N594AA

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,755 hrs · 28,512 cycles

THE 1510 CANT FRAME CRACKED BELOW MAINTENANCE LIGHT SWITCH. INSTALLED DOUBLER PER SRM 53-01-00.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 65,083 hrs · 27,658 cycles

DFW - CREW REPORTED RIGHT ENGINE GENERATOR TRIPPED IN FLIGHT, ACCOMPANIED BY AC CROSSTIE LOCKOUT LIGHT. ACCOMPLISHED QRH PROCEDURE AND RESTORED POWER WITH AUXILIARY POWER UNIT. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,169 hrs · 27,177 cycles

GOUGE IN FUSELAGE 7 INCHES FORWARD OF RIGHT NUMBER 1 DOOR AND 4 INCHES BELOW LONGERON 18 RIGHT. REPAIRED FUSELAGE DAMAGE JUST AFT OF STATION 160 AND BELOW RIGHT CUSP LINE WITH EXTERNAL DOUBLER PER EA MD80-53-022003.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,169 hrs · 27,177 cycles

DAMAGE TO FORWARD RIGHT FUSELAGE FORWARD OF GALLEY DOOR AND JUST BELOW FLOOR LINE. REPAIRED FUSELAGE DAMAGE JUST AFT OF STATION 160 AND BELOW RIGHT CUSP LINE WITH EXTERNAL DOUBLER PER EA MD80-53-022003.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,144 hrs · 26,661 cycles

FUSELAGE RIGHT SIDE CRACK IN SKIN AT FASTENER HOLE STATION 1380 JUST ABOVE LONGERON 14 RIGHT. INSTALLED DOUBLER PER SRM 53-01-00 AND AARD 53-30-00-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,790 hrs · 26,480 cycles

AUS - CREW REPORTED DURING CLIMBOUT MULTIPLE BIRD STRIKES TO AIRCRAFT. EMERGENCY DECLARED FLIGHT RETURNED AUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT FERRIED TO TUL FOR STRUCTURAL REPAIRS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 61,158 hrs · 25,656 cycles

EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RECONNECTED PLUG THAT WAS PULLED FROM WALL. OPS CHECK NORMAL.

Part: SHROUD — INOPERATIVE (CABIN) · airframe 61,158 hrs · 25,656 cycles

EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 11D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,158 hrs · 25,656 cycles

EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,158 hrs · 25,656 cycles

LEFT NUMBER 1 DOOR HELD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR HELD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,158 hrs · 25,656 cycles

EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR SEAT 12D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

VERTICAL SUPPORT CRACKED BELOW FLOORBEAM 864 AT SEAT TRACK NUMBER 4. INSTALLED NEW VERTICAL SUPPORT AT STATION 864 BELOW SEAT TRACK NUMBER 4 PER SRM 51-30-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CABIN CORROSION ON NUMBER 1 GALLEY TIE DOWN FITTING STATION 160 RIGHT BUTTLINE 51. REPLACED G1 GALLEY TIE DOWN FITTING PER SRM 51-30-02 AND 51-30-05 PER EA MD80-51-010576 DATED 05/06/2010.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CRACK IN CUSP SHEET AT LIGHTENING HOLE OUTBOARD SIDE SEAT TRACK SIX. NEW CUSP SHEET INSTALLED PER SRM 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CABIN CORROSION ON NUMBER 1 GALLEY TIE DOWN FITTING STATION 160 RIGHT BUTTLINE 45. REPLACED G1 GALLEY TIE DOWN FITTING PER SRM 51-30-02 AND 51-30-05 PER EA MD80-51-010576.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

STATION 804 ELONGATED HOLE IN INBOARD FLANGE NUMBER 6 SEAT TRACK. INSTALLED STRAP REPAIR PER EA MD 80-53-010603.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CABIN CORROSION ON NUMBER 1 GALLEY TIE DOWN FITTING STATION 160 RIGHT BUTTLINE 45. COMPLETED INSTALLATION OF G-1 GALLEY TIE DOWN FITTING AT STATION 160 RIGHT BUTTLINE 45 PER SRM 51-30-02 AND 51-30-05.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

FLOOR SUPPORT BRACKET UNDER CUSP AT AFT GIRT BAR ATTACHMENT, AFT SERVICE DOOR, HAS CORROSION AT NUT PLATE HOLES. REPLACED SUPPORT PER SRM 51-30-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CORROSION BEYOND MANUAL LIMITS STATION 1200 TO 1208, RIGHT CUSP. INSTALLED CUSP DOUBLER PER AARD 51-20-00-16 AND SRM 51-10-03, SRM 51-30-01, AND SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CUSP CRACKED AT LIGHTENING HOLE AT STATION 218 RIGHT SIDE OUTBOARD OF SEAT TRACK 6. REMOVED AND REPLACED CUSP SHEET RIGHT SIDE STATION 218 TO 237.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CRACKED CUSP AT LIGHTENING HOLE STATION 218 RIGHT OUTBOARD OF SEAT TRACK NUMBER 6. INSTALLED NEW CUSP SHEET AT RIGHT STATIONS 218 TO 237 PER SRM 51-30-00.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CABIN CORROSION ON NUMBER 1 GALLEY TIE DOWN FITTING STATION 160 RIGHT BUTTLINE 51. COMPLETED INSTALLATION OF NEW G-1 TIE DOWN FITTING STATION 160 RIGHT BUTTLINE 51 PER SRM 51-30-02 AND 51-30-05.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

STATION 877 SEAT TRACK NUMBER 6, CORROSION REMOVAL FROM SEAT TRACK LIP BEYOND MM LIMITS. INSTALLED SEAT TRACK PLUG AND CHANNEL REPAIR PER AARD 53-20-00-10.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

ELONGATED HOLE IN INBOARD FLANGE OF SEAT TRACK NUMBER 6 AT AFT END OF SEAT TRACK SPLICE STATION 804. INSTALLED FREEZE PLUG PER EA MD80-53-010603 AT STATION 804 SEAT TRACK 6. INSTALLED NEW INBOARD STRAP PER EA MD80-53-010603.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CORROSION ON SUB-FLOOR UNDER GIRT BAR BRACKET STATION 1174. REMOVED CORROSION INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,179 hrs · 24,753 cycles

CORROSION ON RIGHT TIE DOWN TRACK STATIONS 1271 TO 1287. INSTALLED SERVICEABLE TIE DOWN TRACK PER SRM 51-30-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

INTERCOSTAL HAS CRACK AT AFT ATTACH FASTENER AIRCRAFT CENTERLINE STATION 1041. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 4 USING SINGLE PIECE MATERIAL PER AARD 53-10-00-15.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CRACK IN TOP OF INTERCOSTAL STATIONS 1271 TO 1287. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,179 hrs · 24,753 cycles

CORROSION ON TOP AND BOTTOM OF INTERCOSTAL STATION 1322 BETWEEN LONGERON 27 RIGHT AND LONGERON 28 RIGHT. INSTALLED INTERCOSTAL PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

SEAT TRACK NUMBER 1 OUT OF LIMITS AT STATION 490 TO 495. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

CABIN VERTICAL SUPPORT BRACKET CRACKED BELOW FLOORBEAM STATION 927 AT SEAT TRACK 4. INSTALLED SUPPORT BRACKET PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,179 hrs · 24,753 cycles

SUB FLOOR CORRODED AT FORWARD SERVICE DOOR. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — CRACKED (CARGO BAY) · airframe 59,179 hrs · 24,753 cycles

AFT CARGO T-CLIP IS CRACKED AT STATION 1203 INBOARD OF LOWER DOOR BEAM. INSTALLED SERVICEABLE T-CLIP AT STATION 1203 PER SRM 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

FUSELAGE DENT WITH CREASE AT STATION 1429 LONGERON 2 LEFT. DYE-CHECKED DENT. INSTALLED DOUBLER REPAIR PER AARD 53-30-00-02.

Part: SKATE ANGLE — CRACKED (PYLON) · airframe 59,179 hrs · 24,753 cycles

FUSELAGE HAS A CRACK IN LOWER SKATE ANGLE BETWEEN LEFT PYLON AND FUSELAGE AT CANT FRAME AT STATION 1463. INSTALLED REPAIR DOUBLER PER AARD 54-20-00-1.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,179 hrs · 24,753 cycles

CRACK IN LEFT SIDE CUSP AT FASTENER HOLE STATION 846. REPAIRED CRACK WITH REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

DENT ON FUSELAGE WITH GOUGE AT STATION 234 BETWEEN 19 LEFT AND 20 LEFT. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02 & BOEING DRAWING SG09530001.

Part: PAN — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

RIGHT SIDE WINDOW PAN CRACKED AT UPPER AFT CORNER. DOUBLER INSTALLED PER REPAIR DOCUMENT 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

RIGHT SIDE WINDOW PAN CRACKED AT LOWER FORWARD CORNER. REPAIR DOUBLER INSTALLED PER REPAIR DOCUMENT 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,179 hrs · 24,753 cycles

FORWARD LEFT FUSLAGE HAS DENT AT STATION 237 BETWEEN LONGERON 17 AND LONGERON 18 NO LATER THAN NEXT HEAVY C CHECK PERFORM PERMANENT REPAIR PER SRM 53-04-00. INSTALLED DOUBLER REPAIR PER SRM 53-04-00 FIGURE 12B AND SRM 53-34-00 FIGURE 2.

Part: SENSOR — FAILED (RUDDER) · airframe 58,453 hrs · 24,417 cycles

EWR - CAPTAIN REPORTED ON APPROACH RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT ILLUMINATE BUT ON SECOND APPROACH LIGHT ILLUMINATED. EMERGENCY DECLARED LANDED EWR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER TRAVEL UN-RESTRICTED SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 57,981 hrs · 24,215 cycles

EMERGENCY LIGHT AT OVERHEAD SEAT ROW 18 HAS MISSING LENS. REPLACED LENS.

Part: SHROUD — MISSING (CABIN) · airframe 57,596 hrs · 24,043 cycles

EMERGENCY LIGHT SHROUD MISSING AT SEAT 27D. REPLACED SHROUD AND LENS AT SEAT 27D.

Part: HEAT EXCHANGER — CRACKED (AC BAY) · airframe 55,319 hrs · 23,072 cycles

PVR - INFLIGHT PVR-ORD. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMB OUT. EMERGENCY DECLARED LANDED PVR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. LEFT HEAT EXCHANGER HAS FOUR INCH CRACK IN LOWER CORNER. APPLIED THREE LAYERS OF SPEED TAPE OVER AFFECTED AREA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 54,710 hrs · 22,808 cycles

CORROSION ON HORIZONTAL FLANGE OF FORWARD CARGO DOOR PAN, STATION 500. REPAIRED PER ESO80559 DATED 11-20-08.

Part: LONGERON — CRACKED (ZONE 200) · airframe 54,710 hrs · 22,808 cycles

LONGERON 2R END FITTING CRACKED AT STATION 1420. REPAIRED PER AARD 53-30-00-2.

Part: LONGERON — CRACKED (ZONE 200) · airframe 54,710 hrs · 22,808 cycles

LONGERON 2L CRACKED JUST AFT OF FRAME 1418. REPAIRED PER AARD 53-30-00-2.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 54,710 hrs · 22,808 cycles

CORROSION ON LOWER SIDE OF CABIN SUBFLOOR BELOW G1 GALLEY. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVAE. REPLACED BATTERY PACK AT B5-23 FOR EMERGENCY LIGHTS AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY FLASHLIGHT AT FORWARD UPPER POSITION HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 29DEF FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 9DEF INOPERATIVE. REPLACED BATTERY PACK AT B5 102 FOR EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20DEF FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,567 hrs · 53,567 cycles

LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25DEF FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: SLIDE — MISALIGNED (L2 DOOR)

LGA - WHEN AFT GALLEY LEFT NR 2 DOOR IS ARMED THE VELCRO TABS ARE NOT ALIGNED WITH GIRT BAR AND MANUAL INFLATION HANDLE IS EXPOSED. REPLACED LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 13D INOPERATIVE AND MISSING LENS COVER. REPLACED LAMPS AND LENS COVER FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (CABIN)

SFO - RED AND WHITE EMERGENCY LIGHTS AT 23D INOPERATIVE. REPAIRED EMERGENCY LIGHT WIRE HARNESS BEHIND SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — BLOWN (A/C BAY)

DEN - FLT 830 - DURING CLIMB-OUT FROM PDX AT 27,000 FEET TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. AFTER RED BOX, LIGHT WENT OUT. LIGHT FLICKERED A FEW TIMES THE NEXT 4 MINUTES. SEEMED TO BE ASSOCIATED WITH RIGHT DUCT TEMPERATURE. LANDED DENT WITHOUT INCIDENT. REPLACED RIGHT TEMPERATURE SENSING DUCT ASSEMBLY AND LOWER FLEX DUCT. RAN PACKS AND LEAK CHECKED. NO LEAKS NOTED, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT REMAINED OFF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK NR 3, CORRODED AT STA 1232, STA 1275, AND STA 1300. C/A: SPLICED IN SERVICEABLE SEAT TRACK FROM STA 1185 TO STA 1309 IAW SRM.

Part: BEAM — CORRODED (FUSELAGE)

AFT SERVICE DOOR JAMB BEAM. FOUND CORROSION ON DOOR JAMB BEAM FROM STA. 1155 TO 1212, REPLACED-OUT OF LIMITS. INSTALLED DOOR JAMB BEAM IAW AARD.

Part: BELTFRAME — CORRODED (FUSELAGE)

BELTFRAME STA 1271, CORROSION ON BELTFRAME STA 1271, LONGERON 30. INSTALLED DOUBLER. (2002-1185, AMC4)

Part: WEB — CRACKED (FUSELAGE)

CUSP WEB, CRACKED AND CORRODED AT STA 150 TO STA 170. REPLACED CUSP WEB SHEET, STA 150 TO STA 170 IAW SRM. (AMC4)

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 4 SEAT TRACK CORRODED AT STA 237. INSTALLED SEAT TRACK PLUG IAW SRM.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN, DENT IN FUSELAGE, STA 180 L4L ABOVE MAIN ENTRY DOOR. BUMPED OUT DENT AND INSTALLED TWO ROW DOUBLER IAW SRM. DYE CHECKED, NO CRACKS FOUND. (AMC4)

Part: WEB — CRACKED (FUSELAGE)

CUSP, STA 1261 RIGHT FUSELAGE CUSP WEB, CRACKED. INSTALLED DOUBLER.

Part: SEAT TRACK — CORRODED (CABIN)

NR 1 SEAT TRACK TOPSIDE AND GALLEY MOUNT HOLE CORRODED STA 1209. REMOVED CORROSION BY ROUTING OUT. INSTALLED PLUG REPAIR IAW SRM. TREATED AND PRIMED IAW SRM.

Part: WEB — CORRODED (FUSELAGE)

CORROSION ON CUSP WEB UNDERNEATH GALLEY TIE DOWN, INBOARD OF SEAT TRACK NR 4 AT STA 218. INSTALLED DOUBLER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 1 SEAT TRACK GALLEY MOUNT CORRODED AT STA 1234. C/A: REMOVED CORROSION BY ROUTING OUT INSTALLED PLUG AS IAW SRM. TREATED AND PRIMED.

Part: SENSOR — DEFECTIVE (TAIL)

LAS - FLT 1598 - EN ROUTE LAS-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF FROM LAS. RETURNED LAS AND LAND WITHOUT INCIDENT. REPLACED BOTH LEFT AND RIGHT TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HEAT EXCHANGER — MALFUNCTIONED (A/C BAY)

DFW - FLT 1645 - IMMEDIATELY AFTER TAKEOFF DFW EN ROUTE PDX, BLUISH GRAY SMOKE APPEARED IN COCKPIT AND CABIN WITH A BURNED RUBBER SMELL. GALLEY POWER ANF RECIRCULATION FAN TURNED OFF. APPROXIMATELY 5 MINUTES LATER SMOKE SEEMED TO THIN. NO LOSS OF ENGINE OIL OR HYDRAULIC FLUID NOTED. ALL ELECTRICAL INDICATIONS NORMAL. RETURNED AND LANDED DFW WITHOUT INCIDENT. INCIDENT UNDER INVESTIGATION. REPLACED RIGHT PRIMARY AND SECONDARY HEAT EXCHANGER, ALSO RIGHT ACM. ACCOMPLISHED PACK BURN AND ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — LEAKING (NR 1 ENGINE)

SAT - FLT 1156 - EN ROUTE MEX-DFW, DETECTED LEFT ENGINE OIL LOSS TO THREE QUARTS. DIVERTED SAT AND LANDED WITHOUT FURTHER INCIDENT. REPLACED OIL PUMP ASSEMBLY. ACCOMPLISHED HIGH POWER ENGINE RUN UP. NO LEAKS NOTED SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROL MODULE — DEFECTIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED AISLE PATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT — REQ'D SERVICE (NLG)

LAX - FLT 2098 - AFTER TAKEOFF LAX, WHEN LANDING GEAR RETRACTED, RED NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED WITH ASSOCIATED WIND NOISE GEAR AREA. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO LAX, LANDING OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OIL AND NITROGEN SERVICING TO NOSE GEAR STRUT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - FLT 0594 - DURING DEPLANING, EMERGENCY EXIT FLOOR PATH LIGHTS ON RIGHT SIDE OF AIRCRAFT FOUND INOPERATIVE. REPAIRED WIRING IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP AFT SECTION. SYSTEM GROUND CHECKS NORMAL OPERATION. (X)