N331EN

Part: BLEED AIR SYS — SMOKE (APU) · airframe 53,812 hrs · 63,820 cycles

APU BLEED CREATES A SMOKE IN THE CABIN.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,798 hrs · 63,802 cycles

TWO AFT MOST CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED THE POWER SUPPLY IN POSITION PS4 AND REPLACED WITH NEW.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,797 hrs · 63,802 cycles

RIGHT FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. REMOVED THE POWER SUPPLY IN POSITION PS4 AND REPLACED WITH NEW.

Part: EEC — INOPERATIVE (NR 2 ENGINE) · airframe 53,768 hrs · 63,760 cycles

ECU ON NR 2 ENGINE INOP. R&R NR 2 EEC IAW AMM 72-01-10. OPS CK GOOD OK FOR SERVICE.

Part: APU — SMOKE · airframe 53,648 hrs · 63,598 cycles

APU REMAINED IN START MODE, SMOKE IN APU AREA, MX INSPECTED FOR HIDDEN DAMAGE.

Part: APU — ODOR · airframe 53,648 hrs · 63,598 cycles

HOT ELECTRICAL ODOR DURING FLIGHT. RAN ENGINES WITH BLEED AIR ON, NO ABNORMAL FUMES OR ODOR NOTICED, IAW PDT RUN MANUAL. RAN APU WITH BLEED ON, MODERATE FUEL ODOR NOTED.

Part: LIGHT — FAILED (COCKPIT) · airframe 53,422 hrs · 63,301 cycles

CIRCUIT BREAKER M4 FOR COPILOTS LIGHT PANEL TRIPPED AND CREATED SMOKE IN THE COCKPIT. REMOVED AND REPLACED ICE DETECTION LIGHT AS REQUIRED. OPS CHECKED GOOD, OK FOR SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 53,104 hrs · 62,891 cycles

AUTOFEATHER DID NOT ARM. REJECTED TAKE OFF AT 50 KTS. FAILS TO ARM STATICALLY. GROUND RAN IAW MM. OPS CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,988 hrs · 62,734 cycles

STRONG BURNING ODOR THROUGHOUT ACFT. EVENTUALLY DISSIPATED IN COCKPIT AND STILL NOTICEABLE IN CABIN. ENGINE PARAMETERS NORMAL, NO CAUTION OR WARNING LIGHTS ILLUMINATED. INSPECTED THE ACFT. NO DEFECTS NOTED. GROUND RAN, NO ODORS NOTED. OK FOR SERVICE

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 52,900 hrs · 62,616 cycles

EMERGENCY FLOOR PATHLIGHTS ARE INOP AT ROWS 2 AND 6. R & R THE EMERGENCY LIGHT LAMPS.

Part: SWITCH — DAMAGED (MLG) · airframe 52,874 hrs · 62,584 cycles

DURING APPROACH, RECEIVED THREE GEAR RED UNSAFE LIGHTS, WITH GEAR HANDLE SELECTED DOWN, NO CAUTION LIGHTS ILLUMINATED. WHILE EXECUTING ALTERNATE GEAR EXTENSION PROCEDURE, RED SWITCH GUARD PUSHED UP, GEAR CAME DOWN WITH THREE GREEN LIGHTS, VERIFIED ALT EXTENSION LIGHT, NORMAL LANDING. PERFORMED PSEU TESTS IAW AMM 32-61-50. NO DEFECTS NOTED. INSPECTED INHIBIT SWITCH AND FOUND LOOSE HARDWARE. REMOVED AND REPLACED THE SWITCH IAW 32-61-00. OPS CHECKED GOOD. OK FOR SERVICE. SWUNG GEAR 14 TIMES AND PERFORMED ALTERNATE L/G EXTENSION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,669 hrs · 62,300 cycles

RED FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 52,615 hrs · 27,298 cycles

CABIN EMERGENCY LIGHT INOPERATIVE.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 51,630 hrs · 60,965 cycles

FA EMERGENCY LIGHT SWITCH DOES NOT OPERATE EMERGENCY LIGHTS. ON MAIN AND AUX BATTERIES, BEING REINSTALLED THE SWITCH CYCLED PROPERLY. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN · airframe 51,323 hrs · 60,548 cycles

NR 2 ENGINE ONLINE, ABORTED NR 1 ENGINE START AT 40 PERCENT NH, DUE TO REPORT OF POSSIBLE SMOKE IN REAR CABIN. PERFORMED 2 NORMAL NR 1 ENGINE START W/NR 2 ENGINE ONLINE. NO SMOKE, FUMES OR ELECTRICAL ODOR NOTED. OPS CK ENGINE BLEEDS AND OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,323 hrs · 60,548 cycles

MULTIPLE INTERIOR EMERGENCY LIGHTS ARE DIM OR OUT. R & R EMERGENCY LIGHT POWER SUPPLIES IAW WC 33-50-05, OPS CHECK IAW WC 33-50-03.

Part: LIGHT — DIM (CABIN) · airframe 51,120 hrs · 60,274 cycles

LEFT AFT EGRESS LIGHT IS DIM. REMOVED COVER. R &R BULB REINSTALLED COVER WITH ATTAIN HARDWARE. OPS GOOD PN OFF AND ON BULB 85.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,120 hrs · 60,274 cycles

13DF FLOOR EMERGENCY LIGHT IS OUT. PULLED UP TRIM R & R BULB. REINSTALLED LIGHT FIXTURE AND TRIM, P/N OFF AND ON OL3071BPEGPL.

Part: CONNECTOR — CORRODED · airframe 50,394 hrs · 59,327 cycles

PUSHER SYS FAIL CAUTION LIGHT ILLUMINATED AND REMAINED ON. FOUND CONNECTOR HEAVILY CORRODED. R & R CONNECTOR IAW 27-20-02.

Part: CONNECTOR — DAMAGED · airframe 50,394 hrs · 59,327 cycles

RUDDER PRESSURE CAUTION LIGHT ILLUMINATED DURING CLIMBOUT, EXTINGUISHED AFTER LANDING. R & R CONNECTOR. OPS CHECKED GOOD IAW 27-20-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 49,928 hrs · 58,689 cycles

EMERGENCY FLOOR LIGHT AT ROW 5 NOT ILLUMINATING. REMOVED FLOOR LENS, STRIP, R & R BULB IN LIGHT MODULE AND REINSTALLED IN FLOOR STRIP AND SECURED LENS COVERING.

Part: CONTROL BOX — MALFUNCTIONED (LIGHT) · airframe 49,194 hrs · 57,729 cycles

EMERGENCY LIGHTS ILLUMINATED ON TAXI FOR 15 SECONDS. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD IAW 33-51-00.OK FOR SERVICE.

Part: CONNECTOR — LOOSE (HYD SYSTEM) · airframe 49,171 hrs · 57,701 cycles

ROLL SPOILER OTBD HYDRAULIC CAUTION LIGHT ON IN FLIGHT. MAINTENANCE CLEANED PRESSURE SWITCH AND ELECTRICAL CONNECTOR. TIGHTENED CONNECTOR ON BACKSHELL, GROUND RAN ACFT, OPS CHECKED GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,032 hrs · 57,517 cycles

EMERGENCY FLOOR LIGHT, 6TH FROM THE FRONT IS INOPERATIVE. R & R BULB FROM EMERGENCY FLOOR LIGHT, OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN LIGHTS) · airframe 48,350 hrs · 56,619 cycles

SMELLED ELECTRICAL SMOKE IN CABIN WITH APU ON. INSPECTED INNER CABIN AREA, OVERHEAD LIGHT, BALLAST AND SURROUNDING WIRING. FOUND LIGHT BULB TUBES AT ROW 6DF AND 5AC BE SUSPECTED. R & R BULBS. NO SMOKE OR ODOR NOTICED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,305 hrs · 56,651 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,858 hrs · 55,970 cycles

EMERGENCY LIGHTS AT 10TH, 15TH AND 27TH POSITION ARE INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 47,869 hrs · 55,985 cycles

PASSENGER DOOR WARNING LIGHT ILLUMINATED DURING CLIMBOUT, EXTINGUISHING AFTER APPROXIMATELY 2-3 MINUTES. ADJUSTED DOOR WARNING SENSOR IAW MM 52-10-00. OPS CHECKED GOOD. CLEARED MEL.

Part: ENGINE — OVERTEMP (NR 2) · airframe 47,284 hrs · 55,208 cycles

NR 2 ENGINE OIL TEMP AT TOP 0F GREEN ARC. ACFT RETURN TO FIELD.

Part: CONNECTOR — CONTAMINATED (GENERATOR) · airframe 47,284 hrs · 55,208 cycles

NR 2 AC GENERATOR CAUTION LIGHT AND NR 2 AC GENERATOR HOT CAUTION LIGHT ILLUMINATED. FOUND AC GEN CONNECTOR PLUG OIL SOAKED. CLEANED CONNECTOR. RAN ACFT, NO HOT LIGHT, BUT WOULD NOT COME ONLINE. R & R NR 2 AC GENERATOR IAW WC 24-20-11.

Part: TUBE — CHAFED (NR 2 NACELLE) · airframe 47,284 hrs · 55,207 cycles

NR 2 NACELLE LOWER OTD SUPPORT TUBE IS CHAFED. REPAIRED CHAFE DAMAGE IAW EO8-54-14-0311.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,048 hrs · 54,877 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE AT ROW 5DF. R & R BULB. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 46,590 hrs · 54,281 cycles

PAX DOOR EXIT EMERGENCY LIGHT IS DIM AT BOTTOM SECTION. R & R BULB ON PAX DOOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,156 hrs · 53,727 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 5DF IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,094 hrs · 53,656 cycles

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

Part: WARNING LIGHT — ILLUMINATED (DC GENERATOR) · airframe 45,616 hrs · 53,053 cycles

MASTER WARNING LIGHT FLASHED UPON GEAR RETRACTION, ALONG WITH NR 1 DC GENERATOR CAUTION LIGHT. R & R NR 1 DC GENERATOR IAW WC 24-30--2. OPS AND LEAKED CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,575 hrs · 52,996 cycles

CEILING EMERGENCY ESCAPE PATH LIGHT IS INOPERATIVE AT ROW 4. R & R BULB ON CEILING EMERGENCY ESCAPE PATH AT ROW 4 IAW MM 33-51-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,575 hrs · 52,996 cycles

EMERGENCY RED LIGHT INOPERATIVE AT ROW 11. R & R BULB IAW MM 33-51-00. OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (NR 1 ENGINE) · airframe 45,120 hrs · 52,388 cycles

LEFT MAIN BUSS FAULT OCCURRED WHEN SELECTING NR 1 ENGINE START BUTTON WITH ELECTRICAL SMELL. R & R NR 1 STARTER GENERATOR IAW WC 24-30-02R. START CONTACTOR 2431K1 WAS REPLACED IAW MM 24-31-09. OPS AND LEAKED CHECKED GOOD.

Part: SKIN PANEL — DAMAGED (DOOR) · airframe 45,102 hrs · 52,362 cycles

BIRDSTRIKE OCCURRED AT 9000 FEET, JUST BELOW CAPTAIN'S WINDSCREEN. INSPECTED AFFECTED AREA IAW -8 MM 05-50-26. FOUND DOOR PANEL 212AL DAMAGED. R & R DOOR SKIN PANEL 212AL.

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 44,942 hrs · 52,150 cycles

AUTOFEATHER ARM LIGHT ILLUMINATED IN FLIGHT, ARM LIGHT STAYS ILLUMINATED UNTIL POWER LEVERS BROUGHT BELOW 60 PERCENT. R & R NR 1 ENGINE WIRING HARNESS. OPS CHECK GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 44,937 hrs · 52,142 cycles

AUTOFEATHER ARM LIGHT ILLUMINATED IN FLIGHT. ARM STAYS ILLUMINATED UNTIL BELOW 60 PERCENT TORQUE. NR 2 DOES NOT TEST. DUE TO AUTOFEATHER ARM LIGHT ILLUMINATED WITH AUTOFEATHER SELECTED. DEACTIVATED AUTOFEATHER SYS BY PULLING RELAYS 6121-K1 AND 6121-K2 FOR FERRY PURPOSE.

Part: TSCU — INOPERATIVE (AUTOFEATHER SYS) · airframe 44,916 hrs · 52,114 cycles

AUTO FEATHER ARMED DURING CLIMB. R & R NR 2 TSCU I AW CMM 72-01-10. R & R RELAYS 6121-K3 AND K4 IAW 61-21-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FAN — ODOR (CABIN) · airframe 44,523 hrs · 51,585 cycles

F/A REPORTED BURNING ODOR IN FORWARD CABIN AREA. GROUND RAN ACFT WITH ENGINE BLEEDS ON, NO DEFECTS NOTED. INSPECTED ALL OVERHEAD LIGHT FIXTURES, NO DEFECTS NOTED. INSPECTED COMPONENTS IN WARDROBE CLOSET AND AVIONICS RACK, NO DEFECTS NOTED. DISABLED COOLING FAN ABOVE WARDROBE AND ODOR DISSIPATED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 44,468 hrs · 51,509 cycles

DIM CEILING EMERGENCY LIGHT AT AFT POSITION. R & R AFT CEILING EMERGENCY LIGHT, SECURED LIGHT LENS.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 44,368 hrs · 51,377 cycles

ON DEPARTURE AT APPROX 500 FEET NR 1 ENGINE APPEARS TO HAVE FLAMED OUT. ENGINE FEATHERED NORMALLY AND ACFT LANDED WITHOUT INCIDENT. R & R NR 1 PROP IAW 61-10-06. PERFORMED WORK CARD 61-20-10 BETA LOCKOUT LOGIC OPS CHECK. OPS CHECKED GOOD. PERFORMED RUN IAW PMM. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,317 hrs · 51,313 cycles

LOWER RT FORWARD EMERGENCY SIGN IS DIM. R & R BULBS IN FWD EMERGENCY SIGN.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 44,264 hrs · 51,245 cycles

AFT RT LOWER EMERGENCY SIGN IS DIM. R & R BULB AT AFT RT LOWER EMERGENCY SIGN AND RESECURED LENS, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,172 hrs · 51,129 cycles

EMERGENCY FLOOR LIGHT AT ROW 5 IS INOPERATIVE. R & R EMERGENCY LIGHT BULB. RESECURED COVER. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ELEVATOR) · airframe 44,115 hrs · 51,061 cycles

ON TAKEOFF ROLL, LT ELEVATOR HORN HEAT CAUTION LIGHT CAME ON. INSPECTED AND FOUND ELEVATOR HORN HEAT SWITCH IN THE ALTERNATE POSITION. CHECKED, NO DML FOUND. SELECTED TO NORMAL, GROUND RAN ACFT. OPS CHECKED GOOD.

Part: CONNECTOR — CONTAMINATED (AUTOFEATHER SYS) · airframe 43,871 hrs · 50,742 cycles

AUTOFEATHER ARM LIGHT WILL NOT EXTINGUISH WHEN AUTOFEATHER IS SELECTED OFF. FOUND AUTOFEATHER STATIC TESTING PROPERLY. FOUND NR 2 TSCU CONNECTOR PLUG OIL SOAKED. CLEANED AND RESEATED CONNECTOR PLUGS. OPS CHECKED GOOD AT THIS TIME.

Part: APU — FIRE (APU BAY) · airframe 43,770 hrs · 50,609 cycles

DISCHARGED, HAND OPERATED DRY FILM FIRE EXTINGUISHER, DUE TO SMALL FIRE IN APU BAY. INSPECTED APU BAY. FOUND NO DAMAGE FROM FIRE OR FIRE EXTINGUISHING AGENT. CLEANED APU COMPARTMENT IAW STANDARD PRACTICES.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,219 hrs · 49,896 cycles

ROW 1 AND ROW 9 EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,188 hrs · 49,857 cycles

FIRST RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED BULB AND INSTALLED NEW BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,602 hrs · 49,085 cycles

ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 4. REMOVED LENS, REMOVED AND REPLACED BULB. REINSTALLED LENS, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,996 hrs · 48,292 cycles

AFTER PUSH BACK F/A REPORTS PLASTIC ODOR IN FWD CABIN. F/A SAID ODOR COULD BE A FISHY ODOR AFTER ASKING HER SEVERAL TIMES. CREW RAN ACFT FOR APROX 30 MIN, WITH MECHANIC AND F/A ON BOARD. OPERATED INVERTERS ONE AT A TIME. NO ODOR NOTED. CHECKED RELAY PANEL & COAT CLOSET. OPERATED CABIN LIGHTS WITH NO ODOR NOTED. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,996 hrs · 48,292 cycles

F/A REPORTS PLASTIC ODOR IN FWD CABIN IN FLIGHT. INSPECTED COCKPIT & COAT CLOSET FROM DEFECTS. NONE FOUND, INSPECTED CABIN LIGHTS FOR DEFECTS NONE FOUND. NO OBVIOUS ODOR AT THIS TIME.

Part: CONTROL CABLE — OUT OF POSITION (ENGINE) · airframe 41,754 hrs · 47,992 cycles

FOUND NR 2 ENGINE CONDITION CONTROL CABLE CAUGHT ON CABIN CEILING PANEL AT ROW 1. REMOVED NR 2 ENGINE CONDITION CABLE FROM CEILING PANEL AT ROW 1. FOUND NO DAMAGE TO CABLE.

Part: FRAME — CORRODED (BS 593) · airframe 41,074 hrs · 47,134 cycles

CORROSION FOUND ON FRAME AT ST X593 BETWEEN STR 30S AND 32S. NEED APPROVAL OF SRM 53-2021.

Part: SEAT TRACK — CORRODED (BS 197-588) · airframe 41,132 hrs · 47,205 cycles

LIGHT SURFACE CORROSION FOUND ON LT INBD SEAT TRACK BETWEEN STA X197 TO X588. R & R WITH NEW ONE IAW SRM 61-42-05.

Part: SWITCH — INOPERATIVE · airframe 40,906 hrs · 46,932 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. DURING ENGINE RUN AND TAKEOFF WARNING CHECK, FOUND NR1 CONDITION LEVER SWITCH 3151-S3 (TO WARNING HORN) OUT OF RIG. HORN SOUNDED WHEN NR1 LEVER BROUGHT BACK .0625". REPLACED AND RIGGED SWITCH 3151-S3 IAW MM 76-10-13. OPS CHECK OF TO WARNING SYS GOOD, CLEARED MEL.

Part: WARNING HORN — FALSE ACTIVATION · airframe 40,899 hrs · 46,924 cycles

REJECTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDING. COMPLIED WITH TAKEOFF AND OVER-SPEED WARNING HORN CHECKS IAW 31-51-01. NO DEFECTS NOTED AND CAN NOT DUPLICATE.

Part: STARTER GEN — FAILED (NR 1 ENGINE) · airframe 40,756 hrs · 46,752 cycles

WITH NR 2 ENGINE AND APU RUNNING, EXPERENCED BUSS FAULT WHEN ATTEMPTING TO START NR 1 ENGINE. RETURN TO GATE. SMOKE WAS SEEN COMING FROM NR 1 COWLING. SHUTDOWN ACFT AND EVACUATED. R & R NR 1 START CONTACTOR 2431K1 AND NR 1 START GENERATOR IAW PWC 24-30-02R. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (ENGINE) · airframe 40,756 hrs · 46,750 cycles

NR 1 NH INDICATOR IS ERRACTIC, ANALOG AND DIGITAL FLUCTUATING. ALL OTHER PARAMETERS STEADY. R & R NR 1 NH PROBE, OPS CHECKED GOOD ON ENGINE RUN. ALSO R & R ENGINE WIRE HARNESS ON THE RT SIDE OF ENGINE. R & R WIRE HARNESS ON LT SIDE OF ENGINE. ALL WORK PERFORMED IAW MM 72-01-10. GROUND CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 40,754 hrs · 76,747 cycles

1 RED FLOOR EMERGENCY LIGHT INOPERATIVE. R & R RED EMERGENCY FLOOR LIGHT BULB AS REQUIRED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,181 hrs · 45,980 cycles

PAX DOOR THRESHOLD IS CORRODED. REMOVED THRESHOLD AND FRAME MEMBER, DRILLED NEW PARTS, PARTIALLY INSTALLED FRAME MEMBER. COMPLETED INSTALLATION OF FRAME MEMBER AND THRESHOLD IAW DWG 85321241.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,181 hrs · 45,980 cycles

AFT SERVICE DOOR THRESHOLD HAS MINOR SURFACE CORROSION. REMOVED CORROSION, ALODINE AND PRIMED AFT SERVICE DOOR THRESHOLD IAW MM 20-16-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,181 hrs · 45,980 cycles

SURFACE CORROSION ON RT INBD SEAT RAIL ABOUT 6 INCHES FROM COCKPIT DOOR. REMOVED CORROSION IAW RD 53-4698. ALODINED AND PRIMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,181 hrs · 45,980 cycles

SURFACE CORROSION ON RT SEAT RAIL 6 INCHES FROM COCKPIT DOOR. REMOVED CORROSION IAW RD8-53-833, ALODINED AND PRIMED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 39,124 hrs · 44,600 cycles

EMERGENCY FLOOR LEVEL RED LIGHT INOP. WIRE PULLED OUT. REPLACED BROKEN WIRE FOR FWD RED EMERGENCY LIGHT. OPS CHECKED GOOD, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,955 hrs · 43,106 cycles

ROW 5 AND 6 FLOOR EMERGENCY PATH LIGHT NOT WORKING. RELAMP ROW 5 AND 6 FLOOR EMERGENCY PATH LIGHTS IAW AMM 33-51-00.

Part: UNKNOWN — MALFUNCTIONED (CONTROL COLUMN) · airframe 37,711 hrs · 42,804 cycles

UNCOMMANDED ROLL DISCONNECT ON APPROACH. LIGHT TURBULENCE WITH MODERATE CHOP NOTED. CAPTAIN AND F/O'S YOKE ROLLED INDEPENDENTLY. CREW HEARD YOKE CLICK BACK IN ON TOUCHDOWN. REMOVED PANEL 122AR AND INSPECTED ROLL SYSTEM DISCONNECT SYSTEM, NO DEFECTS NOTED. C/W WORK CARD 27-60-02Q AND RE-INSTALLED PANEL 122AR. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: REGULATOR VALVE — FAULTY (NR 2 ENGINE) · airframe 37,656 hrs · 42,736 cycles

ON CLIMBOUT NR 2 ENGINE OIL TEMP ROSE TO APPROX 115 DEGREES FOR APPROX 10 MINUTES, REDUCED NR 2 ENGINE POWER AND NR 2 ENGINE OIL TEMP STABILIZED AT APPROX 110 DEGREES C. REMOVED AND REPLACED NR 2 ENGINE OIL TEMP REGULATING VALVE, LEAK CHECKED GOOD AND RAN AIRCRAFT TO HIGH POWER FOR 5 MINUTES, TEMP STABLE AT 90 DEGREES INDICATED. AIRCRAFT OK FOR SERVICE REFERENCE CMM 79-20-11.

Part: BRAKE — SMOKE (LEFT) · airframe 36,373 hrs · 41,138 cycles

GROUND CREW REPORTED SMOKE COMING FROM LT WHEEL ASSY. INSPECTED & BLED NR 1 & 2 BRAKE ASSY'S, TAXIED AIRCRAFT NO DEFECT NOTED, OK FOR SERVICE

Part: SENSOR — DIRTY (SERVICE DOOR) · airframe 35,510 hrs · 40,061 cycles

REJECTED TAKEOFF DUE TO SERVICE DOOR WARNING LIGHT. INSPECTED SERVICE DOOR FOR SECURITY AND FOUND IT TO BE SECURE. CLEANED SERVICE DOOR SENSOR AND LUBED AS REQUIRED. OPERATED DOOR SEVERAL TIMES. NO DEFECTS NOTED.

Part: BOLT — CORRODED (ZONE 500) · airframe 35,338 hrs · 39,834 cycles

BOLT GROOVED AND CORRODED AT LT NR 3 FLAP TRACK BEAM, TO BE REPLACE. REMOVED AND REPLACE BOLT IAW MM 57-50-26.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 25,338 hrs · 39,834 cycles

PAX DOOR THRESHOLD FOUND CORRODED AT SEVERAL PLACES. REMOVED AND REPLACE THRESHOLD IAW SRM 51-40-00.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 35,338 hrs · 39,834 cycles

CORROSION FOUND ON LWR FWD AND AFT BRACKET AND ON MIDDLE AFT BRACKET UNDER PAX DOOR COMPOSITE STRUCTURE. REMOVED AND REPLACE BRACKET IAW MM 20-14-01 AND CLEAN AND PROTECT MIDDLE BRACKET IAW SRM 21-20-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,294 hrs · 39,787 cycles

UPON A LINE CHECK AT SBY FOUR EMERGENCY LIGHTS WERE INOPERATIVE IN THE FIRST FOUR ROWS. RELAMPED EMERGENCIES LIGHTS, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,287 hrs · 39,779 cycles

LIGHT BULB INOP, EMERGENCY FLOOR LIGHTING 2ND ROW FROM AFT. REMOVED AND REPLACED BULB, OPS CHECK GOOD.

Part: APU — LEAKING (APU BAY)

F/A REPORTED SMOKE IN CABIN WHEN ACFT PARKED AT THE GATE. INSPECTED ACFT FOUND NO DEFECTS WITH EXTERNAL DC POWER APPLIED TO ACFT. STARTED APU, BLEEDS OIL MIST AND SMOKE FILLED THE CABIN AND SELECTED APU OFF. GROUND RAN WITH ENGINE BLEEDS SELECTED INDIVIDUALLY, NO OIL OR SMOKE VISIBLE. R&R THE APU.

Part: WARN PANEL — FAULTY (COCKPIT)

SLIGHT SMELL OF BURNING WIRE INSULATION NOTED UPON ENGINE SHUT DOWN THAT LINGERS FOR 2 TO 3 MIN, THEN DISSIPATES. R&R CAUTION PANEL IAW 33-12-00 AFTER INSPECTING AREA OF SMELL. FOUND ODOR COMING FROM CAUTION PANEL, NO HIDDEN DAMAGE NOTED. ACFT OK FOR SERVICE.

Part: RELAY — INOPERATIVE (RUDDER) · airframe 33,635 hrs · 37,713 cycles

FIVE SECS AFTER TAKEOFF RUDDER FULL PRESSURE, NR 2 RUDDER HYD CAUTION LIGHT ILLUMINATED. BOTH NR 1 AND 2 HYD PRESSURE AND QTY REMAINED NORMAL. AIRCRAFT RETURNED TO FIELD. REMOVED AND REPLACED RELAY 2721-K1.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 33,533 hrs · 37,589 cycles

BAD VIBRATION FELT THROUGH NR 2 CONDITION LEVER WHEN NR 2 PROP RPM IS TRANSIENT. INSPECTION FOUND THAT TURBINE ASSEMBLY HAD EXCESSIVE RUBBING AGAINST CASING.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,873 hrs · 36,794 cycles

LAST TWO CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 32,273 hrs · 36,064 cycles

IN FLIGHT CHECKFIRE DETECT WARNING AND MASTER WARNING LIGHT ILLUMINATED ALONG WITH FAULT B ON NUMBER 2 ENGINE FIRE PROTECTION PANEL. INSP AND FOUND CIRCUIT BREAKER LABELED ENGINE NR 2 FIRE PROTECTION POPPED. RESET CIRCUIT BREAKER AND GROUND RAN AIRCRAFT WITH ALL ELECTRICAL BUSSES POWERED. OPS CHECK GOOD.

Part: FIRE DETECTOR — DEFECTIVE (NR 2 ENGINE) · airframe 32,273 hrs · 32,273 cycles

IN FLIGHT CHECK FIRE DETECT WARNING AND MASTER WARNING LIGHTS ILLUMINATED ALONG WITH NR 2 FAULT B ON FIRE PROTECTION PANEL. ALL ENGINE PARAMETERS WERE NORMAL. CIRCUIT BREAKER K8 ON LEFT ESSENTIAL BUSS FOUND POPPED. RESET CIRCUIT BREAKER AND FOUND, WHEN NR 2 SELECTED TO LOOP B ONLY LOOP TEST INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION UNIT AND REPAIRED CHAFED WIRES AT C/P'S 26113P3 AND P5. OPS CHECK GOOD IAW 26-11-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,190 hrs · 35,960 cycles

ELECTRICAL ODOR COMING FROM BEHIND THE COAT CLOSET. INSPECTED AREA BEHIND THE COAT CLOSET AND AVIONICS BAY RESULTING IN NO DEFECTS NOTED. GROUND RAN THE AIRCRAFT AND OPS CHECKED ALL SYSTEMS DURING 20 MIN RUN TIME. COULD NOT DUPLICATE.

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,036 hrs · 35,757 cycles

EMERGENCY LIGHT SYS FAILED OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 32,004 hrs · 35,717 cycles

PILOT REPORT ELECTRICAL SMELL IN COCKPIT. T/S TO CAUTION LIGHT PANEL. REMOVED AND REPLACED CAUTION PANEL. NO EMERGENCY DECLARED.

Part: DISPLAY — FADED (WEATHER RADAR) · airframe 31,861 hrs · 35,554 cycles

RADAR SCREEN FADED AND HARD TO READ. AFTER AIRCRAFT DEPARTED PHL, DISPATCH HAD ACFT RETURN TO FIELD, TO REPAIR RADAR. REMOVED AND REPLACED WEATHER RADAR SYSTEM. OPS CHECKS GOOD.

Part: STIFFENER — CRACKED (NACELLE) · airframe 31,106 hrs · 34,658 cycles

STIFFENER CRACKED ON TOP AFT NACELLE PANEL. REPLACED STIFFENER.

Part: LIGHT — BURNED (CABIN) · airframe 30,622 hrs · 35,422 cycles

STRONG ELECTRICAL SMELL IN CABIN ROW 4. REMOVED AND REPLACED OVERHEAD LIGHTING TUBE.

Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 30,409 hrs · 33,796 cycles

UNSCHEDULED PROP FEATHER NR 2 ENGINE IN FLIGHT. AT 800 FEET JUST BEFORE FLAP RETRACTION THE NR 2 ENGINE FEATHERED BY ITSELF. CAPTAIN SHUT DOWN ENGINE AND DECLARED AND EMERGENCY.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 27,094 hrs · 29,621 cycles

AFTER TAKEOFF, RADAR PAINTED SOLID RED LINE AT 10 MILES AND TILT HAD NO EFFECT THEN RADAR WENT TOTAL INOP. REMOVED AND REPLACED RECEIVER TRANSMITTER AND ANTENNA.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,245 hrs · 27,371 cycles

DURING C CHECK, FOUND FUSELAGE SKIN WITH FIVE DENTS IN SMALL AREA REQUIRING A MAJOR REPAIR. REPAIRED PER EO8-53-04-0693.

Part: ACM — FAILED (CABIN COOLING) · airframe 25,245 hrs · 27,371 cycles

AFTER TAKEOFF, CREW NOTED HOT BURNING SMELL IN ACFT, RET TO FIELD. INSPECTED AND GROUND RAN ACFT, NO BURNING SMELL OR DEFECT NOTED. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED, SUSPECT ODOR FROM ACM PACK HOT CAUTION LIGHT AND NOISY ACM NOTED DURING TAXI IN ON PREVIOUS FLIGHT. ACM WAS MEL'D FOR THAT DISCREPANCY.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 25,163 hrs · 27,277 cycles

WEATHER RADAR SPOKING & WOULD NOT PAINT WEATHER. WEATHER RADAR FAILED DURING FLT TO CLT. DIVERTED TO FAY DUE TO WEATHER IN CLT. REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 23,452 hrs · 25,205 cycles

FORWARD EXIT DOOR WARNING LIGHT ILLUMINATED IN-FLT. ADJUSTED PROX SENSOR GAP, OPS CHECK GOOD.