N437QX

Part: NONE — NONE (ZONE 600) · airframe 27,092 hrs · 29,126 cycles

"DEICE PRESS" CAUTION ILLUMINATED IN CRUISE 62% TORQUE. LEFT MOST INBOARD BOOT LIGHT AND SECOND BOOT THE THE RIGHT MOST INBOARD LIGHT REMAINED ILLUMINATED RAN DEICE PRESS CHECKLIST WITH NO RESULT LIGHTS REMAINED ILLUMINATED UNTIL SHUTDOWN. RETURNED TO FIELD. REMOVED FROM SERVICE. REF Q400 FIM TASK 30-10-00-810-801, PERFORMED ITEM 3 FUNCTIONAL TEST FAILED. FOUND FAULT LOW PRESSURE 4B FAIL IN CDS. REMOVED AND REPLACED #4 DDV (RH INBD DDV) IAW Q400 AMM TASK # 30-11-16-000-801/400/801, OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (ZONE 600) · airframe 27,000 hrs · 29,029 cycles

ON CLIMB THROUGH ABOUT 15000 ' DEICE PRESS CAUTION ILLUMINATED. RAN DEICE PRESS CAUTION CHECKLIST. DEICE PRESS CAUTION EXTINGUISHED, THEN RE-ILLUMINATED. FOUND RIGHT HAND ENGINE INTAKE BOOT NOT INFLATING. DEICE PRESSURE INDICATED BETWEEN 16-18 PSI FOR EVERY BOOT SEGMENT INFLATION. AIRCRAFT WAS OPERATING IN ICING CONDITIONS AT 15,000'. DIVERTED. REMOVED FROM SERVICE. GROUND RAN ENGINE. INTERROGATED CDS FOUND DEICE LOW PRESS. 4A FAIL.MSG., CLEARED CDS. R&R'D #4 DEICE DIST. VALVE IAW Q400 AMM TASKS 30-11-16-000-801/400-801. OPS CKS GOOD, FAULT CODE DID NOT RE-OCCUR. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — LEAKING (ZONE 700) · airframe 26,995 hrs · 29,022 cycles

DURING TIRE CHECK FOUND #3 BRAKE ON THE RIGHT INBOARD TIRE SMOKING. SOME HYDRAULIC LEAK OBSERVED. REMOVED FROM SERVICE. R&R #3 BRAKE ASSEMBLY ON THE RIGHT INBOARD TIRE IAW Q400 TASK CARD # 6324201. NO FURTHER DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 26,280 hrs · 28,303 cycles

UPON REACHING CRUISE @FL250 ENG #2 OIL PSI INDICATION OBSERVED AS WHITE DASHES. SECONDS LATER INDICATION RETURNED BUT SHOWED @ RED 0. IT FLICKERS BETWEEN WHITE DASHES AND ZERO. EVENTUALLY IT STAYED INDICATION W / FLUCTUATING VALUES. NO CAUTIONS/WARNINGS OR ANNUNCIATOR PANEL. RAN EMERGENCY AND ABNORMAL CHECKLIST 7.8 "LOW OIL PRESSURE" CHECKLIST, WHICH DROVE US TO COMMAND A SHUTDOWN DUE TO 0 PRESSURE CONSISTENTLY LESS THAN 44 PSI. OIL TEMPERATURE WAS NORMAL AT ALL PHASES OF FLIGHT. #2 ENGINE SHUTDOWN AND RETURNED TO THE FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED THE THE #2 ENGINE INSTRUMENT WIRING HARNESS AND THE #2 MAIN OIL PRESSURE TRANSDUCER. OPS CHECK GOOD. LEAK CHECK GOOD. RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (DIRECT DRIVE) · airframe 26,212 hrs · 28,234 cycles

ON CLIMB TO RNO WE GOT A DEICE PRESS CAUTION RAN CHECKLIST AND DID NOT RESOLVE ISSUE. DIVERTED. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND FAULT 4 B LOW PRESSURE. REMOVED AND REPLACED #4 DDV REF-400 AMM 30-11-16-000-801, 30-11-16-400801 REF AMM 57-23-01-000-801, 57-23-01-400-801 FOR REMOVAL AND RE INSTALLED LEADING EDGE PANEL #613AR CLEARED ALL FAULTS FROM CDS. C/W OPERATIONAL TEST OF THE PNEUMATIC DE-ICING SYSTEM REF. AMM TASK 30-11-00-710-804 INTERROGATED CDS AND FOUND NO FAULTS AT THIS TIME OPS CK. GOOD NO OTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (DIRECT DRIVE) · airframe 26,212 hrs · 28,234 cycles

DEICE PRESS CAUTION ILLUMINATED IN FLIGHT. RAN THE CHECKLIST AND FOUND THE RIGHT OUTBOARD BOOT FAILED TO INFLATE. RETURNED TO FIELD. REMOVED FROM SERVICE. CHECKED CDS & FOUND ICE PROTECTION FAULT "LOW PRESSURE 2A FAIL" INFLATED RIGHT OUTBOARD DEICE BOOTS & PERFORMED VISUAL & TACTILE INSPECTION. NO DEFECTS FOUND & BOOTS INDICATED NORMALLY. R&R #2 DDV FOR PRECAUTIONARY MEASURES IAW Q400 AMM TASKS 30-11-16-000-801 & 30-11-16-400-801 PER Q400 FIM TASK 30-10-00-810-804. CDS FAULTS CLEARED. OPERATED DEICE BOOTS IN AUTO & MANUAL MODE SEVERAL TIMES. ALL INDICATIONS NORMAL & NO CDS FAULTS RETURNED. AIRCRAFT RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,138 hrs · 28,158 cycles

LOSS OF PRESSURIZATION AT 16,000' MASTER CABIN PRESS. DID CABIN PRESS CHECKLIST, DROVE TO PRESSURIZATION FAIL CHECKLIST THEN DROVE ME TO MANUAL PRESSURIZATION CHECKLIST. THEN DUE TO BEING UNABLE TO CONTROL PRESSURE IN MANUAL DROVE ME TO UNPRESSURIZED FLIGHT CHECKLIST FLEW AT 10,000' TO ORIGINAL DESTINATION. REMOVED FROM SERVICE. C/W W/O 300899 REF N/R-00001, -00002, -00003 FOR ALL WORK PERFORMED. REPLACED CABIN PRESSURE CONTROLLER, AFT CARGO DOOR SEAL, AND AFT OUTFLOW VALVE. FUNCTIONAL CHECK OF PRESSURIZATION GOOD, PRESSURIZED A/C CHECKED GOOD. RETURNED TO SERVICE.

Part: GENERATOR — INOPERATIVE (NR 1) · airframe 25,763 hrs · 27,775 cycles

ON DEPARTURE #1 AC GEN CAUTION ILLUMINATED E&A CHECKLIST DID NOT RESOLVE FAULT. REMOVED FROM SERVICE. PERFORMED FIM TASK 24-20-00-810-801 AND AMM 05-53-00-210-819 NOTHING FOUND ON CHIP DETECTOR AND NO FAULT CODES FOUND. R+R A/C GEN. REF MTC 6242101 OPS CHECK GOOD CAUTION LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 25,599 hrs · 27,613 cycles

EMERGENCY LIGHTS REMAIN ILLUMINATED WITH EMERGENCY LIGHT SWITCH AND BATTERIES IN THE OFF POSITION. REMOVED THE LIGHT SWITCH ON THE WING BULKHEAD IAW AMM 33-51-05-000-801. INSTALLED NEW SWITCH IAW AMM Q400 33-51-05-400-801. EMERGENCY LIGHTS CHECK GOOD IAW Q400 AMM 33-51-00-710-803.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,512 hrs · 27,524 cycles

FA REPORTED ODOR IN CABIN SIMILAR TO IRONING SMELL.CABIN TEMP WAS SET TO F/A AT THE TIME. REMOVED FROM SERVICE. C/W MCN 62172-01 ISSUE 2 & FORM M-744 COMPLETED AND SENT. UPON ARRIVAL TO AIRCRAFT NO ODOR NOTED. CHECKED W/APU BLEED AIR & RECIRC FAN & GROUND RUN A/C WITH ONE ENGINE AT A TIME, ALTERNATING WITH BLEED 1 & 2 FOR TROUBLESHOOTING. NO ODOR OR SMELL NOTED AT DIFFERENT TEMPERATURE SELECTED FROM FLIGHT DECK OR FA PANEL. NO OTHER DEFECTS NOTED. GVI OF SEVERAL PSU'S, BALASTS AT DIFFERENT LOCATIONS, AT WHERE FA MENTIONED WHERE ODOR WAS COMING FROM, REF AMM TASK PSU: 25-28-00-000/400-801 MCN 625660-1 ISSUE 2. FOR INSPECTION OF BALLASTS. RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 24,607 hrs · 26,564 cycles

UPON SELECTING GEAR UP ON DEPARTURE, THE LEFT PLASTIC COVER OF THE LANDING GEAR HANDLE FELL OFF. FLIGHT OPERATED OK. REMOVED FROM SERVICE. REPLACED LANDING GEAR CONTROL PANEL IN REF WITH Q400 AMM TASK 32-31-01-000-801/32-31-01-400-801. MCN 6320826-01 ISSUE 02. C/W FUNCTIONAL TEST OF THE LANDING GEAR CONTROL PANEL. EVERYTHING PASSES EXCEPT 7(A)(5). WT ON WHEELS CAUTION LIGHT DOES NOT EXTINGUISH.SWAPPED OLD LANDING GEAR CONTROL PANEL WITH NEW LANDING GEAR PANEL AND GOT THE SAME RESULTS FOR THE FUNCTIONAL TEST. PERFORMED RIGGING OF ALL MLG WOW SENSORS AND CW FUNCTIONAL TEST OF LGCP. FUNCTIONAL TEST NORMAL. PLASTIC COVER ON LANDING GEAR HANDLE REMAINS IN PLACE. RETURNED TO SERVICE.

Part: BUMPER — DETERIORATED (PAX DOOR) · airframe 24,414 hrs · 26,368 cycles

RUBBER BUMPER IN MAIN CABIN DOOR OPENER IS DISINTEGRATED. REMOVED FROM SERVICE. REPLACED RUBBER BUMPER REF MCN 6520839-01 AND AMM 52-11-11-420-008 CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,218 hrs · 26,225 cycles

RAMP REPORTED EMERGENCY LIGHTS STAYED ON WHEN AIRCRAFT POWER IS OFF. REMOVED FROM SERVICE. REPLACED EMERGENCY BATTERY PACKS REF 33-51-00-820-801. CLEANED FWD FA EMERGENCY SW LT . OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. A/C GOOD FOR SERVICE. EMERGENCY LIGHT STAYS OFF WHEN A/C IS POWERED OFF.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 24,275 hrs · 26,222 cycles

CLIMBING THRU 10000 FT CREW CHECKED PRESSURE INDICATION CONTROL PANEL AND NOTED CABIN RATE INDICATED 500 FT DECENT W/DIFF OF 0 AND CABIN ALT 0. AT 15 K FT WE CALLED MX THINKING THE AFT OUTFLOW VALVE MIGHT BE STUCK CLOSED WITH THIS INDICATION OR GAUGES MIGHT BE BROKEN AND THEY SAID THERE WASN'T ANYTHING THEY COULD HELP WITH INFLIGHT. WE DESCENDED BACK TO 15K FT WITH PANEL INDICATING THE SAME AS IT DID IN CLIMB. WE THEN STARTED FEELING LIGHT HEADED, TINGLY FINGERED, AND POPPING EARS. FLIGHT ATTENDANTS ALSO REPORTED POPPING EARS. TO BE CONSERVATIVE WE DECIDED TO DIVERT TO PDX WHICH WAS RIGHT BELOW US. DESCENDING THRU 8OOO FT CAPTAIN AND FIRST OFFICER BOTH NEEDED SUPPLEMENTAL OXYGEN. NO CAUTIONS OR WARNINGS WERE TRIGGERED THROUGHOUT THE DURATION OF THE FLIGHT. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AS PER AMM TASK 21-31-06-000/400-801. PRESSURIZED AIRCRAFT AS PER TASK 21-00-00-863-801. NO DEFECTS NOTED. NO CPC FAULTS OR CDS FAULTS. BEFORE CHANGING CONTROLLER WE COULD NOT ACCESS CPC FAULTS ON CDS. CARGO COMPARTMENT BLOW OUT PANELS WERE VERIFIED "NOT BLOWN". AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE ASSY — INOPERATIVE (LT MLG) · airframe 23,522 hrs · 25,333 cycles

FELT BRAKES PULL LEFT TWICE ON LANDING. LEFT MAIN GEAR BRAKES SMOKING EXCESSIVELY DURING POST-FLIGHT. REMOVED FROM SERVICE. REMOVED #1 AND #2 WHEEL HUBCAPS. INTERROGATED CDS, FOUND NO ANTI SKID FAULTS. REPLACED #1 & #2 MLG WHEEL/TIRE ASSY AND BRAKES W/ SERVICEABLE PER Q400 MTC 6324201 AND 6324101. BLED ALL FOUR BRAKES PER Q400 AMM 32-44-00-870-801. TAXI'D AIRCRAFT AT VARIOUS SPEEDS AND APPLIED BRAKES. NO DEFECTS NOTED. NO LEAKS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,335 hrs · 25,121 cycles

BURNING ELECTRICAL SMELL NOTED IN THE FLIGHT DECK DURING FAILED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYSTEM (Q400 AMM TASK 30-11-00-720-801). C/W FUNCTIONAL TEST OF AIRFRAME PNEUMATIC DEICING SYSTEM IAW Q400 AMM TASK 30-11-00-720-801 WITH WARDROBE AND FLIGHT DECK DOOR REMOVED AND TECH SERVICES ON BOARD. FUNCTIONAL TEST PASSED AND NO UNUSUAL SMELLS NOTED. SUSPECT COMPRESSOR WASH CROSS CONTAMINATION TO BE THE MISTAKE SOURCE OF UNUSUAL SMELL. NFDN.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 BLEED SYS) · airframe 23,322 hrs · 25,106 cycles

ON TAKE OFF ROLL AT APPROX 55 KNOTS, NR 1 & 2 BLEED HOT CAUTION ILLUMINATED. ABORTED TAKE OFF WITH NO USE OF REVERSE. AND MINIMUM BRAKING. REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE HPSOV IAW AMM 3611-09-000-801/400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (ZONE 200) · airframe 23,213 hrs · 24,972 cycles

ELECTRICAL SMELL STARTED IN CRUISE VERY FAINTLY.DONNED OXYGEN MASKS AND RAN SMOKE CHECKLIST. BLEEDS WERE TURNED OFF SMELL GOT STRONGER DURING DESCENDED AND DISSIPATED AFTER OPENING THE DOOR. NO SMOKE IN THE FLIGHT DECK. FLIGHT ATTENDANT B ALSO SMELLED THE SMELL WAS LIKE A FAINT ELECTRICAL BURNING SMELL. REMOVED FROM SERVICE. INSPECTED AND FOUND RELAY 3000 K5 TERMINAL A2 AND WIRE 86B-08-2 BURNT TERMINAL. REMOVED AND REPLACED RELAY IAW 30-41-01-000-802/400-802 STEP 4A. REPLACED WIRE TERMINAL IAW EC 6-30-0150. C/W AMM 30-30-00 OPS CHECK OF PITOT STATIC ANTI ICING SYSTEM ALL CHECK GOOD NO ELECTRICAL SMELL/SMOKE/BURNT TERMINALS. RETURNED TO SERVICE.

Part: DOOR — MISSING (GROUND INTERCOM) · airframe 23,160 hrs · 24,916 cycles

GND CREW INTERCOM JACK DOOR IS MISSING- GRND INTRPHN COVER (113CL). PLACED ON CDL 868299. RETURNED TO SERVICE.

Part: AXLE — CORRODED (LT MLG) · airframe 23,150 hrs · 24,904 cycles

LEFT MAIN LANDING GEAR AXLE CORRODED BETWEEN INNER AND OUTER BEARING RACES, AND HAS A GOUGE IN SAME AREA. REPLACED AXLE IAW AMM 32-11-04-000-801.

Part: AXLE — CORRODED (RT MLG) · airframe 23,150 hrs · 24,404 cycles

RIGHT MAIN LANDING GEAR AXLE CORRODED BETWEEN INNER AND OUTER BEARING RACES OF BOTH WHEELS. REPLACED AXLE IAW AMM 32-11-04-000-801.

Part: BEAM — CRACKED · airframe 23,071 hrs · 24,816 cycles

SERVICE DOOR #2 BEAM CRACKED BETWEEN FASTENERS. REPLACED #2 BEAM ON AFT SERVICE DOOR WITH NEW PART PN 85217419-104 IAW SRM 51-20-00-00-01, 51-23-00-00-01, 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01 AND 51-42-45-02-01.

Part: FILTER — MALFUNCTIONED (NLG) · airframe 23,005 hrs · 24,735 cycles

NOSE GEAR TOOK EXCESSIVELY LONG TO RETRACT ON TAKEOFF. NOSE GEAR DOORS WERE OPEN AMBER LIGHT ILLUMINATED AND GEAR WAS NOT LOCKED RED LIGHT ILLUMINATED WITH GEAR HANDLE LIGHT ILLUMINATED. NOSE GEAR FULLY RETRACTED 20 SECONDS AFTER MAIN GEAR RETRACTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED THE INLINE FILTERS IN THE NOSE GEAR SEQUENCE VALVE. CHECKS GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 22,313 hrs · 23,929 cycles

EMERGENCY EXIT PATH STRIP LOOSE. REMOVED FROM SERVICE. SECURED LOOSE EMERGENCY EXIT PATH LIGHTING STRIP REF AMM 33-51-16-400-801. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,112 hrs · 23,697 cycles

LAST 2 AFT CEILING EMERGENCY LIGHTS AND AFT CENTER CEILING EXIT SIGN WOULD NOT ILLUMINATE DURING OPS CHECK OF EMERGENCY LIGHTS SYSTEM. REMOVED + REPLACED NR 3 EPSU BATTERY PACKS REF AMM TASK 33-51-00-820-801. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (FEATHER SYSTEM) · airframe 22,056 hrs · 23,632 cycles

NR 2 PROP FAILS TO UNFEATHER WITH FEATHER PUMP (PROP MTX UNFEATHER(S) INOP). REMOVED FROM SERVICE. PLACED ON MEL 61-20-1. NOTE: PROP FEATHERS AND UNFEATHERS NORMALLY WITH ENGINES RUNNING. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 21,271 hrs · 22,774 cycles

ONE PIECE OF THE FLOOR EMERGENCY LIGHT STRIP, JUST INSIDE MAIN CABIN DOOR WAS NOT SECURE. REMOVED FROM SERVICE. SECURED THE EMERGENCY LIGHT STRIP. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (AFT PAX DOOR) · airframe 21,154 hrs · 22,632 cycles

WHEN POWER WAS ADVANCED FOR TAKE OFF, A MASTER WARNING ILLUMINATED AND AFT, LEFT PAX DOOR INDICATED UNSAFE. REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT PAX DOOR LOCK SENSOR IAW WD 52-10-00 IAW AMM 52-71-01-400-802. NO DEFECTS NOTED AFTER AN OPS TEST. RETURNED TO SERVICE.

Part: DOOR — UNSECURE (AFT CARGO) · airframe 21,146 hrs · 22,621 cycles

FUSELAGE DOORS WARNING AFTER LIFTOFF. ACFT DID NOT PRESSURIZE. AIR TURN BACK. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND THE AFT CARGO DOOR HANDLE WAS NOT IN. PERFORMED AN OPS CHECK SEVERAL TIMES ON THE AFT CARGO DOOR IAW AMM 52-31-00-710-801. THE DOOR HANDLE REMAINS IN. NO OTHER DEFECTS NOTED. AND COMPLIED WITH HS 05-0029. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 20,748 hrs · 22,173 cycles

AFTER GEAR RETRACTION ON DEPARTURE, LEFT GREEN GEAR DOWN INDICATION REMAINED ILLUMINATED. DID APPROPRIATE E AND A CHECKLIST.ALSO VISUALLY CONFIRMED THAT GEAR WAS RETRACTED. ALSO VERIFIED WITH ALTERNATE GEAR DOWN LIGHTS ON FLOOR THAT ALL GEAR WERE RETRACTED. AFTER SWITCHING CAUTION / ADVISORY LIGHT SWITCH FROM DIM TO BRIGHT THE LEFT GREEN GEAR DOWN LIGHT EXTINGUISHED. WITH CAUTION / ADVISORY LIGHT SWITCH IN DIM, LEFT GEAR INDICATES DOWN, WITH SWITCH ON BRIGHT ALL GEAR SHOWED RETRACTED. ALSO DID ALTERNATE GEAR EXTENSION CHECKLIST. REPLACED ADVISORY CONTROL UNIT. FOLLOWING REPLACEMENT OF ACU, THE LH DOWNLOCK SENSOR WAS "CHEATED" TO SIMULATE UNLOCKED CONDITION AND CORRECT INDICATION WAS PRESENT IN DIM AND BRIGHT MODES. CHEATER REMOVED AND ALL INDICATIONS RETURNED TO DOWN AND LOCKED. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,553 hrs · 21,971 cycles

EMERGENCY LIGHTS ON THE CEILING PANEL 245EZ DID NOT COME ON DURING AN OPERATIONAL TEST. REPLACED THE BATTERY PACK.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 22,454 hrs · 24,104 cycles

ABORT TAKEOFF DUE TO AUTO FEATHER FAIL TO ARM. ABORT SPEED APROX 75 KNOTS. REMOVED FROM SERVICE. INFO ONLY. RESET AUTO FEATHER ARM IAW SPGRG 61-20-01. SYSTEM RESTORED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 19,923 hrs · 21,285 cycles

LEFT MAIN GEAR INDICATED GREEN, DOWN & LOCKED, AFTER GEAR RETRACTION. NO OTHER INDICATIONS, RAN CHECKLIST AND PERFORMED ALTERNATE GEAR EXTENSION, FA REPORTED GEAR APPEARED TO RETRACT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. OPS TESTED THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM IAW AMM 32-31-00-710-801. DISCREPANCY WAS DUPLICATED. REMOVED AND REPLACED THE LANDING GEAR CONTROL PANEL IAW AMM 32-31-01-000-801, AND 32-31-01-400-801, OPS TESTED GOOD. PERFORMED A LANDING GEAR PRIMARY EXTENSION AND RETRACTION IAW AMM 32-31-00-710-801, OPS TESTED GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (LT DOOR) · airframe 19,864 hrs · 21,225 cycles

DURING CLIMB OUT, THE AMBER DOOR LIGHT ILLUMINATED. PERFORMED THE E/A CHECKLIST AND IAW THE CHECKLIST ACCOMPLISHED THE ALTERNATE GEAR EXTENSION. GEAR EXTENDED OK. LANDING UNEVENTFUL. REMOVED FROM SERVICE. TESTED & WORK PERFORMED, ADJUSTMENT OF LGDRCL SENSOR. PERFORMED SEVERAL EXTENSION & RETRACTION CYCLES, NO DISCREPANCY, AMBER DOOR LIGHT EXTINGUSHED NORMALLY. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 19,491 hrs · 20,836 cycles

FUSELAGE DOOR WARNING ILLUMINATED AFTER TAKEOFF AT 2000FT, RAN THE CHECKLIST & RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED THE ACFT & FOUND AFT CARGO DOOR HANDLE EXTENDED. RESET DOOR HANDLE TO LOCKED. INSPECTED THE LATCH & FOUND TO BE SERVICEABLE, NO WEAR NOTED. PERFORMED AMM 05-0019 05-50-00, CARGO DOOR PASSED ALL PROCEDURE ITEMS. OPERATIONAL TEST OF THE AFT CARGO DOOR GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: TRU — MALFUNCTIONED (RT OTBD) · airframe 19,211 hrs · 20,541 cycles

UNUSUAL HUM AND VIBRATION HEARD FROM NOSE AND FELT IN FLOOR AND RUDDER PEDALS. NOISE STARTED WAITING TO PARK. THE NOISE BRIEFLY STOPPED WHEN PROPS WERE PUT IN START/FEATHER. THE NOISE CONTINUED ABOUT 20 SECONDS AFTER ENGINE SHUTDOWN AND THEN ABRUPTLY QUIT AGAIN. REMOVED FROM SERVICE. FOUND VIBRATION COMING FROM THE RIGHT TRU FAN. ABLE TO DUPLICATE BY CYCLING AC POWER ON/OFF TRU FAN RAN WITH AC POWER OFF. REMOVED RIGHT (OUTBOARD) TRU REF Q400 AMM TASK 24-31-21-000-801. INSTALLED RIGHT OTBD TRU IAW AMM 24-31-21-400-801. OPS TESTED GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CYLINDER — CORRODED (NLG) · airframe 19,119 hrs · 20,439 cycles

DURING SHOCK STRUT REPACK, FOUND DAMAGE & CORROSION TO LOWER BEARING AND INNER CYLINDER RETAINING SLOT. REPLACED INNER CYLINDER IAW CMM 32-21-04 CHAPTER 7. REMOVED AND REPLACED THE NLG SHOCK STRUT.

Part: LIGHT — LOOSE (CABIN) · airframe 18,471 hrs · 19,753 cycles

EMERGENCY LIGHT STRIP IN FRONT OF FORWARD CARGO DOOR PEELING OFF. SECURED, NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,410 hrs · 19,696 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH "NORMAL" POSITION INOP. RELAMPED. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE.

Part: GROUND WIRE — MELTED (BATTERY PACK) · airframe 18,336 hrs · 19,617 cycles

DURING INSTALLATION OF THE NR 1 EMERGENCY LIGHT BATTERY PACK GROUND WIRE INSULATION MELTED AFTER BREAKER RESET. REPLACED CONTAINER FOR EMERGENCY POWER SUPPLY.

Part: LENS — LOOSE (CABIN) · airframe 18,319 hrs · 19,602 cycles

EXIT LIGHT LENS AT SEAT 2E IS LOOSE. RE-ATTACHED LENS TO LIGHT WITH ADHESIVE.

Part: ROPE — EXPOSED (EMERGENCY EXIT) · airframe 18,319 hrs · 19,602 cycles

ROPE EXPOSED ON TYPE II/III EMERGENCY EXIT. OPENED TYPE II/III EMERGENCY EXIT. RE-POSITIONED ROPE. CLOSED TYPE II/III EMERGENCY EXIT DOOR. ROPE NO LONGER EXPOSED. NO PARTS REPLACED.

Part: PROBE — FAULTY (ICE DETECTION) · airframe 18,054 hrs · 19,317 cycles

ICE DETECT CAUTION LIGHT ILLUMINATED IN FLIGHT. DIVERTED, LANDING UNEVENTFUL. PLACED ON MEL. MEL CLEARED BY PERFORMED OPERATIONAL TEST OF THE ICE DETECTION SYSTEM. REF AMM TASK 30-80-00-710-801. NR 2 ICE DETECTOR PROBE INOP. NR 1 ICE DETECTOR PROBE OPERATES NORMALLY. THIS ACTION CLEARS MEL DEFECT 762503. NR 2 PLACED ON MEL. MEL CLEARED BY REMOVED AND REPLACED RT ICE DETECTOR PROBE IAW AMM 30-80-01-000-801/400-801. OPS TEST GOOD IAW 30-80-00-710-801. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 17,895 hrs · 19,158 cycles

AFTER TAKEOFF, AT 5000 FT MSL, HAD A DOORS WARNING AND LOSS OF PRESSURIZATION. THE DOORS PAGE SHOWED THE AFT CARGO DOOR IN RED. AFTER RETURN TO FIELD, GROUND CREWS SAID THE CARGO DOOR HANDLE WAS NOT FLUSHE, PERFORMED GVI OF LATCH AND OPS CHECK OF AFT BAGGAGE DOOR IAW MM 52-31, AND 05-52-00. NO FAULTS NOTED OK FOR CONTINUED SERVICE.

Part: FITTING — DENTED · airframe 17,164 hrs · 18,397 cycles

A DENT WAS FOUND AT THE FWD TOP AIRSTAIR DOOR SHELL MOUNT FITTING. ACCOMPLISHED REPAIR TO AIRSTAIR DOOR SHELL TOP FWD MOUNT FITTING IAW TASK CARD RD8/4-52-1534.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 17,164 hrs · 18,397 cycles

AFT BAGGAGE AFT SHEAR WEB PN 85339627 FROM FS 714 TO FS 783 BETWEEN LBL 10 AND LBL 36 CORRODED IN MULTIPLE LOCATIONS. SHEAR WEB REMOVED IAW SRM 51-42-05 SRM 51-40-15 AND SRM 51-42-45. NEW AFT BAGGAGE AFT SHEAR WEB PN 85339627-111 DRILLED AND TEMPLATED IAW SRM 51-40-07. NEW AFT BAGGAGE AFT SHEAR WEB PN 85339627-111 FROM FS 714 TO FS 783 BETWEEN LBL 10 AND LBL 36 INSTALLED IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-42-45.

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,164 hrs · 18,397 cycles

STIFFENER ANGLE FROM AFT BAGGAGE AFT SHEAR WEB TO VERTICAL WEB AT BS 783 LBL 0 TO LBL 40 CORRODED BEYOND LIMITS. STIFFENER ANGLE FROM AFT BAGGAGE AFT SHEAR WEB TO VERTICAL WEB AT BS 783 REMOVED IAW DASH-8-Q400 SRM 51-42-05. NEW STIFFENER ANGLE5 DRILLED USING TEMPLATE IAW SRM 51-40-07. NEW STIFFENER ANGLE INSTALLED AT BS 783 IAW SRM 51-42-05.

Part: BEAM — CORRODED (EMERGENCY EXIT) · airframe 17,164 hrs · 18,397 cycles

MINOR CORROSION ON EMERGENCY EXIT SILL BEAM. THRESHOLD REMOVED IAW SRM 51-42-05. A NEW THRESHOLD INSTALLED IAW SRM 51-42-05.

Part: DOUBLER — CORRODED (BS 728-783) · airframe 17,164 hrs · 18,397 cycles

AFT BAGGAGE AFT SHEAR THRESHOLD DOUBLER AT BS 728 TO 783 LBL 36 CORRODED BEYOND LIMITS. AFT BAGGAGE AFT SHEAR WEB THRESHOLD DOUBLER AT BS 728 TO 783 LBL 36. REMOVED IAW SRM 51-42-05. NEW THRESHOLD DOUBLER DRILLED IAW SRM 51-40-07. A NEW THRESHOLD SHEAR WEB DOUBLER INSTALLED IAW SRM 51-42-05.

Part: RAIL — CORRODED (ZONE 100) · airframe 17,164 hrs · 18,397 cycles

AFT LEFT OUTBD EQUIPMENT RAIL 25 CORRODED BEYOND LIMITS. THE EQUIPMENT RAIL WAS REMOVED AND REPLACED IAW SRM 51-42-05, SRM 51-42-45 AND INSTALLED IAW SRM 51-40-07.

Part: SHEAR WEB — CORRODED (BS 697-714) · airframe 17,164 hrs · 18,397 cycles

AFT BAGGAGE FWD SHEAR WEB PN 85339527 FROM FS X697 TO FS X714 BETWEEN LBL 10 AND LBL 36 CORRODED IN MULTIPLE LOCATIONS. AFT BAGGAGE FWD SHEAR WEB PN 85339527 FROM FSX 697 TO FSX 714 BETWEEN LBL 10 AND LBL 36 REMOVED IAW DASH-8-Q400 SRM 51-42-05 (RIVETS) SRM 51-42-45 (CHERRY MAX) AND SRM 51-40-15 (HI-LITES). AFT BAGGAGE FWD SHEAR WEB PN 85339527-107 DRILLED AND REAMED IAW DASH-8Q400 SRM 51-40-07. NEW AFT BAGGAGE FWD SHEAR WEB PN 85339527-107 INSTALLED IAW DASH-8-Q400 SRM 51-42-05 (RIVETS) 51-40-15 (HI-LITES) AND SRM 51-42-45 (CHERRY MAX).

Part: DOUBLER — CORRODED · airframe 17,164 hrs · 18,397 cycles

DRAIN MAST INTERNAL AND EXTERNAL DOUBLER AT X 19.400 BETWEEN STRINGERS 32-33R CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-05, AND 51-23-10.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,164 hrs · 18,397 cycles

SEAT TRACK NR 1 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15 AND 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,164 hrs · 18,397 cycles

SEAT RAIL 19 CORRODED BEYOND LIMITS. REMOVED IAW SRM 51-40-15 AND 51-42-05. DRILLED AND REAMED WITH TEMPLATE IAW SRM 51-40-07-02-01. SEAT RAIL 19, PN 85361561-104SP REINSTALLED IAW SRM 51-42-05-02-01, 51-42-90-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,164 hrs · 18,397 cycles

SEAT TRACK NR 15 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07, SRM 51-42-05-02-01 SRM 51-40-15-02-01 & 51-41-05-00-01.

Part: CHANNEL — CORRODED (FWD CARGO DOOR) · airframe 17,164 hrs · 18,397 cycles

FWD CARGO DOOR LOWER SILL PANEL AND CHANNEL CORRODED. THE SILL & CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15, 51-41-15, 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,164 hrs · 18,397 cycles

SEAT RAIL NR 8 CORRODED BEYOND LIMITS. LT INBD AFT CABIN SEAT RAIL NR 8 REMOVED IAW SRM 51-40-15, 51-42-05 AND 51-41-05. NEW LT INBD AFT CABIN SEAT RAIL DRILLED IAW SRM 51-40-07. NEW LT INBD AFT CABIN SEAT RAIL NR 8 INSTALLED IAW SRM 51-40-15, 51-42-05, AND 51-41-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,164 hrs · 18,397 cycles

FWD INBD SEAT TRACK 10 FROM X -34 TO X 10.50 RBL 10 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-42-05, AND 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,164 hrs · 18,397 cycles

SEAT RAIL NR 2 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK MID, OUTBD FROM FS X 228.5 TO FS X 571.50 LBL 40 IAW SRM 51-42-05, 51-42-45 AND 51-40-15. NEW LT MID CABIN OUTBD SEAT RAIL INSTALLED FROM FS X 228.5 TO FS X 571.50 LBL 40 IAW SRM 51-42-05, 51-42-45 AND 51-40-15.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,164 hrs · 18,397 cycles

SEAT TRACK 18 CORRODED BEYOND LIMITS FROM BS 102.50 TO 229.50 RBL 40. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, 51-42-45, AND SRM 51-40-07.

Part: DOUBLER — CORRODED (LAV SERVICE DOOR) · airframe 17,164 hrs · 18,397 cycles

INTERNAL DOUBLER ON LAV SERVICE DOOR STRUCTURE CORRODED IN LWR AFT CORNER. INTERNAL DOUBLER FOR LAV SERVICE STRUCTURE REMOVED IAW SRM 51-40-07 & 51-26-00-02-01. NEW LAV DOUBLER INSTALLED IAW SRM 51-42-05 & 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,164 hrs · 18,397 cycles

SEAT RAIL NR 11 IS CORRODED BEYOND LIMITS. SEAT RAIL NR 11 REMOVED IAW SRM 51-42-05, 51-40-15. NEW SEAT RAIL NR 11 INSTALLED IAW SRM 51-42-05, 51-40-15.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,907 hrs · 18,119 cycles

EMERGENCY LIGHT PUSH BUTTON ON FA BULKHEAD IS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 16,726 hrs · 17,925 cycles

ALL EMERGENCY LIGHTS ARE INOPERATIVE COMING FROM POWER SUPPLY NR 2. REPLACED THE POWER SUPPLY AND BATTERIES IAW AMM 33-51-01-000-801 & 33-51-01-400-801. CHECKED GOOD.

Part: GOVERNOR — MALFUNCTIONED (NR 2 OVERSPEED) · airframe 16,606 hrs · 17,789 cycles

AFTER ENGINE START, THE NR 2 ENGINE PROPELLER TOOK 70 SECONDS TO COME OUT OF FEATHER. REPLACED NR 2 OSG, REPAIRED OSG MOUNT PAD ON RGB, AND REPLACED THE O-RINGS IN NR 2 PROPELLER PISTON. OPS & LEAK CHECKED GOOD. OKAY FOR SERVICE.

Part: DISPLAY — OVERHEATED (ENGINE) · airframe 16,496 hrs · 17,663 cycles

ENGINE DISPLAY (ED) UNIT GOT EXTREMELY HOT. SHUT IT OFF WITH THE SWITCH NOT COOLING AFTER 20-25 MINS. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED DISPLAY UNIT, FILTER HOSES WERE TIGHT AND IN GOOD CONTION FILTER WAS INSTALLED CORRECTLY AND CLEAN. INSTALLED NEW DISPLAY UNIT AND NEW FILTER IAW TASKS 31-61-01-000-801, AND 31-61-01-400-801. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 16,420 hrs · 17,581 cycles

STANDBY INSTRUMENT FLICKERING IN CRUISE FLIGHT. RETURNED TO FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. REPLACED THE STANDBY INSTRUMENT. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 15,717 hrs · 16,819 cycles

MASTER WARNING FUSELAGE DOOR ON TAKEOFF. RAN CHECKLIST. PLANE WAS NOT PRESSURIZING. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND AFT CARGO DOOR HANDLE FOUND POPPED. VERIFIED CANTED BULKHEAD PANEL BLOWOUT WAS NOT BLOWN OUT. PERFORMED OPS TEST OF AFT BAG DOOR IAW 52-31-00-710-801. PERFORMED PRESSURIZATION CHECK IAW 21-00-00-863-801; 21-00-00-863-802.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 15,308 hrs · 16,362 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT AND RAPID DECREASE OF NR 1 OIL PRESSURE INDICATION. ENGINE SHUTDOWN. LANDING UNEVENTFUL. R & R NR 1 ENGINE. REPLACED NR 1 PROP HUB ASSY, BLADE ASSY REMOVAL AND RE-INSTALL. REPLACED ACOC. REPLACED ACOC LINES, REPLACED AC GENERATOR. REPLACED NR 1 PROP BETA TUBE. ALL OPS AND LEAK CHECKS GOOD. ABOVE COMPONENTS REPLACED DUE TO CHIP DETECTOR FINDINGS. RETURNED TO SERVICE.

Part: CAM FOLLOWER — SEIZED (PAX DOOR) · airframe 15,212 hrs · 16,254 cycles

RAMP CREW REPORTS THAT THEY ARE UNABLE TO OPEN THE REAR PASSENGER DOOR. CYCLED AFT PASSENGER DOOR. FOUND UPPER FWD CAM FOLLOWER SEIZED. REMOVED UPPER FWD CAM FOLLOWER IAW AMM TASK 52-12-11-000-801, STEPS 1 THRU 2 AND 4Y THRU 4Z. INSTALLED NEW UPPER FWD CAM FOLLOWER IAW AMM TASK 52-12-11-400-801, STEPS 1 THRU 3, AND 4AI THRU 4AJ AND 5C. MADE NO ADJUSTMENTS TO GUIDE ROLLER SUPPORT BRACKET OR SHIMS. OPS TESTS OF AFT PASSENGER DOOR GOOD IAW AMM ASK 52-12-00-710-802. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (LEFT) · airframe 14,198 hrs · 15,138 cycles

AFTER TAKEOFF, LT PROPELLER RPM INDICATED APPROXIMATELY 20 RPM LOWER THEN THE RIGHT. LT PROP, WHEN REDUCED TO 900 RPM ALSO SHOWED 20 RPM LESS THAN THE RT. WHEN RPM WAS BROUGHT BACK TO 850 RPM THE LT ENGINE RPM ENGINE RPM DROPPED TO 700 RPM. NR 1 PEC CAUTION ILLUMINATED. NR 1 PROP RPM SURGED SEVERAL TIMES AND SETTLED AT 1060 RPM. BECAUSE OF THE ENGINE CONTROLLABILITY CONCERNS, ELECTED TO SHUTDOWN NR 1 ENGINE. AUDIBLE PROP OUT OF PHASE NOISES WERE EVIDENT PRIOR TO SHUTDOWN. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS AND FOUND F/C 158A/B, 236B, 260A. C/W FIM TASK, 158, 61-20-04-810-812. C/W FIM TASK, 236/237, 61-20-05-810-822. C/W FIM TASK, 260, 61-20-06-810-818. NO DEFECTS NOTED, 7/23/15.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 14,101 hrs · 15,040 cycles

WXR RADAR NOT PAINTING, RETURNS WHEN THE WAS KNOWN WEATHER. TURNED OFF, WAITING 20 SECONDS IAW E/C. SAME PROBLEM, TURNED TO STBY AND "WX FAIL" ON MFD. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. R & R WXR TRANSCEIVER IAW MM TASK 34-41-01-000-801 + 34-41-01-400-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH) · airframe 678,458 hrs · 76 cycles

SHORTLY AFTER ROTATION THE LT PROPELLER RPM SETTLED AT 1000 RPM AT ACCEL HEIGHT, MOVED THE CONDITION LEVERS TO 900 RPM. THE LT PROPELLER SETTLED AT ABOUT 860 -+- 20 RPM AT 2500 FT, SET THE CONDITION LEVERS TO 850 RPM THE LT PROPELLER RPM FELL TO ABOUT 600 RPM AND THE LT ENGINE TORQUE INCREASED TO AROUND 106 PERCENT BEFORE WE COULD GET THE POWER LEVERS RETARDED. AT THAT POINT, HAD A NR 1 PEC CAUTION LIGHT AND A POWER PLANT MESSAGE ON ENGINE DISPLAY. COMPLIED THE PEC CAUTION CHECKLIST WHICH LEAD US TO THE ENGINE SHUTDOWN. RETURNED TO FIELD, LANDING UNEVENTFUL. PERFORMED GVI OF NR 1 ENGINE COMPARTMENT NO DEFECTS NOTED INTERROGATED CDS FOUND NR 1 CHANNEL, A-236 CHANNEL B-158, 260. R & R NR 1 PCU IAW AMM TASK 61-20-11-000-801 AND 61-20-11-400-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,081 hrs · 13,945 cycles

PASSENGER CABIN OVERHEAD EMERGENCY LIGHT AT ROW 6 DOES NOT ILLUMINATE WHEN SELECTED ON. REPLACED THE LAMP. CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: PRESSURE SWITCH — MALFUNCTIONED (SPOILERS) · airframe 12,963 hrs · 13,825 cycles

SPOILER OTBD CAUTION ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 235 KIAS. FOLLOWED CHECK LIST AND RETURNED TO FIELD WITH NORMAL LANDING. REPLACED OTBD ROLL SPOILER PRESSURE SWITCH. OPS TEST GOOD. OTBD SPOILER CAUTION LIGHT DID NOT RETURN.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 12,634 hrs · 13,470 cycles

HANDLE DIFFICULT TO LIFT AND OPERATE. CLEANED AND LUBRICATED, FORCE TO UNLOCK THE DOOR, WITHIN LIMITS, REF THE FOLLOWING AMM TASKS 52-11-00-720-802 AND 52-11-00-640-801 FOR WORK PERFORMED. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 12,179 hrs · 12,987 cycles

EMERGENCY DOOR WARNING AFTER TAKEOFF. EMERGENCY DOOR INDICATED UNSAFE. PRESSURIZATION WAS NORMAL. RETURNED TO FIELD. WARNING WENT OUT AFTER LANDING. INTERROGATED PSEU, NO PRESENT FAULTS. PERFORMED GVI OF FWD EMERGENCY EXIT DOOR IAW AMM TASK 52-23-00-210-801. CLEANED, PERFORMED OPS TEST OF FWD EMERGENCY DOOR IAW AMM TASK 52-22-00-710-803. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: ARM — CRACKED (PAX DOOR) · airframe 12,035 hrs · 12,841 cycles

MAIN CABIN DOOR WILL NOT CLOSE. FOUND UPPER HANDRAIL STRUT BENT. REPLACED. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITCH TRIM) · airframe 11,913 hrs · 12,712 cycles

ABORTED TAKEOFF DUE TO PITCH TRIM CAUTION AIRSPEED ABOVE 80 KTS. CAUTION MESSAGE DISAPPEARED AFTER APPROXIMATELY 6 SECONDS IAW MAINT REQUEST WE RAN PITCH TRIP UP AND DOWN. PITCH TRIM OPERATES NORMALLY. PERFORMED GENERAL VISUAL INSPECTION OF BRAKES & TIRES AFTER ABORTED TAKEOFF. NO DEFECTS NOTED. COMPLIED WITH FIM TASK 27-30-00-810-803 PITCH TRIM CAUTION IN CONJUNCTION WITH AMM TASK 27-32-00-710-802. OPS TESTED SATISFACTORY; PITCH TRIM CAUTION DID NOT REAPPEAR DURING TESTS. NO FAULTS LOGGED IN THE CDS AFTER TESTS PERFORMED. ACFT IS OK TO RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 11,721 hrs · 12,523 cycles

DURING DAILY SYS CHECK, AUTOFEATHER CHECK IS ABORTING TEST ON LT SIDE, SEVERAL ATTEMPTS. NO FAULTS IN CDS. OP'S CHECK OF THE PROPELLER AUTOFEATHER SYS IAW AMM TASK 61-20-00-710-801. OP'S CHECKED GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK 10 CORRODED. REMOVED RT FWD SEAT TRACK IAW SRM REF 51-42-05, 51-40-00. DRILLED AND PREPPED RT FWD SEAT TRACK IAW SRM REF 51-41-00 & 51-42-00. INSTALLED NEW SEAT TRACK, ON FWD RT SIDE IAW SRM REF 51-41-00 & 51-42-00.

Part: RIB — CORRODED (FUSELAGE) · airframe 11,634 hrs · 12,438 cycles

RIBS CORRODED AT 88.30 AND 64.20. LOCATED AND DRILLED TWO NEW RIBS IAW SRM 51-40-07, REPAIR 01. REMOVED REMOVED AND REPLACED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (NR 5) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK NR 5 CORRODED. REMOVED SEAT TRACK IAW SRM 51-42-05 AND 51-40-15. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07, REPAIR 01. INSTALLED SEAT TRACK IAW SRM 51-41-00 AND SRM 51-42-05, STEP 4D.

Part: SUPPORT — DAMAGED (LT NACELLE) · airframe 11,634 hrs · 12,438 cycles

FORWARD SUPPORT HAS SEPARATING METAL SEAL ON ENGINE FRAME SIDE. TRIMMED DAMAGED FRAME PLATE ON LT NACELLE FWD UPPER FRAME ASSY OTBD SIDE IAW SRM 54-10-01, STEP 7A (1). FABRICATED REPLACEMENT FRAME PLATE IAW SRM 54-10-01, STEP 7 A(3). FABRICATED REPAIR SPLICE/DOUBLER IAW SRM 54-10-01, STEP 7A-4. COMPLIED ALL STEPS A 2, 5-8 ON SRM 54-10-01, STEP 7.

Part: STRINGER — CORRODED (32 LEFT) · airframe 11,634 hrs · 12,438 cycles

SUSPECTED CORROSION ON STR 32L, FS 22.00. REMOVED SURFACE CORROSION FROM AREA AROUND P CLAMP BRACKET ON STR 32L NEAR FS -22 IAW SRM 51-21-00. REMOVED P-CLAMP FROM STR 32L NEAR FS-22 TO GAIN ACCESS TO CORRODED AREA FOR TREATMENT IAW SRM 51-41-00. INSTALLED P CLAMP, ADEL CLAMP TO STA 32L NEAR FS.22, REF WM 20-12-10, PG 209, STEP 4.E. RESTORED FINISH TO TREATED AREA ON STR 32L REF SRM 51-25-05, PG 207, STEP 5.F(1-4). C/W M-184 AS REQUIRED.

Part: GUSSET — CORRODED · airframe 11,634 hrs · 12,438 cycles

GUSSETS CORRODED. REMOVED AND REPLACED GUSSETS IAW SRM 51-42-05.

Part: SKIN — CORRODED (FUSELAGE) · airframe 11,634 hrs · 12,438 cycles

FWD PAX DOOR SURROUND, CORROSION FOUND ON SKIN. REMOVED CORROSION IAW SRM 51-21-00. RESTORED FINISH IAW SRM 51-21-10, 51-25-10.

Part: THRESHOLD — CORRODED · airframe 11,634 hrs · 12,438 cycles

EDGE BEAM THRESHOLD CORRODED. LOCATED FIT AND DRILLED EDGE BEAM, IAW SRM 51-40-07. REMOVED OLD EDGE BEAM IAW SRM 51-42-05 & SRM 51-41-00. INSTALLED EDGE BEAM IAW SRM 51-42-05.

Part: SKIN — CORRODED (BS 94) · airframe 11,634 hrs · 12,438 cycles

EVIDENCE OF SURFACE CORROSION AT FWD SIDE OF BS 94.8, APPROXIMATELY 2.5 INCHES UP THE FRAME FROM S24R. BLENDED CORROSION IAW SRM 51-21-00, PAGE 3, STEP 4. PERFORMED UT INSPECTION IAW NDTM 51-00-04. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK NR 10 CORRODED. REMOVED SEAT TRACK IAW SRM 57-40-15, 51-42-05 AND 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, STEP 4.D, 3-10, SRM 51-40-15, STEP 6H2 AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (NR 14) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK NR 14 CORRODED. LOCATED, DRILLED AND DEBURRED SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 & 51-40-15.

Part: RIB — CRACKED (NACELLE) · airframe 11,634 hrs · 12,438 cycles

AFT RIB ON UPPER COWL PANEL 424AL IS CRACKED. REMOVED CRACKED STIFFENER ON AFT RIB, UPPER COWLING REF DWG 85414014 & SRM 54-45-10. INSTALLED STIFFENER ON AFT RIB, UPPER COWLING PN 85414014-101 IAW SRM 54-45-10. NO DEFECTS NOTED. RECEIVED NEW STIFFENER PO TX836, PN 85414249-101 IAW DWG 85414014 & RIVETS COMMON TO PART. LOCATED & DRILLED HOLES ON STIFFENER, PN 85414249-101 IAW SRM 51-40-07. PREPPED & PRIMED SURFACE TO AFT RIB SECTION OF UPPER COWL PANEL 424AL AS REQUIRED IAW SRM 51-25-10. RESTORED FINISH TO RIVETED AREA OF PANEL 424AL REF SRM 51-25-05.

Part: SEAT TRACK — CORRODED (NR 6) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK NR 6 CORRODED. REMOVED SEAT TRACK IAW SRM 51-41-00 AND SRM 51-40-15, STEP 6M-N AND INSTALLED IAW SRM 51-41-00-00-01, SRM 51-40-20-02-01 AND SRM 51-42-05-02-01 STEP 4D, 2, 10.

Part: CHANNEL — CORRODED · airframe 11,634 hrs · 12,438 cycles

CHANNEL ASSY CORRODED. REMOVED CHANNEL IAW SRM 51-42-05. NEW CHANNEL INSTALLED IAW SRM 51-42-05.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 11,634 hrs · 12,438 cycles

EDGE CHANNEL IS CORRODED. LOCATED AND DRILLED NEW CHANNEL IAW SRM 51-40-07-02-01. FABRICATED AFT PASSENGER DOOR EDGE CHANNEL IAW DWG 85339542, AND SRM 51-24-35. PERFORMED ET INSPECTION ON FABRICATED EDGE CHANNEL IAW NDTM 51-00-06. NO DEFECTS NOTED.

Part: BEAM — CORRODED (THRESHOLD) · airframe 11,634 hrs · 12,438 cycles

EDGE BEAM UNDER THRESHOLD IS CORRODED. LOCATED AND DRILLED IAW SRM 51-40-07-02-01. INSTALLED, INNER, EDGE BEAM, IAW SRM 51-42-05, STEP 40.

Part: RIB — CORRODED (BS 676-683) · airframe 11,634 hrs · 12,438 cycles

FOUND THREE CORRODED RIBS AT AFT PASSENGER DOOR THRESHOLD BS 676 -683. REMOVED CORRODED RIBS IAW SRM 51-42-05, STEP 4E. FABRICATED BRACKETS. LOCATED AND DRILLED RIBS IAW SRM 51-40-07-02-01. INSTALLED RIBS IAW SRM 51-42-05, STEP 4D.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 11,634 hrs · 12,438 cycles

LOWER EMERGENCY EXIT DOOR CORRODED ON INTERNAL AND EXTERNAL STRUCTURE. BLENDED CORROSION IAW SRM 51-21-00. NO DEFECTS NOTED. FOUND WITHIN TOLERANCE IAW DWG 85227205. RESTORED FINISH IAW SRM 51-21-10-02-01 & 51-25-10-02-01.

Part: SEAT TRACK — CORRODED (NR 15) · airframe 11,634 hrs · 12,438 cycles

SEAT TRACK NR 15 CORRODED. REMOVED INBD SEAT TRACK SPLICE AT FS 612.00, RBL9.25 IAW SRM 51-42-05 4E 1-8 AND 51-40-15 6M 1-5. INSTALLED SEAT TRACK SPLICE IAW SRM 51-42-05, REPAIR-01 AND SRM 51-40-15 REPAIR-01.

Part: BRACKET — CORRODED (INTERCOSTAL) · airframe 11,634 hrs · 12,438 cycles

FWD PAX DOOR SURROUND, WEB TO INTERCOSTAL BRACKET FOUND CORRODED. REPLACED BRACKET IAW SRM 51-40-15, STEP 6H2 AND SRM 51-42-05, STEP 4D(3-10).

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 11,634 hrs · 12,438 cycles

FWD PAX DOOR SURROUND WEB TO SKIN ANGLE X26.7 AND X6.7 FOUND CORRODED. REMOVED ANGLES IAW SRM 51-42-05, STEP 4E. INSTALLED NEW ANGLES IAW SRM 51-42-05, STEP 4D.

Part: ANGLE — CRACKED (RT WING FAIRING) · airframe 11,634 hrs · 12,438 cycles

RIGHT NR 5 FLAP TRACK AFT INBD FAIRING ANGLE IS CRACKED. LOCATED AND DRILLED ANGLE IAW SRM 51-40-07. INSTALLED PLATE NUTS IAW SRM 51-42-75. INSTALLED ANGLE TO THE FLAP TRACK IAW SRM 57-50-50. NO DEFECTS NOTED IN AREA.

Part: GUARD — MISSING (LIGHT SWITCH) · airframe 11,250 hrs · 12,019 cycles

LIGHT SWITCH GUARD AT F/A'S POSITION EMERGENCY LIGHT SWITCH MISSING. INSTALLED NEW GUARD FOR FWD. F/A'S EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD, IAW AMM TASK 33-51-00-710-801. RETURNED TO SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 10,969 hrs · 11,717 cycles

EMERGENCY EXIT SIGN IN FRONT OF SEAT 2DE IS BROKEN. REMOVED SIGN IAW AMM TASK 33-24-00-000-802, PARA 4A, AND INSTALLED SIGN IAW AMM TASK 33-24-00-400-802, PARA 4C. CHECKED GOOD. OK FOR CONTINUED SERVICE.

Part: LIGHT — LOOSE (ROW 1 AB) · airframe 10,701 hrs · 11,443 cycles

EMERGENCY LIGHT STRIP AT ROW 1 A/B LOOSE. SECURED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 10,346 hrs · 11,067 cycles

EMERGENCY LIGHTING CAME LOOSE. SECURED LIGHT. RETURNED TO SERVICE.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 9,553 hrs · 10,214 cycles

F/A REPORTS ROW 2 EXIT SIGN DISCODGED. SECURED EXIT SIGN COVER AT ROW 2. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 9,431 hrs · 10,080 cycles

AFT FUSELAGE DOOR WARNING ILLUMINATED ON ROTATION. ACFT DID NOT PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. INSPECTED AFT CARGO DOOR UPON ARRIVAL, FOUND DOOR HANDLE POPPED OUT. PREFORMED OPS TEST OF DOOR IAW AMM TASK 52-31-00-710-801 AND SUPPLEMENT 52-0028. PRESSURIZED AND DEPRESSURIZED ACFT IAW AMM TASK 21-00-00-863-801 AND 21-00-00-863-802. NO DOOR OPEN INDICATION AND ACFT PRESSURIZED NORMALLY. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DISPLAY — FAILED (ENGINE) · airframe 8,911 hrs · 9,554 cycles

ENGINE DISPLAY FAILED. DIVERTED AND LANDING UNEVENTFUL. REPLACED ED IAW AMM 31-61-01-000-801 AND -400-801. OP CHECKS GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 8,512 hrs · 9,108 cycles

FLOOR PATH LIGHTING STRIP AT ROW 1B AISLE DETERIORATED. REPLACED STRIP.

Part: WARNING LIGHT — ILLUMINATED (PITOT HEAT) · airframe 8,429 hrs · 9,013 cycles

ON CLIMB, RECEIVED A PITOT HEAT STANDBY CAUTION. CIRCUIT BREAKER ON RT ESS L7 TRIPPED DURING ICING CONDITIONS. LOST NR 3 AIRSPEED INDICATION. INSPECTED WIRING TO STANDBY PITOT PROBE. NO DEFECTS NOTED. OPERATED PITOT HEAT ON GROUND. UNABLE TO DUPLICATE PROBLEM. R & R STBY PITOT PROBE AS A PRECAUTIONARY MEASURE IAW AMM 34-12-11-000-801 & 34-12-11-400-801. PROBE OPS CHECKED GOOD. STBY PITOT STATIC LEAK CHECKED GOOD IAW MX 6341102. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,685 hrs · 7,137 cycles

RT FORWARD EMERGENCY EXIT LOWER FORWARD EXIT LIGHT FOUND TO BE INOPERATIVE DURING THE 10 MINUTE FUNCTIONAL TEST. REPLACED THE NR 2 POWER SUPPLY UNIT IAW AMM 33-51-01-000-801. CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 6,520 hrs · 6,962 cycles

F/A REPORTED ODD ODOR DURING TAKEOFF. ODOR DISCIPATED SHORTLY AFTER TAKEOFF AND DID NOT RETURN. DEBRIEFED FLIGHT DECK AND CABIN CREW IAW AIR CONAMINATION CHECKLIST. REMOVED AFT GALLEY MAPCOS AND PERFORMED GVI OF ELECTRICAL SOCKETS AND WIRING W/NO DEFECTS NOTED. INSPECTED FWD CARGO FWD CARGO PIT AND RELATED ELECTRICAL WIRING/LIGHTING, NO DEFECTS NOTED. INSPECTED RECIRC FAN FILTER, WIRING CONNECTORS AND CIRCUIT BOARD, NO DEFECTS NOTED. INSPECTED ALL LIGHTING AND BALLAST IN CABIN, INSPECTED AFT CARGO BAY LIGHTING, INSPECTED LAVATORY LIGHTING AND SWITCHES, INSPECTED GALLEY LIGHTING, SWITCHES AND CONTROL PANEL, NO DEFECTS NOTED. INSPECTED APU GROUND STUD, SHUNT, WIRING AND TERMINALS IN AFT CARGO BAY, NO DEFECTS NOTED. INSPECTED A/C PSU PANELS ROW 14-20, NO DEFECTS NOTED. INSPECTED AREAS COVERED BY CEILING PANELS IN THE AFT GALLEY AND UNDER CENTER AISLE FLOOR PANELS FROM ROW 2-20, NO DEFECTS NOTED. GROUND RAN BOTH ENGINES AND OPERATED BLEEDS 1 AND 2 AT MAX. SHUTDOWN ENGINES. RAN APU AND C/W SL-21-012A, NO DEFECTS OR ABNORMAL SMELLS/ODERS NOTED. RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 6,430 hrs · 6,870 cycles

RIGHT BRAKE NOT WORKING WELL ON LANDING. REPLACED THE NR 3 AND NR 4 WHEEL SPEED TRANSDUCERS IAW AMM TASK 32-46-11-000-801 AND 32-46-11-400-801, TESTED GOOD. RETURNED TO SERVICE.

Part: BRAKE — MALFUNCTIONED (ZONE 700) · airframe 6,147 hrs · 6,579 cycles

AIRPLANE PULLS HARD RIGHT WITH TOE BRAKE APPLICATION BELOW 5 KNOTS GROUND SPEED. R & R BOTH NR 1 & NR 2 MLG BRAKE ASSY IAW T/C 6324201. ALSO R & R NR 1 MLG TIRE ASSY, IAW T/C 6324101. ACFT NOW TAXI'S STRAIGHT WHEN TOE BRAKES ARE APPLIED, OP'S CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: COFFEEMAKER — OVERHEATED (ZONE 200) · airframe 6,091 hrs · 6,515 cycles

DURING DESCENT, BOTH F/A'S REPORT AN ODOR OF "BURNING RUBBER". REPLACED MAPCOS, INSPECTED RECEPTACLES AND WIRING, NO DEFECTS NOTED. CLEANED RECEPTACLES. PERFORMED GVI OF RECIRC FAN, NO DEFECTS OR ODORS PRESENT. INSPECTED BAG COMPARTMENT LIGHTS, NO DEFECTS NOTED. INSPECTED BEHIND AFT GALLEY CONTROL PANEL, NO DEFECTS NOTED. PERFORMED GVI OF HEAT EXCHANGER, ACMS, AND ASSOCIATED PLUMBING, NO DEFECTS OR ODORS PRESENT. INSPECTED BEHIND WARDROBE INSERT AT RELAY PANEL, NO DEFECTS NOTED. PERFORMED PURGE PROCEDURE IAW DH8-400-SL-21-012A. NO DEFECTS OR ODORS NOTED. PERFORMED GVI OF ENGINES FOR FLUID LEAKS, NONE NOTED. INSPECTED UNDER FLOOR CABIN, NO DEFECTS OR ODORS NOTED. RETURNED TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

FWD WING TO BODY PANEL LAND AT FRONT SPAR Y= -42 TO Y=42 HAS SEVERAL AREAS OF FRETTING. BLENDED FRETTING AREAS IAW RD 8/4-53-451. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-451 AND RD 8/4-53-4378. COMPLIED WITH RD 8/4-53-451 AND RD 8/4-53-4378.

Part: FRAME — CORRODED (BS 216) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT STA 216, STR 31P -32P. REMOVED 4 RIVETS AND REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .045", CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, INSTALLED RIVETS AND PAINTED IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT STA 31P - 32P. REMOVED 3 RIVETS, BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .045" CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 5,841 hrs · 6,246 cycles

AFT WING TO BODY PANEL LAND AT REAR SPAR Y-42 TO Y 42 HAS SEVERAL AREAS OF FRETTING. BLENDED FRETTING DAMAGE IAW Q400 RD 8/4-53-451. CONFIRMED AREA CRACK FREE REF NTM 51-00-06-910-801. MIN REMAINING THICKNESS .084" REF NTM 51-00-04-910-801. PANEL LANDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-451.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

LEFT INBD SEAT TRACK 5 CORRODED ON CLAW AT STA 36. REMOVED CORROSION FROM SEAT TRACK IAW RD 8/4-53-844. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4365. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND RD 8/4-53-4365.

Part: SEAT TRACK — CORRODED (BS 664.5) · airframe 5,841 hrs · 6,246 cycles

RIGHT INBD SEAT TRACK CORRODING ON CLAW AT STA 664.5. REMOVED CORROSION FROM SEAT TRACK IAW RD 8/4-53-844. RESTORED ALODINE TO BLENDED AREAS IAW Q400 RD 8/4-53-4371 AND RD 8/4-53-884. BLENDS ARE WITHIN LIMITS IAW RD 8/4-53-4371 AND RD 8/4-53-884. APPLIED SELF LEVELING GREEN IAW RD 8/4-53-4371.

Part: FRAME — CORRODED (BS 301) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT BS 301, STR 33 - 31S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .042", CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, IAW RD 8/4-53-2344. TOP COATED AND APPLIED CPC IAW RD 8/4-53-2344. PAINTED EXTERIOR IAW SRM 51-25-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

RIGHT INBD SEAT TRACK 10 CORRODED ON CLAW AT STA -5.4. REMOVED CORROSION FROM SEAT TRACK IAW RD 8/4-53-2358. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4369. ALODINED AND APPLIED EPOXY IAW RD 8/4-53-4369. APPLIED SELF LEVELING GREEN IAW RD 8/4-53-4369.

Part: FRAME — CORRODED (BS 584.5) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT BS 584.5, S31P - 32S. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .055, CONFIRMED AREA IS CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, AND PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT BS 19.4, S33 - 32S. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .039, CONFIRMED AREA IS CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, AND PAINTED IAW RD 8/4-53-2344.

Part: SEAT TRACK — CORRODED (BS 664.5) · airframe 5,841 hrs · 6,246 cycles

RIGHT OTBD SEAT TRACK CORRODED AT BS 664.5. REMOVED CORROSION FROM SEAT TRACK IAW RD 8/4-53-844. BLENDED AREA FOUND TO BE WITHIN LIMITS PER RD 8/4-53-884. CONFIRMED AREAS CRACK FREE REF NTM 51-00-06-910-801. RESTORE SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND RD 8/4-53-884.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 5,841 hrs · 6,246 cycles

RIGHT INBD SEAT TRACK 11 CORRODED ON CLAW FROM BS 1.00 - 32.4. REMOVED CORROSION FROM SEAT TRACK IAW RD 8/4-53-2358. CONFIRMED CRACK FREE AREA REF NTM 51-00-06-910-801. FOUND TO BE WITHIN LIMITS PER RD 8/4-53-884. RESTORED SURFACE PROTECTION IAW RD 8/4-53-2358.

Part: FRAME — CORRODED (FUSELAGE) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT STA 1.00, STR 31P - 32P. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .048, CONFIRMED AREA IS CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, AND PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 529.5) · airframe 5,841 hrs · 6,246 cycles

CORROSION ON FRAME FLANGE AT BS 529.5, S31 - 32P. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .055, CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED, AND PAINTED IAW RD 8/4-53-2344.

Part: DOUBLER — CORRODED (ANTENNA MOUNT) · airframe 5,841 hrs · 6,246 cycles

T2 RADIO ALTIMETER ANTENNA MOUNT DOUBLER HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. ALODINED IAW SRM 51-21-10-02-01. CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT1 AND 51-00-06-910-801. BLENDS WITHIN LIMITS PER Q400 RD 8/4-53-4370. COMPLIED WITH RD 8/4-53-4370.

Part: DOUBLER — CORRODED (ANTENNA MOUNT) · airframe 5,841 hrs · 6,246 cycles

T1 RADIO ALTIMETER ANTENNA MOUNT DOUBLER HAS LIGHT CORROSION AROUND SCREW HOLES. REMOVED CORROSION IAW SRM 51-21-00-00-02. ALODINED IAW SRM 51-21-10-02-01. CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT1. BLENDS WITHIN LIMITS PER RD 8/4-53-4370. COMPLIED WITH RD 8/4-53-4370.

Part: DOUBLER — CORRODED (ANTENNA MOUNT) · airframe 5,841 hrs · 6,246 cycles

R2 RADIO ALTIMETER ANTENNA MOUNT DOUBLER HAS LIGHT CORROSION AROUND SCREW HOLES. REMOVED CORROSION IAW SRM 51-21-00-00-02. ALODINED IAW SRM 51-21-10-02-01. CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT1 AND 51-00-06-910-801. BLENDS WITHIN LIMITS PER Q400 RD 8/4-53-4370. COMPLIED WITH RD 8/4-53-4370.

Part: DOUBLER — CORRODED (ANTENNA MOUNT) · airframe 5,841 hrs · 6,246 cycles

R1 RADIO ALTIMETER ANTENNA MOUNT DOUBLER HAS LIGHT CORROSION AROUND SCREW HOLES. REMOVED CORROSION IAW SRM 51-21-00-00-02. ALODINED IAW SRM 51-21-10-02-01. CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT1. BLENDS WITHIN LIMITS PER Q400 RD 8/4-53-4370. COMPLIED WITH RD 8/4-53-4370.

Part: IGNITER — MALFUNCTIONED (APU ENGINE) · airframe 5,158 hrs · 5,538 cycles

APU AUTO SHUTDOWN OCCURED DURING START ATTEMPT - GROUND SERVICES ADVISED A LARGE AMOUNT OF SMOKE WAS SEEN FROM APU TAIL PIPE DURING THE START ATTEMPT. PLACED APU ON MEL 49-00-1. REPLACED APU IGNITOR PLUGS IAW MM TASK 49-40-04-000-801 AND 400-801. OPS CHECKED NORMAL IAW MM TASK 49-40-04-710-802 CLEARED DMI 549328 C/W H/S NR 49-0008 NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: RUDDER — FROZEN · airframe 5,122 hrs · 5,498 cycles

ON FINAL APPROACH AT 4000 FT. -5 DEG C IN ICING CONDITIONS FOUND RUDDER FROZEN IN PLACE. CREW TRIED TO MOVE RUDDER AND IT REQUIRED FORCEFUL PULL TO BREAK FREE. THEN NORMAL. LANDING UNEVENTFUL. RUDDER CABLE RUNS WERE INSPECTED, KICK PANELS AROUND RUDDER PEDALS INSPECTED, NO DEFECTS NOTED. OPERATED RUDDER SYS WITH BUNGEES DISCONNECTED, SYS OPERATED SMOOTHLY AND MADE FULL TRAVEL TO STOPS. BUNGEES RECONNECTED WITH REPLACEMENT OF RUDDER FEEL TRIM UNIT, TESTED GOOD. RETURNED TO SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 3,772 hrs · 4,120 cycles

BIRD STRIKE DAMAGE BETWEEN STA YW 510.229 AND YW 494.019. RT WING FWD SPAR, UPPER FLANGE HAS 32 DEGREE DOWNWARD DEFLECTION (APPROX .040") MAX DEFLECTION IS APPROX 3.0" OTBD FROM YW 494.019 DECREASING OTBD APROX 10.0" UPPER SKIN HAS IMPACT DAMAGE TO PAINT IN TOP COAT ONLY. L/E 613CR DAMAGED. C/W RD8/4-57-1558-1, FOR INSP, TEMP REPAIR, AND TEMP ALLOWANCE IAW SAIRD RD. PERMANENT REPAIR IS TRACKED BY ENGINERING THROUGH EC RD -57-1558/3. RETURNED TO SERVICE PENDING PERMANENT REPAIR.

Part: UNKNOWN — ODOR (CABIN) · airframe 3,349 hrs · 3,649 cycles

BOTH FLIGHT ATTENDANT'S AND PASSENGERS SITTING AT ROW 2DE SMELLED A BURNING ODOR FROM THE GASPER VENTS IN 2DE. F/A REPORTED THAT IT SMELLED LIKE A GRINDING METAL. GROUND RAN ACFT, HAD PACKS UP HOT, NO ODOR IN AC, NO OTHER DEFECTS NOTED. COULD NOT DUPLICATE PROBLEM. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 2,206 hrs · 2,437 cycles

MASTER WARNING CHECK FIRE DETECTED WITH APU BOTTLE LOW LIGHT. PERFORMED FIRE TEST OF APU, OPS TEST GOOD. APU FIRE PANEL BTL LOW NOT ILLUMINATED. OPS CHECK OF APU CHECKS GOOD NO DEFECTS NOTED. NO CURRENT FAULTS IN CDS. PERFORMED GVI OF APU AND APU FIRE BOTTLE NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FIRE BOTTLE — MALFUNCTIONED (APU BAY) · airframe 2,207 hrs · 2,438 cycles

MASTER CAUTION CHECK FIRE DETECT BOTTLE LOW APU INTERMITTENT ON APPROACH AND AFTER LANDING, EVENT MARKER PRESSED. R & R APU FIRE EXTINGUISHER BOTTLE IAW AMM TASKS 25-23-01-000-801/ 400-801. SYS TESTED GOOD. RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 1,976 hrs · 2,174 cycles

AFT OVERHEAD EMERGENCY EXIT, BOARDING LIGHT, READING LIGHT, FASTEN SEATBELT, NO SMOKING LIGHT, ALL INOP. INSPECTED AND FOUND CONNECTOR PLUG TO CEILING PANEL 245EZ DISCONNECTED, RECONNECTED, OPS CHECK RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — NOT SEATED (CARGO DOOR) · airframe 1,068 hrs · 1,223 cycles

AT APPROX 12000 MSL FWD CARGO DOOR WARNING LIGHT ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED VISUAL INSPECTION OF FWD BAG DOOR UPON ARRIVAL AT GATE FOUND EXTERIOR HANDLE NOT FULLY SEATED PERFORMED OPS TEST OF FWD BAG DOOR IAW AMM 52-32-00-710-801 DOOR AND DOOR WARNING SYS OPERATED NORMALLY OK FOR CONTINUED SERVICE. NO PARTS REPLACED.