N336EN

Part: PROXIMITY SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 57,136 hrs · 67,832 cycles

SERVICE DOOR OPEN INDICATION ILLUMINATED SHORTLY AFTER TAKEOFF ROLL WAS INITIATED. ADJUSTED AND TESTED THE SERVICE DOOR PROXIMITY SENSOR IAW MM 52-70-00, OPS CHECKED GOOD.

Part: STALL WARNING — FALSE ACTIVATION (NR 2) · airframe 57,004 hrs · 67,677 cycles

NR 2 STALL SYSTEM FAIL AND PUSHER SYSTEM FAILED. CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL. CYCLED SWSP COMP CIRCUIT BREAKERS, STALL SYSTEM 1 AND 2 TESTED NORMALLY.

Part: CONTROLLER — FAILED (AUTOFLIGHT) · airframe 56,320 hrs · 66,792 cycles

AFCS CONTROLLER INOPERATIVE MESSAGE ON 802 PANEL. R & R AFCS CONTROLLER IAW AMM 22-10-01. OPS CHECKED BAD.

Part: PROPELLER — VIBRATION (RIGHT) · airframe 56,157 hrs · 66,564 cycles

MODERATE VIBRATION FROM THE RT PROPELLER. CONSTANT AND WORSENS WITH PROPELLER SPEED CHANGES. R & R THE NR 200 PROPELLER ASSY IAW CARD 61-10-06R, RAN ACFT IAW MOM. OPS CHECKED GOOD NO DEFECTS AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 56,072 hrs · 66,446 cycles

REJECTED TAKE OFF. AUTOFEATHER FAILED TO ARM DURING TAKEOFF. TORQUE WAS AT 88%. R & R THE NR 2 TSCU IAW IAW MM 72-01-10. RAN AIRCRAFT, OPS CHECKED GOOD IAW PDT-8 RUN MANUAL AND W/C 61-21-04Q.

Part: CIRCUIT BREAKER — MALFUNCTIONED (AUTOFEATHER) · airframe 56,055 hrs · 66,420 cycles

REJECTED TAKEOFF AT 88 PERCENT TORQUE. AUTOFEATHER WOULD NOT ARM. RETURNED TO GATE. R & R THE RT TORQUE CONDITIONING CIRCUIT BREAKERS. RAN ENGINES IAW MANUAL CHECKING AUTOFEATHER. PERFORMED AUTOFEATHER STATIC CHECK MULTIPLE TIMES. AUTOFEATHER ARMS AT 60 PERCENT TORQUE AND REMAINS THROUGHOUT THE CHECK. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (NR 1 STRUT) · airframe 56,054 hrs · 66,418 cycles

ABORTED TAKEOFF DUE TO AUTOFEATHER WOULD NOT ARM. COMPLIED WITH FLIGHT CREW PROCEDURES. REMOVED AND RANG OUT THE NR 2 ENGINE STRUT HARNESS AND REINSTALLED . CHECKED GOOD IAW PDT -8 RUN MANUALS. R & R THE NR 1 ENGINE STRUT HARNESS IAW MM 72-01-10.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 56,050 hrs · 66,415 cycles

AUTO FEATHER FAILED TO ARM AT 65 KTS. REJECTED T/O AND RETURNED TO THE GATE. R & R THE NR 1 ENGINE, COMPLIED WITH AUTO FEATHER AND AUX FEATHER RUNS, IAW SRT MANUAL, OPS CHECKED GOOD.

Part: ACTUATOR — FAILED · airframe 56,036 hrs · 66,401 cycles

AUTO FX WOULD NOT ARM. ABORTED TAKE OFF. R & R ACTUATORS FOR 6121-S10,11 FOR BEING FLAT SPOTTED. R & R CIRCUIT BREAKERS FOR LT G-10 & RT G10. CHECKED AUTO FX POWER LVR POTS FOR SERVICEABILITY, CHECKED GOOD. AUTO FX ARMING & STATIC TESTS GOOD IAW SRT MANUAL.

Part: POTENTIOMETER — OUT OF RIG (AUTO FEATER) · airframe 55,966 hrs · 66,309 cycles

REJECTED TAKE-OFF DUE TO A/F ARM LIGHT NOT ON 90 PERCENT TQ. FACT: CHECK AUTO-FEATHER ARMING POTENTIOMETER USING B.O.B AND FOUND TO BE OUT OF RIGGED. RE-RIGGED POTENTIOMETER USING PSM1-83-2ERNO.ER23. RAN ENGINES AND PERFORMED AUTOFX SYSTEM CHECK AS PER DASH 8 SRT OPERATING MANUAL. OPS CHECK GOOD, OK FOR SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 5,566 hrs · 66,309 cycles

AUTOFEATHER WOULD NOT ARM AT 90 PERCENT TQ. ABORTED TAKEOFF.

Part: SWITCH — DIRTY (AUTO FEATHER) · airframe 55,949 hrs · 66,285 cycles

AUTO FEATHER FAILS TO ARM, RETURNED TO GATE. CLEANED THE SWITCHES 6121S6-611. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED (NR 1) · airframe 55,958 hrs · 66,299 cycles

REJECTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING UP TO 90% TORQUE. R & R THE NR 1 TSEU. GROUND RAN ACFT. AUTO-FEATHER SYSTEM OPS NORMAL IAW RUNUP MANUAL,. OK FOR SERVICE AT THIS TIME.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 55,953 hrs · 66,292 cycles

TAKEOFF REJECTED WITH TORQUE SET AT APPROXIMATELY 85 PERCENT DUE TO AUTO FEATHER NOT ARMING. RAN AIRCRAFT AND CHECKED OPERATION OF AUTO FEATHER IAW MANUAL AND AUTO FEATHER ARMED AT 53 PERCENT.NO DEFECTS NOTED.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 55,953 hrs · 66,292 cycles

TAKEOFF REJECTED WITH TORQUE SET AT APPROX. 85 PERCENT DUE TO AUTO FEATHER NOT ARMING. RAN AIRCRAFT AND CHECKED OPERATION OF AUTO FEATHER IAW MANUAL AND AUTO FEATHER ARMED AT 53 PERCENT. NO DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2 PROPELLER) · airframe 55,862 hrs · 66,169 cycles

AUTOFEATHER FAILED TO ARM AT 86% TQ, REJECTED TAKE OFF. R & R THE NR 2 ENG TSCU AND RELAY 6121K5 IAW 72-01-10 AND OPS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (STANDBY HYD) · airframe 55,677 hrs · 65,928 cycles

NR 1 STANBY PUMP WILL NOT COME ON. RESET THE CIRCUIT BREAKER. OPS NORMAL. NO DEFECTS. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SERVICE DOOR) · airframe 55,542 hrs · 65,748 cycles

DURING TAKEOFF ROLL, MASTER WARNING LIGHT ILLUMINATED INDICATING SERVICE DOOR WAS NOT CLOSED. INSPECTED THE SERVICE DOOR, NO DEFECTS NOTED. OK FOR SERVICE

Part: RADAR — FAILED · airframe 55,158 hrs · 65,238 cycles

RADAR FAILED IN FLIGHT. R & R RADAR RIGHT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 55,086 hrs · 65,138 cycles

DURING GEAR RETRACTION GEAR DID NOT RETRACT. THREE AMBER AND RED LIGHTS ON BOTH MAINS. PERFORMED ALTERNATE EXTENSION GEAR DOWN AND LOCKED. SWUNG GEAR MULTIPLE TIMES. SYSTEM OPS NORMAL, OK RETURN TO SERVICE

Part: PANEL — MALFUNCTIONED (ENGINE) · airframe 54,566 hrs · 64,473 cycles

1 AND 2 ENGINES HAD 15 PERCENT TORQUE SURGES AT 400 FEET ALTITUDE. REACHED 105 PERCENT TORQUE. REDUCED TORQUE TO 4 PERCENT. SURGE STOPPED. RETURNED TO FIELD. REMOVED AND REPLACED THE RELAY PANEL AT THE CAPTAIN`S SIDE CONSOLE. GROUND RAN AIRCRAFT FOR BETA BACKUP TEST WITH LOCKOUT SYSTEM. OPS CHECKED GOOD.

Part: PANEL — MALFUNCTIONED (ENGINE TORQUE) · airframe 54,567 hrs · 64,473 cycles

NR 1 AND 2 ENGINES HAD 15 PERCENT TORQUE SURGES AT 400 FT.ALTITUDE. REACHED 105 PERCENT TORQUE. REDUCED TORQUE TO 45 PERCENT. SURGING STOPPED. RETURNED TO FIELD. R & R THE RELAY PANEL AT CAPTAIN`S SIDE CONSOLE. GROUND RAN THE AIRCRAFT FOR BETA BACKUP TEST WITH LOCKOUT SYSTEM MELD. SRT MANUAL OPS CHECK GOOD.

Part: BULB — INOPERATIVE (INOPERATIVE) · airframe 54,556 hrs · 64,460 cycles

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

Part: APU — FAILED · airframe 54,548 hrs · 64,452 cycles

APU FAILED AFTER 20 MINUTES RUNNING TIME WITH BLEEDS OPEN AND CABIN PACK RUNNING.TRIGGERED CHECK FIRE DETECT WARNING LIGHT. AFTER SHUTDOWN. INSPECTED APU COMPARTMENT. NO DAMAGE FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,471 hrs · 64,304 cycles

EMERGENCY LIGHTS AT RIGHT AFT SIDE OF FUSELAGE, CENTER AISLE EXIT SIGN AT ROW 11, AND CENTER OVERHEAD LIGHTS AT ROW 9 AND 13 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW 33-50-05. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,471 hrs · 64,354 cycles

DIM EMERGENCY LIGHT ON RIGHT AFT SIDE OF FUSELAGE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: APU — ODOR · airframe 54,294 hrs · 64,136 cycles

BURNED OIL ODOR IN CABIN AND FLIGHT DECK WHEN USING APU BLEEDS. GROUND RAN AIRCRAFT AND CONFIRMED OIL IN APU BLEEDS. GOES AWAY WITH ENGINE BLEEDS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,200 hrs · 64,014 cycles

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

Part: HYDRAULIC LINE — LEAKING (MLG) · airframe 53,603 hrs · 63,259 cycles

NR 2 HYD QTY WENT TO ZERO AFTER STARTUP. NR 2 NACELLE WET AROUND BRAKES. BOTH ENGINES SHUTDOWN IN LESS THAN A MINUTE. NR 2 HYD QTY IN NACELLE APPEARS TO BE ZERO. VERIFIED BOTH HYD SYSTEMS SERVICED. R & R NR 3 BRAKE FLEX HOSE AS REQUIRED. LEAK CHECK GOOD. BLED NR 3 BRAKE. OK FOR SERVICE.

Part: MONITOR — DEFECTIVE (ELECTRICAL SYS) · airframe 53,603 hrs · 63,259 cycles

WHEN APU SHUTS DOWN A NEGATIVE LOAD DISPLAYED. NO, HAD TO RETURN TO GATE, CX'D AFTER HEA. RING SUSPECTED CONTACTOR WELDED, LATE ACFT. VERIFIED APU GEN CONTACTOR IS NOT WELDED. R & R DC POWER MONITOR IAW -8MM 24-31-05. OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — DIM (CABIN) · airframe 53,348 hrs · 62,910 cycles

LEFT AFT EMERGENCY EXIT DOOR LIGHT DIM. R & R LIGHT .

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,348 hrs · 62,910 cycles

7DF FLOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,873 hrs · 62,265 cycles

BURNING ODOR IN CABIN AFTER APPLYING POWER TO ACFT. NO, MELD APU BLEED, RAN APU WITH AND WITHOUT BLEEDS ON. INSPECTED APU BLEED DUCTS AND ACM AND HEAT EXCHANGER, NO DEFECTS FOUND NO ODOR NOTED AT THIS TIME. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,830 hrs · 60,890 cycles

AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE ON RT SIDE. R & R EMERGENCY LIGHT BATTERIES IAW WORD CARD 33-50-05R.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,830 hrs · 60,890 cycles

FORWARD LT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R PS1 EMERGENCY LIGHT BASE POWER SUPPLY IAW MM 33-51-05.

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG DOOR) · airframe 51,729 hrs · 60,752 cycles

LEVELING OFF A 10,000 FEE, NLG AMBER DOOR LIGHT ILLUMINATED ALONG WITH UNSAFE INDICATION AND NOISE FROM NLG AREA. INDICATION CLEARED AND REMAINED NORMAL FOR REST OF FLIGHT. JACKED AIRCRAFT, SWUNG GEAR. COULD NOT DUPLICATE PROBLEM. R & R MECHANICAL SEQUENCE VALVE IAW MM 32-20-31. OPS AND LEAKED CHECKED GOOD AT THIS TIME.

Part: AUDIO PANEL — FAILED (CABIN) · airframe 51,499 hrs · 60,455 cycles

ODOR AND SMOKE IN FLIGHT IN FRONT PART OF CABIN. EMERGENCY CALL LIGHT FLICKERED AND WAS STUCK. INSPECTED AND FOUND FWD. F/A INTERPHONE CONTROL PANEL WITH FAILED CALL SWITCH. R & R D CONTROL PANEL IAW AMM 23-40-02. OPS CHECK GOOD. PERFORMED HIDDEN DAMAGE INSPECTION. NO DEFECTS FOUND. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,117 hrs · 59,929 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 50,947 hrs · 59,711 cycles

UPPER EMERGENCY F/A SIDEWALL IS BROKEN. REMOVED SHIELD, REPLACED EMERGENCY LIGHT AND REINSTALLED HARDWARE AS REQUIRED. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 50,619 hrs · 59,297 cycles

FLOOR EMERGENCY LIGHTS WILL NOT CYCLE OFF, AFTER ACFT POWERED DOWN. STARTED APU, CYCLED EMERGENCY LIGHT SWITCH ON AND OFF. LIGHTS WENT OFF. OPERATING NORMAL AT THIS TIME.

Part: CDU — FAILED (DISPLAY) · airframe 50,562 hrs · 59,222 cycles

UNS SCREEN WENT BLANK ASSOCIATED WITH ELECTRICAL ODOR. R & R UNS1C CDU IAW MM 34-61-30. UNS SYS OPS CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 50,388 hrs · 58,999 cycles

EMERGENCY LIGHT ABOVE UNDER WING EXIT TURNED ON IN FLIGHT. TURNED OFF 3 MINUTES PRIOR TO LANDING. R & R LIGHT POWER SUPPLY AND BATTERY AT 3351-PS3 IAW 33-51-05. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,901 hrs · 58,362 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 9. R & R BULB, OPS CHECKED GOOD.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 49,901 hrs · 58,362 cycles

WEATHER RADAR DOES NOT PAINT KNOWN WEATHER. R & R RADAR RT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,842 hrs · 58,279 cycles

VARIOUS EMERGENCY LIGHTS ARE OUT ON EXIT SIGNS. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,111 hrs · 57,300 cycles

EMERGENCY LIGHT CENTER CEILING IS INOPERATIVE IN ROW 10. R & R BULB0. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 48,858 hrs · 56,977 cycles

SMOKE DETECTOR LIGHT CAME ON AND REMAINS ILLUMINATED. CREW CHECKED CARGO BAY AND NO SMOKE FOUND. WHILE TAKING RIGHT UP FROM THE CREW - THE LIGHT EXTINGUISHED ON ITS OWN & NR 2 WILL NOT TEST. R & R NR 2 CARGO BAY SMOKE DETECTOR, TEST GOOD, OK FOR SERVICE. SEE ITEM 3 FOR MEL ON NR 1 DETECTOR.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 48,717 hrs · 56,817 cycles

OVERHEAD EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 10. REMOVED LENS, R & R BULB. REINSTALLED LENS. OPS CHECKED GOOD.

Part: AHRS — MALFUNCTIONED (NR 2) · airframe 48,310 hrs · 56,310 cycles

DURING TAXI OUT, NR 2 AHRS DISPLAYED PITCH AND ROLL MISMATCH WITH AHRS DATA INVALID ON 802 PANEL. ADI ROLLED 60 DEGREES AND PITCHED 60 DEGREES UP AND DOWN. R & R NR 2 AHRS IAW 34-20-01. OPS CHECKED GOOD. OK FOR SERVICE. R & R F/O ADI IAW 34-27-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PUMP — LEAKING (FUEL SYS) · airframe 47,218 hrs · 54,932 cycles

ON CLIMB OUT, CREW NOTED LEFT FUEL PUMP ADVISORY LIGHT WAS ILLUMINATED AFTER SELECTING TO OFF. CREW THEN NOTED FUEL VENTING AT LEFT WING NACA SCOOP. LEFT AUX PUMP LIGHT SELF EXTINGUISHED AFTER APPROX 4-5 MINUTES. RETURN TO FIELD. LEFT TANK READS 200 POUND LESS THAN RIGHT TANK. NO LEAKS ON TAXI IN. R & R MFC AND FUEL PUMP ASSY. OPS AND LEAK CHECKED GOOD.

Part: SOLENOID VALVE — LEAKING (FUEL) · airframe 47,209 hrs · 54,915 cycles

CREW NOTICED FUEL LEAKING OUT OF LT WING NACA SCOOPS. SHUTDOWN ENGINE. REMOVED FUEL LID PANELS 524AT AND 524CT. INSPECTED AUX PUMP CHECK VALVE. NO PROBLEM. R & R SOLENOID ARMING VALVE IAW MM 28-25-21. OPS CHECKED FUEL TRANSFER SYS. OPS AND LEAKED CHECKED GOOD. REINSTALLED BOTH FUEL LID PANELS 524AT AND 524CT.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 47,193 hrs · 54,895 cycles

NR 1 FUEL AUX PUMP ADVISORY LIGHT ILLUMINATED APPROX 5 MINUTES. THEN SELF EXTINGUISHED. NR 1 FUEL QTY READ 250 LBS. LOWER THAN NR 2 GAGE. F/A REPORTS FUEL ODOR IN CABIN RESULTING IN NR 1 ENGINE BEING SHUTDOWN BY CREW PRIOR TO APPROACH. FUEL QUANTITIES WERE NR 1 2250 AND NR 2 2500 LBS. GROUND RAN ACFT AND OPS CHECKED OF FUEL TRANSFER AND AUX PUMPS IAW MM 28-23-00. CHECKED NORMAL WITH OUT ANY DEFECTS OR ANY ADVISORY LIGHT MALFUNCTION. NO FUEL ODOR NOTED IN CABIN. (CREW AND MX REPORTS NO LEAKS.)

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,001 hrs · 54,649 cycles

EMERGENCY EXIT SIGNS AT MID CABIN ILLUMINATED/FLICKERED IN FLIGHT. REPLACED EMERGENCY LIGHT CONTROL BOX 3351J1. CHECKED BLOCKING DIODES IAW33-50-06 PERFORMED OPS CHECK IAW W/C 33-50-06, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 46,882 hrs · 54,501 cycles

INOPERATIVE LIGHT FOR NORMAL GREEN ON F/A EMERGENCY LIGHT BUTTON. R & R BULB FOR NORMAL GREEN LIGHT ON F/A EMERGENCY LIGHT BUTTON

Part: ACTUATOR — FAILED (NR 2 MLG) · airframe 46,779 hrs · 54,362 cycles

AFTER TAKE OFF, ALL THREE RED GEAR LIGHTS REMAINED ON. PERFORMED ALTERNATE EXTENSION AND RETURNED TO FIELD. R & R NR 2 MLG RETRACTION ACTUATOR IAW AMM 32-30-01. OPS AND LEAK CHECK GOOD.

Part: STRIP — CORRODED (RT NACELLE) · corrosion level 2 · airframe 45,598 hrs · 54,133 cycles

RIGHT NACELLE REAR CONE, TOP ALUMINUM STRIP IS CORRODED. R & R WITH FABRICATED PART IAW SRM 51-40-00.

Part: STRAP — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 45,596 hrs · 54,133 cycles

FLOOR PANEL STRAP ASSY IS CORRODED. R & R STRAP ASSY ON FLOOR PANEL IAW AMM 20-14-01.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 45,596 hrs · 54,133 cycles

FLOOR PANEL IS CORRODED AND DISBONDED. REPLACED FLOOR PANEL IAW AMM 53-01-01.

Part: SKIN — CORRODED (RT WING) · airframe 45,598 hrs · 54,133 cycles

RIGHT WING UPPER SKIN HAS THREE CORRODED LOCK FASTENERS AT STA YW138. R & R IAW SRM 51-40-10.

Part: SKIN — CORRODED (WING) · airframe 45,596 hrs · 54,133 cycles

TWO LOCK FASTENERS ARE CORRODED ON RT UPPER SKIN SURFACE AT STA YW174. R & R HARDWARE IAW SRM 51-400-10.

Part: STRINGER — DAMAGED (RT NACELLE) · airframe 46,598 hrs · 54,133 cycles

HEAT SHIELD LOWER STRINGER AND REAR STRAP IS DAMAGED ON RT NACELLE R & R LOWER HEAT SHIELD STRINGER AND REAR STIFFENER WITH LOCALLY FABRICATED MATERIAL IAW DWG 85410733 AND 8541-732.

Part: ANGLE — CRACKED (WG-BDY FAIRING) · airframe 46,598 hrs · 51,133 cycles

TEE DUCT SUPPORT ANGLE IS CRACKED IN FORWARD WING BODY FAIRING. R & R TEE DUCT SUPPORT ANGLE IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 46,598 hrs · 54,133 cycles

RT SEAT TRACK IS CORRODED BETWEEN STA.X109 AND X180. R & R RT INBD SEAT TRACK IAW DWG 85322516.

Part: SUPPORT BRACKET — CRACKED (RIGHT) · airframe 46,598 hrs · 54,133 cycles

RT BRACKET TO SUPPORT THE BLEED AIR TUBE FROM RT ENGINE TEE DUCT BLEED AIR TUBE IS CRACKED. R & R RT SUPPORT BRACKET IAW SRM 51-42-05.

Part: FLAP TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 45,596 hrs · 54,131 cycles

LT NR 1 FLAP TRACK CORRODED AT MATTING SURFACE. LT FLAP TRACK REMOVED IAW AMM 57-50-11. NEW LT NR 1 FLAP TRACK INSTALLED IAW AMM 57-50-11.

Part: FLAP TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 45,596 hrs · 54,131 cycles

LT NR 2 FLAP TRACK CORRODED AT MATTING SURFACE. LT NR 2 FLAP TRACK REPLACED IAW AMM 57-50-26.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 46,598 hrs · 54,133 cycles

CRACKED ANGLE FOUND AT INTERSECTION OF LANDING PLATE ON LT NACELLE. R & R ANGLE AT INTERSECTION OF LANDING PLATE IAW DWG 85410245.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 46,598 hrs · 54,133 cycles

PAX DOOR AFT BRACKET IS CORRODED. R & R PAX DOOR AFT BRACKET IAW SRM 20-14-01 AND SRM 51-40-07.

Part: BRACKET — CRACKED (LT WING) · airframe 465,998 hrs · 54,133 cycles

LT WING FRONT SPAR BRACKET IS CRACKED AT STA YW 139. R & R LT FRONT SPAR BRACKET IAW AMM 30-10-21.

Part: FLAP TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 45,596 hrs · 54,131 cycles

LT NR 3 FLAP TRACK CORRODED AT MATTING SURFACE. LT NR 3 FLAP TRACK REPLACED IAW AMM 57-50-26.

Part: BRACKET — CRACKED (LT WING) · airframe 46,598 hrs · 54,133 cycles

BLEED AIR DUCT IS CRACKED ON LT FRONT SPAR AT STA YW75.00. R & R BLEED AIR DUCT BRACKET IAW SRM 51-42-05.

Part: FLAP TRACK — CORRODED (RT WING) · corrosion level 2 · airframe 455,596 hrs · 54,131 cycles

RT NR 1 FLAP TRACK CORRODED AT MATTING SURFACE. RT NR 1 FLAP TRACK REPLACED IAW AMM 57-50-11.

Part: ANGLE — CRACKED (LT WING) · airframe 46,598 hrs · 54,133 cycles

LOWER FORWARD ANGLE IS CRACKED ON LT WING TIP. R & R LOWER ANGLE STRIP IAW SRM 51-42-05 AND SRM 51-40-00.

Part: BRACKET — CRACKED · airframe 46,598 hrs · 54,133 cycles

LEFT BRACKET TO SUPPORT THE BLEED AIR TUBE TEE DUCT IS CRACKED. R & R TEE DUCT AND LT BLEED AIR TUBE IAW AMM 21-11-32 , 20-06-03 AND 21-11-26.

Part: FLAP TRACK — CORRODED (NR 2 TE FLAP) · corrosion level 2 · airframe 44,596 hrs · 54,131 cycles

RT NR 2 FLAP TRACK CORRODED AT MATTING SURFACE. RT NR 2 FLAP TRACK REPLACED IAW AMM 57-50-26.

Part: FLAP TRACK — CORRODED (NR 3 TE FLAP) · corrosion level 2 · airframe 45,596 hrs · 54,131 cycles

RT NR 3 FLAP TRACK CORRODED AT MATTING SURFACE. RT NR 3 FLAP TRACK REPLACED IAW AMM 57-50-26.

Part: BRACKET — CRACKED (LT WING) · airframe 46,598 hrs · 54,133 cycles

BLEED AIR TUBE BRACKET ON LT WING FRONT SPAR IS CRACKED. R & R BLEED AIR TUBE BRACKET WITH LOCALLY FABRACATED MATERIAL.

Part: SUPPORT ANGLE — CORRODED (WINDSHIELD) · corrosion level 2 · airframe 46,598 hrs · 54,133 cycles

RT WINDSHIELD OTBD POST LOWER SUPPORT ANGLE IS CRACKED. R & R LOWER SUPPORT ANGLE IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 46,596 hrs · 54,131 cycles

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

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 46,596 hrs · 54,131 cycles

LEFT FINGERNAIL OTBD RIBLET IS CRACKED. R & R FINGERNAIL RIBLET IAW SRM 51-42-05.

Part: RAIL — CORRODED · corrosion level 2 · airframe 46,596 hrs · 54,131 cycles

LEFT INBD SEAT TRACK IS CORRODED. REPLACED LT INBD SEAT TRACK IAW RD8-53-2797.

Part: CARGO TRACK — CORRODED (BS 588-660) · corrosion level 2 · airframe 46,596 hrs · 54,131 cycles

CORROSION ON LT CARGO TRACK. R & R CARGO TRACK WITH MADE REPAIRED PART.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 46,598 hrs · 54,133 cycles

LT FINGERNAIL INBD RIBLET IS CRACKED. R & R RIBNET IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 630-638) · corrosion level 2 · airframe 46,596 hrs · 54,131 cycles

LT INBD SEAT TRACK IS CORRODED. R & R LT INBD SEAT TRACK IAW SRM 51-40-10, SRM 51-42-05 AND AMM 20-14-01.

Part: HINGE FITTING — CORRODED (VERTICAL STAB) · airframe 46,598 hrs · 54,133 cycles

AFT SPAR VERTICAL STABILIZER LOWER HINGE FITTING IS CORRODED. REPLACED AFT SPAR VERTICAL STAB LOWER HINGE FITTING IAW AMM 20-14-01.

Part: ANGLE — CRACKED (NACELLE) · airframe 46,598 hrs · 54,133 cycles

FORWARD INBD ANGLE IS CRACKED ON LT FINGERNAIL. R & R LT ANGLE IAW SRM 51-42-05 AND SRM 51-40-00.

Part: PLATE — CRACKED (NACELLE) · airframe 46,598 hrs · 54,133 cycles

LEFT LANDING PLATE OF PANEL 412DT, AFT SIDE IS CRACKED. R & R PLATE IN LT NACELLE IAW SRM 51-42-05 AND SRM 51-40-00.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 46,596 hrs · 54,131 cycles

LT NACELLE ANGLE FOUND CRACKED ON OTBD SIDE AT INTERSECTION OF LANDING PLATE AND OTBD SIDE WEB. R & R ANGLE IAW SRM 51-42-05.

Part: HINGE FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 46,596 hrs · 54,131 cycles

UPPER HINGE FITTING ON AFT VERTICAL STABILIZER IS CORRODED. REPLACED UPPER HINGE FITTING IAW AMM 20-14-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,596 hrs · 54,131 cycles

CLOSING ANGLE SUSPECTED CRACKED. SEALEDCLOSING ANGLE IAW RD8-53-2959.

Part: HEAT SHIELD — CRACKED (LT NACELLE) · airframe 46,596 hrs · 54,131 cycles

INBD AND OTBD STRINGER FOUND CRACKED UNDER LT NACELLE HEAT SHIELD, AFT END. R & R WITH MADE REPAIRED PARTS. INSTALLED IAW STRUCTURAL REPAIR MANUAL 51-42-42205

Part: ANCHOR FITTING — CORRODED (FLOOR) · airframe 46,596 hrs · 54,131 cycles

CARGO REAR UPPER FLOOR ANCHOR NUTS WERE FOUND CORRODED. R & R UPPER FLOOR ANCHOR NUTS WITH BLIND RIVETS IAW 51-40-00.

Part: HINGE — CRACKED (CARGO BAY) · airframe 46,596 hrs · 54,131 cycles

CARGO ARTICULATE PLATE PIANO HINGE FOUND CRACKED. R & R PIANO HINGE WITH NEW AND INSTALLED IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (AFT SERVICE DOOR) · corrosion level 2 · airframe 54,131 hrs · 336 cycles

AT BS 600, AFT SERVICE DOOR THRESHOLD WAS FOUND CORRODED. THRESHOLD REPLACED WITH NEW AND INSTALLED IAW SRM 51-42-05.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 46,348 hrs · 53,814 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 10, 11 AND 12. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 46,348 hrs · 53,814 cycles

RIGHT AFT EXTERIOR FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 46,205 hrs · 53,623 cycles

FWD FLOOR PATH EMERGENCY LIGHT SPLICE BROKEN. SPLICED EMERGENCY LIGHT WIRE IAW AMM 20-45-07.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 46,120 hrs · 53,515 cycles

SMOKE MASTER WARNING LIGHT ILLUMINATED AFTER NR2 ENGINE START. INSPECTED BAG BAY. NO FIRE OR SMOKE EVIDENT. TESTED BAG BAY SMOKE DETECTORS. FOUND NR 2 WOULD NOT TEST AND NR 1 LEAVES SMOKE WARNING LIGHT ON. R & R BOTH NR 1 AND NR 2 SMOKE DETECTORS. OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,504 hrs · 52,801 cycles

TWO FORWARD FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AT PS2 IAW AMM 33-51-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 45,520 hrs · 52,743 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE, 4TH RED FROM BACK. R & R LIGHT BULB AND RESPLICED WIRE IAW AMM 33-50-01.

Part: ELECTRONIC UNIT — FAILED (AUTOFEATHER) · airframe 45,456 hrs · 52,653 cycles

ON TAKEOFF ROLL AUTO FEATHER DID NOT ARM. R & R AUTOFEATHER ARM LIGHT RELAY AND NR 1 TSEU IAW MM 72-01-10. GROUND RAN IAW -8 RUNUP MANUAL. ARMED AT 90 PERCENT TORQUE. OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 45,446 hrs · 45,446 cycles

FLOOR EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH THE LIGHT SWITCH. ONLY GOES OUT WHEN APU IS RUNNING. RESEATED CONNECTOR 3352 T3. OPS CHECKED GOOD IAW W/C 33-50-03Q.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 45,418 hrs · 52,605 cycles

SMOKE WARNING LIGHT ILLUMINATED WITH NO EVIDENCE OF FIRE OR SMOKE WHILE ON GATE, THEN LIGHT WENT OUT AND NR 2 CARGO BAY SMOKE DETECTOR WOULD NOT TEST. R & R NR 2 SMOKE DETECTOR IN CARGO BAY IAW AMM 26-12-00. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 45,216 hrs · 52,337 cycles

BAG BAY SMOKE WARNING LIGHT ILLUMINATED ON GROUND. R & R NR 200 BAG BAY SMOKE DETECTOR IAW MM 26-12-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 45,191 hrs · 52,299 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 1. FOUND BROKEN WIRE AT SPLICE. R & R SPLICE IAW STANDARD WIRING PRACTICES.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 44,882 hrs · 51,884 cycles

THREE EMERGENCY LIGHTS INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 44,822 hrs · 51,803 cycles

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

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 44,798 hrs · 51,771 cycles

ONE RED EMERGENCY FLOOR LIGHT ADJACENT TO ROW 1 IS INOPERATIVE. FOUND BULB PULLED FROM RED LAMP INDICATOR. REINSTALLED BULB INTO RED INDICATOR. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FIRE BOTTLE — DISCHARGED · airframe 44,815 hrs · 51,794 cycles

APU SHUTDOWN, CHECK FIRE DETECTOR ILLUMINATED. NO FIRE INDICATED. APU BOTTLE SHOWS CHARGE ELECTRICALLY AND DISCHARGE DISCS INTACT. FOUND FIRE BOTTLE DISCHARGED. R & R APU FIRE BOTTLE IAW WORKCARD 26-21-01. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,781 hrs · 51,751 cycles

DIM LT & RT AFT EMERGENCY LIGHTS. R & R LT & RT AFT EMERGENCY EXIT EGRESS LIGHTS AND SECURED LENS COVER WITH RETAINED HARDWARE. SEALED OUTSIDE OF COVER WITH RTV.

Part: LAMP — WRONG PART (EMERGENCY LIGHT) · airframe 44,781 hrs · 51,751 cycles

INCORRECT BULB INSTALLED FOR LT FWD EMERGENCY EXIT EGRESS LIGHT. REMOVED BULB AND INSTALLED CORRECT BULB. SECURED LENS COVER WITH RETAINED HARDWARE AND SEALED COVER EDGE WITH RTV.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 44,735 hrs · 51,697 cycles

EMERGENCY LIGHT AT FLOOR LEVEL NEAR AIRSTAIR HAS BULB OUT. R & R BULB AS REQUIRED. OPS CHECKED GOOD.

Part: SENSOR — OBSTRUCTED (SERVICE DOOR) · airframe 42,926 hrs · 50,052 cycles

SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL, ABORTED TAKEOFF. FOUND WHITE PLASTIC STRIPE JAMMED NEAR SENSOR. REMOVED STRIPE. OPS CHECKED GOOD, DOOR INDICATION NORMAL.

Part: CONNECTOR — DAMAGED (OIL PRESS XMITER) · airframe 44,528 hrs · 51,407 cycles

NR 1 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 40 TO 55 PSI. OIL PRESSURE WARNING LIGHT DID NOT ILLUMINATED. INSPECTED NR 1 ENGINE OIL PRESSURE TRANSMITTER CONNECTOR AND FOUND PIN 2 WITH BROKEN STRANDS. SPLICED DEFECTIVE WIRE. GROUND RAN ACFT. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. OIL LEVEL CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 44,310 hrs · 51,128 cycles

FLOOR EMERGENCY PATH LIGHTS INOP ROW 2, ROW 13. REMOVED LENS, R & R BULBS SAID LOCATIONS, REINSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,310 hrs · 51,128 cycles

ROW 11AC SIDEWALL EMERGENCY LIGHT HAS ONE INOPERATIVE BULB. R & R 11AC SIDEWALL LIGHT, REF AMM 33-20-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 44,085 hrs · 50,881 cycles

LT SEAT LEVEL EMERGENCY EXIT SIGN HAS BULB INOP AT ROW 11AC. R & R BULB FOR EMERGENCY SEAT LEVEL EMERGENCY EXIT SIGN AT ROW 11AC.

Part: CIRCUIT CARD — FAILED (AUTOPILOT) · airframe 43,672 hrs · 50,367 cycles

DURING TAXI, AFTER STARTING NR1 ENGINE, DC BUSS CAUTION LIGHT ILLUMINATED. AFTER SELECTING NR 1 DC GENERATOR OFF, POPPING SOUND UNDER LT GLARESHIELD, FOLLOWED BY MINIMAL SMOKE. MX INSPECTED AND FOUND AUTOPILOT CIRCUIT CARD FOR ANNUNCIATOR PANEL BURNED AND CIRCUIT BREAKERS G-1 LT ESSENTIAL AND E-3 LT MAIN TRIPPED. DISCONNECTED CONNECTOR ON AUTOPILOT ANNUNCIATOR PANEL. R & R AUTOPILOT DISENGAGE CIRCUIT CARD IAW MM 20-45-04. OPS CHECKED GOOD IAW MM 22-10-04.

Part: CONTROL BOX — FAILED (EMERGENCY LIGHTS) · airframe 43,398 hrs · 50,043 cycles

CABIN EMERGENCY LIGHTS FLICKERED IN FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYS) · airframe 43,076 hrs · 49,636 cycles

UPON TAXI OUT, LOST HYDRAULIC QUANTITY OF NR2 HYD SYS. UPON RETURN TO GATE, FOUND FLUID DRIPPING FROM NR2 MLG BRAKE AREA. R & R NR3 BRAKE LINE. LEAK CHECKED GOOD, SERVICED HYD.

Part: PIPE — LEAKING (BLEED SYSTEM) · airframe 38,638 hrs · 42,773 cycles

ROW 6 AND 7 HAS A BURNED SMELL. INSPECTED OVERHEAD LIGHTS, NO DEFECTS NOTED. FOUND BLEED LEAK AT T PIPE AT FRONT SPAR. TIGHTENED CLAMPS. OPS CHECKED GOOD OK FOR SERVICE.

Part: TSCU — FAILED (NR 1) · airframe 41,931 hrs · 48,164 cycles

AFTER TAKEOFF, AUTO FEATHER ARM FAILED TO DESELECT. CHECKED SWITCH 6121 S7, S8, S9, S19, S11. RESOLDERED 612149L22 TO SWITCH 6121S6. CHECKED FOR GROUND IN THE ENABLE CIRCUIT AT BOTH TSCU'S P6 AND P7 PIN 8 AND 1. NO DEFECTS NOTED. R & R NR 1 TSCU IAW 72-01-10. OPS CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER) · airframe 41,918 hrs · 48,145 cycles

WITH AUTOFEATHER DESELECTED, AUTOFEATHER ARM LIGHT WOULD NOT EXTINGUISH. CREW REPORTED LIGHT EXTINGUISHED ON DECENT. R & R NR 2 TSCU IAW 72-01-10 AND ARM CONTROL RELAY 6121-K5. GROUND RAN ACFT, OPS CHECKED GOOD AT THIS TIME.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,299 hrs · 47,362 cycles

PIT .026 DEEP AT X107.85 AND .75 INCHES INBD OF STRINGER 31S. COMPLIED WITH REPAIR IAW EO8-53-10-0641.

Part: PANEL — CORRODED (FUSELAGE) · airframe 41,299 hrs · 47,362 cycles

623AT INBD STRESS PANEL FLANGE PITTED AND FRETTED ALONG INBD FLANGE. LOCALLY BLEND PITTING AND FRETTED AREA ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.

Part: PANEL — MISREPAIRED (FUSELAGE) · airframe 41,299 hrs · 47,362 cycles

623AT INBD STRESS PANEL FLANGE BLENDED BELOW MINIMUM LIMITS IAW RD8-57-455. REPAIRED 623AT LADDER PLATE FLANGE IAW EO8-57-10-0611.

Part: PLATE — CORRODED (FUSELAGE) · airframe 41,299 hrs · 47,362 cycles

OTBD LADDER PLATE FOR PANEL 623AT HAS FRETTING INBD. LOCALLY BLENDED FRETTING ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,544 hrs · 40,050 cycles

ROWS 11 AND 13 EMERGENCY FLOOR PATH LIGHTS ARE INOP. RELAMPED EMERGENCY FLOOR PATH LIGHTS ANT ROW 11 AND ROW 13 IAW 33-20-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,115 hrs · 47,152 cycles

SIDEWALL EMERGENCY LIGHT ROW 11AC HAS ONE BULB INOP. RELAMPED EMERGENCY LIGHT AT SAID LOCATION IAW AMM 33-20-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,115 hrs · 47,152 cycles

SIDEWALL EMERGENCY LIGHT AT ROW 11DF HAS ONE BULB INOP. RELAMPED EMERGENCY LIGHT AT SAID LOCATION IAW AMM 33-20-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,734 hrs · 46,680 cycles

SEVERAL LIGHTS ON EMERGENCY EXIT BY PASSENGER DOOR ON FLOOR ARE NOT WORKING. R & R BULBS ON EMERGENCY EXIT LOWER FLOOR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,264 hrs · 46,110 cycles

ROW 6 EMERGENCY FLOOR PATH LIGHT INOP. REPLACE BULB AT ROW 6 EMERGENCY FLOOR PATH LAMP, REF MM 33-51-00.

Part: PRESSURE SWITCH — FAILED (RUDDER) · airframe 39,508 hrs · 45,163 cycles

ON CLIMB OUT, ABOVE 140 KNOTS, RUDDER PRESSURE, FOLLOWED BY RUDDER PRESSURE CAUTION LIGHTS ILLUMINATED, BOTH QUANTITIES UNCHANGED. (NEVER GOT HYD CAUTION LIGHT) ACFT RETURNED TO FIELD. MX REMOVED AND REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES, OPS CHECKED AND LEAKED CHECKED GOOD IAW MM 27-20-39. ACCOMPLISHED TEST OF NR1 AND NR2 PRESSURE REGULATOR SOLENOID VALVES AND ISOLATED SOLENID IAW 27-20-38. PERFORMED SYS OPS CHECK WITH PITOT STATIC TESTER SET BETWEEN 100 TO 200 KNOTS INDICATED AIRSPEED. FLUCTUATED AIRSPEED BETWEEN 100 AND 200 KNOTS SEVERAL TIMES, OPS CHECKED OK.

Part: ACM — BROKEN · airframe 38,314 hrs · 43,666 cycles

WHILE SITTING ON THE RAMP WITH APU RUNNING PILOTS HEARD A BANG FROM THE APU COMPARTMENT FOLLOWED BY A CABIN FILLING WITH SMOKE. INSPECTED AND FOUND AFT ACM TO BE INOPERATIVE. REMOVED AND REPLACED AFT ACM WITH AN OPERATIONAL CHECK BEING GOOD AND NO FURTHER ACCOUNTS FOR SMOKE IN THE CABIN.

Part: INDICATOR — FALSE INDICATION (FUEL FLOW) · airframe 38,216 hrs · 43,544 cycles

ON TAKEOFF ROLL NR 2 FUEL FLOW INCREASED TO 1200, ABORTED TAKEOFF. REMOVED AND REPLACED FUEL FLOW INDICATOR IAW MM 73-32-00.

Part: TRU — MALFUNCTIONED (LEFT) · airframe 37,824 hrs · 43,031 cycles

LEFT TRANSFORMER RECTIFIER UNIT FAILED WHEN ON RUNWAY AND RETURNED TO GATE. CREW GROUND RAN AIRCRAFT, PERFORMED TRUE OPS CHECK AND ALTERNATING CURRENT. VARIABLE FREQUENCY GENERATION SYSTEM OPS CHECK. ALL SYSTEMS OPERATE NORMALLY IN ACCORDANCE WITH THE PROCEDURES.

Part: CLAMP — LOOSE (CABIN) · airframe 37,799 hrs · 43,003 cycles

BURNED SMELL IN CABIN AT ROW 4 AND ROW 5 AREA. INSPECTED THE NORMAL CABIN LIGHTING AND EMERGENCY LIGHTING POWER SUPPLY IN THIS AREA, PERFORMED HIDDEN DAMAGE INSPECTION, FOUND NO DAMAGE, DEACTIVATED NORMAL CABIN LIGHTING AS A PRECAUTION. FOUND BLEED T-DUCT CLAMP LOOSE AND LEAKING AIR, CAUSING BURNT PRC SMELL. RE-TORQUED T-DUCT CLAMP. GROUND RAN, NO LEAKS OR SMELLS NOTED. REACTIVATED NORMAL CABIN LIGHTING.

Part: CONNECTOR — SHORTED (NR 2 GENERATOR) · airframe 37,764 hrs · 42,961 cycles

NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. REJECTED TAKEOFF. CYCLED GENERATOR SWITCH IN ACCORDANCE WITH ABNORMAL EMERGENCY CHECKLIST, LIGHT RESET AND GENERATOR OPERATES NORMAL. REMOVED AND REPLACED CONNECTOR 2421-P2 IN ACCORDANCE WITH MAINTENANCE MANUAL 20-45-06, OPS CHECK GOOD.

Part: SENSOR — DEFECTIVE (COCKPIT) · airframe 36,755 hrs · 41,710 cycles

EN ROUTE TO CLT, 40 MILES EAST OF FLO THE CREW SMELLED A STRONG BURNING SMELL. FLIGHT ATTENDANT REPORTED NO SMELL OR SMOKE. THE CREW TURN ON COCKPIT LIGHTS AND COULD SEE A SMALL AMOUNT OF SMOKE. DECLARED AND EMERGENCY AND DIVERTED TO FLO. DESENDING TO 10K FEET, CREW OPENED THE FORWARD OUT FLOW VALVE AND THE SMOKE AND SMELL WENT AWAY. CANCELLED THE EMERGENCY AND CONTINUED ONTO CLT. ARRIVED IN CLT WITH NO PROBLEMS. MAINT FOUND CIRCUIT BREAKER POPPED, UPON TROUBLESHOOTING FOUND COCKPIT ZONE TEMP SENSOR (FAN) INOP. REMOVED AND REPLACED ZONE TEMP SENSOR IAW 21-60-45. OPS CHECK GOOD.

Part: DOOR — OPEN (SERVICE)

RETURNED TO GATE, MAINTENANCE CLOSED DOOR (SERVICE DOOR WARNING LIGHT ILLUMINATED PRIOR TO TAKEOFF). (K)

Part: PIN — LOOSE (CONNECTOR) · airframe 35,725 hrs · 40,421 cycles

WHILE APPLYING POWER ON T/O AND UPON LANDING ROLL EMERGENCY LIGHTS ILLUMINATED FOR ABOUT 5 SECONDS EACH TIME. FOUND PIN ON 3351-J1 CONNECTOR NOT LOCKED IN PLACE. LOCKED PIN IN PROPER POSITION. NO OTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,892 hrs · 39,408 cycles

THE PILOT REPORTED A STRONG ELECTRICAL ODOR ON FLIGHT DECK. THE FLIGHT COMPARTMENT AND DC CONTACTOR BAY WERE INSPECTED FOR DAMAGE NONE FOUND. THERE WAS NO ELECTRICAL ODOR NOTED. STARTED THE ENGINES AND RAN ALL SYSTEMS. NO DEFECTS WERE FOUND AND NO CIRCUIT BREAKERS WERE POPPED. NO ODOR NOTED, OK FOR SERVICE.

Part: TIRE — FLAT (LANDING GEAR) · airframe 34,105 hrs · 38,466 cycles

CREW STOPPED THE AIRCRAFT ON THE TAXIWAY AND REPORTED TO TOWER THAT AIRCRAFT HAD A FLAT TIRE. THE AIRPORT AUTHORITY SENT OVER A VEHICLE AND VERIFIED THAT PLANE HAS TWO FLAT TIRES. PASSENGERS WERE DEPLANED WITH GROUND TRANSPORT. REMOVED AND REPLACED NR 1 TIRE AND NR 2 MWA, OPS CHECK GOOD.

Part: HINGE — BROKEN (NLG DOOR) · airframe 33,839 hrs · 38,143 cycles

AFTER LANDING IT WAS FOUND THAT THE AFT NOSE GEAR DOOR HINGE HAD BROKEN AND THE DOOR HAD RUBBED ON ONE OF THE NOSE TIRES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,780 hrs · 38,075 cycles

THIRD EMERGENCY CENTER FLOOR BULB FROM THE FRONT BURNT OUT. REPLACED BULB, OPS CHECK GOOD.

Part: TERMINAL — BURNED (WINDSHEILD HEAT) · airframe 33,044 hrs · 37,164 cycles

SMOKE AND FLAMES COMING FROM F/O'S WINDSCREEN. SECONDS LATER IND SCREEN SHOWED SEVERAL CRACKS. FOUND TERMINAL END L2 BURNED, REMOVED AND REPLACED TERMINAL END AND F/O'S WINDSHIELD.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 28,906 hrs · 32,017 cycles

ON GEAR RETRACTION NOSE GEAR DID NOT RETRACT, NR 2 HYDRAULIC QUANTITY DROPPED TO .5 QUARTS. CREW PERFORMED EMERGENCY EXTENSION. FOUND PRESSURE LINE TO NOSE GEAR DRAG STRUT ACTUATOR LEAKING. REMOVED AND REPLACED LINE AND COMPLIED WITH GEAR SWINGS.

Part: AHRS — FAILED (NR 2) · airframe 27,837 hrs · 30,678 cycles

NR 2 AHRS FAILED IN FLIGHT, DETECTED BAD WEATHER. REMOVED AND REPLACED NR 2 AHRS, OPS CHECK GOOD.

Part: PIPE — CRACKED (BLEED AIR) · airframe 26,941 hrs · 29,595 cycles

AFTER TAKEOFF F/A REPORTED STRONG BURNING ODOR IN CABIN, THIS HAPPENED RIGHT AFTER BLEED WAS SELECTED. MX ISOLATED ENG BLEED LEAK AT FRONT SPAR BLEED PIPE. REMOVED AND REPLACED BLEED PIPE UNDER PANELS 261JT, NT LEAK CHECK GOOD. GROUND RAN A/C, NO SMELL NOTED.

Part: SKIN — CRACKED (RUDDER) · airframe 26,409 hrs · 28,926 cycles

SEVERE TURBULENCE JOLT OCCURRED AT 17,000 FT. LOST 200 FEET. INSPECTED IAW W/C 05-50-21I ONE DEFECT NOTED FOUND CRACK IN FORE RUDDER. REPAIRED IAW EO 8-55-04-0222

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 25,321 hrs · 27,661 cycles

TWO RED FLOOR EMERGENCY LIGHTS AT ROW 2AC ARE INOP. REMOVED AND REPLACED LIGHT SOCKETS AND REPAIRED BROKEN WIRES.