N444QX

Part: WARNING LIGHT — FALSE ACTIVATION (MASTER CAUTION) · airframe 21,944 hrs · 23,667 cycles

WHILE PERFORMING ACCELERATION HEIGHT FLOW AND TURNING OFF AUTOFEATHER, NOTICED BRIEF ILLUMINATION OF MASTER CAUTION PRESS TO RESET SWITCH. NO CHIME, DID NOT NOTICE ANY MASTER CAUTION LIGHTS. NO OTHER ISSUES AND FLIGHT CONTINUED NORMALLY. REMOVED FROM SERVICE. C/W OPERATIONAL TEST OF PROP AUTOFEATHER UPTRIM SYSTEM REF Q400 AMM 61-20-00-710-810 OPS TEST PASS. C/W OPERATIONAL TEST OF AUX PUMP REF Q400 AMM 28-21-31-710-801. OPS TEST PASS. NO ABNORMAL CONDITIONS OR CAUTION LIGHTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (DEICE SYSTEM) · airframe 21,798 hrs · 23,524 cycles

DURING CLIMB, DEICE PRESS CAUTION ILLUMINATED. COMPLETED E&A CHECKLIST AND LIGHT EXTINGUISHED. 2-3 MIN LATER DEICE PRESS ILLUMINATED AGAIN. E&A CHECKLIST COMPLETED, LIGHT EXTINGUISHED, 2-3 MIN LATER DEICE PRESS ILLUMINATED FOR THE THIRD TIME. RAN E&A CHECKLIST THE OTHER WAY, LEFT MODE SELECT IN SLOW, BOOT AIR SWITCH IN ISO. THE WHOLE TIME BOOT PSI WAS >17 PSI LEFT AND RIGHT. ALL LIGHTS AND DEICE BOOT STATIONS ILLUMINATED CORRECTLY ON ALL 6 STATIONS, ALL ICE WAS BEING SHED FROM AIRPLANE NORMALLY. REMOVED FROM SERVICE. C/W Q400 FIM 30-10-00-810-801. "DEICE PRESS" CAUTION RETURNED DURING FUNCTIONAL. FOUND FAULT "LOW PRESSURE 5B FAIL" IN CDS. R&R #5 DDV IAW Q400 AMM 30-11-16-000-801/400-801 & WM 20-12-10 STEP 3C. OPS & FUNCTIONAL TESTS GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BUMPER — WORN (PAX DOOR) · airframe 21,597 hrs · 23,332 cycles

MAIN CABIN DOOR STOP BUMPER DISINTEGRATED. REMOVED FROM SERVICE. REMOVED AND REPLACED MCD HANDLE BUMPER STOP REF. Q400 AMM 52-11-11-000/400-801. NO ADJUSTMENTS REQUIRED. RETURNED TO SERVICE.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 21,493 hrs · 23,229 cycles

DURING TAKEOFF, WE NOTICED #1 ENGINE OIL PRESSURE WAS FLUCTUATING FROM 71-73 PSI. THESE FLUCTUATIONS WERE MOMENTARY. THIS CONTINUED OCCASIONALLY UNTIL CRUISE. PSI WOULD OCCASIONALLY HIT 73 DURING CRUISE. THIS WOULD BE MOMENTARY. PSI WAS NORMAL DURING DESCENT. ALL OTHER ENGINE INDICATIONS ON #1 SIDE WERE NORMAL AT ALL TIMES. REMOVED FROM SERVICE. PERFORMED GVI OF #1 ENGINE FOR OIL LEAKS, FOUND NO LEAKS, SERVICED #1 ENGINE OIL IAW Q400 AMM 12-10-71-612-802 & HS#12-0006. PERFORMED Q400 FIM TASK 79-00-00-810-803 AND Q400 AMM 71-00-00-780-801. OIL PRESSURE REMAINED NORMAL DURING OIL PRESSURE CHECK. AFTER OIL PSI CHECK PERFORMED GVI OF #1 ENGINE FOR OIL LEAKS, NO LEAKS OR DEFECTS WERE NOTED. ALSO PERFORMED Q400 FIM 79-00-00-810-804, FOUND NO DEFECTS ON CONNECTORS J54&P55. ENGINE OIL PRESSURE CHECK GOOD. RETURNED TO SERVICE.

Part: RELAY — FAULTED (ENG ANTI-ICE) · airframe 21,394 hrs · 23,130 cycles

ENG ADPT HEAT 2 CAUTION ILLUMINATED EN ROUTE. ICE PROTECTION WAS ON FOR 10 MIN BEFORE CAUTION ILLUMINATED. FL250 AT -22C. RETURNED TO FIELD LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND CB 115 VAC INK LIP HTR ENG 2 TRIPPED. SET CB. RAN BOTH ENGINESS FOR 20 MINS WITH HEATERS ON. CB STAYED SET. ENG ADPT HEAT 2 CAUTION DID NOT ILLUMINATE.REPLACED 3000-K4 RELAY FOR PRECAUTIONARY MEASURES IAW Q400 AMM TASK 20-30-16-960-801. RAN BOTH ENGS WITH HEATERS ON USING ICE ON S1X & S2X THERMOSTATS FOR ANOTHER 20 MINS & C/W OPS TEST OF ENG AIR INTAKE ADPT HEATER IAW AMM TASK 30-21-00-710-801. OPS TEST GOOD. CB STAYED SET & ENG ADPT HEAT 2 CAUTION DID NOT ILLUMINATE. RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (ZONE 200) · airframe 21,203 hrs · 22,925 cycles

PITCH TRIM MASTER CAUTION IN-FLIGHT PREFORMED E&A CHECKLIST AND RETURNED TO FIELD. ALL LANDING PARAMETERS NORMAL. REMOVED FROM SERVICE. CDS FAULTS - FCECU FAILURE 67, 63, E7, E3. REMOVED AND REPLACED FCECU IAW Q400 AMM 27-00-01-000-802 AND 27-00-01-400-802. OPS AND FUNCTIONAL CHECK OF FCECU GOOD. FAULTS DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 20,948 hrs · 22,659 cycles

SHORTLY AFTER T/O AT AROUND 10,000FT THE CREW STARTS TO HEAR A HIGH PITCH SQUEAL AND THATS WHEN IN THE FLIGHT DECK WE LOOKED UP AND SAW THE CABIN WAS NOT PRESSURIZING + GOT MASTER WARNING CABIN PRESS. TAN THE CHECKLIST, NO CB'S WERE POPPED. A/C LIMITATIONS WERE NOT EXCEEDED. RETURNED TO FIELD. ON THE GROUND AT THE FATE FA A TOLD ME (CA) THAT SHE NOTICED A GAP IN THE DOOR (MAIN BOARDING DOOR) LIKE THE SEAL WASN'T THERE. REMOVED FROM SERVICE. C/W Q400 FIM TASK 21-30-00-810-801. INSP DOOR SEALS + BLOW OUT PANELS. NO DISCREPANCIES NOTED. NO CURRENT FAULTS. PERFORMED FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL. IAW Q400 AMM TASK 21-31-00-720-801 FUNCTION TEST NORMAL. A/C PRESSURIZED NORMALLY. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 20,846 hrs · 22,562 cycles

AT 1500 AGI ON CLIMBOUT NR 2 ENGINE FADEC CAUTION ILLUMINATED ALONG WITH POWERPLANT MESSAGE AT BOTTOM OF ED. EMERGENCY DECLARED. RETURNED TO FIELD, LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS FOUND FAULT CODE 912 BOTH A & B CHANNELS NR 2 ENGINE. R & R 2.2 INTERSTAGE BLEED VALVE, IAW AMM TASKS 75-31-11-000-801-ARA 1 TO 4A AND 75-31-11-400-801 PARA 1 TO 3 & PARA 4B TO 5K. FAULTS CLEARED AND DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 20,816 hrs · 22,535 cycles

AFTER TAKEOFF, NR 2 AC GEN CAUTION LIGHT ILLUMINATED. E & A CHECKLIST RESET PROCEDURE DID NOT EXTINGUISH THE LIGHT. REMOVED FROM SERVICE. REPLACED NR 2 AC GEN, IAW Q400 T/C 6242101. NO FAULTS NOTED. GROUND RAN, OPERATIONS CHECK & LEAK CHECKS GOOD. A/C OK FOR SERVICE.

Part: BOTTLE — CRACKED (FIRE EXTING) · airframe 20,572 hrs · 22,270 cycles

NACELLE HIGH RATE FIRE BOTTLE AFT DISCHARGE TUBE CRACKED. REMOVED AND INSTALLED SERVICEABLE TUBE PN 82620125-001, IAW Q400 AMM TASK 26-21-01-400-801 PARA 4B STEPS 5 THRU 10.

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 20,084 hrs · 21,740 cycles

FLAP POWER CAUTION ILLUMINATED WHEN FLAPS WERE SELECTED FROM 15-35 DEGREE. ACCOMPLISHED E/A CHECKLIST FLAP POWER CAUTION ILLUMINATED AGAIN. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND FAULT ECS CONTINOUS BIT ERASED FAULTS PER Q400 AMM 45-00-27-743-802. PERFORMED FLAPS OPS TEST PER Q400 AMM 27-50-00-710-801. OPS TEST GOOD. FAULT AND CAUTION DID NOT RETURN. RETURNED TO SERVICE.

Part: PCU — INOPERATIVE (NR 2 ENGINE) · airframe 19,855 hrs · 21,491 cycles

NR 2 PROP DID NOT COMPLETELY FEATHER DURING SHUTDOWN. REMOVED FROM SERVICE. PERFORMED FEATHER CHECK OF NR 2 ENGINE PER AMM TASK 71-00-00-868-819 AND FUNCTIONAL TEST OF NR 2 PROPELLER TIME TO UNFEATHER PER 61-20-00-720-802. NR 2 PROPELLER IS STILL NOT FULLY FEATHERING PRIOR TO SHUTDOWN NO FAULTS IN CDS. NR 2 PROP FULLY FEATHERS USING ALTERNATE FEATHER METHOD. PERFORMED GROUND RUN AND NR 2 PROP FULLY FEATHERED ON SHUTDOWN. REMOVED NR 2 BETA TUBE REF MTC 6610001. REMOVED #2 PCU REF AMM TASK 61-20-11-000-801. INSTALLED NEW PCU REF AMM TASK 61-20-11-400-801. INSTALLED BETA TUBE REF MTC 6710002. PERFORMED RUNS AND OPS CHECKS REF MTC 6710006. OPS AND LEAK CHECKS GOOD. NO FAULTS IN CDS. AIRCRAFT RETURNED TO SERVICE.

Part: STRIP — LOOSE (CABIN) · airframe 19,692 hrs · 21,294 cycles

FWD FLOOR STRIP ON LEFT SIDE PEELING BACK. REMOVED FROM SERVICE. RE-SECURED STRIP WITH CARPET TAPE. AIRCRAFT RETURNED TO SERVICE.

Part: HINGE — MALFUNCTIONED (ZONE 200) · airframe 19,685 hrs · 21,287 cycles

FA A FLIGHTLIGHT COMPARTMENT NOT SPRINGING CLOSED, BELOW A JUMPSEAT. REMOVED FROM SERVICE. R+R DOOR CLOSE SPRINGS AND HINGES ON FWD FA SEAT EMER EQUIPT DOOR WITH NEW FROM STOCK. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 19,517 hrs · 21,087 cycles

PHOTO LUMINESCENT STRIP IN FRONT OF ROW 1 DETACHED. REMOVED FROM SERVICE. REINSTALLED FLOOR STRIP AND SECURED. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 19,362 hrs · 20,906 cycles

EMERGENCY EXIT LIGHTING STRIP IN FWD ENTRY DETACHED FROM FLOOR. REMOVED FROM SERVICE. RE-SECURED FLOOR PATH LIGHTING AT 1A. AIRCRAFT RETURNED TO SERVICE.

Part: POWER UNIT — INOPERATIVE (TE FLAPS) · airframe 18,716 hrs · 20,151 cycles

UPON SETTING FLAPS 15 DEG ON APPROACH FLAP DRIVE CAUTION ILLUMINATED WHEN FLAPS REACHED 15 DEG FLAP DRIVE CAUTION CHECK LIST COMPLETED FLAP 15 DEG LANDING ACCOMPLISHED. REMOVED FROM SERVICE. INTERROGATED CDS FOR FLAP DRIVE FAULT NO FAULTS REPORTED PERFORMED OPERATION TEST OF FLAPS IAW Q400 AMM 27-50-00-710-801. DUPLICATED FLAP DR CAUTION AT 10 AND 15 DEG. FLAP DRIVE CAUTION EXTINGUISHES DURING FLAP MOVEMENT NO FAULTS REPORTED IN CDS. FERRIED. PER FIM 27-50-00-810-801, R&R FPU IAW Q400 AMM 27-52-01-000/400-801. FUNCTIONAL TEST GOOD. NO FLAP DRIVE CAUTION NOTED. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (LAV SERVICE) · airframe 18,005 hrs · 19,308 cycles

LAV SERVICE PORT INTERNAL DOUBLER CORRODED. REPLACED LAV SERVICE PORT INTERNAL DOUBLER IAW SRM 51-42-05 AND 51-40-15. REPAIRED FRAME FLANGE COMMON TO THE SKIN AT FSX4.1 ON RH SIDE BETWEEN STR 24 AND STR 25 IAW SRM 53-00-00 REPAIR #18 .9 NDT CARRIED OUT IAW NDTM6, 51-00-08-250-801.

Part: SWITCH — MALFUNCTIONED (FEATHER SYSTEM) · airframe 17,675 hrs · 18,909 cycles

TESTED NR 1 PROPELLER ALTERNATE FEATHER SWITCH ON PROP CONTROL PANEL USING CDS AND ARCDU IAW AMM 61-20-41-710-801. FOUND CHANNEL 1A TO OPERATE NOTMALLY BUT CHANNEL 1B STAYS ON WITH THE SWITCH IN THE ON AND OFF POSITIONS. REPLACED THE NR 1 ALTERNATE FEATHER SWITCH LIGHT ASSEMBLY IAW AMM 20-30-7-00/400-801. OPERATIONAL CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,675 hrs · 18,908 cycles

NR 1 PROP SPEEC 1070 WITH ASSOICATED NR 1 PEC CAUTION AND POWERPLANT MESSAGE. SHUTDOWN ENGINE IN FLIGHT AND RETURND TO FIELD. LANDING UNEVENTFUL, NOT OVERWEIGHT. AIRCRAFT OUT OF SERVICE FOR REPAIRS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,626 hrs · 18,849 cycles

CLIMB OUT OF FL180 WE GOT INTERMITTENT FUSELAGE DOOR MASTER WARNING. RAN CHECKLIST AND DIVERTED TO GEG. DESCENDING OUT OF 180 LIGHT STAYED OFF. DOOR SHOWING OPEN ON DOORS PAGE WAS EMERG EXIT TYPE II/III. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INDUCTANCE VALUE CHECKED IN THE PSEU IAW AMM 32-61-00-280-801 OF THE EMG DOOR SENSOR EDRCLLK, SENSOR CHECKED NOMINAL, FAULT CODE UNRSNABL FAR U00 LOGGED INTO PSEU FOR PREVIOUS LEG. PRESSURIZED AIRCRAFT IAW 21-00-00-863-801, COULD NOT DUPLICATE DOOR MASTER WARNING, REMOVED AND REPLACED THE PSEU IAW 32-61-01-000/400-801 AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 17,579 hrs · 18,796 cycles

FLIGHT ATTENDANT EMER LIGHTING SWITCH NEXT TO MAIN CABIN DOOR TOP OF SWITCH GREEN NORMAL ILLUMINATION INOP. REMOVED FROM SERVICE. RELAMPED F/A EMER LIGHT SWITCH AS REQUIRED. LAMP CHECK OK. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: DEAD BOLT — DIRTY (COCKPIT DOOR) · airframe 17,276 hrs · 18,448 cycles

FLIGHT DECK DOOR LOCKING MECHANISM GRINDS HARD TO OPEN DOOR WITHOUT PRYING WITH TWO HANDS. REMOVED FROM SERVICE. CLEANED DEADBOLT, NO FURTHER DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: LENS — BROKEN (EXTERIOR LIGHT) · airframe 17,192 hrs · 18,354 cycles

RIGHT HAND EXTERNAL FORWARD EMERGENCY EXIT LIGHT LENS BROKEN. REPLACED LENS IAW AMM 33-51-11.

Part: WIRE HARNESS — DAMAGED (PROP DE-ICE) · airframe 17,032 hrs · 18,192 cycles

PROP DEICE CAUTION ILLUMINATED DURING CRUISE. CYCLED PER E/A CHECKLIST, CAME ON AGAIN. RAN GROUND RESET ON GROUND UNSUCCESSFULLY. AIR TURN BACK. LANDING UNEVENTFUL. CDS SHOWED OPEN PHASE C FOR NR 1 TMCU. FOUND NR 2 AND NR 3 BLADES ON NR 1 PROP TO HAVE BAD DEICE WIRE HARNESS. R&R BOTH NR 2 AND NR 3 WIRE HARNESS IAW AMM 61-10-06-000/400-805. FUNCTIONAL AND CALIBRATION IS GOOD. PROP DEICE DID NOT ILLUMINATE. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (AUTOFEATHER) · airframe 16,525 hrs · 17,614 cycles

CREW REPORTS AUTOFEATHER SELECT SWITCH WILL NOT LATCH. REMOVED FROM SERVICE. REPLACED SELECT SWITCH PER AMM TASKS 31-10-01-000-802 & 31-10-01-400-802 OPS CK OF FUEL TRANSFER SYS PER TASK 28-23-00-710-801 GOOD, OPS TEST OF PROP CTL PNL PER TASK 61-20-41-710-801 GOOD, OPS TEST OF ENG CTL PNL PER TASK 76-10-11-710-801 GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — SHORTED (NR 1 PROPELLER) · airframe 15,990 hrs · 16,980 cycles

PROPELLER DE-ICE CAUTION APPEARED INTERMITTENTLY DURING FLIGHT. APPEARED TO BE ASSSOCIATED WITH THE LT SIDE. DIVERTED. LANDING UNEVENTFUL, AND REMOVED FROM SERVICE. COMPLIED WITH FIM 30-60-00-810-807, FOUND AN OPEN PHASE B ON THE LT PROPELLER, NR 2 BLADE DE-ICE WIRE HARNESS. REPLACED THE WIRE HARNESS IAW AMM 61-10-06-000/400-805, TESTED GOOD. RETURNED TO SERVICE.

Part: SERVO — NOISE (AILERON) · airframe 15,818 hrs · 16,473 cycles

BINDING OR NOISE FROM AILERON AUTOPILOT SERVO. DISCONNECTED BRIDLE CABLES FROM AILERON SERVO TO AILERON PULLEY. AILERON POPPING NOISE AND BUMP IN YOKE TRAVEL STILL EXIST. RE-CONECTED BRIDLE CABLES AND LOOSLELY TENSIONED. RIGGED AND SAFETY CLIPPED AILERON SERVO BRIDLE IAW MM 22-11-16-830-801. OPS CHECKED GOOD. COMPLETED FREEDOM OF MOVEMENT CHECK, , ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED PER GPM 9.2. RETURNED TO SERVICE.

Part: BOLT — FAILED (GALLEY DOOR) · airframe 13,899 hrs · 14,777 cycles

FLIGHT ATTENDENT REPORTED DURING CRUISE THAT THE GALLEY SERVICE DOOR HANDLE HAD FLOPPED INBOARD. THE DOOR SYNOPTIC PAGE SHOWED THE DOOR TO BE CLOSED AND THERE WERE NO CHANGES IN THE PRESSURIZATION. INSPECTED IAW AMM 52-41-01-400-801, FIG 409, ITEMS 5, AND 8 AND FOUND A BOLT FASTENING HANDLE SPRING TO HANDLE SHAFT HAD FAILED. INSTALLED SERVICEABLE HARDWARE IAW AMM 52-41-01-400-801 PAR. 1A-3A, 4C, AND 5B-5G. PERFORMED A FUNCTIONAL CHECK OF AFT SERVICE DOOR IAW AMM 52-41-00-720-801, CHECKED GOOD. SEARCHED INTERIOR OF DOOR VIA BORESCOPE AND RETRIEVED FAILED HARDWARE. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SHAFT — LACK OF LUBE (GALLEY DOOR) · airframe 13,818 hrs · 14,693 cycles

AFT GALLEY SERVICE DOOR DIFFICULT TO OPEN. CLEAN AND LUBED DOOR HANDLE SHAFT AND ROLLERS. C/W OPS CHECK OF SERVICE DOOR IAW Q400 MM 52-41-00-710-801. OPS CHECK GOOD. RETURN TO SERVICE. NO PARTS REPLACED.

Part: ROPE — EXPOSED (EMERGENCY EXIT) · airframe 13,411 hrs · 14,276 cycles

CORD/ROPE SHOWING FROM FRONT LEFT LOWER CORNER OF EMERGENCY EXIT DOOR AT ROW 2. RE-ADJUSTED CORD / ROPE REF AMM 52-22-00-000-801/400-801. CORD / ROPE NO LONGER SHOWING. ALSO REF AMM 52-23-00-210-801. NO PARTS REPLACED.

Part: APU — MALFUNCTIONED · airframe 12,367 hrs · 13,159 cycles

APU FAILED TO START. FUEL DRIPPING AND STRONG FUEL ODOR. PERFORMED OPERATIONAL TEST OF APU IAW AMM 49-00-00-710-801 SEVERAL TIMES WITH NO DEFECTS. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: PANEL — DAMAGED (WIND TO BODY) · airframe 12,254 hrs · 13,029 cycles

WING TO FUSELAGE PANEL 262HT DAMAGED. REMOVED AND REPLACED IAW SRM 51-42-05 REPAIR-01, AND DWG 85700005 REV-A.

Part: FRAME — CORRODED (BS 116) · airframe 12,254 hrs · 13,029 cycles

FRAME BS 116 HAS EVIDENCE OF SURFACE CORROSION, STRINGER 31L. REMOVED CORROSION IAW SRM 53-00-00 REPAIR -09 PARA 6A 6B. C/W ET AND UT INSPECTION IAW NDTM 51-00-06 AND 51-00-04. NO DEFECTS NOTED. FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15 PG.22 ITEM 305.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, AND DWG 85328201 REV E.

Part: STRINGER — CORRODED (BS 216-136) · airframe 12,254 hrs · 13,029 cycles

STRINGER 31R, HAS EVIDENCE OF SURFACE CORROSION, BS 216 - 236. REMOVED CORROSION IAW SRM 51-21-00 -02 PARA 4.A ITEMS 5A THRU 5D. C/W ET AND UT INSPECTION IAW NDTM 51-00-06 AND 51-00-04. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00-00-01 AND SRM 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-05, AND SRM 51-41-00-00-01.

Part: SEAT TRACK — CORRODED (BS 361-489) · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED BS 361 - 489.5. REMOVED AND REPLACED IAW SRM 51-42-05-020-01, 51-41-00-00-01 & DWG 85361501 REV.D. RESTORED FINISH ON TRACK 7 SRM 51-25-10-02-01 & 51-25-25-02-010.

Part: SEAT TRACK — CORRODED · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-05-00-01 & 51-40-15-020-010, AND SRM 51-40-07.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01, 51-41-00-00-01 & 51-40-15-02-01, AND DWG 85328201 REV E.

Part: SEAT TRACK — CORRODED · airframe 12,254 hrs · 13,029 cycles

SEAT TRACK NR 8 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-41-00, 51-40-15, AND 51-40-07.

Part: BEAM — CORRODED (BS 71-94) · airframe 12,254 hrs · 13,029 cycles

BEAM FOUND CORRODED AT EMERGENCY EXIT DOOR BS 71.20 - 94.80. REMOVED CORRODED BEAM. INSTALLED NEW BEAM IAW SRM 51-42-05-02-01, 51-42-45-02-01 AND DWG 85329511, AND 51-41-05-00-01.

Part: SEAT TRACK — NOT REPORTED (NR 9) · airframe 12,254 hrs · 13,029 cycles

REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-41-00.

Part: ACTUATOR — FAILED (OIL TEMP) · airframe 12,033 hrs · 12,791 cycles

NR 1 ENGINE OIL TEMP 108 DEGREES ON INITIAL CLIMB FOR ABOUT 1 MINUTE. CDS DATA SHOWS 108.7 DEGREES FOR 160 SECONDS AND NO FAULT CODES. REPLACED THE NR 1 ENGINE OIL COOLER AIR OUTLET FLAP ACTUATOR.

Part: PROPELLER — UNKNOWN (NR 1) · airframe 11,989 hrs · 12,751 cycles

NR 1 PROPELLER FAILS TO UNFEATHER WITH THE FEATHERING PUMP. REMOVED CONNECTOR P30 FROM THE PCU AND CHECKED CONTINUITY BETWEEN PINS A & B, WAS 49.9 OHMS. REINSTALLED CONNECTOR WITH HEAT SHRINK. PERFORMED OPS CHECK WITH MAINTENANCE 671006. CHECKS GOOD WITH NO DEFECTS.

Part: LIGHT — UNSECURE (CABIN FLOOR) · airframe 11,972 hrs · 12,736 cycles

EMERGENCY LIGHT STRIP FWD FOR F/A SEAT IS NOT ATTACHED TO THE FLOOR. SECURED THE LIGHT IAW AMM 33-51-16-40-801. CHECKED GOOD, RETURNED TO SERVICE.

Part: FLT CONTROLS — MALFUNCTIONED · airframe 11,816 hrs · 12,568 cycles

TAKEOFF ABORTED DUE TO TAKEOFF WARNING AT 105 KNOTS. REPLACED CONDITION QUADRANT. OPS CHECK GOOD. C/W INSPECTION AFTER EXCESSIVE BREAKING. NO DEFECTS NOTED. FUNCTIONAL CHECK OF BRAKES GOOD.

Part: LIGHT — DEGRADED (CABIN) · airframe 9,741 hrs · 10,269 cycles

THE 2 ENTRANCE EMERGENCY LIGHT STIPS ON THE FLOOR ARE DEGRADED. REPLACED THE STRIPS IAW AMM 33-51-16-000/400-801.

Part: WIRE HARNESS — MALFUNCTIONED (MLG) · airframe 8,934 hrs · 9,404 cycles

AFTER TAKEOFF, LT GEAR UNSAFE DOOR, RED, STAYS ILLUMINATED AND GEAR HANDLE RED LIGHT STAYED ON. NOSE AND RT GEAR ALL SHOWED RETRACTED AND DARK. AT APPROXIAMATELY 1000 FT ABOVE FIELD ELEVATION, MAYBE 15-20 SECONDS, LT GEAR UNSAFE LIGHT, RED, AND GEAR HANDLE UNSAFE LIGHT WENT DARK, ALL INDICATIONS NORMAL FOR REST OF FLIGHT, NORMAL GEAR EXTENSION. LANDING UNEVENTFUL. CHECKED PSEU FOR FAULTS. NONE FOUND. REPLACED LT MLG NR 1 AND NR 2 DOWNLOCK PROX SENSOR HARNESSES. CYCLED MLG, OPS CHECK GOOD. ACFT RELEASED FOR CHECK FLIGHT. CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 8,925 hrs · 9,394 cycles

ON TAKEOFF, AUTO FEATHER BRIEFLY ARMED AND THEN REVERTED BACK TO AUTO FEATHER. SELECTED TAKEOFF WAS ABORTED, ABORT WAS AT LESS THAN 60 KTS. INTERROGATED CDS FOUND FAULT CODE 70B ON PEC, NR 1 AND PEC, NR 2 AND 398B ON PEC, NR 1 COMPLIED WITH FIM 61-20-02-810-835 OMITTING STEPS A3 2 61-20-08-810-818, FAULT CODE CLEARED. COMPLIED WITH OPS TEST OF PROPELLER AUTO FEATHER AND UPTRIM SYS IAW AMM 61-20-00-710-801 AUTO FEATHER TEST PASSED. MESSAGE WAS DISPLAYED ON ENGINE DISPLAY. RECHECKED CDS, NO FAULTS CODES WERE DISPLAYED.

Part: CONTROL PANEL — UNKNOWN (MLG) · airframe 8,922 hrs · 9,389 cycles

ON DEPARTURE WE NOTICED UPON GEAR RETRACTION THE LT GEAR WARNING LIGHT REMAINED ON WITH GEAR HANDLE ILLUMINATED . IT REMAINED ON UNTIL APPROXIMATELY 1000 FT WHEN THE GEAR DOORS CYCLED BUT THE RED GEAR UNSAFE REMAINED. AT APPROXIMATELY 2000 FT THE GEAR DOOR CYCLED AGAIN AND THE LT GEAR UNSAFE LIGHT AND GEAR HANDLE LIGHT EXTINGUISHED. ALL INDICATIONS NORMAL AFTER. ACCOMPLISHED ALTERNATE GEAR EXTENSION ON LANDING. LANDING UNEVENTFUL. IAW TASK 32-61-00-742-801 RETRIEVED DATA FROM PSEU. NO CURRENT FAULTS. LAST FLIGHT LEG POSTED NOSE GEAR LOCK 1 & 2 BOTH NEAR, NOSE GEAR DRCL NEAR; DR CL AND LANDING GEAR DR CL BOTH FAR; NOSE GEAR DN1+2 BOTH FAR; NG DRL FAR' DIN01A +01B FAILED. LANDING GEAR UPLOCK NEAR. FOLLOWING AMM 32-73-11 LANDING GEAR DISCREPANCIES GUIDE, ALL FAULT CODES IN HISTORY ABOVE MAY HAVE BEEN INDUCED BY CREW ALTERNATE EXENSION EVENT EXCEPT LANDING GEAR UPLOCK NEAR AND DIN01A FAILED. VERIFIED MH OF LT & RT UPLOCK 8.367 AND 8.410 WITHIN NOMINAL /NEAR IAW AMM 32-61-00-280-801. CW GVI OF NOSE, LT AND RT GEAR AND SENSORS NDN. MLG FAILED TO RERACT WHILE TESTING. FOUND LOOSE TARGET ON LT MLG UPLOCK, TIGHTENED, NO HELP. REPLACED LANDING GEAR CP IAW AMM 32-31-01-000/400-801. LANDING GEAR OPS TESTED GOOD IAW AMM 32-31-00-710-801. RETURNED TO SERVICE.

Part: GUARD — MISSING (EMERGENCY LIGHTS) · airframe 8,672 hrs · 9,111 cycles

F/A REPORTED THAT THE EMERGENCY LIGHT SWITCH GUARD IS MISSING. REPLACED THE SWITCH GUARD ASSY, RETURNED TO SERVICE.

Part: HINGE — DAMAGED (EQUIPMENT DOOR) · airframe 8,563 hrs · 8,998 cycles

AFT F/A EMERGENCY EQUIPMENT DOOR IS NOT SELF CLOSING. REPLACED THE EQUIPMENT DOOR SPRING HINGES AS REQUIRED. OPS CHECK OF DOOR IS GOOD. RETURNED TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 7,668 hrs · 7,996 cycles

DURING CLIMBOUT THROUGH 10,000 FT, CAPTAIN`S PFD DISPLAYED IAS FAIL, ATT FAIL, ALT FAIL, IVSI FAIL, HDG FAIL, AFCS FAIL AND TCAS FAIL. REVERTING TO MFD ALL INFORMATION RETURNED WITH NO FAIL FLAGS. SWITCHING BACK TO PFD ALL ABOVE FAIL FLAGS RETURNED. RETURNED TO FIELD. LANDING UNEVENTFUL. CONFIRMED FAULT. REPLACED CAPT PFD REF TASK CARD 6316104. RETURNED TO SERVICE.

Part: SEAL — OUT OF POSITION (AFT PAX DOOR) · airframe 7,419 hrs · 7,725 cycles

DURING CLIMBOUT, AT 8000 FT, F/A CALLED TO REPORT LOUD HISSING FROM AFT PAX DOOR AS WELL AS 2 INCH GAP OF DAYLIGHT. RETURNED TO FIELD, LANDING UNEVENTFUL. PRESSURIZATION CHECKED IAW AMM 21-00-00 NO DEFECTS NOTED, VERIFIED GAP AT FWD MID DOOR SECTION ADJUSTED SEAL TO PROPER FIT IAW AMM 52-12-21. RETURNED TO SERVICE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 6,415 hrs · 6,599 cycles

THRESHOLD SHOWS EVIDENCE OF CORROSION. INSTALLED NEW THRESHOLD IAW SRM 51-42-05.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 6,415 hrs · 6,599 cycles

AFT PASSENGER DOOR EDGE ANGLE CORRODED AROUND NUTPLATES. REPLACED CHANNEL IAW SRM 51-42-05 AND DWG 85339511, REV B.

Part: CHANNEL — CORRODED (DOOR THRESHOLD) · airframe 6,415 hrs · 6,599 cycles

FOUND CORROSION ON MAIN CABIN DOOR THRESHOLD CHANNEL, INSTALLED NEW CHANNEL AT MAIN CABIN DOOR IAW SRM 51-42-05.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 6,415 hrs · 6,599 cycles

CHEMICAL COATING DAMAGED ON FUEL PANEL 624CT. REMOVED CORROSION ON MATING SURFACE OF PANEL 624CT REF SRM 57-20-35-02-02. ORIGINAL THICKNESS OF PANEL 624CT IS .120". REMAINING MIN ALLOWABLE IS .105". MIN MATERIAL REMAINING IS .121". WITHIN LIMITS REF SRM 57-20-35-02-02. C/W ET INSP ON PANEL 624CT NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH BY TOUCH-UP BARE METAL WITH ALODINE IAW SRM 51-21-10-02-01. RE-IDENTIFIED THE REWORKED PANEL IAW SRM 57-20-35 STEP 7A(7). RE-INSTALLED INNER & OUTER SEAL IAW AMM 57-21-01-400-801 STEP 4E(3).

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 6,415 hrs · 6,599 cycles

FOUND CORROSION ON THRESHOLD PLATE . LOCATED AND DRILLED FASTENER HOLES ON A NEW THRESHOLD PLATE, PAX DOOR IAW SRM 51-40-07. REMOVED PAX DOOR THRESHOLD PLATE IAW SRM 51-42-05 4 (E). INSTALLED A NEW PAX DOOR THRESHOLD PLATE IAW SRM 51-42-05-02-01 4 (D) 1.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 6,415 hrs · 6,599 cycles

SEAT TRACK NR 10 HAS CORROSION UNDER AFT INBD LAVATORY CLEAT AND FWD INBD FWD CARGO CLEAT. FOUND OUT OF LIMITS IAW SRM 53-20-49, REPAIR -03. SEAT TRACK REMOVED IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-41-00. NEW SEAT TRACK DRILLED AND LOCATED IAW SRM 51-40-07. NEW SEAT TRACK INSTALLED IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-41-00.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 6,415 hrs · 6,599 cycles

FOUND CORROSION ON ANGLE AT AT STATION 26.7 ON PASSENGER DOOR SURROUND STRUCTURE. INSTALLED NEW ANGLE IAW SRM 51-40-07.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 6,415 hrs · 6,599 cycles

FOUND CORROSION ON ANGLE AT X 6.7 ON PASSENGER DOOR SURROUND STRUCTURE. REPLACED ANGLE IAW SRM 51-42-06.

Part: BRACKET — CRACKED (UNKNOWN) · airframe 6,415 hrs · 6,599 cycles

FOUND CRACKED BRACKET . REPLACED BRACKET IAW SRM 51-42-05.

Part: VALVE — MALFUNCTIONED (DE ICE SYS) · airframe 4,685 hrs · 4,760 cycles

DE-ICE PRESSURE CAUTION LIGHT. LT OTBD WING STATUS 1-2 DID NOT ILLUMINATE GREEN WITH BOOTS IN FAST OR SLOW MODE. DEICE PRESS 18 PSI (OAT -38 DEC C FL250). DIVERTED FLIGHT, LANDING UNEVENTFUL. REMOVED NR1 DDV LT WING, REF AMM TASK 30-11-16-000-801, REPLACED REF AMM TASK 30-11-16-400-801, PERFORMED OPS TEST REF AMM TASK 30-11-16-710-810, OPS CKECKED GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (COCKPIT LIGHTS) · airframe 3,451 hrs · 3,509 cycles

CAPTAIN'S SIDEWALL LIGHT IS DIM AND THE LENS IS BURNED. LAMPED THE SIDEWALL LIGHT AND REPLACED THE LENS. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LATCH — BROKEN (ZONE 200) · airframe 3,129 hrs · 3,169 cycles

LATCHES FOR FLASHLIGHT AND LIFEVEST COMPARTMENT BENEATH THE FWD F/A SEAT WILL NOT LATCH. REPLACED INBD LATCH ON FLASHLIGHT/LIFEVEST COMPARTMENT BENEATH THE FWD. F/A SEAT AS REQ OP'S CHECKS GOOD. COMPARTMENT NOW LATCHES NORMAL, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CABIN PRESSURE) · airframe 2,717 hrs · 2,757 cycles

FAULT LIGHT ILLUMINATED ON CABIN ALTITUDE CONTROL PANEL. AFTER CONDUCTING CHECK LIST, LIGHT EXTINGUISHED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. COMPLIED WITH FIM TASK 21-30-00-810-802. CDS SHOWS FAULTS; AFT OUTFLOW VALVE FAIL AND CPC/OF VALVE DATA FAIL ON CPCS PAGE. FAULTS CLEARED. COMPLIED WITH FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL IAW AMM TASK 21-31-00-720-801. TESTED GOOD. OUTFLOW VALVE CHECKED GOOD IN MANUAL MODE. INSPECTED MAIN CABIN DOOR SEAL DURING PRESSURIZATION, NO LEAKS NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,012 hrs · 997 cycles

F/A NOTIFIED FLIGHT DECK OF A STRONG ODOR IN BOTH THE FWD GALLEY AND AFT GALLEY. F/A STATED ODOR STARTED JUST AFTER TAKEOFF AND GOT STRONGER AS THE FLIGHT PROGRESSED. F/A STATED ODOR STRONG ENOUGH TOWARDS END OF FLIGHT CAUSING NAUSEOUS FEELING. NO ODOR NOTED IN COCKPIT. INSPECTED FWD & AFT GALLEYS. NO ODOR NOTED. INSPECTED ALL CABINETS, NO LEAKAGE. NO FURTHER DEFECTS NOTED. ALL TRASH CANS INSPECTED. NO OTHER DEFECTS. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONNECTOR — DIRTY (MLG) · airframe 505 hrs · 475 cycles

LANDING GEAR FAILED TO RETRACT (3 RED GEAR LIGHTS). NO ABNORMALITIES IN HYD PRESSURE OR QUANTITY NOTED. NO ADDITIONAL CAUTION OR WARNING LIGHTS. RETURNED TO FIELD, LANDING UNEVENTFUL, FERRIED. INTERROGATED PSEU PRESENT FAULTS FOUND NW CENTER RIGGING FAR GAP TO SMALL. INSPECTED NOSE GEAR AREAS AND HARNESSES, FOUND NR2 RVDT CONNECTOR PLUG WITNESS MARK VISABLE, CLEANED CONNECTOR PLUG AND RESECURED. RAN ACFT AND OPERATED NW STEERING. RECHECKED PSEU WITH NO PRESENT FAULTS SHOWN. INSPECTED LG PROX SENSOR VALUES, NLG DOOR LINKAGE AND SEQUENCE VALVE, NWS NWP1, NWP2, PHCP, AND PEDP VALUES, AND LG SELECTOR VALVE SOLENOID RESISTANCE. NO DEFECTS NOTED. R & R LG CONTROL PANEL AS A PRECAUTIONARY MEASURE. OPS TEST GOOD. C/W OPS TEST OF LG EXTENSION AND RETRACTION SYS IAW TASK 32-31-00-710-801. OPS TEST GOOD. COULD NOT DUPLICATE LG DISCREPANCY ON SEVERAL EXT AND RET CYCLES. OPS CHECK FLIGHT GOOD. RETURNED TO SERVICE.