N448QX

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,470 hrs · 22,056 cycles

SMOKE IN CABIN AFTER BOTH ENGINES STARTED AND APU WAS TURNED OFF. SMELLED ELECTRICAL. VISIBLE SMOKE IN COCKPIT AND CABIN. HEARD AN ODD NOISE COMING THROUGH THE HEADSET AND THEN WE SMELLED THE SMOKE. REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF BOTH ENGINES & APU COMPARTMENT. NO DISCREPANCIES NOTED. RAN APU FOR 15 MINUTES WITH BL AIR ON. NO VISIBLE SMOKE, OR ANY UNUSUAL SMELL/ NOISES. PERFORMED OPS TEST OF AC VARIABLE FREQUENCY GEN SYSTEM, REF Q400 AMM TASK 24-21-00-710-801, OPS TEST PASSED. PERFORMED OPS TEST OF 28 VDCGEN SYSTEM, REF Q400 AMM TASK 24-31-00-710-802, OPS TEST GOOD. PERFORMED OPS TEST OF ENGINE AIR INTAKE ANTI ICE, REF Q400 AMM TASK 30-21-00-710-801. OPS TEST PASSED. PERFORMED RECIRC OPS TEST REF Q400 AMM 21-22-16-710-801, OPS TEST PASSED AND OPS TEST OF BLEED AIR SYSTEM REF Q400 AMM TASK 36-11-00-710-802, OPS TEST PASSED. NO FAULTS LOGGED IN CDS, OR EPCU, NO SMOKE IN CABIN OR FD. NO ODD NOISE IN HEADSET. PERFORMED GVI OF RECIRC FAN, AND VARIOUS RELAYS, NO DEFECTS OR ABNORMALITIES FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — LEAKING (RT MLG) · airframe 19,590 hrs · 21,181 cycles

DURING POST FLIGHT WALK AROUND AIRCRAFT RIGHT SIDE INBOARD BRAKE WAS SMOKING. REMOVED FROM SERVICE. REMOVED AND REPLACED RINBD (#3) BRAKE ASSY IAW Q400 T/C 6324201. A/C OK FOR SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 19,108 hrs · 20,695 cycles

FLUORESCENT FLOOR STRIP IN FRONT OF SEATS 2E 02D IS DETACHED. REMOVED FROM SERVICE. REINSTALLED FLUORESCENT FLOOR STRIP IN FRONT OF SEAT ROW 2D E AS REQUIRED NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 18,962 hrs · 20,547 cycles

EMERGENCY LIGHTING STRIP AT 2D,E CAME LOOSE. REMOVED FROM SERVICE. RE SECURED EMERGENCY LIGHTING STRIP AS NECESSARY AT ROW 2D,E. AIRCRAFT GOOD FOR SERVICE.

Part: GENERATOR — INOPERATIVE (NR 1) · airframe 18,953 hrs · 20,539 cycles

NR 1 AC GEN CAUTION ILLUMINATED AT 60 KIAS ON T/O ROLL ABORTED T/O RAN CHECKLIST. UNSUCCESSFUL RESET. ABORTED TAKE OFF. RETURNED TO GATE. REMOVED FROM SERVICE. A/C GEN R & R CHAPTER 5 INSPECTION. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 18,841 hrs · 20,421 cycles

FLUORESCENT FLOOR STRIP IN FRONT OF 2 D/E CAME UNATTACHED FROM FLOOR. REMOVED FROM SERVICE. RE-SECURED FLUORESCENT STRIP AS REQUIRED, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 18,816 hrs · 20,394 cycles

IN FRONT OF 2 D/E EMERGENCY LIGHT STRIP IS NOT ATTACHED. REMOVED FROM SERVICE. FOUND PHOTO LUMINESCENT STRIP IN FRONT OF SEATS 2 D/E COMING UP. NOTED ADHESIVE NO LONGER STICKING. R & R ADHESIVE TAPE & REINSTALLED STRIP, IAW Q400 AMM 33-51-16-400-801. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 18,757 hrs · 20,338 cycles

RAMP REPORTS PHOTOLUMINESCENT STRIP LOOSE AT 2DE. REMOVED FROM SERVICE. RESECURED W/DOUBLE SIDED TAPE AS NECESSARY. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 18,357 hrs · 19,891 cycles

LUMINESCENT STRIP IN FRONT OF 2D+E PEELING OFF. REMOVED FROM SERVICE. RE-SECURED LUMINESCENT TAPE IN FRONT OF 2D+E. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: APU — SMOKE (APU BAY) · airframe 17,641 hrs · 19,124 cycles

APU FAILED 1ST ATTEMPT ,THEN ON 2ND ATTEMPT RAMP AGENT SAID THERE WAS SMOKE COMING OUT OF IT. THE LAST CREW SAID THAT ,THEY HAS ISSUES WITH IT FAILING THE FIRST ATTEMPT. REMOVED FROM SERVICE. PERFORMED GV INSPECTION OF APU.FOR ANY LEAKS.NO LEAKS .CLEANED RESIDUAL.AND OPS CHECK IAW Q400 AMM TASK 49-00-00-710-801.OPS CHECK GOOD.NO SMOKE OR ABNORMAL NOISES NOTICED.NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,401 hrs · 18,842 cycles

SEAT RAIL NR 16 FROM FSX668-X783,Y9.250 IS CORRODED. REMOVE AND REPLACED SEAT RAIL NR 16 IAW SRM 51-42-05-02-01, 51-40-07-02-01, 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,401 hrs · 18,842 cycles

REMOVE AND REPLACE NR 9 SEAT RAIL IAW SRM 51-42-05-02-01, 51-40-07-02-01, 51-40-15-02-01.

Part: SINK — ODOR (CABIN) · airframe 16,840 hrs · 18,189 cycles

SULFUR LIKE SMELL COMING FROM FLIGHT ATTENDANT WASH BASIN. REMOVED FROM SERVICE. CLEANED WATER BASIN THOROUGHLY. DRAINED WATER BASIN. ODOR IS GONE. NO FURTHER DEFECTS TO BE NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 16,746 hrs · 18,071 cycles

DURING TAKE OFF, HAD TO ABORT AT 70-80 KTS DUE TO FUESLAGE DOOR WARNING LIGHT COMING ON. AFT BAGGAGE DOOR LIGHT WAS INDICATING OPEN. AIRCRAFT REMOVED FROM SERVICE. GVI OF AFT BAGGAGE DOOR IAW Q400 AMM 05-48-13-941-001. NO DEFECTS NOTED WITH EXTERNAL AREA OF AFT BAGGAGE DOOR. OPS TEST OF AFT BAGGAGE DOOR IAW Q400 AMM 52-31-00-710-801. OPS TEST GOOD. DOOR CLOSES AND ALL INDICATIONS SHOW DOOR CLOSED / LOCKED. NOTE: UPON AIRCRAFT ARRIVAL AT GATE, NOTICED AFT BAGGAGE DOOR HANDLE WAS POPPED OUT OF RECESS.COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 16,738 hrs · 18,059 cycles

DURING DEPARTURE IOPS FAIL FOLLOWED QUICKLY WITH ED MON FAIL ALL DATA FROM ED WENT AWAY A/C RETURNED TO FIELD W/O ANY OTHER PROBLEMS AT TOUCH DOWN WEIGHT IN WHEELS FADEC/DU DISPLAYED ON ED WITH AVIONICS CAUTION OCCURED. REMOVED FROM SERVICE. INTEROGATED CDS EDU MON FAIL FAULT DISPLAYED WITH NO OTHER FAULTS INDICATED REPLACED EDU IAW Q400 AMM 31-61-01-000-801/400-801 OPS TEST OF EDU 31-61-01-710-803 C/W IOP 1&2 TEST QX MTC6314101 CHECK GOOD C/W CDS IOPS TEST IN CDS TEST OK. RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (DEICE PRESSURE) · airframe 15,936 hrs · 17,101 cycles

DEICE PRESS CAUTION IN CRUISE RAN CHECKLIST, WENT AWAY. DEICE PRESS CAUTION CAME ON INTERMITTENTLY TWICE AND WENT OFF. BOOT STOP WORKING IN SLOW AND FAST, WORKED ON MANUAL. DIVERTED. REMOVED FROM SERVICE. PERFORMED GVI OF ALL DEICE BOOTS, NO DEFECTS NOTED. C/W FIM 30-11-01-810-801, NO FAULTS FOUND, ALL WIRES CHECK GOOD. R+R TMU AS PRECAUTIONARY REF, Q400 AMM 30-11-01-000/400-801. R+R ICE+RAIN PROTECTION PANEL AS PRECAUTIONARY REF. Q400 AMM 30-10-01-000/400-801. ALL OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HINGE PIN — OUT OF POSITION (SERVICE DOOR) · airframe 15,857 hrs · 17,009 cycles

CREW REPORTS AFT SERVICE DOOR HARD TO OPEN FROM INSIDE AIRCRAFT. REMOVED FROM SERVICE. FOUND EXTERIOR HANDLE FLAP OUT OF POSITION ON AFT SERVICE DOOR. REPOSITIONED HINGE PIN & STAKED TO PREVENT MIGRATION, CHECKS GOOD NO OTHER DESCREPANCIES NOTED AT THIS TIME. REF: AMM TASK 52-00-00-820-801. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WIRE — FAULTY (ZONE 800) · airframe 14,942 hrs · 15,980 cycles

AT FL 240 DURING CRUISE AFT PAX DOOR INDICATION OPEN. PRESSURIZATION NORMAL, OPEN INDICATION REMAINED STEADY. F/A REPORTS DOOR REMAINED CLOSED/LATCHED BUT THE VENT ON THE DOOR WAS OPEN. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. VERIFIED FAULT IN WIRING BETWEEN CONNECTORS 3261-P14 AND J61 WHERE WIRING ENTERS AIRFRAME STRUCTURE. REPLACED SHIELDED PAIR FROM CONNECTOR 3261-P14 PINS A&B TO 3261-J61 PINS 1,2,&3. REMOVED AFT PAX DOOR PROX. SENSOR (LOCK) REF. AMM TASK 52-71-01-000-802. INSTALLED AFT PAX DOOR LOCK SENSOR IAW AMM 52-71-01-400-802 OPS CHECKS GOOD. INSTALLED INTERNAL DOOR HANDLE ON AFT PAX DOOR IAW AMM 52-12-01-400-801 STEP 4A. RETURNED TO SERVICE.

Part: FASTENER — LOOSE (EMERGENCY LIGHT) · airframe 14,235 hrs · 15,222 cycles

EMERGENCY EXIT SIGN AT THE GALLEY SERVICE DOOR WAS DETACHED. REMOVED FROM SERVICE. AFTER INSPECTION, FOUND A LOOSE FASTENER. SECURED THE FASTENER. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: POTENTIOMETER — NO TEST (TILLER) · airframe 13,703 hrs · 14,652 cycles

AIRCRAFT PULLED AGGRESSIVELY TO THE RIGHT DURING TAXI WITH TILLER AND RUDDER PEDALS CENTERED. REMOVED FROM SERVICE. NOSEWHEEL STEERING RVDTS WERE RIGGED, NOSEWHEEL STEERING TILLER POTENTIOMATER FAILED AN OPS TEST AND WAS REPLACED WITH A SERVICEABLE UNIT. TAXIED FROM HANGAR TO GATE, NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: RETAINER — FAILED (CARGO DOOR) · airframe 13,674 hrs · 14,628 cycles

CABIN PRESSURE WARNING CLIMBING THROUGH 12,000 FEET, BLEEDS ON, OUTFLOW VALVES CLOSED, AUTO MODE, CABIN PRESSURE AROUND 10,000, DONNED MASK AND FOLLOWED CABIN PRESSURE CHECKLIST. REMOVED FROM SERVICE. REPAIRED THE CARGO DOOR SEAL RETAINER AND REINSTALLED THE DOOR SEAL. OPS CHECKED GOOD. AIRCRAFT PRESSURIZED TO 5 PSI WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: PLACARD — DAMAGED (CABIN) · airframe 11,829 hrs · 12,680 cycles

DITCHING DAM INSTRUCTION PLACARD ABOVE MAIN CABIN DOOR DAMAGED. A TEMPORARY/FACSIMILE PLACARD IS INSTALLED PLACED ON NEF REF PLC-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON FUSELAGE STRINGER 24P, BETWEEN X321.00 AND X341.00. CORROSION ON FUSELAGE STRINGER 24P BETWEEN X321.00 AND X341.00 WAS REPAIRED IAW RD8/4-53-8107 ISS 2 DATED FEB 24 2017. NO CRACKS FOUND.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON FUSELAGE STRINGER 24P, BETWEEN X388.00 AND X401.00. CORROSION ON FUSELAGE STRINGER 24P BETWEEN X388.00 AND X410.00 WAS REPAIRED IAW RD8/4-53-8104 ISS I DATED FEB 22 2107. NO CRACKS FOUND.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON FUSELAGE STRINGER 24P, BETWEEN X449.50 AND X469.50. CORROSION ON FUSELAGE STRINGER 24P BETWEEN X 449.50 AND X469.50 WAS REPAIRED IAW RD8/4-53-810B DATED FEB 23 2017. NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (BS 624-668) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK AT Y 9.25 RT, BETWEEN BS 624.50 AND 668.90. REPLACED THE SEAT TRACK WITH NEW IAW SRM 51-40-15-02-01, SRM 51-42-05-02-01, AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK FLOOR BOARD SUPPORT FLANGE AT Y 9.25 RT, BETWEEN X 38.40 AND X 176.00. REPLACED SEAT TRACK 12 IAW SRM 51-42-05-02-01, 51-40-15-02-01 REV 16 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CHAFING FOUND ON CABIN SEAT TRACK FLOOR SUPPORT FLANGE AT Y 9.25 LT, BETWEEN X 38.40 AND X 230.0. REPLACED SEAT TRACK 6 IAW SRM 51-42-05-02-01 REV 16, SRM 51-40-15-02-01 REV 16 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK INBD FLOOR BOARD SUPPORT FLANGE AT Y 9.25 LT, BETWEEN X 469.50 AND 564.50. REPLACED SEAT TRACK 7 IAW SRM 51-42-05-02-01 REV 10, 51-40-15-02-01 REV 16 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK INBD FLOOR BOARD SUPPORT FLANGE AT Y 9.25 RT, BETWEEN X 439.50 AND X 564.50. REPLACED SEAT TRACK 13 IAW SRM 51-42-05-02-01 REV 16, SRM 51-40-15-02-01 REV 16 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK INBD FLOOR BOARD SUPPORT FLANGE AT Y 9.25 LT, BETWEEN X 564.50+6" AND 584.50. REPLACED SEAT TRACK 8 AT Y9.25 LT BETWEEN STA X 570.00 AND X670.00 WITH NEW, PN 85338210-109, IAW SRM 51-42-05-02-01, SRM 51-40-15-02-01, AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON AFT BAGGAGE SEAT TRACK BETWEEN X705.00 AND X712.00, AT Y 9.25 LT. REPLACED SEAT TRACK 9 FROM X 670.0 TO X 782.0 AT Y 9.25 LT WITH NEW, PN 85338210-111, IAW Q400 SRM 51-42-05-02-01, SRM 51-40-15-02-01, AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON CABIN SEAT TRACK FLOOR BOARD SUPPORT FLANGE AT X 71.20, Y 9.25 RT. REPLACED SEAT TRACK 11 AT Y9.25 RT BETWEEN X 10.50 AND X 102.50 WITH NEW, PN 85328210-115, IAW SRM 51-42-05-02-01, SRM 51-40-15-02-01, AND AMM 20-10-01-430-801.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

FWD PASSENGER DOOR CUT OUT LOWER THRESHOLD MEMBER BETWEEN X 1.0 AND X 32.40 FOUND CORRODED. REPLACED FWD PASSENGER DOOR CUTOUT LOWER THRESHOLD MEMBER BETWEEN X 1.0 AND X32.40 WITH NEW IAW SRM 51-42-05-02-01 REV 16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON FUSELAGE FRAME LOWER FLANGE AT X 216.00, BETWEEN STR 30L AND STR 31L. CORROSION ON FUSELAGE FRAME LOWER FLANGE AT X 216.00 BETWEEN STR 30L AND STR 31L WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 REPAIR 9 REV 16. PERFORMED A LOOSE ANGLE REPAIR TO FUSELAGE FRAME LOWER FLANGE IAW SRM 53-00-00 REPAIR 18. NO CRACKS FOUND.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,404 hrs · 12,251 cycles

CORROSION FOUND ON FUSELAGE FRAME LOWER FLANGE AT X 321.00, BETWEEN STR 31L AND STR 32L. CORROSION ON FUSELAGE FRAME LOWER FLANGE AT X 321.00 BETWEEN STR 31L AND STR 32L WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 REPAIR 9 REV 16. PERFORMED A LOOSE ANGLE REPAIR TO FUSELAGE FRAME LOWER FLANGE IAW SRM 53-00-00 REPAIR 18. NO CRACKS FOUND.

Part: CONNECTOR — DEFECTIVE (LANDING GEAR) · airframe 11,399 hrs · 12,249 cycles

LEFT GEAR DOOR LIGHT (AMBER) REMAINED ILLUMINATED AFTER GEAR DOWN. FERRIED FOR REPAIRS. NOSE GEAR GROUND LOCK IS ENGAGED ALL LANDING GEAR IS PINNED DOWN AND PINS SAFETY WIRED. ALL GEAR DOORS ARE PINNED OPEN AND PINS SAFETY WIRED. GVI OF LANDING GEAR AND DOOR. NO DEFECTS NOTED. CONNECTOR 3261-J24 REPLACED AND REPINNED. RETRACTION AND EXTENSION OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF RIG (LANDING GEAR) · airframe 11,388 hrs · 12,242 cycles

DURING LANDING ROLLOUT L DOOR (AMBER) LIGHT ILLUMINATED - 3 SECONDS LATER LEFT (GREEN) EXTINGUISHED FOR 1~2 SECONDS. L DOOR LIGHT REMAINED ILLUMINATED FOR ANOTHER FEW SECONDS BEFORE EXTINGUISHING. INTERROGATED PSEU AND FOUND FOLLOWING "LGDLK2 UNREASONABLE NEAR" REF AMM TASK 32-61-00-742-801. C/W RIGGING OF PROX SENSORS PER AMM 32-61-06-830-801. NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL AS PRECAUTIONARY MEASURE PER M/C REQUEST IAW AMM 32-31-01-000/400-801. FUNC CK GOOD PER 32-31-01-720-801. ALSO C/W VISUAL INSPECTION OF LGDLK2 + 1 SENSORS WITH NO DEFECTS NOTED.

Part: WIRE HARNESS — DEFECTIVE (LT MLG) · airframe 11,388 hrs · 12,243 cycles

LT AFT GEAR DOORS CYCLED ON GEAR EXTENSION THEN REMAINED OPEN, PER PILOT. LANDING UNEVENTFUL. INTERROGATED PSEU, FOUND "LGDLK2" POSITION ERRATIC BETWEEN NEAR & FAR. ALSO FOUND "PSEU CHAN B FAIL CHANNEL INOP". REMOVED & REPLACED LT MLG STAB BRACE SENSOR HARNESS ASS'Y RT, REF AMM TASKS 32-61-06-000/400-802 & MCN NR: 632765-01. REMOVED & REPLACED PSEU, REF AMM TASKS 32-61-01-000/400-801 & FIM TASK 32-61-01-810-808. CYCLED MLG AFT DOORS SEVERAL TIMES - NO DEFECTS NOTED. PSEU INDICATES NO PRESENT FAULTS. RETURNED TO SERVICE.

Part: COVER — OUT OF POSITION (CABIN FLOOR) · airframe 10,403 hrs · 11,208 cycles

DURING CABIN WALK THROUGH, FOUND ALL BUT TWO INBOARD SEAT TRACK COVERS DOWN THE CENTER THAT HAVE EDGES THAT OVERLAP THE EMERGENCY EGRESS LIGHT STRIPS. REINSTALLED AS REQUIRED TO CORRECT CONFIGURATION.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 10,301 hrs · 11,102 cycles

NR 1 ENGINE IS SLOW TO UNFEATHER. PERFORMED FUNCTIONAL TEST OF TIME TO UNFEATHER IAW AMM 61-20-00-720-801. NR 2 PROPELLER WAS 16 SECONDS AND NR 1 WAS 21 SECONDS. REPLACED OVERSPEED GOVERNOR. RETURNED TO SERVICE

Part: LIGHT — BROKEN (CABIN FLOOR) · airframe 9,744 hrs · 10,533 cycles

SECTION OF THE EMERGENCY LIGHTING AT THE FORWARD GALLEY IS BROKEN. REPLACED BROKEN SECTION OF EMERGENCY LIGHT IAW AMM 33-51-16-400-801. RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 9,288 hrs · 9,947 cycles

CABIN PRESSURE WARNING, RAN APPROPRIATE CHECK LISTS AND EXTINGUISHED AT 1000'. WARNING OCCURRED ON FLT 2821 AS WELL, SO HAD BEEN MONITORING. HELD PRESSURE THROUGH FL180, THEN AS LEVELING AT FL 220 THE CABIN PRESSURE KEPT CLIMBING ABOVE 9000'. STARTED A DECENT AND LIGHT CAME ON AND CABIN PRESSURE REACHED 11,000' BEFORE DECREASING. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R AFT OUTFLOW VALVE REF AMM 21-31-16-000-801 AND 21-31-16-420-001. ACCOMPLISHED FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL REF AMM 21-31-00-720-801. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 9,090 hrs · 9,787 cycles

FLOOR PATH LIGHTING ROW 1 CAME LOOSE. REPLACED STRIP LIGHTING. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,989 hrs · 9,666 cycles

THE NORMAL LIGHT FOR THE EMERGENCY LIGHT SWITCH ARM IS INOPERATIVE, RELAMPED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (ROW 1) · airframe 8,914 hrs · 9,578 cycles

EMERGENCY LIGHT AT ROW 1 LOOSE. SECURED THE EMERGENCY LIGHT. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 8,875 hrs · 9,539 cycles

EMERGENCY LIGHT STRIP DETACHED FROM THE FLOOR. SECURED THE LIGHT AND RETURNED TO SERVICE.

Part: APU — SMOKE · airframe 8,663 hrs · 9,315 cycles

AT THE GATE WITH APU RUNNING THE CABIN STARTED FILLING WITH SMOKE. SHORTLY FOLLOWED BY APU AUTO SHUTDOWN. C/W GVI OF APU. OIL IS AT SERVICEABLE LEVEL. NO EVIDENCE OF OIL LEAKAGE OR ANY OTHER DEFECTS FOUND. C/W MCN 62172-01 ISSUE NR 2 AND AIR CONTAMINATION CHECKLIST. C/W AMM TASK 21-00-00-160-801 FOR ECS SYS PURGE USING ACFT ENGINES. OIL SMELL WENT AWAY AND DID NOT RETURN. APU PLACED ON MEL. MEL CLEARED BY REPLACING APU. RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (NR 1 PROPELLER) · airframe 7,888 hrs · 8,484 cycles

AFTER NORMAL TAXI OUT TO THE RUNWAY END, THE NR 1 ENGINE PROPELLER WENT INTO FEATHER UNCOMMANDED TO 200 RPM. TAXI BACK TO THE GATE. AFTER 5 MINUTES TAXI BACK TO THE GATE, THE ENGINE CAME OUT OF FEATHER ON ITS OWN. REPLACED THE NR 1 PEC, CHANNEL "A" HARNESS ASSY, NR 1 PCU. OPS CHECKS GOOD. PROPELLER FEATHERED AND UNFEATHERED AS COMMANDED.

Part: ENGINE — OVERTEMP (NOT REPORTED) · airframe 7,703 hrs · 8,273 cycles

HIGH ENGINE OIL TEMP 107 TO 108 DEGREES. RETURNED TO FIELD LANDING UNEVENTFUL.

Part: CONTROL UNIT — MALFUNCTIONED (PROPELLER) · airframe 7,616 hrs · 8,179 cycles

AT AROUND 10000', NR 1 ENGINE POWER SURGED & ENGINE INDICATION CAUTION, NR 1 TORQUE INCREASED TO APR 110 %, DROPPED TO 68 %, NR 1 PEC CAUTION, NR 1 PROP OVERSPEED, 1060 RPM ENG MESSAGE. C/W EMERGENCY ABNORMAL CHECKLISTS. SHUTDOWN NR 1 ENGINE. CONDITION LEVERS TO 850 RPM AT ABOUT 2500' MSL. APPROXIMATELY 5 MINUTES ELAPSED BETWEEN T/O CHECKLIST & NR 1 PEC CAUTION. RETURNED TO FIELD. LANDING UNEVENTFUL. INTEROGATED CDS & FOUND FAULTS FOR NR 1 ENG 260A & 236B. C/W FIM TASK FOR BOTH. C/W AMM TASK'S FOR BOTH OVERTORQUE AND OVERSPEED INDICATIONS. REPLACED PECU, PCU, BETA FEEDBACK TRANSDUCER, AND THE PECU WIRING HARNESS. C/W ENGINE RUNS IAW TC 6710006. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (NR 1) · airframe 7,567 hrs · 8,122 cycles

NR 1 PEC CAUTION WITH POWERPLANT MESSAGE, PROP RPM 1060. SHUTDOWN ENGINE IAW EMERGENCY CHECKLIST 7.14 EMEGRENCY CHECKLIST. LANDED UNEVENTFUL. EMU INTEROGATED FOR FAULT CODES. FIM TASK ACCOMPLISHED FOR DISCOVERED FAULTS. PEC GROUND RUNS COMPLIED WITH IAW MAINTENANCE 6710006, NO DEFECTS NOTED. REPLACED HOT BRAKES AND WHEELS AS REQUIRED, DUE TO ENGINE EVENT. REPLACED PEC FOUND FAULT CODES 236A AND 360A IN CDS.

Part: TRIM PANEL — MALFUNCTIONED (ZONE 200) · airframe 7,357 hrs · 7,909 cycles

AILERON TRIM RUNAWAY FULL DEFLECTION LT & RT. TRIM BUTTON WAS STICKING ON. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R AILERON/RUDDER TRIM CONTROL PANEL, REF AMM TASKS 27-13-16-000-801 & 27-13-16-400-801. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 10,117 hrs · 10,539 cycles

BRAKES ARE UNRESPONSIVE DURING LANDING, BOTH SIDES. COMPLIED WITH FUNCTIONAL CHECK OF BRAKE SYSTEM IAW AMM 32-42-00-720-801. CHECKS NORMAL. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: SWITCH — DIRTY (EMERGENCY LIGHTS) · airframe 6,405 hrs · 6,880 cycles

EMERGENCY LIGHTS WON'T TURN OFF. CLEANED THE EMERGENCY LIGHT SWITCH AT THE F/A FORWARD PANEL. PERFORMED OPS CHECK IAW AMM TASK 33-51-00-710-802. CHECKED GOOD. RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED (PAX DOORWAY) · airframe 6,205 hrs · 6,654 cycles

FOUND MAIN CABIN DOOR HEAD BUMPER CRACKED AND BROKEN.

Part: STOP — OUT OF ADJUST (PAX DOOR) · airframe 5,823 hrs · 6,199 cycles

MAIN CABIN DOOR HANDLE IS DIFFICULT TO LIFT UP. R & R THE FWD, TOP STOP. ADJUSTED IAW AMM TASK 52-11-06-400-801, STEPS 4 B, 1, A, B AND 2, C. FUNCTIONAL CHECKED IAW AMM 52-11-00-720-802. CHECKED NORMAL. RETURN TO SERVICE.

Part: SEAT TRACK — CHAFED (NR 5) · airframe 5,810 hrs · 6,185 cycles

FOUND SEAT TRACK CHAFED IN 5 PLACES. REMOVED CHAFE IAW SRM 53-20-49. FOUND TO BE WITHIN LIMITS IAW SRM 53-20-49, FIG 201, SHT 3. TREATED BLENDED AREAS ON SEAT TRACK NR 2 WITH ALODINE IAW SRM 51-21-10.

Part: SEAT TRACK — CHAFED (NR 19) · airframe 5,810 hrs · 6,185 cycles

SEAT TRACK NR 19 CHAFED BY SEAT FOOT IN THREE PLACES. BLENDED IAW REF SRM 53-20-49. FOUND TO BE WITHIN LIMITS IAW SRM 53-20-49, FIG 201, SHEET 3. TREATED BLENDED AREAS ON SEAT TRACK NR 19 WITH ALODINE REF SRM 51-21-10.

Part: SEAT TRACK — CHAFED (NR 1) · airframe 5,810 hrs · 6,185 cycles

FOUND SEAT TRACK NR 1 CHAFED IN FIVE PLACES. BLENDED IAW IAW SRM 53-20-49. FOUND TO BE WITHIN LIMITS IAW SRM 53-20-49, FIG 201, SHEET 3. TREATED, BLENDED AREAS ON SEAT TRACK NR 1 WITH ALODINE IAW SRM 51-21-10.

Part: SEAT TRACK — CHAFED (NR 5) · airframe 5,810 hrs · 6,185 cycles

FOUND SEAT TRACK NR 5 CHAFED. BLENDED IAW SRM 53-20-49. FOUND TO BE WITHIN LIMITS IAW SRM 53-20-49 FIG 201 SHEET 2. TREATED BLENDED AREAS ON SEAT TRACK NR 5 WITH ALODINE IAW SRM 51-21-10.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 5,271 hrs · 5,614 cycles

FORWARD EMERGENCY LIGHT BATTERY PACKS ARE DEAD. REPLACED NR 1 EMERGENCY LIGHTS POWER SUPPLY BATTERY PACKS IAW AMM 33-51-00-820-801. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 5,271 hrs · 5,614 cycles

EMERGENCY LIGHT CIRCUIT BREAKER G3 ON LT ESS CP PANEL POPPED. REPLACED NR 3 EMERGENCY LIGHTS POWER SUPPLY UNIT IAW AMM TASK 33-51-01-000-801 AND 33-51-01-400-801. OPS CHECK GOOD C/B REMAINS CLOSED. RETURNED TO SERVICE.

Part: RECEPTACLE — BENT (COCKPIT DOOR) · airframe 4,969 hrs · 5,291 cycles

UNABLE TO OPEN FLIGHT DECK DOOR. CHECKED AND FOUND COCKPIT DOOR LATCH RECEPTICLE BENT. REFORMED, RECEPTICLE SECURED. DOOR AND DOOR LATCH CHECKED NORMAL. RETURNED TO SERVICE.

Part: LATCH — DIRTY (COCKPIT DOOR) · airframe 4,766 hrs · 5,075 cycles

FLIGHT DECK DOOR DIFFICULT TO UNLATCH. CLEANED AND LUBRICATED LATCH. DOOR UNLATCHES NORMALLY.

Part: LATCH — MALFUNCTIONED (COCKPIT DOOR) · airframe 4,558 hrs · 4,838 cycles

CLOSED THE FLIGHT DECK DOOR AND THE DOOR LOCK LOCKED. REMOVED DOOR AND SENT TO HANGAR FOR MODIFICATION IAW T/C 6-52-311. REPLACED DOOR LATCH ASSY AND REINSTALLED FLIGHT DECK DOOR. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 4,497 hrs · 4,774 cycles

F/A EMERGENCY LIGHT SWITCH GUARD RETURN SPRING NOT WORKING. REPLACED SWITCH GUARD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 4,497 hrs · 4,774 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SELECTED ON FROM F/A OR FLIGHT DECK. SWITCH AND EMERGENCY LIGHTS DISARM CAUTION FAILS TO ILLUMINATE WHEN SELECTED TO DISARM. SECURED ELECTRICAL CONNECTOR ON THE RT SIDE OF THE F/A EMERGENCY SWITCH BODY. OPS TESTED GOOD IAW AMM 33-51-00-710-801.

Part: SILL — CORRODED (EMERGENCY EXIT) · airframe 4,329 hrs · 4,598 cycles

EMERGENCY EXIT HAS EVIDENCE OF CORROSION ON SILL PLATE ATTACH FASTENER.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR) · airframe 4,251 hrs · 4,525 cycles

COCKPIT DOOR STUCK SHUT. LUBRICATED THE DOOR LATCH MECHANISM. DOOR NO LONGER JAMS AND NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: STRIKER — OUT OF ADJUST (COCKPIT DOOR) · airframe 4,238 hrs · 4,508 cycles

FLIGHT CREW REPORTED THAT THE FLIGHT DECK DOOR IS DIFFICULT TO CLOSE AND OPEN. HIGH AMOUNT OF FORCE NEEDED AT THE LATCH. ADJUSTED DOOR STRIKE PLATE FOR FIT AS REQUIRED. OPS CHECKED GOOD. DOOR OPENS AND CLOSES WITHOUT ANY BINDING OR EXTRA FORCE REQUIRED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — DISLODGED (CABIN) · airframe 3,135 hrs · 3,327 cycles

EMERGENCY LIGHT STRIP NEAR MAIN CABIN DOOR WAS KICKED LOOSE. RESECURED EMERGENCY LIGHT STRIP. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PANEL — LOOSE (CABIN) · airframe 2,434 hrs · 2,570 cycles

INTERIOR PANEL BY RT EMERGENCY EXIT COMING LOOSE. RELOCATED BUMPER PADS IAW WO 151207 MX 6-25-706. RETURNED TO SERVICE.

Part: DOOR — DAMAGED (AFT PAX) · airframe 2,217 hrs · 2,307 cycles

AFT PASSENGER DOOR HAS A SHARP PIECE EXPOSED. APPLIED TEMP REPAIR IAW GPM SECTION 7.2, AND PLACED ON NEF CAB 03. RETURNED TO SERVICE.

Part: DOOR — DIRTY (MAIN PAX) · airframe 2,134 hrs · 2,233 cycles

F/A REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN. OPENED MCD DRAINED WATER CLEANED DEBRIS, REMOVAL AND REINSTALLATION OF FWD LOWER WARDROBE AND INSERT IAW AMM TASKS 25-24-03-000-803/400-803, INSPECTION OF MCD MECHANISM AND FUNCTIONAL CHECK OF MCD. RETURNED TO SERVICE.

Part: STOP FITTING — OUT OF ADJUST (PAX DOOR) · airframe 1,725 hrs · 1,787 cycles

F/A REPORTS MCD HARD TO OPEN. ADJUSTED MCD STOP BOLTS DUE TO DRAGGING ON STOP FITTINGS AND FUNCTIONAL TEST OF MAIN CABIN DOOR AFTER ADJUSTMENTS. MAIN CABIN DOOR OPENS AND CLOSES NORMALLY FROM INSIDE AND OUT. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (NR 1) · airframe 367 hrs · 372 cycles

NR 1 PROPELLER WILL NOT MX GROUND UNFEATHER WITHOUT BLADE BALANCE ASSISTANCE. GROUND RAN ENGINE, MOVED CLA FOR NR 1 PROP SEVERAL TIMES IN AND OUT OF FEATHER POSITION. AFTER SHUTDOWN UNFEATHERED NR 1 PROP IN GROUND MX MODE. PROP UNFEATHERED WITHOUT ASSISTANCE. NO OTHER DEFECTS NOTED. PERFORMED OPS CHECK OF PROPELLER AUTOFEATHER SYS IN MX MODE IAW AMM TASK 61-20-00-710-805. OPS CHECKED GOOD. ALSO PERFORMED OPS TEST OF PROPELLER ALT FEATHER IAW AMM TASK 61-20-00-710-802. OPS TESTED GOOD. NO FAULTS PRESENT. RETURNED TO SERVICE.

Part: SLIDE CHANNEL — LACK OF LUBE (DRAWER) · airframe 285 hrs · 288 cycles

AFT EMERGENCY EQUIPMENT DRAWER WILL NOT OPEN FULLY. CLEANED AND LUBED AFT EMERGENCY EQUIPMENT DRAWER. DRAWER OPENS NORMALLY AND CLOSES NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED.