N442QX

Part: BOOT — TORN (ZONE 600) · airframe 23,359 hrs · 24,954 cycles

ON CLIMB OUT DEICE PRES CAUTION ILLUMINATED.RAN CHECKLIST AND CAUTION WENT AWAY.SELECTING AIRFRAME MODE BACK TO SLOW DEICE PRESS CAUTION ILLUMINATED AGAIN NOTICED THE 2ND FROM THE OUTBOARD BOOT ON THE #2 RIGHT WING DID NOT ILLUMINATE. RETURNED TO FIELD. REMOVED FROM SERVICE. CLEARED DEICE CODES IN CDS. RAN #2 ENGINE. INTERROGATED CDS AND FOUND FAULT CODE LOW PRESSURE 2B FAIL. INSPECTED DEICE BOOTS AND FOUND SMALL TEARS ON UPPER INBOARD SIDE OF LE 613BR. PERFORMED REPAIR OF DAMAGED BOOT IAW Q400 AMM 30-11-00-300-802. PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYS IN REF WITH Q400 AMM TASK 30-11-00-720-801. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 23,312 hrs · 24,910 cycles

FWD EMERGENCY LIGHT SWITCH OUT. REMOVED FROM SERVICE. RELAMPED FWD EMERGENCY LIGHT SWITCH, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — INOPERATIVE (NLG) · airframe 22,733 hrs · 24,308 cycles

AFTER TAKEOFF AND NORMAL GEAR RETRACTION, THE RED NOSE GEAR LIGHT AND GEAR HANDLE ILLUMINATED TWICE. FIRST TIME WAS APPROX 1-1.5 SECONDS. SECOND TIME WAS 3-4 SEC AND FO REPORTED HE FELT LIKE THE DOOR FOR THE NOSE CAME OPEN. AIRSPEED ON SECOND EVENT WAS 215-220 KIAS REST OF FLIGHT WAS NORMAL AND GEAR WAS GREEN FOR A NORMAL LANDING ( LANDING GEAR RETRACTION SYSTEM ). EMERGENCY DECLARED AS A PRECAUTION. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. RETRACTED AND EXTENDED MLG SEVERAL CYCLES(REF AMM 32-31-00-867-801) NO DISCREPANCY. MANIPULATED NGLK1 HARNESS(NEAR SENSOR), RED NOSE GEAR ADV LIGHT FLICKERED ON /OFF AT LEAST FOUR TIMES, THEN REMAINED OFF. FURTHER MANIPULATING OF HARNESS DID NOT CAUSE NOSE RED TO ILLUM. R&R'ED NLG PRIMARY AND ALTERNATE-LOCK ELECTRICAL HARNESSES IAW Q400 MM TASKS 32-21-11-000-801 STEPS 4C(5) TO END & 32-21-11-400-801 STEPS 4B(15) TO END OF 4. PERFORMED RIGGING OF PROXIMITY SENSORS IAW Q400 MM 32-61-06-830-801 STEPS 1-4. PERFORMED FUNCTIONAL TEST OF LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM IAW Q400 MM 32-31-00-720-801, ALL CHECKS GOOD. COMPLETED TASK 32-61-06-830-801 STEP 5 TO END AND 32-21-11-400-801 STEP 5 TO END. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,655 hrs · 24,234 cycles

FA REPORTS A BAD SULFUL SMELL COMING FROM THE AFT GALLEY DURING DESCENT. REMOVED FROM SERVICE. C/W HORIZON AIR FORM M-744 AIR CONTAMINATION CHECKLIST. INSPECTED SUSPECT AREA THAT FLT ATTENDANT REPORTED. ( ON FLOOR AREA AFT GALLEY) INSPECTED AFT GALLEY AND AFT CARGO PIT. NO ODOR NOTED. FA REPORTED NO ABNORMAL SMELL COMING FROM GASPERS IN FLIGHT. REST OF CREW DID NOT SMELL ANYTHING ABNORMAL. NO PREVIOUS HISTORY REPORTED. AREA NO DEFECTS AT THIS TIME. A/C OK FOR CONTINUED SERVICE

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 22,641 hrs · 24,221 cycles

ON DEPARTURE FROM ALW, SELECTED GEAR UP BUT THE GEAR INDICATORS WERE 3 RED, NOSE GEAR WAS GREEN, NOSE GEAR DOOR NOT ILLUMINATED, MAIN GEAR DOORS ILLUMINATED, MAIN GEAR NOT GREEN. ABOUT 30 SECONDS LATER THE LDG GEAR INOP CAUTION ILLUMINATED. AT ACCELERATION HEIGHT WE CLEANED UP THE AIRPLANE AND A FEW SECONDS LATER THE GEAR CAME UP, ALL INDICATIONS WERE NORMAL, AND THE LDG GEAR INOP CAUTION EXTINGUISHED. AIRSPEED WAS BELOW 160 KIAS SO NO OVERSPEED CONDITION EXISTED. LANDING GEAR ALT DOORS + INHIBIT SWITCH WERE ALL IN THEIR NORMAL POSITIONS. WHEN GEAR SELECTED DOWN IN SEA, EVERYTHING CYCLED NORMALLY. ( LANDING GEAR RETRACTION SYSTEM ). REMOVED FROM SERVICE. COULD NOT DUPLICATE DURING NUMEROUS GEAR SWINGS IN HANGER. REF. W/O 303877 N/R-00003 AND N/R-00004 FOR PSEU FAULT CODES DIN01A AND DIN02A AND REPLACEMENT OF GEAR HANDLE. PERFORMED FUNCTIONAL TEST OF GEAR EXTENSION AND RETRACTION SYSTEM REF AMM 32-31-00-720-801, NO DEFECTS NOTED. PERFORMED BLEED OF #2 HYD SYSTEM REF AMM TASK 29-10-00-870-802. PLACARDS REMOVED FROM AML AND AC PANEL. AIRCRAFT RETURNED TO SERVICE.

Part: DRAIN MAST — MISSING (RT NACELLE) · airframe 21,936 hrs · 23,537 cycles

R/H NACELLE AFT I/B MLG DOOR P/N 85424003-001 DRAIN MAST FOUND MISSING . DRAIN MAST REQ REPAIR WITHIN 60 FH IAW DRAWING 85424003. 4/15/2021, REMOVED & REPLACED R/H NACELLE AFT I/B MLG DOOR DRAIN MAST. REF Q400 SRM 51-42-05-02-01 & DRAWING 85424003. PLACARD REMOVED FROM AML. THIS CLEARS DMI. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 21,420 hrs · 23,023 cycles

EMERGENCY LIGHT STRIP NEAR FORWARD CARGO DOOR OFF. REMOVED FROM SERVICE. REINSTALLED EMERGENCY LIGHT STRIP IN FRONT OF FWD CARGO DOOR, REF 400 TASK 33-51-16-400-801. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 20,800 hrs · 22,377 cycles

AFTER TOUCHDOWN, HALFWAY DOWN THE RUNWAY, THE AIRCRAFT PULLED TO THE LEFT OF THE CENTER LINE AFTER APPLICATION OF BRAKES. TAXI TO GATE WAS UNEVENTFUL AND BRAKES SEEMED NORMAL. NO EXCESSIVE BRAKING WAS USED AND NO CAUTIONS ILLUMINATED. REMOVED FROM SERVICE. PERFORMED GVI OF WHEELS AND BRAKES IAW Q400 AMM TASK 32-40-00-210-802, NO DEFECTS NOTED. PERFORMED GVI OF MLG BRAKES AND HYD LINES IAW Q400 AMM TASKS 32-40-00-210-803 AND 32-40-00-210-804. NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: STOP — BROKEN (DOOR HANDLE) · airframe 20,730 hrs · 22,310 cycles

UPON ARRIVAL THE RAMP WAS UNABLE TO OPEN THE MAIN CABIN DOOR. AFTER OPENING THE DOOR FROM THE INSIDE, THE RUBBER HANDLE STOPPER FELL OUT. WITHOUT THE STOPPER THE HANDLE JAMS AGAINST THE FLAP ABOVE IT SO YOU CAN`T ACCESS THE HANDLE TO OPEN THE DOOR FROM THE OUTSIDE. REMOVED FROM SERVICE. INSTALLED NEW BUMPER STOP IN REF WITH Q400 AMM 52-11-11-400-801 & MCN 6520839-01 ISSUE #02. DOOR NOW OPENS FROM THE OUTSIDE. NO FURTHER ACTION. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 20,657 hrs · 22,239 cycles

WITH APU RUNNING, CABIN DUCT TEMP CLIMBED UP TO 60 DEGREES C, PUT PACKS IN MANUAL MODE AND CABIN DUCT TEMP DROPPED TO 50 DEGREES C BUT WOULDN'T GO LOWER. REMOVED FROM SERVICE. PERFORMED MULTIPLE APU & ENGINE RUNS WITH INTERMITTENT HOT AIR POOR FLOW & COLD AIR GOOD FLOW. INTERROGATED CDS FOUND F.C 3003 - PACK FCV. C/W Q400 FIM TASK 21-60-00-810-809 STAP 5.A.(1)(C). R&R PACK FLOW CONTROL & SHUT OFF VALVE REF Q400 AMM TASK 21-52-01-000/400-801. INSPECTED HOSES & WIRING DURING R&R, NO FURTHER DEFECTS. LEAK CHECK IS GOOD OPS TEST 2X WITH BOTH APU AND ENG'S IS GOOD. CONSISTENT COLD AIR & GOOD FLOW. CABIN & F.D DUCT TEMPS BELOW 10 DEGREES C. F.C 3003 DID NOT RETURN - NO PRESENT FAULTS. NO FURTHER ACTION REQUIRED. Q400 MCN 6210194-1 ISSUE 1 WAS C/W. RETURNED TO SERVICE.

Part: COVER — MALFUNCTIONED (NLG STEERING) · airframe 20,600 hrs · 22,174 cycles

ON CLIMB OUT AT 5500 FEET THE NOSE STEERING CAUTION LIGHT ILLUMINATED. AFTER DOING THE CHECKLIST THE LIGHT REMAINED ON. UPON LANDING AT DESTINATION AIRPORT AIRCRAFT WAS SHUTDOWN NORMALLY ON THE TAXIWAY AND WAS TOWED TO THE GATE. REMOVED FROM SERVICE. FOUND FAULT SCU AND RVTX. REPLACED THE STEERING CONTROL UNIT. REPLACED THE NOSE STEERING HARNESS. STEERING FAILS OPERATIONAL CHECK WITH TILLER AND RUDDER INPUT, NO GEAR MOVEMENTS. FOUND FAULT CODES EHVS AND SCU FAULT HISTORY. REPLACED NOSE WHEEL STEERING ECU IAW AMM 32-51-01-000/400-801. OPERATIONAL CHECK FAILED. REPLACED MANIFOLD. OPERATIONAL CHECK FAILS. REPLACED STEERING FEEDBACK COVER ASSEMBLY. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE.

Part: STOP — DETERIORATED (DOOR HANDLE) · airframe 20,485 hrs · 22,054 cycles

MCD EXTERNAL HANDLE BUMPER STOP DETERIORATED AND IS BROKEN. REMOVED FROM SERVICE. REMOVED BUMPER STOP, INSTALLED NEW BUMPER STOP REF MCN# 6520839-01. RETURNED TO SERVICE.

Part: POWER UNIT — MALFUNCTIONED (TE FLAP) · airframe 20,442 hrs · 22,014 cycles

ON APPROACH SET FLAP LEVER TO FLAPS 10, RECEIVED FLAP POWER CAUTION LIGHT. RAN CHECKLIST, NO HELP. FLAP POWER CAUTION LIGHT REMAINS ILLUMINATED. REMOVED FROM SERVICE. REPLACED FLAP POWER UNIT. FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: CARPET — WRINKLED (ZONE 200) · airframe 19,930 hrs · 21,372 cycles

FLIGHT ATTENDANTS REPORTED CENTER AISLE CARPET HAS SEVERAL WRINKLES THAT ARE TRIPPING HAZARD & CATCH ON SERVICE CART. REMOVED FROM SERVICE. REMOVED CENTER AISLE CARPET AND TAPE. CLEANED FLOORBOARDS, APPLIED NEW TAPE AND NEW CARPET. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — DETACHED (AUTO FEATHER) · airframe 19,700 hrs · 21,101 cycles

AUTO FEATHER SWITCH POPPED OUT ON T/O. REMOVED FROM SERVICE. RESEATED AUTO FEATHER SW & PERFORMED OPERATION TEST OF THE PROPELLER AUTO FEATHER AND UPTREAM SYST PER Q400 AMM TASK 61-20-00-710-810-OPS CHECK GOOD.NO OTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (NR 2 NACELLE) · airframe 19,152 hrs · 20,463 cycles

ENGINE ADPT HEAT 2 CAUTION ILLUMINATED. (CB TRIPPED), REMOVED FROM SERVICE. FOUND DAMAGED WIRES SHORTING TO GROUND ON #2 ENGINE INTAKE LIP HEATER. REPLACED HARNESS. GROUND RAN ENGINE AND OPS CHECKED INTAKE ANTI-ICING SYSTEM PER AMM TASK 30-21-00-710-801. NO FAULTS RETURNED & CIRCUIT BREAKER REMAINED UNTRIPPED. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: BUMPER BLOCK — DEFECTIVE (PAX DOOR) · airframe 18,829 hrs · 20,105 cycles

FORWARD PAX DOOR HANDLE BINDING AGAINST FINGER HOLE FLAP, PREVENTING DOOR OPENING. REMOVED FROM SERVICE. REPLACED RUBBER GUIDE STOP REF. AMM TASKS 52-11-11-000-801 AND 52-11-11-400-801. DOOR HANDLE FUNCTIONS CORRECTLY. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PSEU — MALFUNCTIONED (ZONE 200) · airframe 18,822 hrs · 20,096 cycles

ON TAKEOFF AT POSITIVE RATE, MOVED THE GEAR LEVER TO THE UP POSITION . ALL GEAR LIGHTS EXTINGUISHED EXCEPT THE N. DOOR AMBER LIGHT. IMMEDIATELY AFTER THAT, THE LDG GEAR INOP CAUTION LIGHT ILLUMINATED. WE PROCCEEDED WITH CLIMB UP TO 12,000 FT AND REMAINED BELOW 200 KTS. RAN LDG GEAR INOP CAUTION CHECKLIST. RAN ALTERNATE GEAR EXTENSION CHECKLIST. DURING ALTERNATE GEAR EXTENSION CHECKLIST , ALL THREE GREEN LIGHTS ILLUMINATED UPON MOVING THE GEAR SELECTION HANDLE TO THE DOWN POSITION. CONTINUED FLIGHT WITH GEAR DOWN. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED PSEU DUE TO MULTIPLE INTERNAL POWER FAIL FAULTS AND CARD C FAULTS. OPS TEST OF LANDING GEAR SYSTEM GOOD . RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 18,814 hrs · 20,087 cycles

ON DEPARTURE, RIGHT MAIN GREEN LANDING GEAR LIGHT REMAINED ILLUMINATED GEAR CONFIRMED UP WITH DOORS CLOSED, DETEMINED WITH MAINTENANCE IT WAS AN INDICATION ISSUE. REMOVED FROM SERVICE. RELAMPED RT MLG GEAR LIGHT NO HELP. R/R LANDING GEAR CONTROL PANEL IAW 32-31-01-000/400-801. NO HELP STILL RT MAIN GREEN LANDING DOOR LIGHT STILL BRIGHT WHEN SW IS ON DIM. FUNCTIONAL TEST AMM TASK 32-21-01-720-801 LANDING GEAR CTRL PNL FUNCTIONAL CHECKED GOOD. REMOVED AND REPLACED ADVISORY CONTROL UNIT IAW AMM TASK 31-51-06-000/400-801 WITH NEW FROM STOCK. OPS CHECKED IAW AMM TASK 31-51-26-710-801. CHECKS GOOD. RT MLG LIGHT ON LANDING GEAR CONTROL PANEL NOW ILLUMINATES NORMALLY AS REQ'D. NO FURTHER DEFECTS NOTED. A/C OK FOR REUTRN TO SERVICE.

Part: BUMPER — DEFORMED (CABIN DOOR) · airframe 18,784 hrs · 20,055 cycles

THE MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. THE UPPER FINGER BUTTON WILL NOT DEPRESS ENOUGH TO GRAB THE HANDLE. REMOVED FROM SERVICE. ENSURED MCD CLOSES FULLY & INDICATES CLOSED & LOCKED. FERRIED AIRCRAFT. REPLACED DEFORMED BUMPER STOP AND CAP FOR MCD EXTERNAL ENTRY HANDLE. REF. AMM 52-11-11-400-801 STEP4H. OPS CHECKS GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FRAMES 69-90) · airframe 18,283 hrs · 19,452 cycles

TEMPORARY REPAIR FOR 2-OFF BLEND-OUTS ON LOWER FUSELAGE SKIN BETWEEN X-69.90-X-54.00 AND STR 31S-32S. NDT CARRIED OUT IAW RD84-53-9389 ISSUE 1 M. FUSELAGE SKIN BETWEEN X-69.00- X-54.00 AND STR 31S-32S REPAIRED IAW PERMANENT RD84-53-9389 ISS. 1.

Part: SEAT TRACK — CORRODED (BS 670-783) · airframe 18,283 hrs · 19,452 cycles

SEAT RAIL #16 FROM FSX670.00-X783.00, Y9.250 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT RAIL #16 FROM FSX 670.00 -X783.00 Y9.250 IAW SRM 51-42-05, 51-40-15, 51-41-05, 51-40-07.

Part: SEAT TRACK — CORRODED (BS 670-783) · airframe 18,283 hrs · 19,452 cycles

SEAT RAIL #9 FROM FSX670.00-X783.00, Y-9.250 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT RAIL #9 FROM FSX 670.00 -X783.00 Y-9.250 IAW SRM 51-40-07, 51-41-05, 51-40-15, 51-42-05.

Part: SEAT TRACK — CORRODED (BS 670-698) · airframe 18,283 hrs · 19,452 cycles

EQUIPMENT RAIL #23 FROM FSX670.00-X698.00 IS CORRODED THROUGH ON FWD FLOOR BOARD ATTACH HOLE. REMOVED AND REPLACED EQUIPMENT RAIL #23 FROM FSX 670.00 -X698.00 IAW SRM 51-41-05, 51-40-07, 51-42-05.

Part: SEAT TRACK — CORRODED (BS 571-670) · airframe 18,283 hrs · 19,452 cycles

SEAT RAIL #8 FROM FSX571.50-X670.00, Y-9.250 IS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED SEAT RAIL #8 FROM FSX 571.50 -X670.00, Y-9.250 IAW SRM 51-42-05, 51-41-05, 51-40-07, 51-40-15.

Part: STRINGER — CORRODED (BS 624-644) · airframe 18,283 hrs · 19,452 cycles

STRINGER 24P CORRODED BETWEEN FSX624.00-X644.00. STRINGER 24P REPLACED BETWEEN FSX 584.5 -X664.5 IAW 51-40-07-02-01, 51-41-05-00-01, 51-40-15-02-01, 51-25-80-02-01.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 18,283 hrs · 19,452 cycles

FWD PAX DOOR LOWER THRESHOLD CORRODED. FWD PAX DOOR LOWER THRESHOLD REMOVED AND REPLACED IAW SRM 51-42-05 AND 51-42-45.

Part: BEAM — CORRODED (EXIT THRESHOLD) · airframe 18,283 hrs · 19,452 cycles

SUSPECTED CORROSION ON EMERGENCY EXIT LOWER THRESHOLD BEAM. REPLACED LOWER THRESHOLD BEAM ON EMERGENCY EXIT DOOR IAW SRM 51-42-05. 51-42-45 AND 51-41-05.

Part: BEAM — CRACKED (PAX DOOR) · airframe 18,283 hrs · 19,452 cycles

AFT PASSENGER DOOR, #2 BEAM CRACKED BETWEEN FASTENER HOLES. REPLACED AFT PASSENGER DOOR #2 BEAM WITH NEW PART PN 85217419-105 IAW SRM 51-23-00-00-01, 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01, 51-42-45-02-01 AND 51-42-75-02-01.

Part: SEAT TRACK — CORRODED (NR 5) · airframe 18,283 hrs · 19,452 cycles

SEAT RAIL #5 FROM FSX-39.00-X102.50,Y-9.250 IS CORRODED IN SEVERAL PLACES. CORRODED SEAT RAIL #5 FROM X-39.00-X102.50. REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: DOUBLER — CORRODED · airframe 18,283 hrs · 19,452 cycles

LAV SERVICE PORT INTERNAL DOUBLER CORRODED BEYOND LIMITS. LAV SERVICE PORT INTERNAL DOUBLER REPLACED IAW SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 18,283 hrs · 19,452 cycles

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

Part: SEAT TRACK — CORRODED (NR 11) · airframe 18,283 hrs · 19,452 cycles

SEAT RAIL #11 FROM FSX10.50-X102.50,Y9.250 IS CORRODED BEYOND LIMITS. CORRODED SEAT RAIL #11 FROM FS X10.50- X102.50, Y9.250 REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: STRUT — CRACKED (NLG) · airframe 18,283 hrs · 19,452 cycles

REMOVED NOSE LANDING GEAR FOR SCHEDULED LIFE LIMIT. SENT TO VENDOR FOR REPAIRS. AT VENDOR, FOUND THE MOUNT FOR THE CENTERING ACTUATOR ON THE INNER SHOCK STRUT CYLINDER TO BE CRACKED. INNER SHOCK STRUT SCRAPPED.

Part: LIGHT — LOOSE (CABIN) · airframe 18,256 hrs · 19,422 cycles

EMERGENCY EGRESS LIGHT STRIP LOOSE IN FRONT OF TYPE II/III EMERGENCY EXIT. REMOVED FROM SERVICE. REINSTALLED EMERGENCY FLOOR PATH LIGHTING AT FWD EMERGENCY EXIT IAW AMM 33-51-16-400-801. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 17,983 hrs · 19,107 cycles

EMERGENCY FLOOR PATH LIGHTING STRIP AT ROW 2DE IS LOOSE. AIRCRAFT REMOVED FROM SERVICE. RE-SECURED EMERGENCY PATH LIGHTING STRIP AT 2DE. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (LANDING GEAR) · airframe 17,695 hrs · 18,771 cycles

LANDING GEAR TOOK AN EXCESSIVE AMOUNT OF TIME TO EXTEND ON APPROACH. UPON SELECTION OF GEAR DOWN THERE WERE NO ASSOCIATED SOUNDS OF A NORMAL GEAR EXTENSION. REMOVED FROM SERVICE. REPLACED LG CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — SLOW · airframe 17,691 hrs · 18,765 cycles

LANDING GEAR TOOK N 30 SECONDS TO EXTEND AFTER SELECTING GEAR HANDLE DOWN. REMOVED FROM SERVICE. CHECKED PSEU FOR CURRENT & HISTORICAL FAULTS FOR PREVIOUS LEG. NO FAULTS FOUND. COMPLIED WITH FUNCTIONAL TEST OF LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM. NO DISCREPANCIES NOTED. SWING GEAR 8 TIMES. NO FAULTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — DAMAGED (EMERGENCY EXIT) · airframe 17,485 hrs · 18,544 cycles

FOUND UPPER EMERGENCY EXIT DOOR GRAB HANDLE TO BE DAMAGE. REPLACED ACCESS COVER.

Part: DOOR SEAL — DAMAGED (CABIN DOOR) · airframe 17,273 hrs · 18,306 cycles

F/A REPORTS 6 TO 8 INCHES OF THE RUBBER SEAL AROUND THE DITCHING DAM ON THE MAIN CABIN DOOR MISSING. DEFERRED THE REPLACEMENT OF THE SEAL AND RETURNED THE AIRCRAFT TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 17,217 hrs · 18,237 cycles

EMERGENCY LIGHTING STRIP @ ROW 1 COMING LOOSE FROM FLOOR. REMOVED FROM SERVICE. RESECURED EMERGENCY LIGHTING STRIP NEXT TO SEAT 1B. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (ROW 2DE) · airframe 17,120 hrs · 18,122 cycles

EMERGENCY LIGHT STRIP WAS DETACHED AT ROW 2DE. SECURED THE LIGHT STRIP. RETURNED TO SERVICE.

Part: FAULT CODE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 16,211 hrs · 17,108 cycles

POWER PLANT MESSAGE DURING TAKE OFF ROLL, LESS THAN 60 KNOTS. REMOVED FROM SERVICE. INTERROGATED CDS FOR FAULTS, FOUND 130B & 134B ON THE NR 2 ENGINE. CLEARED FAULTS IAW FIM 61-20-03-810-815. FAULT CODE CLEARED AND DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — LOOSE (CARGO BAY) · airframe 16,186 hrs · 17,083 cycles

WHILE PERFORMING ARRIVAL CHECK FOUND MCD ENTRANCE WET FLOOR IN FRONT OF FWD INTERIOR BAG DOOR LOOSE CAUSING A TRIP HAZARD. APPLIED DOUBLE SIDED CARPET TAPE TO UNDERSIDE OF WET FLOOR IN FRONT OF FWD INTERIOR BAG DOOR AND RESEALED AREA WITH SEALANT.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 16,186 hrs · 17,083 cycles

WHILE PERFORMING ARRIVAL CHECK, FOUND THE EMERGENCY LIGHT STRIP IN FRONT OF PAX SEAT 2DE TO BE DAMAGED. REMOVED EMERGENCY LIGHT IAW AMM 33-61-16-000-801. INSTALLED A NEW EMERGENCY LIGHT IAW AMM TASK 33-51-16-400-801.

Part: LIGHT — LOOSE (ROW 2D) · airframe 16,061 hrs · 16,948 cycles

EMERGENCY LIGHT STRIP AT ROW 2D IS LOOSE. SECURED THE LIGHT STRIP. CHECKED GOOD. RETURNED TO SERVICE.

Part: HINGE — BROKEN (EMERGENCY EQUIP) · airframe 15,559 hrs · 16,428 cycles

EMERGENCY EQUIPMENT DOOR UNDER FWD FA JUMPSEAT DOESN'T RETRACT. REMOVED AND REPLACED BOTH SPRING ASSEMBLIES ON FWD FA SEAT EQUIPMENT DOOR AS REQUIRED. DOOR NOW SPRINGS CLOSED NORMALLY. NO FURTHER DEFECTS NOTED.RETURNED TO SERVICE.

Part: SEAL — DEFECTIVE (NR 2 PROPELLER) · airframe 14,723 hrs · 155,741 cycles

PROPELLER SLOW TO UNFEATHER, NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PROPELLER PISTON SEAL REF AMM 61-10-00-960-801. FAILED ENGINE LEAK CHECK. REMOVED SPINNER & CLEANED PROP ASSY. PERFORMED APPLICABLE ENG RUNS, REF MTC 6710006 AFTER REINSTALLING SPINNER. OPS & LEAK CHECKS GOOD. DETERMINED TO BE RESIDUAL. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN FLOOR) · airframe 14,684 hrs · 15,532 cycles

SEVERAL SECTIONS OF EMERGENCY LIGHTS IN MCD ENTRY AREA ARE LOOSE AND REQUIRE SECURING. SECURED THE LIGHT STRIPS.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 13,976 hrs · 14,800 cycles

FORWARD F/A EMERGENCY LIGHT CONTROL PANEL HAS A LIGHT OUT. RELAMPED THE FORWARD F/A EMERGENCY SWITCH LIGHT. CHECKS GOOD. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,249 hrs · 14,042 cycles

EMERGENCY LIGHT SWITCH NORMAL, LAMP NOT ILLUMINATED. RELAMPED LIGHT, ILLUMINATE PROPERLY. RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (COCKPIT) · airframe 13,136 hrs · 13,922 cycles

FLIGHT DECK DOOR CONTACTS LAV DOOR FRAME WHEN ACFT IS PRESSURIZED. WORKS FINE ON GROUND. REQUIRES FORCE TO OPEN IN FLIGHT. REMOVED 1 SHIM FROM TOP & BOTTOM HINGE IAW MCN 652629-001. REQUIRED CLEARANCE WERE PRESENT BETWEEN COCKPIT DOOR & LAV WALL. PRESSURIZED ACFT AMM 21-00-00-863-801 AND RECHECKED CLEARANCES STILL WITHIN LIMITS. OK FOR SERVICE.

Part: BUSHING — UNKNOWN (COCKPIT DOOR) · airframe 12,745 hrs · 13,494 cycles

AT 25,000 FEET, DIFFICULT TO OPEN FLIGHT DECK DOOR. WAS RUBBING AGAINST LAVATORY DOOR TRIM. REPLACED UPPER, MID AND LOWER HINGE BUSHINGS IAW AMM 52-51-01-710-801. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 12,636 hrs · 13,367 cycles

FLOOR PATH LIGHTING STRIP NEAR MAIN CABIN DOOR IN NOT SECURE. REATTACHED THE FLOOR PATH STRIP. RETURNED TO SERVICE.

Part: HINGE — LOOSE (LAV DOOR) · airframe 12,599 hrs · 13,327 cycles

COCKPIT DOOR RUBS ON THE LAVATORY DOOR MAKING IT DIFFICULT TO OPEN AND CLOSE COCKPIT DOOR. TIGHTENED THE LAVATORY DOOR HINGE MOUNT SCREWS. CHECKED THE BUSHINGS ON THE COCKPIT DOOR AND THE HINGE PINS. NO DEFECTS. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,554 hrs · 13,274 cycles

F/A EMERGENCY LIGHT SWITCH IS DIM. ACTION IS NORMAL. RELAMPED SWITCH, CHECKS GOOD. RETURN TO SERVICE.

Part: WIRE — CHAFED (ZONE 400) · airframe 12,506 hrs · 13,221 cycles

NR 1 PEC CAUTION, POWERPLANT MESSAGE ON ED, PROP 1 BETA SOL CB POPPED WHILE TAKING RUNWAY FOR TAKEOFF, POWER LEVERS WERE BELOW FLIGHT IDLE. TAKEOFF ABORTED. REMOVED 1 PEC CONNECTOR P20, CHECKED RESISTANCE OF GROUND BETA SOLENOID AND CIRCUIT PIN J TO J. COIL VALUE GOOD AT 58 OHMS. MANIPULATED HARNESS. NO CHANGE. RE-CONNECTED P20. REMOVED PEC AIRFRAME CONNECTOR P70, FOUND INTERMITTENT SOLID SHORT TO GROUND, .2 OHMS, AT PIN G WHILE MANIPULATING HARNESS INSPECTED HARNESS AND FOUND 2 CHAFED WIRES AGAINST BLEED AIR PRE-COOLER. REMOVED FIREWALL CONNECTOR P502 AND LOOSENED ALL ADEL CLAMPS BETWEEN P502 AND P70. 62200. REPLACED CHAFED WIRES IAW CMM 24-41-13 3542 5/21/16. RE-INSTALLED NR 1 PEC CHANNEL "A" HARNESS IAW MAINTENANCE 6710006. ALSO RAN NR 1 ENGINE AT VARIOUS POWER SETTINGS ABOVE AND BELOW FLIGHT IDLE GATE. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 12,502 hrs · 13,216 cycles

ON ROLLOUT THE NR 1 PEC CAUTION ILLUMINATED. INTERROGATED CDS FOUND FAULT CODE ON ENGINE NR 1 200 AB, 126B , 134B TRIED A PEC FAULT CLEAR FAULT REMAINS. COMPLIED WITH FIM TASK 61-20-05-810-817 FOR FAULT CODE 200AB ALL OTHER FAULTS CLEARED. FOUND CB G5 BETA SOL POPPED. RESET CB IAW GPM 9.2.2 AND CLEARED FAULT IAW AMM TASK 61-20-36-070-801. ALL FAULTS CLEARED AND DID NOT RETURN . GROUND RAN ACFT CYCLED PROPS FEATHER AND UNFEATHER MULTIPLE TIMES CB STAYED IN AND REMAINED SET. NO FAULTS PPLT NR 1 PEC MSG CLEARED AND DID NOT RETURN.

Part: BUSHING — WORN (RT MLG DOOR) · airframe 12,332 hrs · 13,036 cycles

INBD AND OTBD BUSHINGS WORN ON DUAL LUG BRACKET FOR RT MLG FWD DOOR CONNECTING RODS. REMOVED INBD AND OTBD BUSHINGS FROM DUAL LUG BRACKET ON RT MLG UPPER DRAG STRUT, FWD DOOR CONNECTING ROD ATTACH POINTS, IAW MLG DRESSED SHOCK STRUT CMM 32-11-03 FOR PN 46100, SECTION 10, C, 1 ON PAGE 642. INSTALLED INBD AND OTBD BUSHINGS ON DUAL LUG BRACKET ON RT MLG UPPER DRAG STRUT, FWD CONNECTING ROD ATTACH POINTS, IAW MLG DRESSED SHOCK STRUT CMM 32-11-03 FOR PN 46100, SECTION 10, C, 8-10 ON PAGE 643. CONTINUED WITH INSTALL OF INBD AND OTBD BUSHINGS ON DUAL LUG BRACKET ON RT MLG IAW MLG DRESSED SHOCK STRUT CMM 32-11-03, SECTION 10, C 11-15.

Part: HOUSING — DAMAGED · airframe 12,332 hrs · 13,036 cycles

GPU CONNECTOR HSG CASTING, PN 80080104, REQUIRES REPLACEMENT. GPU CONNECTOR HSG DOOR REMOVED REF SRM 51-41-00. GPU CONNECTOR HSG DOOR INSTALLED REF SRM 51-41-00. FASTENERS COMMON TO SKIN/STRINGER 11P, GPU HSG CASTING REMOVED REF SRM 51-42-05. CONTINUED REMOVAL OF GPU HSG CASTING, REF SRM 51-42-05. LOCATED AND DRILLED NEW GPU HSG CASTING, PN 80080104-S105A, REF SRM 53-10-55-02-02 AND DWG 85310014, REV BA 2009-06-01. INSTALLED NEW GPU HSG CASTING, PN 80080104-S105A, FASTENERS COMMON TO SKIN AND STIFFENER 10 AND STIFFENER 11, REF SRM 53-10-55-02-02 AND DWG 85310014, REV BA. CONTINUED INSTALLATION OF GPU HSG CASTING, PN 80080104-S105A, REF SRM 53-10-55-02-02 AND DWG 85310014, REV BA. COMPLIED WITH TASK CARD RD 8/4-53-7275/3. JOB 5435225, OP 54. RESTORED FINISH AROUND GPU CONNECTOR HSG AS NEEDED REF SRM 51-25-05, PG 206-207, ITEM F1-4.

Part: WEB — CORRODED (BS 728-735) · airframe 12,332 hrs · 13,036 cycles

AFT CARGO DOOR AREA, THE FLOOR WEB FROM APPROXIMATELY BS 728 TO 735, BETWEEN THE AFT CARGO DOOR SILL AND THE SEAT RAIL THERE ARE 3 SPOTS WITH EVIDENCE OF POSSIBLE CORROSION AND THE NUTPLATES UNDERNEATH SHOW EVIDENCE OF CORROSION, MARKED. REMOVED 2 EA RIVETS FROM FLOOR WEB REF SRM 51-42-05. INSTALLED 2EA RIVETS IN FLOOR WEB REF SRM 51-42-05. REMOVED CORROSION FROM FLOOR WEB AFT CARGO REF SRM 53-40-43 REPAIR 01 ON TOP SIDE ON STEP 7A 1. FINISHED BLENDING SHEER WEB AT BS 728, REF SRM 53-40-43 REPAIR 01. REMOVED 3 EA RIVETS FROM FLOOR WEB TO GAIN ACCESS TO CORROSION REF SRM 51-42-05. INSTALLED 3 EA RIVETS ON FLOOR WEB REF SRM 51-42-05. C/W ET/UT INSP REF NDTM 51-00-06 + 51-00-04. NO DEFECTS NOTED. MIN THICK=OTBD AREA IS .050", MIDDLE AREA IS .050" AND INBD AREA IS .033". MINIMUM REMAINING THICKNESS AT BLENDED AREA IS 0.033". MINIMUM ALLOWABLE IS 0.046". DAMAGE IS OUT OF LIMITS IAW SRM 53-40-43-02-01. RECEIVED FROM ENGINEERING RD 8/4-53-7405, ISSUE 1. RECEIVED AND COMPLIED WITH TASK CARD RD 8/4-53-7405. COMPLIED WITH FORM M-184. FABRICATED REPAIR DOUBLER FROM 2024T3 .071" PO; T32393, LOCATED AND DRILLED IAW R/D 8/4-53-7405, ISSUE 1. COMPLIED WITH STEP 4 OF RD 8/4-53-7405, ISSUE 1. FILLED, CURED, SANDED AND DRILLED HYSOL EA934NA EPOXY. INSTALLED REPAIR DOUBLER AND SHEAR WEB PACKER REF RD 8/4-53-7405, ISSUE 1. FILLET SEALED AND RESTORED FINISH TO FLOOR WEB AND REPAIR DOUBLER REF RD 8/4-53-7405, ISSUE 1.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 12,332 hrs · 13,036 cycles

DENT ON THE LT WING LOWER FLAP SHROUD SKIN AT YW244 8" L X .75" W. 53.25" OTBD OF LT NACELLE. REMOVED DAMAGED AREA, REF RD8/4-57-3137, GENERAL NOTES 1 AND 2, ISSUE 1. C/W ET INSP IAW RD 8/4-57-3137, ISSUE 1. NO DEFECTS NOTED. FABRICATED PATCH AND PACKER IAW RB 8/4-57-3137 FROM SHEET 2, 2024T-3 0.040"/0.050" PO: T000024927 AND PO: TX00004337/1 ISSUE 1. THIS CLEARS DMI 711433, PERMANENT REPAIR HAS BEEN ACCOMPLISHED IAW RD 8/4-57-3137. PATCH AND PACKER INSTALLED IAW RD 8/4-57-3137, ISSUE 1. FILLET SEALED REPAIR AREA IAW SRM REF 51-23-00. PRIMER APPLIED TO AREA IAW SRM REF 51-25-10-02-01. PAINTED AREA IAW SRM REF 51-25-15-02-01. RECEIVED TC FOR RD8/4-57-3137. COMPLIED TC RD8/4-57-3137.

Part: PANEL — CRACKED (RT WING) · airframe 12,332 hrs · 13,036 cycles

RT WING INBD L/E PANEL 611AR CRACKED OTBD CLOSING RIB PN 85720252-104. DISBONDED DE-ICING BOOT AT OTBD CLOSING RIB LOCATION ON INBD L/E PANEL 611AR REF SRM 57-40-00-02-06. REINSTALLED DE-ICING BOOT AT OTBD CLOSING RIB REF SRM 57-40-00, REPAIR NR 6. CUTOUT DAMAGE AT UPPER AND LOWER SECTION OF OTBD CLOSING RIB ON INBD L/E PANEL 611AR REF SRM 57-40-00-02-07. C/W ET INSP REF A400 NDTM 51-00-06. NO DEFECTS NOTED. FABRICATED QTY 2 REPAIR ANGLES AND QTY 2 TAPERED SHIMS FROM 2024T3, .050", PO: TX4337/1 AND QTY 2 FILLERS FROM 2024T3, .032", PO: TX2606/1 FOR UPPER AND LOWER REPAIR. LOCATED AND DRILLED REF SRM 57-40-00-02-07. INSTALLED UPPER & LOWER REPAIR PARTS REF SRM 57-40-00, REPAIR NR 7. INSTALLED NEW SILICONE SEAL REF AMM 57-13-01-400-801 AND AMM 51-21-26-340-801, ON L/E PANEL 611AR. PERFORMED "CURE CHECK" OF THE BULB SEAL ON OTBD END OF DEICING BOOT PANEL 611AR "CURE CHECK GOOD".

Part: SKIN — CRACKED (LT WING) · airframe 12,332 hrs · 13,036 cycles

LT WING INBD L/E PANEL 511AL CRACKED INBD CLOSING RIB. CUTOUT THE DAMAGE AT 2 LOCATIONS, UPPER AND LOWER FLANGES OF INBD CLOSING RIB ON L/E 511AL IAW SRM 57-40-00-02-07. C/W ET INSP REF NDTM 51-00-06. FABRICATED REPAIR ANGLE AND TAPERED SHIM FROM 2024T3 .050", PO TX 4337 /1 AND FILLER FROM 2024T3, .032" PO: TX 2606/ 1. LOCATED AND DRILLED FOR LOWER RIB REPAIR REF SRM 57-40-00-02-07. FABRICATED REPAIR ANGLE AND TAPERED SHIM FROM 2024T3, .050", PO: TX4337 /1. AND FILLER FROM 2024T3, .032" PO: TX 2606/1. LOCATED AND DRILLED FOR UPPER RIB REPAIR REF SRM 57-40-00-02-07. INSTALLED UPPER AND LOWER REPAIR ANGLES, TAPERED SHIMS AND FILLERS AT UPPER AND LOWER CLOSING INBD RIB REF SRM 57-40-00-02-07. INSTALLED NEW SILICONE SEAL, PN N316-8012, REF AMM 57-13-01-400-801, SUBTASK 57-13-01-420-001, A3, A, B.

Part: SEAT TRACK — CORRODED · airframe 12,332 hrs · 13,036 cycles

SEAT TRACK NR 10 REQUIRES REPLACEMENT, PN 85328210-121. REMOVED GROUND WIRE FROM SEAT TRACK NR 10 BETWEEN BS 34.1 TO BS 18.25 REF SRM 51-41-00. INSTALLED GROUND WIRE ON SEAT TRACK NR 10 AND CARRIED OUT BOND CHECK GOOD, REF SRM 51-80-00. DISPLACED 5 EA WIRE BUNDLE BETWEEN BS-18.25 TO BS 1.00, REF WM 20-12-10 3 D. INSTALLED QTY 5 WIRE BUNDLE BETWEEN BS-18.25 TO BS 1.00 REF WM 20-12-10 3 D. REMOVED KICK PLATE ON BULKHEAD AT ST.-39.10, PN 85311097-001, REF SRM 51-42-45, REPAIR-01. INSTALLED KICKPLATE, PN 85311097-001 AT FS X-39.00 REF SRM 51-42-45-02-01. REMOVED SET TRACK NR 10, PN 85328210-121, REF SRM 51-42-05. INSTALLED SEAT TRACK NR 10 REF DWG: 85328201, REV E. LOCATED AND DRILLED SEAT TRACK NR 10 REF DWG 85328201, REV E. LOCATED AND DRILLED SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11 REF SRM 51-40-07 AND DWG 85328201, REV E. INSTALLED SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11 REF DWG 85328201, REV E.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,332 hrs · 13,036 cycles

SEAT TRACK NR 11 CORRODED. REMOVED SEAT TRACK IAW SRM 51-42-05. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-07 AND DWG 8Z4851, REV B. INSTALLED OF SEAT TRACK IAW DWG 85328201, REV E.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 11,529 hrs · 12,183 cycles

DURING LAST PART OF CRUISE FLIGHT, NR 2 HYD PUMP CAUTION ILLUMINATED. ASSOCIATED CHECKLISTS COMPLETE. THEN ON APPROACH NR 2 SYSTEM HYD QTY FELL FROM 1/3 TO ZERO. IT HAD BEEN STAYING STEADY APPROACH DISCONTINUED WITH ADDITIONAL CAUTION LIGHTS NR 2 HYD PRESS, NR 2 RUD HYD, AND PTU FAIL ALSO SHOWS THE ROLL SOILER OTBD, AND OTBD SPOILER CAUTION ILLUMINATED WHEN BELOW 165KTS. MANUAL GEAR EXTENSION REQUIRED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INSP AND FOUND NR 2 EDP ROTATING GROUP FAILED. R & R 2 EDP IAW AMM TASK 29-11-01-000-801, 29-11-01-400-801 AND MCN 5114929232/1. COMPLIED WITH AMM TASK 05-54-00-280-801. COMPLIED WITH SIMPLIFIED FLUSH OF NR 2 HYD SYS IAW TR 29-188, AMM TASK 29-10-00-617-803, PARA C. EDP OPS CHECK GOOD. NO LEAKS NOTED.

Part: AIR FILTER — ODOR (CABIN) · airframe 11,179 hrs · 11,812 cycles

F/A REPORTS FUEL ODOR IN CABIN ROWS 12 AND AFT, STRONGER AFT ON CLIMBOUT. ODOR DISSIPATED DURING THE FLIGHT. C/W AIR CONTAMINATION CHECK LIST FORM 744. NO FUEL AND OIL ODOR NOTED, ARRIVAL AT GATE. INSPECTED AFT CARGO. NO OIL, FUEL ODOR NOTED. INSPECTED NR 1 & NR 2 ENGINE FOR LEAK. NO LEAK NOTED. FOUND NR 2 ENGINE OIL LEVEL AT JUST ABOVE MAX HOT LINE. REMOVED APPROXIMATELY 480 MIL OIL FROM NR 2 ENGINE. NOW OIL LEVEL IS BETWEEN MAX HOT LINE AND ADD 1 QUART LINE. GROUND RUN NR 1 & NR 2 ENGINE IN RATING WITH INDIVIDUAL BLEED AND RECIRCULATING FAN OFF AND ON. NO ODOR NOTED IN CABIN. C/W TROUBLESHOOTING COMMON SMELLS IN ACFT REF FIM MCN 62172-01 ISSUE NR 2, STEP 2A. C/W NR 1 & NR 2 ENGINE SMOKE OR OILY ODOR OR MIST IN THE CABIN FAULT ISOLATION REF FIM 71-00-00-810-817 PAR 1-4A(1). NO CABIN CONTAMINATION NOTED. R & R RECIRCULATION FILTER REF AMM TASK 21-22-22-000-801, 21-22-22-400-801. CLEANED NR 1 & NR 2 ENGINE NACELLE SHUTOFF VALVE FILTER REF AMM TASK 36-11-00-100-801. NO OTHER DEFECT NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (FWD CABIN) · airframe 10,947 hrs · 1,567 cycles

RAMP AND CREW REPORTS A " FISHY ODOR IN THE FORWARD CABIN AND AFT CARGO BAY, RAMP REPORTS RECENT FLIGHTS HAVE CARRIED FROZEN FISH IN CARGO BAYS. UPON ENTERING THE AC NOTICED FOUL, FISHY LIKE ODOR THAT APPEARED TO BE STRONGER IN THE REAR OF THE AC. INSPECTED FWD LAV TO INCLUDE TOILET & GARBAGE, INSPECTED FWD F/A BS & GARBAGE AREA, INSPECTED AFT GALLEY AREA TO INCLUDE ALL BINS, CUPBOARDS AND GARBAGE CANS. INSPECTED ALL SEATS, FLOORS AND LITERATURE POCKETS FOR THE PRESENCE OF ANYTHING THAT MIGHT BE THE CAUSE OF THE ODOR. THERE WERE NO OBVIOUS SIGNS OF ANYTHING THAT WOULD CAUSE SUCH ODOR. INSPECTED FWD CARGO HOLD AND FOUND NOTHING, INSPECTED AFT CARGO HOLD AND FOUND OBVIOUS SIGNS HOWEVER ODOR APPEARED STRONGER THERE. INBD CREW REPORTED A OFFLOAD OF FISH BUT FISH ODOR HAD BEGUN PREVIOUSLY 46519 8-26-15. REF, MCN. 62172-01, ISSUE NR 2 FOR TROUBLESHOOTING COMMON ODORS IN THE ACFT. REMOVED AND REPLACED RECIRCULATION FILTER IAW AMM TASKS 21-22-22-000-801, 21-22-22-400-801. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BYPASS VALVE — FAILED (NR 2 OIL SYSTEM) · airframe 10,893 hrs · 11,506 cycles

ON CLIMB NR 2, OIL TEMP WAS AT 107, IAW CHECK LIST STARTED CLOCK AT 10 MINS TEMP WAS 121, IAW CK LIST, SHUTDOWN NR 2 ENGINE AND RETURN TO DEPARTURE. LANDING WEIGHT 61,900. LANDING UNEVENTFUL. REPLACED OIL COOLER BYPASS VALVE, MAIN & SCAVENGE FILTER + C/W OIL CHANGE. RETURNED TO SERVICE.

Part: SKIN — DENTED (PAX DOOR) · airframe 10,526 hrs · 11,076 cycles

RAMP AGENT NOTICED A DENT IN THE MAIN CABIN DOOR UPON ARRIVAL. REPLACED THE MAIN CABIN DOOR OUTER SKIN IAW AMM TASK 52-11-06-000-801 AND 52-11-06-400-801. RETURNED TO SERVICE.

Part: BULB — WRONG PART (CARGO BAY) · airframe 10,129 hrs · 10,640 cycles

ODOR REPORTED IN THE AFT CARGO COMPARTMENT. FOUND THE AFT CARGO COMPARTMENT FORWARD LIGHT VERY HOT. FOUND FORWARD LIGHT ASSY IN AFT CARGO COMPARTMENT HAD HIGH WATTAGE LIGHT BULB. R & R LIGHT ASSY AND BULB IAW AMM, TASK 33-31-00-000-801 AND 33-31-01-400-801 AND MCN NR 63331-01. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 9,493 hrs · 9,971 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND THE MAIN CABIN DOOR UPPER FORWARD WEATHER SEAL DAMAGED AND SEPARATED FROM THE ACFT. CLEANED & INSPECTED MCD UPPER WEATHER SEAL. NO DAMAGE NOTED AFTER CLEANING. INSTALLED SEAL IAW AMM 53-20-19-400-801. OK FOR CONTINUED SERVICE.

Part: SWITCH — BROKEN (EMERGENCY LIGHTS) · airframe 8,839 hrs · 9,281 cycles

EMERGENCY LIGHT SWITCH ON F/A PANEL IS BROKEN. SWITCH STAYS STUCK IN WHEN PRESSED. R & R FWD F/A EMERGENCY LIGHT SWITCH, OPS CHECK GOOD. AMM REF 33-51-05-000-801 AND 33-51-05-400-801. RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 8,610 hrs · 9,032 cycles

VERTICAL EMERGENCY EXIT LIGHT INOPERATIVE . FOUND CONNECTOR DISCONNECTED. SECURED THE CONNECTOR AND PERFORMED AN OPS CHECK IAW TASK CAR 335000202-60045. CHECKED GOOD.

Part: BRAKE SYS — MALFUNCTIONED · airframe 7,753 hrs · 8,130 cycles

BRAKES GRABBED AND CAUSED YAW TO RIGHT ON LANDING. POSTFLIGHT WALKAROUND SHOWED BRAKES TOO HOT TO TOUCH ON RT SIDE AND BRAKES COLD TO THE TOUCH ON LT SIDE, BOTH. ACCOMPLISHED GVI, NO DESCREPANCIES NOTED PRESSURIZED SYSTEM NR 1, BLED NR 1 & NR 2 BRAKES REF MM 32-44-00. TAXIED ACFT WHILE DEPRESSING BRAKES, APPLIED PARKING BRAKE NO PULLING TO RT NOTED. BRAKES ALL READ SAME TEMPS. NOTE; ONLY MINIMAL SPEEDS, AS20650. REMOVED ACESS PANEL AND INSPECTED BRAKE CONTROL VALVE FOR FLUID BYPASS. DISCONNECTED LT CABLE FROM CONTROL VALVE ACTUATED VALVE AND NO BYPASS WAS DETECTED. RECONNECTED LT CABLE TO VALVE SAFETIED AND REINSTALLED PANEL REF 32-42-06, 29-00-00 AS07991 NOTE FOR CABLE REMOVAL INSTALLED CABLE BLOCK AND REMOVED CABLE BLOCK AS07991.

Part: LIGHT — UNSECURE (CABIN) · airframe 7,548 hrs · 7,890 cycles

CABIN EMERGENCY LIGHT NEAR ROW 17 IS UNSECURE. SECURED FLOOR LIGHT. RETURNED TO SERVICE.

Part: RELIEF VALVE — MALFUNCTIONED (ZONE 100) · airframe 7,282 hrs · 7,606 cycles

ENROUTE INBD ROLL SPOILER AND NR 1 HYD ISO CAUTION FOLLOWED BY LOSS OF FLUID AND PRESSURE ON NR 1 HYD SYSTEM. RETURNED TO FIELD, LANDING UNEVENTFUL. PERFORMED GVI OF FUSELAGE EXTERIOR, NACELLE INTERIORS AND EXTERIORS AND ACM COMP. FOUND NR 1 HYD RESERVOIR INDICATING ZERO QTY. NO OTHER DEFECT OR EVIDENCE NOTED. SERVICED NR 1 HYD SYS RES IAW AMM 12-10-29-611-801. RAN NR 2 ENG AND STBY PUMP AND OBSERVED FLUID LEAKAGE FROM NR 1 HYD BALANCE RELIEF VALVE DRAIN HOLE. REMOVED PANEL 262BT. REPEATED GROUND RUN AND OBSERVED FLUID LEAKAGE FROM BALANCE RELIEF VALVE DRAIN LINE. BEGAN INSP OF EDP AFTER OPERATION WITHOUT SUFFICIENT FLUIED IAW AMM 05-54-00-280-801 1-5A (1) (A) AND (2)-(6)(A). REF AML FOR DMI ON REINSPECT OF FILTERS AND DPIS. C/W 025-54-00-280-801 5A (B) AND 5 A6 (B) - CLOSE OUT. NO QTYS OF METALLIC PARTICLES FOUND. R+R BALANCE RELIEF VALVE IAW AMM 29-11-51-000-801 AND 29-11-51-400-801, PARA 1-4A, 12 AND PARA 5. CLOSED PANEL 262BT.

Part: BEARING — FAILED (MLG) · airframe 7,196 hrs · 7,515 cycles

AFTER LANDING AND DURING TAXI IN, F/A'S NOTIFIED US THAT SPARKS AND SMOKE FROM RT SIDE MAIN TIRES. RT OUTSIDE TIRE WAS FOUND FLAT BUT INTACT. R & R NR 2 MLG AXLE IAW MM TASK 32-11-04-000-801 AND 32-11-04-400-01. R & R NR 3 AND NR 4 MAIN WHEEL AND BRAKE ASSEMBLIES IAW MAINTENANCE 6324201 AND 6324101. REPLACED NR 4 BRAKE FLEX HOSE IAW MM 32-42-26-000-801 AND 32-42-26-400-801. COMPLIED WITH MM TASK 05-50-61-210-801 FOR TIRE FAILURE. COMPLIED WITH MM TASK 05-50-17-210-801 FOR NR 4 WHEEL BEARING FAILURE. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BEAM — CORRODED (AFT SERVICE DOOR) · airframe 7,167 hrs · 7,483 cycles

AFT SERVICE DOOR EDGE BEAM, FOUND CORRODED. REMOVED EDGE BEAM IAW SRM 51-42-15. INSTALLED EDGE BEAM IAW SRM 51-42-15 PARA 1-5F.

Part: CHANNEL — CORRODED (PAX DOORWAY) · airframe 7,167 hrs · 7,483 cycles

LT FWD PAX DOOR CHANNEL ASSY FOUND CORRODED. REMOVED CHANNEL FROM PASSENGER DOOR SURROUND IAW SRM 51-42-05, STEP 4E (2-8). INSTALLED CHANNEL AT PAX DOOR IAW SRM 51-42-05, STEP 4-D (3-10). LOCATED, DRILLED AND DEBURRED NEW CHANNEL ASSY IAW SRM 51-40-07.

Part: BEAM — CORRODED (PAX DOORWAY) · airframe 7,167 hrs · 7,483 cycles

AFT PAX DOOR LT EDGE BEAM FOUND CORRODED. DRILLED AND FITTED NEW EDGE BEAM IAW SRM 51-40-07. INSTALLED NEW EDGE BEAM IAW SRM 51-42-05, STEP 4, D, 1 THRU 7 AND 51-42-45.

Part: BEAM — CORRODED (EMERGENCY EXIT) · airframe 7,167 hrs · 7,483 cycles

CORROSION ON EDGE BEAM OF EMERGENCY EXIT DOOR HAD EXCESSIVE CORROSION. REMOVED EDGE BEAM IAW SRM 51-42-05. INSTALLED NEW EDGE BEAM IAW SRM 51-42-05.

Part: RELAY — MALFUNCTIONED (TIME DELAY) · airframe 6,410 hrs · 6,679 cycles

"FAIL" LIGHT ON PTU CONTROL SWITCH UNTIL TAXI IN. FAIL LIGHT WAS ON WHEN PTU SWITCH WAS ON. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED RELAY 2-K1. FUNCTIONAL CHECKED NORMAL. RETURNED TO SERVICE.

Part: DISPLAY — FAILED (ZONE 200) · airframe 6,364 hrs · 6,627 cycles

NR 1 ARCDU FAILED IN FLIGHT, CAUSING NR 1 COMM PROBLEMS. RETURNED TO FIELD AND ACCOMPLISHED UNEVENTFUL LANDING. R & R NR 1 ARCDU IAW T/C 6238101. OPS CHECK GOOD. ACFT REMAINS CAT III AND PLACARD IN COCKPIT READS CAT III STATUS. ARCDU WAS REPLACED AS PRECAUTIONARY MEASURE. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PTU) · airframe 5,821 hrs · 6,079 cycles

PTU WHEN SELECTED ON INDICATED FAIL WITH NO GREEN LIGHT ON. NO RELATED FAULTS IN CDS. COMPLIED WITH FIM TASK 29-30-00-810-819. PTU SYS OPERATED NORMALLY. FAIL LIGHT ON HYD CONTROL PANEL DID NOT ILLUMINATE. COMPLIED WITH FUNCTIONAL TEST OF THE POWER TRANSFER UNIT IAW TASK AMM 29-11-61-720-801. TESTED GOOD. ACFT OK FOR CONTINUED SERVICE.

Part: WIRE HARNESS — BROKEN (PROP DEICE) · airframe 5,037 hrs · 5,238 cycles

PROPELLER DE ICE CAUTION LIGHT CYCLED WITH THE NR 2 PROP DE ICE. RAN CHECKLIST AND CONTINUED TO GET CAUTION LIGHT WITH NR 2 PROP DE ICE CYCLING. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS & FOUND "OPEN PHASE B&C ON TMCU 2". PERFORMED ELECTICAL CONTINUITY CHECK OF NR 2 PROP DE ICE IAW TASK 30-61-00-760-801. FOUND PROP DE ICE WIRE HARNESS AT NR 2 BLADE OPEN. REPLACED NR 2 BLADE WIRE HARNESS IAW TASK 61-10-06-400-805 TEMP, REV 61-111. PERFORMED FUNCTIONAL TEST IAW TASK 30-61-00-720-802, NO DEFECTS NOTED. CDS FAULTS DID NOT RETURN. RETURNED TO SERVICE.

Part: HANDLE — DIRTY (PAX DOOR) · airframe 4,764 hrs · 4,952 cycles

F/A REPORTS THAT THE AFT PASSENGER DOOR COULD NOT BE OPENED FROM THE OUTSIDE. F/A OPENED FROM THE INSIDE. CLEANED THE HANDLE FOR THE AFT PASSENGER DOOR. RETURNED TO SERVICE.

Part: SEAL — DIRTY (GALLEY DOOR) · airframe 4,764 hrs · 4,952 cycles

F/A REPORTS THAT THE GALLEY SERVICE DOOR COULD NOT BE OPENED FROM THE OUTSIDE. FROM THE INSIDE WORKS FINE. CLEANED THE GALLEY DOOR SEAL AND RETURNED TO SERVICE. NO PARTS REPLACED.

Part: COVER PLATE — LOOSE (EMERGENCY EXIT) · airframe 4,317 hrs · 4,469 cycles

COVER PLATE OVER EMERGENCY EXIT LOOSE. ATTACHED COVER PLATE OVER EMERGENCY EXIT. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED (AILERONS) · airframe 4,186 hrs · 4,334 cycles

AT 2000 FT ON FINAL, AUTOPILOT OFF, MADE LT WING DOWN AILERON TRIM INPUT. AILERON TRIM CONTINUED TOWARDS FULL LT WING DOWN. PRESSED RT WING DOWN SIDE OF SWITCH, MOVEMENT STOPPED, THEN TRIMMED BACK TO LEVEL FLIGHT. LANDING UNEVENTFUL. COULD NOT DUPLICATE, NO CDS MESSAGES FOUND. AS A PRECAUTIONARY MEASURE R & R AILERON & RUDDER TRIM CONTROL PANEL IAW AMM TASK 27-13-16-000-801, 27-13-16-400-801. OPS TESTED GOOD, ACFT OK FOR CONTINUED SERVICE.

Part: AXLE — DAMAGED (LT MLG) · airframe 2,898 hrs · 2,993 cycles

ON LANDING, BRAKES WERE VERY WEAK. ON POST FLIGHT INSPECTION, FOUND LT MAIN INBD TIRE ASSY AT A 20 DEG ANGLE TO THE GEAR LEG. ALSO FOUND BRAKE PADS SEPARATED FROM BRAKE ASSY. REPLACED NR 1 MLG AXLE REF AMM TASK 32-11-04-400-801. ALSO, REPLACED WHEELS AND BRAKES, RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 2,761 hrs · 2,839 cycles

ON CLIMBOUT, NOTICED THE FUEL OPEN VALVE LIGHT WAS ILLUMINATED ON THE APU FIRE PROTECTION PANEL. THE APU HAD NOT BEEN USED. PULLED AND RESET CIRCUIT BREAKER APU SOV L3. C/W FIM FAULT ISOLATION FIRE PROTECTION PANEL FUEL OPEN LIGHT IN THE APU AREA IAW FIM 26-23-00-810-807, PAR 1-3A1 (A). OP'S CHECKED GOOD. NUMERIOUS TIME POWER ON AND OFF APU SOV OPEN AND CLOSED NORMAL. NO DEFECT NOTED AT THIS TIME. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONNECTOR — BURNED (ZONE 200) · airframe 2,657 hrs · 2,735 cycles

ELECTRIC ODOR NOTICED IN AFT GALLEY WHEN AFT PAX DOOR WAS CLOSED AFTER DE-PLANNING. INSPECTED AND FOUND RT ELECTRICAL CONNECTOR TO HAVE EVIDENCE OF GETTING HOT AND SMELLS BURNED. R & R THE ELECTRICAL CONNECTOR, CHECKED GOOD. NO ABNORMAL ODORS NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,166 hrs · 2,233 cycles

AFT F/A ADVISES A STRONG ODOR ELECTRICAL NEAR AFT GALLEY AREA. RAN BOTH ENGINES WITH PACS ON. OPERATED ALL GALLEY APPLIANCES. NO ODOR NOTED COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.