N450QX

Part: NONE — NONE · airframe 16,560 hrs · 17,875 cycles

DURING CLIMB PASSING 13000 IN MCL THE #TRQ BUG MOMENTARILY DROPPED TO APPROX . 45% THEN IMMEDIATELY RETURNED TO 91% NO POWER CHANGE NOTED AND EVENT MARKER PRESSED. INSPECTED AND CLEANED FADEC AND TORQUE SENSORS CONNECTORS. NO CONTAMINATION WAS FOUND. PERFORMED HIGH POWER ENGINE RUN OPS TEST NORMAL. NO ABNORMAL INDICATIONS. TORQUE BUG WAS NORMAL. CLEANED P1, P2,P11, AND P12 CONNECTORS. REF LP 961816 FOR HEAT SHRINK DMI #1 ENG FADEC PLUGS P1 AND P2. HIGH POWER ENGINE RUN PER Q400 MTC 6710005. #1 ENGINE . NO FAULTS WAS REPORTED IN CDS. RETURNED TO SERVICE.

Part: O-RING — WRONG PART (#1 ENGINE) · airframe 16,515 hrs · 17,824 cycles

CLIMBING OUT, THE #1 OIL PRESSURE STARTED FLUCTUATING. AS TIME PASSED IT OCCASIONALLY DIPPED INTO THE RED AND THE #1 ENGINE OIL PRESS WARNING LIGHT BEGAN TO FLICKER. SHUTDOWN THE ENGINE, RAN THE CHECKLISTS AND RETURNED TO THE FIELD. ACCOMPLISHED OVERWEIGHT LANDING. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND THE #1 ENGINE STARTER / GENERATOR O-RING SPLINE SHAFT TO BE THE INCORRECT ONE. REPLACING THE #1 ENGINE AND PROPELLER.

Part: NONE — NONE · airframe 16,271 hrs · 17,572 cycles

ON T/O FROM PDX WHILE RETRACTING GEAR, HEARD A LOUD BANG AT FRONT OF A/C. LANDING GEAR HAD RETRACTED AT NORMAL SPEED AND NO ANOMALIES WITH LG OR A/C AFTER RETRACTION. LEG EXTENDED AND LOCKED NORMALLY ON APPROACH. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED GVI OF A/C FOR EVIDENCE OF BIRD STRIKES. NO DEFECTS NOTED. PERFORMED GVI OF NLG AND SURROUNDING AREA FOR DISCREPANCIES. NONE NOTED. CYCLED NLG DOORS. AUDIBLE NOISE WHEN DOORS CLOSE. NOISE NOT EXCESSIVE. A/C CLEAR FOR SERVICE.

Part: SINK — CLOGGED (GALLEY) · airframe 16,266 hrs · 17,565 cycles

FA REPORTS AFT SINK NOT DRAINING AND HAS BAD SMELL. UNCLOGGED AFT GALLEY SINK. AFT GALLEY SINK DRAINS NORMALLY, AND BAD SMELL IS NO LONGER. RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (BLEED SYSTEM) · airframe 16,014 hrs · 17,298 cycles

ON TAKEOFF ROLL ADVANCED POWER LEVER JUST FORWARD OF FLIGHT IDLE AND GOT A #1 BLEED HOT CAUTION. HAD NOT SET TAKE-OFF POWER. ABORTED TAKE-OFF AND RETURNED TO GATE AT DIRECTION OF M/C. RAN ETA CHECKLIST AND BLEED HOT CAUTION EXTINGUISHED. REMOVED FROM SERVICE. INTERROGATED CDS & FOUND 4001 ECU DIG CH1 IN PRESENT FAULTS AND 7002 L. WING LEAK IN FLT HISTORY. C/W Q400 FIM TASK 36-10-00-810-853. INSPECTED L. DUCT TEMP SW & FOUND TO HAVE HIGH RESISTANCE BETWEEN PINS B AND C. R&RD L. DUCT TEMP SWITCH IAW Q400 AMM 36-11-21-000/400-801. ALL FAULTS CLEARED & OPS CKS GOOD IAW Q400 AMM TASK 36-11-00-710-802. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 16,008 hrs · 17,290 cycles

ON TAKEOFF ROLL #2 ENGINE PSI HIT 73 PSI STAYED AT 73 PSI TILL POWER WAS TAKEN OUT. ABORTED TAKEOFF. REMOVED FROM SERVICE. INTERROGATED CDS FOR ANY EXCEEDANCE ON THE #2 ENG. NO EXCEEDANCES NOTED. IAW Q400 AMM TASK 45-00-946-001 DETERMINED TO BE IN A TRANSITORY CONDITION ALLOWABLE FOR Q400 AMM TASK 05-11-00-992-802. RETURNED TO SERVICE.

Part: TRANSDUCER — FLUCTUATES (LT ENGINE) · airframe 15,758 hrs · 17,043 cycles

#1 OIL PRESSURE RAPIDLY FLUCTUATING FREQUENTLY HITTING 72 PSI AND TURNING YELLOW. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED AND CLEANED #1 ENGINE OIL PRESSURE TRANSDUCER CONNECTOR, GROUND RAN ENGINE, NO FLUCTUATION OF INDICATION NOTED PER Q400 AMM 71-00-00-780-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: DRAIN — ODOR (WASH BASIN) · airframe 15,604 hrs · 16,895 cycles

STRONG ODOR COMING FROM THE BACK GALLEY. REMOVED FROM SERVICE. VERIFIED ODOR NOT TO BE FUEL, OR OIL, OR HYDRAULIC FLUID. ODOR WAS COMING FROM AFT WASH BASIN DRAIN TANK. EMPTY THE DRAIN TANK, AND ODOR WENT AWAY. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — INOPERATIVE (ENGINE BLEED SYS) · airframe 15,157 hrs · 16,472 cycles

#1 AND #2 BLEED HOT CAUTION ILLUMINATED DURING ROTATION. DURING BLEEDS OFF TAKEOFF. RUNNING THE CHECKLIST CAUSED CAUTIONS TO EXTINGUISH. DIVERTED. REMOVED FROM SERVICE. FOUND FAULTS 7008,7004,3801 AND 3102 IN FAULT HISTORY FOR LEFT CHANNEL AND 7008,7004,3801,3102, AND 1006(RNAPRSOV) FOR RIGHT CHANNEL. DURING HIGH POWER RUNS DUPLICATED BOTH BLEED HOT CAUTION LIGHTS ON WITH BLEEDS SELECTED OFF. AND PRESENT FAULTS 3102,7008,7004,1601 IN BOTH CHANNELS. REPLACED RNAPRSOV REF AMM 36-11-19-000-801/400-801 FOR CODE 1006. WHILE PERFORMING OPERATIONAL TEST OF BLEED AIR SYSTEM REF AMM 36-11-00-710-802, BOTH #1 AND #2 HPSOV VALVES FAILED OPS TEST. REPLACED BOTH HPSOV VALVES REF AMM 36-11-09-000-801/400-801. OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY AGAIN AT HIGH POWER SETTINGS. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (NR 2 ENGINE) · airframe 15,086 hrs · 16,403 cycles

ON CLIMB OUT 10 MIN AFTER DEPARTURE AT APPROXIMATELY 20,000 FT. NOTICED A MOMENTARY REDUCTION IN THE #2 ENGINE TORQUE TO ABOUT 50%. MONITORED SYSTEM, NO OTHER ANOMALIES NOTED. REMOVED FROM SERVICE. PERFORMED GVI OF #2 FADEC. ON TACTILE INSP OF CANNON PLUG P50+P2, NOTED CANNON PLUGS NOT FULLY SEATED. REMOVED HEAT SHRINK FOR CONNECTORS P50+P2 & DISCONNECTED TO FOM. REMOVED HEAT SHRINK FOR CONNECTORS P40, P1 & CHARACTERIZATION PLUG. NOTED RED BAND SHOWING ON CONNECTOR P40+P1. RESECURED CONNECTORS P40, P1, & CHARACTERIZATION PLUG. REINSTALLED CONNECTORS P50+P2. PERFORMED SUBTASK Q400 AMM 73-21-01-710-011, "UPLOAD OF PLA, CLA, TORQUE & T6 TRIM VALVES." NO DEFECTS OR FAULTS CODES NOTED. PERFORMED #2 ENG START X2. NO DEFECTS OR FAULT CODES IN CDS. AIRCRAFT IS OK FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 15,012 hrs · 16,334 cycles

LENS FOR EXIT SIGN IN ROW 2 FELL OFF. REMOVED FROM SERVICE. RE SECURED EXIT SIGN LIGHT LENS AT SEAT 2E REF Q400 AMM 33-51-06-000-804. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BUSS BAR — DAMAGED (CONTACTOR BOX) · airframe 14,984 hrs · 16,310 cycles

STANDBY CONTACTOR BOX BUS BAR DAMAGED/BURNT. REMOVED FROM SERVICE. REMOVED AND REPLACED STANDBY CONTACTOR BOX PER AMM 24-31-36-000/400-801. CONTACTOR BOX OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FADEC — FLUCTUATES (NR 2 ENGINE) · airframe 14,943 hrs · 16,272 cycles

ON TAKEOFF WE NOTICED A FLUCTUATION OF TRQ 1% AND 2% ABOVE AND BELOW TRQ RATING. NH AND PROP RPM FLUCTUATION ALSO TOOK PLACE. AFTER SETTING CLIMB POWER, EVERYTHING SEEMED TO STABILIZE. REMOVED FROM SERVICE. NR 2 ENG FMU & FADEC WERE R & R AS PRECAUTIONARY PER ENGINEERING. ALL ASSOCIATED OPS TESTS WERE NORMAL FOR ALL COMPONENTS CHANGED & NO FLUCTUATIONS WERE NOTED. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 100) · airframe 14,829 hrs · 16,148 cycles

FLAP POWER CAUTION SELECTING FLAPS 35. RAN ASSOCIATED CHECKLIST, FLAP POWER CAUTION RETURNED AFTER CB RESET. FLAPS WERE STUCK JUST PAST 15 DEGREES. REMOVED FROM SERVICE. INTERROGATE CDS, FOUND "ECU CONTINUOUS BIT" PRESENT FAULT. ERASED PRESENT FAULTS, RAN BOTH ENGINES, PERFORMED OPERATIONS TEST OF WING FLAPS, IAW Q400 AMM TASK 27-50-00-710-801. FLAP POWER CAUTION LIGHT REMAINS EXTINGUISHED. FAULTS DID NOT RETURN. OPERATIONS CHECK PASSED. C/W FIM TASK 27-50-00-810-802. PER MTX CONTROL REQUEST, REF Q400 FIM TASK 27-50-00-810-807. R & R FLAP CONTROL UNIT, IAW Q400 AMM TASK 27-51-01-000/400-801. PERFORMED OPERATIONS TEST OF WING FLAPS, IAW Q400 AMM TASK 27-50-00-710-801. OPERATIONS TEST PASSED. FLAP POWER CAUTION LIGHT DID NOT ILLUMINATE. NO FAULTS PRESENT IN CDS. RETURNED TO SERVICE.

Part: APU — FIRE (EXHAUST) · airframe 14,574 hrs · 15,894 cycles

RAMP REPORTS FLAME FROM APU EXHAUST DURING START. REMOVED FROM SERVICE. OPENED APU COWLS, PERFORMED GVI OF APU, NO DEFECTS NOTED. CLOSED COWLS AND STARTED APU, NO DEFECTS NOTED DURING START. A/C OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 14,390 hrs · 15,714 cycles

#1 HYD QTY INDICATION REDUCED TO ZERO. INITIAL ASSOCIATED ROLL SPLR INBD HYD AND #1 HYD ISO VLV MASTER CAUTIONS ILLUMINATED, THEN EXTINGUISHED WHEN QTY REACHED ZERO. FOLLOWED BY #1 ENGINE HYD PUMP MASTER CAUTION. REMOVED FROM SERVICE. REPLACED LEAKING #1 EDP AND #1 SYSTEM FLUSH. OPS AND LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: LIGHT — OVERHEATED (GALLEY) · airframe 14,107 hrs · 15,404 cycles

RAMP REPORTS AFT GALLEY WORK LIGHT OVERHEATING / SMOKING WHEN TURNED ON

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 14,105 hrs · 15,402 cycles

PHOTO-ILLUMINESCENT FLOOR STRIP LOOSE AT ROW 1 A&B. REMOVED FROM SERVICE. RESECURED EMERGENCY FLOOR PATH LIGHT AT ROW 1A/B REF AMM 33-51-16-400-801. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BUMPER BLOCK — MISSING (PAX DOOR HANDLE) · airframe 13,909 hrs · 15,176 cycles

MAIN CABIN DOOR LOWER EXTERIOR HANDLE NEEDS ADJUSTMENT. IT SETS TOO FAR INTO THE NOTCH. REMOVED FROM SERVICE. INSPECTED AND FOUND FWD PAX DOOR OUTSIDE HANDLE BUMPER STOP MISSING. REPLACED MCD HANDLE BUMPER STOP REF. Q400 AMM TASK 52-11-11-420-008. HANDLE CLOSES FLUSH WITH SKIN. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (DEICE PRESSURE) · airframe 13,826 hrs · 15,077 cycles

AT 8000 IN LEVEL CRUISE FLIGHT PROPS 850 DEICE PRESS CAUTION ILLUMINATED. AFTER RUNNING CHECKLIST CAUTION LIGHT REMAINED ILLUMINATED. DEICE BOOT PRESSURES AT 19 PSI AT ALL TIMES. AIR FRAME SWITCH POSITION IN FAST. RETURNED TO FIELD. REMOVED FROM SERVICE. C/W FIM TASK Q400 30-10-00-810-801. INTERROGATED CDS FOR FAULTS NO FAULTS FOUND PERFORMED FUNCTIONAL TEST OF AIR FRAME PNEUMATIC DEICE SYSTEM REF TO AMM 30-11-00-720-801. DEICE PRESSURE CAUTION DID NOT COME ON OPS CHECK GOOD. RECHECKED CDS FOR FAULTS AGAIN NO FAULTS RECORDED. A/C IS GOOD FOR SERVICE NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 13,749 hrs · 14,984 cycles

EMERGENCY FLOOR LIGHTING COMING LOOSE IN FRONT OF DOOR TO THE FORWARD CARGO COMPARTMENT. REMOVED FROM SERVICE. RESECURED FLOOR LIGHTING FWD CABIN BY FWD. DOOR CARGO COMPARTMENT NO OTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 13,703 hrs · 14,928 cycles

PIECE OF EMERGENCY LIGHTING FLOOR TRACK STRIP PULLED UP. REMOVED FROM SERVICE. REINSTALLED EMERGENCY LIGHTING FLOOR TRACK STRIP, REF Q400 AMM TASK 33-51-16-400-801

Part: BOOT — TORN (LT WING DEICE) · airframe 13,697 hrs · 14,921 cycles

LEFT WING OUTBOARD DE-ICE BOOT TORE OPEN IN FLIGHT. DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. SMALL AIRCRAFT VIBRATION FELT. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED LEADING EDGE 513CL IN REF WITH FUNCTIONAL TEST PASS. BOOTS INFLATE NO FURTHER DEFECT. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 13,612 hrs · 14,823 cycles

PHOTO LUMINESCENT STRIP AT BASE OF BULKHEAD IN FRONT OF SEATS IN ROW 2 E & D PEELED UP AND LOOSE. REMOVED FROM SERVICE. REINSTALLED EMERGENCY FLOOR PATH LIGHT FWD OF SEATS 2 E & D IAW Q400 AMM 33-51-16-400-801. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 13,498 hrs · 14,689 cycles

EMERGENCY EGRESS LIGHTING STRIP AT ROW 2 D AND E IS DELAMINATING. REMOVED FROM SERVICE. REATTACHED GLOW STRIP WITH DOUBLE SIDED TAPE TO FLOOR. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SPRING — INOPERATIVE (MLG UPLOCK) · airframe 13,281 hrs · 14,443 cycles

AFTER GEAR RETRACTION, #1 SIDE SHOWED UNSAFE INDICATION FOR DOORS, GEAR, AND HANDLE REMAINED ILLUMINATED. #1 DOORS REMAINED OPEN. PERFORMED ALTERNATE GEAR EXTENSION AND SHOWED 3 GREEN. REMOVED FROM SERVICE. GEAR AND MLG DOOR PINS INSTALLED. CLEANED AND INSPECTED #1 UPLOCK ASSY. FOUND ONE EXTENSION SPRING BROKEN. REMOVED AND REPLACED SPRING IAW Q400 TASKS 32-31-21-000-803 AND 400-803. OPS CHECK C/W 6 TIMES. OPS CHECK GOOD. LUBED #1 UPLOCK ASSY IAW AMM TASK 12-20-01-640-803. GEAR AND MLG DOOR PINS REMOVED AND STOWED. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — SMOKE (RIGHT) · airframe 12,607 hrs · 13,643 cycles

RT INSIDE MAIN LANDING GEAR SMOKING AFTER PARKED AT THE GATE. STOPPED SMOKING AFTER ABOUT 15 MINS. REMOVED FROM SERVICE. PERFORMED GVI OF BOTH #3 & #4 MLG BRAKES NO FLUID LEAKING OBSEVERED, CYCLED BRAKES 3 - 4 TIMES CYCLED PARKING BRAKE NO DEFECTS NOTED AIRCRAFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,582 hrs · 13,613 cycles

AFT LH EXTERNAL EMERGENCY LIGHT INOP. REPLACED #4 POWER SUPPLY UNIT REF AMM 33-51-01-000/-400-801. ALSO REPLACED L4 AND R4 EPSU BATTERY PACKS REF AMM 33-51-00-820-801. EMERGENCY LIGHT SYSTEM OP CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,151 hrs · 13,083 cycles

DURING CRUISE FA CALLED REPORTING A RUBBER BURNING SMELL IN FORWARD CABIN. NO INDICATION OF FIRE OR SMOKE. TURNED BLEEDS TO FULL COLD AND MAX. SMELL DISSIPATED. REMOVED FROM SERVICE. NO SMELL OR UNUSUAL ODOR DETECTED. PERFORMED GVI OF CABIN & FLT DECK AREA NO DEFECTS FOUND. OPERATED ALL CABIN INTERIOR LIGHTS. OPERATED LAVATORY LIGHTS AND FLUSH. OPERATED PSU FUNCTIONS. GROUND RAN BOTH ENGINES IN IDLE WITH BLEEDS ON, AUTO, MAX FLOW. STABILIZED FOR FIVE MINUTES IN EACH FULL COLD AND HOT. NO CAUTIONS, WARNING, ABNORMAL INDICATIONS OR SMELLS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PIN — UNSECURE (EMERGENCY DOOR) · airframe 11,914 hrs · 12,788 cycles

PIN STICKING OUT ON FORWARD EMERGENCY DOOR HANDLE AND AFT HANDLE AFT PASSENGER DOOR. REMOVED FROM SERVICE. RESECURED PINS ON DOORS AS REQUIRED. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 11,880 hrs · 12,745 cycles

INTERMITENT DEICE PRESS CAUTION LIGHTS FOLLOWED BY BOOTS NOT INFLATING IN SLOW OR FAST MODE BOOTS DID INFLATE WHEN SELECTED MANUALLY. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS FOUND NO FAULT CODES, NO CAUTION ON CAUTION ADVISORY PANEL. PERFORMED FUNCTIONAL TEST IAW AMM 30-11-00-720-801 FUNCTIONAL TEST GOOD. R&R TMU AS A PRECAUTIONARY, PERFORMED FUNTIONAL TEST REF AMM 30-11-00-720-801 FUNCTIONAL TEST GOOD. FOUND NO FAULT CODES, NO CAUTION ON CAUTION ADVISORY PANEL. R&R OF TMU WAS DONE IAW AMM 30-11-01-000-801/400-801.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 11,820 hrs · 12,677 cycles

PHOTOLUMINESCENT STRIP AT BULKHEAD IN FRONT OF 2 D/E IS COMING UP. REMOVED FROM SERVICE. RESECURED LIGHTING STRIP. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 11,775 hrs · 12,626 cycles

FLOOR STRIP AT 2D/E COMING UP. REMOVED FROM SERVICE. RESECURED FLUORESCENT STRIP @ 2DE WITH TAPE AS REQUIRED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (SEAT 2D) · airframe 11,609 hrs · 12,442 cycles

LUMINESCENT STRIP AT SEAT 2D IS PEELING UP ( FLOOR PROX LIGHTING INOP ) REMOVED FROM SERVICE. R & R LUMINESCENT STRIP FORWARD OF SEAT 2D IAW Q400 AMM 33-51-16-000-801/-400-801 & MCN 625868-001, ISSUE 2. THIS CLEARS MEL. MAINT CONTROL NOTIFIED. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (PAX DOOR) · airframe 11,367 hrs · 12,173 cycles

AFT PASSENGER DOOR, 2 BEAM CRACKED. REMOVED CRACKED BEAM FROM AFT PASSENGER DOOR IAW SRM 51-42-05-02-01. FIT AND DRILLED NEW BEAM PN 85217419-105 IAW SRM 51-40-07-02-01. INSTALLED NEW BEAM PN 85217419-105 ON AFT PASSENGER DOOR IAW SRM 51-23-00-00-01, 51-40-15-02-01, 51-42-05-02-01 AND 51-42-45-02-01.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 11,367 hrs · 12,173 cycles

SEAT RAIL #10 FROM FSX-39.00 -X10.50 Y9.250 IS CORRODED. REMOVED SEAT RAIL #10 FROM FSX -39.00 - FSX 10.50 AT Y9.250 IAW SRM 51-42-05-00-01, 51-41-05-00-01 AND 51-40-15-02-01. INSTALLED SEAT RAIL #10 FROM FSX -39.00 -FSX 10.50 AT Y9.250 IAW SRM 51-42-05-00-01, 51-41-05-00-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (NR 9) · airframe 11,367 hrs · 12,173 cycles

SEAT RAIL 9 FROM FSX 670.00-X783.00 Y-9.250 IS CORRODED. CORRODED SEAT RAIL 9 FROM FS X670.00 -X783.00 Y-9.250 REMOVED AND REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 11,367 hrs · 12,173 cycles

SEAT RAIL 11 FROM FSX10.50-X102.50 IS CORRODED. REMOVED SEAT RAIL #11 FROM FSX 10.50- X102.50 IAW SRM 51-42-05-00-01, 51-41-05-00-01 AND 51-40-15-02-01. INSTALLED SEAT RAIL #11 FROM FSX 10.50 -X102.50 IAW SRM 51-42-05-00-01, 51-41-05-00-01 AND 51-40-15-02-01.

Part: GOVERNOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 11,107 hrs · 11,891 cycles

ON INITIAL CLIMB, NR 1 RPM SHOWED 1010 WITH CONDITION LEVERS MAX. CONDITION LEVERS BROUGHT BACK TO 900. NR 1 PROP RPM DROPPED TO 890. THEN EVENTUALLY 850. TORQUE WAS CONSISTENTLY 6% OVER TORQUE BUG, BUT NEVER EXCEEDED ANY LIMITS. PRECAUTIONARY RETURN TO FIELD LANDING WAS MADE. DURING APPROACH, CONDITION LEVERS SELECTED TO 1020 (THEY WERE NEVER SELECTED TO 850) AND RPM ON NR 1 PROP REMAINED AT 850. NO OTHER CAUTIONS, WARNINGS OR MESSAGES DISPLAYED AT ANY TIME. EVENT MARKER PUSHED. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 OSG. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 2 DC) · airframe 11,067 hrs · 11,842 cycles

RAMP REPORTED SPARKS COMING FROM #2 ENGINE. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 DC GEN IAW Q400 AMM TASKS 24-31-01-000-801/24-31-01-400-801 DUE TO GENERATOR SHAFT SHEAR. PERFORMED OPS TEST IAW Q400 AMM TASK 24-31-00-710-802. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — LEAKING (FEATHERING SYS) · airframe 10,953 hrs · 11,718 cycles

NR 2 ENGINE FEATHERING PUMP IS LEAKING AT LOWER PUMP HOUSING COVER. REPLACED NR 2 ENGINE FEATHERING PUMP IAW MM TASK NR'S 61-20-31-000-801 AND 61-20-31-400-801. NR 2 PROPELLER ALTERNATE FEATHER OPERATIONAL TEST GOOD IAW MM TASK 61-20-00-710-802. NO LEAKS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED SYSTEM) · airframe 10,852 hrs · 11,610 cycles

AFTER V1, THE NR 1 AND 2 BLEED HOT CAUTION ILLUMINATED. UNABLE TO PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTEROGATED CDS AND FOUND FAULT CODES 7008 ON LT AND RT SIDE PERFORMED IAW FIM 36-10-00-810-857 AND 36-10-00-810-856. PERFORMED AN OPERATIONAL TEST OF THE BLEED AIR SYSTEM FAULTS, NO LONGER PRESENT, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SPRING — BROKEN (MLG) · airframe 10,736 hrs · 11,471 cycles

AFTER TAKEOFF, THE LT DOOR & RED LANDING GEAR LIGHT & GEAR SELECTOR LIGHT REMAINED ILLUMINATED. RAN RED LEFT NOSE, RIGHT GEAR LIGHTS REMAINS ILLUMINATED ANDGEAR HANDLE LIGHT ILLUMINATED. CHECKLIST THAT LED TO THE LANDING GEAR FAILED TO RETRACT CHECKLIST. AFTER CONFIGURATION CHECK IAW LANDING GEAR FAILS TO RETRACT CHECKLIST & EP, WE RAN ALTERNATE GEAR EXTENSION CHECKLIST. AFTER COORDINATING WITH DISPATCH, I ELECTED TO DIVERT TO PDX. NOTE: NEVER EXCEEDED 185KIAS. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CHECKED PSEU FOR FAULTS AND FOUND LGUPLK AND LGDRCL UNRSNALRL FAR FAULTS. PERFORMED INDUCTANCE VALUE CHECK OF LGUPLK AND LGDRCL WITH GEAR RETRACTED AND DOOR CLOSED REF M/M TASK 32-61-00-280-801, VALUES OF SENSORS ARE GOOD. INSPECTED LEFT GEAR UPLOCK ASSY AND FOUND ONE SPRING BROKEN. 62200. REF Q400 AMM 32-31-21-000-803 REMOVED BROKEN MLG UPLOCK SPRING. REF Q400 AMM 32-31-21-400-803 INSTALLED NEW MLG UPLOCK SPRING. OPS CHECK GOOD. REF Q400 AMM 32-31-00-710-801 PERFORMED LANDING GEAR OPS TEST. OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 10,290 hrs · 10,950 cycles

RIGHT DOOR AND RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKE OFF AND GEAR RETRACTION. RIGHT MAIN GEAR RETRACTED, BUT GEAR DOOR REMAINED OPEN. ALTERNATE GEAR EXTENSION CHECKLIST ACCOMPLISHED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE.

Part: WHEEL — SMOKE (MLG) · airframe 8,899 hrs · 9,521 cycles

ON POST FLIGHT INSPECTION. NOTED SMOKE COMING FROM RT MLG WHEELS. LANDING, BRAKING AND TAXI IN ALL NORMAL. REMOVED FROM SERVICE. RECORDED TEMPS OF MLG BRAKES / WHEEL ASSY'S WITH DIGITAL THERMOMETER, HIGHEST RECORDED TEMPS AT 10 MIN. POST ARRIVAL WERE 1-426 DEG. F. , 2-428 DEG. F. , 3-638 DEG. F. AND 4 627 DEG. F. AT INNER BRAKE / AXLE MATING AREAS. PERFORMED GVI OF MLG WHEEL / BRAKE ASSY'S IAW AMM 32-40-0-210-802, NO DEFECTS NOTED. NO LEAKS, EXCESSIVE GREASE OR DISTORTION OF ANY COMPONENTS NOTED. JACKED R/H MLG ( AFTER COOLING WITH FANS UNTIL ALL TEMPS WERE < 250 DEG. F). ROTATION OF WHEELS NORMAL WITH BRAKES RELEASED & ALL TIRE PRESSURES NORMAL FOR MLG. NO OTHER DEFECTS NOTED, NO FURTHER SMOKING NOTED AFTER INITIAL COOL - DOWN. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — MALFUNCTIONED (RUDDER SYS) · airframe 8,490 hrs · 9,079 cycles

ABNORMAL RESISTANCE FELT WITH RUDDER PEDAL INPUT TO RIGHT SIDE REQUIRING MORE FORCE THAN NORMAL. WAS ABLE TO OVERCOME RESISTANCE. RUDDER CONTROL WAS AVAILABLE FOR LANDING. SIGNIFICANTLY GREATER PRESSURE ON CLIMB OUT THAN ON APPROACH. NEGLIGIBLE DIFFERENCE ON GROUND RUDDER CHECK. STANDARD SETTINGS. GREATER RESISTANCE NOTED BY CA THAN BY FO. C/W OPERATIONAL CHECK OF RUDDER CONTROL SYSTEM REF AMM 27-20-00-710-802/803 AND TR 27-438, C/W VISUAL INSPECTION OF PILOTS RUDDER PEDALS FREEDOM OF MOVEMENT IN ALL RUDDER PEDAL CONFIGURATIONS, C/W HANDS ON AND VISUAL OF RUDDER ASSY, NO DEFECTS NOTED, NO HISTORY LAST 90 DAYS C/W FREEDOM OF MOVEMENT CHECK IAW GPM 9.2.5. OPERATIONAL CHECK FLIGHT PER GPM 7.4.2 (8F). OPERATIONAL CHECK FLIGHT SATISFACTORY. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,383 hrs · 8,957 cycles

EMERGENCY LIGHTS SWITCH BULB AT THE FLIGHT ATTENDENT A STATION BURNED OUT AT THE NORMAL POSITION. REPLACED THE BULB, OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,207 hrs · 8,768 cycles

FLIGHT ATTENDANTS NOTICED A FOREIGN ODOR IN THE CABIN DURING CRUISE. IT WAS A STRONG SCENT OF BURNING PLASTIC BETWEEN ROWS 10-15 FOR ABOUT 3-5 MINUTES. NO SMOKE WAS OBSERVED. FIVE MINUTES PRIOR TO THE ODOR, PROPELLER HEAT AND ENGINE HEAT WAS SELECTED ON. COMPLIED WITH AIR CONTAMINATION CHECKLIST . F/A'S NOTED ODOR STRONGEST AT ROWS 12 & 13. PERFOMED GVI OF MID CABIN AREA, NO ODORSOR DISCOLORATION NOTED. LOWERED PSU PANELS ABOVE ROWS 12 & 13, NO DEFECTS NOTED. GROUND RAN BOTH ENGINES, TURN ON EVERY CABIN LIGHT, RAN BOTH PACKS AND COMPLIED WITH OPS TEST OF ENGINE AIR INTAKE ANTI-ICING AND FUNCTIONAL TEST OF PROP DECING SYSTEM. NO ODORS NOTED. NO RECENT HISTORY. INSTALLED LOWERED PSU PANELS. IAW AMM TASKS 30-61-00-720-801, & 30-21-00-710-801. ACFT OK FOR CONTINUE SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,085 hrs · 8,634 cycles

AFTER DEPARTURE FROM FCA RECEIVED CABIN ALTITUDE WARNING. UPON ARRIVAL INSPECTED ALL DOORS, N/D/N. INTERROGATED CDS AND FOUND FAULT CODE 'CPC/OF VALVE DATA FAIL' C/W FIM TASK 21-30-00-810-804. DOOR SEAL INTEGRITY CHECKS GOOD. A/C PRESSURIZES NORMALLY. FAULT CODE DID NOT RE-OCCUR. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 8,060 hrs · 8,607 cycles

FA'S REPORT FLOOR EMERGENCY LIGHTING STRIPS LOOSE BY ROWS 1 AND 2. SECURED LOOSE LIGHTING STRIPS. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 7,999 hrs · 8,543 cycles

SMOKE MASTER WARNING IS INTERMITTENTLY ILLUMINATING. IN CONJUNCTION WITH THE WARNING LIGHT, THE BAGGAGE AFT VENT INLET VALVE OUTLET CLOSED. GUARDED SMOKE EXTG AND FIRE BOTTLE AFT ILLUMINATES. REMOVED AND REPLACED AFT CARGO AFT SMOKE DETECTOR PER Q400 AMM 26-12-01-400-801. OP'S CK GOOD. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 8,000 hrs · 8,544 cycles

SMOKE WARNING ILLUMINATED. UNABLE TO DUPLICATE. "SMOKE" WARNING NOT ILLUMINATED. R & R FORWARD SMOKE DETECTOR IN AFT CARGO BAY. IAW AMM 26-12-01-00-801 AND 26-12-01-400-801. OPS TEST PASSED. SMOKE WARNING DOES NOT ILLUMINATE. RAN BOTH ENGINES TO DUPLICATE ACTIVE AIRCRAFT VIBRATIONS. SMOKE WARNING DOES NOT ILLUMINATE. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 7,925 hrs · 8,464 cycles

SMOKE WARNING AND CHECK FIRE DETECT WARNING LIGHT ILLUMINATED IN FLIGHT. FIRE BOTTLE DISCHARGED. NO SMOKE OR FIRE DETECTED. FLIGHT CONTINUED. LANDING UNEVENTFUL. INSPECTED AND FOUND NO SIGN OF FIRE OR SMOKE. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW AMM 26-12-06-000-801/400-801 OPS CHECK GOOD IAW 26-12-06-710-801. FIRE BOTTLE REPLACED. RETURNED TO SERVICE.

Part: BLOWOUT PANEL — DISLODGED (AFT CARGO BAY) · airframe 7,776 hrs · 8,312 cycles

DURING CLIMBOUT, THE CABIN RATE SPIKED TO OVER 3000 FPM. FLIGHT ATTENDENT LATER REPORTED HEARING A BANG. RAN THE PRESSURIZATION FAIL CHECKLIST AND WERE ABLE TO CONTROL THE PRESSURIZATION IN MANUAL MODE. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND AFT CARGO BAY AFT BLOW OUT PANEL DISLOGED. INSTALLED AFT CANTED BULKHEAD BLOW OUT PANEL IAW AMM 25-52-01-400-802. PERFORMED FUNCTIONAL TEST OF THE PRESSUIZATION CONTROL IAW AMM 21-31-00-720-801. TESTS GOOD. PERFORMED INTEGRITY CHECK OF THE AFT CARGO DOOR SEAL. CHECKS GOOD. ACFT OK FOR SERVICE. INTEGRITY CHECK WAS DONE IAW AMM 52-31-26-790-801. RETURND TO SERVICE.

Part: LIGHT — LOOSE (ROW 2) · airframe 7,170 hrs · 7,654 cycles

EMERGENCY LIGHT STRIP AT ROW 2 IS DISLODGED. CLEANED AND REATTACHED WITH NEW TAPE. RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 6,947 hrs · 7,416 cycles

FLAP POWER CAUTION LIGHT DURING FINAL APPROACH, WHEN SELECTING FLAPS 35 DEG. CANCELLED APPROACH KEEPING THE AIRSPEED UNDER FLAPS 15 SPEED LIMITATION AND RAN THE CHECKLIST. THE FLAP POWER CAUTION LIGHT ILLUMINATED AGAIN, AFTER THE FLAPS CONT CICUIT BREAKER RESET. EXECUTED A NORMAL FLAP 15 LANDING. NO CURRENT FAULTS IN CDS. CYCLED A/C POWER PERFORMED OPS TEST OF WING FLAPS IAW AMM 27-50-00-710-801. OPS TEST PASSED. EXTENDED AND RETRACTED THE FLAPS FIVE TIMES, PERFORMED GVI O FLAPS FROM GROUND WHILE AT 35 DEG. NO DEFCETS NOTED. "FLAP POWER" CAUTION DID NOT ILLUMINATE AT ANY TIME. FLAPS OPERATE NORMAL. NO PARTS REPLACED.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 5,806 hrs · 6,181 cycles

EDGE CHANNEL ON AFT SERVICE DOOR CORRODED. REPLACED IAW SRM 53-40-21, SRM 51-24-35, REPAIR-01 AND DWG. 85339543, REV-A.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 5,806 hrs · 6,181 cycles

FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-05, AND SRM 51-42-05.

Part: BEAM — CORRODED (ZONE 100) · airframe 5,806 hrs · 6,181 cycles

OUTER EDGE BEAM FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-07, DWG 8533951, AND SRM 51-42-05.

Part: BEAM — CORRODED (CORRODED) · airframe 5,806 hrs · 6,181 cycles

INNER EDGE BEAM FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-07, SRM 51-42-75, SRM 51-41-05, AND 51-42-45.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,578 hrs · 5,948 cycles

EMERGENCY LIGHT SWITCH LAMP IS INOPERATIVE. REPLACED THE LAMP. RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — FAILED (WINDSHIELD) · airframe 5,527 hrs · 5,886 cycles

WINDSHIELD CENTRAL CAUTION, AFTER TAKOFF FOUND CIRCUIT BREAKER LT WINDSHIELD HEAT TRIPPED. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED LT WINDSHIELD HEAT CB FOUND BURNED AND DAMAGED IAW AMM'S 24-00-00-000-801/400-801. RETURNED TO SERVICE.

Part: ROLLER — DAMAGED (TE FLAPS) · airframe 5,244 hrs · 5,579 cycles

ON CLIMBOUT WHILE RETRACTING FLAPS FROM 15 TO 0, FELT A SHUDDERING. AFTER CONSULTING WITH MAINTENANCE CONTROL IT RESULTED IN A RETURN TO FIELD. LANDING UNEVENTFUL. UPON APPROACH, WHILE EXTENDING THE FLAPS FOR LANDING WE FELT THE SAME SHUDDERING WHILE EXTENDING FLAPS TO ALL POSITIONS. PERFORMED GVI OF FLAP DRIVE SYSTEM, FPU, FLAP ACTUATORS, AND INBD AND OTBD FLAP TRACK ROLLERS. REPLACED RT INBD FLAP ROLLERS, ALL 4. COMPLETED FREEDOM OF MOVEMENT, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED. OPS CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: STRUCTURE — OUT OF POSITION (LAVATORY DOOR) · airframe 4,433 hrs · 4,733 cycles

COCKPIT DOOR STICKS ON THE LAVATORY DOOR TRIM ON THE TOP OF THE OPENING. REPOSITIONED TRIM ON LAVATORY DOOR. DOOR NOW OPERATES NORMALLY. RETURNED TO SERVICE.

Part: SEAL — DIRTY (PAX DOOR) · airframe 4,021 hrs · 4,304 cycles

AFT PASSENGER DOOR DIFFICULT TO OPEN. INSPECTED AND FOUND SEAL STICKY. CLEANED AND LUBED SEAL. DOOR OPERATES NORMALLY. RETURNED TO SERVICE.

Part: SEAL — CONTAMINATED (AFT PAX DOOR) · airframe 4,021 hrs · 4,304 cycles

AFT PASSENGER DOOR DIFFICULT TO OPEN. FOUND BULB SEAL TO BE STICKY. CLEANED AND LUBED SEAL. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: BEARING — DAMAGED (SERVICE DOOR) · airframe 3,174 hrs · 3,392 cycles

SERVICE DOOR IS DIFFICULT TO OPEN. TURN FORCE WAS 60 LBS. FERRIED FOR REPAIRS. REPLACED EXTERNAL HANDLE ROTATIONAL PIVOT BEARINGS AND BUSHING. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST · airframe 2,982 hrs · 3,200 cycles

DURING DAILY SYSTEM CHECK OF THE AUTOFEATHER SYSTEM, AF TEST "ABORT" OBSERVED ON DISPLAY. INTERROGATED CDS NO FAULTS CHECKED. CIRBUIT BREAKERS FOUND K4 RT C/B UP. RESET K-4 REF GPM 9.2.2.1. RAN ENGINES K-4 C/B, RIGHT STAYED SET. C/W AUTO FEATHER TEST AMM TASK 61-20-00-710-805, TEST PASSED. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: COVER — BROKEN (LIGHT SWITCH) · airframe 2,627 hrs · 2,815 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH COVER BROKEN. SECURED THE COVER. RETURNED TO SERVICE.

Part: BUMPER — FAILED (PAX DOOR) · airframe 2,454 hrs · 2,637 cycles

MAIN CABIN DOOR HANDLE RETRACTS TOO FAR INTO RECESS, IS VERY HARD TO OPEN. APPEARS A BUMPER IS BROKEN. REMOVED & REPLACED MCD HANDLE BUMPER STOP AS REQUIRED. OPS CHECKED OF DOOR HANDLE GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 953 hrs · 1,023 cycles

F/A REPORTED FLOOR EMERGENCY LIGHT LOOSE AT ROW 2 D/E. SECURED LIGHT, NO OTHER DEFECTS NOTED.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 790 hrs · 839 cycles

DURING CLIMB, GEAR DOOR INDICATOR SHOW RED ON THREE GEAR. AIRSPEED BETWEEN 220-225KTS. AFTER SLOWING BELOW 200KTS GEAR CYCLED, CAME UP NORMAL. NORMAL AFTER THAT. CHECKED PSEU FAULT HISTORY FOR LEG OF ORIGINAL WRITE UP AND FOUND FAULTS NWCTR UNREASONABLE FAR, DIN02A UNREASONABLE TRUE AND DINO1A UNREASONABLE FALSE. NOSEWHEEL CENTER PROXIMITY SENSOR INDUCTANCE VALUE CHECKED GOOD IAW MM TASK 32-61-00-280-801, NOSEWHEEL STEERING SYS FUNCTIONAL TEST GOOD IAW MM TASK 32-51-00-720-801, REPLACED PSEU IAW MANAGEMENT REQUEST. REPLACED LANDING GEAR CONTROL PANEL IAW MANAGEMENT REQUEST. LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM FUNCTIONAL TESTED GOOD FIVE TIMES IAW MM TASK 32-31-00-720-801. RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 473 hrs · 512 cycles

F/A REPORTS UNABLE TO PREFLIGHT RT EMERGENCY EXIT DITCHING DAM. LUBED ACCESS DOOR FOR HANDLE. OP'S CHECKED GOOD. RETURNED TO SERVICE.

Part: HINGE — OUT OF ADJUST (COCKPIT DOOR) · airframe 309 hrs · 346 cycles

FLIGHT DECK DOOR IS STICKING. DIFFICULT TO OPEN AND CLOSE. ADJUSTED UPPER AND MID HINGES FOR IMPROVED FIT OF DOOR. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 196 hrs · 214 cycles

ON THE GROUND WITH APU RUNNING AND BLEEDS ON, FLIGHT DECK AND CABIN FILLED WITH WHITE SMOKE LIKE SUBSTANCE. WHEN APPROACHING ACFT, NOTICED ACFT WAS RECENTLY DE-ICED PERFORMED GVI OF APU AREA, NOTICE APU COMPARTMENT WAS WET W/ DE-ICE FLUID. CLEAN APU AREA. COMPLIED WITH MCN NO 62172-01 FOR TROUBLESHOOTING OF SMELL IN ACFT, REF PROCEDURE 3, ODOR OR SMOKE WAS CAUSED FROM DE-ICE FLUID FROM APU. COMPLIED WITH AMM TASK 21-00-00-160-801 FOR REMOVAL OF ODOR FROM ACFT DUCT. NO ODOR WAS NOTED DURING CHECK AND NO SMOKE WAS NOTED. TAXI ACFT TO RUN PAD AND GROUND RAN ENGINES AT POWER WITH BLEEDS ON AND NO ODOR OR SMOKE LIKE SUBSTANCES NOTED IN CABIN OR FLT DECK. PERFORMED OPS TEST OF PSU IAW AMM TASK 21-22-00-710-801. OPS TEST GOOD. NO ODOR OR SMOKE LIKE SUBSTANCES NOTED. NO OTHER DEFECTS NOTED.

Part: WIRE — CROSSED (CABIN PRESSURE) · airframe 13 hrs · 10 cycles

ACFT WOULD NOT PRESSURIZE IN FLIGHT. RAN E & A CHECKLIST, STILL WOULD NOT PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND WIRES 2131-102A-22-4 AND 2131-148A-22-4 CROSSED. RETERMINATED ACCORDING TO WM 46-30-01 HS 46-002. WIRE RINGS OUT GOOD. CDS SHOWS NO PRESENT FAULTS. RETURNED TO SERVICE.