N452QX

Part: PUMP — INOPERATIVE (#2 ENGINE) · airframe 16,083 hrs · 17,347 cycles

UNABLE TO MOVE #2 PROPELLER INTO FULL REVERSE POSITION USING FEATHERING PUMP DUE TO PROP 2 AUX PUMP BREAKER POPPING. REMOVED #2 FEATHERING PUMP IAW AMM 61-20-31-000-801. INSTALLED NEW #2 FEATHERING PUMP IAW AMM 61-20-31-400-801. OPS CHECK GOOD PROP MOVED TO FULL REVERSE AND BACK TO FEATHER WITH OUT CB POPPING.

Part: LAMP — NONE (ZONE 200) · airframe 15,871 hrs · 17,134 cycles

F/A EMERGENCY LIGHT SWITCH BULB BURNT OUT. REMOVED FROM SERVICE. RE-LAMPED F/A EMERGENCY LIGHT SWITCH AS REQUIRED. RETURNED TO SERVICE.

Part: HINGE PIN — MIGRATED (SERVICE DOOR) · airframe 15,625 hrs · 16,871 cycles

DURING PRE-DEPARTURE WALK AROUND, FOUND AFT SERVICE DOOR HANDLE FWD FLAP COVER AFT SPRING BROKEN. REMOVED FROM SERVICE. UPON FURTHER INSPECTION, SPRING WAS NOT BROKEN, FOUND FLAP DOOR HINGE PIN MIGRATED OUT OF POSITION. RE-SET HINGE PIN AND CHECKED FLAP DOOR FOR OPERATION AND PROPER CLEARANCE, CHECKS GOOD. A/C OK FOR CONTINUED SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (OIL PRESSURE) · airframe 15,401 hrs · 16,558 cycles

HIGH OIL PRESSURE DURING T/O 73 PSI MAX FOR ABOUT 2 SECONDS. ABORTED TAKEOFF. UNEVENTFUL. RETURNED TO GATE. REMOVED FROM SERVICE. FAST SYSTEM RECORDED NO EXCEEDANCE CMC RECORDED NO EXCEEDANCE. NO MAINTENANCE ACTION REQUIRED. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 15,285 hrs · 16,525 cycles

NORMAL/ON EMERGENCY LIGHT SWITH NEXT TO FWD FA SEAT INOP. REPLACED SWITCH.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 15,236 hrs · 16,477 cycles

EMERGENCY FLOOR LIGHTING @ ROW 2 IS COMING LOOSE. IT IS THE STRIP FROM THE EXIT TO THE MAIN CABIN ISLE. REMOVED FROM SERVICE. RE SECURED EMERGENCY FLOOR LIGHTING @ ROW 2. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LATCH — INOPERATIVE (STOWAGE DOOR) · airframe 14,694 hrs · 15,937 cycles

FA REPORTS FRONT STORAGE COMPARTMENT UNDER FA SEAT NOT LATCHING. REMOVED FROM SERVICE. REPLACED RH LATCH ON FWD FA SEAT EMERGENCY EQUIPMENT STOWAGE DOOR. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,536 hrs · 15,779 cycles

DURING OPS TEST, 4 EMERGENCY FLOOD LIGHTS IN THE AFT PAX CABIN AND 2 EXIT SIGNS (AFT CABIN) DID NOT ILLUMINATE. REMOVED AND REPLACED #3 EMERGENCY LIGHT POWER SUPPLY AND BATTERIES PER Q400 AMM 33-51-01-000-801, 33-51-01-400-801, 33-51-01-000-802, 33-51-01-400-802, OP TEST GOOD

Part: WIRE SPLICE — DAMAGED (ZONE 200) · airframe 14,410 hrs · 15,666 cycles

STBY PITOT HEAT CAUTION LIGHT ILLUMINATED DURING CRUISE. WHILE COMPLETING THE CHECKLIST IT EXTINGUISHED AGAIN. REMOVED FROM SERVICE. INSPECTED JUMPER WIRE 3410-4252E-16-2 AT IRPS TIMER MONITOR AND FOUND SPLICE 3410-E1 VERY DARK AND SHOWING SIGNS OF HEAT DAMAGE, REPLACED SPLICE PER Q400 WM 20-16-05, NO OTHER DEFECTS NOTED, OP TEST OF STBY PITOT HEAT GOOD PER AMM 30-30-00-710-801. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 14,327 hrs · 15,591 cycles

FA NOTIFIES PHOTOLUMIN STRIP IN FRONT OF ROW 2D IS COMING UP. REMOVED FROM SERVICE. RE SECURED EMERGENCY FLOOR PATH LIGHT IAW Q400 AMM 33-51-16-400-801. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUIDE — DAMAGED (HANDLE STOP) · airframe 14,185 hrs · 15,439 cycles

TOW TEAM REPORTS UNABLE TO OPEN MAIN CABIN DOOR DUE TO HANDLE BEING UNDER FLUSH. REMOVED FROM SERVICE. REPLACED STOP GUIDE. INSTALLATION SERVICEABLE PER Q400 MCN 6520839-01 ISSUE 2. OPS CHECK GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: STOP — DAMAGED (DOOR HANDLE) · airframe 14,161 hrs · 15,414 cycles

RAMP UNABLE TO OPEN MCD FROM OUTSIDE. OPENED DOOR FROM INSIDE. REMOVED FROM SERVICE. FOUND MCD EXTERNAL HANDLE BUMPER SPLIT, CAUSING EXTERNAL TO BE CAUSE FOUND. MCD EXTERNAL HANDLE BUMPER SPLIT, CAUSING EXTERNAL HANDLE TO BECOME RECESSED. REMOVED AND REPLACED EXTERNAL HANDLE BUMPER, REF Q400 AMM TASK 52-1-00-820-801, PAR 4D (3). OPERATIONAL TEST OF MCD GOOD IAW AMM TASK 52-11-00-710-802. NO OTHER DEFECTS NOTED, RETURNED TO SERVICE.

Part: STOP — MALFUNCTIONED (DOOR HANDLE) · airframe 14,156 hrs · 15,408 cycles

UPON ARRIVAL MAIN CABIN DOOR WOULDN'T OPEN. REMOVED FROM SERVICE. REPLACED BUMPER STOP FOR FWD PASSENGER DOOR HANDLE IAW Q400 AMM 52-11-11-000/400-801 & MCN NO. 6520839-01 ISSUE #2. DOOR HANDLE IS FLUSH WITH FUSELAGE SKIN. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUIDE STOP — DAMAGED (PAX DOOR) · airframe 14,070 hrs · 15,324 cycles

MAIN CABIN DOOR EXTERNAL HANDLE RELEASE BUTTON IS DIFFICULT TO PUSH. REMOVED FROM SERVICE. INSPECTION FOUND MCD HANDLE RUBBER BUMPER BROKEN. REF Q400 AMM 52-11-11-000/400-801 & Q400 MCN 6520839-01 ISSUE: 01, REMOVED BROKEN BUMPER & REPLACED WITH NEW. DOOR OPENS & CLOSES AS NORMAL. MCD HANDLE NO LONGER DIFFICULT TO OPEN. AIRCRAFT RETURNED TO SERVICE.

Part: BUMPER — CRACKED (PAX DOOR) · airframe 14,042 hrs · 15,296 cycles

MAIN CABIN DOOR HANDLE STOP GUIDE BUMPER STOP WAS CRACKED. REPLACED THE MCD HANDLE STOP GUIDE IAW T/C 6-52-0834.

Part: COMPUTER — MALFUNCTIONED (EGPWS) · airframe 13,822 hrs · 15,045 cycles

ON SHORT FINAL GOT "TO LOW FLAPS" WARNING TWICE ALL INDICATIONS WERE NORMAL. PERFORMED A GO AROUND, ON SECOND APPROACH GOT ANOTHER TO LOW FLAPS WARNING AS WE TOUCHED DOWN. ( EGPWS - WARNING SYSTEM ) REMOVED FROM SERVICE. INTERROGATED CDS AND DID NOT FIND ANY FAULTS, PERFORMED OP TEST OF EGPWS SYS PER Q400 AMM 34-42-00-710-802, OP TEST GOOD, SYSTEM SHOWS NO FAULTS, REMOVED AND REPLACED EGPWS COMPUTER PER AMM 34-42-01-000-801, 34-42-01-400-801 OP TEST GOOD, PLACARDS REMOVED, NO CB'S OUT, CLEAR MEL. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 13,786 hrs · 15,000 cycles

FLOOR COVERING AT ROW 2D IS PEALING UP AND CREATING A TRIPPING HAZARD. REMOVED FROM SERVICE. CLEANED AND DRIED FLOORING AND SECURED FLOORING. TRIPPING HAZARD GONE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GOVERNOR — INOPERATIVE (NR 1 PROP OVRSPD) · airframe 13,737 hrs · 14,948 cycles

#1 PROPELLER DOES NOT APPEAR FULLY FEATHERED AFTER SHUTDOWN. REMOVED FROM SERVICE. REMOVED AND REPLACED #1 PROP OSG IAW Q400 MM 61-20-26-000-801 AND 61-20-26-400-801. OPS CHECK GOOD. C/W PROP FEATHER CHECK IAW Q400 MM 71-00-00-868-819. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLADE — DAMAGED (NR 1 PROPELLER) · airframe 13,649 hrs · 14,851 cycles

SUSPECT #1 PROP #4 BLADE WAS SHOWED SIGNS OF SPARKING ON APPROACH. REMOVED FROM SERVICE. FOUND #4 BLADE OF #1 PROP HAD DAMAGED DEICE BOOT. R+R #4 BLADE. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 13,370 hrs · 14,527 cycles

ON TAKEOFF ROLL "AVIONICS" CAUTION LIGHT ILLUMINATED, ALSO PFD2 MON FAIL ED MESSAGE. ABORTED TAKEOFF RETURNED TO GATE. REMOVED FROM SERVICE. REMOVED & REPLACED #2 PFD IAW MTC 6316104. PERFORMED LLM RTS TEST IAW MTC 6316104. AIRCRAFT REMAINS CAT III QUALIFIED. COCKPIT PLACARD REMAINS CAT III. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 12,353 hrs · 13,308 cycles

FWD F/A EMERGENCY SWITCHLIGHT NOT ILLMINATING. REMOVED FROM SERVICE. RELAMPED FWD F/A EMERGENCY "NORMAL" SWITCH LIGHT. LAMP CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 12,344 hrs · 13,298 cycles

ESCAPE PATH LIGHTING STRIP IN FRONT OF SEAT 2D LOOSE. AIRCRAFT REMOVED FROM SERVICE. RESECURED STRIP. RETURNED TO SERVICE.

Part: PLUNGER — DIRTY (EXTENTION DOOR) · airframe 12,297 hrs · 13,241 cycles

LANDING ALT EXTENSION DOOR FLOOR DOES NOT FULLY OPEN. REMOVED FROM SERVICE. SUSPECT SPILL CONTAMINATION ON ALTERNATE SELECT VALVE ACTUATOR PLUNGER. CLEANED IAW Q400 AMM MCN 61225-01 ISSUE 1 ALT EXTENSIION DOOR OPERATES NORMAL RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — LOOSE (ROW 1) · airframe 11,983 hrs · 12,865 cycles

CREW REPORTS EMERGENCY LIGHT STRIP LOOSE BY MCD @ ROW 1. REMOVED FROM SERVICE. RESECURED EMERGENCY LIGHT STRIP AT ROW 1 AND SEALED WET FLOOR AS REQUIRED. NO FURTHER DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 11,914 hrs · 12,786 cycles

PHOTO ILLUMINESCENT STRIP IN FRONT OF SEAT 2D COMING UP. REMOVED FROM SERVICE. REPLACED DELAMINATED STRIP IN FRONT OF SEAT 2D USING DOUBLE-SIDED TAPE AS REQUIRED. RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FEATHER SYSTEM) · airframe 11,885 hrs · 12,751 cycles

#1 PROPELLER WILL NO UNFEATHER USING THE MAINTENANCE PANEL. AIRCRAFT DOWN FOR REPAIRS.

Part: SEAT TRACK — CORRODED (FRAME 10.5-102.5) · airframe 11,733 hrs · 12,576 cycles

SEAT RAIL 11 FROM FSX10.50-X102.50,Y9.250 IS CORRODED BEYOND LIMITS. SEAT RAIL 11 FROM FSX 10.50-X102.50,Y9.250 REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (FRAME 39) · airframe 11,733 hrs · 12,576 cycles

SEAT RAIL 10 FROM FSX-39.00-X10.50 IS CORRODED BEYOND LIMITS. SEAT RAIL 10 FROM FSX -39.00-X10.50 REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (BS 612-670) · airframe 11,733 hrs · 12,576 cycles

SEAT RAIL 15 FROM FSX612.00-X670.00, Y9.250 IS CORRODED. REPLACED SEAT RAIL 15 FROM FSX 612.00 -X670.00, Y9.250 IAW SRM 51-42-00, 51-40-00 AND 51-40-15.

Part: SPRING — BROKEN (LT MLG UPLOCK) · airframe 11,334 hrs · 12,120 cycles

AFTER SELECTING GEAR HANDLE UP WE RECIEVED AN ABNORMAL GEAR INDICATION. THE GEAR HANDLE REMAINED ILLUMINATED. WE ALSO HAD A L. DOOR AMBER LIGHT AS WELL AS A LEFT RED INDICATION FOR THE GEAR DOORS. FLIGHT ATTENDANTS REPORTED THE LEFT GEAR DOORS DID NOT FULLY RETRACT. OUR AIRSPEED REACHED A MAX AIRSPEED OF AROUND 205. WE COMPLED A ABNORMAL GEAR EXTENSION CHECKLIST. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED PSEU AND FOUND THE FOLLOWING FAULTS: LGUPLK UNRSNABL FAR AND LGDRLK UNRSNABL FAR. UPON INSP OF LH MLG FOUND RH EXTENSION SPRING BROKEN ON LH MLG UPLOCK ACTUATOR. REMOVED AND REPLACED RH EXTENSION SPRING ON LH MLG UPLOCK ACTUATOR IAW Q400 AMM 32-31-000/400-803. OPS CHECK GOOD. JACKED A/C IAW TC 6071001. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM IAW AMM 32-31-00-710-801 MULTIPLE TIMES. NO DEFECTS NOTED. LOWERED A/C IAW TC 6071001. A/C OK FOR SERVICE. PSEU FAULTS CLEARED AND DID NOT REPOST. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 10,066 hrs · 10,704 cycles

FORWARD FA EMERERGENCY LIGHT SWITCH GUARD BROKEN. REPLACED THE GUARD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 10,066 hrs · 10,704 cycles

AFT GALLEY AND AFT EGRESS EMERGENCY LIGHTS DO NOT COME ON DURING TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-00-820-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,907 hrs · 10,529 cycles

FA EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED THE LAMPS, OP CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,502 hrs · 9,077 cycles

BOTH EGRESS LIGHTS IN THE RIGHT SIDE, ONE AT EMERGENCY EXIT AND ONE AT AFT SERVICE DOOR ARE INOP. RELAMPED THE FORWARD LIGHT IAW AMM 33-51-11-00-801/400-801, AND THE AFT LIGHT REFLECTOR REPLACED. OPERATIONAL CHECKS GOOD.

Part: COVER — UNSECURE (EMERGENCY LIGHTS) · airframe 7,977 hrs · 8,525 cycles

EMERGENCY EXIT LIGHT COVER AT 2DE KEEPS FALLING OFF. SECURED THE COVER.

Part: CONTROLLER — MALFUNCTIONED (NR 1 PROPELLER) · airframe 7,842 hrs · 8,386 cycles

CLIMBING THROUGH 7000 FT, POWERPLANT MESSAGE ILLUMINATED ON ED. NOTICED LEFT FUEL INLET TEMPERATURE FLUCTUATING RAPIDLY AND DISPLAYED DASHED LINES. FUEL INLET TEMP RETURNED TO NORMAL AND THEN REPEATED FLUCTUATION AFTER ABOUT 3 MINUTES. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED THE NR 1 PEC IAW AMM TASK 61-20-36-000-801/400-800. ALL OPS AND FUNCTIONAL TESTED GOOD IAW MTC 6710006, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (NR 1JUNCTION BOX) · airframe 7,436 hrs · 7,969 cycles

ABORTED TAKEOFF BELOW 80 KIAS DUE TO POWERPLANT MESSAGE ON ENGINE DISPLAY. REMOVED AND REINSTALLED PROPELLER ELECTRONIC CONTROL UNIT IAW AMM 61-20-36-000-801 & 61-20-36-400-801. REMOVED & REPLACED POWER QUADRANT IAW AMM TASK 76-10-01-000-801, 76-10-01-400-801. INITIAL TROUBLESHOOTING FOUND POWERPLANT 198 MESSAGE NR 2 ENGINE. REMOVED & REPLACED 6100-3-K2 RELAY IN #1 JUNCTION BOX, DAUGHTER BOARD. IAW AMM 24-50-60-000-801, AMM 24-50-60-400-801. PERFORMED OPERATIONAL TEST OF AUTOFEATHER AMM 61-20-00-710-801, AMM 71-00-00-868-806 ENGINE POWER ASSURANCE CHECK, AMM 71-00-00-868-814 REVERSE MAXIMUM GOVERNING, AMM 71-00-00-868-816 NPT UNDERSPEED GOVERNING CHECK, AMM 71-00-00-868-817 FADEC TRIM FOR PLA, AMM 24-50-60-865, 24-50-60-710-020. PERFORMED TC 6710005 & 6710006. ALL CHECKS GOOD. RETURNED TO SERVICE.

Part: GROUNDING STRAP — DAMAGED (APU) · airframe 7,332 hrs · 7,858 cycles

TROUBLESHOOTING APU PROBLEM, FOUND POSSIBLE ARCHING AND HEAT DAMAGE ON THE EXTRUSION ON THE AIRFRAME SIDE WHERE THE MAIN GROUND STRAP FOR THE APU CONNECTS TO THE EXTRUSION. VERIFIED THAT THE HARDWARE CONNECTION WAS TIGHT. CLEANED THE MOUNTING POINTS AND PERFORMED A VISUAL INSPECTION WITH A 10X MAGNIFY GLASS. NO DEFECTS NOTES. C/W MTC RD8/4-55-1379/1 FOR TEMPORARY ALLOWANCE FOR CONTINUED SERVICE WITH BURN DAMAGE TO ISOLATOR MOUNT (APU AFT) GROUND STUD. EDDY CURRENT AND ELECTRICAL BONDING CHECKS ARE SATISFACTORY.

Part: STRIP — LOOSE (CABIN) · airframe 7,223 hrs · 7,736 cycles

FLOOR PATH LIGHT STRIP AT ROW 2 IN NOT SECURE TO THE FLOOR. RESECURED STRIP AS REQUIRED. RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (SMOKE DETECTOR) · airframe 7,144 hrs · 7,845 cycles

DURING AIRCRAFT MOVEMENT, THE SMOKE CAUTION ILLUMINATED AND THE AFT CARGO CAUTION LIGHT CAME ON. INSPECTION FOUND THE AFT CARGO COMPARTMENT FORWARD SMOKE DETECTOR TO HAVE THE FAULT LIGHT ILLUMINATED. CLEANED AND SEATED PINS TO THE DETECTOR AND REINSTALLED THE CONNECTOR IAW AMM 26-12-01-400-801. OPERATIONAL TESTS GOOD IAW AMM 26-12-06-710-801. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 7,147 hrs · 7,649 cycles

CLIMBING THROUGH 18,000 FEET, THE SMOKE WARNING LIGHT ILLUMINATED. PER THE CHECKLIST, DISCHARGED THE FIRE BOTTLE FOR THE AFT BAGGAGE COMPARTMENT. NO VISIBLE SIGN OF SMOKE IN THE FLIGHT DECK OR THE CABIN. RETURNED TO FIELD AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED AND REPLACED FWD SMOKE DETECTOR CONNECTOR AND PINS IAW SWPM. REMOVED & REPLACED AFT SMOKE DETECTOR IAW AMM TASKS 26-12-06-000-801/400-801. OPS TESTED GOOD. REMOVED & REPLACED CONTROL AMPLIFIER, IAW AMM TASKS 26-10-01-000-801/400-801. OPS TESTED GOOD. REPLACED BOTTLES AND CARTRIDGES. ALL OPS TESTED GOOD. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 7,142 hrs · 7,643 cycles

SMOKE MASTER WARNING AFTER STARTING NR 2 ENGINE ON GROUND. REPLACED THE AFT BAGGAGE COMPARTMENT FORWARD SMOKE DETECTOR IAW AMM 26-12-06. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE.

Part: WHEEL — WORN (MLG) · airframe 6,357 hrs · 6,789 cycles

ON LANDING ROLLOUT, INITIAL BRAKE APPLICATION SEEMED TO HAVE NO EFFECT. AFTER ABOUT 2-3 SECONDS THE BRAKES SUDDENLY ENGAGED AND ACFT LURCHED FROM SUDDEN DECELERATION. DURING TAXI, THE BRAKES SEEMED NORMAL. AT PARKING THE GROUND CREW NOTICED SMOKE FROM THE LT TIRES. AFTER 20 MINUTES SMOKE WAS STILL PRESENT BUT IN SMALLER QTY. EXCESSIVE BRAKING INSPECTION C/W. ALL 4 MAIN WHEEL/TIRE ASSY'S REPLACED. FUNCTIONAL CHECKS OF ANTISKID SYS AND MAIN BRAKE SYS C/W. NO FAULTS FOUND. ALL CHECKS GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 6,323 hrs · 6,755 cycles

EMERGENCY LIGHTING "NORMAL" LIGHT IS INOPERATIVE, REPLACED THE LAMP. OPERATIONAL CHECKS GOOD, RETURNED TO SERVICE.

Part: ENGINE — SURGES (UNKNOWN) · airframe 6,059 hrs · 6,466 cycles

DURING CLIMB OUT, WITH THE POWER LEVERS AT RATED DETENT AND MCL ON, THE ENGINES SURGED SLIGHTLY. IT IS UNCERTAIN WHICH ENGINE SURGED BUT IT WAS ENOUGH TO MAKE THE AIRPLANE YAW SLIGHTLY. DIVERTED, LANDING UNEVENTFUL. INTEROGATED CDS FOR ENGINE FAULTS AND FOUND FAULT CODE 1505 ON NR 1 AND NR 2 ENGINES. C/W MQAR DOWNLOAD IAW TASK CARD 4620EFBQ24-RDS, MQAR DOWNLOAD REVEALED A VERTICAL ACCELERATION AT TIME OF REPORTED EVENT WITH NO ENGINE PARAMETER CHANGES. C/W POWER ASSURANCE RUN ON NR 1 AND NR 2 ENGINES IAW MAINTENANCE NR 6710005, NO DEFECTS NOTED. REF'S LOG PAGES, 740740 AND 740741 FOR C/A OF NR 1 AND NR 2 ENGINE. FAULT CODES ON WO 203171 WHICH CONTAINS THE TC'S USED AND NR-00001 AND /R-00002 FOR DOWNLOADS SIGN-OFF. ACFT OK FOR SERVICE.

Part: GUARD — MISSING (SWITCH) · airframe 5,862 hrs · 6,272 cycles

F/A EMERGENCY LIGHT SWITCH GUARD IS MISSING. REPLACED SWITCH COVER IAW AMM 33-51-05-000/400-801. RETURNED TO SERVICE.

Part: CARGO TRACK — CORRODED (BS 751-781) · airframe 5,843 hrs · 6,251 cycles

LEFT INBD AFT CARGO TRACK IN AFT BAGGAGE COMPARTMENT, CARGO TRACK NR 9 HAS CORROSION AROUND FLOORBOARD SCREW HOLES AT FS 751 - 781 LBL Y 10. CORROSION BLENDED IAW SRM 51-21-00. NDT CARRIED OUT IAW RD 8/4-53-7377.

Part: SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 5,714 hrs · 6,116 cycles

AFT SERVICE DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBED THE DOOR SEAL AND SURROUND AREA. DOOR OPENS SMOOTHLY AND NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 5,613 hrs · 6,016 cycles

DURING OPS CHECK OF EMERGENCY LIGHT SYSTEM, AFT GALLEY LIGHTS WOULD ILLUMINATE, BUT ONLY STAY LIT FOR ABOUT 10 SECONDS. REPLACED THE LT AND RT NR 3 POWER SUPPLIES IAW AMM 33-51-01-000/400-801. CHECKS GOOD.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 5,394 hrs · 5,767 cycles

PLASTIC COVER FOR EMERGENCY EXIT LIGHT AT ROW 2 IS NOT SECURE. REINSTALLED EMERGENCY LIGHT COVER. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 5,394 hrs · 5,765 cycles

F/A EMERGENCY LIGHT SWITCH GREEN LAMP NOT ILLUMINATING, REPLACED THE LAMP. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 4,842 hrs · 5,191 cycles

FORWARD EMERGENCY LIGHT FAILED OPS CHECK IAW EMERGENCY CK-800. REPLACED THE LT AND RT EMERGENCY POWER SUPPLY BATTERIES IAW AMM TASKS 33-51-01-000/400-801. LIGHTS CHECK NORMAL.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 4,552 hrs · 4,875 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH "NORMAL" LIGHT INOPERATIVE, RELAMPED. CHECKS GOOD, RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (AFT SERVICE) · airframe 3,613 hrs · 3,889 cycles

AFT SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED THE AFT SERVICE DOOR IAW AMM TASK 12-20-01-640-811. OPS CHECKED GOOD IAW 52-41-00-710-801. PERFORMED GVI. NO OBVIOUS DEFECTS NOTED. RETURNED TO SERVICE.

Part: PIN — BACKED OUT (DOOR HINGE) · airframe 2,178 hrs · 2,329 cycles

AFTER MCD WAS CLOSED FOR DEPARTURE THE RAMP PERSONNEL FOUND THE DOOR THAT COVERS THE HOLE FOR THE MCD ASSIST WAS NOT FLUSH AND ASKEW. UPON CLOSER EXAMINATION THE PIN THAT GOES THROUGH THE HINGE FOR THE DOOR HAS PARTIALLY BACKED OUT OF POSITION. FERRIED ACFT FOR REPAIRS. REINSTALLED HINGE PIN IN AFT HINGE POINT OF MCD DOOR ASSIST COVER. STAKED ENDS OF HINGE REF MM TASK 20-10-30-400-801 FOR STAKING OF HINGES. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 1,178 hrs · 1,270 cycles

WHILE ATTEMPTING OPS TEST OF THE AUTOFEATHER AND UPTRIM SYS AMM 61-20-00-710-801. RECEIVED A "AF TEST ABORT" MESSAGE. FOUND FAULT CODES 30 AND 366 AND 794. REPLACED THE NR 1 PECU. CHECKS GOOD. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOFEATHER SYS) · airframe 1,176 hrs · 1,267 cycles

WHILE DOING DAILY SYS CHECKS, RECEIVED TWO ABORT MESSAGES WHILE TESTING AUTOFEATHER. CLEARED FAULT CODES FROM NR 1 ENGINE 30A-794A AND 366B. C/W FIM TASK 73-20-00-810-850. OPS CHECKED GOOD. COULD NOT DUPLICATE. DEFERRED DOWNLOAD OF EMU DATA.

Part: LIGHT — UNSECURE (CABIN) · airframe 466 hrs · 474 cycles

F/A REPORTS STRIP LIGHTING LOOSE. ADHARED EMERERGENCY LIGHTING STRIP TO FLOOR. NO FURTHER DEFECTS NOTED.

Part: DOOR — MALFUNCTIONED (COCKPIT) · airframe 157 hrs · 148 cycles

COCKPIT DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE, ONCE LATCHED. REPLACED COCKPIT DOOR IAW AMM TASKS 52-51-00-000-801 & 52-51-00-400-801. OPS TESTED GOOD. DOOR OPENS NORMALLY FROM OUTSIDE & INSIDE. RETURNED TO SERVICE.