR 2 HYDRAULIC QUANTITY INDICATOR IS ZERO. AIRCRAFT WAS FLOWN WITH ZERO FLUID FOR 50 MINUTES. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE DRIVEN PUMP, CASE DRAIN FILTER AND BROKEN RIGHT HAND NOSE LANDING GEAR DRAG STRUT ACTUATOR HYDRAULIC LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 10,383 hrs · 14,628 cycles

SEA- FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR IS HARD TO OPERATE. CLEANED AND LUBED HANDLE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: REGULATOR — FAILED (ZONE 300) · airframe 10,233 hrs · 14,418 cycles

PDX - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF AND PASSING 140KTS, THEY RECEIVED CAUTION LIGHTS FOR "RUDD FULL PRESS" AND "RUDD PRESS". BELOW 14O KTS THE LIGHT WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RUDDER DUAL PRESS REGULATOR IAW THE MAINTENANCE MANUAL. OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — CONTAMINATED (MAIN SYS) · airframe 10,233 hrs · 14,417 cycles

PDX - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDD FULL PRESS CAUTION LIGHT FOLLOWED BY A RUDD PRESS CAUTION LIGHT. BOTH LIGHTS WENT OUT WHEN FLAPS WERE AT 15 DEGREES PRIOR TO LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND AIR IN THE HYDRAULIC SYSTEM. SYSTEM WAS BLED AND SERVICED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — DEFECTIVE (PAX DOOR) · airframe 10,077 hrs · 14,179 cycles

SEA- PASSENGER CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED LOWER GAS SPRING STRUT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLEX LINE — LEAKING (ZONE 700) · airframe 10,071 hrs · 14,167 cycles

PDX- HOLDING SHORT OF RUMWAY, STARTED LOOSING NO.2 HYDRAULIC QUANTITY. NO.2 ENGINE HYDRUALIC PRESSURE LIGHT CAME ON. SHUT DOWN ENGINES AND WAS TOWED BACK TO THE GATE. REMOVED AND REPLACED FLEX LINE BETWEEN NO.3 MAIN LANDING GEAR BRAKE FITTING AND MAIN LANDING GEAR HARD LINE SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (T/E FLAP) · airframe 9,981 hrs · 14,038 cycles

PDX - OUTBOARD FLAP HAS TWO AREAS OF CHAFE DAMAGE ON THE UPPER INBOARD SURFACE. REPAIRED IAW DHC-8-200 SRM 51-20-16.

Part: SKIN — CHAFED (T/E FLAP) · airframe 9,981 hrs · 14,038 cycles

PDX - INBOARD FLAP HAS CHAFE DAMAGE ON UPPER SURFACE AT THE PREVIOUS PATCH. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-26.

Part: DOUBLER — CHAFED (T/E FLAP) · airframe 9,981 hrs · 14,038 cycles

PDX - RIGHT HAND OUTBOARD FLAP REPAIR PATCH ON TOP SIDE AT INBOARD END IS CHAFED FROM CONTACTING UNDERSIDE OF WING TRAILING EDGE. REPAIRED IAW RD 8-57-122 AND DHC-8 SRM 51-20-26.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - RIGHT HAND FUSELAGE SKIN IS CREASED AT X446-X450, Z107.0. REPAIRED IAW HORIZON AIR EA 2-53-407.

Part: SKIN — DENTED (NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - DENT IN NACELLE SKIN, INBOARD SIDE OF NACELLE, AT APPROXIMATELY STATION XN121.2, ZN20.25, JUST FORWARD OF DRAIN MAST. REPAIRED IAW HORIZON AIR EA 2-54-146.

Part: SUPPORT — CHAFED (LT NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - LT NACELLE UPPER INBOARD ENGINE SUPPORT TUBE IS CHAFED WHERE WIRE BUNDLE IS IN CONTACT APPROXIMATELY 12 INCHES FROM AT END OF TUBE. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - FLOORBEAM SEAT TRACK NR 7 ATTACH HOLE OVERSIZED AT APPROXIMATELY 405.737 AND YR9.25. REPAIRED IAW HORIZON AIR EA 2-53-405, FIGURE 4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 9,981 hrs · 14,038 cycles

PDX- PITTING CORROSION ON RIGHT HAND INBOARD SEAT TRACK NUMBER 7 AT STATION 182-222. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11, RD 8-53-1339 AND RD 8-53-1102.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - FLOORBEAM SEAT TRACK NR 7 ATTACH HOLE IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2-53-405.

Part: SUPPORT — CHAFED (LT NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - LT NACELLE LOWER INBOARD ENGINE SUPPORT TUBE IS CHAFED APPROXIMATELY 22 INCHES FROM FORWARD END. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LT OUTBOARD SEAT TRACK X546 HAS TWO GOUGES IN CHANNEL AND SEVERAL ON TOP FLANGE. REPAIRED IAW DHC-8-202 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK AT X484 HAS NICKS IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK X317 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK X375 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 12 AT STATION 540. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT PITS IN TOP FLANGE X520. REPAIRED IAW DHC-8-202 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK X391.45 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK AT X438 HAS LIGHT CORROSION IN THE CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 515. REPAIRED IAW RD 8-53-3644 DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK X504 HAS NICKS IN TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 12 AT STATION 528. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CHANNEL AT X424. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK LIGHT CORROSION FROM X332 TO X334. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION PITS IN ITS CHANNEL AT X467. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHTNING STRIKE BURN EXIT MARK, LEFT HAND LOWER FUSELAGE AT STATION X361.0, Z-84. REPAIRED IAW HORIZON AIR EA 2-53-408.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND INBOARD SEAT TRACK X438.5 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW RD 8-53-4472, RD 8-53-4473, RD 8-53-1102 AND DHC-8 SRM 51-40-11.

Part: SUPPORT — CHAFED (RT WING) · airframe 9,981 hrs · 14,038 cycles

PDX - RT WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING FLAP WHILE IN UP POSITION, AT YW174. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-57-1549, PAGE 3, STEPS 1, 3, AND 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - PITTING CORROSION ON RIGHT OUTBOARD SEAT TRACK AT STATION 309-312. REPAIRED IAW DHC-8-200 SRM 51-40-11.

Part: SUPPORT — CHAFED (LT WING) · airframe 9,981 hrs · 14,038 cycles

PDX- LEFT HAND WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING OUTBOARD FLAP WHILE IN THE UP POSITION. REPAIRED IAW DHC-8 RD 8-57-1549.

Part: SHIM — OUT OF POSITION (RT NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - SHIM OUT OF POSITION AT FORWARD END OF CHANNEL, LOCATED AT OUTBOARD SIDE OF RIGHT MAIN WHEEL WELL ZN15.00 AND XN170.60, IN RIGHT NACELLE. REPAIRED IAW HORIZON AIR EA 2-564-144.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - PITTING CORROSION ON RIGHT HAND INBOARD SEAT TRACK NR 8 AT STATION 500. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - RIGHT SIDE FRAME 4 STRINGER 3, STRAIGHT UP LOOKING THROUGH PANEL 311AB HAS APPROXIMATELY 1 INCH CRACK. REPAIRED IAW RD 8-55-199.

Part: FRAME — CRACKED (HORIZ STAB) · airframe 9,981 hrs · 14,038 cycles

PDX - LEFT HAND SIDE FRAME 4 STRINGER 3, LOOK UP FROM PANEL 331AB OVER SUPPORT BRACKET, HAS .5 INCH CRACK. REPAIRED IAW RD 8-55-199.

Part: SPAR CAP — SCRATCHED (RT WING) · airframe 9,981 hrs · 14,038 cycles

PDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG AT YW225. REPAIRED IAW RD 8-57-1119.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LT INBOARD SEAT TRACK X230 TO X235 HAS CORROSION PITS IN RADIUS OF OUTBOARD FLANGE. REPAIRED IAW DHC-8-202 SRM 51-40-11 AND SRM 51-40-16.

Part: SPAR CAP — SCRATCHED (RT WING) · airframe 9,981 hrs · 14,038 cycles

PDX - RT WING FRONT SPAR BOTTOM CAP SCRATCHED BETWEEN YW207 AND YW279. REPAIRED IAW RD 8-57-1119.

Part: SPAR CAP — SCRATCHED (RT WING) · airframe 9,981 hrs · 14,038 cycles

PDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG OUTBOARD OF YW279. REPAIRED IAW RD 8-57-1119.

Part: CONTROL COLUMN — EXCESS PLAY (COCKPIT) · airframe 9,981 hrs · 14,038 cycles

PDX - COPILOT CONTROL COLUMN HAS .1875 INCH OF FREE PLAY FOR AND AFT RELATIVE TO CAPTAINS CONTROL COLUMN IN MIDDLE OF TRAVEL. REPAIRED IAW HORIZON AIR EA 2-27-61.

Part: SKIN — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX- FUSLEAGE SKIN BELOW UPPER TCAS ANTENNA HAS PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-16.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - CENTER FORWARD CARGO FLOOR AFT FLOOR FLANGE ANGLE BETWEEN LEFT AND RIGHT INBOARD SEAT RAILS AT X600.00 HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-20-36.

Part: SPAR — CHAFED (CENTER WING) · airframe 9,981 hrs · 14,038 cycles

PDX - CENTER, AFT WING SPAR FLANGE HAS CHAFING FROM LEFT HAND WING YW48.00 TO RIGHT WING YW48.00. REPAIRED IAW RD 8-57-1434.

Part: SKIN — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - THERE IS CORROSION ON FUSELAGE SKIN SURFACE UNDER LOWER TRANSPONDER ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 3 AND SRM 51-20-11.

Part: BOLT — FAILED (RT WING) · airframe 9,981 hrs · 14,038 cycles

PDX - RIGHT WING TO FUSELAGE ATTACHMENT BOLT FAILED ULTRA SONIC INSPECTION. REPLACED BOTH IAW HORIZON AIR EA 2-57-167.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 450. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 470. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 490. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 485. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.

Part: SKIN — CORRODED (NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-202 SRM 54-00-16, TABLE 1 ON PAGE 2.

Part: SKIN — CORRODED (NACELLE) · airframe 9,981 hrs · 14,038 cycles

PDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-200 SRM 51-00-26, TABLE 2 ON PAGE 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHT CORROSION ON RIGHT OUTBOARD SEAT TRACK (NR 11) AT STATION 438. REPAIRED IAW DHC-8-202 SRM 51-20-16 AND SRM 51-20-36.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHT CORROSION ON RIGHT HAND INBOARD SEAT TRACK NR 9 AT STATION 531. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.

Part: STRUT — CHAFED (RT ENGINE) · airframe 9,981 hrs · 14,038 cycles

PDX - LIGHT SURFACE CHAFING ON INBOARD SIDE OF LOWER RIGHT ENGINE STRUT, ON RIGHT NACELLE. REPAIRED IAW DHC-8 RD 8-54-036.

Part: PLATE — CORRODED (WING) · airframe 9,981 hrs · 14,038 cycles

PDX - LADDER PLATE FOR PANEL 622AT HAS FRETTING CORROSION AROUND ONE BOLT HOLE. REPAIRED IAW DHC-8-200 RD 8-57-1471.

Part: SKIN — CORRODED (FUSELAGE) · airframe 9,981 hrs · 14,038 cycles

PDX - MATING AREA FOR PANEL 144HZ HAS LIGHT CORROSION AROUND PERIMETER. REPAIRED IAW DHS-8-200 SRM 51-20-11, PAGE 7 AND CPC MANUAL CHAPTER 5, PAGE 5.

Part: DETECTOR — DEFECTIVE (CABIN) · airframe 9,305 hrs · 13,050 cycles

SEA-MASTER WARNING ILLUMINATED SEVERAL TIMES DURING FLIGHT. CREW MEMBERS IN CABIN CHECKED LAVATORY AND BAGGAGE AREA FOR SMOKE. NO SMOKE FOUND. MAINTENANCE REMOVED AND REPLACED #2 SMOKE DETECTOR IN BAGGAGE COMPARTMENT. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (LAVATORY) · airframe 8,121 hrs · 11,335 cycles

SEA - LAVATORY LIGHT IS INTERMITTENT WITH A SLIGHT SMELL OF BURNING ELECTRICAL WIRING. PULLED AND INSTALLED COLLAR ON CIRCUIT BREAKER TO LAVATORY LIGHT. REMOVED BULB FROM SOCKET ASSEMBLY, LOCKED AND PLACARDED LAVATORY DOOR. FOUND BROKEN PIN CONNECTOR. REPINNED THE CONNECTOR. OPERATIONAL CHECK IS GOOD. NO SMELL OF BURNING. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 7,643 hrs · 10,610 cycles

EAT - CREW REPROTED STRONG ELECTRICAL SMELL EMINATING FROM THE LAV. REMOVED AND LAMP. STOWED ELECTRICAL CABLES. PLACED ON DEFERED MAINTENANCE LIST. AIRCRAFT RETURNED TO SERVICE.

Part: BRUSH BLOCK — MALFUNCTIONED (PROPELLER) · airframe 6,334 hrs · 8,741 cycles

PDX- EMERGENCY LIGHTS IN CABIN FLASH ON AND OFF DURING FLIGHT. RIGHT STALL WARNING CAUTION LIGHT ILLUMINATED REPEATEDLY DURING FLIGHT. REMOVED AND REPLACED NR 2 BRUSH BLOCK AND CURRENT LIMITER 2421-F10. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (MAIN CABIN) · airframe 5,948 hrs · 8,211 cycles

PDX- FLIGHT ATTENDANT HAS DIFFICULTY OPENING MAIN CABIN DOOR TO DE-PLANE. INSPECTED MAIN CABIN DOOR OVERCENTER FORCE. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LOOP — MALFUNCTIONED (NR 1 ENGINE) · airframe 5,295 hrs · 7,301 cycles

SEA- FAULT B LIGHT ON NR 1 ENGINE ILLUMINATED. REMOVED AND REPLACED LOOP B COMPRESSOR CASE LOOP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 4,995 hrs · 6,893 cycles

PDX- RIGHT HAND WING NR 1 FLAP TRACK TOP SURFACE OF THE LOWER RAIL HAS SURFACE CORROSION. REPAIRED IAW RD 8-57-985.

Part: SKIN — DAMAGED (TE FLAP) · airframe 4,995 hrs · 6,893 cycles

PDX- SPAN WISE CHAFE DAMAGE ON UPPER SURFACE OF LEFT HAND OUTBOARD FLAP FROM STATION YW 174.00 TO YW 252.00. REPAIRED IAW RD 8-57-1022 AND RD 8-57-1241.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 4,995 hrs · 6,893 cycles

PDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1167.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,995 hrs · 6,893 cycles

PDX- AFT RIGHT HAND INBOARD SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW DASH 8 SRM 51-40-11 AND SRM 51-40-00.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 4,995 hrs · 6,893 cycles

PDX- LEFT HAND FLAP HAS CHIPPED PAINT AND DELAMINATION ON LOWER SURFACE NEAR TRAILING EDGE AT STATION YW 100.00. REPAIRED IAW RD 8-57-1696.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 4,995 hrs · 6,893 cycles

PDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1168.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,995 hrs · 6,893 cycles

PDX- EMERGENCY LIGHTS WILL NOT TURN ON FROM FLIGHT ATTENDANTS PANEL. REPAIRED IAW DASH 8 SRM 33-51-01.

Part: SKIN — DAMAGED (TE FLAP) · airframe 4,995 hrs · 6,893 cycles

PDX- SPAN WISE CHAFE DAMAGE ON UPPER SURFACE OF LEFT HAND INBOARD FLAP. REPAIRED IAW RD 8-57-1022 AND RD 8-57-1241.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,995 hrs · 6,893 cycles

PDX- RIGHT HAND INBOARD SEAT TRACK AT END POSITION IS CORRODED BEYOND LIMITS. REPAIRED IAW DASH 8 SRM 51-40-11 AND SRM 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,995 hrs · 6,893 cycles

PDX- LEFT HAND END SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW DASH 8 SRM 51-40-11 AND SRM 51-40-00.

Part: SKIN — DAMAGED (TE FLAP) · airframe 4,995 hrs · 6,893 cycles

PDX- RIGHT HAND OUTBOARD FLAP TOP SKIN AT INBOARD END STATION YW176.00. REPAIRED IAW RD 8-57-1022.

Part: STOP — WORN (CARGO DOOR) · airframe 4,995 hrs · 6,893 cycles

PDX- BAGGAGE DOOR STOP FITTINGS ARE WORN AND FRETTED. REPAIRED IAW DASH 8 RD 8-53-104 ISSUE 3 AND DASH 8 MM 52-30-00, PAGE 509-510.

Part: SKIN — SCRATCHED (EMPANAGE) · airframe 4,995 hrs · 6,893 cycles

PDX- SCRATCH ON EMPENNAGE, LEFT HAND SIDE AT STATION 718.252 AT STRINGER 16P. REPAIRED IAW DASH 8 SRM 53-30-2A, PAGE 5, FIGURE 1.

Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 4,995 hrs · 6,893 cycles

PDX- DOUBLER ON FRAME AT AFT BAGGAGE DOOR SURROUND HAS 2 CHAFE MARKS, STATION X597.6, 2141.0. REPAIRED IAW DASH 8 SRM 51-20-11, PAGE 3, SECTION B, AND SRM 51-20-16, PAGE 4, SECTION C AND SRM 51-20-36, PAGE 6, SECTION F-J SRM 51-20-51.

Part: SMOKE — DETECTED (CABIN)

SEA - AFTER TAKEOFF NOTICED BREIF SMELL OF SMOKE, WENT AWAY QUICKLY AND SEEMED TO BE ASSOCIATED WITH BLEEDS TURNED ON. ALL ELSE NORMAL. GROUND RAN AIRCRAFT AT 80 PERCENT TORQUE FOR 10 MINUTES. CYCLED NR 1 AND NR 2 BLEED ON AND OFF. RAN DUCT FULL HOT AND COLD. NO SMOKE OR ODOR IN CABIN OR COCKPIT NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: RHEOSTAT — FAILED (LIGHTS)

LWS- NOTICED SMOKE COMING FROM AREA IN OVERHEAD PANEL WHERE HGS COMBINDER HINGE ATTACHES TO OVERHEAD. FOUND FLIGHT COMPARTMENT OVERHEAD RHEOSTAT HAS SMOKED. DISCONNECTED CANNON PLUG 3311-P5. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

PDX - LIGHT BULBS INOPERATIVE AT FLIGHT ATTENDANT'S EMERGENCY LIGHT SWITCH. RESEATED CONNECTOR FOR FLIGHT ATTENDANT'S EMERGENCY LIGHT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SMOKE DETECTOR — MALFUNCTION (CARGO COMPT)

PDX- ON APPROACH, MASTER WARNING LIGHT ILLUMINATED WITH SMOKE WARNING LIGHT (BAGGAGE COMPARTMENT) INTERMITTENTLY ILLUMINATED. MAINTENANCE REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS, OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — FAILED (CABIN)

EMERGENCY FLOOR LIGHT SECTION INOPERATIVE. REPAIRED CONNECTOR TO FLOOR LIGHTING. TESTED EMERGENCY ESCAPE PATH LIGHT SYSTEM. ALL LIGHTS CHECK GOOD. NO PARTS REPLACED.