N480AA

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 77,394 hrs · 41,208 cycles

L1 DOOR PORTABLE EMER LIGHT DOES NOT TURN OFF AFTER EMER LIGHT TEST. ON & OFF SWITCH ON LIGHT ASSEMBLY HAS TO BE CYCLED. REPLACED L1 DOOR PORTABLE EMER LIGHT ASSEMBLY IAW AMM 33-53-00. TESTED OK.

Part: CASTING — CRACKED (FUSELAGE) · airframe 75,579 hrs · 40,179 cycles

MID CARGO COMPARTMENT FWD CTR DOOR STOP CASTING IS CRACKED. R & R CASTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: RIB — CRACKED (LT WING) · airframe 75,543 hrs · 40,152 cycles

LEFT WING, NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. INSTALLED REPAIR DOUBLER IAW EA 57-038352 DATED 1/28/15.

Part: RIB — CRACKED (RT WING) · airframe 75,543 hrs · 40,152 cycles

NUMBER 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. ACCOMPLISHED DOUBLER & FILLER REPAIR IAW EA 57-038347 DATED 01/28/2015.

Part: TIRE — FAILED (RT MLG) · airframe 74,445 hrs · 39,478 cycles

RIGHT HAND TIRE CAP DEPARTED ACFT ON DEPARTURE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT FLAP DENTED FROM TIRE CAP LOSS & EVIDENCE OF RT ENG COWL IMPACT & BLADE IMPACT FROM TIRE CAP LOSS. REPLACED RT INBD FLAP WEDGE AT OUTER POSITION. REPLACED NR 2 ENG ON 08/08/2014. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,379 hrs · 39,441 cycles

TAIL SLIDE EMER LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,379 hrs · 39,441 cycles

TAIL CATWALK EMER LIGHTS FAILED TEST. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: SPAR — DAMAGED (STABILIZER) · airframe 73,809 hrs · 39,101 cycles

LEFT SPAR, 8TH HOLE BELOW ZFS 52.267 DISTRESSED & OUT OF LIMITS. INSTALLED 3 REPAIR STRAPS IAW DWG SG09550005 & EA MD80-55-034937.

Part: FITTING — CRACKED (LT WING) · airframe 72,126 hrs · 38,143 cycles

LEFT HAND WING FITTING CRACKED INBOARD SIDE OF NUMBER 4 SLAT TRACK. INSTALLED DOUBLER PER EA MD80-57-031567.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,538 hrs · 37,794 cycles

INTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED INTERIOR EMERGENCY BATTERY POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,538 hrs · 37,794 cycles

EXTERIOR EMERGENCY LIGHTS FAILED TO COME ON DURING MX TEST. REPLACED EXTERIOR EMERGENCY LIGHTS POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: APU — FAILED (ZONE 200) · airframe 70,238 hrs · 37,073 cycles

ABQ INFLIGHT LAS-DFW - CREW REPORTED AUXILIARY POWER UNIT FAILED WITH RIGHT GENERATOR ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,709 hrs · 36,796 cycles

LONGERON 24 LEFT CRACKED AT STATION 200. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00, FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,709 hrs · 36,796 cycles

LONGERON 25 LEFT CRACKED AT STATION 160. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: CONTROLLER — FAILED (ANTI-SKID SYS) · airframe 68,226 hrs · 35,954 cycles

STL - CREW REPORTED WHEN GEAR WAS EXTENDED ANTISKID LIGHTS ILLUMINATED. LEFT OUTBOARD ANTISKID LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURE. FLIGHT LANDED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTISKID CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CUSP CORROSION AT FRAME STATIONS 836 TO 840 RIGHT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — GOUGED (ZONE 100) · airframe 68,158 hrs · 35,919 cycles

DENT IN FUSELAGE SKIN WITH GOUGE AT STATION 294, LONGERON 24 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-34-02.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CORROSION UNDER AFT SERVICE DOOR AFT GIRT BAR FITTIING. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CORROSION ON INTERCOSTAL STATION 1174 BETWEEN LONGERONS 29 AND 28 RIGHT. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL AT STATION 1174 LONGERON 29 TO 28 RIGHT PER AARD 51-10-00-5 AND SRM 51-30-00.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CORROSION ON SUBFLOOR AT STATIONS 190 TO 200 8 INCHES INBOARD OF FORWARD SERVICE DOOR JAMB. INSTALLED NEW DOUBLER ON SUB-FLOOR FROM STATIONS 180 TO 200, RIGHT BUTTLINES 42 TO 57 PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,158 hrs · 35,919 cycles

INTERCOSTAL CRACKED AT FLOORBEAMS CENTERLINE OF AIRCRAFT BETWEEN STATIONS 1309 AND 1287. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,158 hrs · 35,919 cycles

CABIN ABOVE AFT BULKHEAD AT STATION 1338 STIFFENER CRACKED AT TOP. INSTALLED NEW STIFFENER AND CLIP ABOVE VAULT DOOR STATION 1338 PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,158 hrs · 35,919 cycles

HEAVY CARGO/AFT- CRACK ON RIGHT CUSP, STATION 1303. INSTALLED CUSP FROM STATIONS 1250 TO 1309 RIGHT PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

RIGHT CUSP FROM STATIONS 1176 TO 1178 CORRODED. INSTALLED DOUBLER FROM STATIONS 1173 TO 1189 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CRACK IN CUSP SHEET UNDER SEAT TRACK NUMBER 6 AT STATION 218. INSTALLED CUSP SHEET FROM STATIONS 218 TO 237 RIGHT PER AARD 53-20-00-16 AND AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CORROSION ON RIGHT CUSP FROM STATIONS 532 TO 535. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

CORROSION ON CUSP UNDER FORWARD GIRT BAR FITTING, STATION 1143. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,158 hrs · 35,919 cycles

CUSP UNDER NUMBER 5 SEAT TRACK HAS DAMAGED ATTACH HOLES FROM STATIONS 237 TO 247. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (LE SLAT) · airframe 68,158 hrs · 35,919 cycles

LEFT NUMBER 5 SLAT HAS SHARP DENT IN LEADING EDGE UPPER SKIN. REWORKED DENTED AREA PER ESO 80117 TO WITHIN LIMITS. DYE CHECK AFTER REWORK SHOWS NO CRACKS.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,158 hrs · 35,919 cycles

RIGHT CUSP AT STATION 678 CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,158 hrs · 35,919 cycles

RIGHT CUSP FROM STATIONS 488 TO 490 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,847 hrs · 35,170 cycles

OVERWING EXIT WINDOW EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EXIT WINDOW EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 66,790 hrs · 35,139 cycles

LAX INFLIGHT SAN-DFW. CREW REPORTED LEFT ENGINE LOST OIL QUANTITY AND OIL PRESSURE AFTER TAKEOFF. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 23 MINS). EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT LAX ON 09/18/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,218 hrs · 33,723 cycles

STATION 1380 SKIN CRACK ABOVE PYLON. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,218 hrs · 33,723 cycles

LONGERON 2 RIGHT IS CRACKED ON OUTBOARD FLANGE AFT OF FRAME 1418. REPAIRED LONGERON PER AARD 53-30-00-2.

Part: TIRE — BLOWN (MLG) · airframe 61,345 hrs · 32,129 cycles

NUMBER 2 MAIN LANDING GEAR TIRE BLEW ON LANDING. REPLACED NUMBER 1 & 2 MAIN TIRES, CHECKS NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,258 hrs · 31,536 cycles

EMERGENCY HELD LIGHT INOPERATIVE. INSTALLED SERVICEABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR/FLIGHT ATTENDANT SEAT AREA AND PERFORMED OPERATIONAL CHECK PER MCM CARD 4289.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,213 hrs · 31,516 cycles

EMERGENCY LIGHT BATTERY PACK WEAK FORWARD DROP DOWN CEILING PANEL. REPLACED BATTERY PACK AND CHECKED PER WORK CARDS 4289 AND 4854.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,213 hrs · 31,516 cycles

SMALL CRACK AT FASTENER IN SKIN .25 INCH LONG AT STATION 1380 LONGERON 13R-14R. FABRICATED AND INSTALLED REPAIR DOUBLER PER AARD 53-30-00-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,213 hrs · 31,516 cycles

STATION 1485 CANTED FRAME WEB IS CRACKED AT UPPER HI-LOK IN THE LOUVER BOX ANGLE JUST OUTBOARD OF THE EMERGENCY LIGHT ASSEMBLY. INSTALLED DOUBLER PER AARD 53-10-00-32.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 60,082 hrs · 31,436 cycles

EWR - SLIDE PACKAGE IN FORWARD GALLEY SERVICE DOOR CAME LOOSE. SLIDE DID NOT DEPLOY. REPLACED RIGHT NUMBER 1 DOOR SLIDE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT SEAT ROW 11 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD RIGHT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 19D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT OVERHEAD LEFT SEAT ROW 19 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD LEFT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR — OPEN (NLG)

MEM INFLIGHT T1725/22APR DURING CLIMB CREW REPORTED NOSE GEAR VIBRATIONS AND GEAR DOOR LIGHT ILLUMINATED. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOOR OPEN. CLOSED DOOR AND FOUND ALL INDICATIONS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO OVERWING EMERGENCY EXIT LIGHTS ON FORWARD LEFT AND RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS ON FORWARD LEFT AND RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - OVERWING EMERGENCY EXIT LIGHTS AT AFT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERIWNG EMERGENCY EXIT LIGHTS AT AFT LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TUBE — BLOWN (LEFT ENGINE)

TPA INFLIGHT - LEFT ENGINE START VALVE ANNUNCIATOR ILLUMINATED. CREW SHUT NUMBER ONE ENGINE DOWN. NUMBER ONE ENGINE WINDMILLED APPROXIMATELY 20 MINUTES. LANDED TPA WITHOUT INCIDENT. REPLACED LEFT REAR ANTI ICE TUBE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHT AT ROW 8 OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT ROW 8 IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHT IN EXTERNAL AFT CARGO INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN EXTERNAL AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT FROM SEAT 21DEF TO 30DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 21DEF TO 30DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 30D)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR DIM. REPLACED LIGHT ASSEMBLY FOR OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — UNSECURE (BATTERY)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS ROW 7-11 INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT BATTERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS IN FIRST CLASS WILL NOT FULLY EXTINGUISH. REPAIRED EMERGENCY EXIT LIGHT BATTERY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: UPLOCK SENSOR — INOPERATIVE (NLG)

ORD - FLT 9689 - NOSE LANDING GEAR WOULD NOT RETRACT LANDED ORD WITHOUT INCIDENT. SWUNG GEAR 7-8 TIMES, COULD NOT DUPLICATE ON GROUND. NEXT DAY REPEAT CONDITION. REPLACED NOSE GEAR UP SENSOR AND LOCK SENSOR, PROXIMITY BOX, AND NOSE GEAR BUNGEE NOSE LANDING GEAR. CONDUCTED FERRY FLIGHT AND NOSE LANDING GEAR DID NOT RETRACT, INDICATOR PIN RELEASED NOSE LANDING GEAR LIGHT ON. NOISE AND VIBRATION INDICATED GEAR WAS EXTENDED OR GEAR DOORS OPEN. MADE 2 ATTEMPTS TO RETRACT. LANDED ORD WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (GALLEY DOOR)

ATL - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR SLIDE PARTIALLY DEPLOYED. REPLACED FORWARD GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER BAG — CONTAMINATED (A/C BAY)

ORD - FLT 386 - EN ROUTE ORD-LGA DURING CLIMB-OUT, DETECTED WHITE SMOKE IN COCKPIT. RETURNED TORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING AND MAIN CABIN INOPERATIVE. REPLACED JUMPER WIRE FOR EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (TAIL)

ORD - FLT 0453 - AFTER TAKEOFF ORD, SMOKE WAS DETECTED IN THE CABIN. FLIGHT ATTENDANTS NOTED SMOKE IN THE CABIN AND COCKPIT CREW EXPERIENCED SMOKE IN THE COCKPIT WITH THE SMELL OF BURNING OIL OR RUBBER. AIR CONDITIONING PACKS WERE TURNED OFF IMMEIDATELY; AFTER PACKS WERE TURNED OFF, IT APPEARED THAT NO FURTHER SMOKE WAS PRODUCED, BUT SMOKE REMAINED IN THE AIRCRAFT. AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. APU IS LEAKING OIL. REPLACED APU. ACCOMPLISHED LEFT AND RIGHT PACK BURN IAW MM. REPLACED COALESCER BAGS IAW MM. OPERATION AND LEAK CHECKS NORMAL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM AFT GALLEY DOOR TO AFT OF AIRCRAFT INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MODULE — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION DIM. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: NOSE COWL — CRACKED (LT ENG)

SAT - DURING ROUTINE MAINTENANCE, FOUND A CRACK AT THE 6 O'CLOCK POSITION ON THE LEFT ENGINE NOSE COWL. CRACK IS LOCATED 1.5 INCHES AFT OF NOSE COWL LIP SEAM AND ABOUT 3 INCHES OUTBOARD OF NOSE COWL INSPECTION PANEL. APPLIED SPEED TAPE TO DAMAGED AREA, APPROVED FOR ONE TIME FLIGHT FROM SAT TO DFW FOR NOSE COWL REPLACEMENT. FLEW FROM SAT TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE COWL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT STRIP — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP FOUND DISCONNECTED BETWEEN PAX SEAT ROWS 20 AND 21. RESECURED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)