N839EX

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,924 hrs · 66,908 cycles

TW0 MOST FORWARD FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT ROW 3, RIGHT HAND CEILING LOCATION. OPS CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (PFCS) · airframe 58,797 hrs · 66,750 cycles

WITH FLAPS OUT OF ZERO DETENT, LT RUDDER TRAVEL IS ONLY 10 DEGREES AND RT IS 16 DEGREES. R & R PFCS INDICATOR GROUND RAN ACFT, OPS CHECK GOOD IAW 27-05-00.

Part: SWITCH — MALFUNCTIONED (HEATER) · airframe 57,927 hrs · 65,725 cycles

LT ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED WITH NO LOADS. SWAPPED ELEVATOR HORN HEAT SWITCH 3015-S4 AND 3015-S5 TO ALTERNATE POSITION. GROUND RAN ACFT WITH CREW. OPS CHECKED GOOD IAW SRT MANUAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,776 hrs · 65,543 cycles

EMERGENCY OVERHEAD LIGHT IS INOPERATIVE. R & R BULBS IN OVERHEAD EMERGENCY LIGHT . OPS CHECKED GOOD.

Part: INVERTER — ODOR (PRIMARY) · airframe 57,728 hrs · 65,489 cycles

FISH ODOR STRONG IN GALLEY AREA. R & R PRIMARY INVERTER IAW 24-22-00. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 57,539 hrs · 65,258 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 8DF. REPAIRED EMERGENCY FLOOR PATH LIGHT WITH NEW WIRE SPLICE IAW MM 20-45-07. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,550 hrs · 61,988 cycles

CABIN FLOOR EMERGENCY LIGHT IS INOPERATIVE, 6TH FROM FRONT. R & R BULBS FOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,245 hrs · 64,904 cycles

FORWARD LT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. , R & R THE BULB. OPS CHECKED GOOD.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 56,601 hrs · 64,121 cycles

NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED, ROLL SPOILER INBD HYD CAUTION LIGHT CAME ON AND OFF SEVERAL TIMES, BUT EXTINGUISHED. HYDRAULIC PRESSURE WAS GOOD FOR THE FLIGHT, BUT QUANTITY WAS LOW. ALL OTHER INDICATIONS NORMAL. R & R O-RING ON PRESSURE FITTING, OTBD ROLL SPOILER ACTUATOR. GROUND RAN. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,580 hrs · 64,097 cycles

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

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,016 hrs · 63,418 cycles

F/A EMERGENCY SWITCH LIGHT GREEN BULB INOPERATIVE ON F/A SWITCH PANEL ABOVE WARDROBE. REMOVED COVER LENS R & R BULB AND REINSTALLED COVER LENS.

Part: WARNING HORN — FALSE ACTIVATION · airframe 55,652 hrs · 62,996 cycles

DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. RETURNED TO GATE. RAN ACFT IN PROPER CONFIGURATION AND NO DISCREPANCIES NOTED.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 55,271 hrs · 62,546 cycles

EMERGENCY EXIT SIGN ON FLOOR BESIDE PASSENGER DOOR IS DIM. R & R BULB. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 54,962 hrs · 62,178 cycles

HYDRAULIC LEAK IN NOSE WHEEL WELL. INSTALLED NLG DRAG STRUT ACTUATOR BLUE FLEX LINE. CYCLED GEAR. NO LEAKS NOTED. CHECKED GOOD.

Part: CONTACTOR — BURNED (APU) · airframe 54,500 hrs · 61,619 cycles

APU FAIL LIGHT ILLUMINATED DURING START. AUX AND MAIN CIRCUIT BREAKERS TRIPPED. SMOKE, FIRED BOTTLE. FOUND APU START CONTACTOR WELDED. COLLARED CIRCUIT BREAKER. R & R APU START CONTACTOR AND SMALL CABLE ASSY, EGT, SWAP HARNESS IAW BULLETIN 49-8. OPS CHECKED GOOD.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR) · airframe 54,228 hrs · 61,288 cycles

WEATHER RADAR NOT PAINTING CORRECTLY. R & R RADAR TRANSCEIVER IAW MM 34-41-04 AND BULLETIN 34-18. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,150 hrs · 61,191 cycles

FORWARD EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 1DF. R & R BULBS AT EMERGENCY FLOOR PATH LIGHT IN ROW 1DF. OPS CHECKED GOOD.

Part: BRUSH BLOCK — DIRTY (NR 1 GENERATOR) · airframe 53,532 hrs · 60,450 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED ON TAKEOFF RUN. CREW ABORTED TAKEOFF. CYCLED NR 1 AC GENERATOR SWITCH IAW CHECKLIST. CAUTION LIGHT EXTINGUISHED. OPS NORMAL. R & R NR 1 BRUSH BLOCK ASSEMBLY AND CLEANED BRUSH BLOCK CONNECTOR. SEATED CONNECTOR. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 53,499 hrs · 60,403 cycles

AFTER DEPARTURE, NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED AND WILL NOT RESET. R & R NR 1 AC GENERATOR AND NR 1 AC GCU IAW WC 24-20-11R. GROUND RAN AIRCRAFT. OPS CHECKED GOOF AT THIS TIME. OK FOR SERVICE.

Part: SOCKET — OVERHEATED (CABIN LIGHT) · airframe 52,838 hrs · 59,607 cycles

HOT ELECTRICAL ODOR OVER ROW 4. INSPECTED AND FOUND OVERHEAD LIGHT 3DF OVERHEATING AT SOCKET AND BASE. REMOVED BULB, PULLED AND COLLARED CIRCUIT BREAKERS S1, S2 AND R2. CABIN INTERIOR NORMAL LIGHTING SYS, R & R SOCKET AT LAMP ASSY ON ROW 3DF. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 52,580 hrs · 59,289 cycles

SMOKE COMING FROM TOP OD F/O'S WINDSHIELD IN WARM UP MODE. CREW TURNED OFF WINDSHIELD HEAT AND SMOKE DISSIPATED. R & R F/O'S WINDSHIELD IAW WC 56-00-00R. OPS CHECKED GOOD.

Part: CONTACTOR — FAILED (APU START) · airframe 52,580 hrs · 59,289 cycles

APU FAILED. CIRCUIT BREAKER N-8 TRIPPED. R & R APU START CONTACTOR. RESET CIRCUIT BREAKER N-8. OPS CHECKED GOOD.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 52,581 hrs · 59,289 cycles

SMOKE COMING FROM TOP OF F/O WINDSHIELD IN WARM UP MODE. CREW TURNED OFF WINDSHIELD HEAT SMOKE DISSIPATED. R & R F/O WINDSHIELD IAW W/C 56-00-00R. OPS CHECKED GOOD.

Part: CONTACTOR — SHORTED · airframe 52,581 hrs · 59,289 cycles

APU FAILED AUX CIRCUIT BREAKER N-8 TRIPPED. MX INSPECTED FIRE BOTTLE STILL CHARGED. NO OBVIOUS DEFECTS OR DAMAGE NOTED. R & R APU START CONTACTOR, RESET CIRCUIT BREAKER N8. OPS CHECKED GOOD. FOUND CONTACTOR SHORTED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,514 hrs · 59,207 cycles

RIGHT VERTICAL STIFFENER IS CRACKED AT UPPER MOST RIVET. REPAIRED IAW RD8-53-7275 AND EO8-53-13-0416.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,522 hrs · 59,210 cycles

SEAT TRACK SECTION AT LAV AND GALLEY AREA ARE CORRODED. R & R SPLICED SECTION OF SEAT TRACK AT LAV AND GALLEY AREA IAW RD8-53-3074.

Part: BOLT — MISINSTALLED (COCKPIT) · airframe 52,522 hrs · 59,218 cycles

IMPROPER JO-BOLT INSTALLATION IN COCKPIT BELOW LT WINDSCREEN SIDE POST AT WINDSCREEN DRAIN LINE. REMOVED JO-BOLT. PERFORMED HFEC INSPECTION. NO DEFECTS NOTED REPAIRED MISDRILLED FASTENER HOLE IAW RD8-53-13-4.

Part: FIREWALL — CHAFED (NR 2 NACELLE) · airframe 52,514 hrs · 59,207 cycles

NR 2 ENGINE FIREWALL IS CHAFED ON OTBD SIDE. REPAIRED NR 2 NACELLE FIREWALL IAW RD8-54-991.

Part: SPOILER SYS — OUT OF RIG · airframe 52,522 hrs · 59,218 cycles

RIGHT HAND INBOARD ROLL SPOILER DOES NOT INDICATE STOWED PRIOR TO TAKEOFF. REMOVED FLAP WELL PANELS 632BB,CB DB ON RT WING, R & R RT INBD FLIGHT SPOILER IAW MM 27-14-06. RIGGED AND OPS CHECKED GOOD IAW MM 27-14-00. REINSTALLED ALL FLAP WELL PANELS.

Part: CONNECTOR — UNSECURE (NR 2 GENERATOR) · airframe 52,520 hrs · 59,214 cycles

NR 2 AC GENERATOR CAUTION LIGHT CAME ON DURING CLIMB OUT, CREW PERFORMED CHECKLIST AN TURNED GENERATOR OFF. ACFT RETURNED TO DEPARTURE. FOUND CONNECTOR PLUG ON GENERATOR LOOSE. RESECURED CONNECTOR PLUG. GROUND AIRCRAFT. OPS CHECKED GOOD.

Part: PLATE — CRACKED · airframe 52,514 hrs · 59,207 cycles

LADDER PLATE UNDER STRESS PANEL 622AT IS CRACKED AT THE FWD INBD CORNER. REPAIRED LADDER PLATE UNDER STRESS PANEL 622AT AT FWD INBD CORNER IAW EO8-57-13-039.

Part: PLATE — CRACKED · airframe 52,514 hrs · 59,207 cycles

1" LONG CRACK AT FWD INBD CORNER OF STRESS PANEL 522AT LADDER PLATE. REPAIRED CRACK AT FWD INBD CORNER OF LADDER PLATE AT STRESS PANEL 522AT IAW EO8-57-13-0394A.

Part: PLATE — CRACKED · airframe 52,514 hrs · 59,207 cycles

2.5" LONG CRACK AT CORNER OF LADDER PLATE FOR PANEL 522AT AT STA YW139.000, AFT OTBD CORNER. REPAIRED CRACK AT CORNER OF LADDER PLATED FOR PANEL 522AT AT STA YW139.000 IAW EO8-57-13-0398.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 52,524 hrs · 59,207 cycles

MOST AFT CENTER EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R BULB IN MOST AFT CENTER EMERGENCY CEILING LIGHT.

Part: SEAT TRACK — CORRODED (BS 222-242) · corrosion level 2 · airframe 52,514 hrs · 59,207 cycles

CORROSION AT LT INBD SEAT TRACK BETWEEN BS 222 AND 242 UNDER WATER DRAIN DRIP TRAY. CUT SEAT TRAC IAW RD8-53-3074. SECURED WITH NEW SECTION OF SEAT TRACK ASSEMBLED AND INSTALLED FASTENERS IAW RD8-53-3074.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 52,514 hrs · 59,207 cycles

AIRSTAIR DOOR THRESHOLD IS CORRODED AROUND MOUNTING SCREW HOLES. R & R THRESHOLD IAW DWG 85321241.

Part: STRUCTURE — CHAFED (NR 1 NACELLE) · airframe 52,465 hrs · 59,143 cycles

INBD ZEE MEMBER CHAFED ON NR 1 NACELLE. REPAIRED FIREWALL ZEE MEMBER IAW EO 8-54-13-0268.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 52,465 hrs · 59,143 cycles

FIREWALL ANGLE CRACKED IN NR 1 NACELLE ABOVE JET PIPE. R & R FIREWALL ANGLE IAW DWG NR 85410024.

Part: BULB — WEAK (EMERGENCY LIGHT) · airframe 51,925 hrs · 58,482 cycles

SIDE WALL EMERGENCY EXIT SIGN IS DIM AT PAX DOOR. R & R BULBS IN SIDE WALL EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 51,727 hrs · 58,239 cycles

NR 2 HYD QTY AT .5 WITH FLUID LEAKING IN NR 2 NACELLE WITH RUDDER ISOLATION VALVE CAUTION LIGHT ILLUMINATED. INSPECTED NR 2 WHEEL WELL AND FOUND HYD LINE FOR AFT GEAR DOOR FROM ELECTRIC SEQUENCE VALVE ACTUATOR RUPTURED. INSTALLED TEMP FLEX LINE IAW SP20.1 SERVICED NR 2 HYD SYS. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD.

Part: LIGHT — FAILED (CABIN) · airframe 51,667 hrs · 58,166 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. R & R LIGHT ASSY IAW MM 33-52-00. OPS CHECKED GOOD.

Part: INVERTER — FAILED · airframe 51,709 hrs · 58,217 cycles

OILY BURNING SMELL AROUND FORWARD CABIN AREA AND FLIGHT DECK. FOUND AUX INVERTER FAILED. R & R AUX INVERTER. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 51,444 hrs · 57,892 cycles

EMERGENCY LIGHTS FLICKERED ENROUTE. R & R EMERGENCY LIGHT CONTROL BOX IAW 61-10-11. OPS CHECKED GOOD. EMERGENCY LIGHTS DID NOT ILLUMINATED.

Part: BRUSH BLOCK — INOPERATIVE (PROPELLER) · airframe 51,444 hrs · 57,892 cycles

R & R NR 2 PROP BRUSH BLOCK IAW 61-10-11. OPS CHECKED GOOD.

Part: BRUSH BLOCK — FAILED (NR 2 PROPELLER) · airframe 51,434 hrs · 57,879 cycles

IN FLIGHT, RT AC BUSS CAUTION LIGHT ILLUMINATED WITH FAILURE OF ASSOCIATED SYS. REMOVED NR 2 PROP BRUSH BLOCK ASSY IAW AMM 61-10-11. OPS CHECKED SLIP RINGS ON NR 2 PROP IAW AMM 61-10-00. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED · airframe 51,374 hrs · 57,797 cycles

ON CLIMBOUT, RT AC BUSS, RT STALL WARNING, RT TRU AND ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. CLEANED CONNECTOR PLUGS AT NR 2 AC GEN. R & R NR 2 AC GCU. OPS CHECKED GOOD IAW MM 24-21-00. OK FOR SERVICE. ON CLIMB OUT, RT AC BUSS, RT STALL WARNING, RT TRU AND ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED. CREW REPORTED NO LOAD ON ALL 3 PHRASES. R & R TRU LOGIC RELAY 2431-K13 AND K14. GROUND RUN ACFT, OPS CHECKED GOOD.

Part: BRUSH BLOCK — DIRTY (PROPELLER HEAT) · airframe 51,359 hrs · 57,775 cycles

ON CLIMB OUT, EMERGENCY LIGHTS FLICKERED MOMENTARILY. OPS NORMAL AT THIS TIME. INSPECTED AND CLEANED BRUSH BLOCK AND CONNECTOR PLUGS. GROUND RAN ACFT. PROPELLER HEAT AND EMERGENCY LIGHTS OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (A/C BUSS) · airframe 51,322 hrs · 57,725 cycles

RT AC BUSS C/L ILLUMINATED INFLIGHT. WITH ASSOCIATED C/L. CONFIRMED OK WITH RT TRU DISABLED.

Part: TRU — MALFUNCTIONED (RIGHT) · airframe 50,953 hrs · 57,246 cycles

RT BUSS FAULT IN FLIGHT WITH RT TRU CAUTION LIGHT AND RT STALL WARNING CAUTION LIGHT. INSPECTED WIRING IN AND AROUND RT CONTACTOR BOX, TRU AND AC GENERATOR. NO DEFECTS NOTED. R & R RT TRU AS REQUIRED. OPS CHECKED GOOD AT THIS TIME.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 50,891 hrs · 57,172 cycles

ELECTRICAL ODOR IN CABIN MID TO AFT AREA, ROW 7. R & R PUSH BUTTON SOCKET END FOR CABIN OVERHEAD LIGHT AT 7AC. R & R BALLAST FOR OVERHEAD LIGHT. OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (MLG DOOR) · airframe 50,470 hrs · 56,656 cycles

DURING GEAR RETRACTION, LEFT MAIN GEAR DOOR AMBER CAUTION LIGHT ILLUMINATED. CYCLED IAW CHECKLIST. LIGHT EXTINGUISHED. R & R FORWARD LT GEAR DOOR ACTUATOR IAW MM 32-10-36. OPS AND LEAK CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,860 hrs · 55,951 cycles

RIGHT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. REMOVED LENS, R & R BULB, AT SAID LOCATION, REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,860 hrs · 55,951 cycles

RT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT DIM. REMOVED LENS, REMOVED AND REPLACED BULB , AT SAID LOCATION. REINSTALLED LENS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,860 hrs · 55,951 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,860 hrs · 55,951 cycles

EMERGENCY EXIT AIRSTAIR DOOR SIGN LIGHT IS INOPERATIVE. R & R PAX DOOR EMERGENCY EXIT SIGN LIGHT BULB. OPS CHECKED GOOD.

Part: BRUSH BLOCK — UNKNOWN (PROPELLER) · airframe 46,595 hrs · 52,448 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT WITH HIGH LOADS ON NR 2 PROPELLER A AND B PHASES. R & R NR 2 BRUSH BLOCK ASSY IAW MM 61-10-11. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,860 hrs · 55,951 cycles

EMERGENCY EXIT LOWER SIDEWALL SIGN LAMP AT ROW 4DF IS INOPERATIVE. R & R SIDEWALL EMERGENCY SIGN BULB IN ROW 4DF. OPS CHECKED GOOD.

Part: PANEL — CRACKED (SPOILER) · airframe 49,618 hrs · 55,690 cycles

MOST OTBD LIGHTNING HOLE UNDER OTBD ROLL SPOILER PANEL 632EB IS CRACKED. REPAIRED OTBD CRACKED LIGHTNING HOLE UNDER PANEL 632EB IAW EO8-57-12-0040.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,611 hrs · 55,680 cycles

EMERGENCY FLOOR LIGHT UNDER TRIM AT ROW 8 IS INOPERATIVE. REPOSITIONED TRIM AND LIGHT. OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 49,611 hrs · 55,680 cycles

EMERGENCY FLOOR LIGHT LOOSE AT ROW 3. REPOSITION LIGHT ASSY. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 49,610 hrs · 55,679 cycles

LEFT AFT EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY ON LT SIDE AT ROW 3AC IAW MM 33-51-00.

Part: MODULE — WRONG PART (EMERGENCY LIGHTS) · airframe 49,610 hrs · 55,679 cycles

LENS ON EMERGENCY FLOOR LIGHT AT ROW 8 IN NOT RED. R & R LENS COVER. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 49,610 hrs · 55,679 cycles

LEFT EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY ON LT SIDE AT ROW 3 IAW 33-51-00. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 49,611 hrs · 55,679 cycles

TAIL STRUCK DEICING TRUCK BOOM. DAMAGE TO LT HORIZONTAL STABILIZER, LT ELEVATOR, LT TRIM TAB, AND LT L/E. R & R HORIZONTAL STAB IAW 55-10-00 AND WC 55-50-01.

Part: LIGHT — FAILED (CABIN) · airframe 49,447 hrs · 55,482 cycles

OVERHEAD LIGHT AT ROW 2DF FAILED. R & R LAMP HOLDER, BULB AND BALLAST AT SEAT 2DF. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (RT WING) · airframe 49,260 hrs · 55,264 cycles

RT WING INSPECTION LIGHT POPS CIRCUIT BREAKER. INSPECTED CONTROL PANEL AND WIRING IN LOWER NR 2 COWLING. NO DEFECTS FOUND. CLEANED CONTROL PANEL AND R & R BULB AND OPS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 47,592 hrs · 52,193 cycles

WEATHER RADAR INOP. NOT PAINTING GROUND OR WEATHER. R & R WEATHER RADAR RT IAW 34-41-04. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 48,896 hrs · 54,836 cycles

NR 1 AMBER ADVISORY LIGHT ON LT GEAR, STAYS ILLUMINATED FOR APPROX 50 SECONDS AFTER GEAR RETRACTION. ADJUSTED FORWARD NR 1 MLG DOOR MECHANISM IAW MM 32-10-21. CYCLED LANDING GEAR SEVERAL TIMES. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (AUX) · airframe 48,236 hrs · 54,089 cycles

AUXILIARY BATTERY HOT CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. R & R MAIN AND AUX BATTERIES IAW 24-32-00. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (ENGINE TEMP) · airframe 47,843 hrs · 53,656 cycles

NR 1 ENG OIL TEMP FLUXS INTO THE RED. ACFT RETURNED TO GATE. CLEANED AND TIGHTENED OIL TEMP GROUND WIRE AND CLEANED AND RESEATED TEMP BULB CONNECTOR PLUG. GROUND RAN ACFT. RAN NORMAL AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,911 hrs · 52,608 cycles

ROW 9, EMERGENCY FLOOR PATH LIGHT INOP. R & R ROW 9 EMERGENCY PATH LIGHT. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,738 hrs · 52,402 cycles

(2) EMERGENCY EXIT MARKER LIGHTS ON LOWER AIR STAIR DOOR MARKER ARE NOT WORKING. RELAMPED EMERGENCY LIGHT AT SAID LOCATION BY REMOVING LENS, R & R BULBS AND RE-INSTALLED LENS.

Part: LANDING GEAR — WARNING LIGHT · airframe 46,100 hrs · 51,686 cycles

LANDING GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED AFTER GEAR OPEN. VISUAL INSP CONFIRMED FWD DOOR OPEN. CREW PERFORMED CHECKLIST CYCLED GEAR, LANDED WITHOUT FURTHER INCIDENT. INSPECTED NR 1 MAIN GEAR DOOR ACTUATOR AND PROX SENSOR. NO DEFECTS NOTED, CHECKED SENSOR GAP. GAP CHECKED GOOD. JACKED ACFT, CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED. OK FOR SERVICE, IAW MM 32-10-21 AND 32-10-36.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,038 hrs · 51,617 cycles

ONE FLOOR LEVEL EMERGENCY LIGHT IS NOT WORKING AT ROW 7. REMOVED AND REPLACED ONE FLOOR LEVEL EMERGENCY LIGHT LAMP AT ROW 7. CLOSED ACCESS PANEL.

Part: SWITCH — MALFUNCTIONED (STALL WARN TEST) · airframe 46,038 hrs · 51,617 cycles

ON CLIMB-OUT, BOTH STALL WARNING STICK SHAKERS ACTIVATED AND FIRST OFFICER'S FAST SLOW INDICATOR SHOW 10 TO 20 KNOTS SLOW. PULLED AND COLLARED CIRCUIT BREAKERS STALL WARNING AND HEATER NR 2, STALL FAIL MON 2, STALL TRANSPONDER AND HEATER 2. REMOVED AND REPLACED STALL WARNING TEST SWITCH INSTALLATION CHECKED GOO IAW WORKCARD 27-33-00. CHECKED CALIBRATION OF NR 2 STALL WARNING LIFT TRANSDUCER IAW WORKCARD 27-30-05F. OPS CHECKED GOOD AT THIS TIME.

Part: BULB — BROKEN (CABIN LIGHTS) · airframe 45,400 hrs · 50,888 cycles

OVERHEAD LIGHT AT ROW 1AC EXPLODED. CLEANED UP BROKEN BULB. REPLACED WITH NEW BULB, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 44,510 hrs · 49,931 cycles

AT 24,000 FEET, NR 2 ENGINE ITT INCREASED FROM 705 TO 770, BLEED HOT CAUTION LIGHT ILLUMINATED. CREW SELECTED BLEED OFF, ITT DECREASED AND HOT CAUTION LIGHT EXTINGUISHED. SELECTED BLEED ON AND DISCREPANCY REPEATED. FLIGHT DIVERTED TO SBY FOR MAINTENANCE. SBY MAINTENANCE REMOVED AND REPLACED THE NR 2 HP BLEED SHUTOFF VALVE IAW AMM 21-11-16. AS A PRECAUTION, MAINTENANCE ALSO REPLACED THE NR 1 AND NR 2 ENGINE MP BLEED PRESSURE SWITCHES AND THE NR 2 BLEED HOT CAUTION LIGHT TEMPERATURE SWITCH, DONE IAW AMM 21-10-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,787 hrs · 49,157 cycles

FIRST WHITE EMERGENCY LIGHT, FLOOR PATH LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB, OPS CHECK GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-11.

Part: PSEU — FAULTED (LANDING GEAR) · airframe 42,594 hrs · 47,800 cycles

UPON TAKEOFF LANDING GEAR WARNING HORN SOUNDED FOLLOWED BY THREE RED LANDING GEAR UNSAFE LIGHTS. ABORTED TAKEOFF, PERFORMED PSEU BITE TEST, PSEU MEMORY RECALL CODES 45 AND 54 WERE RETRIVED.(45 "NOSE WHEEL STEERING" AND 54 "PSEU DRIVER CARD 1A"). REMOVED AND REPLACED PSEU IAW 32-61-50, PERFORMED GEAR SWING IAW 32-30-00. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT ABOVE AIRSTAIR DOOR INOPERATIVE. ALSO, LT FWD EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED 3351PS1, CHECK GOOD BY OBSERVING LIGHT ILLUMINATE. (K)

Part: BULB — BROKEN (CABIN LIGHTS) · airframe 41,554 hrs · 41,554 cycles

OVERHEAD LIGHT AT 6DF CAME LOOSE AND BROKE IN FLIGHT, THOUGHT TO BE BROKEN BY PASSENGER OPENING OVERHEAD BIN. CLEANED BROKEN GLASS FROM OVERHEAD BIN, FLOOR AND SEATS. REPLACED BULB, OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 41,395 hrs · 46,443 cycles

AFTER TAKEOFF, LEFT GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. WHEN GEAR WAS EXTENDED, THE LEFT GEAR SHOWED AN UNSAFE CONDITION. CREW DID NOT NOTE POSITION OF L/G DOORS AT THIS TIME. CREW CHECKED ALTERNATE EXTENSION SYSTEM AND IT ALSO INDICATED AN UNSAFE CONDITION ON THE LEFT GEAR. ALTERNATE EXTENSION PROCEDURES WERE FOLLOWED AND AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED LEFT GEAR AND DOORS AND NOTED NO OBVIOUS DEFECTS. PROXIMITY SENSOR ON FORWARD GEAR DOOR ACTUATOR WAS FOUND TO BE OUT OF ADJUSTMENT. SENSOR WAS ADJUSTED AND GEAR WAS SWUNG ON GROUND IAW MM PROCEDURES. CHECKS WERE GOOD. HYDRAULIC SYSTEM WAS BLED AND SERVICED. AIRCRAFT WAS RELEASED FOR EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. ADDITIONAL INFORMATION SUPPLIED.

Part: HMU — DEFECTIVE (NR 2 ENGINE) · airframe 41,372 hrs · 46,420 cycles

NR 2 ENGINE SURGED DURING CLIMB, TORQUE, FUEL FLOW, AND AIRCRAFT SURGED. A 3.5 TO 4 INCH KNOB SPLIT WITH NR 2 ADVANCED DURING APPROACH. REPLACED NR 2 HMU, OPERATIONAL AND LEAK CHECKS GOOD.

Part: SKIN — DETERIORATED (LT ELEVATOR) · airframe 41,111 hrs · 46,123 cycles

WHILE PAINTING THE AIRCRAFT, RIVET HEADS WERE FOUND TO HAVE BEEN SANDED DOWN ON THE LT ELEVATOR LOWER SKIN. REMOVED AND REPLACED THE RIVETS IAW SRM 51-40-00 AND EO 8- 57-07-3382.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 41,046 hrs · 46,046 cycles

BOTH STRINGERS CRACKED IN LEFT NACELLE UNDER HEAT SHIELD FOR EXHAUST. BOTH STRINGERS CUT AND REPAIRED IAW RD8-54-310, INSTALLED WITH SOLID RIVETS AND HI-LOKS IAW SRM 51-40-00.

Part: STRINGER — CRACKED (NACELLE) · airframe 41,046 hrs · 46,046 cycles

BOTH STRINGERS CRACKED IN LEFT NACELLE UNDER HEAT SHIELD FOR EXHAUST. BOTH STRINGERS CUT AND REPAIRED IAW RD8-54-310, INSTALLED WITH SOLID RIVETS AND HI-LOKS IAW SRM 51-40-00.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,046 hrs · 46,046 cycles

PAX DOOR CORRODED AROUND TEFLON STRIP. PAX DOOR THRESHOLD REPLACED WITH NEW PART 85320686-101 AND 85321229-101 NYLON RUBSTRIP INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00.

Part: SEAT TRACK — CORRODED (BS 597) · airframe 41,046 hrs · 46,046 cycles

CORROSION FOUND ON RIGHT SEAT TRACK AT STATION X597.500. RIGHT INBOARD SEAT TRACK REPLACED FROM STATION X526.500 TO X618.00. INSTALLED WITH SOLID RIVETS PER SRM 51-41-00.

Part: PANEL — CORRODED · airframe 41,046 hrs · 46,046 cycles

CORROSION FOUND ON RIGHT STRESS PANEL 622AT. GREEN PRIMER APPLIED ON COUNTER SINKS OF PANEL 622AT AS PER AMM 20-34-11 CORROSION FOUND OUT OF LIMITS, NEW ACCESS PANEL INSTALLED PER 05-00-21.

Part: UPLOCK HOOK — WORN (MLG) · airframe 40,913 hrs · 45,924 cycles

AFTER GEAR RETRACTION LEFT GEAR DOOR REMAINED IN YELLOW. CYCLED GEAR PER PROCEDURE THEN THE LEFT GEAR WOULD NOT COME DOWN AT ALL. USED ALTERNATE EXTENSION, GOT ALL GREEN LIGHTS. CIRCLED AND RETURNED TO HPN. NO EMERGENCY WAS DECLARED BUT CAPTAIN DID REQUEST CFR TRUCKS. FOUND LEFT GEAR ACTUATOR UPLOCK HOOK WORN. REPLACED BUSHING, RIGGED ACTUATOR AND PROX SWITCH IAW -8 MM 32-10-21, OPS CHECK GOOD.

Part: STRINGER — CORRODED (BS 467 S29R) · corrosion level 2 · airframe 40,772 hrs · 45,757 cycles

LIGHT CORROSION AT STR 29 AND X467.00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 40,772 hrs · 445,757 cycles

LITE CORROSION AT STR 29 STRAP BETWEEN STA X467 AND X488.500.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,772 hrs · 4,757 cycles

LITE CORROSION ON STR 29 BETWEEN X488.500 AND X510.00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 40,772 hrs · 45,757 cycles

LIGHT CORROSION BETWEEN X510.00 AND X531.500 ON STR 29 STRAP.

Part: STRINGER — CORRODED (BS 291) · corrosion level 2 · airframe 40,772 hrs · 45,757 cycles

LIGHT CORROSION AT STR 29 AND STA X291.400 JOINING AREA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 40,772 hrs · 45,757 cycles

LITE CORROSION BETWEEN X510.00 AND X531.500 ON STR 29 STRAP.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,772 hrs · 45,757 cycles

HORIZONTAL ANGLE AT TOP OF RIGHT NLG WELL TRUNNION WEB IS CRACKED WHERE IT ATTACHES BETWEEN THE WEB AND VERT TRUNNION MOUNT BEAM.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,039 hrs · 43,866 cycles

SMOKE SMELL IN COCKPIT LAV SMOKE DETECTOR SOUNDED. REMOVED AND REPLACED CAUTION PANEL FOR TROUBLESHOOTING. PN INFORMATION TO FOLLOW.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 35,271 hrs · 39,702 cycles

NR 2 HYD CAUTION LIGHT ILLUMINATING DURING GEAR RETRACTION. FLIGHT RETURNED. MAINTENANCE JACKED AIRCRAFT AND SWUNG THE LANDING GEAR SEVERAL TIMES. BLED THE NR 2 HYDRAULIC SYSTEM AND SERVICED AS NEEDED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAILSAFE — BROKEN (LT MLG WW) · airframe 34,288 hrs · 38,684 cycles

FLIGHT 3806 LGA TO BURLINGTON EXPERIENCED A PROBLEM WITH THE LEFT MAIN GEAR DOOR FAILING TO RETRACT. THE AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO MIDDLETOWN FOR MAINTENANCE. IT WAS DISCOVERED THAT THE ATTACH POINT FOR THE PRE MOD GEAR DOOR ACTUATOR HAD BACKED OUT DUE TO THE FAILSAFE RETAINING TAB BEING BROKEN OFF, WHICH ALLOWED THE ACTUATOR PIVOT PIN TO MISALIGN AND PREVENT PROPER UPLOCK. FAILSAFE WAS REPLACED AND THE GEAR OPERATIONAL CHECKED. ALL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (NR 2) · airframe 34,112 hrs · 38,491 cycles

NR 2 SMOKE DETECTOR INOPERATIVE DURING TEST. MAINTENANCE REMOVED AND REPLACED NR 2 UNIT AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — SMOKE (ROW 8 & 9) · airframe 33,999 hrs · 38,373 cycles

REPORTED SMOKE FROM THE OVERHEAD LIGHT ABOVE SEATS IN ROW 8 AND 9.MAINTENANCE COMPLIED WITH MEL AND REMOVED THE LAMP AND PULLED AND BANDED ASSOCIATED CIRCUIT BREAKER. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — STICKING (LT CONTROL LEVER) · airframe 33,482 hrs · 37,836 cycles

FLIGHT 3755 FROM SYRACUSE HAD TO RETURN TO GATE DUE TO RECEIVING THE TAKEOFF WARNING HORN WITH THE AIRCRAFT PROPERLY CONFIGURED FOR TAKEOFF. MAINTENANCE FOUND THE LT CONDITION LEVER SWITCH 3151-S3 TO BE STICKING. MAINTENANCE REPLACED SWITCH AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (LT GEAR DOOR) · airframe 32,965 hrs · 37,256 cycles

AIRCRAFT 839EX, FLIGHT NR 3698, ROCHESTER, HAD TO PERFORM A SECOND GEAR SWING DUE TO AN AMBER LEFT GEAR DOOR LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. CREW PERFORMED GEAR SWING AND THE LIGHT EXTINGUISHED ON SECOND ATTEMPT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FORWARD GEAR DOOR ACTUATOR AND ALL OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD, AIRCRAFT WAS RETURNED TO SERVICE.

Part: DIODE — FAILED (EMERGENCY LIGHT) · airframe 32,404 hrs · 36,662 cycles

DURING ROUTINE MAINTENANCE VISIT FOUR RED FLOOR EMERGENCY LIGHTS AT ROW 4 WERE FOUND TO BE INOPERATIVE. ALSO, FORWARD AND AFT LEFT AND RIGHT UPPER SIDEWALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. EMERGENCY LIGHTING SYSTEM WAS TROUBLESHOT AND A BURNT WIRE ON A POST CONNECTOR FOR POSITION 500 POWER SUPPLY WAS FOUND. POWER SUPPLY WAS REPLACED AT POSITION 500. ALSO FOUND WAS A BAD DIODE FOR THE RED FLOOR LIGHTS. DIODE WAS REPLACED. ALL EMERGENCY LIGHT BATTERIES WERE REPLACED DURING TROUBLESHOOTING. OPERATIONAL CHECK OF ALL EMERGENCY LIGHTS WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 32,184 hrs · 36,421 cycles

CREW REPORTED LOSS OF NR 2 HYDRAULIC CONTENTS AFTER TAKE OFF. HYDRAULIC ISOLATION VALVE LIGHT ILLUMINATED. EMERGENCY WAS DECLARED, AND AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A HYDRAULIC FLEX LINE AT THE NOSE GEAR DRAG STRUT ACTUATOR. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,723 hrs · 35,940 cycles

CREW REPORTED NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 31,723 hrs · 35,940 cycles

DCA- FLIGHT 182, CREW REPORTED NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 31,405 hrs · 35,592 cycles

LGA-FLIGHT 3920 CREW REPORTED WITH POWER LEVERS AT FLIGHT IDLE BLEED AIR SMELLS OILY AND MAKES EYES BURN. MAINTENANCE CHECKED BOTH OIL LEVELS AND FOUND THEM TO BE PROPERLY SERVICED. AIRCRAFT GROUND RAN WITH BOTH BLEEDS ON FOR 20 MINUTES. OPERATIONAL CHECK WAS GOOD ON THE GROUND. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP ON 18 MARCH 2003, RIGHT ENGINE ASSEMBLY SERIAL NUMBER 121354 WAS REPLACED DUE TO A HISTORY OF ODOR IN BLEED AND OIL CONSUMPTION.

Part: ODOR — DETECTED (CABIN) · airframe 31,258 hrs · 35,428 cycles

PJL-FLIGHT 3800 CREW REPORTED A BURNT OIL ODOR FROM BLEEDS WITH POWER BELOW 30 PERCENT TORQUE DURING DESCENT. ODOR WAS MORE NOTICEABLE ON THE NR 2 ENGINE. MAINTENANCE RAN THE AUXILIARY POWER UNIT BLEED AND FOUND NO DEFECTS. BOTH ENGINES WERE RUN WITH P3 AIR ON, AND NO OIL ODOR WAS NOTED FROM EITHER ENGINE. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — LOOSE (LT COWL) · airframe 27,817 hrs · 31,709 cycles

DURING FLEET INSPECTION SEVERAL RIVETS FOUND LOOSE ON LEFT COWLING OUTBOARD END JUST BELOW FLAP TRACK. RIVETS REPLACED IN ACCORDANCE WITH CALLAHAN REPAIR SERVICES DER AUTHORIZATION CAS-AAL-09. AIRCRAFT RETURNED TO SERVICE.

Part: SOCKET — BURNED (CABIN) · airframe 26,553 hrs · 30,309 cycles

DTW FLIGHT 3529. CREW REPORTED SMOKE AND FLAME COMING FROM OVERHEAD LIGHT 8 AC. CONTRACTED MAINTENANCE INSPECTED AND CONFIRMED LIGHT SOCKET AT ROW 8AC OVERHEAD AT FAULT, LIGHT SOCKET ISOLATED. MAINTENANCE CONTROL ISSUED MEL 33-02. AIRCRAFT SCHEDULED TO BGM MAINTENANCE THAT NIGHT, LIGHT SOCKET AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COFFEEMAKER — BURNED (GALLEY) · airframe 25,861 hrs · 29,578 cycles

FLIGHT NR 3800 BDL-ROC AT 16000 FT OVER ALB AIRPORT FLIGHT ATTENDANT REPORTED SLIGHT BURNING ODOR FROM GALLEY AREA. FLIGHT DIVERTED TO ALB WHERE MAINTENANCE FOUND AFT HOT JUG RECEPTICLE BURNT. HOT JUG REMOVED AND MEL ISSUED. HOT JUG RECEPTICLE SOCKET REPLACED 19 NOV 2000 IN MDT.

Part: BRACKET — DAMAGED (AIRSTAIR)

BWI FLIGHT 3852 - THE AIRSTAIR DOOR WAS FOUND TO FREEFALL WHEN OPENED. MAINTENANCE INSPECTED AND FOUND THE LOWER CABLE SUPPORT BRACKET CAUSING PROBLEM. REMOVED AND REPLACED THE CABLE BRACKET PN 85210159-103. OPERATIONAL CHECK WAS PERFORMED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.

Part: INDICATOR — MALFUNCTIONED (NR 1 ENGINE)

SYR-LGA - FLIGHT 3863, CREW SHUTDOWN NR 1 ENGINE AS A PRECAUTION DUE TO LOW OIL PRESSURE INDICATION, OIL PRESSURE LIGHT REMAINED OUT UNTIL ENGINE WAS SHUTDOWN. AIRCRAFT WAS DIVERTED INTO BGM, PASSENGERS DEPLANED NORMALLY. EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED AND REPAIRED WIRE 10005C22 IN PANEL 412DT PER DEHAV INSTRUCTIONS. LEAK AND OPERATIONAL CHECK PROVED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE LIGHT — ILLUMINATED (BAGGAGE COMPT)

FLT 3800 - BDL AFTER TAKEOFF THE BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BAG BAY, NO EVIDENCE OF SMOKE OR FIRE, CLEANED ELECTRICAL CONNECTORS, RAN AIRCRAFT WITH ENGINE BLEEDS ON, NO DEFECTS NOTED.

Part: WINDOW — CRACKED (LT COCKPIT)

EN ROUTE TO BWI, THE CAPTAINS SIDE WINDOW CRACKED. A/C LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M)

Part: DIODE BLOCK — FAILED (CABIN)

SEVERAL CENTER EMERGENCY FLOOR PROXIMITY LIGHTING SYSTEM LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT DIODE BLOCK. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. ACTT: 18,385:42 HOURS. ACTC: 21,191. (X)

Part: LIGHT — FAILED (CABIN)

ONE LIGHT INOPERATIVE IN EMERGENCY FLOOR PROXITY LIGHTING SYSTEM. FOUND WIRES PULLED OUT OF LIGHT MODULE. REMOVED AND REPLACED EMERGENCY LIGHT MODULE. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

TWO LIGHTS INOPERATIVE IN EMERGENCY FLOOR PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRES IN EMERGENCY FLOOR PROXIMITY LIGHTING CIRCUIT. A/C RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

SEVERAL EMERGENCY EXIT SIGN BULBS ARE INOPERATIVE. REMOVED AND REPLACED LAMPS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. ACTC: 20,443. (X)