N333EN

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,977 hrs · 65,860 cycles

LEFT AFT EXTRIOR EMERGENCY LIGHT DIM. R & R THE BULB, OPS CHECKED GOOD.

Part: CONTACTOR — INOPERATIVE (APU) · airframe 54,566 hrs · 65,320 cycles

APU WOULD NOT SHUT OFF. SUSPECTED WELDED APU CONTACTOR. CREW NOTICED EXCESSIVE SMOKE FROM APU AND PULLED THE APU FIRE BOTTLE. R & R THE APU GENERATOR IAW CARD 24-30-02. R & R APU START CONTACTOR IAW STANDARD PRACTICES AND APU GCU IAW AMM 24-49-03 AS PRECAUTION. RAN AND SHUT DOWN APU SEVERAL TIMES WITH NO FAULTS.

Part: BOLT — SHEARED (MLG ACTUATOR MNT) · airframe 54,227 hrs · 64,939 cycles

DURING GEAR RETRACTION RIGHT GEAR UNSAFE LIGHT AND 3 AMBER INDICATIONS. PERFORMED CHECKLIST USING GEAR ALTERNATE EXTENSION. HYD PRESSURE AND QTY ARE NORMAL. INSPECTED THE NR 2 MLG. FOUND MLG RETRACT ACTUATOR FITTING ATTACH BOLTS SHEARED AT MAIN FRAME.

Part: RECEPTACLE — SMOKE (DC POWER) · airframe 54,167 hrs · 64,787 cycles

DC POWER EXTERNAL RECEPTACLE WAS SMOKING WITH GPU CONNECTED. SHUT-DOWN AND DISCONNECTED GPU. FACT: INSPECTED AND FOUND HEAT DAMAGE TO AFT PIN IN EXT.P POWER RECEPTICLE. AIRCRATF SYSTEM OPS NORMAL

Part: CONNECTOR — DIRTY (NR 2 GENERATOR) · airframe 53,037 hrs · 63,267 cycles

NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED DURING TAXI. CLEANED THE CONNECTOR PLUG. GROUND RAN ACFT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,983 hrs · 63,204 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 5. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (AC BUSS) · airframe 52,835 hrs · 63,012 cycles

RT AC BUSS CAUTION LIGHT ILLUMINATED INFLIGHT ALONG WITH THE ASSOCIATED CAUTION LIGHTS. CYCLED AC GENERATOR SWITCH. GROUND RAN AIRCRAFT C/N/D. AC SYSTEM OPERATES NORMAL. OK FOR SERVICE.

Part: BRUSH BLOCK — DAMAGED (PROPELLER HEAT) · airframe 52,794 hrs · 62,958 cycles

EMERGENCY LIGHT FLICKERED WITH PROP HEAT ON. RIGHT "A" PHASE. REMOVED AND REPLACED NR 2 PROP BRUSH BLOCK IAW MM 66-10-11. GROUND RAN AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,266 hrs · 62,817 cycles

STRONG ELECTRICAL ODOR IN CABIN AT ROWS 1 AND 2. COULD NOT DUPLICATE. GROUND RAN AIRCRAFT. TURNED ON ALL LIGHTS, RAN BLEED AIR, NO ODOR NOTED. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 52,666 hrs · 62,789 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 1DF. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,426 hrs · 62,499 cycles

FIRST EMERGENCY FLOOR LIGHT IS INOP. REMOVED AND REPLACED FIRST EMERGENCY LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,407 hrs · 62,477 cycles

FLOOR EMERGENCY LIGHT IS OUT AT ROW 3DF. REMOVED AND REPLACED BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,307 hrs · 62,345 cycles

4TH EMERGENCY FLOOR LIGHT FROM FRONT IS INOPERATIVE. R & R 4TH EMERGENCY FLOOR LIGHT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,060 hrs · 62,012 cycles

RIGHT AFT EMERGENCY EXIT SIGN DIM. R & R THE BULB.

Part: CABLE — MISSING (EMERGENCY LIGHT) · airframe 52,041 hrs · 61,991 cycles

MISSING ONE EMERGENCY LIGHT IN THE CABIN. INSTALLED EMERGENCY LIGHT CABLE ASSY.

Part: CONTACTOR — INOPERATIVE (APU) · airframe 520,009 hrs · 61,944 cycles

APU GENERATOR WARNING LIGHT REMAINS ILLUMINATED AFTER APU SHUTDOWN. APU GENERATOR LOAD SHOWS HIGH, SUSPECT WELDED CONTACTOR. R & R APU START CONTACTOR. APU GENERATOR WARNING LIGHT NO LONGER ILLUMINATED. UNABLE TO OPS CHECK DUE TO APU FAILING TO START.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 51,990 hrs · 61,922 cycles

7TH FROM LAST EMERGENCY LIGHT IS INOPERATIVE. TROUBLESHOT AND DETERMINED BULB TO BE DEFECTIVE. R & R BULB ON 7TH FROM LAST EMERGENCY FLOOR LIGHT. OPS CHECK GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,906 hrs · 61,818 cycles

EMERGENCY LIGHTS, 4TH RED LIGHT BULB OF FWD MOST SET OF RED FLOOR LIGHTS INOPERATIVE. REMOVED FWD MOST SECTION OF EMERGENCY FLOOR LIGHT COVER. R & R 4TH RED FLOOR LIGHT OF FWD MOST SET OF RED LIGHTS SECURED FLOOR LIGHTS COVER IN TRACK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,671 hrs · 61,513 cycles

RED EMERGENCY LIGHT AT ROW 13 INOPERATIVE. REPLACED THE LAMP AT ROW 13.

Part: FITTING — CRACKED (NR 2 NACELLE) · airframe 51,396 hrs · 61,153 cycles

NR 2 ENGINE HOSE COLLAR AFT FLANGE IS CRACKED IN 2 LOCATIONS, BOTH 1" LONG LOCATED 3.5" TO LT OF CENTER BOTH VERTICAL ROWS OF RIVETS. R & R RIVETS AND DAMAGED RADIUS IAW RD8-54-3774.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 51,261 hrs · 60,983 cycles

FORWARD RT EMERGENCY EXIT KNEE LIGHT IS DIM. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,103 hrs · 60,769 cycles

EMERGENCY ESCAPE PATH FLOOR LIGHT IS INOPERATIVE AT 7TH FROM FRONT, R & R. OPS CHECKED GOOD.

Part: UNKNOWN — LEAKING (NR 1 ENGINE) · airframe 50,971 hrs · 60,599 cycles

NR 1 ENGINE SUSPECTED FUEL LEAK. INSPECTED NR 1 ENGINE FOR FUEL LEAK. GROUND AN AIRCAFT. NO LEAK NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,835 hrs · 60,416 cycles

FORWARD 2 EMERGENCY ESCAPE PATH FLOOR LIGHTS ARE INOPERATIVE. R & R BULBS FOR FLOOR EMERGENCY ESCAPE PATH LIGHT, OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 50,835 hrs · 60,416 cycles

LEFT AFT EMERGENCY EGRESS LIGHT IS DIM. R & R AFT EMERGENCY EGRESS LIGHT, OPS CHECKED GOOD,

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,670 hrs · 58,844 cycles

FLOOR EXIT SIGN A PASSENGER DOOR AND 1DF ARE INOPERATIVE. R & R BULBS AT PASSENGER DOOR FLOOR EMERGENCY LIGHTS AND ROW 1DF. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,670 hrs · 58,844 cycles

EMERGENCY FLOOR LIGHT IS OUT AT ROW 10DF. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,355 hrs · 58,438 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 1. R & R BULB AT ROW 1 EMERGENCY FLOOR PATH LIGHT, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,024 hrs · 58,019 cycles

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

Part: UNKNOWN — ODOR (CABIN) · airframe 48,857 hrs · 57,798 cycles

STRONG ELECTRICAL ODOR COMING FROM CLOSET. INSPECTED WIRING AND COMPONENTS IN CLOSET UPPER AND LOWER AVIONICS RACKS AND BEHIND PILOT AND F/O. INSPECTED NOSE COMPARTMENT. NO FAULTS FOUND. GROUND RAN AIRCRAFT. ALL SYSTEMS OPERATED NORMAL. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,281 hrs · 57,042 cycles

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

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,330 hrs · 55,781 cycles

STRONG ODOR IN FLIGHT DECK, GROUND RAN ACFT, EXERCISED ACFT AND D/C POWER, NO ABNORMAL ODORS FOUND AT THIS TIME. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,118 hrs · 55,518 cycles

EMERGENCY LIGHT HAS A WIRE BROKEN. SPLICE WIRES IAW PPS 9.09 (5.7). OPS CHECKED GOOD.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 47,101 hrs · 55,492 cycles

CABIN OVERHEAD LIGHT AT 8 A/C INTERMITTENT WITH LIGHT ODOR. FOUND LT SOCKET DAMAGED. CABIN OVERHEAD LIGHTS DEACTIVATED CIRCUIT BREAKERS S1, S2 & R2. CABIN INTERIOR NORMAL LIGHTING SYSTEM, SPECIAL PROCEDURE 33.1 HAS BEEN COMPLIED WITH.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 46,659 hrs · 54,909 cycles

EMERGENCY SIDEWALL LIGHT IS INOPERATIVE AT ROW 11AC. R & R BULB. OPS CHECKED GOOD.

Part: INDICATOR — FAILED (TORQUE) · airframe 46,317 hrs · 54,471 cycles

TAKEOFF WARNING HORN SOUNDED AFTER TAKEOFF, 70 PERCENT TORQUE. ACFT CONFIGURED PROPERLY. R & R FAULTY SWITCH. OPS CHECKED GOOD. FAILED ENGINE RUN. R & R NR 1 TORQUE INDICATOR IAW AMM 77-1-5. OPS CHECKED GOOD WITH ENGINES RUNNING.

Part: SKIN — CORRODED (BS 593) · corrosion level 2 · airframe 46,313 hrs · 54,468 cycles

FUSELAGE SKIN INNER SIDE FOUND CORRODED UNDER FRAME. BLENDED SKIN ON WAFFLE IAW SRM 51-20-11. COMPLIED WITH HFEC INSPECTION. SKIN REPAIRED IAW EA15-2013-430.

Part: FRAME — CRACKED · airframe 46,313 hrs · 54,468 cycles

FLIGHT COMPARTMENT FRAME BRACKET IS CRACKED BETWEEN LOWER PILOTS WINDOW AND SIDE WINDOW. R & R FRAME BRACKET BETWEEN LOWER SIDE WINDOW AND PILOTS WINDSHIELD WITH NEW PARTS AND INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05 AND HI-LOKS IAW SRM 51-40-10.

Part: STRINGER — CORRODED (BS 582) · corrosion level 3 · airframe 46,313 hrs · 54,468 cycles

STRINGER 31S FOUND CORRODED. R & R WITH NEW IAW RD8-53-1312, RD8-51-015 AND SRM 51-42-05.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 46,184 hrs · 54,302 cycles

F/A REPORTS MILD ELECTRICAL ODOR IN CABIN OVERHEAD LIGHTS. DEACTIVATED BY PULLING AND COLLARED C/B SI,S2,R2 IAW S.P.33.1. R & R BULB HOLDER AND BALLAST ASSY IAW MM 20-45-07. OPS CHECKED GOOD. PERFORMED HIDDEN DAMAGE INSPECTION. NO DEFECTS NOTED IN SURROUNDING AREA AT THIS TIME.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,759 hrs · 53,749 cycles

NR 2 HYD QTY DROPPED TO .5 QUARTS FOLLOWED BY ISO VALVE CAUTION LIGHT. R & R DRAG STRUT ACTUATOR STARBOARD FLEX LINE. CLEANED AREA, SERVICED HYD, GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 45,724 hrs · 53,700 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF. R & R F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD IAW WC 33-50-03Q.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,135 hrs · 52,922 cycles

FORWARD RT TOP, LT AFT AND RT MOST AFT TOP EMERGENCY SIGNS ARE DIM. R & R BULBS IN EMERGENCY EXIT SIGNS. OPS CHECKED GOOD. RESECURED LENS.

Part: GCU — FAILED · airframe 44,984 hrs · 52,730 cycles

ACFT OUT OF POSITION DUE TO RT AC BUSS AND TRU CAUTION LIGHTS. MX REPLACED AC GCU AND AC GEN SWITCH. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 44,797 hrs · 52,495 cycles

CEILING EMERGENCY LIGHT AT ROW 10AC IS INOP. PARTIALLY LOWERED HEADLINER AT ROW 10AC. FOUND WIRE DISCONNECTED. RECONNECTED WIRE TO LIGHT AT 3351/P23. RESECURED HEADLINER AT ROW 10 AC. OPS CHECKED GOOD.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 44,753 hrs · 52,449 cycles

STRONG ELECTRICAL ODOR COMING FROM AROUND ROW 6. INSPECTED AND FOUND DAMAGED OVERHEAD LIGHT SOCKET AT ROW 8 AND 9DF. R & R SOCKET ASSY AT ROW 8 AND 9DF. OPS CHECKED GOOD.

Part: FIXTURE — BURNED (CABIN LIGHTS) · airframe 43,815 hrs · 51,226 cycles

CABIN O/H LIGHT AT 6D/F FWD FIXTURE END SMOKING. MX INSPECTED AND FOUND FWD END BURNED AND PULLED AND COLLARD CIRCUIT BREAKERS S1, S2, AND R2 PER SP 33.1.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,743 hrs · 51,130 cycles

ROW 7 CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED LENS, R & R BULB, AT SAID LOCATION. REINSTALLED LENS. OPS CHEKCED GOOD.

Part: SIGN — DISLODGED (CABIN) · airframe 43,641 hrs · 50,998 cycles

EMERGENCY EXIT SIGN ABOVE AIRSTAIR FALLING OFF. RESECURED. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 43,060 hrs · 50,232 cycles

FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. R & R BULB. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 42,845 hrs · 49,955 cycles

LOST HYD NR 2 SYS ISOLATION VALVE, CAUTION LIGHT ILLUMINATED, HAD TO PERFORM ALTERNATE EXTENSION OF GEAR. HYD PRESSURE APPEARED NORMAL. INSPECTED AND FOUND NR 2 QTY AT 1 QT. INSTALLED TEMP FLEX LINE FROM RESERVOIR TO TEE FITTING. OPS AND LEAKED CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 42,670 hrs · 49,745 cycles

CARGO SMOKE WARNING LIGHT ILLUMINATED DURING TAXI OUT. R & R BOTH FWD AND AFT BAG BAY SMOKE DETECTORS IAW AMM 26-12-01. OPS CHECKED IAW 26-12-00, OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 42,184 hrs · 49,156 cycles

WITH EITHER BLEED SELECTED ON, ACFT PRESSURIZED AND CABIN HEATS UP. VERFIED BOTH REAR OUTFLOW VALVES OPEN. GROUND RAN ACFT AND OPERATED NR 2 BLEED AND BOTH PACKS CHECKED GOOD, OK FOR SERVICE.

Part: SIGN — FAILED (CABIN) · airframe 40,796 hrs · 47,323 cycles

FWD EMERGENCY SIGN FAILED BETA LIGHT FUNCTION CHECK. R & R EMERGENCY SELF POWERED LIGHT.

Part: LIGHT — FAILED (CABIN) · airframe 40,296 hrs · 47,323 cycles

AFT RT EMERGENCY EXIT SIGN FAILED BETA LIGHT FUNCTION CHECK. R & R AFT RT EMERGENCY SELF POWERED LIGHT AND LENS.

Part: LIGHT — FAILED (CABIN) · airframe 40,796 hrs · 47,323 cycles

AFT LT EMERGENCY EXIT SIGN FAILED BETA LIGHT FUNCION CHECK. R & R EMERGENCY SELF POWERED LIGHT AND LENS.

Part: FRAME — CRACKED (BS 128.1 S25-26R) · airframe 40,794 hrs · 47,320 cycles

FRAME STA 128.1 CRACKED BETWEEN STRINGER 25R AND 26R. REPAIRED FRAME STATION 128.1 BETWEEN STRINGER 25R AND 26R IAW -8300 SRM 53-20-21, PAGE 2.

Part: PANEL — CRACKED (COCKPIT) · airframe 40,794 hrs · 47,320 cycles

COCKPIT ENTRANCE FLOOR CLOSE OUT PANEL CRACKED. REMOVED AND FABRACATED COCKPIT ENTRANCE CLOSE OUT PANEL IAW DWG 85311097. INSTALLED PANEL IAW -8300 SRM 51-40-11. PART MAKE OF 2024T3 .040, BATCH 37.

Part: ACCESS PANEL — CORRODED (FUSELAGE) · airframe 40,794 hrs · 47,320 cycles

CORROSION INSIDE PANEL 132AR. CORRODED PANEL REMOVED, NEW DOOR PANEL INSTALLED AS REQUIRED. ALL WORK DONE IAW SRM 51-40-07, 51-40-11. FINISH PAINT AS REQUIRED ON EXTERIOR SURFACE OF DOOR PANEL.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,794 hrs · 47,320 cycles

SERVICE DOOR SILL HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION FROM SERVICE DOOR SILL AROUND NUTPLATE HOLE IAW SRM 51-20-00. FOUND TO BE WITHIN LIMITS. ALODINE, PRIMED AND REPAINTED SERVICE DOOR SILL.

Part: SHAFT — CORRODED (FLAP CARRIAGE) · airframe 40,794 hrs · 47,320 cycles

RT NR 4 FLAP CARRIAGE HAS 3 WORN AND CORRODED MAIN ROLLER SHAFTS. R & R RT NR 4 FLAP CARRIAGE MAIN ROLLER SHAFT IAW -8300 AMM 57-50-43.

Part: CLAMP — CORRODED (DE ICE SYSTEM) · airframe 40,794 hrs · 47,320 cycles

ADEL CLAMP ON RT L/E DEICE LINE BETWEEN YW106.800 AND RT NACELLE IS CORRODED. R & R ADELL CLAMP ON RT L/E DEICE LINE BETWEEN YW106-800 AND RT HAND NACELLE.

Part: SHAFT — CORRODED (NR 5 SLAT) · airframe 40,794 hrs · 47,320 cycles

LEFT NR 5 FLAP CARRIAGE FWD AND AFT OTBD MAIN ROLLER SHAFT WORN AND CORRODED. R & R LT NR 5 FLAP CARRIAGE FWD AND AFT OTBD MAIN ROLLER SHAFT IAW -8300 AMM57-50-53.

Part: BUSHING — CORRODED (ROLLER SHAFT) · airframe 40,794 hrs · 47,320 cycles

RT NR 5 FLAP CARRIAGE UPPER DEAD WEIGHT ROLLER SHAFT BUSHING CORRODED. R & R RT NR 5 FLAP CARRIAGE DEAD WEIGHT ROLLER SHAFT BUSHING IAW -8300 AMM57-50-53.

Part: BOLT — CORRODED (FLAP CARRIAGE) · airframe 40,794 hrs · 47,380 cycles

RT NR 4 FLAP CARRIAGE HOOK ROLLER GUARD BOLT IS CORRODED. R & R NR 4 RT FLAP CARRIAGE HOOK ROLLER GUARD BOLT IAW -8300 AMM 57-50-43.

Part: STRUCTURE — CORRODED (SPOILER) · airframe 40,794 hrs · 47,320 cycles

HARDWARE FOR FLIGHT SPOILER POSITION INDICATOR LT OTBD SPOILER IS CORRODED. R & R HARDWARE ON LT OTBD FLGHT SPOILER POSITION INDICATOR.

Part: STRUCTURE — RUSTED (WINDSHIELD WIPER) · airframe 40,794 hrs · 47,320 cycles

CO-PILOTS WINDSHIELD WIPER HARDWARE RUSTED. R & R RUSTED HARDWARE AT CO-PILOTS WINDSHIELD WIPER IAW AMM30-42-00.

Part: SHAFT — CORRODED (TE FLAP CARRIAGE) · airframe 40,794 hrs · 47,320 cycles

LT NR 4 FLAP CARRIAGE HAS 3 MAIN ROLLER SHAFTS THAT ARE WORN AND CORRODED. R & R LT NR 4 FLAP CARRIAGE MAIN SHAFTS ISW -8300 AMM57-52-00.

Part: FLOORBOARD — CORRODED (GALLEY) · airframe 40,794 hrs · 47,320 cycles

AFT GALLEY FLOORBOARD HARDWARE CORRODED. R & R AFT GALLEY FLOORBOARD HARDWARE.

Part: BOLT — CORRODED (FLAP CARRIAGE) · airframe 40,794 hrs · 47,320 cycles

LT NR 4 FLAP CARRIAGE GUARD BOLT IS CORRODED. R & R LT NR4 FLAP CARRIAGE GUARD BOLT IAW -8300 AMM 57-50-43.

Part: CLAMP — CORRODED · airframe 40,794 hrs · 47,320 cycles

2 ADEL CLAMPS ON LT L/E DEICE LINE BETWEEN FUSELAGE AND NACELLE ARE CORRODED. R & R 2 ADEL CLAMPS,

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,794 hrs · 47,320 cycles

RT INBD SEAT RAIL HAS GOUGES, NICKS AND CORROSION. RT INBD SEAT TRACK REWORKED AND CORROSION REMOVED AS REQUIRED. SEAT TRACK REMAINING IS BEYOND LIMITS IAW RD8-53-784 AND RD8-53-4936. R & R ORIGINAL SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-07, 51-40-10, AND 51-42-05.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 40,380 hrs · 46,777 cycles

EMERGENCY FLOOR LIGHT AT ROW 10DF INOP. R & R BULB IN EMERGENCY FLOOR LIGHT AT ROW 10DF, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 6) · airframe 40,007 hrs · 46,293 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 6 IS INOP. R & R ROW 6 EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 39,461 hrs · 45,576 cycles

FORE RUDDER ON LT TOP SIDE HAS AN AREA OF IMPACT DAMAGE. REPAIRED IAW EO8-55-10-0379.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 39,308 hrs · 45,394 cycles

EMERGENCY EGRESS LIGHT IN ROW 8. REPOSITIONED LIGHT ASSY INTO MODULE. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,784 hrs · 44,762 cycles

RT EMERGENCY EXIT LOWER SIDEWALL LIGHT BULB IS INOP. R & R RT AFT EMERGENCY EXIT LOWER SIDEWALL LIGHT BULBS AS REQUIRED.

Part: SWITCH — SPARKS (AIRSTAIR LIGHT) · airframe 38,665 hrs · 44,604 cycles

AIR STAIR DOOR LIGHT SWITCH SPARKS WHEN PRESSED. R & R AIR STAIR DOOR SWITCH AND TESTED IAW MM 33-20-00. RESET CIRCUIT BREAKER, SYS TESTED WELL.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 38,010 hrs · 43,797 cycles

DURING RON INSP, A FLOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REMOVED AND REPLACE AND THE OPS CHECK WAS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 380,010 hrs · 43,797 cycles

LT EMERGENCY LIGHT IS INOPERATIVE. R & R LT FWD EMERGENCY LIGHT BULB, OPS CKD GOOD.

Part: BETA SWITCH — FAILED (NR 2 ENGINE) · airframe 37,977 hrs · 43,756 cycles

NR 2 ENG TORQUE SURGED APPROX 30 PERCENT RANGE JUST AFTER TAKEOFF. AFTER TAKEOFF NR 2 ENGINE TORQUE SURGED TO APPROX 119 PERCENT AND PROP SURGED TO APPROX 1000 RPM. ACFT AT 100 AGL AND CLEARED UP AFTER LANDING. REACTIVATED BETA LOCKOUT SYS. R & R NR 2 ENG BETA SWITCH IAW STANDARD PRACTICE. PERFORMED BETA LOGIC, OPERATES CKD GOOD. CLEAR MEL.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 37,099 hrs · 42,631 cycles

PILOT REPORTED A BURNING SMELL IN COCKPIT, STATED THAT IT WAS POSSIBLY COMING FROM THE CAPT 802 PANEL. MAINTENANCE REMOVED AND REPLACED 802 ADVISORY PANEL, INSPECTED, AND DRIED OUT AREA. OPERATIONAL CHECK WAS GOOD IAW DASH-8 MM 22-10-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,805 hrs · 42,269 cycles

UPON INSPECTION AT SBY, AIRCRAFT N333EN WAS FOUND TO HAVE AN EMERGENCY LIGHT INOPERATIVE. THE EMERGENCY LIGHT BULB WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 36,790 hrs · 42,253 cycles

UPON INSP, IT WAS FOUND THAT AN EMERGENCY LIGHT WAS INOPERATIVE. LIGHT BULB WAS REPLACED AND THE OPS CHECK WAS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 33,767 hrs · 42,225 cycles

UPON INSP, IT WAS FOUND THAT AN EMERGENCY LIGHT WAS INOPERATIVE. THE BULB ON THE EMERGENCY LIGHT WAS REMOVED AND REPLACED. OPS CHECK GOOD.

Part: AHRS — FAILED (NR 1)

IN FLIGHT CAPTAIN AUTOMATIC DIRECTION INDICATOR PITCH UP ALONG WITH ATTITUDE HEADING AND REFERENCE SYSTEM DATA INVALID MSG ON 802 PANEL ALSO CAPTAIN HORIZONTAL SITUATION INDICATOR AND FIRST OFFICER RADIO MAGNETIC INDICATOR DISPLAYED ERRONEOUS INFORMATION. R&R NR 1 ATTITUDE HEADING AND REFERENCE SYSTEM IAW 34-21-01 OPS CHECK GOOD.

Part: FILTER ELEMENT — CLOGGED (NR 2 ENGINE) · airframe 35,516 hrs · 40,658 cycles

ON TAKEOFF ROLL NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED. ABORTED TAKEOFF. REMOVED, INSPECTED & REPLACED HP & LP FUEL FILTER REF (WORK) CARD 73-10-02R AND 73-10-04R AND MAINT MANUAL 72-00-01 AND REPLACED HP FILTER BYPASS SWITCH REF P&W MAINT, RUNUP CHECKS GOOD.

Part: SWITCH — DEFECTIVE (COCKPIT)

AT AN ALTITUDE OF APPROXIMATELY 100 FEET AND AFTER THE LANDING GEAR WAS SELECTED UP, THE NR 1 ENGINE BETA LOCKOUT FAILED. PROP SPEED DROPPED TO 990 RPM AND FLUCTUATED UP TO 1080 RPM. THE EMERGENCY CHECKLIST WAS PERFORMED AND THE ACFT WAS RETURNED TO THE ORIGINATING FIELD. AN EMERGENCY WAS NOT DECLARED. WHILE TRYING TO DEACTIVATE THE BETA SYSTEM, THE PROP WOULD STILL CYCLE IN AND OUT OF BETA RANGE. MX TROUBLESHOOTING DISCOVERED THE POWER LEVER MICRO-SWITCH 6141-S3 TO BE DEFECTIVE. THE SWITCH WAS CHANGED AND SYSTEM RE-ACTIVATED. THE SYSTEM WAS THEN OPS CHECKED WITH APPLICABLE WORKCARD AND CHECKED GOOD. ACFT WAS THEN RELEASED FOR SERVICE.

Part: WINDSCREEN — CRACKED (COCKPIT)

F/O WINDSCREEN DEVELOPED CRACKS AFTER DEPARTURE. REMOVED AND REPLACED F/O WINDSCREEN. (K)

Part: COFFEEMAKER — BURNED (GALLEY)

HOT JUG IN WARMER NR 1 HAS BURNING SMELL. REPLACED HOT JUG. FOUND ONE BURNED PIN IN OLD JUG. (K)-

Part: WIRE — BROKEN (EMERGENCY LIGHT)

ROW 11AC EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN GROUND WIRE AS REQUIRED, OPS CHECK GOOD. (A)

Part: MOUNT — BROKEN (NR 1 ENGINE) · airframe 34,530 hrs · 39,388 cycles

NR 1 ENGINE AFT OUTBOARD STRUT MOUNT FOUND TO BROKEN. INSP GENERATED BY INSPECTION CARD 71-20-03.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 34,431 hrs · 39,268 cycles

ELEVATOR TRIM IS DIFFICULT TO MOVE AND TRAVEL IS LIMITED. REMOVED AND REPLACED ELEVATOR TRIM SERVO. OPS CHECK GOOD IAW -8 MM.

Part: ENGINE — MAKING METAL (NR 1) · airframe 34,244 hrs · 39,035 cycles

NR 1 ENGINE FAILED INFLIGHT. CREW WAS FLYING ALONG AT 9000 FT ABOUT 5 MILES WEST OF CLT WHEN NR 1 ENGINE SHUT ITSELF DOWN. THE CREW FEATHERED THE ENGINE AND DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PULLED THE FDR AND WILL SHIP TO ROA. MAINTENANCE INSPECTED THE ENGINE, PULLED THE STARTER AND SPUN THE ENGINE BY HAND AND THE ENGINE WAS MAKING NOISE. MAINTENANCE THEN PULLED NL PROBE AND FOUND THE NL PROBE PACKED WITH METAL. MORE INFORMATION TO FOLLOW.

Part: GCU — HOT (NR 2 ENGINE) · airframe 33,878 hrs · 38,582 cycles

AN "ELECTRICAL SMELL" IN FLIGHT DECK ON F/O SIDE, FOUND NR 2 ENG GCU HOT. REPLACED GCU, OPS CHECK GOOD, "ELECTRICAL SMELL GONE", HIDDEN DAMAGE INSP C/W.

Part: MASTER CAUTION — UNKNOWN (COCKPIT) · airframe 33,405 hrs · 38,023 cycles

DURING CREW SWAP IN CLT, ARRIVING CREW FOUND A FISH ODOR IN COCKPIT AREA. MAINTENANCE CHECKED OVERHEAD PANELS IN COCKPIT. SLIGHT ODOR WAS NOTICED COMING FROM MASTER CAUTION PANEL. REMOVED AND REPLACED CAUTION PANEL AND OPS CHECKED GOOD PER AMM 33-12-01. SMELL DISSIPATED AFTERWARDS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 32,934 hrs · 37,445 cycles

AFTER TAKEOFF CYCLED GEAR UP, LEFT MAIN GEAR DOOR AMBER LIGHT ILLUMINATED (DOORS REMAINED OPEN). LANDING GEAR INOP CAUTION LIGHT ILLUMINATED, PERFORMED ALT EXTENSION PROCEDURES. INSPECTED LT MAIN GEAR PROX SENSORS FOR DEFECTS AND PROPER GAPS, GEAR AND GEAR DOOR SENSORS CHECK GOOD IAW MM 32-10-00. JACKED A/C, SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. REMOVED AND REPLACED PSEU AS PRECAUTIONARY, OPS CHECK GOOD.

Part: DISK — BURST (DITCHING DAM) · airframe 32,678 hrs · 37,133 cycles

LEFT DITCHING DAM PRESSURE READS ZERO PSI. FOUND DISK BURST BUT DITCHING DAM DID NOT DEPLOY. REMOVED AND REPLACED DITCHING DAM DISK, BOTTLE AND BAG PER W/C 25-60-10R AND W/C 25-60-07R PARTS REPLACED - BURST DISK ADAPTER P/N A 68641, NITRO CLYLINDER P/N 410870-3, S/N 450, DITCHING DAM P/N 4MAN25-10, S/N F2548.

Part: CYLINDER — CORRODED (NLG) · airframe 32,398 hrs · 36,792 cycles

NLG INNER CYLINDER LOWER BORE CORRODED. REMOVED AND REPLACED NLG INNER CYLINDER WITH NEW BEARING AND THRUST SET 8821-1 IAW CMM 32-20-01 NLG STRUT S/N DCL291/90.

Part: GENERATOR — LIGHTNING STRIKE (LT & RT) · airframe 31,998 hrs · 36,301 cycles

LIGHTNING STRIKE DURING CLIMB & LOST BOTH DC GENS. C/W LIGHTNING STRIKE INSP W/C. NO DEFECTS NOTED AT THIS TIME. STARTER/GEN P/N: 23088-008, S/N-POS 1:788, POS 2:1159. NO GENERATOR CHANGED.

Part: TRANSMITTER — FALSE INDICATION (ENG OIL PRESSURE) · airframe 27,711 hrs · 30,917 cycles

NR 2 ENGINE OIL PRESSURE WENT TO ZERO PSI AND THEN WENT TO 40 PSI WITH NO OIL PRESSURE LIGHT AFTER TAKEOFF. REMOVED AND REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER.

Part: BOTTLE — LEAKING (SLIDE/RAFT) · airframe 26,736 hrs · 29,687 cycles

DURING LAYOVER DITCHING DAM RT EMERGENCY EXIT DOOR WATER DAM WAS ACTIVATED BUT DID NOT DEPLOY. DURING LAYOVER F/A ATTEMPTED TO OPEN EXIT DOOR TO VENT A/C. F/A HERD A HISSING NOISE AND STOPPED REMOVING DOOR. FOUND HISSING NOISE TO BE NITROGEN FROM DITCHING DAM BOTTLE. SERVICED BOTTLE, OPS CHECKED DITCHING DAM SYSTEM NO DISCREPANCY NOTED AND THEN SERVICED AND REACTIVATED SYSTEM.

Part: PROPELLER (#1 PROP) · airframe 22,747 hrs · 24,647 cycles

NUMBER 1 PROPELLER DUE TO POSSIBLE OVR TORQUE CONDITION. REMOVED AND INSPECTED PROP AND REINSTALLED.

Part: BOTTLE — LEAKING (CABIN) · airframe 22,004 hrs · 23,673 cycles

RIGHT HAND DITCHING DAM PREESURE AT 1200 PSI. DITCHING DAM REMOVED AND PUR IN BAG BIN. REPLACED DITCHING DAM NITROGEN BOTTLE AND REINSTALLED DITCHING DAM.