N815EX

Part: COMPUTER — OUT OF ADJUST (STALL WARNING) · airframe 56,722 hrs · 62,987 cycles

UNCOMMANDED STICK SHAKERS ON DURING ROTATION. RETURNED TO FIELD. SHAKERS STOPPED WHEN ACFT ON THE GROUND. FOUND NR 1 STALL WARNING COMPUTER SLIGHTLY OUT OF ADJUSTMENT. CALIBRATED NR 1 AND NR 2 STALL WARNING COMPUTER. OPS AND FUNCTION CHECKED GOOD IAW MM 27-33-00. OK FOR SERVICE. CLEARED MEL.

Part: BRUSH BLOCK — SHORTED (PROP HEAT) · airframe 56,704 hrs · 62,967 cycles

EMERGENCY LIGHTS FLICKERED AND CYCLED ON/OFF WITH PROP HEAT ON AND PROPS AT 1050. GOOD WITH PROP HEAT OFF. INSPECTED NR 2 PROP, A PHASE SLIP RINGS AND LEADS. NO DEFECTS NOTED. R & R NR 2 BRUSH BLOCK. GROUND RAN. OPS CHECKED NORMAL AT THIS TIME.

Part: BATTERY — UNKNOWN · airframe 56,445 hrs · 62,667 cycles

AUXILIARY BATTERY HOT WARNING LIGHTS IN FLIGHT. AUXILIARY BATTERY TEMP IS 65 DEGREES. COMPLIED WITH CHECKLIST. R & R AUX BATTERY IAW MM 24-32-00. OPS CHECKED GOOD.

Part: FIREWALL — CHAFED (NR 1 NACELLE) · airframe 56,038 hrs · 62,178 cycles

NR 1 NACELLE, INBD Z MEMBER HAS CRACK IN LIP AT ABOUT 4" ABOVE START OF LIP IN FIREWALL WEB CHAFE. RIMMED FIREWALL PLATE IAW RD8-54-991. REPAIRED CHAFE AND TRIMMED OUT AREA IAW EO8-54-15-0176.

Part: NONE — NONE (NONE) · airframe 55,022 hrs · 60,963 cycles

POSSIBLE ANIMAL STRIKE DURING ROLL OUT. INSPECTED PLANE AND FOUND NO EVIDENCE OF ANIMAL STRIKE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,931 hrs · 60,859 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROWS 1, 3 AND 7. R & R BULBS FOR EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,885 hrs · 60,799 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R POWER SUPPLY 3351, PS3 IAW MM 33-51-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,885 hrs · 60,799 cycles

CEILING EMERGENCY LIGHT AT ROW 3 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IN ROW 3 CEILING LIGHT. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (CONTROL PANEL) · airframe 54,765 hrs · 60,656 cycles

EMERGENCY LIGHTS SWITCH NORMAL GREEN LIGHT INOPERATIVE. R & R LAMP, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,753 hrs · 60,640 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,974 hrs · 72,933 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,546 hrs · 62,356 cycles

9TH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 4,419 hrs · 60,270 cycles

DURING POWER UP FOR TAKEOFF AT 65 PERCENT TORQUE, TAKEOFF WARNING HORN SOUNDED. REJECTED TAKEOFF. CLEANED AND INSPECTED FLAP INDICATOR CONNECTOR. NO DEFECTS NOTED. CREW GROUND RAN ACFT AND INSPECTED SYS IAW MM 31-51-00. HORN STILL SOUNDED DURING POWER RUNS. RESET CIRCUIT BREAKER A-4. OPS CHECKED IAW WC 31-50-00Q. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 54,419 hrs · 60,270 cycles

DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF. CYCLED FLAPS, ELEVATOR TRIM AND ECU MODE SWITCHES. GROUND RUN ACFT, HORN DID NOT SOUND. CONFIRMED FLAP INDICATOR CAUSING TAKEOFF WARNING WHILE IN PROPER CONFIGURATION. R & R FLAP INDICATOR. OPS CHECKED GOOD WITH WC 31-50-00Q. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,270 hrs · 60,104 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 3, 4 AND 6. R & R THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,270 hrs · 60,104 cycles

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

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 54,142 hrs · 59,953 cycles

THE 6TH EMERGENCY FLOOR PATH LIGHT BETWEEN ROWS 1 AND 2 IS INOPERATIVE. REPLACED BULB, OPS CHECKED GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 54,142 hrs · 59,953 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHT FAILED COMPARATOR CHECK. R & R THE LIGHT ASSY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,972 hrs · 5,977 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 3. R & R LIGHT BULB FOR CEILING EMERGENCY PATH LIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,958 hrs · 59,737 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,866 hrs · 59,620 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 4 AND 8. R & R BULBS IAW MM 33-51-11. OPS CHECKED GOOD.

Part: GENERATOR — FAILED (NR 1) · airframe 53,743 hrs · 59,473 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED AND WILL NOT RESET. R & R NR 1 AC GENEREATOR AND GCU IAW WC 24-20-11R AND MM 24-21-02. OPS AND LEAK CHECKED GOOD.

Part: KNOB — UNSECURE (CONTROL PANEL) · airframe 53,482 hrs · 59,161 cycles

FIRST OFFICER`S TRANSMIT SELECT KNOB ON ACP LOOSE. SECURED SELECT KNOB. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — WEAK (EMERGENCY LIGHT) · airframe 53,310 hrs · 58,961 cycles

LEFT AFT EXTERNAL FUSELAGE EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 53,209 hrs · 58,846 cycles

RED FLOOR EMERGENCY LIGHT MISSING. INSTALLED RED FLOOR LIGHT MODULE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 53,121 hrs · 58,745 cycles

EMERGENCY CEILING LIGHT DIM AT ROW 1AND 3. R & R EMERGENCY EMERGENCY CEILING LIGHT BULBS AT ROW 1 AND 3. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,606 hrs · 58,139 cycles

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

Part: FLANGE — CRACKED (LT NACELLE) · airframe 52,512 hrs · 58,022 cycles

LEFT NACELLE COLLAR FLANGE IS CRACKED AT FORWARD END. R & R FORWARD ANGLE ON LT COLLAR IAW AMM 54-40-04, 54-40-06 AND EO8-54-13-0696.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,328 hrs · 57,814 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 52,328 hrs · 57,814 cycles

EMERGENCY EXIT DOOR SIGN IS DIM. R & R EXIT SIGN BULBS. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,301 hrs · 57,780 cycles

EMERGENCY LIGHT INOPERATIVE AT ROWS 1 AND 3. R & R BULBS, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 53,305 hrs · 57,784 cycles

ON APU BLEED START, STRONG FUEL ODOR ENTERED CABIN. NO LEAKS FOUND OR OBVIOUS DEFECTS. GROUND RAN ACFT WITH DOORS OPEN FOR 10 MINUTES AND CABIN ODOR CLEARED AT THIS TIME,

Part: UNKNOWN — ODOR (CABIN LIGHTS) · airframe 51,962 hrs · 57,378 cycles

ELECTRICAL BURNING ODOR APPEARS TO BE COMING FROM OVERHEAD LIGHTS AT ROW 7DF. R & R LAMP HOLDER, BULB AND BALLAST. OPS CHECKED GOOD.

Part: AHRS — FAILED (NR 2) · airframe 51,477 hrs · 56,797 cycles

NR 2 AHRS FAILED. NR 2 ADI READ 10 DEGREES PITCH OP. CYCLED NR 2 AHRS, CIRCUIT BREAKER ADI CORRECTED PITCH. R & R ARHU. OPS CHECKED GOOD IAW 34-20-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,375 hrs · 56,679 cycles

TWO RED FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R ONE LAMP AND ONE LIGHT SOCKET AT ROW 1. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 51,108 hrs · 56,452 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-00.

Part: UNKNOWN — SMOKE (NR 2 NACELLE) · airframe 51,102 hrs · 56,346 cycles

F/A REPORTS SMOKE FROM NR 2 NACELLE. OPENED NR 2 NACELLE AND INSPECTED. NO LEAKS OR SMOKE NOTED. GROUND RAN ENG AND OPS NORMAL W/ NO DISCREPANCIES.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 51,004 hrs · 56,228 cycles

SMOKE NOTED FROM OVERHEAD LIGHTS AT ROW 1AC. INSPECTED AND FOUND DAMAGE SOCKET. OVERHEAD LIGHT CIRCUIT BREAKERS S1, S2 AND R2 ARE DEACTIVATED. R & R BALLAST AND LIGHT SOCKET. REACTIVATED OVERHEAD LIGHTS. OPS CHECKED GOOD.

Part: NONE — NONE · airframe 50,888 hrs · 56,080 cycles

AIRSTAIR DOOR EMERGENCY LIGHT SYS WOULD NOT EXTINGUSH. OPS CHECKED EMERGENCY LIGHT SYS IAW WC 33-50-03. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,479 hrs · 55,575 cycles

EMERGENCY SIDEWALL LIGHT IS INOPERATIVE AT ROW 4AC. R & R BULB.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,328 hrs · 55,403 cycles

LEFT AFT FUSELAGE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED LENS, R & R BULB, AT SAID LOCATION. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,602 hrs · 54,501 cycles

SIDEWALL LIGHT, FORWARD MOST POSITION ABOVE EMERGENCY EXIT INOPERATIVE. R & R BULB. OPS CHECKED OK. REINSTALLED LENS.

Part: YAW DAMPER — FAILED · airframe 49,610 hrs · 54,511 cycles

BOTH YAW DAMPENERS FAILED. YAW DAMPENERS BOTH CHANNELS DE-ACTIVATED IAW APENDIX 1/22-4-1.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,602 hrs · 54,501 cycles

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

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,437 hrs · 54,295 cycles

F/A'S EMERGENCY LIGHT SWITCH BACKLIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: GROUND WIRE — DAMAGED (MLG) · airframe 49,431 hrs · 54,289 cycles

DURING TAXI, RT RED GEAR UNSAFE LIGHT HANDLE LIGHT AND HORN SOUNDED, CREW INSTALLED GEAR PINS. REPAIRED BROKEN GROUND WIRE AT SENSOR. SWUNG LANDING GEAR SEVERAL TIMES IAW AMM 32-30-00. NO FAULTS NOTED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LOCK NUT — LOOSE (RUDDER TRIM) · airframe 49,284 hrs · 54,117 cycles

RUDDER TRIM WILL NOT OPERATE TO THE RIGHT. OK TO LEFT. INSPECTED, FOUND TRIM SWITCH LOCK NUT LOOSE. RETIGHTEN LOCK NUT. TRIM OPS CHECKED NORMAL IN BOTH DIRECTIONS.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 49,072 hrs · 53,883 cycles

APPROXIMATELY FIVE SECONDS BETWEEN ELEVATOR COMMAND AND ELEVATOR REACTION. FOUND ELEVATOR SERVO MOTOR TIGHT. R & R ELEVATOR SERVO IAW -8 MM 22-13-00. OPS CHECKED SERVO IAW MM 22-10-01 USING STARDARD MX ENGAGING A/P ON GROUND, GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 48,906 hrs · 53,700 cycles

ONE RED EMERGENCY LIGHT IS OUT AT RT FWD EXIT. RELAMP 1 RED EMERGENCY LIGHT AT RT FWD EXIT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 48,484 hrs · 53,210 cycles

EMERGENCY FLOOR LIGHT PATH ROW 9 IS TOO FAR UNDERNEATH SEAT AT ROW 9. (MOVE FWD TO FRONT EDGE OF SEAT). REMOVED LENS, POSITIONED ROW 9 EMER FLOOR PATH LIGHT, OUT TO FRONT EDGE OF SEAT, REINSTALLED LENS.

Part: WIRE — DAMAGED (PFCS) · airframe 48,337 hrs · 53,047 cycles

CIRCUIT BREAKER 1Q FOR PFCS INDICATOR POPPED AFTER TAKEOFF. RETURN TO FIELD. INSTALLED TEMP WIRE IAW SP 24.4. LOCATED BETWEEN 9800J172 AND 2705P10. WIRE IDENT IS IAB22. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 48,274 hrs · 52,968 cycles

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

Part: HANDLE — MALFUNCTIONED (PARKING BRAKE) · airframe 48,093 hrs · 52,760 cycles

PARKING BRAKE HANDLE WILL NOT SET. WHEN PARK BRAKE HANDLE IS MOVING TOWARD SET, GUST LOCK RELEASES. TIGHTENED HARDWARE ON PARKING BRAKE AND GUST LOCK STOP BRACKET. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 48,064 hrs · 52,725 cycles

TWO RED EMERGENCY LIGHTS ARE OUT IN ROW 1 AND 4. R & R BATTERY PACK AT P-2. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 47,997 hrs · 52,649 cycles

NR 3 FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB.

Part: SIGN — DISLODGED (CABIN) · airframe 47,902 hrs · 52,541 cycles

EXIT SIGN AT F/A JUMPSEAT IS FALLING OFF. R & R EMERGENCY EXIT LIGHT ASSY OPS CHECKED GOOD. CLEARED MEL.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 47,079 hrs · 51,622 cycles

NR 2 ENGINE TQ WENT TO 117 PERCENT, THEN FELL BACK TO 40 PERCENT, THEN WENT TO 80 PERCENT AND STABILIZED FOR 30 SECONDS, THEN WENT TO 121 PERCENT WITH NO INPUTS. THEN SHUTDOWN ENGINE. HEARD ENGINE PITCH CHANGE AND FELT YAW. GROUND RAN ACFT FOR MORE THAN 20 MINUTES AT DIFFERENT POWER LEVER SETTINGS, COULD NOT DUPLICATE ORIGINAL PROBLEM. F/O STATED LATER THAT THE PROP SPEED DID NOT FLUX. STAYED AT 900 AND ITT DID RISE, BUT COULD NOT STATE HOW MUCH. JUST SEEN IT MOVE. PULLED AND COLLARD CBS M8/H3. RT NR 2 EEC IAW WORKCARD 72-20-01R. GROUND RAN ACFT. SYS OPS AND LEAKED GOOD.

Part: CONTROL CABLE — CORRODED (MLG) · airframe 46,819 hrs · 51,328 cycles

MLG ALTERNATE EXTENSION SYS CONTROL CABLE SHOWING SIGNS OF CORROSOIN IN MAIN LANDING GEAR WELL TO REAR DOOR RELEASE. R & R LEFT MLG ALTERNATE EXTENSION SYS CONTROL CABLE IAW -8 -100, MM 32-35-00.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 46,819 hrs · 51,328 cycles

RT NR 8 CABIN WINDOW AT X456.500 HAS CORROSION ON LOWER PORTION AT STR 168. REMOVED ALL CORROSION AT RT NR 8 CABIN WINDOW FRAME IAW -8,-100, RD8-53-623. PERFORMED HFEC INSPECTION IAW -8 -100 SERIES NTM 51-00-06. NO DEFECTS NOTED.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 46,819 hrs · 51,321 cycles

CORROSION AFT PAX DOOR LOWER SILL AT DOOR SEAL INFLATION FITTING. REMOVED CORROSION IAW SRM 51-20-11. FOUND TO BE WITHIN LIMITS, TREATED WITH ALODINE, PRIMED IAW -8 -100 SRM51-20-26.

Part: CABLE — RUSTED (GUST LOCK) · airframe 46,819 hrs · 51,328 cycles

GUST LOCK CABLES AFT, ON WING, TOP OF FUSELAGE ARE RUSTED. R & R GUST LOCK CABLE IAW MM 27-70-00. PERFORMED RIGGING OF GUST LOCK CABLE IAW DASH 8 -100 MM 27-70-00.

Part: SHAFT — CORRODED (PAX DOOR) · airframe 46,819 hrs · 51,328 cycles

PAX DOOR HAND RAIL STRUT SHAFT BEARINGS WORN AND CORRODED. R & R PAX DOOR HAND RAIL STRUT SHAFT, FORK AND BUSHINGS IAW -8 -100 MM 20-12-04.

Part: FRAME — CORRODED (BS 202.75) · airframe 46,819 hrs · 51,321 cycles

FRAME AT X202.75, STR 31S IS CORRODED AND THE CORROSION GOES BETWEEN THE TENSION FITTING AND FLOORBEAM SUPPORT STRUT. CORROSION GOES FROM 30S TO 32S. REMOVED FRAME X202.75 BETWEEN STR 28S AND STR 28P. REPLACED WITH NEW FRAME, REMOVED RT FORWARD TENSION FITTING AND REPLACED WITH NEW PART. ALL WORK IAW DWG 85320247. ALSO, IAW -8-100 SRM 51-20-00, 51-20-26, 51-40-07, 51-40-11, 51-42-05 AND 51-20-26.

Part: SHAFT — CORRODED (PAX DOOR) · airframe 46,819 hrs · 51,328 cycles

SHAFT FOR AFT PAX DOOR HANDRAIL PITTED AND CORRODED. R & R SHAFT FOR AFT PAX DOOR HANDRAIL IAW MM 52-10-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 48,819 hrs · 51,328 cycles

PAX DOOR THRESHOLD SUPPORT CHANNEL CORRODED. BLENDED OUT CORROSION AT PAX DOOR THRESHOLD SUPPORT CHANNEL AND WAS FOUND TO BE OUT OF LIMITS IAW -8 RD8-53-8921. REPLACED THRESHOLD SUPPORT IAW SRM 51-40-11, ALODINE, PRIMED IAW SRM 51-20-26.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,819 hrs · 51,328 cycles

RIGHT SEAT RAIL HAS NICKS AND CORROSION THE ENTIRE LENGTH BETWEEN X548.1 TO X593.062. REPAIRED SEAT RAIL IAW RD8-53-784. FOUND TO BE WITHIN LIMITS OF RD8-53-784. HFEC INSP PERFORMED IAW -8, -100 NTM 51-00-06. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,819 hrs · 51,328 cycles

RIGHT MID SEAT RAIL HAS NICKS AND CORROSION THE ENTIRE LENGTH ON INBD SEAT RAIL. REPAIRED SEAT RAIL IAW RD8-53-1339. FOUND TO BE WITHIN LIMITS OF RD. HFEC INSPECTION PERFORMED IAW NTM 51-00-06. NO DEFECTS NOTED.

Part: DOOR — CORRODED (LAV SERVICE) · airframe 46,819 hrs · 51,328 cycles

LAV SERVICE PANEL HAS CORROSION AROUND WASTE DRAIN. REMOVED DAMAGE IAW RD8-53-2103. HFEC INSP WAS PERFORMED IAW NTM 51-00-06. NO DEFECTS NOTED. NO LEAKS NOTED IAW MM 21-30-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,819 hrs · 51,328 cycles

SURFACE CORROSION ON ACFT SKIN AT STATION X510.000 AND Z81.000. REMOVED CORROSION ON ACFT SKIN AT STA X510.00 AND Z81.000. FOUND TO BE IN LIMITS IAW SRM CHAPTER 53-00-16. ALODINE, PRIMED AND PAINTED IAW CH 51-20-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,819 hrs · 51,328 cycles

LEFT MID SET RAIL HAS NICKS AND CORROSION THE ENTIRE LENGTH ON THE INBD SEAT REAL. REPAIRED SEAT RAIL IAW RD8-53-1339. FOUND TO BE WITHIN LIMITS OF RD. HFEC INSPECTION PERFORMED IAW DHC 8-100 SERIES NTM 51-00-06. NO DEFECTS NOTED.

Part: COVER — CORRODED (AILERON HINGE) · airframe 46,819 hrs · 51,328 cycles

RT AILERON HINGE COVER HARDWARE CORRODED ON PANELS 643FR, 643ER, 643DR, 643CR, 643BR AND 643GB. REPLACED RT AILERON HINGE COVERS HARDWARE IAW -8 MM 27-12-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 46,819 hrs · 51,321 cycles

PAX ENTRANCE FLOORBOARD CHANNEL TRIM HARDWARE CORRODED. R & R PAX ENTRANCE FLOORBOARD CHANNEL TRIM HARDWARE IAW -8-100, MM 25-22-10.

Part: HINGE BRACKET — CORRODED (PAX DOOR) · airframe 46,819 hrs · 51,328 cycles

LEFT AND RIGHT PAX DOOR FLOOR HINGE BRACKET HARDWARE CORRODED. R & R PAX DOOR FLOOR HINGE BRACKET HARDWARD IAW -8 MM 20-14-01.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 46,819 hrs · 51,328 cycles

PAX AIRSTAIR STRUCTURE BRACKETS HAVE CORROSION. R & R PAX AIRSTAIR STRUCTURE BRACKETS IAW -8 MM 20-14-01.

Part: HMU — ERRATIC (ENGINE) · airframe 46,339 hrs · 50,774 cycles

NR 2 TORQUE FLUCTION ON CLIMBOUT. THEN DURING CRUISE TORQUE DROPPED BY 50 PERCENT WITH NO ACCOMPANIED INDICATION. NR 2 ENGINE MANUAL CAUTION LIGHT DID NOT ILLUMINATE, CREW CYCLED NR 2 ECU TO MANUAL. ENGINE OPERATIONS NORMAL IN MANUAL MODE. CHECKED TORQUE PROBE RESISTANCE AND CHARACTERIZATION OF PLUGS FOR PROP CLASS AND CONTINUITY. CLEANED EEC, HMU AND TORQUE PROBE CONNECTORS. REF CARD 72-01-10X. CHECKED EEC INPUTS FOUND HMU POT ERRACTIC. R & R HMU IAW CARD 73-20-01R, RUN CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,636 hrs · 48,815 cycles

BURNED MARKS 34 TO 42; LOCATED ALONG STA 31P, NEAR X342. REPAIRED WITH DOUBLER IAW EO8-53-10-0222.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,270 hrs · 48,405 cycles

EMERGENCY LIGHT ROW 4 AC ON SIDEWALL HAS ONE LAMP INOP. REMOVED LENS, REMOVED BURNT LIGHT BULB AND INSTALLED NEW BULB, RE-INSTALLED LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,206 hrs · 48,324 cycles

ONE FLOOR LEVEL EMERGENCY LIGHT AT ROW 5 IS NOT WORKING. R & R BULB, CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,096 hrs · 48,193 cycles

EMERGENCY EXIT SIGN ABOVE PAX DOOR ILLUMINATED MOMENTARILY WHEN SELECTED ON FROM FLIGHT ATTENDANT PANEL OR COCKPIT. EMERGENCY LIGHT BATTERIES REMOVED AND REPLACED.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 43,913 hrs · 47,948 cycles

FWD RED FLOOR EMERGENCY HAS 2 BULBS OUT. FOUND BULBS LOOSE, UNATTACHED TO RECEPTACLE. ATTACHED BULBS TO RECEPTACLE. CHECKED GOOD.

Part: SMOKE DETECTOR — BROKEN (CARGO BAY) · airframe 43,888 hrs · 47,955 cycles

IT WAS FOUND THAT THE NR1 BAG BAY SMOKE DETECTOR WAS INOPERATIVE. THE NR 2 SMOKE DETECTOR TESTED OK. THE SMOKE DETECTOR WAS R & R AND THE OPS CHECK WAS GOOD.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 43,856 hrs · 47,914 cycles

RADAR WOULD NOT PAINT WEATHER. R & R RADAR RT IAW MMB 34-29, OPS CKD GOOD.

Part: BULB — BURNED OUT (CABIN LIGHTS) · airframe 43,600 hrs · 47,635 cycles

ELECTRICAL ODOR IN CABIN ROW 9, RT SIDE ASSOCIATED WITH OVERHEAD LIGHTS ON ROW 9. INSPECTED OVERHEAD BIN LIGHTS ON ROW 9, FOUND LAMP HOLDER BURNED ON ROW 9AC AND ROW 9DF. REMOVED AND REPLACED HOLDERS, REMOVED AND REPLACED BALLAST IAW MM 32-20-00. CABIN LIGHTS WERE DEACTIVATED IAW SPP 33.1 CIRCUIT BREAKER SI,S2,AND R2 WERE PULLED AND COLLARED BEFORE MX TASK COULD BE DONE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,447 hrs · 47,459 cycles

ONE RED FLOOR EMERGENCY LIGHT AT ROW 4 IS INOPERATIVE. RELAMP FLOOR EMERGENCY LIGHT IAW AMM 33-52-00.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 43,320 hrs · 47,328 cycles

UPON GEAR EXTENSION, NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED WITH NR 2 HYD QTY INDICATING HALF QT. GEAR WELL SATURATED WITH HYD FLUID. INSTALLED TEMP FLEX LINE AT AFT GEAR DOOR ACTUATOR. OPS/LEAK CHECK GOOD. INSTALL PERMANENT LINE OR COMPLETE WORK CARD 20-50-52T WITHIN 70 HRS.

Part: ADC — FAILED (COCKPIT) · airframe 43,213 hrs · 47,207 cycles

AFTER STARTING NR 2 ENGINE, BURNING ODOR IN COCKPIT. REMOVED AND REPLACED NR 2 DADC IN ACCORDANCE WITH AMM 34-12-02. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH PIEDMONT BULLETIN 34-55

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 42,023 hrs · 45,882 cycles

SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 SMOKE DETECTORS IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 26-12-01. PERFORMED HIDDEN DAMAGE INSPECTION, NO DISCREPANCIES NOTED.

Part: ACTUATOR — FAILED (NLG) · airframe 41,674 hrs · 45,506 cycles

NOSE LANDING GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR EXTENSION, COMPLY WITH ALTERNATE GEAR EXTENSION & NOSE GEAR EXTENDED & LOCKED. CREW REPORTED NO NLG DOOR LIGHT, REMOVED AND REPLACED NLG DOOR ACTUATOR, OP'S CHECK SEVERAL TIMES, LEAK CHECK GOOD IAW MM 32-20-26.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,499 hrs · 45,315 cycles

DURING 'C' CHECK INSPECTIONS, THE RT FORWARD I/B SEAT RAIL WAS FOUND TO HAVE CORROSION MEASURING .020 DEEP. THE SEAT RAIL SECTION WAS REPLACED IAW DHC RD8-53-3074.

Part: SELECTOR VALVE — FAILED (COCKPIT) · airframe 41,475 hrs · 45,288 cycles

NOSE GEAR FAILED TO EXTEND BY NORMAL PROCEDURE, REQUIRED ALTERNATE EXTENSION. REMOVED AND REPLACED GEAR SELECTOR VALVE IN REFERENCE MAINTENANCE MANUAL 32-30-41. REMOVED AND REPLACED GEAR HANDLE SELECTOR VALVE IN ACCORDANCE WITH MAINTENANCE MANUAL 32-30-41. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 41,450 hrs · 45,263 cycles

HOT ODOR COMING FROM NUMBER ONE HOT JUG AREA. PERFORMED HIDDEN DAMAGE INSPECTION ON NUMBER ONE HOT JUG SOCKET (IN ACCORDANCE WITH SPECIAL PROCEDURE 33.1) NO DAMAGE NOTED. PULLED AND COLLARED NUMBER ONE HOT JUG CIRCUIT BREAKER. ITEM ON MEL 25-7, SEE SEQUENCE ONCE, THIS LOG PAGE.

Part: DOUBLER — CRACKED (FUSELAGE)

UPON GEAR EXTENSION DURING FINAL APPROACH TO RUNWAY 35, THE NOSE GEAR RED UNSAFE LIGHT INDICATION ILLUMINATED. BOTH MAIN GEARS LOCKED AND ILLUMINATED GREEN INDICATIONS. THE CREW DISCONTINUED THE APPROACH AND PERFORMED THE ALTERNATE GEAR EXTENSION PROCEDURE. THE GEAR WAS NOT CYCLED PRIOR TO PERFORMING THE ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. OUT OF SERVICE. THE ACFT WILL MAINT FERRY FOR FURTHER IINSPECTION. LT SIDEWALL AT J BEAM DOUBLER CRACKED. (K)

Part: DOUBLER — CRACKED (NLG WW) · airframe 21,233 hrs · 45,035 cycles

UPON GEAR EXTENSION DURING FINAL APPROACH TO RUNWAY 35, NOSE GEAR RED UNSAFE LIGHT INDICATION ILLUMINATED. BOTH MAIN GEARS LOCKED AND ILLUMINATED GREEN INDICATIONS. CREW DISCONTINUED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION PROCEDURED. GEAR WAS NOT CYCLED PRIOR TO PERFORMING THE ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. OUT OF SERVICE. THE AIRCRAFT WILL MTC FERRY TO SBY FOR FURTHER INSPECTION. UPON INSPECTION AT SBY AIRCRAFT DAMAGE RECORDING DESCRIPTION: LT SIDEWALL AT J-BEAM DOUBLER CRACKED. LOCATION: X97.00 AND Z110.00 APPROX. DIMENSIONS: WIDTH-N/A, LENGHT-3.5IN, DEPTH-N/A. DISTANCE FROM FASTENER 1.0IN, STRINGER 1.0IN, FRAME 1.0IN. TYPE OF NDT PERFORMED:

Part: ACTUATOR — BYPASSING (NLG) · airframe 41,157 hrs · 44,959 cycles

FLIGHT 4165 LGA TO ROA. THE GEAR WAS SELECTED DOWN ON APPROACH. THE MAIN GEAR INDICATION WAS NORMAL AND THE NOSE GEAR INDICATION WAS RED. THE ALTERNATE INDICATION WAS NOT INDICATING AND THE APPROACH WAS MISSED. THE GEAR WAS THEN CYCLED FOR A SECOND TIME AND ALL INDICATIONS WERE NORMAL. ALL THREE GEAR DOWN AND LOCKED INDICATED WERE ILLUMINATED BY THREE GREEN LIGHTS. THE PLANE LANDED WITHOUT INCIDENT. IN ROA THE NOSE GEAR WAS SWUNG. IT WAS REPORTED THAT THE NOSE GEAR WAS SLOW AND THE DOORS WOULD STUTTER WHEN OPENING. FLUID COULD ALSO BE HEARD BYPASSING IN THE GEAR WELL. THE NOSE RETRACTION ACTUATOR WAS REMOVED AND REPLACED IN ACCORDANCE WITH MM 32-30-31. THE GEAR WAS AGAIN CYCLED AND THE OPERATIONAL CHECK WAS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING TAKEOFF ROLL THE NR 1 ENGINE MANUAL LIGHT ILLUMINATED. ACFT WAS RETURNED TO THE FIELD. MX CYCLED THE BETA LOGIC CIRCUIT BREAKER AND GROUND RAN THE ACFT. NO DEFECTS WERE NOTED AT THAT TIME. THE ENGINE CONDITION PANEL WAS ALSO CHECKED AND NO FLAGS WERE NOTED AT THAT TIME. ACFT THEN CONTINUED IN SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2)

FLIGHT 4376 - LYH - DURING CRUISE FLIGHT, WHILE REDUCING PROPELLER SPEED TOWARD 900 RPM, NR2 CONDITION LEVER WENT BELOW MIN POSITION RESULTING IN A LOSS OF POWER. WHEN TORQUE RETURNED TO 0, A SUCCESFUL AIR START WAS ACCOMPLISHED. REMOVED FOR AND SENT TO ROA FOR READING RESULTING IN A NO OVERTORQUE CONDITION. INSPECTED ENG MOUNTS AND ECP FOR FLAGS. NO DEFECTS NOTED. IT INSTALLED NEW FDR REFERENCE LOG PAGE 262163-1. PERFORMED POWER ASSURANCE RUN AND AUTOFEATHER CHECK. ALL CHECKS GOOD. (S)

Part: WIRE — BROKEN (HYDRAULIC SYS) · airframe 39,914 hrs · 43,567 cycles

AFTER TAKEOFF NR 1 ENGINE HYD PUMP C/L CAME ON AND WOULD NOT RESET, QTY AND PRESS NORMAL. SBY MX MET A/C, FOUND BROKEN WIRE AT HYD PRESSURE SWITCH CONNECTOR. REPAIRED BROKEN WIRE IAW CHAPTER 20 STANDARD MTN PRACTICES.

Part: ACCESS PANEL — DAMAGED · airframe 39,914 hrs · 43,567 cycles

DURING INSPECTION AFTER INFLIGHT FIRE, ACCESS PANEL 419AT WAS FOUND TO HAVE FIRE DAMAGE. MAINTENANCE REPLACED THE PANEL.

Part: SUPPORT BEAM — DAMAGED (NR 3 FLAP TRACK) · airframe 39,914 hrs · 42,567 cycles

DURING INSPECTION AFTER INFLIGHT FIRE, THE OUTBOARD NR 3 FLAP TRACK SUPPORT BEAM WAS FOUND TO HAVE FIRE DAMAGE. MAINTENANCE REPLACED SUPPORT BEAM.

Part: HYDRAULIC LINE — LEAKING (NR 1 NACELLE) · airframe 39,913 hrs · 43,566 cycles

AFTER DEPARTURE FROM ABE, AT APPROX 200 FT THE CREW NOTICED THE ILLUMINATION CAUTION LIGHTS ASSOCIATED WITH THE NR 1 HYDRAULIC SYSTEM AT APPROX 400 FT. THE CREW WAS ABLE TO VERIFY THAT THE NR 1 HYDRAULIC SYSTEM QUANTITY WAS AT ZERO. THE CREW RETURNED TO THE FIELD AND SHUT THE ENGINES DOWN ON THE RUNWAY AND AWAITED THE GROUND CREW TO TOW THE AIRCRAFT BACK TO THE GATE. ALL PAX ARE OK. AFTER INVESTIGATION OF LEAK MX DISCOVERED EVIDENCE OF A FLASH FIRE UNDER PANEL 419AT, WITH WIRE COATINGS BURNED OFF. LEAK ORIGINATED 8 INCHES OUTBOARD OF NACELLE UNDER PANEL 532AB. PINHOLE FOUND IN HYDRAULIC LINE. LINE WAS REPLACED WITH A TEMP FLEX LINE AND WIRING REPAIRED AFTER BEING FERRIED TO MDT.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 37,435 hrs · 40,856 cycles

RED NOSE GEAR ADVISORY LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CREW DECLARED AND EMERGENCY, CYCLED GEAR BUT INDICATION REMAINED UNSAFE, PERFORMED SEVERAL TOWER FLYBY'S AND GEAR APPEARED TO BE DOWN. FLIGHT LANDED SAFELY. FOUND SEVERAL LARGE CRACKS IN THE NOSE GEAR DECK. REPAIRED DECK AND SURROUNDING STRUCTURE IN ACCORDANCE WITH ENGINEERING ORDER EO8-53-07-3059.

Part: CARRIER ASSY — BURNED (LIGHT SOCKET) · airframe 37,105 hrs · 40,501 cycles

ELECTICAL BURNING ODOR AT ROW 9 LEFT SIDE, CREW FOUND SIDEWALL LIGHT SOCKET BURNED. REPLACED LAMP CARRIER.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,105 hrs · 40,501 cycles

F/A REPORTS BURNING ODOR FROM GALLEY OVERHEAD GASPER VENT. INSPECTED ASSOCIATED AREA NO HIDDEN DAMAGE NOTED, RAN APU WITH BLEEDS ON AND ALL LIGHTS ON, NO DEFECTS NOTED AT THIS TIME.

Part: SEAL — LOOSE (COCKPIT WINDOW) · airframe 35,897 hrs · 39,219 cycles

RATTLING SOUND HEARD FROM ABOVE CAPTAINS SEAT OUTSIDE AIRCRAFT AFTER TAKEOFF. FOUND CAPTAINS WINDSHIELD UPPER INNER PRC SEAL LOOSE, TRIMMED EXCESS PRC SEAL.

Part: SMOKE — DETECTED (COCKPIT) · airframe 35,746 hrs · 39,049 cycles

SMOKE IN CABIN AT 22,000 FEET. MAINTENANCE GROUND RAN AIRCRAFT WITH CREW AND COULD NOT DUPLICATE PROBLEM. UPDATE 07/06/2006 GROUND RAN AIRCRAFT TO MAX POWER WITH BLEEDS ON FOR 10 MINS. FOUND OIL LEVEL IN BOTH ENGINES OVERSERVICED, LOWERED TO PROPER LEVEL.

Part: SENSOR — MISRIGGED (MLG DOOR) · airframe 32,864 hrs · 36,028 cycles

JUST AFTER TAKEOFF THE RIGHT SIDE FORWARD GEAR DOOR CAME OPEN. CREW ELECTED TO RETURN BACK TO MDT. DID NOT DECLARE AN EMERGENCY. FOUND PROXIMITY SWITCH OUT OF RIG, RE-RIGGED, OP'S CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (NR 2 PROP BETA) · airframe 32,761 hrs · 35,930 cycles

NR 2 PROP BETA LOCKOUT FAILURE ON CLIMBOUT. INSTALLED TEST HARNESS AT CONNECTOR J38 & J39 AND TESTED SWITCHES 6121-S10 & S1, 6141 S3 & S4. COMPLETED JOB CARD 61-20-10Q GROUND OPS CHECK OF BETA LOCKOUT. FOUND NO FAULTS WITH BETA LOCKOUT SYSTEM.

Part: WARNING LIGHT — ILLUMINATED (NR 2 HYD SYSTEM) · airframe 32,658 hrs · 35,822 cycles

AFTER TAKEOFF, DURING GEAR RETRACTION, NR 2 ENGINE HYD PUMP CAUTION LIGHT CAME ON. QUANTITY GOOD, GEAR RETRACTED SLOWER THAN NORMAL, 15 SECONDS OR SO, ALSO LIGHT CAME ON DURING SUBSEQUENT GEAR EXTENSION. MAINTENANCE BLEED AIR FROM SYSTEM, SERVICED HYD QUANTITY. RETURNED AIRCRAFT TO SERVICE.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 32,239 hrs · 35,381 cycles

FO'S WINDSCREEN SPIDERWEBBED. REMOVED AND REPLACED FO'S WINDSCREEN OPS CHECK GOOD.

Part: SWITCH — STUCK (RUDDER TRIM) · airframe 31,490 hrs · 34,566 cycles

FLIGHT 4039 NORFOLK TO LGA REPORTED HAVING A RUDDER TRIM ACTUATOR RUNAWAY CONDITION. CREW FOLLOWED THE ABNORMAL PROCEDURES CHECKLIST AND CONTINUED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGA TROUBLESHOT SYSTEM AND FERRIED AIRCRAFT TO MIDDLETOWN FOR MAINTENANCE. MAINTENANCE FOUND THE RUDDER TRIM SWITCH TO BE HANGING UP WHEN SELECTED TOWARDS THE LEFT HAND POSITION. SWITCH WAS REMOVED AND REPLACED. SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SELECTOR — FAULTY (NLG) · airframe 31,465 hrs · 34,543 cycles

RETURNED TO FIELD DUE TO HAVING THE NOSE GEAR INDICATING DOWN AFTER GEAR WAS SELECTED UP. GEAR WAS CYCLED DOWN AND THE CREW RECEIVED 3 GREENS. FLIGHT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT WAS FERRIED FOR REPAIRS. MAINTENANCE FOUND THE GEAR SELECTOR HANDLE TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. GEAR WAS OPERATIONAL CHECKED SEVERAL TIMES WITH NO FAULTS. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 31,051 hrs · 34,125 cycles

FLIGHT 3921 REPORTED CARGO SMOKE LIGHT ILLUMINATING FOR 3 TO 4 SECONDS THEN EXTINGUISHING. FLIGHT ATTENDANT INSPECTED THE AREA AND FOUND NO SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM, ALL CHECKS GOOD.

Part: WIRE — BROKEN (EMERGNECY LIGHT) · airframe 29,731 hrs · 32,781 cycles

PILOT REPORTED EMERGENCY FLOOR LIGHTING ADJACENT TO SEAT 1D WAS BROKEN. MAINTENANCE FOUND ONE RED ROW 1 LIGHT INOPERATIVE, AND REPAIRED AFFECTED WIRE. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 29,369 hrs · 32,392 cycles

DURING ROUTINE MAINTENANCE VISIT LEFT FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. AFTER TROUBLESHOOTING SYSTEM IT WAS DISCOVERED THAT THE EMERGERGENCY LIGHT BATTERY IN POSITION 100 WAS DEFECTIVE. EMERGENCY LIGHT BATTERY WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — SHORTED (GALLEY) · airframe 26,894 hrs · 29,834 cycles

ROC-LGA FLIGHT 3905. CREW REPORTED DURING DESCENT NOTICED A SMOKE ODOR IN COCKPIT AND GALLEY AREA. MAINTENANCE INSPECTED AND FOUND NR 2 HOT JUG RECEPTACLE SHORTED OUT. RECEPTACLE AND HOT JUG REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 26,309 hrs · 29,140 cycles

DURING ROUTINE MAINTENANCE VISIT NOSE GEAR FLOORBEAM AT STATION X97 FOUND CRACKED. CRACK WAS REPAIRED AT FUSELAGE FLOOR BEAM 85310380 AND NESTED DOUBLER IN ACCORDANCE WITH DER CAS AAL76 REVISION A AND DEHAVILLAND REPAIR DRAWING RD8-53-1336 ISSUE 5. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,832 hrs · 26,502 cycles

SYR-FLIGHT 3997. CREW REPORTED FRONT TWO RED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND POWER SUPPLY BAD. POWER SUPPLY AND BATTERY REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,214 hrs · 24,699 cycles

MDT- DURING FLEET INSPECTION, REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4 STRINGER 4 LEFT AND RIGHT SIDES IN APU AREA. CRACKS WERE REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD 8-55-199. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,214 hrs · 24,699 cycles

MDT- DURING FLEET INSPECTION, REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4 STRINGER 4 LEFT AND RIGHT SIDES IN APU AREA. CRACKS WERE REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD 8-55-199. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (PAX DOOR)

BWI - FLT 3900 - MAIN CABIN DOOR VERY DIFFICULT TO OPEN. MAINTENANCE LUBED AND INSPECTED THE AIRSTAIR DOOR LIFT MECHANISM IAW CHAPTER 52. CHECKED WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — FAILED (COCKPIT)

EN ROUTE TO BOS FROM MDT, THE NR 1 ENGINE OIL TEMP WENT OFF SCALE. THE AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND THE TEMP INDICATION AT FAULT. THE OIL TEMP INDICATOR AND BULB WERE REMOVED AND REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — OVERTEMP (E/E BAY)

DURING FLIGHT, THE MAIN BATTERY HOT LIGHT ILLUMINATED THE AIRCRAFT DIVERTED INTO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MAIN BATTERY AT FAULT. REMOVED AND REPLACED MAIN BATTERY IAW DHC PROCEDURES, OPERATIONAL AND TEMPERATURE CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: WINDOW — CRACKED (LT COCKPIT)

DURING CRUISE FLIGHT FROM BOS TO SYR, THE CAPTAINS SIDE WINDOW CRACKED. A/C LANDED WITHOUT INCIDENT IN SYR. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

RIGHT AFT FUSELAGE EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT POSTION NR 600. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERIVCE. (X)

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT PANEL HAS INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: PSEU — MALFUNCTIONED (LANDING)

UPON APPROACH INTO PHL, THE LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. CREW PERFORMED GO AROUND AND THEN GEAR EXTENDED NORMALLY. MAINTENANCE TROUBLESHOT SYSTEM, COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED PSEU AS A PRECAUTION. A/C RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

SEVERAL EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED BULBS. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

TWO LIGHTS INOPERATIVE IN EMERGENCY FLOOR PATH LIGHTING. REPAIRED OPEN CIRCUIT IN EMERGENCY FLOOR PATH LIGHTING WIRING. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (BS 182-222)

DURING A ROUTINE C-CHECK, THE LEFT INBOARD CABIN SEAT RAIL WAS FOUND CORRODED FROM STATION X182.0 TO X222.0. REMOVED CORRODED SECTION OF LEFT SEAT RAIL AND SPLICED IN NEW SECTION IAW RD8-53-1932. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — OIL LEAK (LEFT)

EN ROUTE TO LGA, FLT ATTENDANT REPORTED A HAZE AND SMELL OF SMOKE IN CABIN. LAVATORY SMOKE DETECTOR WAS SOUNDING. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND LEFT ENGINE LEAKING OIL INTO COMPRESSOR SECTION, CAUSING OIL VAPORS TO ENTER CABIN THROUGH BLEED SYSTEM. REMOVED AND REPLACED LEFT ENGINE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: APU BLEED — MALFUNCTIONED (APU COMPT)

UNKNOWN SOURCE OF SMOKE FILLED COCKPIT AND CABIN SHORTLY AFTER TAKEOFF FROM ISP. A/C RETURNED TO FIELD, ISP. MAINTENANCE INSPECTED AND FOUND APU MAKING POPPING NOISE WHEN BLEED IS SELECTED ON. INOP APU BLEED SYSTEM UNDER MEL, RAN A/C, OPERATED ENGINE BLEEDS. FOUND NO DEFECTS. SUBSEQUENT TEST FLIGHT OF A/C PROVED SATISFACTORY. A/C RETURNED TO SERVICE. (M)

Part: CONTL BOX — MALFUNCTIONED (LT MLG)

FLT 3924 - DURING APPROACH, LEFT MAIN LANDING GEAR UNSAFE ANNUNCIATOR DID NOT ILLUMINATE DURING GEAR EXTENSION. REMOVED AND REPLACED ADVISORY LIGHT CONTROL BOX. RETRACTION AND OPERATIONAL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: UPLOCK SWITCH — FAILED (LT MLG)

LEFT MAIN GEAR WILL NOT STAY UP AND LOCKED, GEAR REPEATEDLY UNLOCKS, THEN RETRACTS UP AND LOCKED. REPLACED LT UPLOCK ACTUATOR PROX SWITCH, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. ACTC: 7994. (X)

Part: TEMP MONT — FAILED (BATTERY COMPT)

MAIN AND AUX BATT HOT MASTER WARNING LIGHTS ILLUMINATED. ACFT DIVERTED INTO MDT. REMOVED AND REPLACED BATTERY TEMP MONITOR OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W)