N809EX

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,213 hrs · 66,532 cycles

FORWARD EMERGENCY EXIT LIGHT, CEILING LIGHT AND CENTER CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY BASE.OPS CHECKED GOOD.

Part: PSEU — FAILED · airframe 59,177 hrs · 66,486 cycles

NOTICED ELECTRICAL ODOR IN FLIGHT DECK AND CABIN. INSPECTED AND FOUND PSEU HAD OVERHEAT AND FAILED. R & R PSEU IAW 32-61-50, OPS CK GOOD, OK FOR SERVICE.

Part: HANDSET — MALFUNCTIONED · airframe 58,878 hrs · 66,114 cycles

F/A PANEL EMERGENCY CALL BUTTON ILLUMINATES AND COMMUNICATIONS IS INTERMITTENT. R & R F/A CONTROL PANEL NO FIX. REINSTALLED ORIGINAL PANEL. R & R HANDSET AND CRADLE ASSY. OPS CHECK GOOD IAW MM 23-40-06. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,765 hrs · 65,969 cycles

4TH RED FLOOR EMERGENCY LIGHT OF FWD MOST OF RED LIGHTS INOPERATIVE. REMOVED FWD MOST SECTION OF EMERGENCY FLOOR LIGHT COVER. R & R BULB FOR 4TH RED EMERGENCY FLOOR LIGHT IN FWD MOST SET OF RED LIGHTS. INSTALLED AND SECURED LIGHT COVER IN TRACK INSTALLED, REMOVED BULB, PN OL3071BPEGPL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,765 hrs · 65,969 cycles

RED FLOOR EMERGENCY LIGHT BULB AFT OF FWD LEG OF SEATS 5DF INOPERATIVE. R & R BULB .

Part: UNKNOWN — ODOR (CABIN) · airframe 58,669 hrs · 65,854 cycles

INTERMITTENT ODOR IN FLIGHT DECK DURING FLIGHT. RUBBER LIKE ODOR IAW CREW. RAN BOTH ENGINES WITH BLEEDS SELECTED ON, NO ABNORMAL ODORS NOTED AT THIS TIME OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,674 hrs · 65,861 cycles

AT 3000 FT ON DESCENT A STRONG RUBBER ODOR PRESENT IN FLIGHT DECK, NEAR FLIGHT DECK DOOR. BLEEDS SELECTED OFF NO CHANGE. NO SMOKE VISIBLE, AVIONICS COOLING FAN P/C C/B E-10, WRONG C/B PULLED. RESET C/B E-10 AND PULLED C/B N3 CLG FAN- NO ODOR NOTED.

Part: WARNING HORN — UNKNOWN (TE FLAPS) · airframe 58,650 hrs · 65,826 cycles

FLAPS OUT OF 5 DEG ARC, T/O WARNING SOUNDED ON T/O ROLL. R & R FLAP POSITION INDICATOR GROUND RUN, OPS CHECKED GOOD.

Part: INVERTER — FAILED (PRIMARY) · airframe 58,644 hrs · 65,820 cycles

CREW HEARD CIRCUIT BREAKER TRIP WITH ASSOCIATED SMOKE FROM PANEL. CAPTAIN`S FLIGHT INSTUMENTS AND TRANSPONDER F-8/F-9. FLT DIVERTED. R & R PRIMARY INVERTER, OPS GOOD RESET F-8/F-9. OPS GOOD NO OTHER DAMAGE.

Part: TIMER — INOPERATIVE (DE ICE BOOTS) · airframe 58,304 hrs · 65,417 cycles

RANDOM BOOTS WILL NOT INFLATE IN SEQUENCE ON OCCASION. THREE BOOTS ILLUMINATED AT THE SAME TIME. LIGHTS TESTED NORMAL. PRIMARILY IN FAST. R & R DEICE TIMER. RAN ACFT IAW MM 30-10-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,933 hrs · 64,955 cycles

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

Part: WIRE — OPEN

LT ELEVATOR HORN HEAT CONTROL LIGHT ON IN FLIGHT. FOUND OPEN WIRE BETWEEN PLUGS 3015-J5 AND 3015-J3. R & R WIRES. OPS GOOD.

Part: INVERTER — SMOKE · airframe 57,672 hrs · 64,643 cycles

SMOKE EMANATING FROM LT CIRCUIT BREAKER PANEL. INSPECTED PRIMARY INVERTER CIRCUIT BREAKER PANEL AND ASSOCIATED COMPONENTS. SWAPPED TO AUXILIARY INVERTER, POWERED ACFT WITH NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,374 hrs · 63,068 cycles

FORWARD EMERGENCY EGRESS LIGHT IS DIM ON RIGHT SIDE. R & R BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,324 hrs · 63,068 cycles

MULTIPLE EMERGENCY LIGHTS ARE OUT IN MID CABIN EGRESS LIGHT, AFT CEILING AND AISLE LIGHTS. R & R ALL EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R, 33-50-03R. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,363 hrs · 63,052 cycles

AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY 3351-PS4. OPS CHECKED GOOD.

Part: DISPLAY — INOPERATIVE (WX RADAR SYS) · airframe 56,307 hrs · 62,982 cycles

DURING TAKEOFF, WEATHER RADAR SCREEN WENT BLANK, TCAS OFF MESSAGE AND FDR CAUTION LIGHT ILLUMINATED. SUSPECT RT TRU FAILURE. LOAD AT .07 POWERED DOWN AND POWERED UP ACFT. GROUND RAN ACFT. OPERATED AC AND DC SYSTEMS AND TRU'S IAW DASH 8 RUN UP MANUAL. NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,285 hrs · 62,954 cycles

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

Part: VALVE — INOPERATIVE (DE ICE BOOT) · airframe 56,254 hrs · 62,912 cycles

NR 1 ENGINE INTAKE BOOT DOES NOT APPEAR TO INFLATE WITH LT NR 3 WING BOOT ADVISORY LIGHT NO ILLUMINATING. R & R DISTRIBUTOR VALVE & PRESSURE SWITCHES IN REF TO D8MM 30-10-16. OPS CHECK GOOD AT THIS TIME. HA300 SEQ NR 4 FOR L/E R & R.

Part: WINDOW — BURNED (COCKPIT) · airframe 56,246 hrs · 62,902 cycles

EVIDENCE OF HEATING ELEMENT BURNED ON CAPTAIN'S WINDOW. VISIBILITY WAS OBSCURED WITH HEAT APPLIED. REPLACED CAPTAINS SIDE WINDOW REF W/C 56-00-01R.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,684 hrs · 62,233 cycles

EMERGENCY LIGHT ON RIGHT SIDE BURNED OUT. R & R THE BULB. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,608 hrs · 62,131 cycles

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

Part: PCU — UNKNOWN · airframe 55,460 hrs · 61,953 cycles

DURING TAKEOFF ROLL, ADJUSTED NR 1 PCU SPEEDER SCREW COUNTER CLOCKWISE APPROX. .2500 TURN IAW MM 61-22-00. GROUND RAN ACFT. OPS CHECKED GOOD IAW RUN UP MANUAL.

Part: APU — SMOKE · airframe 55,415 hrs · 61,905 cycles

WHILE APU IS RUNNING WITH BLEEDS OFF, NOTICED WHITE SMOKE COMING FROM VENT, FROM UNDER APU EXHAUST. AUXILIARY POWER UNIT COMPLIED WITH MAINTENANCE PROCEDURES.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,084 hrs · 61,487 cycles

FORWARD EMERGENCY EXIT SIDEWALL LIGHT HAS ONE BULB INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (CONTROL PANEL) · airframe 54,739 hrs · 61,079 cycles

F/A'S EMERGENCY LIGHT SWITCH BACKLIGHTING IS INOPERATIVE IN NORM POSITION. R & R BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,618 hrs · 60,928 cycles

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

Part: UNKNOWN — ODOR (CABIN) · airframe 54,592 hrs · 60,896 cycles

ODOR IN CABIN, OPERATED ENGINE BLEEDS IN VARIOUS MODES. NO ODOR.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 53,961 hrs · 60,127 cycles

DURING TAKEOFF ROLL, NR 2 OIL PRESSURE ADVISORY LIGHT ILLUMINATED. SHUTDOWN ENGINE AND RETURNED TO GATE. LOWER COWL AND FOUND OIL DRIPPING FROM FORWARD END DRAINS. REMOVED LOWER COWLING. CLEANED EXCESSIVE OIL AND R & R NR 2 ENGINE IAW WC 71-00-01A AND 71-00-02A. REINSTALLED LOWER COWLING. OPS AND LEAKED CHECKED GOOD. AC GENERATOR DETACHED FROM THE MOUNTING FLANGE, STUDS STILL ATTACHED TO GENERATOR. MOUNTING PAD, MPN 3106143-01.

Part: WARNING HORN — FALSE ACTIVATION · airframe 53,838 hrs · 59,982 cycles

BETA LOCKOUT HORN CAME ON AFTER 50 FEET CONTINUOUSLY. RETURN TO FIELD, FUNCTION CHECKED SYSTEM. OPS CHECKED OK IAW 61-20-10.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 53,750 hrs · 59,874 cycles

INBD SIDE OF NR 2 NACELLE HAS SEVERAL RIVET HEADS WORN AT LOWER FWD CORNER OF SKIN. REMOVED RIVETS AND INSTALLED PATH ON INBD FORWARD SIDE SKIN OF NR 2 NACELLE IAW RD8-54-1045. COMPLIED WITH HFEC INSPECTION.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 53,750 hrs · 59,874 cycles

CORROSION ON RT FORWARD SEAT TRACK IN AREA OF LAVATORY AND GALLEY. REPAIRED RT SEAT TRACK IAW RD8-53-3074.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 53,750 hrs · 59,874 cycles

CRACKED ANGLE ON FORWARD SIDE OF NR 2 NACELLE HORSE COLLAR ABOVE OTBD BOLT. COMPLIED WITH EO8-54-13-0677.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 53,750 hrs · 59,874 cycles

PAX DOOR THRESHOLD MEMBER CORRODED. R & R PAX DOOR THRESHOLD ASSY IAW DWG 85321241.

Part: MONITOR — FAULTED (AC SYSTEM) · airframe 53,688 hrs · 59,799 cycles

NR 1 AC GENERATOR SHOWING NO VOLTAGE ON PHASE A OR B IN FLIGHT. FOUND ACFT POWER MONITOR AT FAULT. R & R ACFT POWER MONITOR. RAN ACFT, OPS CHECKED GOOD IAW MM 24-21-05.

Part: INDICATOR — INOPERATIVE (STDBY ATTITUDE) · airframe 53,203 hrs · 59,228 cycles

STANDBY ATTITUDE INDICATOR WILL NOT CAGE AND SHOWS INVERTED. R & R STANDBY INDICATOR IAW MM 34-22-01. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 52,854 hrs · 58,805 cycles

F/A EMERGENCY LIGHT ON/OFF SWITCH IS OUT. REMOVED SWITCH, R & R BULB, REINSTALLED FILLER PANEL. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 52,854 hrs · 58,805 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,793 hrs · 58,724 cycles

RT FUSELAGE MOUNTED AFT EMERGENCY LIGHT IS DIM. REMOVED LENS, R & R BULB. REINSTALLED LENS, OPS CHECKED GOOD.

Part: CONTROL CABLE — OUT OF ADJUST (RUDDER) · airframe 51,911 hrs · 57,641 cycles

DURING DESCENT ACFT ENCOUNTERED MODERATE WIND SHEAR CAUSING ACFT TO EXCEED 260 KNOTS FOR 3 SECONDS. NO LOSS OF CONTROL JUST MODERATE BUFFETING. CHECKED CABLE TENSION OF RUDDER CONTROL SYS. FOUND TENSION LOW ON RUDDER CABLE CIRCUIT. ADJUSTED IAW MM 27-20-00. CHECKED CABLE TENSION ON ELEVATOR CONTROL SYS FOR TENSION. LOW ON LT CIRCUIT. ADJUSTED IAW MM 37-32-00. OPS CHECKED GOOD. CHECKED AILERON CONTROL SYSTEM. FOUND CABLE TENSION TO BE WITHIN LIMITS. OK FOR SERVICE.

Part: SOCKET — DAMAGED (CABIN LIGHT) · airframe 51,716 hrs · 57,417 cycles

CENTER ISLE LIGHT AT 1DF STARTS TO SMOKE. CIRCUIT BREAKERS S1, S2 AND R2 WERE PULLED AND COLLARED.

Part: WINDSCREEN — SMOKE (COCKPIT) · airframe 51,539 hrs · 57,208 cycles

IN FLIGHT, LT WINDSHIELD PRODUCED SMOKE AND WAS THEN TURNED OFF. HAD NO ASSOCIATED CAUTION LIGHTS. R & R CAPTAIN'S WINDSCREEN IAW WC 56-00-00R. OPS AND LEAKED CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 51,337 hrs · 56,961 cycles

EMERGENCY FLOOR PATH LIGHT, THIRD FROM FRONT IS INOPERATIVE. R & R BULB FOR FLOOR EMERGENCY PATH LIGHT, 3RD FRONT FRONT. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,881 hrs · 55,220 cycles

NR 2 HYD QTY DROP TO .5 QT IN FLIGHT, NR 2 ISOLATION VALVE LIGHT ILLUMINATED. INSPECTED AND FOUND HYD LINE LEAKING BEHIND NR 1 GRAVEL GUARD. INSTALLED TEMP FLIGHT LINE IAW SP20.1. SERVICE HYD, GROUND RAN ACFT, LEAK CHECKED GOOD.

Part: FIREWALL — CRACKED (NR 2 NACELLE) · airframe 49,827 hrs · 55,157 cycles

RADIUS CRACK NOTED ON NR 2 NACELLE AFT FIREWALL. REPAIRED IAW RD 8-54-1565. COMPLIED WITH HFEC INSP AFTER REMOVING DAMAGE. NO CRACKS NOTED.

Part: SHROUD — CRACKED (JET PIPE) · airframe 49,827 hrs · 55,157 cycles

AFT NACELLE FIREWALL JET PIPE SHROUD ABOVE THE JET PIPE IS CRACKED AT THE 10 O'CLOCK AND 11 O'CLOCK POSITION. REMOVED NACELLE ANGLE. LOCATED, DRILLED ANGLE. INSTALLED ANGLE IAW DWG 85410224 AND SRM 61-40-11. PROSEAL AREA WITH PROSEAL 700 ON NR 2 NACELLE.

Part: ANGLE — CRACKED (NACELLE FIREWALL) · airframe 49,827 hrs · 55,157 cycles

CRACKS NOTED ON NR 2 NACELLE AFT FIREWALL. REMOVED ANGLE, PARTIALLY DRILLED ANGLE TO EXISTING FIREWALL STRUCTURE. INSTALLED ANGLE IAW DWG 85410224 AND SRM 51-40-11. SEALED WITH PRO-SEAL 700.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 49,826 hrs · 55,155 cycles

LT FUSELAGE FORWARD EMERGENCY EGRESS LIGHT IS INOPERATIVE. R & R BATTERY IAW MM 33-51-00. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,826 hrs · 55,155 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,180 hrs · 54,389 cycles

EMERGENCY FLOOR PATH LIGHT INOPERATIVE AT ROW 4DF. R & R BULB IAW MM 33-51-11.

Part: ACTUATOR — CRACKED (SPOILER) · airframe 49,180 hrs · 54,389 cycles

NR 1 HYD ISOLATION LIGHT ILLUMINATED ALONG WITH INBD ROLL SPOILER HYD CAUTION LIGHT. NR 1 HYD QUANTITY AT 1.1. FOUND BACK SIDE OF ACTUATOR CRACKED. R & R SPOILER ACTUATOR IAW MM 27-14-05. PERFORMED OPS CHECK IAW AMM 27-14-00. LEAKED CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,969 hrs · 54,150 cycles

ROW 1 RED FLOOR EMERGENCY LIGHT IS BURNED OUT. R & R ROW 1 FLOOR EMEERGENCY LIGHT BULB AS REQUIRED. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 48,809 hrs · 53,961 cycles

EMERGENCY LIGHT AT ROW 1DF NOT WORKING (3RD 1 FROM FRONT) FOUND BROKEN WIRE SPLICE, R & R WITH NEW SPLICE. OPS CHECKED GOOD.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 48,593 hrs · 53,722 cycles

PAX DOOR STAIR ASSY VERTICAL SUPPORT, FORWARD OTBD AND INBD BRACKET HAS CORROSION ON IT. REMOVED BOTH BRACKETS, INSTALLED NEW BRACKETS IAW DWG 85210004.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 48,593 hrs · 53,722 cycles

FORWARD UPPER PAX DOOR SKIN TO STEP ATTACH POINT IS CRACKED ON STAIR ASSY. REMOVED OLD BRACKET. INSTALLED NEW BRACKET IAW DWG 85210004.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,593 hrs · 53,722 cycles

RT OTBD SEAT RAIL HAS MINOR CORROSION AT LOCATION X240, X264, X290, X328 AND X342. BLENDED CORROSION AWAY WITHIN LIMITS IAW RD8-53-1342. PERFORMED HFEC. NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,593 hrs · 53,722 cycles

LEFT OTBD SEAT RAIL HAS MINOR CORROSION. BLENDED CORROSION AWAY WITHIN LIMITS IAW RD8-53-1342 AND RD8-53-3644. PERFORMED HFEC INSP. NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (BS 200-205) · airframe 48,593 hrs · 53,722 cycles

LT SIDE INBD SEAT RAIL SEVERLY CORRODED AT X200 TO X205. CUTOUT CORRODED SET RAIL SECTION IAW RD8-53-3074, SPLICED LT INBD SEAT RAIL IAW RD8-53-3074 AND DWG NR 8520019.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 48,593 hrs · 53,722 cycles

PAX DOOR THRESHOLD PANEL AREA CORRODED. REMOVED PAX DOOR THRESHOLD ASSEMBLY. INSTALLED NEW THRESHOLD ASSEMBLY IAW DWG 85321241.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,593 hrs · 53,722 cycles

RT SIDE INBD SEAT RAIL HAS MINOR CORROSION AROUND LAV MOUNTING HOLES. BLENDED CORROSION AWAY WITHIN LIMITS IAW RD8-53-4698. PERFORMED HFEC INSP, NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,593 hrs · 53,722 cycles

LT INBD SEAT RAIL HAS MINOR CORROSION AT LOCATIONS X345, X372. BLENDED CORROSION AWAY WITHIN LIMITS IAW RD8-53-1339. COMPLIED WITH HFEC INSP, NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,593 hrs · 53,722 cycles

LIGHT INBD SEAT RAIL HAS FRETTING CORROSION FROM FLOOR PANELS AT X224 TO X312. BLENDED CORROSION AWAY WITHIN LIMITS IAW RD8-53-1339 AFT OF STA X262. PERFORMED HFEC. NO CRACKS FOUND.

Part: SWITCH — OUT OF ADJUST (COCKPIT) · airframe 45,186 hrs · 49,853 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS. ADJUSTED NR 1 CONDITION LEVER MICRO SWITCH AND PERFORMED WORKCARD 31-50-00Q. OPERATIONAL CHECKED GOOD.

Part: ANTI-ICE SYSTEM — FAILED (WINDSHIELD) · airframe 45,004 hrs · 49,654 cycles

IN FLIGHT FIRST OFFICERS WINDSHIELD LOST POWER, NO LOADS. FOUND 3041 K6 INTERMITTENT CYCLED NORMALLY 2 OR 3 TIMES, THEN FAILED. REPLACED K6 OM FIRST OFFICER'S WINDSHIELD, CYCLED NORMALLY. REFERENCE WIRE MANUAL 30-41.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,455 hrs · 49,035 cycles

ROW 1 FLOOR EMERGENCY LIGHTS HAS ONE LAMP NOT WORKING. REMOVE AND REPLACE BULB ON ROW 1 FLOOR EMERGENCY LIGHT. REF AMM 33-51-11.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 44,405 hrs · 48,980 cycles

DURING CLIMB OUT NR 1 ENG TORQUE FLUCTUATED FROM 90 PERCENT TO 50 PERCENT THEN BACK TO 90 PERCENT WITH NO ASSOCIATED CAUTION LIGHTS. INSPECTED AND FOUND C/B J7, NOT PULLED AND COLLARD IAW MEL 73-2. NR 1 ENG ECU PREVIOUSLY ON MEL REFERENCE LOG PAGE 036751, ITEM 1, PULLED AND COLLARED CB J7 ON RT ESSENCUAL BUSS, GROUND RUN ACFT, OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 44,316 hrs · 48,884 cycles

AT 8,000 FT. DESCENDING FOR AIRPORT, NR 1 RUDDER ISO VALVE C/L AND ROLL SPOILER INBD HYD C/L ILLUMINATED. NR 1 HYD QTY INDICATION 1.2 QUARTS AND NACELLE GAUGE INDICATES 0.5 QUARTS. (CAPTAIN DECLARED EMERGENCY, LANDED UNEVENTFUL. INSTALLED TEMP FLEX LINE FROM NR 2 NACELLE TO RT INBD ROLL SPOILER. SERVICED HYD SYS, BLED LINES, RE SERVICED HYD SYS. RUN UP LEAK CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,953 hrs · 47,347 cycles

FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTING ON RIGHT FUSELAGE IAW 33-51-00-08. NO FIX. RE-ATTACHED BULB CONNECTION BEHIND LAVATORY. OPERATIONAL CHECK GOOD.

Part: PSU — SMOKE (CABIN) · airframe 42,345 hrs · 46,664 cycles

PSU AT ROW 4 DF SMOKED. PERFORM HIDDEN DAMAGE INSPECTION, DEACTIVATED UNIT PER SP 23.3

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS FLASHED OFF AND ON DURING TOUCHDOWN. PILOT REPORTED TO MAINTENANCE. PERFORMED EMERGENCY LIGHTS CHECK PER WORK CARD 33-50-03. OPS CHECK GOOD. (S)

Part: LIGHT — BROKEN (CABIN) · airframe 41,079 hrs · 45,234 cycles

EMERGENCY LIGHT AT 4DF ON SIDEWALL IS BROKE. REPLACED EMERGENCY EXIT LIGHT, OPS CHECK GOOD.

Part: OIL SYSTEM — LOW (APU) · airframe 40,757 hrs · 44,875 cycles

OIL SMELL IN CABIN. APU BLEED AIR ON. APU WAS FOUND TO BE LOW ON OIL.

Part: LIGHT — BROKEN (CABIN) · airframe 40,005 hrs · 44,055 cycles

FLOOR LEVEL EMERGENCY LIGHTING AT ROW 4 IS BROKEN. REINSTALLED ONE RED EMERGENCY FLOOR LIGHT CAPTION. OPERATIONAL CHECK GOOD.

Part: RADAR — INOPERATIVE (WEATHER RADAR) · airframe 39,293 hrs · 43,263 cycles

FLIGHT 4353 MDT/PHL RETURNED TO MDT DUE TO THE WX RADAR WENT INOP. DUE TO WEATHER EN ROUTE THE FLIGHT COULD NOT CONTINUE. THE FLIGHT RETURNED TO MDT WITHOUT INCIDENT.

Part: DIODE — ACTIVE (MLG) · airframe 387,989 hrs · 42,711 cycles

AFTER GEAR RETRACTION RECEIVED AN AMBER LEFT GEAR DOOR LIGHT. CYCLED GEAR RESULTING IN LEFT GEAR DOOR LIGHT ILLUMINATED MOMENTARY, THEN EXTINGUISHED. THEN LANDING GEAR INOP C/L. RETURNED TO FIELD. REMOVED AND REPLACED DIODE 3261-CR3. OPS CHECK GOOD.

Part: PSEU — UNKNOWN (MLG)

AFTER GEAR RETRACTION GOT AN AMBER LEFT GEAR DOOR LIGHT FOLLOWED BY A CLUNKING NOISE AND FLASHING GEAR INOP CAUTION LIGHT. ACFT DIVERTED TO ROA AND SWAPPED WITH ACFT 943/HRH. CREW PERFORMED AN ALTERNATE EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG LANDING GEAR SEVERAL TIMES. CND, REMOVED AND REPLACED PSEU AS A PRECAUTION. OPS CHECK GOOD.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 38,504 hrs · 42,407 cycles

AIRCRAFT DEPARTED DCA, ON CLIMBOUT, THE CREW HEARD A CRACKING NOISE COMING FROM THE CAPTAIN'S SIDE WINDSHIELD. LEVELED OFF AT 5000 FT AND THE NOISE WENT AWAY. CAPTAIN MADE AN INSPECTION OF WINDSHIELD AND FOUND LIKE WINDOW IS CRACKING. THE CAPTAIN DIVERTED TO BWI. MAINTENANCE INSPECTED WINDOW AND FOUND NO CRACKS. NO DEFECTS FOUND. CAPTAINS SIDE WINDOW REPLACED 4/22/07 AS A PRECAUTION.

Part: ECU — FAILED (ZONE 400) · airframe 36,446 hrs · 40,123 cycles

ON CLIMBOUT NR 1 ENGINE SURGED 10 TO 15 PERCENT TQ. ALSO NR 1 ENGINE WOULD NOT GO TO FLIGHT IDLE. REMOVED AND REPLACED NR 1 ECU GROUND RAN AND TRIMMED BOTH ENGINES.

Part: STRUT — CRACKED (NLG) · airframe 32,962 hrs · 36,417 cycles

DURING MAINTENANCE MIDDLETOWN, IT WAS DISCOVERED THAT AIRCRAFT 809EX HAD A 7 INCH CRACK FROM THE TOP AFT CENTER EDGE OF NOSE LANDING GEAR STRUT BODY DOWNWARD. MAINTENANCE REMOVED AND REPLACED THE STRUT ASSEMBLY.

Part: WARNING HORN — MALFUNCTIONED (BETA SYSTEM) · airframe 32,841 hrs · 36,293 cycles

FLIGHT NR 4082 REPORTED HAVING THEIR BETA WARNING HORN SOUND WITH LOSS OF NORMAL BRAKING WHEN POWER LEVERS WERE SELECTED BELOW FLIGHT IDLE DURING GROUND HANDLING. IT WAS DETERMINED THAT THE BETA WARNING HORN SYSTEM WAS AT FAULT, SYSTEM WAS MEL'D AND DEACTIVATED. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,749 hrs · 35,140 cycles

MAINTENANCE REPORTED A HOLE IN FUSELAGE AFT OF AIRSTAIR DOOR AT STATION 264.THE HOLE WAS REPAIRED PER CALLAHAN RD CAS-AAL170, WHICH REQUIRED THE DAMAGE BE REMOVED AND CRACK CHECKED THEN INSTALLING A BOLT WASHER AND NUT AND SEALING SAME WITH PRC.DAMAGE DRAWING WAS SUBMITTED TO BOMBARDIER FOR TOLERANT ANALYSIS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: REGULATOR VALVE — FAULTY (RUDDER) · airframe 31,483 hrs · 34,849 cycles

FLIGHT 3996 HAD TO RETURN TO FIELD DUE TO HAVING THE NR 2 RUDDER HYDRAULIC, RUDDER PRESSURE, AND RUDDER FULL PRESSURE LIGHTS ILLUMINATE AFTER TAKEOFF. MAINTENANCE FOUND THE RUDDER PRESSURE REGULATOR VALVE TO BE AT FAULT. THE RUDDER PRESSURE REGULATOR VALVE WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAULTY (FIRE DETECTION) · airframe 31,304 hrs · 34,677 cycles

AIRCRAFT APU HAS A HISTORY OF THE FIRE FAULT AND CHECK FIRE DETECT LIGHTS ILLUMINATING AFTER SHUTTING DOWN THE APU. MAINTENANCE HAS COMPLIED WITH SEVERAL CHECKS AND HAS REPLACED THE RELAYS 2623-K1 AND 2622-K2.SYSTEM HAS NO HISTORY SINCE. SYSTEM OPERATIONAL CHECK GOOD.

Part: SILL — DAMAGED (FUSELAGE) · airframe 30,717 hrs · 34,089 cycles

WHILE AIRCRAFT 809EX WAS IN ROUTINE MAINTENANCE, IT WAS FOUND THAT THE BAGGAGE DOOR UPPER SILL HAD BEEN DAMAGED FROM THE BAGGAGE DOOR HANDLE COMING IN CONTACT WITH THE SILL. MAINTENANCE COMPLIED WITH REPAIR DRAWING8-53-3334 ISSUE 2. AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: ANGLE — CRACKED (NLGWW) · airframe 29,292 hrs · 32,516 cycles

DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING A INSPECTION TASK 5340/01 NOSE LANDING GEAR WELL RT ZEE MEMBER AT STATION X97, NOSE LANDING GEAR WELL TRUNNION RIGHT SIDEWALL WEB AND SIDEWALL ANGLE AT STATION X101 WERE FOUND TO BE CRACKED. CRACKS WERE REPAIRED IN ACCORDANCE WITH DEHAVILLAND DASH 8 REPAIR DRAWINGS RD8-53-764, RD8-53-458, AND RD8-53-3630. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 27,023 hrs · 30,089 cycles

DURING ROUTINE MAINTENANCE VISIT CENTER AISLE EMERGENCY LIGHT ON CEILING FOUND INOPERATIVE. CANNON PLUG FOUND TO BE DISCONNECTED IN CEILING. CANNON PLUG RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,733 hrs · 29,773 cycles

MDT-BOS. FLIGHT 3715. CREW REPORTED DURING CRUISE FLIGHT 20 MI FROM MDT OUTER LAYER OF CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT RETURNED TO MDT FOR REPAIRS. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IAW MM 56-10-11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPRING — BROKEN (RIGHT) · airframe 26,477 hrs · 29,477 cycles

DURING A CHECK INSPECTION RIGHT MAIN LANDING GEAR UPLOCK HOOK FOUND TO HAVE ONE BROKEN RETRACTION SPRING. SPRING WAS REPLACED IN ACCORDANCE WITH MESSIER DOWTY COMPONENT MAINTENANCE MANUAL 32-30-21. AIRCRAFT RETURNED TO SERVICE.

Part: LINK — WORN (NLG) · airframe 26,005 hrs · 28,955 cycles

MDT- CREW REPORTED NOSE WHEEL SHIMMY ON LANDING ROLL OUT. MAINTENANCE REPLACED THE NOSE LANDING GEAR SHOCK STRUT PISTON CAP, LINK , UPPER AND LOWER PINS. ALSO REPLACED WERE THE NOSE GEAR STEERING ACTUATOR LINKS. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (LEFT) · airframe 25,727 hrs · 28,635 cycles

BOS-ABE FLIGHT#3898. WHILE ENROUTE TO ABE @ 14,000 FT CAPTAIN SIDE WINDOW CRACKED. FLIGHT DIVERTED TO BGM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CAPTAINS SIDE WINDOW IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — LOOSE (LT NACELLE) · airframe 25,522 hrs · 28,404 cycles

DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, ONE RIVET FOUND MISSING AND ONE FOUND PULLING THROUGH ON LEFT NACELLE OUTBOARD END PLATE JUST BELOW FLAP TRACK. THREE RIVETS REPLACED ON OUTBOARD LEFT NACELLE JUST BELOW FLAP TRACK IN ACCORDANCE CALLAHAN REPAIR SERVICES DER 8110 FORM CAS-AAL09. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 25,162 hrs · 28,013 cycles

DURING ROUTING MAINTENANCE VISIT RIGHT SIDE NOSE COMPARTMENT FLOOR CRACKED. CRACK REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD 8-53-3893. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT)

IN CRUISE FLIGHT AT 17,000 FEET THE CAPTAIN SIDE WINDOW CRACKED. CREW DESCENDED AND LANDED AT AVP WITHOUT INCIDENT.

Part: TRIM — FROZEN (ELEVATOR)

BUF-BWI - FLIGHT 3610 RETURNED TO BUF - DURING CRUISE ATTEMPTED TO DESCEND USING THE AUTO PILOT. CREW RECEIVED A MISTRIM LIGHT AND TURNED OFF AUTO PILOT. EXPERIENCED AN OUT OF TRIM CONDITION. THE ELEVATOR TRIM WOULD NOT ADJUST MANUALLY, TEMPERATURE -19C. MAINTENANCE INSPECTED AND FOUND THE ELEVATOR TRIM TO OPERATE NORMALLY, FREEZING SUSPECTED. THE TABS AND ACTUATORS WERE INSPECTED AND LUBRICATED IAW DHC PROCEDURES. OPERATIONAL CHECK PROVED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (RUDDER)

BGM-DURING PERFORMANCE OF AN A1 INSPECTION THE TRAILING RUDDER WAS FOUND CRACKED IN TWO PLACES. MAINTENANCE PERFORMED REPAIRS IAW BOMBARDIER RD8-55-158.

Part: BULB — FAILED (CABIN)

FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH INTERNAL LAMP INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (COCKPIT)

COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT REMAINS ILLUMINATED WHEN POWER IS SHUT OFF. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: WIRE — FAILED (CABIN)

FORWARD CENTER AISLE CABIN FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPAIRED FORWARD CENTER AISLE FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM WIRING. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BULBS — FAILED (CABIN)

THREE FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BURNED BULBS, SYSTEM CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: VALVE — FAILED (RT ENGINE)

RIGHT ENGINE OIL TEMP REACHED 113 DEGREES AND WAS SLOWLY CLIMBING. MADE PRECAUTIONARY DIVERSION INTO BGM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, FOUND THE NR 2 ENGINE OIL COOLER DIVERTER VALVE AT FAULT. VALVE WAS REPLACED, SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: LIGHT — LOOSE (CABIN)

ROW ONE EMERGENCY EXIT LIGHT DETACHED FROM WALL. RESECURED EMERGENCY LIGHT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: LIGHT — CRACKED (CABIN)

LEFT MID CABIN, LOWER EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

THREE EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPAIRED OPEN CIRCUIT UNDER FLOOR PANEL. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COVER — MISSING (CABIN)

EMERGENCY EXIT LIGHT COVER MISSING IN ROW 4F, RT SIDE. INSTALLED NEW ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — FAILED (NR 1 ENGINE)

NR 1 ENGINE FAILED WHEN ECU SELECTED TO MANUAL. FOUND LEFT ECU WING ROOT CANNON PLUG 9811-P13 WET, BACK SHEEL FULL OF WATER AND DE-ICE FLUID. CLEANED, DRIED AND RECONNECTED CONNECTOR. UPON ENGINE RUN, CIRCUIT BREAKER L6 POPPED AND WOULD NOT RESET. REMOVED AND REPLACED ELECTRICAL CONNECTOR 9811-P13. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

DURING CRUISE FLIGHT, THE CREW NOTICED A STRONG ODOR OF SMOKE OR OIL COMING FROM THE BLEED SYSTEM. A/C MADE AN EMERGENCY LANDING IN BOS. MAINTENANCE PERFORMED AN INSPECTION AND RELEASED THE A/C FOR A FERRY FLIGHT TO MDT. (NOTE: ODOR/SMOKE DISSIPATED WHEN THE ENGINE BLEEDS WERE SELECTED OFF). MDT MAINTENANCE TROUBLESHOT THE BLEED SYSTEM AND DETERMINED THE LEFT ENGINE WAS AT FAULT. REMOVED AND REPLACED THE LEFT ENGINE IAW MM. A/C RETURNED TO SERVICE. (X)