N7546A

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 66,357 hrs · 34,544 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FAILED TEST. REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 65,176 hrs · 33,859 cycles

FORWARD EMERGENCY LIGHT IN AFT STAIR WELL DAMAGED. REPLACED LAMP FOR FORWARD EMERGENCY LIGHT IN AFT STAIR WELL. OPERATIONS CHECKED NORMAL.

Part: SWITCH — INOPERATIVE (MLG) · airframe 63,990 hrs · 33,201 cycles

CREW REPORTED LANDING GEAR UNSAFE INDICATION. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED S1-89 GEAR HANDLE SWITCH. SYS GROUND CHECK NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,742 hrs · 33,063 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 9 TO 19DEF INOPERATIVE. REPLACED MODULE AND BATTERY PACK AT M10953.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,964 hrs · 32,629 cycles

EMERGENCY LIGHTS AT FORWARD GALLEY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,946 hrs · 32,620 cycles

ALL EMERGENCY LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED ROW 6 BIN BATTERY PACK. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,081 hrs · 31,571 cycles

THE 1418 FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED REPAIR DOUBLERS PER SRM 53-03-0.

Part: CASTING — CRACKED (RT SPOILER) · airframe 61,081 hrs · 31,571 cycles

RIGHT WING GROUND SPOILER CASTING IN TRAILING EDGE OF WING IS CRACKED AT FORWARD OUTBOARD SIDE. INSTALLED NEW CASTING PER AARD 51-10-00-05.

Part: DUCT — DAMAGED (AC BAY) · airframe 59,846 hrs · 30,859 cycles

OKC - CREW REPORTED TAIL TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED OKC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BOOT OFF RAM AIR Y DUCT AND PIN HOLE IN THE DUCT. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,396 hrs · 30,602 cycles

FORWARD OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

SKIN AROUND AUXILIARY POWER UNIT EXHAUST DUCT HAS HEAT DAMAGE STATION 1418. INSTALLED SKIN REPAIR DOUBLER PER EA MD80-53-012437.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

HEAVY CARGO / AFT- CORROSION ON RIGHT TIE DOWN TRACK FROM STATIONS 1212 TO 1322. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-01.

Part: WEB — DAMAGED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

DAMAGE IN LIGHTENING HOLE OF WEB STATION 862 ABOVE LONGERON 15. INSTALLED WEB REPAIR PER EA MD80-012389.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

AFT CARGO CORROSION ON FORWARD RIGHT TIE DOWN TRACK BETWEEN STATIONS 1155 TO 1117. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

CRACK FOUND IN RADIUS OF FRAME STATION 864 RIGHT SIDE. COMPLETED INSTALL FRAME REPAIR PER SR 09530282 AND K3290AG AND SERVICE BULLETIN MD80-53A301.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

HEAVY CARGO AFT CORROSION ON RIGHT TIE DOWN TRACK FROM STATIONS 1212 TO 1322. INSTALLED TIE DOWN TRACK PER SRM 51-30-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

HEAVY CARGO AFT CORROSION ON LEFT TIE DOWN TRACK FROM STATION 1007 TO 1220. INSTALLED NEW TIE-DOWN TRACK PER SRM 51-30-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

SHEAR TIE CRACKED AFT SIDE OF STATION 1451 LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE PER AARD 51-00-00-012 SRM 51-30-05.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

STIFFENER AFT SIDE OF STATION 1451 CRACKED AT LONGERON 2 LEFT. INSTALLED NEW STIFFENER PER AARD 51-00-00-012 AND SRM 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

LOWER FORWARD CORNER OF DOORWAY FITTING IS CORRODED. INSTALLED NEW FITTING PER DWG 5930483 AND AARD 51-00-00-012.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

CUSP MEMBRANE CORRODED AT FORWARD ENTRY IN SEVERAL PLACES BETWEEN STATION 180 AND 200. REPAIRED PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

SKIN CRACKED AT STATION 1380 ABOVE STRINGER 14 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

SEAT TRACK 5 OUTBOARD FLANGE CORRODED AT STATION 204. REMOVED AND REPLACED SEAT TRACK 5 STATION 200 TO 246 AND INSTALLED SPLICE PER SRM 53-05-00 FIGURE 4.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

LONGERON 14 AT STATION 1410 HAS HEAT DAMAGE. REMOVED DAMAGED SECTION OF LONGERON 14 FROM STATION 1389 TO STATION 1435 AND INSTALLED A NEW SERVICEABLE SECTION OF LONGERON PER ATTACHED EA MD80-53-012438.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

CRACK IN RIGHT CUSP STATION 219 UNDER NUMBER 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

TWO CRACKS IN LEFT CUSP BETWEEN STATIONS 218 AND 237. REMOVED AND REPLACED LEFT CUSP SHEET BETWEEN STATIONS 218 AND 237 PER AARD53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

LEFT CUSP STATION 612 TO 615 CORROSION ON BOTTOM SIDE OUT OF LIMITS. INSTALLED NEW CUSP DOUBLER FROM STATION 608 TO STATION 630 LEFT PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

FORWARD CABIN SUB FLOOR HAS CORROSION AT STATION 200 TO 208 RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 56. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

LEFT CUSP STATION 518-519 CORROSION ON LOWER SIDE OUT OF LIMITS. REMOVED CORROSION PER AARD 53-20-00-16. INSTALLED DOUBLER AT LEFT CUSP STATION 518-519 PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

AFT CARGO LOWER AFT CORNER OF DOORWAY FITTING IS CORRODED. INSTALLED NEW FITTING AFT CORNER OF DOOR PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

SUB FLOOR WEB HAS CORROSION AND WORN SPOTS STATION 1136 TO 1174. INSTALLED LEFT CUSP DOUBLER REPAIR AND CUSP FILLER PER AARD 53-20-00-16 UNDER AFT GIRT BAR FITTING STATION 1170.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

RIGHT CUSP AT STATION 620 TO 628 IS OUT OF MANUAL LIMITS. INSTALLED RIGHT CUSP DOUBLER AT STATION 620 TO 628 PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

AFT CARGO LOWER FORWARD CORNER DOORWAY FITTING IS CORRODED. INSTALLED NEW FITTING PER DWG 5930483 & AARD 51-00-00-012.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

FUSELAGE SKIN CRACKED BELOW FASTENER HOLE STATION 1380 ABOVE STR 14R. INSTALLED DOUBLER PER SRM 53-34-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

CORROSION ON SHEAR TIE AT STATION 1287 LONGERON 29 RIGHT TO LONGERON 30. FABRICATED SERVICEABLE SHEAR TIE AND REPAIR SPLICES PER SRM 53-03-00. TREATED, PRIMED AND PAINTED ALL BARE AREAS PER SRM 51-10-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

RIGHT CUSP AT STATION 560 TO 565 OUT OF LIMITS. INSTALLED DOUBLER RIGHT CUSP STATION 555 TO 568 AS PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

AFT CARGO CORROSION ON LOWER SIDE OF LEFT CUSP AT STATION 1140. INSTALLED CUSP REPAIR DOUBLER AT LEFT STATION 1140 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

CORROSION ON RIGHT CUSP STATION 620 TO 628. REMOVED CORROSION INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

CORROSION ON SUBFLOOR UNDER AFT SERVICE DOOR AFT GIRT BAR FITTING. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,245 hrs · 29,369 cycles

DENT IN FUSELAGE SKIN STATION 252 ABOVE LONGERON 18 LEFT. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-04-00 FIGURE 38 SHEET 36.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 57,245 hrs · 29,369 cycles

FUSELAGE AFT LAV SVC PANEL HAS CORROSION BETWEEN THE SKIN AND THE PAN AT THE LOWER AFT CORNER. INSTALLED NEW AFT LAVATORY SERVICE PANEL PAN PER AARD 53-30-00-07.

Part: BUSHING — WORN (LE SLAT) · airframe 57,245 hrs · 29,369 cycles

BUSHING WORN ON KNUCKLE RIB ON SLAT 1041. REPLACED WORN BUSHING PER ESO 80117 ON SLAT 1041.

Part: PAN — CRACKED (WINDOW) · airframe 57,245 hrs · 29,369 cycles

LEFT UPPER AFT WINDOW PAN TAB CRACKED AT STATION 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,245 hrs · 29,369 cycles

LEFT UPPER AFT WINDOW PAN TAB CRACKED AT STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 55,048 hrs · 28,161 cycles

LEFT NR 1 DOOR PORTABLE EXIT LIGHT INOPERATIVE. REPLACED PORTABLE LIGHT ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,414 hrs · 27,234 cycles

AFT FLIGHT ATTENDANT SEAT AT AFT SERVICE DOOR, EMERGENCY LIGHT BATTERY WEAK. REPLACED BATTERY PACK FOR AFT SERVICE DOOR EMERGENCY LIGHT.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 53,414 hrs · 27,234 cycles

EMERGENCY BATTERY PACK INOPERATIVE AT STATION 211 CENTER. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,414 hrs · 27,234 cycles

THE 1418 FRAME CRACKED AT LONGERON 2R. DOUBLER INSTALLED PER SRM 53-01 FIGURE 2 AND EA MD80-53-005611.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,414 hrs · 27,234 cycles

LONGERON 2R IS CRACKED AFT OF STATION 1418. INSTALLED REPAIR PER AARD 53-30-00-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,414 hrs · 27,234 cycles

CRACK IN BULKHEAD SKIN AT RIGHT BOTTOM ALIGNMENT PIN FOR RADOME, STATION 37. INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,414 hrs · 27,234 cycles

CANT FRAME AT STATION 1510 CRACKED ABOVE MAINTENANCE LIGHT. INSTALLED DOUBLER PER EA MD80-53-00-5606.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,414 hrs · 27,234 cycles

CANTED FRAME CRACKED BELOW MAINTENANCE LIGHT SWITCH AT STATION 1510. INSTALLED DOUBLER PER EA MD80-53-00-5606.

Part: WIRE — BROKEN (CABIN) · airframe 51,010 hrs

DFW - EMERGENCY LIGHT AT LEFT STAIRWELL HAS BROKEN WIRE. REPLACED QUICK DISCONNECT TERMINAL FOR EMERGENCY LIGHT AT LEFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 51,005 hrs

DFW - EMERGENCY LIGHT AT FORWARD TAIL COMPARTMENT WALL LENS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD TAIL COMPARTMENT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — OIL CONSUMPTION (LEFT)

DFW INFLIGHT T569/20APR IN DESCENT WITH THROTTLES AT IDLE LEFT OIL PRESSURE LOW LIGHT ILLUMINATED ALONG WITH OIL PRESSURE OF ZERO. SHUT DOWN LEFT ENGINE. LANDED DFW WITHOUT INCIDENT. SINGLE ENGINE TIME 15 TO 20 MINUTES. REPLACED NUMBER ONE ENGINE ON 23 APR 2007 AT DFW DUE TO OIL PRESSURE LOSS, OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT FORWARD OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FORWARD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (SEAT 20)

DEN) OVERHEAD EMERGENCY LIGHTS AT SEAT 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT 20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — DAMAGED (AFT FUSELAGE)

AIRCRAFT EN ROUTE ORD TO YYC, CREW OBSERVED SMOKE IN THE CABIN THAT WOULD NOT DISSIPATE. AIRCRAFT RETURNED TO ORD. REPLACED APU PERFORMED PACK BURN OUT AND CHANGED COALESCER BAGS. LEAK CHECKED AND SYSTEM GROUND CHECKED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE ABOVE FORWARD OVERWING EXITS. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE AT LOCATIONS B5-23. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND HORIZONTAL FLOORBOARD SUPPORT AT STATION 200 HAS AREA OF CORROSION AT RBL 49. INSTALLED NEW FLOOR SUPPORT AT STATION 200 RBL 49 SRM 51-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND LONGITUDINAL FLOOR SUPPORT AT RBL 52 HAS AREA OF CORROSION AT STATION 172 AND 195. INSTALLED NEW LONGITUDINAL FLOORBOARD SUPPORT AT RBL 52 STATION 172-195 SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED STATION 1306. INSTALLED NEW CUSP SECTION FROM LEFT 1250 TO 1306 AS PER SRM 53-05 FIG 97. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN NR 2 SEAT TRACK APPROX STATION 1250. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1240-1309 PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, UNDER NR 1 SEAT TRACK STATION 1175. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-00-00-02. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO DOOR CUT OUT LOWER DOOR BEAM. REMOVED AND REPLACED AFT CARGO CUT OUT LOWER DOOR BEAM PER AARD 53-10-00-3. (M)

Part: WEB — PUNCTURED (FUSELAGE)

TUL - FOUND LEFT CUSP HAS FOUR PUNCTURE HOLES AT NR 1 SEAT TRACK, STATION 1200 TO 1214. INSTALLED DOUBLER AS PER AARD 53-00-00-02 SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND FLOOR WEB HAS CORROSION STATION 190-200, RBL 49-52. CUT OUT CORROSION INSTALLED DOUBLER PER SRM 51-01 FIG 2 SHEET 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND FLOOR WEB HAS CORROSION STATION 178-180 RBL 50 TO 52. CUT OUT CORROSION INSTALLED DOUBLER PER SRM 51-01 FIG 2 SHEET 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND THREE SMALL AREAS SURFACE CORROSION LEFT CUSP STATION 526. CUT OUT CORROSION, FABRICATE DOUBLER ALODINED, AND PRIMED. REPAIR AREA AND DOUBLER, INSTALLED DOUBLER AS PER AARD 53-00-00-02. (M)

Part: WIRE — BROKEN (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. RE-SPLICED OVERHEAD EMERGENCY EXIT LIGHT WIRE AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT AFT STAIR SLIDE WALL INOPERATIVE. REPLACED EMERGENCY LIGHT SPLICE AT AFT STAIR SLIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW DURING OVERNIGHT MAINTENANCE OVERHEAD EMERGENCY EXIT LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DEFECTIVE (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT TAIL CONE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE RELEASE HANDLE EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED ENVIRONMENTAL SPLICE ON TAIL CONE RELEASE HANDLE EMERGENCY FLOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM WING EXITS AFT INOPERATIVE. REPAIRED WIRE IN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRS EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REPAIRED WIRE ON AFT STAIRS EMERGENCY EXIT FLOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLIGHT ATTENDANT FLASHLIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED EMERGENCY FLIGHT ATTENDANT FLASHLIGHT AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FILTER — CLOGGED (RT ENGINE)

DFW - FLT 2083 - EN ROUTE DFW/IAH IN CRUISE, RIGHT ENGINE OIL STRAINER CLOGGIN G LIGHT ILLUMINATED. OIL TEMPERATURE WAS 128 DEGREES AND OIL PRESSURE 45 PSI. RETARDED THROTTLE AND LIGHT WENT OUT. DECLARED AN EMERGENCY AND AIR INTERRUPTED. ACCOMPLISHED REDUCED THRUST APPROACH TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE OIL FILTER, DRAINED AND SERVICED OIL TO FULL. RAN ENGINE AT HIGH POWER, NO DISCREPANCIES NOTED, LEAK CHECK GOOD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: COALESCER — CONTAMINATED (ACM BAYS)

DFW - FLT 0425 - AFTER TAKEOFF DFW DURING CLIMB-OUT, ACRID ODOR NOTED IN CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LT AND RT COALESCER BAGS AND ACCOMPLISHED PACK BURN-OUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (X)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT FORWARD PART AND MID SECTION OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT IN FORWARD SECTION OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)