N343EN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,982 hrs · 63,468 cycles

WITH THE NR 2 ENGINE RUNNING, AND GPU DISCONNECTED, ALL ACFT LIGHTS EXTINGUISH. NR 2 DC GENERATOR DOES SHOW LOAD. STARTED THE NR 1 ENGINE, FLT DECK LIGHTS ILLUMINATED AND CABIN EXIT LIGHTS WOULD NOT TURN ON AND FA UNABLE TO TURN ON EMERGENCY LIGHTS. EMERGENCY LIGHTS OPS NORMAL FROM FLT DECK. GROUND RAN ENGINES AND OPERATED ALL AVAILABLE LIGHTS, NR 2 GENERATOR OPERATED NORMAL, OK FOR SERVICE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,965 hrs · 63,444 cycles

EMERGENCY EXIT LIGHT AT CENTER AISLE CEILING IS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: SOCKET — BURNED (OVERHEAD LIGHT) · airframe 51,958 hrs · 63,434 cycles

OVERHEAD LIGHT AT SEAT 2DF HAD A BURNED ODOR. PERFORMED AN INSPECTION TO THE OVERHEAD LIGHT. FOUND THE LIGHT SOCKET BURNED.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 51,870 hrs · 63,308 cycles

FLOOR EMERGENCY LIGHT AT ROW 5 & 6, FOUND THE WIRES PULLED OUT AND PLASTIC COVER SECTION DETACHED. REPLACED THE LAMPS. INSTALLED THE PLASTIC COVERS. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: CONTACTOR — FAILED (NR 2 STARTER) · airframe 51,741 hrs · 63,136 cycles

WHEN STARTING NR 2 ENGINE, A BUSS FAULT OCCURED AND ENGINE STARTED. START SWITCH RETURNED TO NEUTRAL. MAIN BATTERY LOAD OF 1.99 AND ELECTRICAL ODOR IN FLT DECK. MAIN BATTERY TEMP IN YELLOW. NR 2 DC GENERATOR DID NOT COME ON LINE. R & R THE NR 2 START CONTACTOR 2431-K2 AND NR 2 STARTER GENERATOR IAW W/C 24-30-02R AND NR 2 DC GCU. GROUND RAN ENGINE. OPS AND LEAK CHECKED GOOD.

Part: STARTER GEN — FAULTY (NR 2 ENGINE) · airframe 51,740 hrs · 63,135 cycles

ON START DC GEN DID NOT COME ONLINE, SMOKE REPORTED FROM NR 2 NACELLE. SHUT DOWN USING T-HANDLE AND FIRED BOTH BOTTLES. R&R NR 2 STARTER/GENERATOR. START/RUN/OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 51,075 hrs · 62,244 cycles

ONE CABIN FLOOR EMERGENCY LIGHT IS MISSING, SUSPECT IT TO BE UNDER THE FLOOR. REMOVED CENTER FLOOR FROM ROWS 1-12 FOUND LIGHT UNDER FLOOR AT ROW 12. SECURED LIGHTS AND SECURED THE FLOOR PANELS FROM ROW 1-12 WITH RETAINED HARDWARE.

Part: CONNECTOR — FAILED (FUEL INDICATOR) · airframe 50,442 hrs · 61,425 cycles

NR 1 ENGINE FUEL GAUGE FLUCTUATING ON THE GROUND. INSPECTED WIRES AT GAUGE CONNECTOR PLUG. PINNED THE CONNECTOR PLUG AT HE FUEL TEMP BULB. GROUND RAN AIRCRAFT. OPS CHECKED GOOD.OK FOR SERVICE.

Part: APU — FAILED · airframe 50,247 hrs · 61,189 cycles

APU FAILED AFTER 30 MINUTES. CHECK FIRE DETECTOR, LIGHT ILLUMINATED. MAINTENANCE VERIFIED BOTTLE DISCHARGED AND RED FUSELAGE DISC BLEW.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,146 hrs · 59,781 cycles

CLOSE CABIN FLOOR EMERGENCY LIGHT AT SEAT 9D-F WILL NOT ILLUMINATE. REMOVED FLOOR LENS COVER R & R LAMP IN MODULE ASSY AND RE-INSTALLED AND SECURED FLOOR LENS COVER, PN OL3071BPEGPL.

Part: WARNING HORN — ACTIVATED · airframe 49,012 hrs · 59,588 cycles

T/O WARNING SOUNDED AT T/O POWER. REJECTED T/O, CYCLED FLAPS, OPS CK NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,927 hrs · 594,758 cycles

3RD FROM FRONT CEILING EMERGENCY LIGHT IS BROKEN, LENS WILL NOT STAY IN PLACE. R & R THE LENS.

Part: WARNING LIGHT — ACTIVATED (STICK PUSHER) · airframe 48,795 hrs · 59,304 cycles

PUSHER SYSTEM FAIL. CAUTION LIGHT ILLUMINATED ON TAXI. DE-ACTIVATED PUSHER SYS IAW APPROXIMATELY 1, 27-9.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,734 hrs · 59,223 cycles

RIGHT FORWARD EMERGENCY EGRESS LIGHT IS INTERMITTENT, THEN INOPERATIVE. R & R BULB, EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW 33-51-05 AT PS2.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,734 hrs · 59,223 cycles

EMERGENCY EXIT SIDEWALL LIGHTS ARE INOPERATIVE. R & R BULBS ON SIDEWALL PANEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,734 hrs · 59,223 cycles

MULTIPLE CEILING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AND BULBS.

Part: SKIN — BULGED (BS 358) · corrosion level 2 · airframe 48,734 hrs · 59,223 cycles

SKIN BULGED OUT AROUND RIVETS ON FUSELAGE BELLY ON AFT END OF BLANKING PLATE AT BS 358, SUGGESTING POSSIBLE CORROSION. FABRAICATED EXTERNAL AND EXTERNAL DOUBLER AND INSTALLED AT STA 358 ON BELLY IAW EO8-53-16-0105 AND RD8 53 14545.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,734 hrs · 59,223 cycles

EMERGENCY EXIT LIGHTS BURNED OUT ON CEILING PANEL C1. R & R BULBS, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,734 hrs · 59,223 cycles

EMERGENCY LIGHT ON CABIN CEILING PANEL IS INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE · airframe 48,438 hrs · 58,816 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT OW 6DF, 5TH FROM AFT END. R & R BULBS AND EMERGENCY LIGHT AT ROW 6DF. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,391 hrs · 58,752 cycles

F/A REPORTS, ELECTRICAL BURNING SMELL DURING FLIGHT IN CABIN, THEN SHORTLY DISSAPATED.....PERFORMED INSPECTION, SUSPECTED ROW 6 AC OVERHEAD LIGHT AT FAULT SEE SEQUENCE 2 FOR MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,350 hrs · 58,697 cycles

3RD EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 48,208 hrs · 58,514 cycles

FUEL ODOR IN CABIN AND COCKPIT AFTER APU START. INSPECTED ACFT AND GROUND RAN BLEED SYSTEM WITH ENGINE AND APU BLEEDS. FOUND FUEL ODOR WITH APU BLEED ONLY. NO SIGN OF FIRE OR OVERHEAT IN APU COMPARTMENT.

Part: APU — ODOR · airframe 48,204 hrs · 58,508 cycles

RAMP REPORTED BURNING ODOR IN CARGO BAY AREA, WHEN APU WAS STARTED. INSPECTED CARGO BAY. NO EVIDENCE OF SMOKE OR FIRE. FOUND OIL VAPOR COMING FROM APU VENT MAST. SERVICE APU OIL. GROUND RAN APU. OPERATED APU BLEEDS, NO LEAK OR ODOR NOTED. AIRCRAFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,288 hrs · 57,309 cycles

RIGHT AFT EGRESS LIGHT AND AFT EXIT CEILING LIGHT IS OUT. R & R EMERGENCY LIGHT BATTERY PS6 IAW WC 33-50-05R. OPS CHECKED GOOD.

Part: PROPELLER — VIBRATION (NR 2) · airframe 47,023 hrs · 56,968 cycles

VIBRATION FELT FROM NR 2 ENGINE BELOW START FEATHER AND DURING ENGINE SHUTDOWN. R & R NR 2 PROP ASSY IAW WC 61-10-06R, 61-00-09R, 61-10-07R AND 61-10-00. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 46,861 hrs · 56,742 cycles

AFTER TAKEOFF AND AUTOFEATHER DISENGAGED. ARM LIGHT REMAINED ILLUMINATED UNTIL DESCENT AND POWER REDUCED, ARM LIGHT EXTINGUISHED. CYCLED SWITCH SEVERAL TIMES. STATIC CHECK AND GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2 ENGINE) · airframe 46,861 hrs · 56,742 cycles

WHILE APPLYING TAKEOFF POWER, NR 2 PROP FEATHERED. ARM LIGHT WAS NOT ILLUMINATED. R & R NR 2 ENGINE TSCU. OPS CHECKED GOOD IAW PIEDMONT RUN UP MANUAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,807 hrs · 56,668 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 1. R & R BULB FOR EMERGENCY FLOOR PATH LIGHT AT ROW 1. OPS CHECKED GOOD.

Part: BRAKE — SMOKE (LEFT) · airframe 46,776 hrs · 56,624 cycles

PASSENGER REPORTED LT BRAKE SMOKING. INSPECTED BRAKE, NO DEFECTS NOTED. OK FOR SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 46,724 hrs · 56,560 cycles

ROW 11 EXIT DOOR SIGN FLICKERED. R & R PS-3 POWER SUPPLY BASE. OPS CHECKED GOOD. GROUND RAN ACFT. OPS CHECKED GOOD WITH PROP HEAT ON. OPS NORMAL. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT A/C BUSS) · airframe 46,660 hrs · 56,470 cycles

RIGHT AC BUSS C/L CAME ON AT CLIMBOUT WITH ASSOC. C/L'S. R & R RT AC GCU AND OPS CHECKED GOOD DURING 15 MINUTE RUN.

Part: BRUSH BLOCK — DAMAGED (PROP DE ICE) · airframe 46,567 hrs · 56,343 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. R & R NR 1 AND NR 2 BRUSH BLOCK ASSYS IAW MM 61-10-11. COMPLIED WITH EMERGENCY LIGHT SYSTEM, OPS CHECK WC 33-50-03Q. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,477 hrs · 56,237 cycles

EMERGENCY LIGHT AT FORWARD EMERGENCY EXIT SIDEWALL IS DIM. R & R THE BULBS. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,477 hrs · 56,237 cycles

EMERGENCY LIGHT BY PAX DOOR IS DIM. R & R THE BULBS, OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 46,453 hrs · 56,206 cycles

AFTER TAKEOFF, CEILING AND WALL EMERGENCY LIGHTS FROM ROW 4 BACK FLICKERED ON AND OFF. R & R EMERGENCY LIGHT CONTROL BOX, OPS CHECKED GOOD IAW MM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,458 hrs · 56,213 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE WHEN ON. R & R BULB, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,421 hrs · 56,160 cycles

EMERGENCY EXIT AND OVERHEAD EMERGENCY LIGHTS AT ROW 11 ILLUMINATED IN FLIGHT. R & R POWER SUPPLY AND BATTERY A PS4. PERFORMED OPS CHECKED IAW MM 33-51-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 46,414 hrs · 56,156 cycles

EMERGENCY LIGHTS AFT OF ROW 4 ILLUMINATE INTERMITTENTLY. R & R EMERGENCY LIGHT BATTERIES AND POWER SUPPLIES AT LOCATION PS6 AND PS7 IAW MM 33-51-05. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,314 hrs · 56,024 cycles

WHILE IN FLIGHT, EMERGENCY SIGN AT ROW 11 ISLE LIGHTS, INCLUDING ROWS 4, 7 AND 10 FLICKERED INTERMITTENTLY. R & R POWER SUPPLY AND BATTERY AT PS6 IAW MM 33-51-05. GROUND RAN ACFT. CHECKED WITH PROP HEAT AND BOTH TIMERS ABOVE AND BELOW. OPS CHECKED GOOD. READY FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 46,166 hrs · 55,834 cycles

EMERGENCY LIGHTS FLICKER AND ARE DIM.

Part: BRUSH BLOCK — DAMAGED (PROPELLER HEAT) · airframe 45,578 hrs · 55,045 cycles

EMERGENCY LIGHTS FLICKERED WITH PROPELLER HEAT ON. R & R NR 1 BUSH BLOCK. CLEARED NR 2 BRUSH BLOCK CONNECTOR AND SLIP RINGS. GROUND RAN ACFT. PROPELLER HEAT OPS CHECKED GOOD, NO FLICKERING OF EMERGENCY LIGHTS.

Part: BRUSH BLOCK — CORRODED (PROPELLER HEAT) · airframe 45,267 hrs · 54,627 cycles

EMERGENCY LIGHTS FLICKERING INTERMITTENTLY DURING FLIGHT. FOUND ALL HEATER LEADS ON NR 1 PROPELLER CORRODED. R & R ALL HEATER LEADS IAW MM 61-10-00 AND BRUSH BLOCK. GROUND RAN . OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BRUSH BLOCK — CORRODED (PROPELLER HEAT) · airframe 45,261 hrs · 54,621 cycles

EMERGENCY LIGHTS FLICKERED INTERMITTENELY IN FLIGHT. FOUND LEADS ON NR 1 PROPELLER FILLED WITH WATER AND CORRODED. R & R LEADS ON NR 1 PROPELLER HS MM 61-10-00. R & R NR 1 BRUSH BLOCK IAW 61-10-00, REINSTALLED BOTH PROP SPINNER. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CLAMP — LOOSE (CHECK VALVE) · airframe 44,851 hrs · 54,084 cycles

BURNING ODOR IN AREA OF ROW 7 WITH HOT OVERHEAD PANELS. INSPECTED AND FOUND WING ISOLATION CHECK VALVE CLAMPS LOOSE. TORQUED AS REQUIRED. NO FURTHER LEAKS NOTED OR ODOR IN CABIN. OK FOR SERVICE.

Part: WIRE — CHAFED · airframe 44,741 hrs · 53,954 cycles

RIGHT AC BUSS CAUTION LIGHT, RT TRU AND ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED IN FLIGHT. CREW RETURN TO FIELD. MAINTENANCE FOUND WIRE CHAFED AGAINST NR 2 AC GCU. REPAIRED WIRE 20003A18B-1. R & R NR 2 AC GCU. GROUND RAN ACFT. NO DEFECTS NOTED. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 44,708 hrs · 53,915 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. FOUND BROKEN WIRE AND REPAIRED IAW AMM 20-4-07. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,494 hrs · 53,641 cycles

SECOND AND THIRD FLOOR PATH EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS FOR SECOND AND THIRD FLOOR PATH EMERGENCY LIGHTS. OPS CHECKED GOOD. REINSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,382 hrs · 53,504 cycles

SECOND RED EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,521 hrs · 52,381 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. R & R BULB, OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (NR 2 ENGINE) · airframe 43,466 hrs · 52,313 cycles

NR 2 ENGINE WOULD NOT START. NO NH INDICIATION. R & R NR 2 STARTER GEN IAW WC24-30-02R, OPS & LEAK CHECKED GOOD.

Part: BLEED AIR SYS — ODOR (NR 1 ENGINE) · airframe 43,322 hrs · 52,132 cycles

FOUL ODOR COMING FROM BLEEDS IN CABIN. R & R NR 1 ENGINE IAW 71-02-02 AND 71-00-01.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 43,316 hrs · 52,122 cycles

HAZE NOTED IN CABIN WITH ODD ODOR ON FLIGHT DECK AND CABIN. GROUND RAN ACFT ACFT AND OPERATED ENGINE AND APU BLEEDS. CYCLED LT AND RT PACKS AND CYCLED NR 1 AND NR 2 ENGINE BLEEDS. CANNOT DUPLICATE DISCREPANCY ON GROUND. OK FOR SERVICE.

Part: PROPELLER — VIBRATION (NR 1) · airframe 43,316 hrs · 52,122 cycles

AFTER TAKEOFF, ENGINE VIBRATION FELT AND CONTINUED TO WORSEN UNTIL RUNUP, NR 1 ENGINE VIBRATION INCREASES WHEN OUT OF FEATHER. COMPLIED WITH INSPECTION IAW AMM 05-50-65 AND REPLACED NR 1 PROP ASSY IAW CARDS 61-10-06 AND 61-10-07 FOR BLADE R & R. RUN AND LEAK CHECKED GOOD.

Part: SOCKET — MISSING (EMERGENCY LIGHT) · airframe 43,082 hrs · 51,815 cycles

EMERGENCY FLOOR PATCH LIGHTS HAS ONLY 28 LIGHTS IN VIEW ILLUMINATED. INSTALLED EMERGENCY LIGHT SOCKET ASSY AT ROW 7 IAW DWG 82520977. OPS CHECKED GOOD.

Part: RCCB — INOPERATIVE · airframe 43,077 hrs · 51,809 cycles

NR 2 STDBY PUMP INOPERATIVE. CREW PERFORMED TEST TO CONFIRM NO INDICATION. FOUND STDBY CIRCUIT BREAKER IN COCKPIT TRIPPED. RESET CIRCUIT BREAKER. OPS CHECKED GOOD. R & R RCCB FOR NR 2 STANDBY PUMP USING RETAINED HARDWARE. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: FITTING — CORRODED (TAB BEARING) · corrosion level 2 · airframe 43,065 hrs · 51,791 cycles

RIGHT ELEVATOR INBD SPRING TAB BEARING FITTING HAS LIGHT COROSION. R & R SRING TAB BEARING FITTING ON RT ELEVATOR IAW SRM 51-42-45 AND SRM 51-42-05.

Part: ANGLE — CRACKED (WING) · airframe 43,065 hrs · 51,791 cycles

CLOSING ANGLE IS CRACKED ON RT SIDE. SEALED CRACK AT SAID LOCATION IAW RD8-53-3050. ALLOWED CONTINUED OPERATION FOR AN ADDITIONAL 40,000 FLIGHTS UNTIL REPLACEMENT.

Part: SILL — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 43,065 hrs · 51,791 cycles

PAX DOOR SILL IS CORRODED. R & R PAX DOOR SILL IAW SRM 51-42-05.

Part: INTERCOSTAL — CRACKED (DOOR HINGE) · airframe 43,065 hrs · 51,791 cycles

LEFT CENTER DOOR FWD HINGE INTERCOSTAL CRACKED. R & R CENTER DOOR HINGE WITH NEW PARTS IAW SRM 51-42-05 AND SRM 51-42-45.

Part: BRUSH BLOCK — FAILED (PROP HEAT) · airframe 43,053 hrs · 51,777 cycles

LEFT 'B' PHASE PROPELLER HEAT HAS NO LOAD OR LIGHT ON BOTH TIMERS. R & R NR 1 BRUSH BLOCK IAW MM 61-10-11. GROUND RAN ACFT IAW OPS MANUAL. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SEQUENCE VALVE — LEAKING (MLG) · airframe 42,834 hrs · 51,490 cycles

AFTER GEAR EXTENSION, NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED AND FOLLOWED BY LOSS OF NR 2 HYD QTY, HYD QTY INDICATED 0.5. INSPECTED AND FOUND NR 2 MAIN GEAR DOOR SEQUENCE VALVE LEAKING. R & R VALVE IAW MM 32-10-51.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,627 hrs · 51,209 cycles

SECOND EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BULB. RESECURED COVER. OPS CHECKED GOOD.

Part: ENGINE — SMOKE (NR 2) · airframe 42,512 hrs · 51,061 cycles

SMOKE IN CABIN REPORTED AFTER ENGINE START. R & R NR 2 ENGINE IAW WC 71-00-01R.

Part: SWITCHING UNIT — FAILED (CABIN AIR) · airframe 42,512 hrs · 51,061 cycles

SMOKE REPORTED IN CABIN AFTER ENGINE STARTS. RAN APU AND BOTH ENGINES INDEPENDENTLY. SMOKE ONLY APPEARS WITH NR 2 ENGINE. R & R AIR SWITCHING VALVE IAW 72-30-00. RAN NR 2 ENGINE. NO FIX.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,799 hrs · 50,114 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOP AT ROW 8, 11 AND 12. R & R EMERGENCY FLOOR PATH LIGHT BULBS AT ROW 8, 11 AND 12. CLOSED ACCESS PANELS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 40,992 hrs · 49,036 cycles

ROW 2DF FLOOR PATH EMERGENCY LIGHTS HAS 2 BULBS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 40,920 hrs · 48,947 cycles

FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE AT ROW 10. R & R BULB. OPS CHECKED GOOD.

Part: PSEU — FAULTED (MLG) · airframe 40,817 hrs · 48,810 cycles

WOW CAUTION LIGHT ILLUMINATED IN FLT. FOUND CARD FAULT ON PSEU R & R PSEU IAW MM 32-61-50. OPS CHECK GOOD, SWUNG GEAR 4 TIMES OPS NORMAL. READ OUT WOW SENSORS, NO DISCREPANCIES NOTED.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 40,388 hrs · 48,251 cycles

DURING CRUISE, NR 2 HYD PUMP CAUTION LIGHT ILLUMINATED WITH ZERO QTY. ENGINE OPERATED APPROX 30 MINUTES DURING RETURN TO FIELD. NO HYD PUMP HOT LIGHT ILLUMINATED. R & R FORWARD FITTING O-RING AT PRESSURE MANIFOLD. INSPECTED DELT- P FOR BYPASS. NONE FOUND. SERVICED HYD SYS AND OPS CHECKED GOOD. R & R NR 2 HYD PUMP ASSY IAW WORK CARD 29-00-00 AND COMPLIED WITH WORK CARD 29-12-02 TO SATISFY REQUIRED AMM 05-50-33.

Part: STRUT — CHAFED (ENGINE MOUNT) · airframe 40,240 hrs · 48,064 cycles

NR 2 NACELLE OTBD LOWER ENGINE SUPPORT STRUT CHAFED AT THE OIL COOLER RETURN LINE. MEASURED AT 0.013". REPAIRED IAW RD8-54-1264.

Part: MODULE — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 40,240 hrs · 48,064 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 7 DIM. R & R 1 LIGHT MODULE AT SAID LOCATION IAW AMM 20-45-07.

Part: LIGHT — UNSECURE (ROW 4DF) · airframe 39,664 hrs · 47,373 cycles

ROW 4DF FLOOR EMERGENCY LIGHT INOPERATIVE. FOUND LIGHT NOT SECURED IN HOLDER, RESECURED LIGHT. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 39,619 hrs · 46,524 cycles

TAKEOFF REJECTED DUE TO AUTOFEATHER NOT ARMING ON TAXIWAY WITH BRAKES SET, ADVANCED POWER LEVERS AND SYS OPS NORMAL. ANOTHER TAKEOFF OK WITHOUT MX. GROUND RAN ACFT IAW SRT MANUAL. COMPLIED WITH AUTOFEATHER OPS CHECKED MULTIPLE TIMES WITH NO DEFECT NOTED. CLEARED MEL 25-6-2.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 38,993 hrs · 46,484 cycles

EMERGENCY FLOOR PATH LIGHT INOP AT ROW 11. R & R EMERGENCY FLOOR LIGHT IN ROW 11.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 38,842 hrs · 46,282 cycles

2 RED FORWARD EMERGENCY LIGHTS ON FLOOR ARE OUT. R & R LIGHT BULBS. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (NR 2 PROPELLER) · airframe 38,539 hrs · 45,890 cycles

DURING TAKEOFF ROLL, WHILE ADVANCE POWER FOR TAKEOFF, NR2 PROP RPM DROPPED TO 500 RPMS AND CONTINUE TO DROP. REPLACED NR 100 TSCU CONTROLLER AND SECURED, OPS CHECKED ACFT IAW -8 MAINT. OPERATING MANUAL. REFERRING TO COMPONENT CHANGE OUT. OPS CHECKED GOOD ON THE GROUND.

Part: LAMP — INOPERATIVE (LIGHT PANEL) · airframe 38,079 hrs · 45,340 cycles

EMERGENCY BUTTON ON F/A CONTROL PANEL AT FWD CABIN IS NOT BACKLIT. RELAMP EMERGENCY BACK LIGHTING, OPS CHECKED GOOD. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,208 hrs · 53,470 cycles

ROW 2 EMERGENCY EXIT SIGN HAS 1 INOPERATIVE LAMP. R & R ROW 2 EMERGENCY EXIT SIGN, OPS CHECKED GOOD.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 37,965 hrs · 45,197 cycles

HARD TO CONTROL NOSE WHEEL STEERING ON LANDING. CREW REPORTED NO CONTROL PROBLEMS UPON LANDING. OK FOR SERVICE. NOSE STEERING LINKS REQUIRED INSP AND OPS CHECK DUE TO PREVIOUS INSTALLLATION. RETRACTED GEAR ON JACKS, OPS CHECKED NOSE STEERING ON GREASE PLATES AND INSPECTED STEERING LINKS, OK FOR SERVICE.

Part: GENERATOR — FAILED (DC) · airframe 37,775 hrs · 44,956 cycles

SUSPECTED LIGHTNING STRIKE LOST NR 1 AND NR 2 DC GENERATORS. IAW MX CONTROL, SUBSEQUENCE RESET AND RUN INDICATES GENERATORS OPERATE NORMAL.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 37,679 hrs · 44,838 cycles

RIGHT SIDE CABIN UNDERFLOOR STRINGER 27S CORRODED JUST BELOW LAV PAN.....REMOVED STRINGER, LAV BOX, AND DOUBLER. BOND TESTED SKIN OPENING. NO DEFECTS NOTED. INSTALLED LAV BOX AND DOUBLER IN ACCORDANCE WITH DEHAV DRAWING 85330983. INSTALLED NEW STRINGER SECTION BELOW LAV PAN 27S.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,973 hrs · 43,899 cycles

CEILING EMERGENCY LIGHT IS DIM ROW 13. RELAMPED ROW 13 CEILING EMERGENCY LIGHT IAW AMM. 33-20-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,973 hrs · 43,899 cycles

ROW 7 FLOOR EMERGENCY ESCAPE PATH LIGHT INOP. RELAMPED ROW 7 FLOOR EMERGENCY PATH LIGHT IAW AMM 33-20-02.

Part: PRESSURE SWITCH — FAILED (NR 1 BLEED) · airframe 36,973 hrs · 43,899 cycles

EXPERIENCED ENGINE SURGE ON NR 1 AND 2 ENGINE OF 8 TO 10 PERCENT TORQUE DURING CLIMBOUT,AFTER SELECTING NR 1 ENGINE BLEED OFF, ENGINE OPPS NORMAL, SURGE RETURNS IF NR 1 BLEED IS SELECTED ON. R & R BOTH NR 1 HIGH PRESSURE SWITCHES. REF DASH8 MM 21-11-21. OPS CK GOOD AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 36,802 hrs · 43,682 cycles

EMERGENCY FLOOR LIGHT AT ROW 8 IS NOT WORKING. REMOVED LENS, REMOVED COVER, R & R BULB. OPS CHECKED GOOD. INSTALLED COVER AND LENS.

Part: PSEU — MALFUNCTIONED (NLG) · airframe 36,764 hrs · 43,638 cycles

NLG PERFORMED UNCOMMANDED PARTIAL EXTENSION WITH ASSOCIATED IN TRANSIT AND UNSAFE INDICATIONS. PERFORMED PSEU TEST AND CODE 58 READ. R &R PSEU IAW 32-61-50. R & R LANDING GEAR HANDLE IAW 32-30-00. CYCLED GEAR SEVERAL TIMES AND CHECKED GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 36,699 hrs · 43,546 cycles

NLG PERFORMED UNCOMMANDED PARTIAL EXTENSION WITH ASSOCIATED IN TRANSIT AND UNSAFE INDICATIONS. INSPECTED NOSE GEAR AND HARNESS FOR OBVIOUS DEFECTS NOTED. CHECKED NOSE GEAR SENSOR GAPES, CHECKED GOOD. R & R LANDING GEAR SELECTOR VALVE IAW WORK CARD 32-30-41R. OPS CHECKED GOOD. CHECKED GEAR IAW 32-30-00.

Part: GARLOCK SEAL — LEAKING (HYD PUMP) · airframe 36,263 hrs · 42,993 cycles

ON TAKEOFF ROLL, NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED JUST AFTER TAKEOFF POWER APPLIED. OIL PRESSURE INDICATOR IN LOWER PORTION OF THE GREEN BAND ABORTED TAKEOFF. FLIGHT CREW VISUALLY NOTED OIL ON INBD GEAR DOORS. NO OTHER LEAKS NOTED. R & R NR 2 ENG HYD PUMP GARLOCK SEAL ASSY AND SERVICE WITH OIL, GROUND RAN ENGINE, NO LEAKS NOTED, OPS CHECKED GOOD.

Part: MODULE — INOPERATIVE (CABIN) · airframe 34,745 hrs · 41,091 cycles

ON JULY 21, IN SBY A FLOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE MODULE WAS REMOVED AND REPLACED AND THE OPERATIONAL CHECK WAS GOOD.

Part: DOOR — UNSECURE (SERVICE DOOR) · airframe 34,558 hrs · 40,879 cycles

TAKEOFF REJECTED AT APPROXIMATELY 20 KNOTS DUE TO UNSAFE SERVICE DOOR WARNING LIGHT. SECURED SERVICE DOOR AS REQUIRED. OPS CHECK NORMAL, NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,168 hrs · 40,362 cycles

LAST TWO EMERGENCY LIGHT AT ROW 8 AND 9 FLOOR LAMP INOP. REMOVED AND REPLACED LIGHT BULB.

Part: AHRS — FAILED (NR 2) · airframe 33,334 hrs · 39,299 cycles

NR 2 ATTITUDE HEADING AND REFERENCE SYSTEM FAILED AFTER ENGINE START. R&R NR 2 ATTITUDE HEADING AND REFERENCE. OPS CHECK GOOD IAW MM 34-20-01 OK FOR SERVICE.

Part: SEAL — TORN (SERVICE DOOR) · airframe 32,739 hrs · 38,561 cycles

AT 18K FEET AIRCRAFT 343EN LOST CABIN PRESSURE WITH A SQUEAL FROM THE REAR SERVICE DOOR. PGV INSPECTED CABIN DOORS. CLEANED AND RESEATED DOOR SEAL AND PLACED PRESSURIZATION ON MEL. ROA MAINT REMOVED AND REPLACED REAR SERVICE DOOR SEAL ASSY IAW AMM 52-36-00. PRESSURIZED AIRCRAFT TO 5.5 DIFF WITH NO LEAKS, CLEAR MEL.

Part: SKIN — DAMAGED (FUSELAGE)

SBY-CLT, FLIGHT 4649. ABORTED TAKEOFF AFTER MULTIPLE BIRD STRIKES TO RIGHT SIDE OF ACFT. RETURNED TO GATE. FOUND BIRD STRIKE BELOW RT WINDSCREEN CLEANED AREA. NO DEFECTS NOTED. INSPECTED PROPS. NO DEFECTS NOTED. (S)

Part: GENERATOR — FAILED (NR 1) · airframe 31,180 hrs · 36,634 cycles

NR 1 AC GENERATOR FAILED IN FLIGHT. THE FLIGHT RETURNED TO CLT. THE NR 1 AC GENERATOR AND AC GENERATOR CONTROL UNIT WERE REPLACED, OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — DISTORTED (COCKPIT) · airframe 30,958 hrs · 36,366 cycles

CAPTAINS SIDE WINDOW HEATING ELEMENT BURNT, AND HAS SEVERAL AIR BUBBLES. WHEN HEAT IS SELECTED ON, VIEW THROUGH WINDOW IS DISTORTED. MAINTENENCE INSPECTED SIDE WINDOW AND OK'ED AIRCRAFT FOR FERRY FLIGHT TO SBY. SIDE WINDOW REMOVED AND REPLACED. OP'S CHECK GOOD.

Part: PIPE — CRACKED (BLEED AIR SYS) · airframe 30,586 hrs · 35,942 cycles

F/A REPORTS, ELECTRICAL SMELL IN MID CABIN. FOUND BLEED PIPE CRACKED. FERRY TO ROA FOR REPAIR.

Part: WARNING HORN — ACTIVATED · airframe 27,968 hrs · 32,784 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. CREW CYCLED GUSTLOCK AND HORN OPS CHECKED NORMAL.

Part: CONTROL BOX — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 27,886 hrs · 32,683 cycles

AFTER TAKEOFF NR 1 ENGINE FEATHERED, TORQUE CLIMBED TO 120 PLUS. AIRCRAFT SHUTDOWN AND RETURNED TO FIELD. REMOVED AND REPLACED AUTO FEATHER CONTROL BOX.

Part: WIRE — DAMAGED (ENGINE OIL SYS) · airframe 27,802 hrs · 32,576 cycles

NR 1 OIL PRESSURE PEGGED ABOVE 100 PSI. REPAIRED WIRES BETWEEN CONNECTORS 9811-P17 AND P29.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 27,761 hrs · 32,521 cycles

INFLIGHT NOSE GEAR UNSAFE LIGHT & LOUD NOISE COMING FROM NOSE WHEEL WELL. PROBLEM CORRECTED ITSELF. SECONDS LATER CREW REPORTS INSTANCE HAPPENED THREE TIMES THROUGHOUT FLIGHT. CHECKED NOSE GEAR DRAG STRUT PROXIMITY SENSOR GAP. CLEANED & CHECKED CONNECTOR PINS AT NLG DRAG STRUT PROXIMITY SENSOR AT BULKHEAD. CYCLED GEAR, NO FAULTS NOTED. TEST FLT UNSATISFACTORY. CYCLED GEAR, ALL RETRACTED BUT THE NOSE GEAR DOOR LIGHT REMAINED ON. CYCLED GEAR DOWN DOOR AMBER LIGHT WENT OUT UNSAFE RED LIGHT ILLUMINATED FOR NOSE GEAR & CREW PERFORMED ALTERNATE EXTENSION. ADJUSTED NOSE GEAR DOOR ACTUATOR ROD END AND DOOR PROXIMITY SENSOR. REMOVED & REPLACED 3261-S10, DRAG STAY SENSOR & HARNESS. TEST FLT SATISFACTORY.

Part: AHRS — FAILED (COCKPIT) · airframe 27,761 hrs · 32,521 cycles

CAPTIANS ADI STICKS IN PITCH MODE STABLE IN LEVEL FLIGHT AND ROLL MODE. REMOVED AND REPLACED NR 1 AHRS COMPUTER AND NR 1 ADI. EVALUATION FLIGHT SATISFACTORY. HSI AND ADI FLAGGED, POWER DOWN AND UP OPS CHECK OK, REMOVED AND REPLACED NR 1 AHRS.

Part: COMPUTER — FAULTED (AHRS NR 1) · airframe 27,752 hrs · 32,508 cycles

CAPTS ADI LOCKED 10 DEG NOSE UP AFTER T/O, CYCLING FAIL FLAG INDICATION ON ADI. NORMAL WHEN LEVELING OFF BUT ADI JERKS DURING PITCH CHANGES. CHECKED WIRING IN ROLL PITCH SYNCHRO SYS & ATTITUDE INVALID SYS FROM NR 1 AHRS TO NR 1 ADI. INSP CONNECTOR & WIRING 3427-P1-1 & 3420-TB5. R&R AFCS INTERFACE BOX, PERFORMED GRD MX TEST ON AHRS COMPUTER NR 1 & NR 2, OPS CK GOOD. STANDBY ADI VARIES 6 TO 8 DEG. R&R STANDBY ADI, OPS CK GOOD. CAPTS ADI STICKS IN PITCH MODE, STABLE IN LVL FLT & TURNS, INST 3 NEW WIRES FROM NR 1 AHRS COMPUTER PINS 8, 9 & 10 AT 3420-P1 TO NR 1 ADI PINS N, U, T CONNECTOR 3427-P3-1-1 NR 1 PITCH SYNCHRO LINES. TEST FLT UNSATISFACTORY. R&R NR 1 AHRS COMPUTER & NR 1 ADI. TEST FLT SATISFACTORY.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 27,745 hrs · 32,501 cycles

NOSE GEAR WOULD NOT LOCK IN UP POSITION. REMOVED AND REPLACED DRAG STRUT ACTUATOR ON NLG IAW 32-20-11. REMOVED AND REPLACED RELAY FOR UP LOCK ACTUATOR IAW 32-30-01.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 24,066 hrs · 27,804 cycles

PASSING THROUGH 7,700 FT, RT FORWARD EMERGENCY EXIT WARNING LT ILLUMINATED. LT EXTINGUISHED AFTER DUMPING PRESSURE PER EMERGENCY CHECK LIST. ADJUSTED DOOR PROXIMITY SENOR RAN A/C PRESSURIZED TO MAX DIFFERENTIAL. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: ENGINE — SURGES (NR 2) · airframe 21,919 hrs · 25,190 cycles

AFTER AUTOFEATHER WAS SELECTED IT DID NOT INITIALLY ARM DURING TAKEOFF ROLL. WHEN IT DID ARM, IT CAUSED NR 2 ENGINE TO SURGE UNCOMMANDED. GROUND RAN AIRCRAFT AND PERFORMED AUTOFEATHER AND STATIC TEST WITH NO DEFECTS NOTED. PERFORMED POWER RUN AND CONFIRMED AUTO FEATHER ARMING AT APPROXIMATELY 70 PERCENT TORQUE NUMEROUS TIMES WITH NO SURGING NOTED.

Part: PSEU — DEFECTIVE (MLG) · airframe 21,360 hrs · 24,557 cycles

ALL THREE AMBER LIGHTS ILLUMINATED THREE TIMES IN FLIGHT. REPLACED PSEU.

Part: BEARING RACE — BROKEN (NR 2 PROPELLER) · airframe 19,362 hrs · 21,942 cycles

NOISE COMING FROM NR 2 PROPELLER WHEN ROTATING. REPLACED NR 2 PROPELLER ASSEMBLY. DISASSEMBLY SHOWED DAMAGE TO THE NR 2 BLADE AND ITS SPLIT RING BEARING RACE. APPROXIMATELY ONE INCH OF MATERIAL HAS CRACKED/BROKEN AWAY FROM THE END OF ONE BEARING SPLIT RING HALF. FIVE BLADE BEARINGS WERE LOOSE INSIDE THE PROP HUB.

Part: SELECTOR VALVE — INOPERATIVE · airframe 15,951 hrs · 17,396 cycles

AFTER TAKE-OFF THE LANDING GEAR WOULD NOT RETRACT.

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 15,426 hrs · 16,656 cycles

AT 9000 FT, CREW REPORTED A LOUD EXPLOSION AND SIMULTANEOUSLY NR 1 DC GENERATOR DROPPED OFF LINE. NO VISIBLE LIGHTNING IN AREA AND LIGHT PRECIP ON RADAR. THE F/A REPORTED SEEING A BRIGHT FLASH AND LOUD BOOM IN THE ROW 2 AREA OF THE CABIN. CREW COMPLETED IN-FLIGHT LIGHTNING CHECK AND RETURNED TO CLT.