N330EN

Part: AUTOFEATHER SYS — FAILED · airframe 54,420 hrs · 65,558 cycles

AUTOFEATHER FAILED TO ARM DURING TAKE OFF AT 80% AND 80 KNOTS. RESET THE AUTOFEATHER SYS AND FAILED TO ARM.

Part: AUTOFEATHER SYS — FAILED · airframe 54,404 hrs · 65,540 cycles

AUTOFEATHER FAILED TO ARM AT 86%, ABORTED T/O.

Part: BRAKE — LEAKING (NR 2) · airframe 54,195 hrs · 65,261 cycles

FLUID LEAK ON NR 1 MLG. NR 2 HYD QTY DROPPED WHILE AWAITING TAXI FOR DEPARTURE. REMOVED AND REPLACED THE NR 2 BRAKE ASSY IAW MM 32-42-11. LEAK CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 54,128 hrs · 65,169 cycles

ABORTED TAKEOFF AT 90 PERCENT TORQUE. AUTOFEATHER WOULD NOT ARM. GROUND RAN ACFT, SYSTEM ARMED WITH NR 1 ENGINE AT 74 PERCENT AND NR 2 ENGINE AT 70 PERCENT. OPS CHECKED GOOD IAW RUNUP MANUAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 54,089 hrs · 65,113 cycles

EMERGENCY LIGHTS INTERMITTEN DURINB FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. R & R THE EMERGENCY LIGHT BASE AT PS4. R & R PS 1 THRU 7 BATTERIES. OPS CHECKED GOOD IAW 33-51-05.

Part: CONTROLLER — FAILED (EMERGENCY LIGHTS) · airframe 54,078 hrs · 65,095 cycles

EMERGENCY LIGHTS ARE ILLUMINATED IN THE ARM POSITION. WOULD NOT EXTINGUISH. R & R THE EMERGENCY LIGHT CONTROLLER IAW W/C 33-50-05R. OPS CHECKED GOOD.

Part: TSCU — INOPERATIVE (AUTO FX) · airframe 53,973 hrs · 64,955 cycles

AUTO FX WOULD NOT ARM DURING TAKEOFF ROLL. R & R THE NR 2 TSCU, OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 53,676 hrs · 64,563 cycles

EMERGENCY LIGHT BELOW FWD FLIGHT ATTENDANT SEAT AT TOP OF AIR STAIRS HAS BURNED OUT BULB

Part: WARNING HORN — FALSE ACTIVATION · airframe 53,366 hrs · 64,148 cycles

TAKE OFF WARNING HORN SOUNED WHEN POWER LEVERS WERE ADVANCED. CYCLED FLAPS PERFOMED GROUND RUN. WARNING HORN DID NOT SOUND. OPS CHECK GOOD. OK FOR SERVICE

Part: LIGHT — SMOKE (CABIN) · airframe 53,270 hrs · 64,028 cycles

SMOKE REPORTED FROM ABOVE BIN 3AC. CABIN OVERHEAD LIGHTING DEACTIVATED. SP 33.1 HAS BEEN COMPLIED WITH. EMERGENCY DECLARED. COMPLIED WITH SP 33.1, CIRCUIT BREAKERS PULLED AND COLLARED.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 52,756 hrs · 63,330 cycles

NR 2 STANDBY HYD PUMP HOT C/L ILLUMINATED IN FLT. PSI AT 0. REMOVED & REPLACED AUX HYDRAULIC PUMP IAW AMM 29-11-17 & CMM 29-11-22. OPS & LEAK CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (DE ICE BOOTS) · airframe 52,617 hrs · 63,143 cycles

THREE OTBD DEICE BOOTS FOR LEFT WING INFLATE INTERMITTENTLY IN SLOW, FAST AND NORMAL. REMOVED AND REPLACED OUTBOARD DISTRIBUTOR VALVE IAW MM 30-10-16. OK FOR SERVICE.

Part: WARNING HORN — FALSE ACTIVATION · airframe 52,408 hrs · 62,887 cycles

WHEN POWER LEVERS WERE ADVANCED TO TAKEOFF, WARNING HORN SOUNDED. DEPARTED RUNWAY AND PUSHED POWER LEVERS FORWARD. NO WARNING HORN SOUNDED. CYCLED FLAPS THROUGH COMPLETE RANGE. PUSHED POWER LEVERS FORWARD, TAKEOFF HORN DID NOT SOUND. OK FOR SERVICE.

Part: APU — FAILED · airframe 51,948 hrs · 62,288 cycles

APU FAILED. GENERATOR OVERHEAT CAUTION LIGHT ILLUMINATED. APU MAIN CIRCUIT BREAKER TRIPPED, AND CHECK FIRE DETECTION WARNING LIGHT ILLUMINATED. CREW DISCHARGED BOTTLE. MX PREFORMED HIDDEN DAMAGE INSPECTION AND FOUND NO OBVIOUS DAMAGE COLLARED CB Q8 APU MAIN.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,875 hrs · 62,190 cycles

LEFT FWD EMERGENCY EXIT EGRESS LIGHT INOPERATIVE. R & R THE BULB.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 51,255 hrs · 61,370 cycles

AFTER ENGINE SHUTDOWN AND APU RUNNING WITH EMERGENCY LIGHTS SWITCHED OFF, EMERGENCY LIGHTS STAYED ON. NO HISTORY, PD/PU SYS, OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 51,170 hrs · 61,269 cycles

WEATHER RADAR SPOKING, NO HISTORY R & R RADAR RT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,045 hrs · 61,102 cycles

EMERGENCY FLOOR RED LIGHT IS INOPERATIVE INFRONT OR SEAT ROW. R & R BULB ON RED LIGHT FOR EMERGENCY FLOOR LIGHTS. OPS CHECK GOOD AS REQUIRED P/N OFF AND ON.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,864 hrs · 60,861 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 9. REMOVED LENS, R & R EMERGENCY LIGHT CEILING LIGHT BULB. REINSTALLED LENS WITH RETAINING HARDWARE, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,517 hrs · 60,420 cycles

LEFT AFT EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (SPOILERS) · airframe 47,582 hrs · 54,431 cycles

AT TAKEOFF, POWER SPOILER, SWITCH/ LIGHT FLICKERED, THEN ILLUMINATED AND EXTINGUISHED WHEN POWER LEVERS WERE RETARDED. R & R LT WING TOP SPOILER JAM SWITCH 2762-S7 IAW MM 27-14-38. OPS CHECKED GOOD ON THE GROUND.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,290 hrs · 60,105 cycles

EMERGENCY SIDEWALL EXIT SIGN DIM AT 11AC...... REMOVED AND REPLACED BULBS FOR EMERGENCY EXIT SIGN AT 11AC. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,290 hrs · 60,105 cycles

EMERGENCY SIDEWALL EXIT SIGN DIM AT 11AC. R & R BULBS FOR EMERGENCY EXIT SIGN AT 11AC. OPS CHECKED GOOD.

Part: RELAY — FAILED (APU) · airframe 50,185 hrs · 59,971 cycles

DURING GROUND POWER. NOTICED SMOKE FROM APU COMPARTMENT. FIRE DETECTOR LIGHT ILLLUMINATED. MANUALLY DISCHARGED FIRE BOTTLE. RED DISK DID NOT DISCHARGE. R & R 2449-K62 RELAY IAW MM 24-31-09. PN ON AND OFF AJ-A4N-176. R & R START GENERATOR FOR APU IAW WC 24-30-02R. REACTIVATED SYSTEM, RAN APU, OPS CHECKED GOOD.

Part: INVERTER — ODOR (COCKPIT) · airframe 50,158 hrs · 59,941 cycles

SLIGHT FISHY ODOR IN FLIGHT DECK. SECONDARY INVERTER 117 VOLTS WITH .41 LOAD. INSPECTED, NO USUAL ODOR NOTED. MEL'D SECONDARY INVERTER DUE TO HIGHER THAN NORMAL VOLTS AND LOADS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,058 hrs · 59,814 cycles

1ST ROW, 3RD FROM FRONT EMERGENCY LIGHT IS INOPERATIVE. REMOVED COVER, R & R BULB. OPS CHECKED GOOD. REINSTALLED COVER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,010 hrs · 59,756 cycles

EMERGENCY ESCAPE PATH FLOOR LIGHT IS INOPERATIVE, SECOND RED LIGHT FROM FRONT AT ROW 7DF. R & R BULB AT ROW 7DF EMERGENCY ESCAPE PATH FLOOR LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,813 hrs · 59,480 cycles

4TH RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R 4TH RED FLOOR EMERGENCY LIGHT BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,780 hrs · 59,438 cycles

EMERGENCY LIGHT IS INOPERATIVE. R & R THE LIGHT. OPS CHECKED GOOD.

Part: TUBE — DAMAGED (CABIN PRESSURE) · airframe 49,648 hrs · 59,259 cycles

REGARDLESS OF POSITION OF DUMP VALVE, AIRCRAFT PRESSURIZED WHEN BLEED IS SELECTED ON. R & R DAMAGED PRESSURIZATION TUBE AT APU LINK UP ASSY IAW MM 20-06-01.

Part: STALL WARNING — MALFUNCTIONED · airframe 49,637 hrs · 59,241 cycles

NR 1 STALL SYS FAIL AND STICK PUSHER FAIL, CAUTION LIGHT ILLUMINATED. POWERED DOWN STALL SYSTEM. CHECKED VANE ALIGNMENT. POWERED UP SYSTEM. PERFORMED SYSTEM CHECK. ALL CHECKED OK AT THIS TIME. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,626 hrs · 59,227 cycles

EMERGENCY LIGHTS AT ROWS 1DF AND 4DF ARE INOPERATIVE. R & R THE BULBS, OPS CHECKED GOOD.

Part: STICK SHAKER — MALFUNCTIONED · airframe 49,226 hrs · 58,681 cycles

PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL FOR APPROXIMATELY 5 SECONDS. NR 1 AND 2 STALL SYSTEM CAUTION LIGHT ILLUMINATED INTERMITTENTLY. CREW POWERED DOWN ACFT FOR APPROXIMATELY 5 MINUTES SYS, OPS CHECKED, OPS AND SELF TEST NORMAL ON POWER UP. PERFORMED WC 27-30-08Q, STICK PUSHER AND SWAP COMPUTER TEST AND PRESSURE INDICATION CHECK. NO DEFECTS NOTED AT THIS TIME.

Part: SWITCH — DIRTY (EMERGENCY LIGHTS) · airframe 49,155 hrs · 58,583 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF. CLEANED AND INSPECTED F/A'S EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,842 hrs · 58,164 cycles

EMERGENCY SIDEWALL LIGHT ROW 2D-F, BULB INOPERATIVE. R & R THE BULB

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,610 hrs · 57,858 cycles

TWO FORWARD EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (LIGHT SWITCH) · airframe 56,027 hrs · 62,356 cycles

F/A EMERGENCY LIGHT SWITCH IS INOPERATIVE. R & R BULB FOR F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 48,361 hrs · 57,538 cycles

EMERGENCY EXIT SIGN AT AIR STAIR DOOR IS DIM. R & R THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,913 hrs · 56,949 cycles

UPPER EMERGENCY EXIT SIGN INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (ARM LIGHT) · airframe 47,877 hrs · 56,895 cycles

AUTO FEATHER ARM LIGHT INOPERATIVE. DOES NOT TEST. R & R BOTH BULBS IN AUTO FEATHER ARM LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,844 hrs · 56,853 cycles

EMERGENCY SIDEWALL LIGHT DIM AT ROW 11DF. R & R TWO BULBS FROM LOWER SIDEWALL LIGHT ASSY. OPS CHECKED GOOD.

Part: SYMBOL GENERATOR — FAILED (COCKPIT) · airframe 47,449 hrs · 56,323 cycles

CAPT'S SYMBOL GENERATOR FAILED IN FLIGHT. R & R CAPT'S SYMBOL GENERATOR. OPS CHECKED GOOD IAW MM 34-28-02.

Part: ELECTRICAL SYS — LOW · airframe 47,161 hrs · 55,957 cycles

AC VOLTS DROP TO 110, DURING BOTH PROPELLER DEICE CHECKS, GROUND RAN AC, PROPELLER HEAT OPS CHECKED GOOD IAW MM 30-61 00. R & R BOTH GCU`S AND RELAY 2421 FOR PRECAUTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,174 hrs · 55,973 cycles

AFT EMERGENCY OVERHEAD LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 46,869 hrs · 55,574 cycles

BROKEN CLEAR LENS ON EMERGENANCY FLOOR PATH LIGHTS ROW 12DF. REMOVED BROKEN CLEAR LENS PLACED NEW CLEAR LENS TO BASE MATERIAL ROW 12DF AND SECURED OPS CHECK GOOD.

Part: UPLOCK ACTUATOR — DAMAGED (MLG) · airframe 46,784 hrs · 55,470 cycles

DURING GEAR EXTENSION, NOSE AND RT MAIN UP WITH IN TRANSIT AND LT MAIN GEAR RED( UNSAFE) LIGHT ILLUMINATED. PERFORMED ALT. EXTENSION AND LANDED. GEAR PINS INSTALLED AT GATE. JACKED ACFT, SWUNG GEAR. VERIFIED LT GEAR WOULD NOT EXTEND AS COMMANDED. INSPECTED AND FOUND UPLOCK ACTUATOR HOOK GROOVED. R & R UPLOCK ACTUATOR IAW AMM 32-30-27. OPS CHECKED AND LEAKED CHECKED GOOD.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 46,211 hrs · 54,729 cycles

NOSE WHEEL STEERING CAUTION LIGHT CAME ON DURING TAXI OUT. R & R STEERING MANIFOLD ASSY IAW MM 32-50-16. OPS CHECKED AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: CAUTION PANEL — FALSE INDICATION · airframe 46,066 hrs · 54,545 cycles

MASTER CAUTION LIGHT ILLUMINATED WITH NO ATTENDING CAUTION LIGHTS. AFTER CANCELING, LIGHT RETURNS. R & R MASTER CAUTION PANEL. OPS CHECKED GOOD IAW MM 33-12-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,040 hrs · 54,512 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 3 AND 29. R & R BULBS AT FLOOR PATH EMERGENCY LIGHTS IN ROWS 3 AND 29. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 46,040 hrs · 54,512 cycles

FLOOR EMERGENCY LIGHT HAS BROKEN WIRE AT NR 29. R & R PATH LIGHT FLOOR EMERGENCY LIGHT MODULE. OPS CHECKED GOOD.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 45,867 hrs · 54,296 cycles

NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED DURING FLIGHT AT 9000 FT. ACCOMPANIED BY AN ENGINE SURGE AND ODOR IN REAR CABIN. FOUND RT CLAMP ON BLEED AIR NR 2 DUCT LOOSE ON TOP OF FUSELAGE. TIGHTENED CLAMP. R & R NR 2 OVER TEMP SWITCH. GROUND RAN ACFT. OPS CHECKED GOOD IAW 21-11-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,841 hrs · 54,264 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 1 AND ROW 11. R & R BULBS. OPS CHECKED GOOD.

Part: PLATE — CRACKED · airframe 45,834 hrs · 54,256 cycles

FWD INBD CORNER OF STRESS PANEL LADDER PLATE IS CRACKED AT PANEL 622AT. REMOVED DAMAGE AND REPLACED WITH NEW PART FABRICATED IAW RD 8-57-2287. COMPLIED WITH BOND TEST AND HFEC INSPECTION. NO OTHER CRACKS NOTED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,834 hrs · 54,256 cycles

FORWARD ANGLE FOUND CRACKED ON LT FRAME X63 BELOW COCKPIT WINDSHIELD LOWER FRAME. REPAIRED LT FRAME ANGLE IN COCKPIT LOWER FRAME IAW SRM 51-42-05 AND SRM 51-40-10.

Part: FRAME — CORRODED (THRESHOLD) · corrosion level 2 · airframe 45,834 hrs · 54,256 cycles

PAX DOOR THRESHOLD FRAME CORRODED. R & R THRESHOLD FRAME WITH NEW IAW SRM 51-42-05 AND DWG 85321241.

Part: PLATE — CRACKED · airframe 45,834 hrs · 54,256 cycles

STRESS PANEL LADDER PLATE IS CRACKED ON OTBD AFT CORNER OF PANEL 622AT. REMOVED DAMAGE IAW RD8-57-2375. COMPLIED WITH HFEC INSPECTION. NO FURTHER DAMAGE FOUND. REPAIRED DAMAGE IAW RD8-57-6133.

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 45,834 hrs · 54,256 cycles

LT INBD SIDE OF FIREWALL IS CRACKED. REPAIRED FIREWALL DAMAGE IAW SRM 51-42-05 AND DWG NR 85411312.

Part: SEAT TRACK — CORRODED (BS 570) · corrosion level 2 · airframe 45,834 hrs · 54,256 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT BS 570. FABRACATED SECTION OF SEAT TRACK IAW RD 8-53-3886 AND RD 8-53-4472.

Part: ANGLE — CRACKED (NACELLE FIREWALL) · airframe 45,817 hrs · 54,236 cycles

FIREWALL ANGLE FOUND CRACKED ON LT NACELLE, INBD SIDE. REPAIRED FIREWALL ANGLE WITH NEW AND INSTALLED IAW RD8-54-0651.

Part: CONTROL UNIT — FAILED (AUTOFEATHER SYS) · airframe 45,805 hrs · 54,226 cycles

AUTOFEATHER FAILED TO ARM DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 70 KNOTS. R & R NR 2 TSCU IAW MM 72-01-10. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,694 hrs · 54,092 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,694 hrs · 54,092 cycles

EMERGENCY LIGHT BAR AT PAX DOOR HAS BULB INOPERATIVE. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,694 hrs · 54,092 cycles

F/A PANEL EMERGENCY LIGHT SWITCH AT PAX DOOR IS INOPERATIVE. REMOVED LIGHT LENS, FILTER. R & R BULB. OPS CHECKED GOOD. INSTALLED LENS AND FILTER.

Part: TSCU — FAILED (AUTOFEATHER SYS) · airframe 45,624 hrs · 54,002 cycles

AUTOFEATHER ARM LIGHT REMAINED ON AFTER SELECTING SWITCH OFF. LIGHT EXTINGUISHED AFTER ACFT LEVELED OFF AND POWER LEVER RETARDED TO APPROX 40 PERCENT TORQUE DURING DESCENT AUTOFEATHER LIGHT RE-LLUMINATED AND EXTINGUISHED BEFORE TOUCH DOWN. R & R TSCU AND CLEANED CONNECTOR PLUGS ON NR 2 TSCU. GROUND RAN ACFT. OPS CHECKED GOOD. CHECKED AUTOFEATHER TEST 12 TIMES IAW MX. RUN MANUAL. AUTOFEATHER ARMS AT 40 DEGRESS AND 54 PERCENT TORQUE. ARM LIGHT EXTINGUISHES EVERY TIME BELOW 54 PERCENT TORQUE.

Part: TSCU — INOPERATIVE (AUTOFEATHER SYS) · airframe 45,624 hrs · 54,002 cycles

AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. ABORTED TAKE OFF. R & R NR 1 TSCU. OPS CHECKED IAW -8 RUN UP MANUAL. CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 45,619 hrs · 53,995 cycles

AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. OAT +28, ABORTED TAKEOFF AND AUTOFEATHER ARMED ON TAXI WAY. INSPECTED SWITCHES, NO DEFECTS NOTED, GROUND RAN ACFT IAW -8 MX RUNUP MANUAL. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 45,606 hrs · 53,979 cycles

2 FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1 AND 8. R & R BULBS AT ROWS 1 AND 8 FOR FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 45,497 hrs · 53,843 cycles

NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT WITH LOSS OF HYD FLUID. FOUND PRESSURE LIN TO NR 2 HYD PUMP LEAKING ABOVE RETRACTION ACTUATOR. INSTALLED TEMP FLEX LINE BETWEEN FIREWALL AND PRESSURE MANIFOLD IAW SP 20.1. OPS AND LEAKED CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 45,497 hrs · 53,843 cycles

NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 2 ENGINE HYD PUMP IAW WC 29-00-00R AND CASE DRAIN FILTER IAW WC 29-12-03R. COMPLIED WITH LOSS OF FLUID INSPECTION IAW AMM 05-50-33. SERVICE AND BLED HYD. OPS AND LEAKED CHECKED GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 45,497 hrs · 53,943 cycles

DURING ALTERNATE GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH AMBER GEAR DOOR LIGHT ON. ALTERNATE GEAR VERIFICATION INDICATED UNSAFE. INDICATION CLEARED UPON LANDING. R & R NLG DRAG STRUT IAW WC 32-20-11R. PERFORMED NUMEROUS GEAR RETRACTIONS FOLLOWED BY BOTH NORMAL AND ALTERNATE EXTENSIONS. OPS CHECKED NORMAL. NLG DOWN AND LOCKED, INDICATION GOOD AT BOTH GEAR PANEL AND ALTERNATE PANEL.

Part: RELAY — INOPERATIVE (AUTOFEATHER SYS) · airframe 45,313 hrs · 53,603 cycles

AUTOFEATHER WOULD NOT ARM ON TAKEOFF ROLL. R & R RELAY 61-21 K5. OPS CHECKED GOOD IAW MX RUN UP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,180 hrs · 53,431 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT PAX DOOR IN INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,147 hrs · 53,387 cycles

RIGHT FWD EMERGENCY EXIT DOOR OVERHEAD LIGHT IS INOPERATIVE AT F/A OVERHEAD EMERGENCY LIGHT PANEL. R & R EMERGENCY POWER SUPPLY PS2 IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,134 hrs · 53,371 cycles

TWO EMERGENCY EXIT FLOOR LIGHTS ARE INOPERATIVE AT ROW 12. R & R EMERGENCY LIGHT BATTERY AT ROW 12, LT SIDE. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 44,893 hrs · 53,052 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,893 hrs · 53,052 cycles

LEFT AFT EMERGENCY EXIT LIGHT IS DIM. R & R BULBS. OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,879 hrs · 53,036 cycles

LT LOWER EMERGENCY LIGHT COVER IS BROKEN. R & R SUB ASSY COVER IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,247 hrs · 52,214 cycles

INOPERATIVE EMERGENCY PATH LIGHT AT ROW 5. REMOVED AND REPLACED BULB FOR EMERGENCY PATH LIGHT AT ROW 5 AND SECURED LENS COVER.

Part: SOCKET — FAILED (CABIN LIGHTS) · airframe 44,213 hrs · 52,170 cycles

SEAT 2DF HAS SMOKE COMING FROM OVERHEAD LIGHT. R & R LAMP HOLDER AT ROW 2DF IAW AMM 33-20-00 AND LIGHT BALLAST IAW AMM 33-21-02. OPS CHECKED GOOD.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 44,137 hrs · 52,070 cycles

OVERHEAD LIGHTING AT ROW 6AC SMOKING WITH BURNING ODOR. OVERHEAD LIGHTS DEACTIVATED IAW SP 33.1. INSPECTED AND FOUND OVERHEAD LIGHT HOLDER SOCKET BETWEEN 5C-6C BURNED UP. R & R HOLDER SOCKET AND BALLAST FOR OVERHEAD LIGHT AT 5C/6C IAW STANDARD PRACTICE.

Part: BULB — DAMAGED (CABIN LIGHTS) · airframe 43,914 hrs · 51,784 cycles

CABIN OVERHEAD LIGHTS AT ROW 12DF SMOKING. DAMAGED BULB REMOVED AND CABIN OVERHEAD LIGHTNING DEACTIVATED, PULLING CIRCUIT BREAKERS S1, S2 AND R2 ON RT MAIN BUSS. PULLED BULB AND CABIN OVERHEAD LIGHTNING DEACTIVATED. AT NEXT RUN, R & R ASSOCIATED BALLAST, BULB HOLDERS AND PERFORM HIDDEN DAMAGE INSPECTION. REPAIR AS REQUIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,780 hrs · 51,617 cycles

PLASTIC ODOR FROM DUCTS. GROUND RAN AIRCRAFT. SUSPECT RESIDUAL FROM PERI SEAL R & R. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: TRU — OVERHEATED (LEFT) · airframe 43,659 hrs · 51,454 cycles

HOT ELECTRICAL ODOR IN FORWARD CABIN AND COCKPIT IN FLIGHT. DECLARED AN EMERGENCY. LANDED SAFELY. GROUND RAN ACFT. INSPECTED WARDROBE CLOSET AND DC CONTACTOR BOX. NO ELECTRICAL ODOR FOUND. ODOR FROM LT TRU AND TRU WAS HOT TO THE TOUCH.

Part: PANEL — CORRODED · airframe 43,171 hrs · 50,798 cycles

FOUND CORRODED HARDWARE ON L/E PANEL 513AL. REMOVED OLD HARDWARE AND INSTALLED NEW HARDWARE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 42,866 hrs · 50,376 cycles

TWO FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 2 AND ROW 13. R & R BULBS AT ROWS 2 AND 13. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,499 hrs · 49,896 cycles

EMERGENCY EXIT LOWER DOOR SIGN HAS BULBS INOP AT ROW 2DF. R & R EMERGENCY EXIT LOWER DOOR SIGN BULBS. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,337 hrs · 49,703 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R EMERGENCY FLOOR PATH LIGHT AND CLOSED ACCESS PANEL AT ROW 9.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,059 hrs · 49,349 cycles

ROW 4 EMERGENCY FLOOR PATH LIGHT IS INOP. R & R ROW 4 EMERGENCY FLOOR PATH LIGHT, REMOVED LENS R & R BULB, REINSTALLED LENS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,333 hrs · 48,421 cycles

FORWARD MOST FLOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WIRE — CHAFED (SMOKE DETECTOR) · airframe 41,276 hrs · 48,351 cycles

BAG BAY SMOKE WARNING LIGHT ILLUMINATED INFLIGHT WITH ELECTRICAL ODOR IN CARGO BAY. FOUND CHAFED WIRES AT NR 2 CONNECTOR PLUG. REPAIRED WIRES AND R & R SMOKE DETECTOR. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 41,124 hrs · 48,161 cycles

CARGO SMOKE WARNING LIGHT FLICKERED FOR APPROX 2 SECONDS WHILE OFF LOADING BAGS. CARGO BAY SMOKE DETECTOR WAS INSPECTED AND FOUND CEILING SMOKE DETECTOR HOT TO THE TOUCH. R & R CARGO BAY NR 1 SMOKE DETECTOR.

Part: WARNING HORN — FALSE ACTIVATION · airframe 41,003 hrs · 48,002 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. RESET ELEVATOR TRIM AND FLAPS, HORN DID NOT SOUND. PERFORMED WORKCARD 31-50-03. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 40,682 hrs · 47,584 cycles

TWO FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 ARE INOP. LOWERED CEILING PANELS AT ROW 11, REPLACED BATTERY AT 3352-PS1. OPS GOOD. REINSTALLED PANEL.

Part: A/C PACK — SEIZED (CABIN) · airframe 40,648 hrs · 47,539 cycles

DURING TAXI, F/A REPORTED SMOKE AND ELECTRIC BURNING IN CABIN. INSPECTED ACFT AND FOUND PROBLEMS TO BE CABIN PACK SEIZED. REF LOG PAGE 33847-1 FOR ACTION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 40,422 hrs · 47,234 cycles

27 EMERGENCY FLOOR LIGHTS ON TOP, ALL RED LIGHTS AT ROW AFT OF EMERGENCY EXIT, 2 RED LIGHTS AFT FWD EXIT AND WHITE LIGHT ABOUT ROW 3 ARE NOT WORKING. FOUND PLUG DISCONNECTED AT AFT EMERGENCY ROW AND 3352-PS2 LOW IN POWER AND SEVERAL BULBS.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,422 hrs · 47,234 cycles

PAX DOOR THRESHOLD CORRODED. 1 FASTNER HOLE ELONGATED AND SURROUND DOOR PITS ALONG RADIUS OF THRESHOLD MEMBER. REMOVED THRESHOLD MEMBER. INSTALLED PAX DOOR THRESHOLD IAW DWG 85321241.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,422 hrs · 47,234 cycles

AT EITHER END OF SERVICE DOOR THRESHOLD, THERE IS SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION. APPLIED ALODINE AND PRIMED AS NECESSARY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,312 hrs · 45,826 cycles

ROW 11AC SIDEWALL EMERGENCY LIGHTS ARE INOP. RELAMP EMERGENCY LIGHT AT ROW 11AC SIDEWALL AS NEEDED IAW AMM 33-20-00.

Part: APU — SMOKE · airframe 38,405 hrs · 44,719 cycles

ON TOUCH DOWN, DC BUSS FAULT CAUTION LIGHT ILLUMINATED DURING TAXI. NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED, ON APPLYING GPU, SMOKE CAME FROM APU BAY AREA. DEACTIVATED APU START CONTACTOR IAW SP 49.1. POWERED ACFT FROM GPU AND GROUND RAN ENGINES, ALL OTHER SYS OPERATED NORMALLY. INSPECTED APU AREA, NO EVIDENCE OF FIRE DAMAGE NOTED.

Part: ACM — FAILED (AC BAY) · airframe 38,070 hrs · 44,321 cycles

FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, CLOSED TO CEILING. BURNING RUBBER SMELL DETECTED. INSPECTED AND FOUND AFT CABIN ACM FAILED. GROUND RAN AC WITH CABIN ACM OFF FOR 20 MINUTES. NO ODOR OR SMOKE FOUND. OKAY FOR SERVICE. APU COMPARTMENT HAS NO DAMAGE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 37,798 hrs · 43,993 cycles

ONE RED FLOOR EMERGENCY LIGHT AT ROW 1 IS NOT WORKING. R & R BULB. CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 37,798 hrs · 43,993 cycles

ONE WHITE FLOOR EMERGENCY LIGHT IS NOT WORKING AT ROW 3, THIRD LIGHT FROM END. R & R BULB, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,652 hrs · 43,818 cycles

WHILE USING THE ENG BLEEDS THERE WAS A CHEMICAL ODOR THROUGHOUT THE ACFT. NO SMOKE OR MIST WAS SEEN. GROUND RAN BOTH ENGINES CYCLING THE BLEEDS ON SEPARATE AND TOGETHER. NO CHEMICAL ODOR. EVALUATION FLIGHT WAS SATISFACTORY.

Part: ELEVATOR SYSTEM — STIFF · airframe 37,420 hrs · 43,549 cycles

ACFT FAILED TO ROTATE DUE TO EXCESSIVE ELEVATOR FORCE REQUIRED, ABORTED TAKEOFF. VISUALLY INSPECTED ACFT AND FLIGHT CONTROL SURFACES. NO OBVIOUS OBSTRUCTIONS OR ICE ACCUMULATIONS NOTED. FLIGHT CONTROLS MOVE FREELY AT THIS TIME, ACFT OK FOR SERVICE.

Part: TRANSCEIVER — BROKEN (WX RADAR) · airframe 36,837 hrs · 42,840 cycles

RADAR DISPLAYS ANTENNA MESSAGES INTERMITTENTLY AND SPIKES. ALSO DOES NOT PAINT KNOWN WEATHER. THE RADAR RT WAS REMOVED AND REPLACED AND THE OPERATIONAL CHECK WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 36,736 hrs · 42,705 cycles

DURING INSPECTION IN SBY, IT WAS FOUND THAT AN EMERGENCY LIGHT WAS INOPERATIVE. LIGHT BULB WAS REMOVED AND REPLACE AND THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,634 hrs · 42,579 cycles

ON AUGUST 20, 2009 IN SBY THE LEFT AFT EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT AND THE OPERATIONAL CHECK WAS GOOD.

Part: RELAY — FAILED (PROPELLER) · airframe 36,424 hrs · 42,367 cycles

AUTO FEATHER FAILED TO ARM DURING TAKEOFF RUN. REMOVED AND REPLACED RELAY 6121-K5. GROUND RAN ACFT IAW MX RUN UP MANUAL AND DASH-8 MM CHAP 61. AUTO FEATHER ARMS CORRECTLY, CLEAR MEL.

Part: AHRS — MALFUNCTIONED (COCKPIT) · airframe 35,792 hrs · 41,534 cycles

NUMBER ONE ATTITUDE HEADING AND REFERENCE SYSTEM FAILED. DATA INVALID MESSAGE. CANNOT DUPLICATE. ATTITUDE HEADING AND REFERENCE SYSTEM SELF TEST CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (PITOT SYSTEM) · airframe 35,792 hrs · 41,534 cycles

NUMBER TWO PITOT HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT FOLLOWED BY LOSS OF AIRSPEED. MAINTENANCE INSPECT WIRING AT PITOT SELECT SWITCHES. INSPECT CONNECTOR 9811930 AT RELAY PANEL 1. INSPECTED BOTH PITOT TUBES, NO DEFECTS NOTED. PERFORMED OPS CHECK OF PITOT STATIC SYSTEM IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 30-31-00, OPS NORMAL AT THIS TIME.

Part: UNKNOWN — UNKNOWN (FLT CONTROLS) · airframe 35,376 hrs · 41,017 cycles

UNABLE TO ROTATE ACFT ON TAKE OFF ROLL. VISUAL AND OPS INSPECTION OF ACFT ELEVATOR FLIGHT CONTROLS AND SURFACES, NO DEFECTS NOTED. OK FOR SERVICE. ACFT RELEASED FOR AN EVALUATION FLIGHT DUE TO UNABLE TO ROTATE ACFT ON TAKE-OFF, MX ACTION COMPLETE SUBJECT TO SATISFACTORY EVAL FLT. EVALUATION FLIGHT SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,356 hrs · 40,991 cycles

NR 4 EMERGENCY AISLE MARKER LIGHT INOP. R&R NR 4 EMERGENCY AISLE MARKER AISLE LIGHT IAW 33-51-03. OPS CHECK GOOD.

Part: SOCKET — BURNED (CABIN) · airframe 35,307 hrs · 40,931 cycles

THE ROW 8DF OVERHEAD LIGHTING WAS FOUND TO HAVE A BURNT SOCKET RECEPTACLE. A HIDDEN DAMAGE INSPECTION WAS PERFORMED AND BULB REMOVED FROM THE AFFECTED LIGHT FIXTURE. THE SYSTEM C/B WAS COLLARED TO DEACTIVATE THE SYSTEM IAW SPECIAL PROCEDURES AND PLACED ON THE MEL LIST FOR THIS ACFT. WHEN THE ACFT REACHED AN RON BASE, MX REPLACED THE LIGHT SOCKET AND ASSOCIATED BALLAST AND INSTALLED A NEW BULB. OPS CHECKS WERE GOOD AND THE ITEM WAS REMOVED FROM THE MEL LIST.

Part: REGULATOR — FAILED (NR 1 ENGINE) · airframe 35,175 hrs · 40,766 cycles

NR 1 ENGINE TEMPERATURE WENT TO MAX PERMISSIBLE LIMIT OF 125 DEGREES, IMMEDIATELY PULLED POWER BACK TO BRING TEMPERATURE TO 115 DEGREE WITH IN LIMITS. R&R THERMO VALVE ON NR 1 ENGINE OIL COOLER IAW 79-20-11, OPS CHECK GOOD.

Part: INDICATOR — DEFECTIVE (FLAP POSITION) · airframe 34,826 hrs · 40,351 cycles

TAKEOFF WAS ABORTED WHEN THE TAKEOFF WARNING HORN SOUNDED. MAINTENANCE CYCLED THE CONDITION LEVER AND SYSTEM OPERATED NORMALLY. THE FLAP POSITION INDICATOR WAS CHANGED OUT AND SYSTEM CHECK WAS PERFORMED. NO DEFECTS WERE NOTED AT THAT TIME AND AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: AUTOFEATHER SYS — INOPERATIVE

AUTOFEATHER WOULD NOT ARM DURING TAKEOFF. RETRIMMED BOTH ENGINES AUTOFEATHER ARMED AT 40 DEGREES OF P/LEVER ANGLE WITH A TORQUE OF 74 PERCENT. OPS CHECK GOOD. (K)

Part: RELAY — FAILED (PROPELLER) · airframe 33,908 hrs · 39,214 cycles

AUTO FX WOULD NOT ARM DURING TAKEOFF.

Part: TSCU — FAULTED (AUTOFEATHER SYS) · airframe 33,908 hrs · 39,214 cycles

AUTO FEATHER WOULD NOT ARM DURING TAKEOFF ROLL.

Part: POTENTIOMETER — MISRIGGED (AUTOFEATHER SYS) · airframe 33,910 hrs · 39,217 cycles

AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL.

Part: RELAY — FAULTY (AUTOFEATHER SYS) · airframe 33,665 hrs · 38,924 cycles

AUTO FX WILL NOT ARM ON TAKEOFF ROLL STATIC TEST.

Part: SELECTOR PANEL — FALSE INDICATION (MLG) · airframe 33,831 hrs · 39,268 cycles

AFTER GEAR WAS SELECTED DOWN, THE RIGHT MAIN INDICATION DID NOT LIGHT UP GREEN. THE ALTERNATE EXTENSION INDICATIONS ALL INDICATED GREEN AS NORMAL. THE FLIGHT LANDED SAFELY AND DID NOT DECLARE AN EMERGENCY BUT ISP TOWER SENT OUT EMERGENCY VEHICALS ANYWAY, INDICATING IT IS THEIR PROCEDURE TO TREAT THIS AS AN EMERGENCY.

Part: CONTACTOR — SEIZED (APU STARTER) · airframe 32,511 hrs · 37,513 cycles

MAIN BATTERY TEMP AT 55 DEG AND VOLTAGE AT 15 VOLTS WITH MAIN AND AUX BATTERY CAUTION LIGHTS ILLUMINATED, AIRCRAFT RETURNED TO GATE AND SHUTDOWN POWER. WHEN EXTERNAL POWER APPLIED, FIRE DETECTION WARNING LIGHTS ILLUMINATED AND APU FIRE PANEL WAS BLANK, CREW NOTED SMOKE COMING FROM APU COMPARTMENT. THE CREW WAS ADVISED TO SHUT OFF POWER AND CONTACT THE FIRE DEPARTMENT. THE FIRE DEPARTMENT RESPONDED, NO FIRE WAS NOTED, BUT A LOT OF SMOKE WAS COMING FROM THE APU COMPARTMENT. APU START CONTACTOR APPEARS TO BE WELDED AND CIRCUIT BREAKER N-8 (APU AUX) WAS POPPED CAUSING THE STARTER TO OVERHEAT AND GENERATE THE SMOKE. REMOVED AND REPLACED APU START CONTACTOR AND STARTER/GENERATOR, OPS CHECK GOOD. PERFORMED HIDDEN DAMAGE INSPECTION, NO FURTHER DAMAGE FOUND.

Part: RELAY — UNKNOWN (APU BAY) · airframe 32,511 hrs · 37,513 cycles

CREW ATTEMPTED TO DISCHARGE APU FIRE BOTTLE. FIRE BOTTLE DID NOT DISCHARGE. (VERIFIED IN ROA ON 2 OCT 07). VERIFIED 28 VOLTS AT SQUIB CONNECTOR. REPLACED SQUIB AS PRECAUTION. OPS CHECKED OLD SQUIB, CHECKED GOOD. SUSPECT FAULT CAUSED BY APU AIR/GROUND RELAY 7615-K4 WHICH IS ENERGIZED BY RT MAIN BUS, DE-ENERGIZED WHEN APU GENERATOR CONTACTOR FAILED CAUSING LARGE BUSS VOLTAGE DROP TAKING POWER FROM SQUIB CARTRIDGE. REMOVED AND REPLACED RELAY 7615-K4 AS PRECAUTION.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,654 hrs · 35,283 cycles

BURNING SMELL IN CABIN APPEARS STRONGEST IN COAT CLOSET. SUSPECT P/A AMP CAUSING ODOR, OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (MLG DOOR) · airframe 29,742 hrs · 34,166 cycles

NOSE GEAR DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED NOSE GEAR PROXIMITY SENSOR.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 27,714 hrs · 31,591 cycles

DC BUSS FAULT ILLUMINATED IN FLIGHT FOLLOWED BY NUMEROUS OTHER CAUTION LIGHTS, AUX INV RUDDER FULL PRESS, GPWS, PAX DOOR, BAG DOOR, FWD EXIT DOOR, SERVICE DOOR. REMOVED AND REPLACED NR 1 DC GENERATOR.

Part: DOOR FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,139 hrs · 27,137 cycles

LIP AT PAX DOOR ENTERANCE WAY IS CORRODED ENTIRE LENGTH OF FLANGE, R&R AIRSTAIR DOOR THRESHOLD

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 23,736 hrs · 26,664 cycles

ELECTRICAL OVERHEAT ODOR AT CABIN ROWS 11, 12, 13. FOUND LAMP HOLDER 1AC BURNED. REMOVED BULB IAW EO AND MEL LIGHT.

Part: NUT — DAMAGED (#2 WHEEL ASSY) · airframe 19,471 hrs · 21,144 cycles

DURRING WHEEL REMOVAL AND REPLACEMENT, #2 WHEEL ASSEMBLY AXEL NUT WAS FOUND DAMAGED. REPLACED NUT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,223 hrs · 19,453 cycles

THIRD AND FOURTH RED FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 AND 4 WHITE FLOOR LEVEL EMERGENCY LIGHTS AT ROW 4 WERE INOP. REPLACED EMERGENCY LIGHT BATTERY PACKS 3351-PS2 & PS3 AND BATTERY PACK POWER SUPPLY 3351-PS2.