N447QX

Part: NONE — NONE · airframe 23,188 hrs · 24,978 cycles

DURING DE-ICE PROP TEST AIRBORNE. LIGHTS FAILED TO CYCLE. DURING TEST POSITION LIGHT CYCLED. ATTEMPTED ON POSITION AGAIN NO LIGHTS. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED CALIBRATION PROCEDURE FOR THE TMCU, REF Q400 AMM TASK 30-61-06-820-801. CALIBRATION GOOD, NO FAULTS LOGGED IN CDS. DROPPED STATIC AIR TEMP TO BELOW 5*C, RAN ENGINE AT MIN, OPERATED HEAT AND BOTH PROP ADVISORY PROP ADVISORY LIGHTS CAME ON DURING OPERATION. SAW ADDITIONAL AC LOAD DETECTED WHEN BOTH PROP HEAT WAS ACTIVATED ON BOTH AC GENS. NO CAUTION LIGHTS ILLUMINATED DURING OPERATION. NO FAULTS LOGGED IN CDS. RETURNED TO SERVICE.

Part: SHEAR WEB — CORRODED (AFT CARGO) · airframe 22,934 hrs · 24,710 cycles

FWD SHEAR WEB IN AFT CARGO AREA CORRODED BEYOND LIMITS. FWD SHEAR WEB REMOVED IAW SRM 51-40-07-02-01. NEW FWD SHEAR WEB INSTALLED IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-42-45-02-01.

Part: SHEAR WEB — CORRODED (AFT CARGO) · airframe 22,934 hrs · 24,710 cycles

AFT BAGGAGE AFT SHEAR WEB CORRODED BEYOND LIMITS. AFT BAGGAGE AFT SHEAR WEB REMOVED IAW SRM 51-40-07-02-01. REPLACED AFT BAGGAGE AFT SHEAR WEB IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (BS 698-716 BL0) · airframe 22,934 hrs · 24,710 cycles

SEAT RAIL 23 FROM FS X 698 TO FS X 716 BL 0 IS CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 23 IAW SRM 51-42-05-02-01, 51-41-05-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,934 hrs · 24,710 cycles

SEAT RAIL 11 FROM FSX10.50-X102.5, Y9.250 IS CORRODED BEYOND LIMITS. SEAT RAIL 11 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-05-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,934 hrs · 24,710 cycles

SEAT RAIL 10 FROM FSX-39.00-X10.50, Y9.250 CORRODED BEYOND LIMITS. SEAT RAIL 10 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-05-00-01.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 22,934 hrs · 24,710 cycles

CABIN INTERIOR FORWARD LEFT WING BULKHEAD EMERGENCY EXIT SIGN LENS IS DISCOLORED. REPLACED.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 22,581 hrs · 24,371 cycles

ON CLIMB OUT OF KSEA APPROX. FL190 #2 HYD ISO VLV MASTER CAUTION, THEN #2 ENG HYD PUMP, THEN #2 RUD HYD MASTER CAUTIONS ILLUMINATED IN SEQUENCE. #2 HYD QTY INDICATED 10% #2 HYD PRESS INDICATED 0 PSI PERFORMED #2 ENG HYD PUMP CAUTION E&A CHECKLIST, THEN #2 HYD SYSTEM FAILURE LANDING CHECKLIST, THEN ALTERNATE GEAR EXTENSION. RETURNED TO FIELD, LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN PUMP & REPAIRED DAMAGED HYD LINE. OPS & LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — FAILED (NR 2) · airframe 22,576 hrs · 24,366 cycles

#2 HYDRAULIC SYSTEM FAILURE AFTER REACHING CRUISE ALTITUDE/ DECLARED EMERGENCY AND RETURNED TO FIELD. LANDING UNEVENTFUL. AIRCRAFT OUT OF SERVICE FOR REPAIRS.

Part: UNKNOWN — SPARKS (GALLEY) · airframe 22,545 hrs · 24,333 cycles

FLIGHT ATTENDANT SAW AND HEARD A FLASH AND SMALL POP SOUND ALSO SMELLED AN ACIDIC SMOKE SMELL. CB WAS STILL SET. REMOVED FROM SERVICE. C/W MCN 62172-01 ISSUE 02 & FORM M-744 COMPLETED AND SENT UPON ARRIVAL TO AIRCRAFT NO ODOR OR SMELL NOTED. INSPECTED AFT GALLEY, COFFEE WARMER SOCKETS TERMINALS, GALLEY LIGHTS, SWITCHES AND WIRING. NO DEFECTS FOUND. ASO INSPECTED CIRCUIT BREAKERS IN THE COCKPIT AND GALLEY. NO DEFECTS FOUND. INSPECTED COFFEE MAKERS FOR ANY ABNORMALITIES, NONE FOUND. CREW ALSO REPORTED THAT WAS NOTED ONLY WITH GROUND POWER OPERATING. ALL INSPECTIONS DONE IN SAME CONFIGURATION. NO DEFECTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — FAULTED (CABIN WARNING) · airframe 22,359 hrs · 24,141 cycles

FORWARD OVERHEAD EXIT, NO SMOKE, FASTEN BELTS, AND LAV LIGHTS NOT ILLUMINATING DURING NORMAL OPERATION OR DURING TEST. REMOVED FROM SERVICE. C/W Q400 FIM TASK 32-24-00-810-803. WIRING TESTS GOOD. REPLACED RELAY 3323-K1 DONE IAW Q400 AMM 20-30-16-960-801. NO HELP. REPLACED PAX WARNING PANEL IAW Q400 AMM 31-51-10-000-801/400-801. OPS TESTS GOOD. ALL LIGHTS ON PAX WARNING PANEL ILLUMINATE NORMALLY. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,306 hrs · 24,088 cycles

ON TAKEOFF ROLL #1 BLEED HOT CAUTION AND #2 BLEED HOT CAUTION ILLUMINATED. AIRCRAFT DIVERTED LANDING UNEVENTFUL. REMOVED FROM SERVICE. CDS FAULTS ARE PRESENT FLT L CHANNEL 1007-L NAPRSOV, 1006-L NAPRSOV, 3003 PACK FCV. PRESENT FAULTS R CHANNEL 1203-R P2.2 SOV, 3003 PACK FCV, 1901-R PRCLR TEMP SWITCH. CLEARED FAULTS. GRD RAN APU AND OPERATED PACKS, CHECKED FOR OBVIOUS LEAKS IN PACK AREA, NONE NOTED. FAULT CODES DID NOT RETURN. 3600 5-6-21. REF: W/O 299663, N/R-00001 FOR WORK PERFORMED. R&R OF #1 NACELLE SHUTOFF VALVE. OPS TEST GOOD, NO FAULTS FOUND. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (NLG) · airframe 22,306 hrs · 24,088 cycles

NOSE LANDING GEAR OPEN LIGHT ILLUMINATED WITH THE NOSE LANDING GEAR DOOR CLOSED. REMOVED FROM SERVICE. CYCLED NOSE GEAR DOORS OPEN TO CLOSED. LIGHT EXTINGUISHED. RETURNED TO SERVICE.

Part: FLOOR MAT — BULGED (CABIN FLOOR) · airframe 21,659 hrs · 23,456 cycles

AFT GALLEY FLOORING HAS BUBBLED TO THE POINT OF SERVICE CART INTERFERENCE AND A POTENTIAL TRIPPING HAZARD. REMOVED FROM SERVICE. PULLED BACK FLOORING, CLEANED ALL TRACES OF WATER CONTAMINATION. APPLIED NEW TAPE AND RESECURED FLOORING WITH EDGE SEALANT, REF Q400 AMM 25-25-01-400-802. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED SYSTEM) · airframe 21,594 hrs · 23,381 cycles

REJECTED TAKEOFF DUE TO NR 1 BLEED HOT CAUTION LIGHT ON TAKEOFF ROLL. NR 2 BLEED HOT CAUTION SHORTLY AFTER CLEARING RUNWAY, RAN CHECKLIST. CAUTION LIGHTS CLEARED. BLEED FLOW SELECTOR WAS IN "MIN" DUCT & CABIN TEMPS APPEARED TO BE NORMAL. TAKEOFF REJECTED BELOW 80 KTS. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND FAULT 3003-PACK FCV ON BOTH CHANNELS. C/W FIM TASK 36-20-00-810-805. OPERATIONS TEST WAS GOOD AND FAULTS REMAINED EXTINGUISHED. DUE TO HAVING 3003 PREVIOUSLY R & R PACK FLOW CONTROL AND SHUTOFF VALVE, IAW Q400 AMM TASKS 21-52-01-000-801 AND 21-52-01-400-801 STEPS 1-5C. C/W REMAINING STEPS OF Q400 AMM TASK 21-52-01-400-801, LEAK CHECK & OPERATIONS CHECK IS GOOD. NO FAULTS PRESENT IN CDS UNDER ECS SYSTEM. C/W BLEED AIR OPERATIONS TEST, REF Q400 AMM TASK 36-11-00-710-802. OPERATIONS TEST IS GOOD. ALL INDICATIONS ARE NORMAL, NO FURTHER ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — DAMAGED (RT WING TE FLAP) · airframe 20,966 hrs · 22,715 cycles

NR 4 FLAP TRACK MAKING GRINDING NOISE AND VIBRATING DURING FLAP EXTENSION AND RETRACTION ON THE RIGHT WING. FOUND THE UPPER DEAD WEIGHT ROLLER CAUSING THE NOISE. REMOVED THE ROLLER AND CLEANED THE ROLLER AND SHAFT AND RE-INSTALLED. CHECKED ADJUSTMENT IAW AMM 27-52-00-802. NO OBVIOUS DEFECTS NOTED. OPERATED FLAPS NORMALLY WITH NO NOISE OR VIBRATIONS.

Part: BUMPER — BROKEN (CABIN DOOR) · airframe 20,783 hrs · 22,508 cycles

FORWARD MAIN CABIN DOOR OUTER RELEASE HANDLE STOP BUMPER BROKEN. REMOVED FROM SERVICE. REPLACED FWD MCD OUTER HANDLE BUMPER STOP WITH NEW FROM STOCK. OPS CK GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 20,636 hrs · 22,331 cycles

EMERGENCY LIGHT STRIP IN FRONT OF THE FORWARD GALLEY SLIDES OUT OF TRIM. REMOVED FROM SERVICE. R & R EMERGENCY FLOOR PATH LIGHT PANEL IN FWD GALLEY IAW Q400 AMM 33-51-16-000/400-801. OPC GOOD.

Part: AXLE — CORRODED (MLG) · airframe 20,557 hrs · 22,237 cycles

#1 MAIN GEAR AXLE HAS PITTING CORROSION UNDER THE BRAKE ASSEMBLY. REPLACED AXLE ASSEMBLY.

Part: ACTUATOR — BYPASSING (NLG) · airframe 20,554 hrs · 22,234 cycles

AFTER SELECTING GEAR DOWN, MAIN GEAR EXTENDED NORMALLY. NOSE GEAR LAGGED ABOUT 2 SECONDS BEHIND MAIN GEAR, BUT DID EXTEND PROPERLY. MAIN GEAR WAS DOWN AND LOCKED. NOSE GEAR WAS STILL IN TRANSITION. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED OPS TEST OF L/G PRIMARY EXTENSION AND RETRACTION. FOUND MAIN GEAR ON EXTENSION DOWN IS 8 SECONDS AND NOSE GEAR DOWN IN 12 SECONDS. FOUND NLG RETRACTION ACTUATOR BYPASSING. REMOVED NLG RETRACTION ACTUATOR REF Q400 AMM TASK 32-31-46-000-801. INSTALLED NEW NLG RETRACTION ACTUATOR REF Q400 AMM TASK 32-31-46-400-801. GEAR SWINGS FUNCTIONAL TEST GOOD REF Q400 AMM TASK 32-31-00-720-801. RETURNED TO SERVICE.

Part: FILTER — MALFUNCTIONED (ZONE 700) · airframe 20,556 hrs · 22,236 cycles

SELECTED GEAR DOWN ON FINAL. NOSE GEAR RED WITH AMBER DOOR UNSAFE LIGHT. RAN CK-LIST, INHIBIT SWITCH TO INHIBIT NOSE GEAR DROPPED WITH GREEN LIGHT. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND PSEU FAULTS NGDN2, NGNGLK2, NGDRCL. FAULTS CLEARED AFTER RESETTING INHIBIT SWITCH & HYD PWR. REF FIM 32-00-00-810-814 FOR T/S C/W GVI ON MECH SEQ. VALVE. NO DEFECTS NOTED. PROX SENSOR INDUCT VALVE NORMAL RANGE C/W GVI ON MLG NO DEFECTS NOTED. INSPECTED & REPLACED SSU FILTERS. C/W BYPASS CHECK OF NLG DOOR ACT CHECK GOOD. PER FIM 32-00-00-810-826. C/W BYPASS CHECK OF NLG DOOR ACT CHECK GOOD PER FIM 32-00-00-810-826.C/W NOSE GEAR RETRACT & EXTENSION CHECK IAW Q400 AMM 32-31-00-867-802. NO DEFECTS NOTED INDICATES NORMAL. WITH SPU AS HYD SOURCE UP TIME 7 SECONDS DOWN 10 SEC A/C RTS. RETURNED TO SERVICE.

Part: SPRING — WEAK (DOOR SPRING) · airframe 20,324 hrs · 21,966 cycles

FWD F/A JUMPSEAT COMPARTMENT SPRING IS WEAK. REMOVED FROM SERVICE. INSTALLED NEW SPRING FOR FWD FA EMERGENCY DOOR COMPARTMENT. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LATCH — INOPERATIVE (FLASHLIGHT COMP) · airframe 20,328 hrs · 21,968 cycles

FORWARD CABIN FLASHLIGHT COMPARTMENT LATCHES WONT LATCH, REMOVED FROM SERVICE. REMOVED AND REPLACED LATCH AS REQ. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (PROP DE-ICE) · airframe 20,175 hrs · 21,789 cycles

PROP DEICE CAUTION ILLUMINATED DURING CYCLING OF #2 PROP DEICE. #1 PROP DEICE OPERATED NORMALLY. CHECKLIST RUN. NO HELP. DIVERTED. ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. REPLACED # 2 PROP #6 DEICE HARNESS. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (APU) · airframe 19,147 hrs · 20,563 cycles

APU START ABORTED DUE TO RAMP REPORT FLAME FROM EXHAUST ( APU INOP ). RESET APU CB L3. OPS TESTED APU PER AMM 49-00-00-869-801. APU FAILED TO START. RE-ACCOMPLISHED MEL MTX PROCEDURE TO CONTINUE MEL 49-00-1. APU CB L3 IS PULLED/COLLARED. CDS SHOWED 270-0/RUN (DMM TEMP SENSOR) AND 054-2/RUN (IGNITOR PLUG A OPEN) FAULTS. PLACED APU ON MEL 49-00-1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,575 hrs · 19,871 cycles

FORWARD FA JUMPSEAT EMERGENCY LIGHT SWITCH NOT ILLUMINATED. REMOVED FROM SERVICE. RELAMPED FWD FA EMERGENCY LIGHT SWITCH. ALL LAMPS ILLUMINATE. EMERGENCY LIGHTS NORMAL. RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 18,182 hrs · 19,390 cycles

AFTER PUSH BACK, DURING THE AFTER START FLOW WE GOT ON THE PFD 2 A: 1. HDG FAIL, 2. WX FAIL, 3. TERR FAIL, & 4 TCAS FAIL MSG. AFTER RUNNING THE HDG FAIL CHECK LIST (4.18) AND DOING THE SPGRG AHRU RESET, MX REQUESTED TO RETURN TO GATE. DURING THE TAXI BACK TO THE GATE, WE NOTICED AN ELECTRICAL BURN SMELL IN THE COCKPIT. REMOVED FROM SERVICE. PERFORMED THE AIR CONTAMINATION CHECKLIST, DETERMINED THAT ELECTRICAL SMELL WAS EXTERNAL OF AIRCRAFT. POWERED OFF AND ON THE AIRCRAFT, NO FAIL MESSAGES OCCURRED. PERFORMED OPS TEST OF THE WEATHER RADAR IAW Q400 AMM 34-41-00-710-804, TEST GOOD. PERFORMED OPS TEST OF THE EGPWS IAW AMM 34-42-00-710-802, TEST GOOD. PERFORMED OPS TEST OF THE TCAS IAW AMM 34-43-00-710-801, TEST GOOD. PERFORMED OPS TEST OF THE AHRU CONTROLLER IAW MTC 6342102, TEST GOOD. PERFORMED AHRU COMPUTER OPS TEST IAW MGTC 6342101, TEST GOOD. PERFORMED HGS OPS TEST IAW MTC 6343510, TEST GOOD. FAIL MESSAGED DID NOT RETURN. NO OTHER DEFECTS NOTED. AIRCRAFT STATUS REMAINS CAT III. COCKPIT PLACARD READS CAT III. MTX CONTROL NOTIFIED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — INOPERATIVE (NR 1 PROPELLER) · airframe 17,771 hrs · 18,924 cycles

ON START UP #1 ENG TOOK APPROX 1 MIN TO COME OUT OF FEATHER. ++REMOVED FROM SERVICE. REPLACED #1 ENGINE PCU. PROPELLER FEATHERS AND UN FEATHERS WITHIN TIME LIMITS. OPS CKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 17,592 hrs · 18,724 cycles

DURING CLIMBOUT AT APPROXIMATELY 2000 FEET MSL THERE WAS A LOUD THUMP AND OUR EARS POPPED. DURING CLIMBOUT THE PLANE WOULD NOT PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PLACED PRESSURIZATION SYSTEM ON MEL 21-30-5A. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 570-668) · airframe 17,540 hrs · 18,673 cycles

SEAT RAIL 8 FROM FS X 570.0 TO FS X 668 LBL Y 9.25 CORRODED IN MULTIPLE LOCATIONS. SEAT RAIL 8 FROM FSX 570.0 TO FSX 668 LBL Y 9.25 REPLACED IAW SRM 51-42-05, 51-42-15 & 51-41-05.

Part: SEAT TRACK — CORRODED (BS 698-715) · airframe 17,540 hrs · 18,673 cycles

SEAT TRACK 25 FROM FS X 698 TO FS X 715 LBL Y 30 CORRODED. SEAT TRACK 25 FROM FSX 698 TO FSX 715 LBL Y 30 BLENDED IAW SRM 53-20-49-02-02. FOUND TO BE BEYOND LIMITS. SEAT TRACK 25 FROM FSX698 TO FSX 715 LBL Y 30 REPLACED IAW SRM 51-42-05-02-01 AND 51-42-15-02-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,365 hrs · 18,491 cycles

FORWARD F/A EMERGENCY LIGHTS SWITCH DOES NOT ILLUMINATE IN THE NORMAL POSITION. RELAMPED IAW AMM 33-51-05-000-801 AND 33-51-05-400-801. OPERATIONAL CHECKS GOOD.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 16,999 hrs · 18,064 cycles

AFTER ENGINE START, BROUGHT PROPS LEVERS TO 1020. NR 1 ENGINE TOOK 1 MINUTE LONGER TO UNFEATHER THAN THE NR 2. REPLACED THE NR 1 OVERSPEED GOVERNOR. NO FURTHER DEFECTS NOTED. PROP UNFEATHERS NORMALLY. RETURNED TO SERVICE.

Part: PROPELLER — LACK OF LUBE (NR 1) · airframe 16,983 hrs · 18,048 cycles

AFTER ENGINE START AND AFTER CONDITION LEVER SELECTED TO 1020RPM, THE NR 1 PROP TO GO OUT OF FEATHER. AFTER BEING INSTRUCTED BY MAINT TO PUT THE NR 1 PROP BACK TO START/FEATHER POSITION AND THEN BACK TO 1020RPM POSITION, IT TOOK THE PROP 35 SECONDS TO GET OUT OF FEATHER. C/W FIM 61-20-00-810-803 STEPS 1-4(A). ADDED 600ML OF PROP GREASE. NO LEAKS FOUND. UNFEATHERED NR 1 PROP 3X WITH AN AVERAGE TIME TO UNFEATHER OF 16 SECONDS. A/C IS CLEARED FOR RETURN TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 1 AC) · airframe 16,603 hrs · 17,638 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED DURING CRUISE FLIGHT. PERFORMED E/A CHECKLIST, CYCLED THE AC GENERATOR OFF THEN ON, NO HELP. LEFT AC GENERATOR OFF FOR REMAINDER OF FLIGHT. DIVERTED AND LANDED UNEVENTFULLY. COMPLIED WITH AMM 05-53-00-210-819, AND AMM 45-00-73-742-801. NO CHIP DETECTED OR OIL BYPASS FAULTS NOTED. NO FURTHER ACTION IAW 05-53-00-210-819. REPLACED THE NR 1 AC GENERATOR IAW MTC 6242101. OPS CHECKED GOOD IAW AMM 24-21-00-710-801. RETURNED TO SERVICE.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 16,584 hrs · 17,620 cycles

RADAR INTERMITTENTLY INOPERATIVE. WOULD NOT PAINT ANY ECHOS, NO TEST. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED, OPS TESTED GOOD THE WEATHER RADAR TRANSCEIVER IAW AMM 34-41-01-000/400-801. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 15,947 hrs · 16,959 cycles

OPS TEST OF EMERGENCY LIGHTS SYSTEM FAILED. R & R OF EPSU BATTERY PACKS, OPS TESTED GOOD IAW AMM 33-51-00-820-801.

Part: TIRE — FAILED (RT MLG) · airframe 14,940 hrs · 15,924 cycles

RIGHT INBOARD MAIN TIRE BLOWN ON LANDING. NO OTHER DAMAGE NOTED. PERFORMED INSPECTION AFTER TIRE FAILURE IAW AMM TASK 05-50-61-210-801. NO OTHER DEFECTS NOTED. REPLACED #3 + #4 MLG WHEEL AND TIRE ASSYS. NO FURTHER DEFECTS.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 14,560 hrs · 15,511 cycles

DURING CLIMB OUT AT 11000 FT, FUSELAGE DOOR WARNINGS AND MASTER WARNINGS. RAN THE CHECKLIST FROM THE EA AND CONFIRMED THE AFT CARGO DOOR INDICATED UNSECURE. PRESSURE HELD STEADY FOR APPROXIMATLEY 8 MINUTES. RETURNED TO FIELD. LOST PRESSURE DURING THE APPROACH. THE AFT FA REPORTED HEARING SEVERAL HARD THUMPS. LANDING UNEVENTFUL. NO HISTORY. NOTED AFTER AIRCRAFT TAXIED TO GATE THAT THE AFT CARGO DOOR HANDLE WAS EXTENDED. PERFORMED GVI OF THE AFT CARGO DOOR, DOOR SEALS AND BLOWOUT PANELS. FOUND THE AFT BLOWOUT PANEL DISLODGED. RESET THE AFT BLOWOUT PANEL. PERFORMED OPS TEST OF THE AFT CARGO DOOR IAW AMM 52-31-00-710-801. OPS TESTED GOOD. AFT CARGO DOOR HANDLE SECURE ALL INDICATIONS NORMAL. PRESSURIZED THE AIRCRAFT IAW AMM TASKS 21-00-00-863-801 & 802. AIRCRAFT PRESSURIZED NORMALLY AND MAINTAINS PRESSURIZATION. NO FURTHER DEFECTS NOTED. PERFORMED INSPECTION OF THE AFT CARGO DOOR HANDLE IAW HS 05-0029 WITH NO DEFETCS NOTED. RETURNED TO SERVICE.

Part: PANEL — UNLATCHED (RT WING) · airframe 14,509 hrs · 15,454 cycles

FUELING ON LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF. FOUND OUTBOARD LATCH ON FUEL / REFUEL PANEL UNLATCHED. DID GVI OF LATCH AND SWITCH AND FOUND NO DEFECTS. CLOSED FUEL PANEL DOOR AND RE-SECURED AND LATCHES AND REFUEL LIGHT WENT OUT. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 14,008 hrs · 15,005 cycles

UPON WALK THROUGH FOUND MCD ENTRYWAY EMERGENCY LIGHT STRIPS LOOSE AND REQUIRING SEALANT. COMPLIED WITH TASKCARD. REFERENCE TASKCARD FOR WORK ACCOMPLISHED. RESECURED FLOOR STRIP. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 14,088 hrs · 15,005 cycles

UPON WALKTHROUGH, FOUND EMERGENCY LIGHT STRIP AT SEATS 3AB AND 4AB REQUIRING RESECURING. COMPLIED WITH TASKCARD. REFERENCE TASKCARD FOR WORK ACCOMPLISHED. RESECURED LIGHT STRIP. NO PARTS REPLACED.

Part: ENGINE — LEAKING (NR 2) · airframe 13,391 hrs · 14,208 cycles

ON APPROACH, FA NOTIFIED EXCESS OIL COMING OUT OF THE NR 2 ENGINE. ALL INDICATIONS OF OIL PRESSURE AND TEMPERATURE INDICATED NORMAL. ON POST FLIGHT, DISCOVERED OIL TRAILING FROM THE FORWARD OUTFLOW VENT TO THE FAR AFT OF THE NACELLE. PERFORMED GVI ON NR 2 ENGINE IAW FIM TASK 79-00-00-810-807. CLEANED ENGINE NACELLE, EMPTIED FRONT DRAIN COLLECTOR, RAN #2 ENGINE FOR 5 MINUTES, AND CONFIRMED THERE IS NO SIGNS OF OIL LEAKAGE FROM THE FORWARD OUTFLOW VENT TO THE FAR AFT OF THE NACELLE AT THIS TIME. THERE IS ALSO NO SIGNS OF OIL LEAK FROM DRAIN COLLECTOR. PERFORMED GVI OF THE RH ENGINE OIL LEVEL IAW HORIZON TASK CARD 791000201, ADDED 16 PINTS OF OIL. NO OTHER DEFECTS NOTED. A/C IS OK FOR RETURN TO SERVICE.

Part: FAN — ODOR (RECIRCULATION) · airframe 13,293 hrs · 14,091 cycles

DURING TAXI IN, ELECTRICAL ODOR FROM FLIGHT DECK VENTS. SELECTING RECIRCULATION FAN OFF, AND ODOR STOPPED. FOUND THE FAN FAILED. REMOVED AND REPLACED THE FAN IAW AMM TASK 21-22-16-000-801, 21-22-16-400-801 PARA 1-4, STEP 5. FOUND BAD FUSE. REPLACED AS REQUIRED. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE — LOOSE (WINDSHIELD) · airframe 12,876 hrs · 13,671 cycles

A BURNING OR ACRID ODOR NOTICED AT HIGH POWER SETTINGS. REDUCTION OF ENGINE POWER, SEMS TO DISSIPATE. COMPLETED AIR CONTANIMATION CHECKLIST. NO ODORS NOTED IN THE CABIN. NOTICED SLIGHT HOT ELECTRICAL ODOR IN FLIGHT DECK STRONGER. CLOSEST TO F/O WINDSHIELD TERMINAL BLOCK. FOUND A LOOSE SCREW AND SIGNS OF ARCHING ON L2 TERMINAL. R EPLACED THE RT WINDSHIELD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT BUTTON) · airframe 12,203 hrs · 12,917 cycles

NORMAL SEGMENT OF F/A EMERGENCY LIGHT BUTTON INOPERATIVE, RELAMPED. CHECKS GOOD IAW AMM 33-26-03-960-801 AND MCN 6-33-100. RETURNED TO SERVICE.

Part: ANGLE — CORRODED (BS 669-697) · airframe 11,882 hrs · 12,578 cycles

AFT ENTRY DOOR SILL EDGE ANGLE BETWEEN X669.300 AND X697.600 IS CORRODED. AFT ENTRY DOOR SILL EDGE ANGLE BETWEEN X669.300 AND 697.600 REMOVED IAW SRM 51-42-05. AFT ENTRY DOOR SILL EDGE ANGLE BETWEEN X669.300 AND X697.600. REPLACED IAW SRM CHAPTER 51-42-05 AND 51-42-45.

Part: CHANNEL — CORRODED (BS 669-697) · airframe 11,882 hrs · 12,578 cycles

AFT ENTRY DOOR SILL EDGE CHANNEL BETWEEN X669.300 AND X697.600 IS CORRODED. AFT ENTRY DOOR SILL EDGE CHANNEL, PN 85339542-101, BETWEEN X669.300 AND X697.600. REMOVED IAW SRM CHAPTER 51-40-07. AFT ENTRY DOOR SILL EDGE CHANNEL, P/N 85339542-101 BETWEEN X669.300 AND 697.600, CHAPTER 51-42-05, & CHAPTER 51-42-45.

Part: FLOOR SUPPORT — CORRODED (BS 669-697) · airframe 11,882 hrs · 12,578 cycles

FLOOR SUPPORT ANGLE LOCATED BETWEEN X669.3 - 697.6 CORRODED. FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-40-07, 51-42-05 AND 51-40-15.

Part: DOOR SILL — CORRODED (BS 669-697) · airframe 11,882 hrs · 12,578 cycles

AFT ENTRY DOOR SILL CHANNEL SUPPORT MID RIB BETWEEN 669.300 AND X697.600 SHOWS SIGNS OF CORROSION. ATTACHING RIB AT BS 690.525 ON AFT PAX DOOR LWR THRESHOLD REMOVED IAW SRM CHAPTER 51-40-07. NEW ATTACHING RIB AT BS 690.525 ON AFT PAX DOOR LWR THRESHOLD INSTALLED IAW SRM CHAPTER 51-42-05.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 11,882 hrs · 12,578 cycles

LEFT OTBD MID FUSELAGE SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRAC IAW SRM 51-42-05, 51-40-15, AND 51-42-45,

Part: SUPPORT CHANNEL — CORRODED (BS 667-669) · airframe 11,882 hrs · 12,578 cycles

AFT ENTRY DOOR SILL, CHANNEL SUPPORT, MID AFT RIB BETWEEN X669.30 AND X697.600 SHOWS SIGNS OF CORROSION. SUPPORT RIB, PN 85339515-101 BETWEEN BS X669.30 AND 697.600 ON AFT PAX DOOR THRESHOLD REMOVED IAW SRM CHAPTER 51-140-07. SUPPORT RIB, PN 85339515-101 BETWEEN BS X669.30 AND 697.600 ON AFT PAX DOOR THRESHOLD REPLACED IAW SRM CHAPTER 51-42-05.

Part: CHANNEL — DAMAGED (DOOR FRAME) · airframe 11,882 hrs · 12,578 cycles

AFT PAX LOWER SURROUND OF DOOR, EDGE CHANNEL ATTACHING RIB IS DAMAGED. ATTACHING RIB AT BS X683.450 ON LWR THRESHOLD OF AFT PAX DOOR REMOVED IAW SRM CHAPTER 51-40-07, DRILLING AND REAMING. NEW ATTACHING RIB AT BS 683.450 ON AFT PAX DOOR LOWER THRESHOLD INSTALLED IAW SRM CHAPTER 51-42-05.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 11,882 hrs · 12,578 cycles

CORROSION ON TOP OF AFT SERVICE DOOR EDGE BEAM, INNER. REMOVED SCREWS, QTY 2 FROM AFT SERVICE DOOR EDGE BEAM, INNER IAW SRM 51-40-00. REMOVED AFT SERVICE DOOR EDGE BEAM, INNER, PN: 85339543-101 IAW SRM 51-40-07 AND SRM 51-42-45-02-01. LOCATED HOLES AND ANCHOR NUTS IN NEW EDGE BEAM, PN: 85339543-101 IAW SRM 51-40-07 AND SRM 51-42-75-02-01. INSTALLED NEW EDGE BEAM TO AFT SERVICE DOOR LOWER SILL IAW SRM 51-42-05 & SRM 51-23-00 SRM 51-42-45-02-01 AND INSTALLED SCREWS, QTY 2 IAW SRM 51-41-05-00-01. REPROTECTED EDGE BEAM IAW SRM 51-25-20.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 11,882 hrs · 12,578 cycles

CORROSION ON AFT SERVICE DOOR EDGE BEAM OUTER. REMOVED OUTER EDGE BEAM FROM AFT SERVICE DOOR LOWER SILL IAW SRM 51-40-07. LOCATED HOLES IN NEW EDGE BEAM, PN 85339542-101 IAW SRM 51-40-07 AND SRM 51-42-05. INSTALLED NEW EDGE BEAM TO AFT SERVICE DOOR LOWER SILL IAW SRM 51-42-05 AND SRM 51-23-00. APPLIED ENAMEL PAINT TO EDGE BEAM IAW SRM 51-25-20.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 11,882 hrs · 12,578 cycles

CORROSION BEYOND LIMITS ON CARGO TRACK . REMOVED AND REPLACE THE CARGO TRACK IAW DWG 85338210 AND SRM 51-42-05, 51-40-15, AND 51-41-05.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,882 hrs · 12,578 cycles

LEFT OTBD FWD FUSELAGE SEAT TRACK NR 1 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15-02-01, 51-41-05-02-01.

Part: SEAT TRACK — CORRODED (BS 102-229) · airframe 11,882 hrs · 12,578 cycles

RIGHT OTBD FWD FUSELAGE SEAT TRACK BS 102.5 - 229.5 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, 51-42-45, 51-40-07-02-01, AND DWG 85361551.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 11,882 hrs · 12,578 cycles

CORROSION FOUND IN SEVERAL SPOTS ON FWD BAGGAGE DOOR THRESHOLD. REMOVED FWD AND AFT GUSSETS, REMOVED FWD AND AFT SCUFF PLATES. REMOVED FWD AND AFT CORNER COMBINGS. REMOVED SILL CHANNEL ANGLE. REMOVED EDGE CHANNEL. REMOVED CHANNEL SUPPORT RIBS 1, 2, AND 3 IAW SRM 51-40-07, SRM 51-42-15-02-01 AND SRM 51-42-45-02-01. NEW EDGE CHANNEL ASSY, PN 85329604-001 INSTALLED IAW SRM 51-42-05-02-01 SOLID RIVET INSTALLATION. 3 SUPPORT RIBS RE-INSTALLED IAW SRM 51-42-05-02-01. FWD AND AFT SCUFF PLATES AS WELL AS FWD AND AFT COMBING INSTALLED IAW SRM 51-42-05-02-01 AND SRM 51-41-05-00-01. INSTALLED FWD AND AFT GUSSETS IAW SRM 51-40-15 AND SRM 51-25-25. APPLIED CORROSION INHIBITING COMPOUND TO FWD BAGGAGE LOWER SURROUND IAW MODEM IS4Q5100004.

Part: ANGLE — CORRODED · airframe 11,882 hrs · 12,578 cycles

SHEAR ANGLE OTBD OF LEFT INBD SEAT TRACK AT FS X1.0 TO X19.5 CORRODED ON TOP SURFACE WHERE F/A SEAT BOLTS. SHEAR ANGLE REMOVED IAW SRM 51-42-05. NEW SHEAR ANGLE INSTALLED IAW SRM 51-42-05.

Part: BEAM — CORRODED (ZONE 200) · airframe 11,882 hrs · 12,578 cycles

CORROSION FOUND ON TYPE 2 EMERGENCY EXIT BEAM ASSY. REMOVED LOWER EMERGENCY EXIT DOOR DITCHING DAM IAW AMM 52-23-00. REMOVED 16 BOLTS FROM LOWER BEAM ASSY IAW SRM 51-40-07. REMOVED LOWER EDGE BEAM ASSY IAW SRM 51-42-05, SRM 51-40-07 AND SRM 51-42-90. INSTALLED ANCHOR NUTS ON NEW BEAM AND INSTALLED NEW BEAM, PN 85329514-101 IAW SRM 51-42-05, SRM 51-42-90 AND SRM 51-23-00. INSTALLED 16 BOLTS ON FLOOR RETAINER ATTACHING TO BEAM ASSY IAW SRM 51-41-05. INSTALLED LOWER DITCHING DAM DOOR IAW AMM 52-23-00 AND SRM 51-23-00.

Part: SEAT TRACK — CORRODED (RIGHT) · airframe 11,882 hrs · 12,578 cycles

RIGHT OTBD MID FUSELAGE SEAT TRACK NR 19 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, AND 51-42-45.

Part: ANGLE — CORRODED (BS 783) · airframe 11,882 hrs · 12,578 cycles

AFT CARGO SHEAR WEB TO SHELF WEB ANGLE AT FS 783, LBL 20 TO LBL 24 HAS CORROSION ON TOP SURFACE, PN 85339286. SHEAR WEB TO SHELF ANGLE AT FS 783, LBL20 TO 24 REMOVED IAW SRM 51-42-05. NEW ANGLE INSTALLED AT FS 783, LBL 20 TO 24 IAW SRM 51-42-05.

Part: ANGLE — CORRODED (BS 100) · airframe 11,882 hrs · 12,578 cycles

CORRODED RIB AT EMERGENCY DOOR THRESHOLD STN 100.80, RT SIDE. REPLACED RIB AT EMERGENCY DOOR LOWER SURROUND RT SIDE X100.80 IAW SRM 51-42-05.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 11,882 hrs · 12,578 cycles

RT INBD CARGO TRACK CORRODED BEYOND LIMITS. REMOVED THE CARGO TRACK IAW SRM 51-42-05, 51-40-15 & 51-41-00. NEW CARGO TRACK DRILLED & REAMED IAW SRM 51-40-07, AND INSTALLED IAW SRM REF 51-42-05, 51-40-15 AND 51-41-00.

Part: SEAT TRACK — CORRODED (BS 612-670) · airframe 11,882 hrs · 12,578 cycles

RIGHT INBD AFT FUSELAGE SEAT TRACK NR 15 CORROSION BEYOND LIMITS. SEAT RAIL BS 612 - 670 REMOVED IAW SRM 51-42-05, 51-40-15 & 51-41-00. NEW SEAT TRACK DRILLED & REAMED IAW SRM 51-40-07 AND INSTALLED IAW SRM 51-42-05 & 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,882 hrs · 12,578 cycles

RIGHT INBD FUEL FUSELAGE SEAT TRACK NR 10 CORRODED BEYOND LIMITS. REPLACED THE SEAT TRACK IAW DWG 85328201, SHEETS 1 TO 4 AND SRM 51-42-05.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,882 hrs · 12,578 cycles

RIGHT INBD FWD FUSELAGE SEAT TRACK CORROED BEYOND LIMITS. REPLACED THE SEAT TRACK IAW DWG 85328201, SHEETS 1 TO 4 AND SRM 51-42-05, 51-40-15, , 51-41-05, AND AMM 51-80-00.

Part: SKIN — CORRODED · airframe 11,882 hrs · 12,578 cycles

CORROSION FOUND AROUND DRAIN HOLES ON LOWER SKIN AROUND FWD PAX DOOR. LIGHT SURFACE CORROSION REMOVED FROM THE INNER SURFACE OF THE FUSELAGE SKIN AROUND THE FORWARD PASSENGER DOOR DRAIN HOLES IAW STRUCTURAL REPAIR MANUAL 53-20-17, REPAIR 02 STEP 7S, 1-5 ONLY. REF ALSO FIGURE 201, SHEET 1, FORM M-184 AND NON-DESTRUCTIVE TESTING REPORT ATTACHED. NDT CARRIED OUT IAW SRM 53-20-17, REPAIR 02 M.

Part: ANGLE — CORRODED (ZONE 800) · airframe 11,882 hrs · 12,578 cycles

ANGLE AT FS 6.70 & 26.70, STR 25-27L AT FWD PAX DOOR CORRODED. ANGLE REMOVED AND REPLACED IAW SRM 51-42-05 AND SRM 51-42-05.

Part: SWITCH — BURNED (COCKPIT) · airframe 11,085 hrs · 11,734 cycles

F/A REPORTS A HOT METALLIC ODOR IN AFT GALLEY NEAR THE MAPCO. AFTER TURNING THE MAPCO OFF, THE ODOR SEEMED TO GO AWAY. PERFORMED ODOR CHECKLIST IAW M-744 REF FIM TASK MCN 62172-01 FOUND MILD ELECTRICAL SMELL TO COME FROM THE LT MAPCO SWITCH ASSY. REPLACED SWITCH ASSY OPS CHECKS GOOD NO FUTHER ELECTRICAL ODOR NOTED IN AFT GALLEY AREA. RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (PROP DE ICE) · airframe 9,195 hrs · 9,697 cycles

PROPELLER DE-ICE CAUTION LIGHT ILLUMINATES WHEN NR 1 PROPELLER IS HEATING. DIVERTED, LANDING UNEVENTFUL. CDS FAULT IS OPEN HEATER PHASE A NR 1 TMCU. R & R NR 1 BLADE DE-ICE HARNESS ON NR 1, PROP REF AMM 61-10-06-000-805, 61-10-06-400-805. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 9,025 hrs · 9,504 cycles

RUDDER TRIM RUNAWAY OCCURED IN FLIGHT. AUTOPILOT WAS ENGAGED, AIRCRAFT YAWED, TRIM INDICATION WAS MOVING RAPIDLY LEFT. PHASE OF FLIGHT WAS CLIMB ATTITUDE AND TRIM WAS NOT BEING USED AT THE TIME. IAW EMERGENCY CHECKLIST, CIRCUIT BREAKER FOR RUDDER TRIM ACTUATOR WAS PULLED. LANDING UNEVENTFUL. INTEROGATED CDS, NO FAULTS PERTAINING TO ATA 22 OR 27. R & R AILERON AND RUDDER TRIM CONTROL PANEL IAW MM 27-13-16-000-801 + 27-13-16-400-801 AS A PRECAUTIONARY MEASURE. OPS TEST OF AILERON AND RUDDER CONTROL SYSTEM GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2) · airframe 8,812 hrs · 9,289 cycles

DURING CLIMBOUT, RECEIVED A POWERPLANT MESSAGE ON ED. RETURNED TO FIELD, LANDING UNEVENTFUL. R & R NR 2, P2.2 SHUTOFF VALVE AND NR 2, P2.2 INTERSTAGE BLEED VALVE. GROUND RAN ENGINES AND NO POWERPLANT MESSAGE ILLUMINATES. RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 8,607 hrs · 9,081 cycles

NR 2 ARCDU WOULD INTERMITTENTLY GO DARK. WHEN CYCLED OFF THEN BACK ON, IT WOULD INDICATE NORMAL FOR A WHILE THEN GO DARK AGAIN. ARCDU FAIL MSG CAME UP ONCE THEN WENT DARK. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED AND INSTALLED NR 2 ARCDU WITH SERVICEABLE UNIT IAW MAINTENANCE 6238101, OPS CHECKS GOOD. C/W LLM RTS IAW MAINTENANCE 6238101, PASSED SATISFACTORILY. ACFT REMAINS CAT III QUALIFIED. RETURNED TO SERVICE.

Part: LAMP — DIM (LIGHT SWITCH) · airframe 7,841 hrs · 8,221 cycles

F/A EMERGENCY LIGHT SWITCH "NORMAL" LIGHT DIM, REPLACED THE LAMP.

Part: ACTUATOR — MALFUNCTIONED (NLG DOOR) · airframe 7,312 hrs · 7,647 cycles

WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR LIGHT REMAINED RED AND THE GEAR DOORS FOR THE NOSE REMAINED OPEN. AFTER ABOUT 1.5 MINUTES THE NOSE GEAR CAME DOWN AND INDICATED GREEN AND THE DOORS CLOSED ABOUT 30 SECONDS LATER. ABORTED APPRAOCH. CYCLED GEAR AND PERFORMED UNEVENTFUL LANDING. PERFORMED VISUAL INSPECTION OF THE NLG, NLG DOORS & SURROUNDING AREA. NO OBVIOUS DEFECTS WERE FOUND DURING INSPECTION. INTERROGATED PSEU & FOUND FAULT, FERRIED ACFT FOR REPAIRS. REPLACED NLG DOOR ACTUATOR. OPS CHECK OF PRIMARY EXTENSION AND RETRACTION SYS COMPLIED WITH IAW AMM TASK 32-31-00-710-801. NO DEFECTS NOTED, OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 6,952 hrs · 7,249 cycles

EMERGENCY LIGHTS ARE ON WITH THE SWITCH IN THE OFF POSITION. REMOVED AND CLOCKED EMERGENCY LIGHTS SWITCH IAW AMM TASK 31-51-10-000-801 AND 31-51-10-400-801. RETURNED TO SERVICE.

Part: SKIN — GOUGED (PAX DOOR) · airframe 6,491 hrs · 6,738 cycles

AIRSTAIR DOOR SHELL GOUGED AT LOWER FWD AND AFT ATTACH POINTS. INSTALLED AIRSTAIR DOOR STOP FITTING NR1 IAW AMM 52-11-09-400-801, STEP 4A. INSTALLED DOOR SUPPORT BRACKET IAW SRM 51-41-00-00-01. REMOVED PAX DOOR LOWER PANEL REF SRM 51-42-05, STEP 4, E AND SRM 51-42-15, STEP 5,G. NDT IAW NDTM 51-00-04, 51-00-06. NO DEFECTS LOWEST REMAINING THICKNESS .033 REF ATTACHED NDT REPORT. FABRICATED REPAIR DOUBLER FOR AFT PASSENGER DOOR LOWER INNER SKIN. FABRICATED REPAIR DOUBLER FOR AFT PASSENGER DOOR LOWER INNER SKIN IAW EO NR DASH 8-52-I00458 P2 MATERIAL USED PO T000015587, PN 2024T-3. PERFORM NDT IAW EO DASH8-52-I00458, P2, 11/12/13 WORK STEP 5 AND GENERAL NOTE 7. C/W ET INSEPCTION ON CUT OUT & REWORK & REPAIR PARTS IAW EO NR DASH 8-52-I00458 (P2, 11/12/13) WORK STEP 5 & GENERAL NOTE 7. NO DEFECTS NOTED. FABRICATED FILLER FROM 2024T-3 .0321 MATERIAL IAW EO NR DASH8-52-I00458. FABRICATED SHIM AND LOCATED HOLES USING 2024T-3 .040 PO T000015687 IAW EO NR DASH 8 52-I00458 P2. STARTED LOCATING HOLES ON REPAIR DOUBLER IAW EO NR DASH8-52-I00458 P2. LOCATED AND DRILLED REPAIR DOUBLER REF EO NR DASH8-52-I00458 DATED 11/12/2013 PRELIMINARY P2. RECEIVED FINAL EO NR DASH8-52-I00458A AND COMPLIED WITH TC DHC-8-52-I00458A. INSTALLED PAX DOOR LOWER PANEL DURING INSTALLATION OF REPAIR REF SRM 51-42-05 PG 204-205 PAR D STEPS 1-10 AND SRM 51-42-05, PG 203-204, PAR G 1-7.

Part: PLUG — MISSING (HAND RAIL) · airframe 6,491 hrs · 6,738 cycles

HAND RAIL MISSING BUTTON PLUGS ON BOTH SIDES, HARDWARE UNDER PLUG RUSTED. REMOVED RUSTED HARDWARE ON BOTH SIDES OF PAX DOOR HANDRAILS REF AMM 52-11-21-000-801, STEPS 1-3 AND 4E, 1,2,6. INSTALLED NEW HARDWARE AND PLUGS ON BOTH SIDES OF PAX DOOR HANDRAILS REF AMM 52-11-21-400-801, STEPS 1-3 AND 4F, 4-7.

Part: ACCESS PANEL — CORRODED (WING) · airframe 6,491 hrs · 6,738 cycles

CENTER WING FUEL PANEL 623AT HAS CORROSION ON NUMEROUS COUNTERSINK LOCATIONS. REMOVED CORROSION FROM COUNTERSINKS ON CENTER WING FUEL PANEL 623AT REF SRM 57-10-35, REPAIR-03, PG 202-203, PROCEDURE 6A, STEPS 1-2. PERFORMED E/T INSP OF PANEL 623AT COUNTERSINK HOLES IAW NDTM 51-00-06. NO DEFECTS NOTED. MEASURED DIAMETER OF REWORKED COUNTERSINKS OF .6470 MAX AND FASTENER HEAD OF .0135 BELOW FLUSH MAX, COUNTERSINKS ARE WITHIN LIMITS REF SRM 57-10-35. APPLIED ALODINE ON COUNTERSINK HOLES ON PANEL 623AT, REF AMM TASK 51-25-16-390-801.

Part: ACCESS PANEL — CORRODED (WING) · airframe 6,491 hrs · 6,738 cycles

CENTER WING FUEL PANEL 622BT HAS CORROSION ON NUMEROUS COUNTERSINK LOCATIONS. REMOVED CORROSION FROM COUNTERSINK LOCATIONS ON CENTER WING FUEL PANEL 622BT REF SRM 57-10-35, REPAIR-03, PG 202-203, PROCEDURE 6A, STEPS 1-2. PERFORMED E/T INSP OF PANEL 622BT COUNTERSINK HOLES IAW NDTM 51-00-06. NO DEFECTS NOTED. MEASURED DIAMETER OF REWORKED COUNTERSINKS OF .655 MAX AND FASTENER HEAD AT .0125 BELOW FLUSH REWORKED COUNTERSINKS ARE WITHIN LIMITS REF SRM 57-10-35. APPLIED ALODINE ON COUNTERSINK HOLES ON PANEL 622BT REF AMM TASK 51-25-16-390-801.

Part: ACCESS PANEL — CORRODED (WING) · airframe 6,491 hrs · 6,738 cycles

CENTER WING FUEL PANEL 522CT HAS CORROSION ON NUMEROUS COUNTERSINK LOCATIONS. REMOVED CORROSION FROM COUNTERSINKS ON CENTER WING FUEL PANEL 522CT REF SRM 57-10-35, REPAIR -03, PG 202-203, PROCEDURE 6A, STEP 1-2. PERFORMED E/T INSP OF PANEL 522CT COUNTERSINK HOLES IAW NDTM 51-00-06. NO DEFECTS NOTED. MEASURED DIAMETER OF REWORKED COUNTERSINKS OF .650 MAX AND FASTENER HEAD MEASURED .011 BELOW FLUSH. REWORK COUNTERSINKS ARE WITHIN LIMITS REF SRM 57-10-35. APPLIED ALODINE ON COUNTERSINK HOLES ON PANEL 522CT REF AMM TASK 51-25-16-390-801.

Part: ACCESS PANEL — CORRODED (WING) · airframe 6,491 hrs · 6,738 cycles

CENTER WING FUEL PANEL 522BT HAS CORROSION ON NUMEROUS COUNTERSINK LOCATIONS. REWORKED COUNTERSINKS ON CENTER WING FUEL PANEL 522BT IAW SRM 57-10-35 AND SRM 57-10-35, PG 202, STEP 6A (12EA). PERFORMED E/T INSP ON PANEL 522BT COUNTERSINK HOLES IAW NDTM 51-00-06. NO DEFECTS NOTED. MEASURED DIAMETER OF REWORKED COUNTERSINKS OF .6475 MAX AND FASTENER HEAD OF MAX OF .010 BELOW FLUSH. REWORKED COUNTERSINKS ARE WITHIN LIMITS REF SRM 57-10-35. APPLIED ALODINE ON COUNTERSINK HOLES ON PANEL 522BT REF AMM TASK 51-25-16-390-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 6,491 hrs · 6,738 cycles

SEAT TRACK CORRODED OUT OF LIMITS. REMOVED SEAT TRACKIAW SRM 51-42-05. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07. INSTALLED REF SRM 51-40-15 AND SRM 51-42-05.

Part: SEAT TRACK — CORRODED · airframe 6,491 hrs · 6,738 cycles

RT OTBD SEAT TRACK NR 18 HAS CORROSION. BLENDED OUT CORORSION IAW SRM 53-20-49. FOUND TO BE WITHIN LIMITS. PERFORMED E/T INS OF RT OTBD SEAT TRACK NR 18 IAW NDTM 51-00-06-910-801. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 657.5-664.5) · airframe 6,491 hrs · 6,738 cycles

RIGHT INBD SEAT TRACK NR 15 CORRODED FS 567.5 - 664.5. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, STEP 4D, AND SRM 51-40-15-02-01.

Part: SEAT TRACK — CORRODED · airframe 6,491 hrs · 6,738 cycles

SEAT TRACK NR 10 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05 & SRM 51-40-15. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (BS 664) · airframe 6,491 hrs · 6,738 cycles

RIGHT INBD SEAT TRACK NR 15 HAS CORROSION AT BS 664. FOUND OUT OF LIMITS DUE TO CORROSION REMOVAL IAW SRM 53-20-49, PGS 201-204, FIG 201, SHT 2. REMOVED SEAT TRACK IAW SRM 51-42-05 & SRM 51-40-15. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (BS 595-663) · airframe 6,491 hrs · 6,738 cycles

LEFT INBD SEAT TRACK NR 8 CORRODED AT BS 595, 605, 625, 653 AND 663. FOUND OUT OF LIMITS IAW SRM 53-20-49. SEAT TRACK REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: TRANSCEIVER — MALFUNCTIONED (NR 2 VHF) · airframe 5,275 hrs · 5,479 cycles

NR 2 VHF COMM INOPERATIVE ON BOTH ARCDU'S. RETURNED TO FIELD, LANDING UNEVENTFUL. R & R NR 2 TRANSCEIVER AS A PRECATIONARY MEASURE, IAW AMM TASK 23-11-01-000-801 AND 23-11-01-400-801. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 5,049 hrs · 5,246 cycles

F/A AND GROUND CREW REPORT THAT THE AFT PASSENGER DOOR IS DIFFICULT TO OPEN AND CLOSE. INSPECTED DOOR FOR ANY DEFECTS NONE NOTED LUBED DOOR HANDLE SHAFT MECHANISM. C/W OPEREATIONAL TEST OF AFT PASS. DOOR IAW AMM TASK 52-12-00-710-802. OPS TEST GOOD NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (NLG STEERING) · airframe 4,981 hrs · 5,177 cycles

AFTER TAKEOFF, THE NOSE WHEEL STEERING CAUTION ILLUMINATED. DIVERTED FLIGHT, LANDING UNEVENTFUL. R & R NLG STEERING HARNESS IAW AMM TASK 32-21-11-000-801/ 32-21-11-400-801. REPLACED WITH A SERVICABLE HARRNESS FROM STOCK NO FAULTS FLAGGED IN THE NWS ECU. ALL OPS CHECKED GOOD, ALL INDICATIONS NORMAL AND CAUTION DID NOT REOCCUR. RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (ZONE 200) · airframe 4,617 hrs · 4,779 cycles

FREQUENT CAUTIONS FOR: RUD CTRL, ROLL SPOILER OTBD HYD, PITCH TRIM, ELEVATOR FEEL. NR 2 IAS + ALTITUDE FAILURES, *CUE* ON AIRSPEED INDICATIONS. RETURNED TO FIELD. LANDING UNEVENTFUL. C/W ADU NR 2 WIRING TESTS & REPLACEMENT OF ADU. RETURNED TO SERVICE.

Part: BOLT — BROKEN (DOOR HANDLE) · airframe 4,586 hrs · 4,747 cycles

AFT SERVICE DOOR WILL NOT OPEN. FOUND OUTSIDE HANDLE BOLT BROKEN. REPLACED BOLT AND WASHERS. RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 4,436 hrs · 4,580 cycles

DE-ICE PRESSURE CAUTION, WITH BOOTS IN FAST, TORQUE AT 64 PERCENT, LT TAIL INBD ADV LIGHT DID NOT ILLUMINATE. DE-ICE PRESSURE GAUGE INDICATED NORMAL PRESSURE WITH BOOT ISO SWITCH ON AND OFF. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. L/E 331AL & 341BR AND DDV NR 6 REPLACED. PERFORMED FUNCTIONAL CHECK OF PNEUMATIC DE-ICE SYS IAW AMM 30-11-00-720-801, INCLUDING HS 30-0012. CHECKED GOOD. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (PROPELLER) · airframe 4,408 hrs · 4,550 cycles

NR 1 PROPELLER WOULD NOT COME OUT OF FEATHER, JUST HUNG AT 400 RPM WITH ERRATIC INDICATION IN TORQUE AND PROPELLER SPEED. INTERROGATED CDS NO FAULTS FOUND. RAN ACFT BUT COULD NOT DUPLICATE. R & R OVERSPEED GOVERNOR AS A PRECAUTION IAW AMM TASK 61-20-26-000-801, AND 61-20-26-400-801 PERFORMED OPS TEST IAW AMM TASK 61-20-710-803. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 4,275 hrs · 4,411 cycles

EMERGENCY STRIP LIGHTING AT THE ENTRYWAY IS MISSING. SECURED THE FLOOR STRIP LIGHTING SECTION. RETURNED TO SERVICE.

Part: GLOWSTRIP — DISLODGED (CABIN) · airframe 4,275 hrs · 4,411 cycles

PHOTO ILLUMINESCENT STRIP AT ROW 1A AND 1B IS DISLODGED. SECURED FLOOR STRIP. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 4,110 hrs · 4,240 cycles

LOOSE EMERGENCY LIGHTING STRIP IN FRONT OF MCD. RESECURED EMERGENCY LIGHTING STRIP, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: COFFEEMAKER — CONTAMINATED (ZONE 200) · airframe 2,992 hrs · 3,070 cycles

AFT F/A REPORTS AN ODOR IN AFT CABIN. INSPECTED AFT CABIN. CONFIRMED ODOR, BOTH MAPCO`S ON. FOUND RUBBER BAND ON TOP OF MAPCO HANDLE. REMOVED RT MAPCO. COULD NOT DETECT ODOR. R & R RIGHT MAPCO. OPS CHECKED GOOD. COMPLIED WITH AIR CONTAMINATION CHECKLIST.

Part: GENERATOR — FAILED (NR 1) · airframe 2,658 hrs · 2,744 cycles

ON ROTATION, NR 1 AC GENERATOR FAILED WITH ASSOCIATED CAUTION LIGHT. FOLLOWED CHECKLIST, WAS UNABLE TO GET IT BACK ON LINE. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 AC GENERATOR IAW TC 6242101. REPLACED NR 1 AC GENERATOR CONTROL UNIT IAW MM TASK 24-21-06-000/400-801. LEAK AND OPS CHECKED GOOD. NO CAUTION LIGHTS NOTED. RETURNED TO SERVICE.