N446QX

Part: DISPLAY — NONE (ZONE 200) · airframe 22,806 hrs · 24,450 cycles

#1 ARCDU CONTINUES TO CYCLE ON AND OFF. DIVERTED. REMOVED FROM SERVICE. REMOVED AND REPLACED #1 ARCDU IAW CAT III RTS TC 6238101 ALSO REMOVED #2 ARCDU TO FOM AND REINSTALLED IAW RTS TC 6238101 OPS CKS GOOD AIRCRAFT REMAINS CAT III PLACARD READS CAT III MTX CONTROL NOTIFIED. AIRCRAFT RETURNED TO SERVICE.

Part: STARTER GEN — MALFUNCTIONED (APU) · airframe 22,452 hrs · 24,076 cycles

WHEN APPLYING POWER TO THE AIRCRAFT, THE APU STARTER GENERATOR STARTS TO SMOKE WITHOUT TURNING ON THE APU. REPLACED THE APU STARTER GENERATOR IAW Q400 AMM 24-33-01-000-801/400-801.

Part: ADJUSTER — OUT OF ADJUST (OIL PRESSURE) · airframe 22,407 hrs · 24,029 cycles

OIL PSI FLUCTUATION 5+= MOVED INTO THE YELLOW ARC ON THE HIGH SIDE. DIVERTED. REMOVED FROM SERVICE. REF Q400 AMM 71-00-00-780-801 ADJUSTED OIL PRESSURE ADJUSTER APPROX ONE QUARTER TURN COUNTER CLOCKWISE ON #2 ENG. RUNS AND LEAK CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER LEVER — MALFUNCTIONED (ZONE 200) · airframe 21,746 hrs · 23,359 cycles

#2 PEC CAUTION DURING LANDING ROLL THROUGH 50 KTS. POWERPLANT MESSAGE ON ED. RETRIEVED FAULT CODES IAW Q400 AMM 77-31-00-710-803. HAD FAULT CODE 200 AB, 126A, AND 134 (ON #2 SIDE). REPLACED RELAY 6100-3-K2 RJB1 IAW AMM TASK 24-30-16-960-801. OPS TEST GOOD IAW AMM TASK 24-60-710-801. REPLACED PLA IAW AMM 76-10-01-000-801 + 76-10-01-400-801. ALL OPS TEST GOOD. ALL FAULT CODES CLEARED AND DID NOT REAPPEAR. RETURNED TO SERVICE.

Part: POWER LEVER — MALFUNCTIONED (ZONE 200) · airframe 21,563 hrs · 23,179 cycles

#2 PEC CAUTION AFTER TOUCHDOWN WHILE DECELERATING THROUGH 60KTS WITH POWERPLANT MESSAGE DISPLAYED ON ED WHILE PULLING INTO THE GATE. REMOVED FROM SERVICE. INTERROGATED CDS FOUND FAULT CODE "200" IN BOTH CHANNELS. C/W Q400 FIM TASK 61-20-05-810-817 STEP 4(E). FAULT CODE DID NOT RETURN. #2 PEC CAUTION LIGHT REMAINS EXTINGUISHED. REF LP 937216 FOR 50 FH DMI TO REPLACE PLA QUADRANT AND K-3 RELAY OR K-2 RELAY. RETURNED TO SERVICE. RETRIEVED FAULT CODES IAW Q400 AMM 77-31-00-710-803. HAD FAULT CODE 200 AB, 126A, AND 134 (ON #2 SIDE).REPLACED RELAY 6100-3-K2 RJB1 IAW AMM TASK 24-30-16-960-801. OPS TEST GOOD IAW AMM TASK 24-60-710-801. REPLACED PLA IAW AMM 76-10-01-000-801 + 76-10-01-400-801. ALL OPS TEST GOOD. ALL FAU

Part: POWER LEVER — MALFUNCTIONED (ZONE 200) · airframe 21,564 hrs · 23,179 cycles

#2 PEC CAUTION LIGHT ILLUMINATED. REQUIRES TO REPLACE THE PLA QUADRANT, AND K-3 OR K-2 RELAY WITHIN 50 FLT AFTER DISCOVERY OF THE FAULT CODE POSTING PER Q400 MCN 6610594 ISSUE NO. 2. 3/10,RETRIEVED FAULT CODES IAW Q400 AMM 77-31-00-710-803. HAD FAULT CODE 200 AB, 126A, AND 134 (ON #2 SIDE). REPLACED RELAY 6100-3-K2 RJB1 AND PLA, ALL PLACARDS REMOVED. CB'S SET THIS CLEARS DMI. RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (AOA INDICATE SYS) · airframe 21,344 hrs · 22,973 cycles

IN CRUISE AT 25000 'PUSHER SYST FAIL' CAUTION LIGHT ILLUMINATED. RAN E&A CHECKLIST TURNED OFF STICKER PUSHER SHUTOFF. NO LOW SPEED CUE ON AIRSPEED TAPE. AFTER LANDING ON ROLLOUT BOTH NR 1 & NR 2 STALL SYST FAIL CAUTION LIGHTS ILLUMINATED. REMOVED FROM SERVICE. FOUND CB AT LEFT AOA HEAT POPPED. RESET CB AND PERFORMED ENGINE RUNS WITH CREW, CB POPPED. R & R LT AOA TRANSDUCER REF Q400 AMM TASK 27-33-26-000-801 & 27-33-26-400-801. PERFORMED FUNCTIONAL TEST REF AMM 27-33-26-720-801. FUNCTIONAL TEST GOOD. RESET BREAKER & PERFORMED ENG RUN. CB DID NOT POP. PERFORMED AOA SENSOR-HGS RETURN TO SERVICE CATIII OPS TEST IAW MTC 6273302. AC REMAINS CAT I QUALIFIED. COCKPIT PLACARD READS CAT I. MTX CONTROL NOTIFIED. AC REMAINS CAT DUE TO FMS NR 1 MEL.. AIRCRAFT RETURNED TO SERVICE.

Part: MANIFOLD — INOPERATIVE (HYD SYSTEM) · airframe 21,303 hrs · 22,932 cycles

AFTER COMPLETING THE AFTER TAKEOFF CHECKLIST THE STBY HYD PRESS GUAGE SHOWED 3000 PSI STBY HYD PRESS SWITCH WAS CONFIRMED OFF (OUT), DIVERSION. REMOVED FROM SERVICE. RAN NR 1 ENGINE AND WAS ABLE TO DUPLICATE DISCREPANCY, WHEN ENGINE HYDRAULICS COME ONLINE, STBY HYD PRESS SLOWLY INCREASES. REPLACED PORT MOUNTED CHECK VALVE ON NR 1 HYD MANIFOLD, NO HELP, REF AMM 29-11-71-000/400-801. R & R NR 1 HYD MANIFOLD, REF AMM 29-11-31-000-801. STBY HYD SYS OPERATIONS CHECKS GOOD. LEAKS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DISTRIBUTION VLV — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 21,185 hrs · 22,795 cycles

ON CLIMB DE-ICE PRESS CAUTION ILLUMINATED. WOULD CYCLE THROUGH TO LEFT OUTBOARD BOOT WOULD NOT DEFLATE ON "SLOW" OR "FAST" BUT WORKED IN MANUAL MODE. DIVERTED AND ACCOMPLISHED AN UNEVENTFUL LANDING. REMOVED FROM SERVICE. C/W DETAILED INSPECTION OF DE-ICING BOOTS, IAW Q400 AMM TASK 30-11-00-280-802 STEPS (1-4). C/W DETAILED INSPECTION OF DE-ICE BOOTS, IAW Q400 AM 30-11-00-280-802 STEP 5. REPLACED LEADING EDGE AND DDV NR 6 REMOVAL AND REPLACEMENT. DE-ICE CAUTION LIGHT DID NOT ILLUMINATE. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (MLG SELECTOR) · airframe 21,086 hrs · 22,686 cycles

UPON GEAR DOWN THE RT MAIN GEAR INDICATION DID NOT INDICATE GEAR DOWN. RAN GEAR DOWN FAILS TO INDICATE DOWN CHECKLIST. OBTAINED POSITIVE GEAR DOWN FROM ALT GEAR DOWN IND AND FLIGHT ATTENDANTS. LANDED UNEVENTFULLY. REMOVED FROM SERVICE. FOUND INDICATION HEAD PERIODICALLY WORKING WHEN MOVED. REMOVED LANDING GEAR CONTROL PANEL, PER AMM 32-31-01-000-801. INSTALLED NEW UNIT, PER AMM 32-31-01-400-801. FUNCTIONAL TEST GOOD. A/C OK FOR CONTINUED SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,798 hrs · 22,395 cycles

DEPARTING, THROUGH 12,500 WE GOT A CABIN PRESS WARNING. WE RAN THE CABIN PRESS CHECKLIST (IAC) AND PRESS FAIL CHECKLIST (EAC) AND CONFIRMED THE BLEEDS WERE ON AND THE OACKS WERE IN AUTO W/ THE PRESS LDG ALT PROPERLY SET. THERE WAS NO FAULT LIGHT ON THE PRESS PANEL. WE SED THE O2 MASKS AND O2 IS NOW LOW. WE RETURNED TO RDM WITH NO FURTHER ISSUES. RETURNED TO FIELD. CHECKED CDS & CPCS FAILURE REPORTING SYSTEM NO FAULTS FOUND. ECS SHOWS 3801-0255 & 3003-PACK PCV. REQUIRES FURTHER T/S & PRESSURIZATION AH 19292. C/W FIM SUBTASK 21-30-00-810-001. AFT CAGO PANEL (BLOWOUT) OK. DOOR SEALS OK. ECS BAY OK. NO ACTIVE FAULTS FOUND IN ECS, CDS/CPCS. FUNCTIONAL TEST GOOD. NO CURRENT FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: TIMER — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 20,258 hrs · 21,773 cycles

ON CLIMB OUT WE ENCOUNTERED ICING AND AFTER TURNING ON THE BOOT THE DEICE TIMER CAUTION ILLUMINATED IN SLOW & FAST. PERFORMED E&A CHECKLIST,BOOTS WORKED IN MANUAL. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CHECKED CDS FOR FAULTS. ICE/RAIN FAULTS ARE UNAVAILABLE DUE TO ICE/RAIN SYS UNAVAILABLE. REMOVED AND REPLACED TMU IAW Q400 AMM TASKS 30-11-01-000-801 AND 400-801. USING ENGINES, C/W FUNCTION TEST OF AIRFRAME PNEUMATIC DEICING SYSTEM IAW Q400 AMM TASK 30-11-00-720-801. FUNCTION TEST GOOD. NO FAULTS POSTED IN CDS. DEICE TIMER CAUTION DID NOT ILLUMINATE. RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED · airframe 20,169 hrs · 21,670 cycles

WHILE IN CRUISE, CREW RECEIVED ENG ADPT HEAT 2 CAUTION ENG INTAKE HTR ADVISORY LIGHT WENT OUT AT THE SAME TIME. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND "INTAKE LIP HTR ENG 2" CIRCUIT BREAKER POPPED. PUSHED C/B IN, CLEARED CDS FAULT REF GPM 9.2.2.1. PERFORMED ENGINE AIR INTAKE ANTI-ICING OPS TEST REF Q400 AMM 30-21-00-710-801. OPS CHECK GOOD. NO FAULTS RETURNED. CLEAR DEFECT, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,906 hrs · 21,345 cycles

FWD PAX DOOR ENTRY WAY EMERG LIGHTS INOP. REMOVED LH 1 BATTERY PACK AND REPLACED WITH SERVICEABLE UNIT FROM STOCK IAW AMM TASK 33-51-00-820-801 OPS CHECK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,906 hrs · 21,345 cycles

FWD RH FUSELAGE EMERGENCY EGRESS LIGHT INOP. REMOVED FWD RH FUSELAGE EMERGENCY EGRESS LAMP REF Q400 AMM 33-51-11-000-801 INSTALLED SERVICEABLE LAMP REF AMM 33-51-11-400-801. OPS CHECK DID NOT PASS ON STEP 5C. REMOVED & REPLACE BOTH BATTERY PACKS REF Q400 AMM 33-51-00-820-801 COMPLETED AMM TASK 33-51-11-400-801 STEP(S) 5C AND F OPS CHECK OK.

Part: FILTER — MALFUNCTIONED (ZONE 700) · airframe 19,864 hrs · 21,296 cycles

NOSE GEAR TOOK ABOUT 15 SECONDS LONGER TO SAFELY EXTEND THAN THE MAIN GEAR. THREE GREEN INDICATED EVENTUALLY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED BOTH FILTERS ON THE NLG DOORS SOLENOID VALVE. NLG EXTENSION/RETRACTION ON THE GROUND IS GOOD- ACCOMPLISHED WITHIN 5 SECONDS. CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 19,857 hrs · 21,285 cycles

NOSE GEAR UNSAFE AND NOSE DOOR ILLUMINATED. AFTER GEAR EXTENSION ON FINAL. AFTER MISSED APPROACH GEAR CAME DOWN WITH 3 GREEN. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED PSEU. NO FAULTS FOUND. PERFORMED FIM TASK 32-00-00-810-814. PERFORMED AMM 32-31-00-867-802. PERFORMED AMM 32-31-00-867-802 STEP 5F AND H. NO DEFECTS NOTED. OPERATIONAL CHECK FLIGHT RELEASED. CHECKS SATISFACTORY. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 19,782 hrs · 21,202 cycles

FORWARD FLIGHT ATTENDENT EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATED IN THE NORMAL POSITION. REMOVED FROM SERVICE. RELAMPED FWD F/A EMERGENCY LIGHT SWITCH NORMAL POSITION OPS CK. GOOD REF AMM TASK 33-51-710-802 NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,769 hrs · 21,183 cycles

FUSELAGE DOORS WARNING AFTER TAKEOFF. TYPE II / III EMERGENCY EXIT INDICATED OPEN. REMAINED ON FOR 5 MINUTES AND THEN WAS INTERMITTENT AFTER THAT. NO ISSUE WITH CABIN PRESSURE". RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. RIGGED THE EMERGENCY DOOR PROX SENSOR (EDRCCLK). CHECKS GOOD, DOOR WARNING LIGHT DID NOT RETURN. RETURNED TO SERVICE.

Part: SENSOR — OUT OF RIG (MLG) · airframe 19,605 hrs · 20,090 cycles

ON LANDING ROLL AT 60 KIAS, THERE WAS NO TILLER AUTHORITY OR STEERING. RUDDER PEDALS AND HAD NO STEERING VIA RUDDER PEDALS. WE STARTED TO EXIT THE CENTERLINE OF THE RUNWAY AS I WAS GETTING ON THE BRAKES. WT ON WHEELS CAUTION ILLUMINATED AND STAYED ON FOR ABOUT 5 SECONDS. CAUTION WENT OUT AND STEERING VIA TILLER AND RUDDER PEDALS RETURNED. REMOVED FROM SERVICE. FOUND MLG WOW SENSORS OUT OF RIG, RIGGED WITHIN LIMITS. OPS TEST OF NOSE WHEEL STEERING GOOD. NO FURTHER DEFECTS NOTED.RETURNED TO SERVICE.

Part: BEARING — FAILED (MLG) · airframe 19,365 hrs · 20,698 cycles

L MAIN OUTBOARD WHEEL SMOKING AFTER PARKING. METAL SHAVINGS OBSERVED IN AND AROUND WHEEL. CRACK IN OUTBOARD HUBCAP. REMOVED FROM SERVICE. REMOVED LT 1 MLG TIRE ASSEMBLY REF MTC 6324201, PERFORMED ITEMS 1-3 STEP 12. ACCOMPLISHED FORM M-745. REMOVED LT #2 MLG TIRE AND BRAKE REF MTC 6324201, STEPS 1-7. REMOVED #1 MLG AXLE REF TASK 32-11-04-000-801. REMOVED LT #1 BRAKE MTC 6324201 STEPS 3-7. PERFORMED INSPECTION AFTER WHEEL BEARING FAILURE REF TASK 05-50-17-210-801. FOUND AXLE, #1 WHEEL ASSY, #1 BRAKE ASSY, AND #1 WHEEL SPEED TRANSDUCER DAMAGED. NO OTHER DAMAGE NOTED. REPLACED #1 MLG AXLE REF TASK 32-11-04-000-801 AND 32-11-04-400-801. INSTALLED NEW #1 AND #2 MAIN WHEEL / TIRE ASSYS REF MTC'S 6324101. INSTALLED NEW #1 BRAKE ASSY REF MTC 6324201. RE-INSTALLED #2 BRAKE ASSY REF MTC 6324201. REPLACED #1 WHEEL SPEED TRANSDUCER REF TASK 32-46-11-000-801 AND 32-46-11-400-801. RETURNED TO SERVICE.

Part: SCREW — MISSING (ZONE 800) · airframe 14,290 hrs · 20,614 cycles

HARDWARE NOT INSTALLED IN MAIN CABIN DOOR DITCHING DAM TRACK (1EA), UPPER RIGHT SIDE NEAR CABIN DOOR EXIT HANDLE. REMOVED FROM SERVICE. INSTALLED NEW HARDWARE @ MAIN CABIN DOOR DITCHING DAM TRACK, QTY 1, UPPER FWD SIDE NEAR MAIN CABIN DOOR EXIT HANDLE. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LINE — CHAFED (BRAKE) · airframe 19,029 hrs · 20,302 cycles

HYDRAULIC LEAK FROM #2 BRAKE LINE. LINE BLEW AT GATE UPON PARKING BRAKE APPLICATION. AFTER PARKING IN PDX, RAMP REPORTED SMOKE FROM #2 SIDE BRAKE. FIRE DEPARTMENT WAS CALLED TO AIRCRAFT. INITIAL EVALUATION INDICATES A LEAKING HYDRAULIC LINE. REMOVED FROM SERVICE. INSPECTED # 3 BRAKE, FOUND #3 BRAKE LINE CHAFFED THROUGH. REMOVED AND REPLACED #3 BRAKE LINE REF AMM TASK 32-42-26-000-801, 32-42-26-400-801. BLED BRAKE AND LEAK CHECK GOOD. NOTE: #2 HYD SYSTEM WAS AT 3.5 QUARTS. CHAPTER 5 INSPECTION NOT REQUIRED. REF AMM TASK 12-10-29-611-801 FOR SERVICING #2 HYD SYSTEM. AIRCRAFT RETURNED TO SERVICE.

Part: PROBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 18,986 hrs · 20,252 cycles

ON CLIMBOUT PITOT HEAT 2 CAUTION ILLUMINATED. SWITCH WAS ALREADY IN THE ON POSITION. RAN CHECKLIST WITH NO ABNORMALITIES NOTED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED #2 PITOT-STATIC PROBE REF. AMM TASK 34-11-06-000-801 AND REPLACED WITH NEW PROBE REF. AMM TASK 34-11-06-400-801. OPS TEST GOOD. LEAK CHECK PERFORMED REF. TASK CARD 6341102. LEAK CHECK GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (RUDDER SYS) · airframe 18,880 hrs · 20,120 cycles

ON TAKE OFF AND LANDING ROLL FO'S RIGHT RUDDER INPUT SLOW TO RESPOND. TO KEEP AIRCRAFT ON CENTER LINE. CAPTAIN HAD TO TAKE THE AIRPLANE ON LANDING ROLL OUT AT 70KTS TO MAINTAIN CENTER LINE WITH THE TILLER. REMOVED FROM SERVICE. PERFORMED MTX TAXI, ALL RUDDER INPUT NORMAL TO RESPOND. NO EXCESSIVE FORCE REQUIRED TO TO KEEP A/C ON CENTER LINE, ON BOTH THE CAPTAINS AND FO'S RUDDER PEDALS ALL CONTROLS FEEL AND OPERATE NORMALLY. OPENED PANEL 121DZ INSPECTED RUDDER QUADRANT, LINKAGES, AND CABLES, NO DEFECTS NOTED. REINSTALLED PANEL 121 DZ REF AMM 53-23-01-400-801. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PANEL — NOT SEATED (SIGNS) · airframe 17,885 hrs · 18,973 cycles

BACKLIGHTING FOR THE FASTEN BELTS SIGN, NO SMOKING SIGN, AND THE EMERGENCY LIGHTS SWITCH ARE VERY DIM. REMOVED FROM SERVICE. RESEATED PANEL FACE. OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

LIGHT CORROSION FOUND ON INTERNAL DOUBLER FOR DRAIN MAST FWD OF FRAME X32. REPLACED EXTERNAL DOUBLER, INTERNAL DOUBLER AND PLATE ASSY'S PN 853228855-101 85328856-101 AND 85328857-001 WITH NEW PARTS IAW SRM 51-40-07-02-01, 51-23-00-00-01 AND 51-42-05-02-01 APPLIED ALLUMIZED PAINT TO INTERNAL SURFACE IAW SRM 51-25-25-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

SEAT RAIL NR 7 FROM FS X228.50-X570.00 IS CORRODED IN SEVERAL PLACES. SEAT RAIL NR 7 BLENDED BEYOND LIMITS IAW SRM 53-20-40-02-07. SEAT RAIL NR 7 REPLACED IAW SRM 51-40-15-02-01, 51-41-05-00-01 AND 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

SEAT RAIL NR 15 FROM FS X612.00-X670.00 IS CORRODED IN SEVERAL PLACES. SEAT RAIL NR 15 BEYOND LIMITS IAW SRM 53-20-19-02. SEAT RAIL NR 15 REPLACED IAW SRM 51-40-15-02-01, 51-41-05-00-01 AND 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

SEAT RAIL NR 13 FROM FS X228.50-X570.00 IS CORRODED IN SEVERAL PLACES. SEAT RAIL NR 13 BLENDED BEYOND LIMITS IAW SRM 53-20-49-02-07. SEAT RAIL NR 13 REPLACED IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

SEAT RAIL NR 8 FROM FS X570.00-X668.00 IS CORRODED IN SEVERAL PLACES. SEAT RAIL NR 8 BLENDED BEYOND LIMITS IAW SRM 53-20-49-02. SEAT RAIL NR 8 REPLACED IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

EXTERNAL LAV DOUBLER CORRODED BEYOND LIMITS. EXTERNAL LAV DOUBLER REPLACED IAW SRM 51-42-05-02-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 17,710 hrs · 18,787 cycles

FWD PAX DOOR THRESHOLD CORRODED BEYOND LIMITS. THRESHOLD REPLACED IAW SRM 51-42-05 USING RIVETS.

Part: PROPELLER — CONTAMINATED (NR 1) · airframe 17,470 hrs · 18,512 cycles

NR 1 PROPELLER TIME TO UNFEATHER WAS 50 SECONDS. REMOVED FROM SERVICE. ON GREASE LEVEL CHECK, FOUND GREASE TO BE DARK BROWN IN COLOR AND VERY LOW VISCOSITY. POSSIBLE CONTAMINATED WITH ENGINE OIL. REPLACED THE P[ROPELLER GREASE AND ALSO THE OVERSPEED GOVERNOR. RETURNED TO SERVICE.

Part: BRAKE — SMOKE (MLG) · airframe 17,427 hrs · 18,459 cycles

AFTER PREVIOUS CREW LANDED, FOUND THE NR 3 AND 4 BRAKES TO BE SMOKING FOR SEVERAL MINUTES. REMOVED FROM SERVICE. COMPLIED WITH A GVI OF THE NR 3 AND 4 BRAKE ,AND TIRE ASSY, LINES AND LANDING GEAR, NO LEAKS NOTED. NO DEFECTS NOTED. BRAKES AND TIRES ARE SHOWING NORMAL WEAR. ACFT OKAY FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: ENGINE — ABNORMAL (NR 1) · airframe 16,627 hrs · 17,777 cycles

DURING DAILY SYSTEM CHECK OF THE AUTOFEATHER SYSTEM, THE NR 1 ENGINE CONSISTENTLY SHOWING 10% TORQUE LESS THAN IT SHOULD. FOUND NO FAULTS IN CDS. COMPLIED WITH PEC CALIBRATION IAW AMM 61-20-36-720-801. AUTOFEATHER TESTED GOOD IAW AMM 61-20-00-710-810. NO FURTHER DEFECTS NOTED. AFTER CALIBRATION TORQUE INDICATONS MATCH. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 16,692 hrs · 17,634 cycles

EMERGENCY LIGHT STRIP CAME LOOSE OF FLOOR. OUT OF SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT. RETURNED TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 16,399 hrs · 17,334 cycles

NR 1 HYD PUMP CAUTION WITH LOSS OF NR 1 HYD PRESSURE & ASSOCIATED CAUTION LIGHTS. RAN CHECKLIST AND PRESSURE WAS RESTORED BY THE STANDBY HYD PUMP. LANDED WITHOUT INCIDENT. REPLACED THE NR 1 HYD PUMP IAW AMM 29-11-01-000-801/400-801. OPS CHECKED GOOD. PERFORMED SIMPLIFIED FLUSH OF SYSTEM. RETURNED TO SERVICE.

Part: DOOR — STICKING (ALT MLG EXTEND) · airframe 15,393 hrs · 16,276 cycles

DURING PREFLIGHT INSPECTION, LANDING GEAR ALTERNATE LANDING GEAR EXTENSION DOOR ON FLOOR DOES NOT OPEN ALL THE WAY. REMOVED AIRCRAFT FROM SERVICE. CLEANED & LUBRICATED DOOR MACHANISM, OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,249 hrs · 16,118 cycles

EMERGENCY EXIT AND EMERGENCY EGRESS LIGHTS NOT WORKING FOR RT FWD TYPE II EMERGENCY EXIT. REMOVED & REPLACED BATTERY PACKS INSIDE EMERGENCY POWER SUPPLY 2, IAW AMM 33-51-01-000-801, 33-51-01-400-801 AND PERFORMED OPS TESTS IAW TASK 33-51-00-710-802. ALL TESTS ARE GOOD.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 15,120 hrs · 15,990 cycles

FORWARD FA EMERGENCY LIGHT SWITCH INOPERATIVE. REPLACED THE LAMPS. CHECKED GOOD.

Part: SEAL — MALFUNCTIONED (NR 1 PROP) · airframe 14,860 hrs · 15,705 cycles

NORMAL ENGINE START WHEN CONDITION LEVERS SET TO MAX 1020. NR 1 PROP TOOK 56 SECONDS TO COME OFF 220 RPM; 70 SECONDS TO UN FEATHER. FOR REFERENCE, NR 2 PROP CAME OFF 220 RPM IN 14 SECONDS AND UNFEATHERED AT 26 SECONDS. REMOVED AND REPLACED NR 1 PROPELLER PISTON SEAL IAW AMM 61-10-00-960-801 PARA 1 THROUGHT 5D. COMPLETED INSTALLATION OF PROPELLER PISTION SEAL IAW AMM 61-10-00-960-801, PARA 5E. RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (PROP DE ICE) · airframe 14,398 hrs · 15,214 cycles

PROP DE-ICE CAUTION IN FLIGHT RAN CHECKLIST RESET PROPELLER HEAT CAUTION LIGHT WENT OUT. PROPELLER ADVISORY LIGHTS DID NOT COME ON. NO DRAW NOTED ON ELECTRICAL PAGE. GROUND OPS TESTED SYSTEM NO FUNCTION. REMOVED AND REPLACED ICE PANEL IAW AMM TASKS 30-10-01-000-801, 30-10-01-400-801, COMPLIED WITH ALL ASSOCIATED OPS AND FUNCTIONAL TESTS. TESTED GOOD, NO CDS MESSAGES FOUND COMPLIED WITH FUNCTIONAL TEST AND CALIBRATION IAW AMM 30-61-00-720-800, CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 13,549 hrs · 14,286 cycles

DURING APPROACH WHEN SELECTING FLAPS 35, THE FLAPS STUCK AT 16 & THE FLAP POWER CAUTION ILLUMINATED. FLAP CONT CIRCUIT BREAKER HAD NOT TRIPPED, RESET ONCE IAW THE E & A CHECKLIST. FLAP POWER REMAINED ILLUMINATED. COMPLIED WITH E & A CHECKLIST LANDED WITH FLAPS 15 NORMALLY WITHOUT INCIDENT. FLAP HANDLE WAS OPERATED SLOWLY IAW FSM INSTRUCTIONS. NO PRESENT FAULTS NOTED IN CDS. PERFORMED FLAP NVM RESET. C/W FIM TASK 27-50-00-810-802 STEPS 1 THRU 3A(3). OPERATIONAL TEST OF WING FLAPS GOOD IAW AMM TASK 27-50-00-710-801. CYCLED WING FLAPS 3 TIMES. NO FAULTS NOTED, NO FURTHER CAUTION LIGHT NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 10,531 hrs · 11,351 cycles

DURING TAXI IN, THE FLAP POWER CAUTION ILLUMINATED. FLAP HANDLE WAS NOT IN DETECT AS ZERO SETTING. RESET CIRCUIT BREAKER L7 PER CHECKLIST. FLAP POWER AND FLAP DRIVE BOTH ILLUMINATED AFTER CIRCUIT BREAKER RESET. PERFORMED NVM RESET OF FLAPS AND OPERATIONAL TEST IAW AMM 27-50-00-710-801. NO DEFECTS NOTED, RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,236 hrs · 13,943 cycles

BURNED PLASTIC OR BURNED ELECTRICAL ODOR IN FRONT CABIN UPON ENTRY. COMPLIED WITH FIM 21-20-00 MCN 62172-01 FORM M-744 AND AMM TASK 21-00-00-160-801. NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ICE SHIELD — DENTED (BS 258) · airframe 12,457 hrs · 13,125 cycles

1 DENT UNDER ICE SHIELD RT SIDE LOCATED ON STR 12S, 7.82" AFT OF X258.50. DENT UNDER RT ICE SHIELD AT FS X266.5 BETWEEN STR 12S AND 13S MAPPED AND THD CONTACTED IAW SRM 51-15-05. DOUBLER FABRICATED IAW RD8/4-53-7507. NDT CARRIED OUT IAW RD8/4-53-7507. INSTALLED DOUBLER ON RT FS X266.50 UNDER ICE SHIELD IAW BBD RD8/4-53-7507.

Part: STRINGER — CORRODED (BS 604-624) · airframe 12,457 hrs · 13,125 cycles

CORROSION AROUND RIVET TAILS ON STRINGER 24L BETWEEN BS 604 AND 624. STRINGER REPLACED IAW SRM 51-42-05, 51-40-15 & DWG 85337033.

Part: STRINGER — CORRODED (BS 258-281) · airframe 12,457 hrs · 13,125 cycles

CORROSION AROUND RIVET TAILS ON STR 24 LT SIDE BETWEEN BS X258.00 AND 281.00. STRINGER 24LT, PN 85360221-255 CUT AT BS X267 APPROXIMATELY AND REMOVED IAW RD8/4-53-7509. NEW SECTION OF STR 24LT, 85360221-255, BS X258.5 TO X267 INSTALLED IAW RD 8/4-53-7509. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. APPLIED EPOXY PRIMER IAW SRM TASK 51-25-10-0201. APPLIED TOP COAT IAW SRM TASK 51-25-15-02-01.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 12,457 hrs · 13,125 cycles

FORWARD AIRSTAIR DOOR THRESHOLD MEMBER, FS X1 TO X 32.40 HAS SURFACE CORROSION. AIRSTAIR DOOR THRESHOLD MEMBER, BLENDED AND FOUND TO BE BEYOND SERVICEABLE LIMITS IAW SRM 53-20-23. AIRSTAIR DOOR THRESHOLD MEMBER. REPLACED IAW SRM 51-42-05-02-01, SRM 51-25-10-02-01, SRM 51-25-15-02-01 AND SRM 51-23-0-00-01.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 12,457 hrs · 13,125 cycles

CORROSION ON FWD BAGGAGE DOOR LWR SILL ON TOP PLATE AND EDGE CHANNEL. FS X4.10 - FS X32.40. 1. REMOVED CORRODED FORWARD BAGGAGE DOOR LOWER SIL TOP PLATE AND EDGE CHANNEL AT FS 4.10 X34.20 IAW SRM 51-42-05 & 51-42-15. FIT DRILLED AND INSTALLED NEW FWD BAGGAGE DOOR LOWER SIL EDGE CHANNEL AT FS X4.10-X34.20 IAW SRM 51-42-05. FIT DRILLED AND INSTALLED NEW FORWARD BAGGAGE DOOR LOWER SILL EDGE PANEL, PN 85329603-103S AT FSX4.1-X34.20 IAW SRM 51-42-05,51-40, 15, 51-42-45 AND 51-42-15.

Part: STRINGER — CORRODED (BS 373-388) · airframe 12,457 hrs · 13,125 cycles

CORROSION AROUND RIVET TAILS ON STR 24 LT SIDE BETWEEN BS 373 AND 388. REMOVED RIVETS AND LOOSENED FRAME FS X388, PN 85361318, LT STR 20P-28P, FLOORBEAM FS X388 LBL10-LBL40, PN 85361343 AND FLOOR SUPPORT ANGLE LBL 40 FS X370 -X460, PN 85361611 TO PROVIDE ACCESS FOR STRINGER REMOVAL IAW SRM 51-42-05. LT STR 24P FROM FS X373-FSX428, PN 85360221-311, REPLACED IAW SRM 51-42-05 AND 51-40-15. RIVETS INSTALLED IN FRAME, PN 85361318, FLOORBEAM, PN 85361343 AND FLOOR SUPPORT ANGLE, PN 85361611 IAW SRM 51-42-05.

Part: SHEAR WEB — CORRODED (CARGO BAY) · airframe 12,547 hrs · 13,125 cycles

AFT BAGGAGE BAY AFT SHEAR WEB CORRODED IN MULTIPLE LOCATIONS. AFT SHEAR WEB REMOVED AND REPLACED IAW SRM 51-42-15 AND SRM 51-42-05 & DWG 85339627.

Part: RAIL — CORRODED (E/E BAY) · airframe 12,547 hrs · 13,125 cycles

CENTER AFT EQUIPMENT RAIL NR 23, BS 697.6 TO 782.102, CORRODED BEYOND LIMITS. CENTER AFT EQUIPMENT RAIL NR 23, BS 697.600 TO 782.102. REPLACED IAW SRM 51-42-05 & DWG 85337843.

Part: SHEAR WEB — CORRODED (BS 697) · airframe 12,547 hrs · 13,125 cycles

CORROSION ON AFT SHEAR WEB, BS 697.6, LBL Y10 AND LBL Y30. REMOVED IAW SRM 51-42-05 AND 51-40-15. REPLACED IAW Q400 51-42-05, 51-40-15 & DWG 85339527.

Part: SEAT TRACK — CORRODED (BS 670-782) · airframe 12,547 hrs · 13,125 cycles

SEAT TRACK NR 9, BS 670 TO 782 LT SIDE INBD CORRODED BEYOND LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05 AND 51-40-15 & DWG 85338210.

Part: SEAT TRACK — CORRODED (BS 570-670) · airframe 12,547 hrs · 13,125 cycles

SEAT TRACK NR 8, BS 570 TO 670, LT SIDE INBD CORRODED BEYOND LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05 AND 51-40-15 & DWG 85338210.

Part: SEAT TRACK — CORRODED · airframe 12,547 hrs · 13,125 cycles

CORROSION ON SEAT TRACK NR 10 RT SIDE INBD UNDER LAV AT 2 LOCATIONS. CORROSION REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 53-20-49-02-03. SEAT TRACKREPLACED IAW SRM 51-42-05, 51-40-15 & ORCU NR 85328210 AND 85328201.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 12,547 hrs · 13,125 cycles

SEAT TRACK NR 11, BS 10.50 TO 102.50. RT SIDE INBD CORRODED BEYOND LIMITS. SEAT TRACK REPLACED IAW SRM 51-42-05, 51-40-15 & ORCU 85328210 AND 85328201.

Part: WIRE HARNESS — FAILED (PROP DEICE) · airframe 12,448 hrs · 13,118 cycles

PROP DEICE CAUTION LIGHT. SEEMED RELATED TO NR 1 ENGINE ASSOCIATED NR 1 AC GEN CAUTION LIGHT FLICKERING WHILE PROP CAUTION LIGHT ILLUMINATED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INTEROGATED CDS, FOUND NR 1 PROP PHASE A OPEN. FOUND NR 4 BLADE DEICER WIRE HARNESS SHORTED. R & R NR 4 BLADE HARNESS IAW AMM TASK 61-10-06-000/400-805, NO OTHER DEFECTS NOTED. FUNCTIONAL TEST AND CALIBRATION IAW AMM TASK 30-61-00-720-802. TEST GOOD. PERFORMED OPS TEST OF AC GENERATOR IAW AMM TASK 24-21-00-710-801, TEST GOOD. COMPLIED WITH FIM TASK 24-20-00-810-801 STEP 4,A,1. FOR AC GENERATOR CHIP INSPECTION. NO FAULTS FOUND. ACFT OK FOR CONTINUED SERVICE.

Part: TRIM SWITCH — MALFUNCTIONED (RUDDER) · airframe 12,051 hrs · 12,676 cycles

RUDDER TRIM RUNAWAY DURING CRUISE FLIGHT. RUDDER TRIM ACT CIRCUIT BREAKER F7 PULLED AS DIRECTED BY CHECKLIST. INTERROGATED THE CDS: NO FAULTS NOTED, NO HISTORY FOUND. REPLACED THE RUDDER TRIM SWITCH IAW AMM 27-22-11-000-801, 2722-11-400-801. C/W AN OPS CK OF THE AILERON TRIM SYS IAW AMM 27-13-00-710-802. OPS CK'S NORMAL. ACFT OK FOR CONTINUED SERVICE, COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT. NO DEFECTS NOTED IAW GPM 9.2.

Part: WIRE HARNESS — MALFUNCTIONED (NR 2 PROPELLER) · airframe 11,952 hrs · 12,564 cycles

PROP DEICING CAUTION CYCLES ON WITH PROP NR 1 INDICATOR LIGHT. SWITHED CYCLED IAW EMERGENCY CHECKLIST. NO CHANGE AC GEN NR 1 & NR 2 VOLTAGE LOADS NORMAL. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. ERFORMED RESISTANCE CHECK OF NR 1 PROP HEATER LEADS. FOUND HIGH RESISTANCE ON NR 2 LEADS. PERFORMED GVI OF NR 1 PROP BLADE HEATERS, NO DEFECTS NOTED. R & R NR 2 BLADE HEATER LEADS IAW AMM 61-10-06-000-805 AND 61-10-06-400-805, OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,787 hrs · 12,389 cycles

INBOUND AT 16000 FT FA REPORTED A VERY LOCALIZED ELECTICAL ODOR IN VICINITY ROW 16DE. NO VISIBLE SMOKE, NO ABNORMAL INDICATIONS ANYWHERE ELSE IN ACFT. ODOR LASTED APPROXIMATELY 2 MIN AND DID NOT REPEAT. OPENED ROW 14 AND 15DE PSU PANEL DISCONNECTED READING LIGHT AT ROWS 14+15D INSTALLED NEW READING LIGHT 14D AND 15D. REINSTALLED ROW 14 AND 15 D/E PSU PANELS OPS TEST GOOD OF READING LIGHTS ROW 14+15 D/E 25-28-00-010-801 AND 25-28-00-410-801. PERFORMED GVI OF AREA WHILE PSU PANELS WERE DOWN NO DEFECTS FOUND. C/W AIR CONTAMINATION CHECK LIST FORM M-744ALSO OPENED ROW 16D/E PSU PANEL FOUND NO DEFECTS CLSOE DPUSH PANEL 16 D/E.

Part: PANEL — MALFUNCTIONED (ZONE 400) · airframe 11,413 hrs · 11,959 cycles

FUELER REPORTS SMOKE AND AN ELECTRICAL BURNING ODOR COMING FROM THE TANK 1 REFUEL SHUTOFF LAMP ON THE FUELING PANEL. SMOKE STOPPED AFTER POWER WAS REMOVED FROM THE PANEL, 1 MINUTE LATER. R & R REFUEL DEFUEL CONTROL PANEL IAW 28-24-01. PERFORMED OPS CHECK OF REFUEL DEFUEL PANEL CONTROL IAW MM 28-24-01. NO FAULTS NOTED. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,403 hrs · 11,947 cycles

F/A REPORTS THAT THE EMERGENCY LIGHT SWITCH NOT ILLUMINATING. RELAMPED AS REQUIRED. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 11,398 hrs · 11,943 cycles

BAGGAGE DOOR WARNING WHILE CLIMBING THROUGH 11,000 FT. RETURNED TO DEPARTURE. DESCENDING THROUGH 5000 FT, PRESSURIZATION DROPPED. ON ARRIVAL, AFT BAGGAGE DOOR HANDLE WAS EXTENDED. INSPECTED DOOR HANDLE LOCK, MACHANISM, NO DEFECTS NOTED. ACCOMPLISHED AFT BAGGAGE DOOR, OPS TEST IAW AMM 52-31-00-710-801, DOOR OPS NORMAL, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (NR 2 PROPELLER) · airframe 10,855 hrs · 11,344 cycles

DURING CLIMBOUT, POWERPLANT MESSAGE DISPLAYED. RETURNED TO FIELD, LANDING UNEVENTFUL. INTERAGATED CDS FOUND NR 2 PROPELLER FAULTS 130A, & 134A. CLEARED PEC FAULTS. INSPECTED SECURITY OF CONNECTORS ON NR 2 PEC AND NR 2 BETA FEED BACK TRANSDUCER. ELECTRICAL CONNECTOR SECURITY CHECKED GOOD. REPLACED NR 2 ENGINE PEC IAW AMM 61-20-36-000-801 AND 61-20-36-0400-801, OPS CHECK GOOD. RETURNED TO SERVICE.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 10,372 hrs · 10,816 cycles

ON SHORT FINAL ABOUT 1000 FT, ACFT CABIN FILLED WITH MODERATE AMOUNT OF VAPOR OF UNKNOWN SOURCE, OBSTRUCTING F/A VISION. ALSO ODOR OF HOT WET BLEED AIR. LANDING UNEVENTFUL. AFTER WALKAROUND COMPLETED, FOUND OIL LEAKING OUT OF NR 1 ENGINE DRAIN. ALSO ON MAINTENANCE START UP OF NR 1 ENGINE, GROUND CREW REPORTED SMOKE AND OIL OUT OF THE P2.2 EXHAUST VENT. NR 1 ENGINE REPLACED. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 10,238 hrs · 10,669 cycles

AT AROUND 800FT AFT BAGGAGE DOOR OPENED IN FLIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. VERIFIED THE AFT CARGO DOOR HANDLE WAS EXTENDED IN THE UNLOCKED POSITION. PERFORMED GVI ON HANDLE LATCH MECHANISM AND ASSOCIATED HARDWARE WITH NO DEFECTS NOTED. FOUND THE AFT BLOW OUT PANEL IN THE AFT CARGO COMPARTMENT OUT. RESET THE BLOW OUT PANEL. PERFORMED OPS TEST OF THE AFT CARGO DOOR IAW AMM TASK 52-31-00-710-801 AND HS 52-0028. OPS TEST GOOD. PRESSURIZED A/C IAW AMM TASKS 21-00-00-863-801 & 802. PRESSURIZATION NORMAL, AFT CARGO DOOR REMAINED LOCKED CLOSED AND INDICATED CLOSED. NO FURTHER DEFECTS NOTED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 9,650 hrs · 9,994 cycles

RIGHT MAIN GEAR DOOR CONTINUED TO CYCLE AFTER GEAR RETRACTION. ALT GEAR EXTENSION ACCOMPLISHED. RETURNED TO FIELD. LANDING UNEVENTFUL. ADJUSTED PROXIMITY SENSOR, PERFORMED EXTENSION/ RETRACTION OF MLG. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 9,383 hrs · 9,700 cycles

EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN THE SWITCH IS SELECTED TO ARM POSITION. FOUND CONNECTOR BLOCK LOOSE FROM THE MOUNTING SLEEVE AT THE LIGHT SWITCH. CONNECTED IAW AMM 33-51-05-400-801. PERFORMED OPS TEST IAW AMM 33-51-00-710-802. CHECKS GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 9,280 hrs · 9,589 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH "NORMAL" LEGEND NOT ILLUMINATED. REPLACED THE LAMP. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 9,167 hrs · 9,464 cycles

FOUND THE EMERGENCY EXIT DOOR LIGHT COVER ON THE FLOOR. REINSTALLED COVER. RETURNED TO SERVICE.

Part: PLACARD — DISLODGED (CABIN) · airframe 8,557 hrs · 8,799 cycles

EXIT PLACARD IN 2E FELL OFF. INSTALLED EXIT PLACARD. RETURNED TO SERVICE.

Part: RIB — CORRODED (EMERGENCY DOOR) · airframe 8,409 hrs · 8,655 cycles

CORRODED RIB EDGE AFT AT EMERGENCY DOOR. REMOVED AND REPLACED RIB IAWSRM 51-42-05, STEP 4.D, 3 THRU 6, 51-40-15, SRM 51-21-00 AND SRM 51-25-10.

Part: GUSSET — CORRODED (EMERGENCY EXIT) · airframe 8,409 hrs · 8,655 cycles

EMERGENCY EXIT DOOR FWD GUSSETS SHOW SIGNS OF CORROSION. REMOVED AND REPLACE IAW SRM 51-40-07 AND SRM 51-42-05.

Part: RIB — CORRODED (EMERGENCY EXIT) · airframe 8,409 hrs · 8,655 cycles

CORRODED RIB EDGE AT EMERGENCY EXIT DOOR. REMOVED AND REPLACED THE RIB IAW DWG 85329513, AMS 2770, REV L, AMS 2658, REV C, SRM 51-40-07, AND SRM 51-42-05-02-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 8,409 hrs · 8,655 cycles

ANGLE AT CENTER FUSELAGE, STA X6.7 HAS EVIDENCE OF CORROSION. REMOVED CORRODED ANGLE IAW SRM 51-42-05 4, E. INSTALLED NEW ANGLE IAW SRM 51-42-05 4, D, 3.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 8,409 hrs · 8,655 cycles

AIRSTAIR DOOR ANGLE AT STA X26.7 HAS EVIDENCE OF CORROSION. FOUND OUT OF LIMITS IAW SRM 51-21-00, 4(A)5 PAGE 3 AND DWG 85329576, DETAIL -104, REV -A REPLACED THE ANGLE IAW SRM 51-40-07, PAGES 201 TO 204.

Part: ANGLE — CORRODED (CENTER FUSELAGE) · airframe 8,409 hrs · 8,655 cycles

ANGLE CENTER FUSELAGE AT STA X26.7 HAS EVIDENCE OF CORROSION. REMOVED CORRODED ANGLE IAW SRM 51-42-05 4 (E). INSTALLED NEW ANGLE IAW SRM 51-42-05 4(D).

Part: ANGLE — CORRODED (PAX DOOR) · airframe 8,409 hrs · 8,655 cycles

AIRSTAIR DOOR ANGLE STA X6.700 HAS EVIDENCE OF CORROSION. FOUND OUT OF LIMITS IAW SRM 51-21-00 4, A 5, PAGE 3 AND DWG 85329576 DETAIL -103, REV -A. INSTALLED NEW ANGLE IAW SRM 51-40-07, PAGES 201 TO 204.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 7,499 hrs · 7,691 cycles

NR 2 ENGINE SLOW TO COME OUT OF FEATHER. REPLACED NR 2 ENGINE OVER SPEED GOVERNOR IAW AMM TASKS 61-20-26-000-801 & 61-20-26-400-801. LEAK, OPS TEST & BONDING CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF THE PROPELLER TIME TO UNFEATHER IAW AMM TASK 61-20-00-720-801. FEATHERS WITHIN 20 SECONDS NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: SIGN — LOOSE (AFT CABIN) · airframe 6,993 hrs · 7,153 cycles

AFT PASSENGER DOOR EXIT SIGN IS LOOSE. SECURED SIGN WITH ORIGINAL HARDWARE. CHECKED GOOD, RETURNED TO SERVICE.

Part: LINKAGE — BENT (NLG DOOR) · airframe 6,605 hrs · 6,760 cycles

DURING WALK AROUND, FOUND NOSE GEAR RT AFT DOOR LINKAGE ROD BENT AT INBD KNUCKLE. INSTALLED NEW LINKAGE IAW MM TASK 32-22-01-400-801, PAR 1-4. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FWD) · airframe 6,495 hrs · 6,634 cycles

FWD INBD SEAT TRACK CORRODED. OUT OF LIMITS IAW SRM 53-20-49-02-02. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,382 hrs · 6,524 cycles

FORWARD F/A EMERGENCY LIGHT BUTTON DOES NOT ILLUMINATE. REPLACED LAMP. CHECKED GOOD. RETURNED TO SERVICE.

Part: FEEL UNIT — MALFUNCTIONED (RUDDER) · airframe 5,654 hrs · 5,750 cycles

RUDDER STICKS AND SUDDENLY RELEASES WHEN PRESSURE APPLIED PARTICULAR LT RUDDER. REF TC6-27-232 FOR RUDDER FEEL TRIM UNIT AND RII REPLACEMENT, EA 6-27-250 FOR INSPECTION OF RUDDER SYS. C/W FREEDOM OF MOVEMENT CHECK (RUDDER) ENSURED FULL TRAVEL AND VERIFED PROPER DIRECTION OF MOVEMENT REF GPM 9.2.5, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (INTAKE DOOR) · airframe 5,432 hrs · 5,519 cycles

NR 2 ENGINE INTAKE BYPASS DOOR CLOSED (GREEN) LIGHT IMMEDIATELY ILLUMINATED WHEN PUSH BUTTON SWITCH PUSHED OUT. RETURNED TO FIELD, LANDING UNEVENTFUL. REPLACED NR 2 ENGINE INTAKE BYPASS DOOR ACTUATOR ASSY IAW AMM 71-61-06-000-801/400-801. OPS CHECK GOOD. SWITCH LIGHT OPERATES PROPERLY. RETURNED TO SERVICE.

Part: WIRE — BROKEN (LOCK SENSOR) · airframe 4,844 hrs · 4,905 cycles

AT CABIN PSID ABOVE 1PSI AFT CARGO INDICATES OPEN. RETURNED TO FIELD. LANDING UNEVENTFUL. REPAIRED BROKEN WIRE FOR AFT BAGGAGE DOOR LOCK SENSOR AT AREA ABOVE BAG DOOR. REPAIR DONE IAW QM 20-16-20 AND 52-30-00 CONFIG 2. DOOR LOCK SENSOR OPS CHECKED GOOD IAW AMM 31-62-00-710-801. PRIOR TO REPAIR PROBLEM DUPLICATED, DASHES SHOWN IN PSEU LOCK SENSOR VALUE. RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 4,795 hrs · 4,860 cycles

WITH BLEED FLOW AT MIN AND BOTH BLEED SWITCHES ON, NR 1 & NR 2 BLEED HOT CAUTION LIGHTS ILLUMINATED WHEN THROTTLES WERE ADVANCED FOR TAKEOFF. LOW SPEED T/O ABORT (30 KNOTS). DUCT TEMP NORMAL. CDS FAULT CODES 7004L & R - BLEED OVER PRESSURE, 3102 - PACK LT PRESSURE BOTH CHANNELS. PERFORMED NVM RESET IAW FIM TASK 36-20-00-810-805. ALL FAULTS CLEARED. PERFORMED OPS TEST OF BLEED AIR SYSTEM IAW AMM TASK 36-11-00-710-802 & RAN A/C AT PWR. NO FAULTS OF DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 4,230 hrs · 4,299 cycles

CABIN EMERGENCY LIGHT SYS FLICKERING ON AND OFF. PERFORMED GVI OF CABIN EMERGENCY LIGHT SWITCH, FOUND CONNECTOR BLOCK WAS LOOSE ON TO THE MOUNTING SLEEVE OF THE EMERGENCY LIGHT SWITCH, ON THE WING BULKHEAD ASSY. PERFORMED OP'S CHECK, IAW AMM TASK 33-51-00-710-802. OP'S CHECKS GOOD AFTER SECURING CONNECTOR BLOCK TO MOUNTING SLEEVE, CABIN EMERGENCY LIGHTS NO LONGER FLICKER, NO FUTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 4,229 hrs · 4,298 cycles

CABIN EMERGENCY LIGHT SYS ILLUMINATED WITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE "ARM" POSITION. INSPECTED AND FOUND THE SWITCH LIGHT SCREW LOCK LOOSE AT THE FWD F/A POSITION. TIGHTENED THE SCREW AND PERFORMED A OPS CHECK IAW AMM 33-51-00-710-802. CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GUARD — BROKEN (EMERGENCY LIGHTS) · airframe 4,229 hrs · 4,297 cycles

F/A EMERGENCY LIGHT SWITCH COVER BROKEN. REPLACED SWITCH GUARD. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 3,996 hrs · 4,055 cycles

FLOORING LIFTING AT TOP OF FORWARD STAIRS. REPLACED LOOSE STRIP OF WET FLOORING AT TOP OF MCD STAIRS. RETURNED TO SERVICE.

Part: ANTENNA — MALFUNCTIONED (VHF SYSTEM) · airframe 3,730 hrs · 3,777 cycles

NR 2 COMMS INTERMITTENTLY WILL NOT RECEIVE CLEAR COMMUNICATION, ONLY GARBLED. COMPANY FREQ COULD HEAR US FINE BUT ONLY GARBLED WHEN RECEIVING. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 2 VHF ANTENNA IAW AMM TASKS 23-11-26-000-801, 23-11-26-400-801. PERFORMED OPS TEST OF NR 2 VHF IAW AMM TASK 23-11-06-710-801. ALL CHECKED GOOD AND CLEAR. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,450 hrs · 3,482 cycles

FLAP POWER CAUTION WHEN SELECTING FLAPS TO 35 DEGREES. FLAPS STAYED AT 15 DEGREES. FOLLOWED EAC CHECKLIST, FLAP POWER CAUTION RETURNED. LANDING UNEVENTFUL. PERFORMED FIM TASK 27-50-00-810-802. FAULT NOTED AS CURRENT - ECU CONTINUOUS BIT. PERFORMED FIM TASK 27-50-00-810-807. FAULT CLEARED. FLAPS CHECKED GOOD. RAN FLAPS 10 DEGREES-15 DEGEES-35 DEGREES SEVERAL TIMES FOR GOOD MEASURE. OK FOR SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 3,380 hrs · 3,397 cycles

F/A (B) REPORTS AN ELECTRICAL ODOR IN THE AFT GALLEY AFTER BOARDING PASSANGERS COMPLETE. AFT PAX DOOR CLOSED AND LOCKED. FOUND SOURCE TO BE THE AFT CARGO COMPARTMENT LIGHTS.

Part: FLEX DUCT — DAMAGED (ZONE 200) · airframe 1,426 hrs · 1,453 cycles

CABIN PRESSURE WARNING LIGHT CAME ON AT FL230 FOLLOWED CHECKLIST, CANNOT CONTROL THE CABIN IN MANUAL MODE. FOUND HOT RE-HEATER INLET DUCT DAMAGED. REPLACED HOT RE-HEATER DUCT REF AMM TASKS 21-51-66-000-809, 21-51-66-400-809. PERFORMED FUNCTIONAL TEST OF PRESSURIZATION CONTROL IAW AMM TASK AMM TASK 21-31-720-801. CHECKS GOOD. CLEARS DMI 543592. RETURNED TO SERVICE.