N443QX

Part: CONTROLLER — FAILED (ZONE 200) · airframe 24,162 hrs · 26,243 cycles

AIRCRAFT DID NOT PRESSURIZE CLIMBING OUT OF PSC. A FEW MINUTES LATER FA REPORTED MAIN CABIN DOOR WAS NOT SEALING AND VERY LOUD. ON FINAL, FA SAID THAT DOOR DID APPEAR TO SEAL UP. REMOVED FROM SERVICE. FOUND EXCESS MOISTURE AROUND PAX DOOR SEAL. CLEANED PAX DOOR SEAL AND PRESSURIZED. CABIN PRESSURIZED NORMALLY. DURING DEPRESSURIZATION, FAULT LIGHT ILLUMINATEED ON CP PANEL. PRESSURIZED AGAIN AND SAME THING HAPPENED. CDS SHOWED CP CONTROLLER FAIL. R&R CP CONTROLLER, REF AMM 21-31-06-000/400-801. OPS TEST GOOD. AIRCRAFT CABIN PRESSURIZED/DEPRESSURIZED NORMALLY DURING BOTH ATTEMPTS, REF AMM 21-00-000-863-801, 21-00-00-863-802. RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,155 hrs · 26,232 cycles

F/A REPORTS THAT THE EMERGENCY LIGHT SWITCH BACKLIGHTING IS INOP. REMOVED FROM SERVICE. RELAMPED EMERGENCY LIGHT SWITCH. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (ZONE 200) · airframe 24,132 hrs · 26,199 cycles

#1 PROP FAILED PROP OVERSPEED GOVENOR TEST. REPLACED OFF SWITCH IAW AMM 31-31-03-960-801 C/W OPERATIONAL TEST OF PROP OVERSPEED GOVERNOR IAW AMM 61-20-00-710-803 NO DEFECTS NOTED.

Part: TUBE — OBSTRUCTED (EXTINGUISHER) · airframe 24,018 hrs · 26,047 cycles

LAVATORY COMPARTMENT WASTE CONTAINER FORE EXTINGUISHER DISCHARGE TUBES ARE BLOCKED BY SEALANT. CLEARED DISCREPANCY.

Part: NONE — NONE · airframe 23,792 hrs · 25,736 cycles

FLAP POWER CAUTION LIGHT FLAP STOPPED BETWEEN 10" AND 15" AFTER TAKE OFF. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W FIM TASK 27-50-00-810-802 FLAP PWR CAUTION.PERFORMED RESET FLAP POR AND CHECKED CDS FOR FAULTS.NO FAULTS FOUND.PERFORMED OPS TEST OF WING FLAPS.OPS CHECKS GOOD.NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: FIRE DETECTOR — FALSE INDICATION · airframe 23,221 hrs · 25,096 cycles

SMOKE WARNING ILLUMINATED AT GATE FOR AFT CARGO. CARGO DOOR WAS OPEN AND EMPTY. REMOVED FROM SERVICE. CLEANED SMOKE DETECTORS IN AFT CARGO. PERFORMED OPS EST OF THE BAGGAGE SMOKE DETECTORS IAW Q400 AMM 26-12-06-710-801. OPS TEST GOOD. SMOKE WARNING STAYS OFF AFTER THE TEST. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE · airframe 23,164 hrs · 25,031 cycles

EXTERIOR LIGHT AT AFT CABIN PASSENGER DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED ON. REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM TASK 33-51-00-710-802. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 22,928 hrs · 24,769 cycles

LDG INOP CAUTION CAME ON IN CRUISE. PERFORMED CHECKLIST AND DECLARED EMERGENCY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PLACED LANDING GEAR RETRACTION SYSTEM ON MEL 32-30-1 ( LANDING GEAR RETRACTION SYSTEM ),

Part: WARNING LIGHT — FALSE ACTIVATION (GENERATOR) · airframe 21,741 hrs · 23,533 cycles

ON DECENT THE FO NOTICED THE #1 & #2 AC GEN CAUTION LIGHT FLICKERING, AS WELL AS THE MASTER CAUTION LIGHT. REMOVED FROM SERVICE. FOUND FAULT CODE 28 "#2 AC GCU" IN EPCU. COMPLIED WITH Q400 FIM TASK 24-21-06-810-802, PARA 1 THRU 3.D. OPS TEST OF AC GEN SYSTEM IAW Q400 AMM 24-24-00-710-801 IS GOOD. FAULT CODE DID NOT RETURN. OKAY FOR SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (DE ICE SYSTEM) · airframe 21,440 hrs · 23,228 cycles

DEICE PSI CAUTION ENROUTE IN CLOUDS. FOLLOWED E&A CHECKLIST ON PG 12.4 AFTER SELECTING MANUAL & THEN RETURNING BACK TO SLOW SETTING, CAUTION EXTINGUISHED & REMAINED OFF. NO OTHER ABNORMALITIES. REMOVED FROM SERVICE. C/W FIM TASK 30-10-00-810-801 PERFORMED FUNCTIONAL TEST OF THE AIRFRAME DE-ICE SYSTEM IAW AMM 30-11-00-720-801 OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR ACTUATOR — MALFUNCTIONED (ZONE 400) · airframe 20,990 hrs · 22,785 cycles

#1 ENGINE INTAKE BYPASS DOOR REMAINS CLOSED WHEN SWITCH IS PRESSED TO OPEN. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. VERIFIED INTK DEF ACT 1 CB (P6) WAS IN. DEPRESSED #1 ENG. INTAKE BYPASS DOOR SWITCH. CLOSED LIGHT REMAINED ILLUMINATED AND BYPASS DOOR REMAINED CLOSED. J.A. 3493. REMOVED #1 ENGINE INTAKE BYPASS DOOR ACTUATOR IAW DASH 8 Q400 AMM 71-61-06-000-801. INSTALLED SERVICEABLE BYPASS DOOR ACTUATOR, IAW DASH 8 Q400 AMM 71-61-06-400-801, PARA 1-5E. E.A. 3510. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (NR 1 OVERSPEED) · airframe 20,642 hrs · 22,408 cycles

NR 1 PROPELLER TOOK =35 SEC TO UNFEATHER ON START UP. REMOVED FROM SERVICE. REPLACED OVERSPEED GOVERNOR ON NR 1 ENGINE, IAW Q400 AMM TASK 61-20-26-000-801 AND 61-20-26-400-801. OPERATIONS TEST GOOD, NO FURTHER DEFECTS NOTED. PERFORMED FUNCTIONAL TEST OF PROP TIME TO UNFEATHER, IAW Q400 AMM TASK 61-20-00-720-802. FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (NR 1) · airframe 20,637 hrs · 22,403 cycles

NR 1 PROP WAS SLOW TO UNFEATHER ABOUT 10-15 SECONDS LONGER THAN NR 2. NR 1 PROP DID NOT COMPLETELY FEATHER WHEN SHUTDOWN. REMOVED FROM SERVICE. PERFORMED FUNCTIONAL TEST OF TIME TO UNFEATHER, IAW Q400 AMM TASK 61-20-00-720-802 AND THE AUTOFEATHER TEST IAW Q400 AMM TASK 61-20-00-710-810. ALL TIMES GOOD, TESTS PASSED. NR 1 PROPELLER FULLY FEATHER AFTER SHUTDOWN. RETURNED TO SERRVICE.

Part: PROPELLER — MALFUNCTIONED (FEATHERING) · airframe 20,629 hrs · 22,390 cycles

DURING MTX TAXI, NR 1 PROP FAILS TO UNFEATHER, ATTEMPTED TO UNFEATHER 5 TIMES NO HELP. C/W FIM 61-20-00-810-803 PARA 1-5A (5),6. C/W FUNCTIONAL TEST OF THE NR 1 PROPELLER TIME TO UNFEATHER CHECK, NO DEFECTS NOTED (17 SEC) TWO TIMES. UNFEATHER TEST WAS, IAW AMM 61-20-00-720-802. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HINGE — DAMAGED (EMER EQUIP DOOR) · airframe 20,147 hrs · 21,861 cycles

FORWARD FLIGHT ATTENDANT JUMP SEAT EMERGENCY EQUIPMENT COMPARTMENT WON'T SPRING SHUT. REMOVED FROM SERVICE. REPLACED OUTBOARD MOST HINGE SPRING FOR THE FWD FLIGHT ATTENDANT SEAT EMERGENCY EQUIPMENT DOOR AS REQUIRED. FWD FLIGHT ATTENDANT SEAT EQUIPMENT DOOR CLOSES ON ITS OWN NORMALLY. NO FURTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 19,514 hrs · 21,128 cycles

FLAP DRIVE CAUTION MSG ILLUMINATES WITH FLAP EXTENSION. FLIGHT LANDED SAFELY. REMOVED FROM SERVICE. EXTENDED FLAPS AND ACCOMPLISHED GVI OF FLAPS AND ACTUATORS. NO DEFECTS NOTED. RETRACTED FLAPS TO 5 DEGREES. FERRIED AIRCRAFT. R AND R FLAP CONTROL UNIT (FCU) IAW Q400 AMM TASK 27-51-01-000-801/400-801. PERFORMED FUNCTIONAL TEST OF THE FLAP CONTROL SYSTEM REF WITH Q400 AMM TASK 27-51-00-720-801. OPS TEST NO GOOD. REMOVED FLAP POWER UNIT (FPU) IN IAW Q400 AMM TASK 27-52-01-000-801. INSTALLED FLAP POWER UNIT (FPU IAW Q400 AMM 27-52-01-400-801. PERFORMED FUNCTIONAL TEST OF THE FLAP DRIVE SYSTEM IAW Q400 AMM 27-52-00-720-801. OPS TEST GOOD. NO FAULT CODE FOUND. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — LOOSE (CABIN) · airframe 18,179 hrs · 19,545 cycles

CABIN EMERG. LIGHTS REMAIN ILLUMINATED WITH FLIGHT DECK EMER. LIGHTS SWITCH IN THE ARM POSITION. REMOVED FROM SERVICE. FOND THE EMER LIGHT SW BODY MODULE ON THE WING BULKHEAD ASSY LOOSE. TIGHTENED BODY MODULE IAW AMM TASK 33-541-05-400-801. C/W OPS CK OF EMER LIGHT SYS IAW AMM TASK33-51-00-710-802. OPS TEST GOOD. EMER LIGHTS DO NOT ILLUMINATE WHEN SW IS IN ARM POSITION WITH POWER ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 200) · airframe 17,846 hrs · 19,140 cycles

ON GEAR RETRACTION LEFT MAIN GEAR DOWN INDICATOR REMAINED ILLUMINATED, GEAR DOORS SEQUENCED NORMALLY. CONFERED WITH FA'S THAT GEAR ACTUALLY DID RETRACT. UPON GEAR EXTENSION, LEFT MAIN GEAR DOWN INDICATOR BECAME VERY BRIGHT. GEAR EXTENDED NORMALLY AND CONFURED WITH FSA'S THAT LEFT MAIN WAS DOWN. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED LEFT GEAR DOWNLOCK LIGHT ON GEAR SELECTOR PANEL AND FOUND BULB HAD SHORTED TO CONTACTS BEHIND LIGHT LENS. REMOVED BULB AND RELAMPED IAW AMM 32-31-01-960-801. NO HELP. LIGHT REMAINED FULL BRIGHT WHEN BRIGHT/DIM SWITCH WAS SET TO DIM. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW AMM 32-31-01-000-801/400-801. FUNCTIONAL CHECK FAILED ON STEP 4. A. (20) OF AMM 32-31-01-720-801. DISCREPANCY REMAINED: LEFT GEAR DOWNLOCK LIGHT REMAINED FULLY ILLUMINATED WHEN BRIGHT/DIM WAS SET TO DIM. IN REF TO SDS 31-51-00-001 AND WM 32-61-00-1. REMOVED AND REPLACED ACU IAW AMM 31-51-06-000-801/400-801. OPS TEST GOOD. LEFT GEAR DOWNLOCK LIGHT FUNCTIONED CORRECTLY WITH CORRESPONDING BRIGHT/DIM SWITCH POSITION. PERFORMED FUNCTIONAL TEST OF LANDING GEAR CONTROL PANEL IAW AMM 32-31-01-720-801. FUNCTIONAL TEST GOOD. NO FURHTER DEFECTS NOTED. RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

FLOORBEAM AT FSX 683.00,Y-30 AT FLOOR BOARD SUPPORT BRACKET IS CRACKED. REMOVED FLOORBEAM @ FSX683.00 Y30 IAW SRM 51-40-07-02-01. INSTALLED NEW SECTION OF FLOORBEAM @ FSX683.00 Y30 LT IAW SRM 51-40-07-02-01 & 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

EQUIPMENT RAIL 23 FROM FSX670-X698, IS CORRODED BEYOND LIMITS AROUND FWD FLOOR BOARD ATTACH HOLE. REPLACED EQUIPMENT RAIL 23 FROM FSX670-X698 IAW SRM 51-40-07-02-01, 51-41-00-00-01 & 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

SEAT RAIL 15 FROM FSX612.00-X670.00,Y9.250 IS CORRODED. REPLACED SEAT RAIL 15 FROM FSX612.00-X670.00 Y9.250 IAW SRM 51-40-07-02-01, 51-41-00-00-01, 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

SEAT RAIL 16 FROM FSX670-X783,Y9.250 IS CORRODED. REPLACED SEAT RAIL 16 FROM FSX670-X783, Y9.250 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-41-00-00-01 AND 51-42-05-02-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

TYPE2/3 DOOR LOWER THRESHOLD BEAM CORRODED. REPLACED TYPE 2/3 DOOR LOWER THRESHOLD BEAM PN 85329514-101 IAW SRM 51-23-00-00-01, 51-40-07-02-01, 51-41-00-00-01, 51-42-05-02-01, 51-42-45-02-01 AND 51-42-75-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,749 hrs · 19,020 cycles

SEAT RAIL NR 8 FROM FSX 570.00-X668,Y-9.250 IS CORRODED. REPLACED SEAT RAIL NR 8 FROM FSX 570.00 - X668 AND Y-9.250 IAW SRM 1-40-07-02-01,51-40-15-02-01 & 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FRAMES 10.5-39) · airframe 17,749 hrs · 19,020 cycles

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

Part: BEAM — CRACKED (AFT PAX DOOR) · airframe 17,749 hrs · 19,020 cycles

AFT PASSENGER DOOR #2 BEAM CRACKED BETWEEN FASTENER HOLES. REMOVED AFT PASSENGER DOOR #2 CRACKED BEAM IAW SRM 51-40-07-02-01. INSTALL AFT PASSENGER DOOR #2 BEAM IAW SRM 51-40-15-02-01, 51-41-15-02-01, 51-42-05-02-01, 51-42-02-01.

Part: SEAT TRACK — CORRODED (NR 5) · airframe 17,749 hrs · 19,020 cycles

SEAT RAIL #5 FROM FSX-39.00-X102.50,Y-9.250 IS CORRODED. SEAT RAIL #5 FROM FSX-39.00-X102.50 Y-9.250 REPLACED WITH NEW IAW SRM 51-42-05-02-01, 51-42-45-02-01, 51-40-15-02-01, 51-41-05-00-01.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 17,749 hrs · 19,020 cycles

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

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,687 hrs · 18,947 cycles

PROP DEICE CAUTION ILLUMINATED. RETURNED TO FILED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERREGTED CDS + FOUND NO FAULTS C/W FUNC. TEST OF PROP DEICE SYSTEM OPS TEST GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,647 hrs · 18,899 cycles

MAIN CABIN DOOR EMERGENCY LIGHT AND EXTERNAL MAIN CABIN DOOR EGRESS LIGHTS ARE INOP. REPLACED THE BATTERY PACK LT 1 POSITION IAW AMM 33-51-00-820-801. OPERATIONAL CHECKS GOOD.

Part: WIRE HARNESS — MALFUNCTIONED (NR 1 PROPELLER) · airframe 17,496 hrs · 18,721 cycles

ON DESCENT, SPARKS WERE NOTICED IN THE PROP ARC OF THE #1 ENGINE EVERY 30 SECONDS. REMOVED FROM SERVICE. #1 PROP #1 BLADE DEICE HARNESS REPLACED, AND #3 AND #6 BLADES ON #1 PROP HAD DEICE BOOT REPAIRS ACCOMPLISHED. TESTS SHOW NO SPARKS OR ISSUES FROM #1 PROP DURING USAGE OR TESTS. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — BROKEN (FUEL SYSTEM) · airframe 17,224 hrs · 18,415 cycles

POST FLIGHT INSP RIGHT WING FUEL MAG STICK INTERNALS APPEAR MISSING. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. REMOVED REMNANTS OF BROKEN INDICATOR FROM #2 MAGNASTICK INDICATOR BODY. INSTALLED SERVICABLE INDICATOR ASSY IN #2 MAGNASTICK INDICATOR BODY. #2 FUEL QUANITY CHECKS GOOD WITH MAGNASTICK IAW DHC-8-400-MM TASK# 28-40-26-610-801. RETURNED TO SERVICE.

Part: DISPLAY — INOPERATIVE (PRIMARY FLT) · airframe 17,154 hrs · 18,331 cycles

IN LEVEL CRUISE FLIGHT AT FL 230, ALL INSTRUMENTS ON THE CAPTAINS PFD FAILED AND DISPLAYED RED FAILURE MESSAGES. AFCS FAIL DISPLAYED AT TOP OF PFD. AVIONICS CAUTION ILLUMINATED ON TAXI INTO THE GATE. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. NO FAULTS IN CDS. CYCLED POWER TO CAPTAINS PFD. CAUTION LIGHTS AND MESSAGES EXTINGUISHED. ALL APPROPRIATE DATA ENTRIES RETURNED TO CAPTAINS PFD. MTX REQUESTS ADDITIONAL TROUBLESHOOTING. FOUND "NO DATA FROM PFD 1" FAULT IN CDS. REPLACED THE #1 PFD. OPS CHECK GOOD. NO FAULTS. AIRCRAFT REMAINS CAT III QUALIFIED. COCKPIT PLACARD SHOWS CAT III. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,671 hrs · 16,693 cycles

AFT RIGHT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-00/400-801. OPS CHECKED GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 15,389 hrs · 16,398 cycles

CABIN FAILED TO PRESSURIZE IN AUTO MODE, AFTER E & A CHECKLIST, AND SELECTION OF MANUAL MODE ON PRESSURIZATION CONTROLLER, CABIN RATE INITIALLY UNCONTROLLABLE, FLIGHT AT 10,000 FT THEN 9000 FT. AFTER STABILIZED, THE MANUAL PRESSURIZATION WORKED DURING CRUISE & DESCENT. NO CABIN PRESSURE WARNING DUE TO CABIN PRESSURE ONLY REACHED ABOUT 9400 FEET, AFTER STABLIZING IN MANUAL MODE, CABIN WAS ABLE TO BE DECENDED TO PROPER LEVELS. REMOVED FROM SERVICE. REMOVED AND REPLACED THE OUTFLOW VALVE IAW MM 25-31-16-000-801, AND MM 21-31-16-400. ERASE DATA ON THE CDS CABIN PRESSURE CONTROL SYSTEM IAW 45-00-21-743-802. FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL IAW 21-31-00-720-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 14,043 hrs · 14,996 cycles

DURING CRUISE FLIGHT FA'S REPORTED AN ELECTRICAL ODOR IN THE CABIN AROUND ROW 3 AND 4. THERE WAS NO VISIBLE SIGN OF FIRE OR SMOKE. FA'S REPORTED ODOR GOT STRONGER IN TO DESCENT. THERE NEVER WAS ANY SMOKE AT ANY POINT. DIVERTED. LANDING UNEVENTFUL. FOUND THE NR 1 ENGINE OVER SERVICED. REMOVED 1 QUART OF OIL FROM ENGINE. GROUND RAN ENGINE, VERIFIED OIL LEVELS IN LIMITS. NO ODOR NOTED.

Part: LINK — MALFUNCTIONED (SERVICE DOOR) · airframe 13,631 hrs · 14,557 cycles

AFT SERVICE DOOR IS HARD TO OPEN. INNER LINER IS CATCHING ON THE AFT SURROUND STRUCTURE. REPLACED THE LOWER SWING LINK IAW AMM 52-41-16-400-801.

Part: SWITCH — LOOSE (ZONE 200) · airframe 12,975 hrs · 13,861 cycles

EMERGENCY LIGHT SWITCH COVER BROKEN AT FORWARD FA POSITION. SECURED SWITCH. CHECKS GOOD RETURNED TO SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 12,926 hrs · 13,803 cycles

CLIMBING THROUGH 5000 FEET, CAPTAIN NOTICIED ACFT NOT PRESSURIZING. LEVELED AT 10000 FEET AND RAN THE PRESSURIZATION FAIL CHECKLIST AND RETURNED TO FIELD WITH MANUAL CONTROL BUT IT DIDNT WORK CORRECTLY EITHER. ACCESSED CDS DATA FOUND CPC/OF VALVE DATA FAIL. ACCOMPLISHED FIM TASK 21-30-00-810-804. CAWP CABIN PRESS LT WAS NOT ON. DUE HISTORY REMOVED & REPLACED AFT OUT FLOW VALV PER AMM 21-31-16-000-801 & 21-31-16-400-801. OPS TEST OF PRESS CONTROL GOOD REF AMM 21-31-00-720-801 NO FAULTS MESSAGES CURRENTLY DISPLAYED ON CDS. RETURNED TO SERVICE.

Part: STOP FITTING — ICED (PAX DOORWAY) · airframe 12,913 hrs · 13,787 cycles

PLANE PRESSURIZED NORMALLY, AFTER PASSING 12500 FEET CABIN PRESSURE WARNING ON TOP OF FUSELAGE DOORS WARNING OCCURED. THE FUSELAGE DOORS CHECKLIST WAS ACCOMPLISHED. DOOR WAS VERIFIED SHUT. RETURN TO FIELD. LANDING UNEVENTFUL. PERFORMED FIM TASK 21-30-00-810-801 FOR UNABLE TO PRESSURIZE CABIN, NO FAULTS FOUND IN CDS, PERFORMED FUNCTIONAL TEST OF PRESSURIZATION SYS IAW AMM TASK 21-31-00-220-801. ACFT FAILED TO PRESSURIZE. PERFORMED GVI OF AFT PAX DOOR SEAL NO DEFECTS FOUND. INSPECTED AFT PAX DOOR SEAL, NO DAMAGE OR DEFECTS NOTED. GVI AFT CARGO BAY BLOWOUT PANEL SECURE. INSPECTED AFT CARGO DOOR SEAL, NO DEFECT NOTED. PRESSURIZED ACFT IAW FIM 21-31-00-720-802. FOUND INTERNAL PAX DOOR HANDLE NOT SECURE DUE TO ICE ON DOOR STOPS APPLIED HEAT TO MELT THE ICE OPS TEST OF AFT PAX DOOR PER TASK 52-12-00-710-802.OPS TEST GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (ZONE 200) · airframe 12,692 hrs · 13,547 cycles

MASTER WARNING INDICATION SMOKE. DONNED MASKS AND RAN CHECKLISTS. WARNING WENT OUT AND REILLUMINATED TWICE. BAG AFT SMOKE ANNUNCIATOR ALSO TEMPORARILY ILLUMINATED ON SHORT FINAL STAYED STEADY ON GROUND. ACCOMPLISHED TO 2016102416 REPLACED BOTH AFT SMOKE DETECTORS REF MM 26-12-01 & NN 26-12-06 SYSTEM OPS NORMAL. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SWITCH) · airframe 12,662 hrs · 13,514 cycles

F/A SWITCHLIGHT FOR THE EMERGENCY LIGHTS INOP. RELAMPED PUSH BUTTON SWITCH. CHECKS GOOD. RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 12,607 hrs · 13,452 cycles

EMERGENCY LIGHTS DON'T TEST CORRECTLY. REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LATCH — OUT OF ADJUST (FUEL DOOR) · airframe 12,567 hrs · 13,412 cycles

"FUELING ON" CAUTION ILLUMINATED DURING TAKEOFF AT 60 KNOTS. TAKEOFF ABORTED. RETURNED TO THE GATE. FOUND THE OUTBOARD LATCH OF THE FUELING PANEL MISALIGNED WITH RELEASE HOLE AND NOT LATCHED. REPOSITIONED THE LATCH AND RESECURED IAW AMM 52-44-01-400-801. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BUSHING — FAILED (BRAKE PEDAL) · airframe 11,824 hrs · 12,592 cycles

WHEN QUICK, FIRM PRESSURE APPLIED TO THE CAPTAIN'S TOE BREAKS, THE ENTIRE FOOT PEDAL ASSEMBLY SLIDES FORWARD. REPLACED CAPTAIN'S RUDDER PEDAL ADJUSTMENT SHAFT, BOSS, AND BUSHINGS. PERFORMED OPS TEST IAW AMM 27-20-00-710-802. NO DEFECTS. RETURNED TO SERVICE.

Part: BEARING — CORRODED (SERVICE DOOR) · airframe 11,778 hrs · 12,545 cycles

AFT SERVICE DOOR IDLER LINK ASSY HAS CORRODED BEARINGS. REMOVED AFT SERVICE DOOR IDLER LINK ASSY IAW AMM 52-41-001-000-801, STEP 4.B. INSTALLED SERVICEABLE NEW FROM STOCK AFT SERVICE DOOR IDLER LINK IAW AMM 52-41-01-400-801, STEP 4.G, NO ADJUSTMENTS MADE REF TASK CARD 524100Q02-60379 FOR FUNCTIONAL CHECK.

Part: RIB — CRACKED (LT WING) · airframe 11,778 hrs · 12,545 cycles

LEFT WING L/E 511AL HAS CRACKED RIB DOUBLERS 1EA INBD AND 1EA OTBD. DISBONDED L/E DE-ICE BOOT TO GAIN ACCESS TO RIB REPAIR REF AMM 30-11-76-000-801 4.A, 1. BONDED EXISTING DEICE BOOT ON CORNER AT L/E REF AMM 30-11-76-400-801. PG 408, PROCEDURE 4.C.1. REMOVED 1EA INBD AND 1EA OTBD RIB DOUBLER REF SRM 51-42-05, REPAIR -01, PARA 4.E, 1-8. INSTALLED 1EA INBD AND 1EA OTBD REPAIR PANELS ON RIBS REF SRM 57-40-00, REPAIR -07. FABRICATED 2EA REPAIR ANGLES FROM 2024-T3.050 PO:TX-4337/1 REF SRM 57-40-00, REPAIR -07, PARA 7, A,3, FIG 201.

Part: SEAT TRACK — NOT REPORTED (NOT REPORTED) · airframe 11,778 hrs · 12,545 cycles

SEAT TRACK 13, REQUIRES REPLACEMENT. REMOVED DRIP TRAY REF SRM 51-41-00 SEAT TRACK 12 & 13. INSTALLED 3EA DRIP ANGLES COMMON TO SPLICE 12-13, SEAT TRACK, AND FWD AND AFT SEAT TRACK NR 13 REF SRM 51-42-05-02-01. REMOVED DRIP ANGLES COMMON TO SPLICE 12 AND 13, AND DRIP ANGLE FWD SEAT TRACK NR 13, AND AFT SEAT TRACK NR 13. INSTALLED 3EA DRIP ANGLES COMMON TO SPLICE 12-13, SEAT TRACK, AND FWD AND AFT SEAT TRACK NR 13 REF SRM 51-42-05-02-01. REMOVED SEAT TRACK SPLICE COMMON TO SEAT TRACK 12 AND 13 REF SRM 51-42-05 AND 51-40-15. INSTALLED SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 12 AND NR 13 REF DWG 85361501, REV E 213-020-12. REMOVED SEAT TRACK SPLICE COMMON TO SEAT TRACK 13 AND 14 REF SRM 51-42-05 AND 51-40-15. INSTALLED SEAT TRACK SPLICE COMMON TO SEAT TRACK 13 AND 14 REF DWG 85361501, REV E 213-02-02. REMOVED SEAT TRACK NR 13, PN 85361510-104, REF SRM 51-42-05 AND 51-41-05. INSTALLED SEAT TRACK NR 13, PN 85361510-104, REF SRM 51-42-05-020-01, 51-41-00-00-01, 51-40-15-02-01 AND DWG NR 85361501, REV E. LOCATED AND DRILLED NEW SEAT TRACK NR 9, PN 85361510-104, REF SRM 51-40-07-02-01. BOND CHECK COMPLETED IAW AMM 51-80-00-760-801 0.03MO TUC5893 08, JUL 215 CAL DUE, BOND CHECK GOOD. FINISH RESTORED IAW SRM 51-21-10-02-01, IAW SRM 51-25-10-02-01 AND IAW SRM REF 51-25-15-02-01.

Part: SEAT TRACK — NOT REPORTED (NOT REPORTED) · airframe 11,778 hrs · 12,545 cycles

SEAT TRACK NR 9 REQUIRES REPLACEMENT. REMOVED SPLICE AT FS 670.0 Y-9.250 COMMON TO SEAT TRACK 8 AND 9, REF SRM 51-42-05, REPAIR -01, PARA 1-4, E AND SRM 51-40-15 PARA 6 M AND N. INSTALLED SPLICE AT FS 670.00, Y-9.250 COMMON TO SEAT TRACK 8 AND 9 REF SRM 51-42-05, REPAIR -01 PARA 1-4, E AND SRM 51-40-15, PARA M TO N. REMOVED SEAT TRACK NR 9 PN 85338210-111, REF SRM 51-42-05, REPAIR -01, PARA 1-4 E. INSTALLED SEAT TRACK NR 9, PN 85338210-111 IAW SRM 51-42-05, REPAIR - 01, PARA 1-4 E AND 51-40-15. REMOVED CLIP AT FS 712.0, LBL 9.250, REF SRM 51-42-05 REPAIR -01 1-4, E. INSTALLED CLIP AT FS X712.000, LBL 9.250, REF SRM 51-42-05-02-01, STEP 4D, 3-10. LOCATED AND DRILLED REPLACEMENT SEAT TRACK REF SRM 51-40-07, REPAIR -01, PN 85330210-111. DRILLED COMPLETE SEAT TRACK NR 9 REF SRM 51-40-07. INSTALLED BOLTS, 6 EA, AT BS X697.600, X714.602 AND X728.102, REF SRM 51-41-00-00-01. INSTALLED FASTENERS COMMON TO SEAT TRACK 9 AND SHEAR WEB ROM BS X697.600 TO X703.10, REF SRM 51-42-05-02-01, STEP 4D, 3-10 AND DWG 85336201.

Part: CHANNEL — CORRODED (THRESHOLD) · airframe 11,778 hrs · 12,545 cycles

MCD THRESHOLD SUPPORT CHANNEL ASSY CORRODED. MCD THRESHOLD PLATE REMOVED REF SRM 51-42-05. MCD THRESHOLD PLATE INSTALLED REF SRM 51-42-05. MCD THRESHOLD CHANNEL NUTPLATES REMOVED REF SRM 51-42-05. MCD TRESHOLD CHANNEL NUTPLATES 5 EA INSTALLED REF SRM 51-42-05. MCD THRESHOLD CHANNEL CORROSION BLENDED/REMOVED, REF SRM 53-20-23 REPAIR-01. C/W ET/UT INSP REF NDTM 51-00-06 AND 51-00-04. NO DEFECTS NOTED. MIN THICK =.049". MCD THRESHOLD CHANNEL WITHIN LIMITS REF SRM 53-20-23, REPAIR-01.

Part: SEAT TRACK — NOT REPORTED (ZONE 100) · airframe 11,778 hrs · 12,545 cycles

SEAT TRACK NR 16 REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 23 AND ATTACHED WEB TO FOM REF SRM 51-42-05 AND SRM 51-41-00. INSTALLED SEAT TRACK NR 23 AND ATTACHED WEB REF SRM 51-42-05, SRM 51-41-00 AND DWG 85338806, REV. REMOVED GROUND CABLE ON SEAT TRACK NR 16 AT BS 790.00, REF SRM 51-410-00. INSTALLED GROUND CABLE ON SEAT TRACK NR 16 AT BS 790.00, REF SRM 51-41-05. REMOVED SPLICES AT BS 664.500, REF SRM 51-42-05, SRM 51-40-15. SPLICES COMMON TO SEAT TRACK NR 15 & NR 16. INSTALLED SPLICES COMMON TO SEAT TRACK NR 15 AND NR 16 AT BS 664.500, REF SRM 51-42-05, SRM 51-40-15 AND DWG 85338201, REV A. REMOVED ALL FASTENERS COMMON TO SEAT TRACK NR 16 AND WEBS BETWEEN BS 664.500 AND BS 783.00 REF SRM 51-42-05. INSTALLED ALL FASTENERS COMMON TO SEAT TRACK NR 16 AND WBS BETWEEN BS 783.00, REF SRM 51-42-05, REPAIR 01 AND DWG 85338201, REV A. LOCATED AND DRILLED NEW SEAT TRACK NR 16 REF SRM 51-40-07-02-01, SEAT TRACK, PN 85338210-119. REMOVED ALL FASTENERS COMMON TO SEAT TRACK NR 16 AND WEB BETWEEN BS 783.00 AND BS 801.00 REF SRM 51-42-05. INSTALLED ALL FASTENERS COMMON TO SEAT TRACK NR 16 AND WEB BETWEEN BS 783.00 AND BS 801.00, REF SRM 51-42-05, REPAIR 01 AND DWG 85338201, REV A. BOND CHECK COMPLETED IAW AMM REF 51-80-00-760-801. 0.04 MO TUC8593 08JUL2016 CAL DUE. FINISH RESTORED IAW REF SRM 51-21-10-02-01, IAW SRM REF 51-25-10-02-01 AND IAW SRM REF 51-25-15-02-01.

Part: SEAT TRACK — OUT OF LIMITS (ZONE 100) · airframe 11,778 hrs · 12,545 cycles

SEAT TRACK NR 10 FOUND TO BE OUT OF LIMIT, PN 85328210-121, REQUIRES REPLACEMENT. REMOVED GROUND WIRES FROM RT FWD SEAT RAIL AT FS-39 AND -18 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED GROUND WIRES AT RT SEAT TRACK BETWEEN FS -39 AND -18.00 IAW SRM 51-41-05. REMOVED CONNECTOR ATTACHMENT BRACKET AT BW FS-39 AND FS-18.00 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED CONNECTOR ATTACHMENT BRACKET BETWEEN FS -39 AND FS -18.00 IAW SRM 51-42-05. REMOVED 5 TIE MOUNTS AT BW FS-18.00 AND FS 1.00 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED 5 TIE MOUNTS AT BETWEEN FS -18.00 AND FS 1.00 IAW SRM 51-42-05. REMOVED WIRE HARNESS ATTACHMENT BRACKET AT BW FS 1.00 AND FS 16.00 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED WIRE HARNESS ATTACHMENT BRACKET AT BETWEEN FS 1.00 AND S 16.00 IAW SRM 51-42-05. REMOVED KICKPLATE AT FS-39.00 TO FACILITATE SEAT TRACK REMOVAL. INSTALLED KICK PLATE AT FS -39.00 IAW SRM 51-42-45. REMOVED SEAT TRACK NR 10 IAW SRM 51-40-15 AND 51-42-05. LOCATED AND DRILLED SEAT TRACK NR 10 IAW SRM 51-40-07. LOCATED AND DRILLED HOLES THROUGH SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11 IAW SRM 51-40-07. LOCATED AND DRILLED HOLES THROUGH SEAT TRACK COMMON TO SEAT TRACK NR 10 IAW SRM 51-40-07. INSTALLED SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11. INSTALLED SEAT TRACK NR 10 REF SRM 51-41-05 AND SRM 51-42-05, REF DWG 8532820, REV D. BONDING CHECK IS GOOD IAW AMM 51-80-00-760-830.

Part: SEAT TRACK — OUT OF LIMITS (ZONE 100) · airframe 11,778 hrs · 12,545 cycles

SEAT TRACK NR 11 FOUND TO BE OUT OF LIMIT, PN 85328210-115 REQUIRES REPLACEMENT. REMOVED 4 TIE MOUNTS AT BW FS32.00 AND FS49.00 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED 4 TIE MOUNTS AT BETWEEN FS 32.40 AND FS 49.00 IAW SRM 51-42-05. REMOVED 2 FLOOR PANEL TRAY AT FS71.2 AND 116.00 TO FACILITATE SEAT RAIL REMOVAL. INSTALLED DRIP ANGLE ON SEAT TRACK NR 11 REF SRM 51-42-05, DWG 85328201, REV D. INSTALLED SEAT TRACK SPLICE COMMON TO SEAT TRACK 11 & 12 REF SRM 51-40-15, REPAIR 01 AND SRM 51-42-05. REMOVED SEAT TRACK NR 11 IAW SRM 51-40-15 AND 51-42-05. LOCATED AND DRILLED SEAT TRACK NR 11 IAW SRM 51-40-07. LOCATED AND DRILLED HOLES THROUGH SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 11 AND NR 12 IAW SRM 51-40-07. LOCATED & DRILLED HOLES THROUGH SEAT TRACK COMMON TO SEAT TRACK NR 11 IAW SRM 51-40-07. INSTALLED SEAT TRACK NR 11 REF SRM 51-41-05 AND SRM 51-42-05 AND DWG 85328201, REV D.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 11,693 hrs · 12,453 cycles

NORMAL LIGHT ON F/A EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED LAMP CHECKS GOOD. IAW TASK CARD 335000202-60045.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 PROPELLER) · airframe 9,988 hrs · 10,552 cycles

NR 1 PROPELLER CAUTION WHEN THE PROPELLER CYCLES. RETURNED TO FILED. LANDING UNEVENTFUL. TROUBLESHOT IAW FIM TASK 30-60-00-810-807. PERFORMED FUNCTIONAL TEST OF PROPELLERS DEICING SYS PEM MM 30-61-00-720-801. NO FAILURES NOTED. HAS NO OTHER RECENT HISTORY. RETURNED TO SERVICE.

Part: TERMINAL — LOOSE (WARMER) · airframe 9,883 hrs · 10,434 cycles

IN THE AFT GALLEY, THE LIQUID WARMER CIRCUIT BREAKER POPPED AND A BRIGHT FLASH WAS OBSERVED BY THE F/A WHEN THE WARMER WAS TURNED OFF. PLACED THE LIQUID WARMER ON NEF CLEARED 5/14/15 BY:INSPECTED ELETRICAL WIRES AND TERMINALS CONECTORS, FOUND TERMINALS LOOSE AND CONTACTING EACH OTHER, RESECURED WIRES TERMINALS AS NEEDED. OPS TEST GOOD. RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (ZONE 200) · airframe 9,422 hrs · 9,937 cycles

WHILE FLYING CAT III APPROACH ILS INTO BOTH AIRPORTS NO AIII CAME UP ON HUD AND HAP AFTER INITIALLY SHOWING AIII. PASSING FINAL APPROACH FIX, AIII FLICKERED THEN NO AIII. TRIED RESETTING NO HELP. WEATHER BELOW MINIMUMS. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED HGS, NO PRESENT FAULTS LEGS 1 AND 5 HAVE LAT GUIDE COMP AND MAG HDG COMP. REMOVED REPLACED HGS COMPUTER IAW MAINTENANCE 6343501, OPS CK GOOD ACFT REMAINS CAT III PLACARDED, CAT III. RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 9,270 hrs · 9,765 cycles

EMERGENCY LIGHT STRIP IN THE WAY OF THE FORWARD GALLEY DOOR. REMOVED STRIP AND CLEANED FLOOR AND STRIP. INSTALLED SAME STRIP IAW AMM 33-51-16-400-801. GALLEY DOOR CLEARS STRIP. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 9,242 hrs · 9,732 cycles

COVER ON THE EMERGENCY LIGHT SWITCH IN THE MAIN CABIN DOORWAY NEXT TO THE F/A JUMPSEAT IS BROKEN OFF. REPLACED THE SWITCH GUARD IAW AMM 33-51-05-400-401. RETURNED TO SERVICE.

Part: STRUT — MALFUNCTIONED (PAX DOOR) · airframe 9,198 hrs · 9,684 cycles

MAIN CABIN DOOR STICKS PART OF THE WAY OPEN. HAD TO PUSH ON THE HANDRAILS TO GET THE DOOR TO THE FULLY OPEN POSITION. CLEAN, INSPECTED & LUBED DOOR HINGES, RAILS PULLEYS AND CABLES. R & R FWD GAS SPRING ASSY REF AMM 52-11-16-000/ 400-802, C/W FUNCTIONAL TEST OF DOOR IAW AMM 52-11-00-720-801 DOOR OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 9,121 hrs · 9,592 cycles

FORWARD F/A PANEL THE EMERGENCY LIGHT SWITCH GUARD IS MISALIGNED AND BENT. REPLACED LIGHT SWITCH GUARD IAW AMM 33-51-05-000-801. RETURNED TO SERVICE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 9,061 hrs · 9,531 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH STUCK IN THE ON POSITION. REPLACED THE SWITCH IAW AMM 33-51-05-000-801 AND 33-51-05-400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 8,938 hrs · 9,415 cycles

EMERGENCY LIGHT SEAT 1B IS DETACHED FROM THE FLOOR. CLEANED AREA AND REATTACHED THE STRIP. RETURNED TO SERVICE.

Part: ESCAPE ROPE — DISLODGED (SLIDE) · airframe 8,688 hrs · 9,115 cycles

ROPE PROTRUDING FROM THE EMERGENCY EXIT DOOR. REPOSITIONED THE LANYARD FOR THE EMERGENCY EXIT DOOR AND RE-INSTALLED THE UPPER EMERGENCY EXIT DOOR. RETURNED TO SERVICE.

Part: LIGHT — ODOR (ZONE 200) · airframe 8,438 hrs · 8,823 cycles

ELECTRICAL ODOR IN THE AFT GALLEY AREA. COMPLIED WITH AIR CONTAMINATION CHECKLIST IAW M-744. FOUND SOURCE OF ODOR TO BE FOUND AFT CARGP BAY FWD O/H LIGHT. R & R CARGO LIGHT ASSY IAW MM TASK 33-31-01-000-801 + 33-31-01-400-801. OPS CHECK GOOD. ODOR DID NOT RETURN AFTER LIGHT REPLACEMENT. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,654 hrs · 7,926 cycles

FORWARD PASSENGER DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-11/400-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,654 hrs · 7,926 cycles

AFT PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-11-000/400-801.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 7,592 hrs · 7,857 cycles

NR 1 EDP CAUTION MESSAGE. RETURNED TO FIELD, LANDED UNEVENTFUL. AS A PRECAUTION REPLACED THE ENGINE DRIVEN PUMP. RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,234 hrs · 7,471 cycles

EMERGENCY EXIT BEAM FOUND CORRODED. REPLACED BEAM IAW SRM 51-42-05 AND 51-42-45.

Part: BEARING — FAILED (MLG WHEEL) · airframe 6,009 hrs · 6,148 cycles

ON LANDING, OTBD ANTI-SKID CAUTION LIGHT FLASHED. POST FLIGHT WALKAROUND, NR 4 TIRE LOOKED FLAT. GVI OF RT OTBD TIRE FOUND A BEARING FAILURE RESULTING IN DAMAGE TO RT OTBD WHEEL ASSY, RT OTBD BRAKE ASSY AND AXLE. COMPLIED WITH AMM 05-50-17, RT OTBD TIRE, INBD BEARING SEIZED TO AXLE. REPLACED RT TIRES IAW MX 6324101, REPLACED RT BRAKES IAW MX 6324201, REPLACED WHEEL SPEED TRANSDUCEERS, REPLACED RT AXLE. FUNCTIONAL CHECKS OF ANTI-SKID CONTROL SYS IAW AMM 32-46-00-720-801 AND 32-46-00-720-802 ALL CHECKED GOOD. RETURNED TO SERVICE.

Part: HANDSET — MALFUNCTIONED (INTERPHONE) · airframe 5,739 hrs · 5,863 cycles

ON FINAL, HI-LOW CHIME HEARD IN FLIGHT DECK AND CABIN, NOT TRIGERRED. AFT F/A EMERGENCY LIGHT IS NOW ON ALL THE TIME BUT DIMLY LIT. ATTEMPTS TO USE EMERGENCY CALL FROM ALL PILOT & F/A STATIONS DOES NOT TRIGGER THE THE HI-LOW CHIME. THE LIGHT FLASH RED AS NORMAL. ALL OTHER INTERPHONE, PA, CHIMES WORK NORMALLY. REMOVED AFT F/A HAND SET IAW 23-31-11-000-801 INSTALLED NEW UNIT IAW 23-31-11-400-801 C/W OPS TEST IAW 23-31-00-710-801 OPS TEST GOOD.

Part: VALVE — MALFUNCTIONED (ZONE 500) · airframe 5,438 hrs · 5,560 cycles

REOCCURING DEICE PRESSURE CAUTION LIGHT, POWER RATING DETENT CL, OCCURED AT -6000' AND 13000 ' IN SLOW AIRFRAME MODE SELECT. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED TACTILE INSPECTION OF ALL DEICE BOOTS WHILE INFLATING BOOTS. DEICE BOOT 613AR & 613BR DID NOT INFLATE. CHECKED CDS FOR FAULTS, FOUND NO FAULTS. REMOVED L/E PANEL 613AR IAW AMM TASK 57-23-01-000-801. R & R NR 2 DDV IAW AMM TASK 30-11-16-000-801 & 30-11-16-400-801. NO HELP. R & R TMU IAW AMM TASK 30-11-01-000-801 & 30-11-01-400-801. NO HELP. CHECKED CDS AND FOUND FAULT CODE "LOW PRESS 2A". R & R NR 2 DDV IAW AMM TASK 30-11-16-000-801 & 30-11-16-400-801. PERFORMED OPS TEST OF THE AIRFRAME DEICE SYS IAW AMM TASK 30-11-00-710-804. OPS CHECK GOOD. ALL DEICE BOOTS INFLATED NORMALLY, ADVISORY LIGHTS NORMAL AND DEICE PRESS CAUTION DID NOT RETURN. TMU REPLACED AS A PRECAUTIONARY MEASURE. RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (DOOR WARNING) · airframe 4,050 hrs · 4,140 cycles

MASTER WARNING FUSELAGE DOORS ON TAKEOFF ROLL. ABORTED TAKEOFF AT 87 KTS. RAN APPROPRIATE CHECKLISTS. AFT PASSENGER DOOR WAS CONFIRMED TO BE THE DOOR THAT WAS INTERMITTENTLY SHOWING OPEN. VISUAL INSPECTION BY F/A & RAMP SHOWED DOOR CLOSED. REMOVED AFT PAX DOOR SURROUND LINER FOR ACCESS TO PROXIMITY SENSOR. FURTHER DISCONNECTED BOLT ON AFT PAX DR. HANDLE IAW AMM 52-12-01-000-801 STEPS 1A AND 4A(2). R & R SENSOR WIRES BETWEEN PROXIMITY SENSOR S39 AND CONNECTOR 3261.P14. CONTINUITY TEST OF NEWLY INSTALLED WIRES GOOD. REF WM 52-10-00, SHEET 1/1 PG 4, WM 20-12-10 WIRING MX PRACTICES, WM 20-17-10 ELECTRICAL CONNECTORS MX PRACTICES. PERFORMED. INSTALLED AFT PAX DOOR SURROUND IAW AMM 25-26-21-400-801, PARA 4D(1) THRU (15), INCLUDES DOOR HANDLE INSTALLATION. CHECKS GOOD IAW 52-12-00-710-801.

Part: CONTROL CABLE — OUT OF RIG (ELEVATORS) · airframe 3,228 hrs · 3,300 cycles

ON DESCENT, ELEVATOR ASYMMETRY CAUTION LIGHT ILLUMINATED. AUTO PILOT ENGAGED AT THE TIME. ALTITUDE WAS ABOUT 20,000 AIRSPEED VMO-15. CAUTION LIGHT WENT OUT ON TOUCHDOWN. COMPLIED WITH OPS TEST OF THE ELEVATOR CONTROL SYS AND ASYMMETRY CHECKED IAW AMM TASK 29-30-00-710-801, TASK 27-30-00-750-801 AND FIM TASK 27-30-00-810-801. FOUND NO FAULTS. OPS TESTED GOOD. DURING INSPECTION OF ELEVATOR CABLE TENSION, FOUND LT ELEVATOR CABLE TENSION AT 60LBS AND RT AT 50LBS. RIGGED RT & LT ELEVATOR IAW AMM TASK 27-31-11-830-801 AND TASK 27-31-16-830-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,965 hrs · 3,027 cycles

BOTH F/A'S REPORTED BURNING ODOR IN AFT GALLEY. APU WAS WORKING AT THAT TIME. AFTER REPORT FROM F/A, APU WAS SHUTDOWN. COMPLIED WITH AIR CONDITIONING CHECKLIST. RAN APU FOR 10 MIN WITH BLEED AIR ON AND RECIRCULATION FAN ON. INSPECTED MAPCO'S, MAPCO PLUGS, OVERHEAD WORKING LIGHTING AND EXPOSED WIRES. ALSO INSPECTED APU GROUND STUD. NO DEFECTS NOTED. REPLACED MAPCO'S AND C/W ODOR REMOVAL OF A/C DUCTS. (REF AMM TASK 21-00-00-160-801) AS A PRECAUTION IAW AMM TASKS 53-41-01-000-801 AND 53-41-01-400-801 FOR REMOVAL AND REINSTALLATION OF PANEL 145 C2 (APU GROUND STUD ACCESS) COULD NOT DUPLICATE BURNING ODOR AT THIS TIME. ACFT OK FOR CONTINUED SERVICE.

Part: STARTER GEN — MALFUNCTIONED (ZONE 400) · airframe 1,768 hrs · 1,819 cycles

NR 2 DC GENERATOR ILLUMINATED ON ROTATION E/A CHECKLIST DID NOT RESOLVE ISSUE. NO FAULTS IN CDS. GROUND RAN ACFT ABLE TO DUPLICATE PROBLEM, SWAPPED GCU CONNECTORS FAULT REMAINED WITH NR 2 GENERATION SIDE. RETURNED CONECTORS TO ORIGINAL POSITION. R & R NR 2 DC GENERATOR IAW MX 6243101, OPS CHECKS OF GCU'S & NR 2 DC GEN IAW AMM 24-31-06-710-801 & 24-31-00-710-802. ALL OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: RUDDER — BINDING (ZONE 200) · airframe 1,734 hrs · 1,781 cycles

WHILE F/O FLYING ON FINAL AND CONFIGURED, NOTED THE RIGHT RUDDER STUCK. WHILE APPLYING MORE PRESSURE IT BROKE FREE AND HAD NORMAL RUDDER MOVEMENT FOR REMAINDER OF FLIGHT. BINDING STARTED WITH AUTOPILOT ON AND CONTINUED AFTER IT WAS SELECTED OFF, LANDING UNEVENTFUL. RUDDER CABLE INSPECTED, KICK PANELS AROUND RUDDER PEDALS INSPECTED, NO DEFECTS NOTED. OPERATED RUDDER SYS WITH INPUT ROD TO FEEL UNIT DISCONECTED, SYS OPERATED SMOOTHLY WITH NO DEFECTS NOTED. INPUT ROD RE-CONNECTED DURING REPLACEMENT OF RUDDER FEEL AND SUMMING UNIT. ALL OPS TESTED GOOD. REPLACED RUDDER FEEL AND SUMMING UNIT. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,382 hrs · 1,444 cycles

PUNGENT ODOR REPORTED FROM F/A IN REAR GALLEY. OPENED CARGO (AFT) DOOR NO ODOR NOTED. INSPECTED ALL LIGHTING AND ELECTRIAL RELATED COMPONETS NO DEFECTS. OPENED ALL DOORS NO ODOR NOTED. ACFT OK FOR SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.