N335EN

Part: BRUSH BLOCK — DAMAGED (DEICE) · airframe 51,584 hrs · 57,807 cycles

PDIS 335 33-51 1362691 07DEC17 SBY CLOSE FA REPORTED EMERGENCY LIGHTS FLICKERING WHEN PROP HE AT L/H "B" PHASE WAS CYCLING 29311 00 EK FACT 08DEC17 04:55 SBY R&R BOTH ENG BRUSH BLOCKS DURING B1 CK. OPS CK GOOD

Part: UNKNOWN — ODOR (COCKPIT) · airframe 51,313 hrs · 57,459 cycles

BURNING ODOR COMING FROM BETWEEN CAPTAIN`S SEAT AND WARDROBE. INSPECTED AREA FOR HIDDEN DEFECTS. NO DEFECTS NOTED. GROUND RAN THE ACFT. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,307 hrs · 57,449 cycles

F/A REPORTED AN ELECTRICAL BURNING ODOR COMING FROM THE WARDROBE. INSPECTED THE WARDROBE AND FLIGHT ATTENDANT LIGHT PANEL SURROUNDING. NO SIGNS OF BURNING, ARCHING OR SMOKE. GROUND RAN THE AIRCRAFT NO DEFECTS NOTED. OK FOR SERVICE.

Part: HOSE — RUPTURED (NR 2 ENG OIL) · airframe 51,291 hrs · 38,827 cycles

IN FLIGHT, NR 2 ENGINE OIL PSI DROPPED TO ZERO FOLLOWED BY A NR 2 ENGINE FIRE INDICATION. PERFORMED ENGINE SHUTDOWN AND USED BOTH BOTTLES, FIRE INDICATION EXTINGUISHED AND PERFORMED A SINGLE ENGINE LANDING. REMOVED AND REPLACE THE NR 2 ENGINE IAW WC71-02-02. CAUSE OF FIRE DETERMINED TO BE A RUPTURED FLEXIBLE OIL LINE, RT SIDE. THE NR 2 ENGINE WAS REPLACED ON SITE.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 51,085 hrs · 57,143 cycles

WEATHER RADAR WILL NOT PAINT KNOWN WEATHER. R & R THE WEATHER RADAR R/T IAW AMM 34-41-01.GROUND TESTED GOOD, OK FOR SERVICE.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 50,754 hrs · 56,706 cycles

AFTER TAKE OFF, DURING CLIMB THEOUGH 400 FT. BOTH BLEEDS AND LEFT PACK TURNED ON WHEN SMOKE AND A FOUL ODOR FILLED THE FLIGHT DECK. BLEEDS AND PACK TURNED OFF, SMOKE AND ODOR SUBSIDED. GROUND RAN THE ACFT WITH BLEEDS AND PACK ON FOR 10 MINUTES. NO SMOKE OR ODOR NOTED. FOUND HYDRAULIC LEAK UNDER RIGHT FWD SIDE OF COCKPIT FLOOR.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 50,662 hrs · 56,578 cycles

REJECTED TAKE OFF DUE TO AUTOFEATHER FAILURE TO ARM. CYCLED POWER LEVERS AND PDPU. PERFORMED AUTOFEATHER TEST IAW RUN UP MANUAL SYSTEM. OPS CHECKED GOOD, NO DEFECTS NOTED. OK FOR SERVICE.

Part: HOLDER — ARCED (CABIN LIGHTS) · airframe 50,584 hrs · 56,472 cycles

WHEN CABIN OVERHEAD LIGHTS ARE ON, AN ELECTRICAL ODOR IS NOTICED IN MID CABIN. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT AT 3A ARCING. INSPECTED AREA NO FURTHER DAMAGE NOTED. DEACTIVATED OVERHEAD LIGHTS. PULLED AND COLLARED CIRCUIT BREAKERS S1 - S2 AND R2 ON RIGHT MAIN. R & R THE LAMP HOLDER END. R & R THE BALLAST. ALL BREAKERS RESET. OVERHEAD LIGHTS OPS CHECKED WITH NO BURNING ODOR.

Part: IGNITER — FAILED (NR 1 ENGINE) · airframe 50,285 hrs · 56,060 cycles

NR 1 ENGINE WILL NOT LIGHT OFF. REMOVED AND REPLACED THE NR 1 ENGINE IGNITERS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,092 hrs · 55,818 cycles

FIRST RED EMERGENCY LIGHT INOPERATIVE AT ROW 1. R & R BULB.

Part: LENS — DETACHED (CABIN LIGHT) · airframe 50,059 hrs · 55,782 cycles

RIGHT SIDEWALL LIGHT LENS FELL DOWN AFTER TAKE OFF AT ROWS 4-7. REMOVED AND REPLACED SIDEWALL LIGHT LENS AS REQUIRED. OKAY FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,004 hrs · 55,714 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE 4TH AND 20TH FROM FRONT. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — UNKNOWN (DISPLAY) · airframe 49,805 hrs · 55,464 cycles

BOTH FO'S EFIS DISPLAYS ARE BLANK. FOUND CIRCUIT BREAKERS F6 AND G6. RESET THE CIRCUIT BREAKERS AS REQUIRED. EFIS SYSTEM OPS NORMAL OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,579 hrs · 55,108 cycles

EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,487 hrs · 55,068 cycles

EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,433 hrs · 55,005 cycles

LEFT FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT PS1. OPS CHECKED GOOD.

Part: EADI — MALFUNCTIONED (COCKPIT) · airframe 49,347 hrs · 54,887 cycles

F/O EADI WENT BLANK AND CB 6F WAS TRIPPED. RESET CB 6F AND C/W OPS CK OF EHSI. OK FOR SERVICE.

Part: VANE — MALFUNCTIONED (NR 2 AOA) · airframe 49,268 hrs · 54,782 cycles

NR 2 STALL SYS FAIL AND STICK PUSHER FAIL C/L DURING TAXI. RE-SET NR 2 AOA VANE. C/L EXTINGUISHED. OPS CHECK GOOD. OK FOR SERVICE.

Part: CIRCUIT BREAKER — FAILED (BOOST PUMP) · airframe 48,807 hrs · 54,180 cycles

NR 1 AUXILIARY PUMP APPEARED NOT TO WORK. DISCONNECTED MAIN AND AUXILIARY BATTERY CONNECTORS. SHORT SIGNED 281933. FOUND CIRCUIT BREAKER NR 1 FUEL AUXILIARY PUMP BAD. RNR C/B 2821-CB1, NR 1 FUEL AUXILIARY PUMP, AUXILIARY PUMP, OPS CHECK GOOD RECONNECTED MAIN AND AUXILIARY BATTERY CONNECTORS, PN 335-29-11 1305913, CIRCUIT BREAKER, PN MS3320-5, NR 1 AUXILIARY PUMP APPEARED NOT TO WORK.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 48,807 hrs · 54,179 cycles

LAV SMOKE DETECTOR WILL NOT TEST. R & R LAV SMOKE DETECTOR USING RETAINED HARDWARE, OPS CK GOOD, PN PU90-461.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 48,807 hrs · 54,179 cycles

CENTER FLOOR LIGHT WIRE BROKEN ON EMERGENCY LIGHTS. SPLICED NEW WIRE, OPS GOOD.

Part: DIODE — BROKEN (EMERGENCY LIGHTS) · airframe 48,807 hrs · 54,179 cycles

DIODE BROKEN CENTER FLOOR ON EMERGENCY LIGHT. R & R DIODE.

Part: PRESSURE SWITCH — INOPERATIVE · airframe 49 hrs · 54,099 cycles

DURING FLIGHT, NR 1 TORQUE INDICATIONS FLUCTUATING PLUS, MINUS 5 PCT WITH NR 1 BLEED HOT CT LIGHT ILLUMINATION. SELECTED NR 1 BLEED OFF AND NR 2 TORQUE INDICATOR FLUCTUATING, 5 PCT WITH NR 2 BLEED HOT CT LIGHT ILLUMINATED, SEL NR 2 BLEED OFF. TORQUE INDICATOR NORMAL AND CT LIGHTS EXTINGUISHED. R & R BOTH AIR MOD BLEED AIR PSI SWITCHES, GROUND RAN ACFT, BLEEDS OPS CHECK GOOD IN AIR AND GROUND MOD. NO BLEED HOT LIGHTS OR TORQUE FLUCTUATIONS NOTED OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,744 hrs · 54,099 cycles

DURING CRUISE, A STRONG OIL ODOR IN FLT DECK. DISSIPATED WITH BLEEDS SELECTED OFF. NO ODOR IN CABIN NOTED. REF SEQ 1 SAME LP. PERFORMED OPS CHECK OF BLEEDS WITH FLIGHT DECK PACK, NO OIL ODOR NOTED. PACK OPS NORMAL, OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIOGHT) · airframe 48,726 hrs · 54,078 cycles

FORWARD F/A EMERGENCY LIGHT ROCKER SWITCH BULB IS INOPERATIVE IN NORMAL POSITION. R & R BULB IN F/A EMERGENCY LIGHT ROCKER SWITCH. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,210 hrs · 53,412 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 4DF AND 11DF. PULLED EMERGENCY ESCAPE FLOOR PATH LIGHT COVER. R & R BULBS. OPS CHECKED GOOD. REINSTALLED COVER.

Part: SMOKE DETECTOR — FAILED (AFT CARGO BAY) · airframe 47,394 hrs · 52,302 cycles

AFT CARGO SMOKE DETECTOR IS HOT AND EMITS AN ODOR. R & R AFT CARGO SMOKE DETECTOR. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 46,913 hrs · 51,684 cycles

LF 26AC BUSS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF, PRIMARY, SECONDARY AND AUX INVERTERS LOADS NORMAL. NO LOSS OF SERVICE FROM LF 26AC BUSS. CAUTION LIGHT EXTINGUISHED AFTER SEVERAL MINUTES. R & R CAUTION LIGHT PANEL IAW 33-12-00. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,405 hrs · 51,001 cycles

OVERHEAD EMERGENCY EXIT LIGHTED SIGN IS INOPERATIVE AT ROW 11. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,335 hrs · 50,914 cycles

LEFT EMERGENCY DOOR LIGHT IS INOPERATIVE AT ROW 11. R & R BULB AT EMERGENCY DOOR. OPS CHECKED GOOD.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,335 hrs · 50,914 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 12. R & R THE LIGHT MODULE AT ROW 12 EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,951 hrs · 50,413 cycles

F/A REPORTS STRONG ODOR CAUSING COUGHING, WHILE TAXIING, AFTER LANDING. FOUND HYD LEAK UNDER SEAT 3DF. REPAIRED USING RING-LOCK IAW 20-55-55 AND SEAT WC 25-00-03R. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,897 hrs · 50,343 cycles

THREE EMERGENCY LIGHTS ARE BURNED OUT. R & R THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,697 hrs · 48,783 cycles

FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (BUTTON) · airframe 44,315 hrs · 48,319 cycles

NORMAL GREEN LIGHT FOR EMERGENCY LIGHT PUSH BUTTON IS INOPERATIVE. R & R BULB IN PUSH BUTTON SWITCH. OPS CHECKED GOOD.

Part: UNKNOWN — HAZE (CABIN) · airframe 44,299 hrs · 48,297 cycles

WITH APU BLEEDS SELECTED ON, CABIN FILLED WITH HAZE. CREW GROUND RAN ENGINES WITH BLEEDS SELECTED ON. NO HAZE OR ODOR NOTED. RAN APU WITH BLEEDS ON. NO ODOR OR HAZE NOTED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,053 hrs · 47,981 cycles

EMERGENCY LIGHT ON FORWARD CABIN ENTRANCE BULKHEAD IS INOPERATIVE. REMOVED LENS, R & R BULB, AT SAID LOCATION. REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 44,053 hrs · 47,981 cycles

RIGHT FORWARD FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. REMOVED LENS, R & R BULB, AT SAID LOCATION, REINSTALLED LENS. OPS CHECKED GOOD.

Part: SEAL — CONTAMINATED (EMERGENCY EXIT) · airframe 43,660 hrs · 47,465 cycles

SMOKE ENTERING CABIN FROM FORWARD EMERGENCY EXIT DOOR. REMOVED FORWARD EMERGENCY EXIT DOOR AND FOUND DEICE FLUID AROUND BOTTOM SEAL. CLEANED AREA AND FOUND THE SMOKE TO BE STEAM FROM THE FLUID EVAPORATING. INSTALLED EXIT DOOR AS REQUIRED. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,539 hrs · 47,313 cycles

F/A AND PASSENGER REPORTED BURNING ODOR IN CABIN, THEN DISAPPATED. INSPECTED ACFT OVERHEAD LIGHTS AND GROUND RAN ACFT WITH BLEEDS ON. NO ODOR NOTED AT THIS TIME. OK FOR SERVICE.

Part: MODULE — BROKEN (EMERGENCY LIGHT) · airframe 43,382 hrs · 47,120 cycles

EMERGENCY LIGHT HAS TWO BROKEN MODULES. R & R LIGHT MODULES IAW AMM 20-45-07. OPS CHECKED GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,231 hrs · 46,926 cycles

LAV DOUBLER CORRODED ON LOWER EDGE, AFT SIDE. CUT OUT CORROSION IAW RD8-53-2103. COMPLIED WITH EDDY CURRENT INSPECTION. NO DEFECTS NOTED. REPAIRED LAV DOUBLER AND INSTALLED NEW LAV DOOR IAW E08-53-13-0473.

Part: PROPELLER — MALFUNCTIONED · airframe 42,968 hrs · 46,585 cycles

UNABLE TO GET NR 1 PROP RPM BELOW 927. ADJUSTED NR 1 PCU SPEED TRIM SCREW IAW MM 61-22-00. PROP SPEED AT 911 RPM. OK FOR SERVICE.

Part: FAN — INOPERATIVE · airframe 42,693 hrs · 46,224 cycles

CIRCUIT BREAKER N5 TRIPPED AND WILL NOT RESET. ACFT OVER PRESSURIZED AND UNABLE TO CONTROL EITHER PACK. FOUND FLIGHT DECK TEMP SENSOR FAN BAD. R & R TEMP SENSOR FAN. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (COCKPIT TEMP) · airframe 42,687 hrs · 46,218 cycles

SMOKE IN FLIGHT DECK ACCOMPANIED BY CIRCUIT BREAKER OPENING. REPLACED FLIGHT DECK TEMP SENSOR.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,665 hrs · 46,193 cycles

EMERGENCY SIDEWALL LIGHT IS INOPERATIVE AT ROW 2DF. R & R BULBS, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,665 hrs · 46,193 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 1. R & R BULB, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 42,188 hrs · 45,575 cycles

EMERGENCY FLOOR LIGHT IS OUT AT ROW 13. R & R BURNED OUT BULB FOR EMEGENCY FLOOR LIGHT. OPS CHECKED GOOD.

Part: BOOT — DAMAGED (DE ICE SYS) · airframe 42,144 hrs · 45,519 cycles

IN ALL MODES, RT MOST INBD DEICE BOOT WILL NOT INFLATE AND HAS NO INDICATION. PATCHED L/E AS NEEDED IAW AMM 30-10-48. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CONTROL BOX — FAILED (EMERGENCY LIGHTS) · airframe 42,104 hrs · 45,466 cycles

EMERGENCY LIGHTS ARE FLICKERING IN FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD IAW DASH 8 RUN UP MANUAL.

Part: WARNING LIGHT — FALSE ACTIVATION (STALL WARNING) · airframe 41,945 hrs · 45,256 cycles

NR 1 AND NR 2 STALL SYS FAIL AND PUSHER FAIL CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL. CYCLED CIRCUIT BREAKERS SWSP COMP 1 AND 2 OPS NORMAL AT THIS TIME. SYS NR 1 FAULTS: VANE 1-B, VANE 1-F, ASCB 1, ICE 1 OFF. SYS NR 2 FAULTS VANE 2, VANE 2-B, VANE 2-E, ASCB 2, ICE 2 OFF. ALL FAULTS CLEARED. COULD NOT DUPLICATE FAULT. SWSP SYS OPS CKS GOOD IAW WC 27-30-08Q. CLEAR MEL.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,579 hrs · 44,771 cycles

EMERGENCY FLOOR LIGHT IS INOP AT ROW 3DF. R & R BULB AT EMERGENCY FLOOR LIGHT. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 41,551 hrs · 44,730 cycles

TWO FORWARD MOST FLOOR PATH EMERGENCY LIGHTS ARE INOPERATIVE. R & R BATTERIES IAW WC 33-50-05R. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 41,511 hrs · 44,686 cycles

SMOKE ENTERED CABIN UPON SELECTING APU BLEEDS ON. BOTH ACM'S OPERATED AT TIME OF EVENT. RAN ACFT WITHOUT APU BLEEDS AND HAD NO SMOKE. RAN APU, NO SMOKE. RAN AFT ACM (CABIN). NO SMOKE. RAN FORWARD ACM (FLIGHT COMPARTMENT) NO SMOKE. RAN BOTH ACMS, NO SMOKE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,469 hrs · 44,632 cycles

FLOOR EMERGENCY LIGHT BETWEEN ROW 11AC AND 11DF ARE INOPERATIVE. R & R LIGHT. OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (NR 1) · airframe 41,475 hrs · 44,638 cycles

WHEN ATTEMPTING START ON NR 1 ENGINE. SMOKE WAS OBSERVED COMING FROM INBD COWLING VENTS OF NR 1 NACELLE. R & R NR 1 START GENERATOR IAW WC 24-30-02R. OPS AND LEAKED CHECKED GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 41,020 hrs · 44,034 cycles

THIRD AFT EMERGENCY FLOOR TRACK LIGHT, THIRD FROM THE REAR IS INOPERATIVE. R & R EMERGENCY FLOOR LIGHT. REINSTALLED TRACK, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 40,793 hrs · 43,725 cycles

LAST EMERGENCY LIGHT IN CELING IS INOPERATIVE AT ROW 12. R & R BULB FOR CEILING EMERGENCY LIGHT AT ROW 12. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,403 hrs · 43,208 cycles

ROW 1 FLOOR EMERGENCY PATH LIGHT HAS 1 RED LAMP INOPERATIVE. R & R LIGHT BULB. OPS CHECKED GOOD. REINSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,199 hrs · 42,943 cycles

AFT RT SEAT LEVEL EMERGENCY LIGHT HAS BULB OUT. R & R BULB AS REQUIRED. OPS CHECKED GOOD.

Part: LIGHT — FAILED (CABIN) · airframe 40,199 hrs · 42,943 cycles

AFT MOST EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT MODULE AS REQUIRED. OPS CHECKED GOOD.

Part: BRUSH BLOCK — BURNED (PROPELLER) · airframe 40,057 hrs · 42,775 cycles

LEFT PROPELLER "B" PHASE INOPERATIVE WITH NO LOADS. INSPECTED AND FOUND NR 1 BRUSH BLOCK BURNED. R & R NR 1 BRUSH BLOCK IAW MM 61-10-11. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 40,049 hrs · 42,767 cycles

ROW 11DF LOWER SIDWALL EMERGENCY EXIT HAS A BULB INOPERATIVE. R & R BULB FOR SIDEWALL EMERGENCY EXIT SIGN AT ROW 11DF AND SECURED LENS COVER.

Part: SWITCH — INOPERATIVE (NR 2 BETA SYSTEM) · airframe 39,985 hrs · 42,687 cycles

NR 2 BETA LOCKOUT FAILED AFTER TAKE OFF. RETURNED TO FIELD. R & R BETA LOCKOUT SWITCH 6141-S6, NO FIX. R & R PLA SWITCH 6141-S4. OPS CHECKED GOOD. PERFORMED BETA LOCKOUT TEST FUNCTION, CHECK IAW RUN MANUAL. OPS CHECK GOOD.

Part: MODULE — WRONG PART (EMERGENCY LIGHTS) · airframe 39,589 hrs · 42,187 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 12 IS SOLID RED. REMOVED SOLID RED AND INSTALLED NEW MODULE WITH ARROW POINTING FORWARD IAW MM 33-52-00.

Part: MODULE — FAILED (EMERGENCY LIGHTS) · airframe 39,460 hrs · 42,021 cycles

ROW 13 HAS 1 INOPERATIVE EMERGENCY FLOOR PATH LIGHT. R & R EMERGENCY FLOOR PATH MODULE BY SPLICING IN NEW MODULE AS REQUIRED.

Part: SEQUENCE VALVE — LEAKING (NR 2 MLG DOOR) · airframe 39,277 hrs · 41,795 cycles

IN FLIGHT, AFTER SELECTING GEAR UP, NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED, ALONG WITH RIGHT GEAR DOOR AMBER LIGHT REMAINING ILLUMINATED WITH NR 2 SYS FLUID LOSS. RETURN TO DEPARTURE IAW CHECK LIST. PERFORMED ALTERNATE GEAR EXTENSION. FOUND SOLENOID SEQUENCE VALVE IN NR 2 NACELLE LEAKING. R & R NR 2 MLG DOOR SOLENOID SEQUENCE VALVE IAW 32-10-51. OPS AND LEAKED CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 39,030 hrs · 41,492 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. COMPLIED WITH WORK CARD 31-50-03. (TAKEOFF WARNING SYS OPS CHECK) NO DEFECTS FOUND AT THIS TIME. CHECKS GOOD, CLEARED MEL.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 38,732 hrs · 41,102 cycles

ROW 9 FLOOR EMERGENCY LIGHT INOP. R & R BULB. OPS CHECKED GOOD.

Part: STRIP — LOOSE (SERVICE DOOR) · airframe 38,703 hrs · 41,060 cycles

BANGING NOISE COMING FROM REAR OF ACFT INFLIGHT. FOUND SERVICE DOOR LOWER RUBBER TRIM STRIP HANGING OUT SERVICE DOOR. REMOVED REMAINING TRIM, NO DAMAGE NOTED TO OUTSIDE OF ACFT.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 38,687 hrs · 41,041 cycles

TROUBLESHOOTING ROW 2 EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. SLAVED NEW POWER SUPPLYS AND BATTERIES TO POSITION PS1, PS2, PS3 AND PS4. NO FIX. SLAVED FLIGHT COMPARTMENT SWITCH AND F/A SWITCH. NO FIX. R & R PS5 POWER SUPPLY AND SECURED WITH RETAINING HARDWARE. OPS CHECKED GOOD.

Part: MODULE — FAILED (EMERGENCY LIGHTS) · airframe 38,687 hrs · 41,041 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOP AT ROW 2 AND 12. R & R FLOOR PATH LIGHT MODULE AT ROW 12.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 38,668 hrs · 41,015 cycles

RED FLOOR EMERGENCY LIGHTS NR3 AND NR4 INOP. R & R EMERGENCY LIGHT BATTERY. ALL EMERGENCY LIGHTS OPS CHECKED GOOD FOR SERVICE IAW DASH 8300 MM 33-51-05.

Part: MODULE — FAILED (EMERGENDY LIGHTS) · airframe 37,892 hrs · 40,046 cycles

AT ROW 11, 1 EMERGENCY PATH LIGHT IS NOT WORKING. R & R LIGHT MODULE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 37,724 hrs · 39,840 cycles

EMERGENCY FLOOR PATH LIGHT CONFIGURATION IS INCORRECT. AFTER FURTHER RESEARCH, THE EMERGENCY FLOOR PATH CONFIGURATION IS CORRECT IAW FCD8-33-20-0133 AND MM 33-51-05.

Part: UNKNOWN — SMOKE (CABIN) · airframe 37,475 hrs · 39,520 cycles

HAZY SMOKE IN CABIN WITH APU BLEED ON, STARTED TO DISSIPATE WITH BLEED SELECTED OFF. INSPECTED APU COMPARTMENT FOR EVIDENCE OF FIRE OR SMOKE DAMAGE. NONE FOUND. RAN APU WITH BLEEDS SELECTED ON FOR APPROX 10 MINUTES. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,266 hrs · 45,764 cycles

NR2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED WITH JUST BELOW E QUARTS ON QTY INDICATOR. INSPECTED AND FOUND HYD LEAK OF NOSE GEAR DOWN BLUE LINE, R & R LINE AS REQUIRED, SERVICED NR2 HYDR SYS UP TO FULL, GROUND RAN NR2 ENGINE WITH BOTH STANDBY PUMPS ON, LEAKED CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 35,790 hrs · 37,382 cycles

MOST FWD CEILING EMERGENCY LIGHT FADES OUT AFTER A FEW SECONDS. R & R EMERGENCY BATTERY IN COAT CLOSET IAW MM 33-51-05.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 35,790 hrs · 37,382 cycles

FWD EMERGENCY EGRESS LIGHTS DIM OUT AFTER 10 SECONDS. R & R EMERGENCY BATTERY IN COAT CLOSET, IAW 33-52-05

Part: PSEU — DEFECTIVE (NLG STEERING) · airframe 35,260 hrs · 36,736 cycles

ON APPROACH, GEAR SELECTED DOWN 3 RED UNSAFE AND GEAR HANDLE LIGHT ILLUMINATED. AFTER ALTERNATE EXTENSION 3 GREEN AFTER LANDING NOSE WHEEL STEERING CAUTION LIGHT ILLUMINATED AND GEAR DOORS REMAINED OPEN. REMOVED AND REPLACED PSEU.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,694 hrs · 36,025 cycles

UPON INSPECTION IN SBY A WHITE ESCAPE PATH LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED WHITE LAMP MODULE AND THE OPERATIONAL CHECK WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 34,262 hrs · 35,478 cycles

UPON INSPECTION IN SBY, IT WAS FOUND THAT AICRAFT 335EN HAD AN EMERGENCY FLOOR PATH LIGHT INOPERATIVE. THE FLOOR PATH LIGHT BULB WAS REMOVED AND REPLACED. THE OPERATION CHECK WAS GOOD THAT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 34,249 hrs · 35,462 cycles

UPON INSPECTION IT WAS DISCOVERED THAT AN EMERGENCY LIGHT WAS INOPERATIVE. THE LIGHT BULB WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD.

Part: SERVO — DEFECTIVE (ELEVATOR TRIM) · airframe 34,151 hrs · 35,332 cycles

ELEVATOR TRIM VERY STIFF TO MOVE AND BINDING, UNABLE TO MOVE IT WITH STANDBY SWITCH. REMOVED AND REPLACED ELEVATOR TRIM SERVO.

Part: WIRE — BROKEN (CABIN) · airframe 34,125 hrs · 35,298 cycles

ONE RED FLOOR LIGHT INOP. INSPECTED WIRE, FOUND TO BE BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT MARKER.

Part: BATTERY — OVERHEATED (NOSE BAY) · airframe 33,969 hrs · 33,969 cycles

AUXILIARY BATTERY TEMPERATURE IN THE YELLOW. REMOVED AND REPLACED FORWARD AND AFT MAIN BATTERIES IN ACCORDANCE WITH WORK CARD 24-30-12R, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,659 hrs · 34,716 cycles

UPON A LINE CHECK INSPECTION AN EMERGENCY LIGHT AT ROW 5 WAS FOUND INOPERATIVE. REMOVED AND REPLACED LIGHT BULB, OPERATIONAL CHECK GOOD.

Part: LIGHT — DETERIORATED (CABIN) · airframe 33,659 hrs · 34,716 cycles

UPON LINE INSPECTION AT SBY A RED EMERGENCY AISLE LIGHT AT ROW 2 WAS FOUND DETERIORATED. THE EMERGENCY LIGHT WAS REMOVED AND REPLACED, OPERATIONAL CHECK WAS GOOD.

Part: FRAME — CORRODED (BS 593)

CORROSION FOUND ON FRAME STA X593.5 BETWEEN STR 30 AND 31 RT SIDE. REPAIRED IAW SRM 51-40-00 AND DRAWING 85330908. (S)

Part: SEAT TRACK — CORRODED (BS 129-197)

CORROSION FOUND ON RT SEAT TRACK BETWEEN STA 129.75 AND 197.50. SEAT TRACK REPLACED FROM STA 109.00 TO 187.00 IAW RD8-53-2797. (S)

Part: FRAME — CORRODED (FUSELAGE)

CORROSION SURFACE FOUND ON FRAMES STA 434.5 TO 445.5 RT STRINGER 31. SURFACE CORROSION REMOVED IAW EO8-53-08-3218 LPI ACCOMPLISHED.

Part: FITTING — CORRODED (FUSELAGE)

CORROSION FOUND AT STR 31 RT AT FRAME 424.12. FITTING REPLACED WITH NEW PART.

Part: BRACKET — CORRODED (PAX DOOR)

CORROSION PAX DOOR BOTTOM BRACKET ZED SUPPORT FWD AND AFT FOUND CORRODED. REPLACED PAX DOOR BOTTOM BRACKET.

Part: BRACKET — CORRODED (PAX DOOR)

CORROSION PAX DOOR BOTTOM BRACKET ZED SUPPORT FWD AND AFT FOUND CORRODED. REPLACED PAX DOOR BOTTOM BRACKET. (S)

Part: SEAT TRACK — CORRODED (BS 593-626)

CORROSION LIGHT SURFACE. SPOTS FOUND ON I/B SEAT RAILS BETWEEN FS 593 AND 626. HFEC DONE - NO CRACKS. SEAT RAIL REPAIRED BY SPLICE RD8-53-3886 AND FSR 07-3003.

Part: STRUCTURE — CORRODED (PAX DOOR)

CORROSION PAX DOOR GOOSENECK FOUND CORRODED FWD AND AFT. REPLACED PAX DOOR GOOSENECK. (S)

Part: ANGLE — CORRODED (FUSELAGE)

CORROSION FOUND ON THE RT SIDE OF LAV, BOTTOM ANGLE. REPLACED ANGLE. (S)

Part: ANGLE — CORRODED (LAVATORY)

CORROSION FOUND ON THE RT SIDE OF LAV, BOTTOM ANGLE. REPLACED ANGLE.

Part: GOOSENECK ASSY — CORRODED (PAX DOOR)

CORROSION PAX DOOR GOOSENECK FOUND CORRODED FWD AND AFT. REPLACED PAX DOOR GOOSENECK.

Part: FITTING — CORRODED (BS 424 S31R)

CORROSION FOUND AT STR 31 RT AT FRAME 424.12. FITTING REPLACED WITH NEW PART. (S)

Part: FRAME — CORRODED (BS 434)

SURFACE CORROSION FOUND ON FRAME BS 434.50 RT STRINGER 31. SURFACE CORROSION REMOVED IAW EO8-53-08-3218 LPI ACCOMPLISHED. (S)

Part: DOOR — CORRODED (LAV SERVICE)

CORROSION FOUND ON LAVATORY SERVICE PANEL. REPLACED LAV SERVICE PANEL. (S)

Part: SEAT TRACK — CORRODED (BS 593-626)

CORROSION - LITE SURFACE, SPOTS FOUND ON I/B SET RAILS BETWEEN FS 593 AND 626. HFEC PERFORMED, NO CRACKS. SEAT RAIL REPAIRED BY SPLICE RD8-53-3886 AND FSR 07-3003. (S)

Part: PIN — DEFECTIVE (CONNECTOR) · airframe 31,937 hrs · 32,577 cycles

NUMBER 2 VOR FLASHES BACK AND FORTH BETWEEN VOR AND ILS WHEN A VOR FREQUENCY IS SELECTED. DUPLICATED FAULT ON GROUND BY MOVING WIRE BUNDLE APPROXIMATELY 6 INCHES BEHIND NR 2 SYMBOL GENERATOR. REPLACED PIN 53 OF 3428-P65-2-1B TO CORRECT FAULT. OPERATIONAL CHECK GOOD USING 402AP TEST SET.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 31,288 hrs · 31,802 cycles

NR 1 HYDRAULIC ISO CAUTION LIGHT ILLUMINATED, NR 1 HYDRAULIC QUANTITY DROPPED TO 0 AND NR 1 HYDRAULIC PRESSURE DROPPED TO 0 PSI WITH CORRESPONDING CAUTION LIGHTS. NR 1 ENGINE HYDRAULIC PUMP OPERATED APPROXIMATELY 14 MINUTES WITH NO PRESSURE. FOUND FLUID DRIPPING FROM RUDDER MANIFOLD AREA. FOUND HYDRAULIC LINE AT RUDDER PRESSURE REGULATOR LEAKING, INSTALLED TEMP FLEX LINE. DURING INSPECTION FOUND THE DELTA-P TRIPPED. REMOVED AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP, THE CASE DRAIN AND PRESSURE MANIFOLD FILTERS. OPERATIONAL AND LEAK CHECK GOOD.

Part: YOKE — BINDING (LANDING GEAR) · airframe 30,950 hrs · 31,398 cycles

ON APPROACH TO AIRFIELD, LANDING GEAR DOWN WAS SELECTED AND NR 1 GEAR DOOR AMBER LIGHT ALONG WITH RED GEAR UNSAFE LIGHT ILLUMINATED. UPON VERIFYING THE CONDITION INDICATED, THE CREW THEN DECLARED AN EMERGENCY AND PROCEEDED TO EXTEND THE LANDING GEAR USING THE ALTERNATE EXTENSION SYSTEM. MAINTENANCE FOUND THE UPPER LANDING GEAR YOKE ASSEMBLY WAS BINDING. YOKE SHIMS WERE REMOVED, RE-MEASURED AND ASSEMBLY WAS RE-SHIMMED TO PROPER SPECS. OPS CHECKS WERE GOOD IAW MM 32-10-13.

Part: SKIN PANEL — CORRODED (BS 445-467) · corrosion level 2 · airframe 29,195 hrs · 29,269 cycles

UPON REMOVAL OF THE NR 2 DME ANTENNA CORROSION WAS FOUND ON THE SKIN PANEL UNDER THE ANTENNA. CORROSION WAS LOCATED AT THE AIRCRAFT CENTER LINE BETWEEN X445 AND 467. REPAIRED PER ENGINEERING ORDER.

Part: WIRE — LOOSE (NR 1 GCU) · airframe 23,658 hrs · 22,341 cycles

AT 10,000 FT MASTER WARNING ILLUMINATED ASSOCIATED W/LOSS OF CABIN PRESS, DOOR WARNING LTS W/ AUX INVERT AND RUDDER FULL PRESS C/L AFTER CAPT'S G/S, SIDE PANEL AND FLIGHT INST WENT OUT, CAPTS 800 PANEL BLANK, A/P FAILED. NR 1 DC GEN C/L ILLUM SELF CORRECT. REMOVED AND REPLACED STARTER GEN AND GCU FOR NR 1 ENG OPS CHECK GOOD. THEN ON TAKEOFF ROLL AT V1 AUX INVERTER C/L ILLUMINATED ALONG WITH ALL EXTERIOR DOOR WARNING LTS CAPT FLT. INST LIGHTS WENT DARK ALONG WITH CAPT 800 PANEL AND RNAV. FOUND WIRE PULLING OUT OF PIN "LITTLE A" ON THE NR 1 DC GCU CONNECTOR. REPINED WIRE ,OPS CHECK GOOD.

Part: FUEL CONTROL — INOPERATIVE (NR 1 ENGINE) · airframe 22,572 hrs · 21,005 cycles

LOSS OF POWER ON NR 1 ENG IN CLIMB. ENG DID REMAIN RUNNING. A/C RETURNED TO FIELD & DECLARED EMERGENCY, DID NOT SHUTDOWN ENG UNTIL ON FIELD. A/C CLIMB THROUGH 7000 FT. ENG PARAM: TQ 0, WF 230, NH 71, NL 59, ITT 447, OIL PRESS GOOD, PROP RPM STABL & CONTROLLABLE W/ COND LEVER. ECU SELECTED TO MAN & BACK, NO EFFECT. MX LOOKING FOR DEFECTS & WILL RUN IF NONE FOUND. SELECTED BOOST PUMP ON, NO EFFECT. AFTER INSPECT, MX TRIED ENG START. RUNS, BUT UNRESPONSIVE TO POWER LEVER INPUTS WITH ECU ON OR OFF. R & R MFC. TRIM RUN COMPLETE. DUPLICATED ON GROUND RUN R & R NR 1 MFC. PERFORMED RIG CHECK PER WC 76-00-02Q AND TRIMMED PER -8 OPERATING MANUAL LEAK AND OPS CHECK GOOD.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 22,249 hrs · 20,602 cycles

AFTER TAKEOFF NR 2 HYD IOS C/L ILLUMINATED AND NR 2 HYD PRESSURE AND QTY DROPPED TO ZERO, FOLLOWED BY ILLUMINATION OF NR 2 ENG HYD PUMP, RUDDER PRESS, RUDDER FULL PRESS & OUTBD ROLL SPLR. C/L ILLUMINATED. LOST PRESSURE AT 0958 ENGINE SHUTDOWN AT 1040. INSTALLED TFL ON FWD SIDE OF NR 2 PRESSURE MANIFOLD SERVICED AND BLEED NR 2 HYD SYSTEM, GROUND RUN, LEAK CHECK.

Part: LANDING GEAR — FROZEN (NOSE) · airframe 21,971 hrs · 20,288 cycles

LOUD NOISE HEARD COMING FROM NOSE AREA DURING TAKEOFF AND CLIMBOUT. SUSPECT LARGE ACCUMULATION OF SNOW AND ICE ON NOSE GEAR AND DOORS. DEICED GEAR AND INSPECTED FOR DAMAGE AND SECURITY, NO DEFECTS NOTED. AIRCRAFT FOUND SATISFACTORY DURING EVALUATION FLIGHT.