N76200

Part: ENGINE — OUT OF ADJUST (RIGHT) · airframe 69,878 hrs · 30,232 cycles

APU ALREADY ON PLACARD, NR 2 ENG GEN WILL NOT HOLD AN ELEC LOAD. THE RT ENG IDLE SPEED WAS LOW. ADJUSTED ENG IAW MCM 71-91-17 & MCM 71-91-73. GEN OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENGINE) · airframe 69,703 hrs · 30,136 cycles

ABORTED TAKEOFF. DURING TAKEOFF ROLL RT ENG INLET FUEL PRESS LOW LIGHT ILLUMINATED. R & R INLET FUEL PRESS SWITCH & LOW PRESS FUEL FILTER. PERFORMED TAKEOFF POWER ENG RUN. SYS CHECKED NORMAL.

Part: DUCT — LEAKING (AC BAY) · airframe 69,268 hrs · 29,916 cycles

DURING CRUISE CABIN STARTED TO CLIMB WITH A PRESSURIZATION FLOW LIGHT AFTER MANUALLY CLOSING OUTFLOW VLV CABIN WAS STILL CLIMBING. BOTH FLOW GOUGES SHOWED AIR TO THE PACKS AT 10000 CABIN STARTED TO DESCEND. CABIN ALTITUDE NEVER EXCEEDED LIMITS. FLIGHT LANDED WITHOUT INCIDENT. FOUND DUCT LEAK AT FLANGE OF RT PACK WATER SEPARATOR. REPLACED DUCT & BOTH WATER SEPARATORS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CONNECTOR — BROKEN (CABIN) · airframe 68,084 hrs · 29,298 cycles

EMERGENCY LIGHT IN LT LOWER SIDEWALL PANEL AT AFT STAIRWAY HAS BROKEN PLUG. REPLACED DAMAGED CONNECTOR FOR EMERGENCY LIGHT IN LT LOWER SIDEWALL PANEL AT AFT STAIRWAY, OPERATIONS CHECKED NORMAL.

Part: CYLINDER — INOPERATIVE (RT MLG) · airframe 67,891 hrs · 29,194 cycles

DFW, REPEAT ITEM, CREW REPORTED AFTER TAKEOFF RT LG HAD A RED GEAR LIGHT INDICATION. GEAR DOOR OPEN LIGHT WAS INITIALLY OFF BUT THEN CAME ON. TURNED ENG HYD PUMPS ON & BOTH LIGHTS WENT OUT. EMERGENCY DECLARED FLIGHT RETURNED TO DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT MLG LATCH CYLINDER & DOOR ACTUATOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 67,878 hrs · 29,184 cycles

DFW CREW REPORTED RT MLG INDICATED DOWN WITH HANDLE UP. GEAR DOOR OPEN LIGHT ON WITH HYD PUMPS ON LOW BUT LIGHT OFF WITH HYD PUMPS ON HIGH. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT MLG UPLOCK SENSOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: DATA UNIT — FAILED (FUEL SYSTEM) · airframe 66,670 hrs · 28,528 cycles

STL INFLIGHT DFW-MKE. CREW REPORTED DURING FUEL CHECK IN FLIGHT, FUEL QUANTITIES WERE ERRATIC. FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. CHECKED AIRCRAFT FUELING PANEL & FOUND LT HAND, RT HAND & CENTER TANK FUEL VALUES WERE OPEN MANUALLY FROM PREVIOUS FUELING. PERFORMED WING FUEL IMBALANCE CHECK IAW SECTION 12 CARD 28-96-01& ALL NORMAL. REPLACED LSDU ON RT WIND FUELING SYSTEM DUE TO PREVIOUS WRITE UP ON CIRCUIT BREAKER Z38 POPPED. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SENSE LINE — DISCONNECTED (AC BAY) · airframe 63,778 hrs · 26,968 cycles

DFW - CREW REPORTED RIGHT PACK FAILED WITH LEFT PACK ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RECONNECTED SENSE LINE TO FLOW CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,718 hrs · 26,939 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FOR ROWS 3 TO 6. OPS CHECK NORMAL.

Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 63,299 hrs · 26,728 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC TEMPERATURE HIGH INDICATION ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT HYDRAULIC RESERVOIR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (NLG WW) · airframe 63,127 hrs · 26,629 cycles

DFW - CREW REPORTED LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AND QUANTITY INDICATED LOW. TURNED OFF LEFT HYDRAULIC PUMP. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC LINE IN NOSE WHEEL THAT WAS CHAFING ON NOSE GEAR/TAXI LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SEAL — LEAKING (LT WING) · airframe 61,569 hrs · 25,858 cycles

IAD - INFLIGHT EWR-DFW. FLIGHT ATTENDANT NOTICED A FUEL LEAK FROM LEFT WING. FIRST OFFICER NOTED LEAK NEAR BOOST PUMP AREA. FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED ACCESS PLATE 1307C LEFT WING AND REPLACED SEAL AND GASKET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,992 hrs · 25,050 cycles

SUBFLOOR INBOARD OF FORWARD SERVICE DOOR FROM STATIONS 160 TO 200 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,992 hrs · 25,050 cycles

CUSP HAS CORROSION STATION 218 BETWEEN NUMBER 5 AND 6 SEAT TRACK. INSTALLED NEW CUSP SECTION, STATION 218 TO STATION 237, BETWEEN NUMBERS 5 AND 6 SEAT TRACKS PER AARD 51-10-00-5 AND EDK3190-5 REV C.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,992 hrs · 25,050 cycles

MID CARGO DOOR JAMB BEAM CORRODED BEYOND MANUAL LIMITS. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-3.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

REPAIR DOUBLER AT STATION 503 BETWEEN LONGERONS 22 TO 23 RIGHT NOT TO SRM STANDARDS. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B SHEET 6.

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,992 hrs · 25,050 cycles

UPPER CARGO DOOR UPPER BEAM AFT EDGE, POSSIBLE CRACK IN RADIUS OF PAN. INSTALLED AFT CARGO DOOR DOUBLER AT RADIUS PER 52-03-00.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,992 hrs · 25,050 cycles

NUMBER 2 GALLEY INBOARD TIE DOOR FITTING HAS CORROSION STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED NEW INBOARD FORWARD GALLEY MOUNT FITTING AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK PER AARD 51-10-00-5 AND CDK 2396 REVISION A.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,992 hrs · 25,050 cycles

AFT CARGO STATION 1155 INBOARD BOTTOM CORNER OF DOOR JAMB T-CLIP HAS CORROSION. INSTALLED CLIP PER SRM 51-30-05, AARD 51-10-00-5, BOEING DRAWING 5936064.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

VERTICAL SUPPORT ANGLE CRACKED BELOW NUMBER 3 SEAT TRACK AT STATION 905. INSTALLED DOUBLER REPAIR PER EA MD80-53-016531.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

VERTICAL SUPPORT ANGLE CRACKED BELOW NUMBER 2 SEAT TRACK AT STATION 927. INSTALLED DOUBLER PER EAMD80-53-016529.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

VERTICAL SUPPORT ANGLE CRACKED BELOW NUMBER 3 SEAT TRACK AT STATION 886. INSTALLED DOUBLER REPAIR PER EA MD80-53-016530.

Part: BRACKET — CRACKED (ZONE 100) · airframe 59,992 hrs · 25,050 cycles

VERTICAL SUPPORT ANGLE CRACKED BELOW NUMBER 4 SEAT TRACK AT STATION 845. INSTALLED NEW BRACKET PER AARD 51-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 59,992 hrs · 25,050 cycles

WINDOW PAN CRACKED LOWER FORWARD CORNER, AFT SIDE OF STATION 1193 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,992 hrs · 25,050 cycles

WINDOW PAN CRACKED, UPPER AFT CORNER, FORWARD SIDE OF STATION 1079 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

FOUND A CREASE 3 INCHES LONG AT STATION 256 BETWEEN LONGERONS 8 AND 9 LEFT AFT OF FORWARD ENTRY DOOR. ACCOMPLISHED REPAIR PER SRM 53-04-00 FIGURE 12B.

Part: PAN — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

WINDOW PAN CRACKED UPPER AFT CORNER FORWARD SIDE OF STATION 1060 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

VERTICAL SUPPORT ANGLE CRACKED BELOW SEAT TRACK NUMBER 4 AT STATION 864. INSTALLED NEW VERTICAL SUPPORT ANGLE BELOW NUMBER 4 SEAT TRACK AT STATION 864 PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

SEAT TRACK NUMBER 6 CORROSION STATION 324. INSTALLED PLUG DDK2704-7 AND CHANNEL 7452952-7 AT SEAT TRACK NUMBER 6 STATION 324 PER AARD 53-20-00-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

FORWARD HOLE FOR WINDOW PAN REPAIR AT UPPER AFT CORNER, FORWARD SIDE OF STA 1060 RIGHT SIDE IS ELONGATED. OVERSIZED HOLE TO .2450 PER AARD 51-60-00-01 AND RE-INSTALLED FASTENER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

SEAT TRACK NUMBER 6 STATION 285 EXCESSIVE MATERIAL REMOVED FROM TAB. INSTALLED PLUG DDK2704-7 AND CHANNEL 7452952-7 AT SEAT TRACK NUMBER 6 STATION 285 PER AARD 53-20-00-10.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,992 hrs · 25,050 cycles

LEFT AFT LAVATORY LOWER VAULT DOOR STOP SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER AARD 51-10-00-5.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 59,914 hrs · 25,005 cycles

RDU - FLIGHT ATTENDANT REPORTED STRONG ELECTRICAL ODER IN CABIN ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN AND NO ODOR NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 59,424 hrs · 24,768 cycles

PHX - INFLIGHT DFW-SAN. CREW REPORTED FIRST OFFICERS OXYGEN MASK LEAKING. FLIGHT DIVERTED LANDED PHX WITHOUT INCIDENT. REPLACED FIRST OFFICERS OXYGEN MASK AND REPLENISHED CREW OXYGEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LINE — DAMAGED (PT2) · airframe 59,164 hrs · 24,642 cycles

CREW REPORTED LEFT ENGINE PRESSURE RATIO FAULTY INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DAMAGED PT2 LONG LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GYRO — MALFUNCTIONED (COCKPIT) · airframe 58,865 hrs · 24,503 cycles

LAX - ON TAKEOFF HEADING ANNUCIATION ON FLIGHT MODE ANNUNCIATOR APPEARED, HEADINGS BEGAN TO DIVERGE. HEADING WOULD NOT RESET. AFTER 10 MIN ALL RETURNED TO NORMAL. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH HEADING GYROS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — FAULTY (FUEL HEAT) · airframe 57,805 hrs · 24,010 cycles

DFW - CREW REPORTED RIGHT ENGINE OVERHEAT VALVE WAS NOT WORKING AND ENGINE OIL TEMPERATURE STAYED IN CAUTION RANGE. RIGHT ENGINE WAS SHUT DOWN AND SINGLE ENGINE TIME WAS EIGHT MINUTES. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT FUEL HEAT TIME DELAY RELAY, MAIN OIL FILTER AND FUEL HEAT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,380 hrs · 23,353 cycles

LONGERON 2 RIGHT CRACKED AT TERMINATION POINT JUST AFT OF FRAME 1418. REMOVED CRACKED SECTION OF LONGERON AND INSTALLED SPLICE PER AARD 53-30-00-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,533 hrs

LGA - THE 18R AISLE EXIT LIGHT INOPERATIVE AND MISSING LENS. REPLACED LAMP FOR 18R AISLE EXIT LIGHT.

Part: LIGHT — ACTIVATED (CABIN) · airframe 54,533 hrs

LGA - THE 18R AISLE EXIT LIGHT INOPERATIVE AND MISSING LENS. REPLACED LENS FOR 18R AISLE EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,770 hrs

LGA - EXTERIOR EMERGENCY LIGHTS AT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,770 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,770 hrs

LGA - FORWARD EMERGENCY LIGHT ON AFT VENTRAL STAIR SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LIGHT ON AFT VENTRAL STAIR SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT AFT CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK B5107 FOR EMERGENCY LIGHTS AT AFT CABIN SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT MID COACH CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK B5104 FOR EMERGENCY LIGHTS AT MID COACH CABIN SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN)

DFW AFT LAV AREA CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR AFT LAV AREA CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOME NUT — LEAKING (LEFT WING)

AIRCRAFT EN ROUTE PDX-ORD OBSERVED FUEL LEAK IN THE LEFT WING ROOT. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT NOT OVERWEIGHT. MAINTENANCE SEALED UPPER WING TANK PLATE DOME NUT AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT GALLEY AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR AFT GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — GOUGED (FUSELAGE)

TUL - DEEP GOUGE IN LEFT FRAME STATION 807 BELOW SLAT DRIVE MECHANISM. CUT OUT DAMAGE INSTALLED DOUBLER REPAIR PER SRM 53-01-00 AND AARD 053-10-00-15. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK, FS 1277-1281. INSTALLED NEW SEAT TRACK PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SUB FLOOR BELOW NR 1 GALLEY DRAIN PAN RBL 49-51 CORRODED AT STAINLESS STEEL FITTING. INSTALLED DOUBLER ON SUB FLOOR BELOW NR 1 GALLEY DRAIN PAN RBL 49-RBL 51 PER SRM 53-01. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND RIGHT AFT OVER WING EXIT JAMB CRACKED AT TOP CENTER, FS 916. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER 53-05-00 FIG 32. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND RIGHT FORWARD OVER WING EXIT JAMB CRACKED TOP CENTER. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-05-00 FIG 32. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 3 STATION 1201-1205. REPLACED SEAT TRACK NR 3 FOR STATION 1186-1307 SRM 51-01. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - TWO CRACKS IN LEFT FORWARD EMERGENCY EXIT DOOR CUTOUT FRAME AT TOP. INSTALLED REPAIR PER SRM 53-05-00 FIG 32. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1280-1282. INSTALLED SEAT TRACK SPLICE PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1. INSTALLED NEW SEAT TRACK PER SRM 53-05. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - TWO CRACKS IN LEFT AFT EMERGENCY EXIT DOOR CUTOUT FRAME AT TOP, FS 916. INSTALLED REPAIR PER SRM 53-05-00 FIG 32. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND AFT LOWER CORNER OF FORWARD GALLEY DOOR CUTOUT CUSP WEB CORRODED STATION 198-200. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

TUL - FOUND FUSE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED IN RADIUS STATION 1463 RIGHT SIDE AND CRACKED IN LOWER LEG BETWEEN FASTENERS. STOP DRILLED CRACK IN RADIUS AND CUTOUT CRACKED AREA BETWEEN FASTENERS AND INSTALLED DOUBLER AND FILLER PER AARD 53-10-00-2. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT DIM. REPLACED EMERGENCY EXIT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (TAIL)

DFW - FLT 1507 - EN ROUTE DFW-YVR, FLIGHT ATTENDANT DETECTED HEAVY SMOKE IN CABIN. DECLARED EMERGENCY. RETURNED DFW, AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU. REPLACED ACM HEAT EXCHANGERS. REPLACED WATER SEPARATORS BAGS. ACCOMPLISHED PACK BURNOUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — DIRTY (AC BAY)

ORD - FLT 1224 - EN ROUTE SAN-ORD, DURING CLIMB-OUT, DETECTED SMOKE AT COCKPIT. TURNED OFF LEFT SIDE PACK, SMOKE DISSIPATED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED LEFT AND RIGHT SIDE COALESCER BAGS. PER PACK BURNOUT PER MM. NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (TAIL OVERHEAT)

DFW - FLT 1890 - DURING CLIMB-OUT, PASSING THROUGH 2,000 FEET, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY PROCEDURE CHECKLIST COMPLIED WITH AND LIGHT EXTINGUISHED. RETURNED DFW AND LANDED WITHOUT INCIDENT. RAN AIRCRAFT FOR EXTENDED PERIOD OF TIME AND COMPLETED LEAK CHECK. PRECAUTIONARY REPLACED OVERTEMP SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)