N7522A

Part: GENERATOR — FAILED (LT ENGINE) · airframe 64,278 hrs · 33,354 cycles

DFW - CREW REPORTED CONSTANT SPEED DRIVE RISE WAS OFF THE SCALE HIGH ON THE LEFT ENGINE. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,149 hrs · 33,278 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NUMBER 9. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,149 hrs · 33,278 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NUMBER 7. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,153 hrs · 33,279 cycles

EMERGENCY EXIT LIGHTS FOR BOTH THE LEFT AND RIGHT AFT OVERWING EXIT LIGHTS WOULD NOT SHUT OFF. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,153 hrs · 33,279 cycles

WITH ELECTRICAL POWER OFF CABIN EMERGENCY LIGHTS STAY ON. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,149 hrs · 33,278 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NUMBER 8. OPS CHECK NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,583 hrs · 32,947 cycles

SHEAR TIE CRACKED IN RADIUS FORWARD SIDE OF FRAME 1380 BETWEEN LONGERONS 13 AND 14 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-20.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,524 hrs · 30,726 cycles

FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,524 hrs · 30,726 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 30 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-107 IN CABIN OVERHEAD. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (AC BAY) · airframe 59,524 hrs · 30,726 cycles

AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES IN B5-109 COMPARTMENT. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,522 hrs · 30,135 cycles

LOWER SIDE OF THE FORWARD CABIN SUB FLOOR IS CORRODED AT STATION 161 RIGHT BUTTLINE 12. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER REF AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,515 hrs · 30,131 cycles

SEAT TRACK NUMBER 5 BLEND OUT OF LIMITS AT STATION 234. REMOVED DAMAGED MATERIAL, INSTALLED NEW PLUG, TREATED AND PRIMED PER SRM 53-05-00 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,515 hrs · 30,131 cycles

SEAT TRACK NUMBER 1 OUT OF LIMITS, STATION 278. REMOVED DAMAGED AREA AND INSTALLED REPAIR PLUG, TREATED AND PRIMED PER SRM 53-05-00 FIGURE 4A.

Part: ENGINE — LEAKING (RIGHT) · airframe 56,638 hrs · 29,119 cycles

ON CLIMB-OUT, RIGHT ENGINE POWER DECREASED TO APPROX 50 PERCENT. UNABLE TO REGAIN ANY POWER. SEVERAL MINUTES LATER, ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. OIL TEMP/ PRESSURE NORMAL. FUEL FLOW WAS EXCESSIVE ON RIGHT ENGINE SHUTDOWN. UPON ARRIVAL AT GATE, RIGHT ENGINE HAD OBVIOUS FUEL LEAK. RELOCATING TO HANGAR FOR FURTHER EVALUATION. OPEN.

Part: VALVE — FAILED (NLG STRUT) · airframe 56,137 hrs · 28,834 cycles

DURING CLIMB LANDING GEAR WOULD NOT RETRACT. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. ON GATE ARRIVAL NOSE GEAR STRUT WAS BOTTOMED OUT. NO DAMAGE NOTED OR EVIDENCE OF NOSE STRUT OIL LOSS. REPLACED INFLATION BOTTLE VALVE.

Part: BEAM — CORRODED (CQARGO BAY) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

AFT CARGO DOOR BEAM HAS CORROSION STATION 1155-1211. REPAIRED UNDER AARD 53-10-00-3.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON STRAP STATION 1212. REPLACED STRAP UNDER EA 53007201 AND SRM 53-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

STATION 1193 LEFT CUSP LOWER SIDE HAS AREA OF CORROSION. INSTALLED CUSP SHEET STA 1179-1200 UNDER SRM 53-20-00-16.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON LOWER CARGO DOOR BEAM, STATION 640-688. INSTALLED DOOR JAMB DOUBLER UNDER AARD 53-10-00-3.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON CUTOUT FOR RADIO ANTENNA STATION 605 LONGERON 30. INSTALLED NEW ANTENNA DOUBLER UNDER SRM 51-30-2 AND 51-30-05.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

FLOORBEAM AT STATION 1098 UNDER SEAT TRACK NUMBER 4 IS DAMAGED. INSTALLED DOUBLER ON FLOORBEAM AT STATION 1098 UNDER EA MD80-53-007159.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

ELONGATED HOLE IN RIGHT CUSP AT STATION 245. INSTALLED DOUBLER UNDER SRM 53-14-02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

SEAT TRACK GOUGED AT STATION 1100 ON SEAT TRACK NUMBER 4. INSTALLED SEAT TRACK PLUG AT STATION 1100 ON SEAT TRACK NUMBER 4 UNDER AARD 53-20-00-10.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON FORWARD CARGO LOWER DOOR PAN. INSTALLED NEW FORWARD CARGO LOWER DOOR PAN UNDER SRM 53-05-00.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON SUBFLOOR AT FORWARD END OF NUMBER 6 SEAT TRACK. INSTALLED DOUBLER UNDER AARD 53-20-00-25.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

CARGO CEILING INTERCOSTAL CRACKED. INSTALLED NEW INTERCOSTAL AT STATION 1041 UNDER SRM 51-30-05.

Part: BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

AFT SERVICE DOOR AFT GIRT BAR BRACKET HAS CORROSION. REPLACED GIRT BAR BRACKET UNDER SRM 51-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

LONGERON L4 CRACKED INBOARD AND OUTBOARD SIDES AT STATION 200. INSTALLED NEW LONGERON FROM STATION 170 TO 229 UNDER SRM 53-02-00.

Part: STOP FITTING — CRACKED (ENTRY DOOR) · airframe 55,968 hrs · 28,729 cycles

FORWARD ENTRY DOOR HAS INTERNAL CRACK IN RADIUS, FORWARD JAMB AT LOWER SIDE OF NUMBER 2 STOP BRACKET SUPPORT STRUCTURE. STOP DRILLED CRACK, DYE-CHECK CONFIRMED, INSTALLED DOUBLER UNDER SRM 52-05-00 FIG 31 (SHEET 3).

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON SUB FLOOR WEB OUTBOARD OF NUMBER 2 SEAT TRACK. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

LEFT CUSP HAS CORROSION AT STATION 1170 UNDER SERVICE DOOR AFT GIRT BAR FITTING. INSTALLED DOUBLER AND FILLER UNDER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 55,968 hrs · 28,729 cycles

RIGHT WING NUMBER 5 SLAT RIB IS CRACKED AT NUMBER 14 SLAT TRACK ATTACHMENT. REPLACED RIB UNDER SRM 57-50-13.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 55,968 hrs · 28,729 cycles

FORWARD ENTRY DOOR NUMBER 6 BEAM CRACKED AT BAYONET CRANK MOUNT HOLE. STOP DRILLED CRACK, DYE CHECKED, INSTALLED PASSENGER DOOR BEAM DOUBLER.

Part: RIB — CRACKED (LE SLAT) · airframe 55,968 hrs · 28,729 cycles

RIGHT WING NUMBER 5 SLAT OUTBOARD RIB IS CRACKED AT NUMBER 15 SLAT TRACK ATTACHMENT. REPLACED RIB UNDER SRM 57-50-13.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

CORROSION ON STRAP LONGERON 23L STATION 1303-1309. REPLACED STRAP UNDER SRM 51-30-05.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

TOP AFT CORNER OF WINDOW PAN IS CRACKED BETWEEN STATION 1060-1041 LEFT. INSTALLED DOUBLER UNDER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

SEAT TRACK NUMBER 5 IS CORRODED STATION 204. REPLACED NUMBER 5 SEAT TRACK UNDER SRM 51-30-05, 51-30-01, 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

CUSP CRACKED STATION 218-237. REPLACED CUSP UNDER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,968 hrs · 28,729 cycles

SEAT TRACK NUMBER 5 HAS CORROSION STATION 204. REPLACED NUMBER 5 SEAT TRACK FROM STATION 218 TO 246 UNDER SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,968 hrs · 28,729 cycles

LONGERON L2 CRACKED AT STATION 160. REMOVED AND REPLACED LONGERON AT STATION 148 TO 170 UNDER SRM 53-02-00.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 55,385 hrs · 28,413 cycles

DFW - CREW REPORTED SMOKE IN CABIN. EMERGENCY DECLARED, RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT AIR CYCLE MACHINE AND LEFT PACK TEMPERATURE CONTROL VALVE. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHT) · airframe 54,780 hrs

LGA - EMERGENCY LIGHT AT CEILING LEFT SIDE JUST FORWARD OF LAVATORY INOPERATIVE. RESEATED EMERGENCY LIGHT BATTERY FOR EMERGENCY LIGHT AT CEILING LEFT SIDE JUST FORWARD OF LAVATORY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - THE AFT OVERWING EMERGENCY LIGHTS STAYED ON WHEN POWERING DOWN THE AIRCRAFT. REPLACED BATTERY PACK FOR AFT OVERWING LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - CABIN CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 27 CAME ON WHEN THE AIRCRAFT POWER IS TURNED OFF. REPLACED BATTERY PACKS FOR ROWS 23 TO 27.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 54,229 hrs

LGA - EMERGENCY LIGHT AR SEAT ROWS 11 INOPERATIVE. REPAIRED WIRING ON CONNECTOR AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 54,229 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. REPAIRED WIRE AT CONNECTOR FOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHTS) · airframe 54,299 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 29 TO 32 INOPERATIVE. SECURED LOOSE BATTERIES ON EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — MALFUNCTIONED (APU BAY) · 53,320 cycles

DFW INFLIGHT T351/22AUG. AFTER TAKE OFF FLIGHT ATTENDANTS REPORTED BLUE HAZE COMING FROM AIR CONDITIONING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT (APU) DUE TO OIL SATURATING APU COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT ROW 29DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DISPLAY — INOPERATIVE (TURN AND BANK)

EWR-MIA, LIGHT SMOKE WITH ELECTRIC BURNING SMELL AT CRUISE. EMERGENCY FIRE SMOKE CHECK LIST COMPLETED. SMOKE ABATED UNTIL LANDING. SMOKE REAPPEARED IN COCKPIT AREA. FOUND NUMBER ONE NAVIGATION DISPLAY BURNED. REPLACED NUMBER ONE NAVIGATION DISPLAY MODE SELECT PANEL SYMBOL GENERATOR CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY PATH LIGHT ABOVE AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHT ABOVE AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - AFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

MAI - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING FOR FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (FS 266)

TUL - FUOND FUSELAGE SKIN DENTED AT RIVET STATION 266 ABOVE LONGERON 23R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24. (M)

Part: FRAME — CRACKED (FS 1485)

TUL - FOUND RIGHT CANT FRAME 1485, RT LOWER END, IS WORN AND CRACKED FROM CONTACT WITH ACTUATOR CASTING. INSTALLED REPAIR DOUBLER AS PER AARD 53-10-00-33 AND RE-INSTALLED FRAME STIFFENER. (M)

Part: SKIN (FS 249)

TUL - FOUND SEVERAL DEEP TOOL MARKINGS AROUND RIVET HEAD RIGHT STATION 249 LONGER 21R, FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: FRAME — DAMAGED (FS 712)

TUL - FOUND DAMAGE TO CARGO FRAME STATION 712, BETWEEN 26L AND 27L. INSTALLED DOUBLER PER AARD 53-10-00-4. (M)

Part: SEAT TRACK — CORRODED (FS 435)

TUL - FOUND CORROSION ON SEAT TRACK NR 4, STATION 435. CUT OUT CORRODED AREA AND INSTALLED PLUG PER HARD 53-20-00-10. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP CORROSION FROM STATION 509 TO 518 RIGHT. INSTALLED DOUBLER FROM STATION 505 TO 522 PER SRM 53-01 FIG 4-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP AT STATION 660. FABRICATED AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP IN SEVERAL AREAS STATION 503-598. REPLACED SECTION OF CUSP WITH NEW PER SRM 52-01 FIG 4-3. (M)

Part: TRACK — CORRODED (FS 1174-1307)

TUL - FOUND CORROSION BEYOND MM LIMITS SEAT TRACK NR 1 STATION 1174-1307. INSTALLED NEW SECTION OF TRACK PER SRM 51-10.

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 580-610. INSTALLED CUSP DOUBLER SRM 53-01 FIG 4-3 WITH HI-LOCKS USED AT AFT END OF DOUBLER UNDER TRACK NR 1 AND ALONG INBOARD OF NR 2 TRACK. (M)

Part: SEAT TRACK — CORRODED (FS 1200)

TUL - FOUND CORROSION ON SEAT TRACK NR 2, STATION 1200. REMOVED CORROSION, INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP OF CUSP RIGHT. CUT OUT CORRODED AREA AND INSTALLED REPAIR DOUBLER SRM 53-01 FIG 4-3. (M)

Part: VALVE — DEFECTIVE (LANDING GEAR)

DFW - FLT 1739 - ON APPROACH DFW, LANDING GEAR INDICATED ALL THREE RED UPON LOWERING GEAR HANDLE. BOTH HYDRAULIC QUANTITY AND PRESSURE WAS NORMAL. PERFORMED EMERGENCY GEAR EXTENSION ACCORDING TO THE OPERATING MANUAL. VISUALLY VERIFIED LANDING GEAR DOWN AND LOCKED THROUGH PORT. LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL VALVE. ACCOMPLISHED GEAR SWING AND LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: AIR DIST — ODOR (CABIN)

DFW - FLT 751 - DURING CLIMB FROM TUL-DFW, SLIGHT BURNING SMELL NOTED IN COCKPIT AND CABIN. SMELL DISSIPATED EN ROUTE. AIRCRAFT LANDED DFW WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT OF BOTH PACKS. NO INDICATION OF SMELL OR SMOKE FOLLOWING BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF FIRST CLASS CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WATER SEPARATOR — CONTAMINATED (A/C BAY)

MAF - FLT 839 - EN ROUTE DFW-SAN, APPROX 45 MINS INTO FLT, AFT CABIN F/A REPORTED STRONG SMELL OF SOMETHING BURNING IN AREA NEAR MID-CABIN. AS COCKPIT DOOR WAS OPENED THE SMELL OF HOT ELECTRICAL/HOT PLASTIC BECAME APPARENT ALONG WITH A LIGHT HAZE IN CABIN. INITIATED EMERGENCY DESCENT, PEFORMED CABIN/COCKPIT FIRE/SMOKE CHECKLIST SMOKE REMOVAL. EMERGENCY LANDED AT MAF W/O INCIDENT. SOURCE OF SMELL COULD NOT BE DETERMINED BUT LINGERED IN A/C CABIN FOR ONE HOUR AFTER COMPLETE POWER DOWN. PERFORMED PACK BURN OUT PER MM. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS, RAN BOTH PACKS FOR 2 HOURS. NO SMELL NOTED, OPERATE ALL OVENS AND ALL LIGHTS WITH NO SMELL OR SMOKE NOTED. CHECKED E/E AND ALL CARGO PITS NO SM

Part: SENSORS — MALFUNCTIONED (TAIL COMPARTMENT)

DFW - FLT 1676 - AFTER TAKEOFF DFW, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. STAYED ON STEADY FOR ABOUT 30 SECONDS. ACCOMPLISHED EMERGENCY PROCEDURES CHECK LIST. THE LIGHT FLICKERED ON AND OFF FOR ABOUT 2 MINUTES. DECISION TO LAND BACK AT DFW WAS MADE AND THE LAST 7 MINUTES THERE WAS NO FURTHER INDICATION OF THE LIGHT. LANDED DFW WITHOUT INCIDENT. RAN ENGINES, APU AND PACKS AND COULD NOT DUPLICATE. CHECKED TAIL COMPARTMENT DUCTING FOR LEAKS, NO LEAKS NOTED. REPLACED BOTH TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHTS — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATED LEFT AND RIGHT OVERWING EXIT INTERIOR LIGHTS. CYCLED AFT EMERGENCY LIGHT SWITCH AND LEFT AND RIGHT OVERWING EXIT INTERIOR LIGHTS CHECKED NORMAL OPERATION. UNABLE TO DUPLICATE PROBLEM. (M)

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

DFW - FLT 797 - AFTER TAKEOFF DFW WHEN LANDING GEAR LEVER RAISED, LANDING GEAR WOULD NOT RETRACT WITH HYDRAULIC PRESSURE INDICATING NORMAL. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LUBRICATED LANDING GEAR AND ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)