N560AA

Part: RIB — CRACKED (LT WING) · airframe 64,101 hrs · 33,364 cycles

LT HAND WING SLAT TRACK RIB IS CRACKED AT TOP AFT LUG. INSTALLED REPAIR DOUBLER & HAT BUSHING IAW EA MD80-57-032638.

Part: RIB — CRACKED (RT WING) · airframe 64,101 hrs · 33,364 cycles

RT HAND WING SLAT TRACK RIB CRACKED AT TOP OF LUG. INSTALLED REPAIR DOUBLER & HAT BUSHING IAW EA MD80-57-032638.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 64,101 hrs · 33,364 cycles

FWD CARGO DOOR, FWD SIDE UPPER STOP PAD FITTING CRACKED. R & R STOP PAD FITTING IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 64,101 hrs · 33,364 cycles

MID CARGO DOOR, FWD SIDE THIRD STOP PAD FITTING FROM THE TOP CRACKED. R & R STOP PAD FITTING IAW AARD 51-00-05-1.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,944 hrs · 33,263 cycles

AB5-3 EGRESS POWER SUPPLY FAILS DUAL FEEDBACK CHECK. REPLACED BATTERY. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,944 hrs · 33,263 cycles

EMERGENCY LIGHTS FROM ROWS 27 TO 31 FAILED. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,924 hrs · 32,117 cycles

CRACK IN FUSELAGE TAIL SECTION LEFT SIDE AT STATION 1477. INSTALLED DOUBLER PER AARD 53-30-00-4 AND SRM 53-01-00.

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 61,707 hrs · 32,001 cycles

DFW - CREW REPORTED THE RIGHT MAIN GEAR DOOR INDICATED UNSAFE AND THE AMBER *GEAR DOOR OPEN* LIGHT REMAINED ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TAB — CRACKED (ELEVATOR) · airframe 60,938 hrs · 31,575 cycles

CRACKS AND DENTS IN OUTBOARD END OF TAB. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-0-10.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 60,743 hrs · 31,466 cycles

DFW - CREW REPORTED LEFT GENERATOR FAILED IN-FLIGHT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,169 hrs · 31,143 cycles

AFT GALLEY DOOR EXIT LIGHT INOPERATIVE. REPLACED MODULE NUMBER 1 BATTERY PACK AT AFT SERVICE DOOR. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,006 hrs · 31,046 cycles

STATION 1510 CANT FRAME CRACKED ABOVE MAINTENANCE LIGHT SWITCH. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER EA MD80-53-024052.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 59,455 hrs · 30,750 cycles

RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESET BATTERY PACK AT FORWARD OVERHEAD CEILING PANEL. OPS CHECK NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 58,271 hrs · 30,075 cycles

DFW - CREW REPORTED CENTER WINDSHIELD CRACKED DURING CRUISE. PULLED K-25 CIRCUIT BREAKER. DESCENDED TO 10,000 FT AND REDUCED PRESSURIZATION DIFFERENTIAL. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTER WINDSHIELD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TARGET — BROKEN (RT MLG) · airframe 57,958 hrs · 29,914 cycles

DEN - CREW REPORTED MAIN LANDING GEAR DOOR WARNING INDICATION. GEAR WAS MANUALLY RELEASED. EMERGENCY DECLARED FLIGHT RETURNED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT MAIN LANDING GEAR DOOR SENSOR TARGET BROKEN. REPLACED GEAR DOOR UP AND LOCKED TARGET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

DAMAGE TO I BEAM STATION 1160. REPLACED I BEAM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

INTERCOSTAL IN CARGO CEILING STATIONS 1271 TO 1287 BUTTLINE-0 IS CRACKED AT FASTENER HOLES. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

SHEAR TIE STATION 180 DAMAGED. INSTALLED SHEAR TIE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

LEFT AFT TIE DOWN TRACK HAS CORROSION SEVERAL PLACES ALONG THE LENGTH APPROXIMATE STATIONS 1220 TP 1322. REMOVED AND REPLACED DAMAGED TRACK PER SRM 51-30-05 AND 51-30-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

DENT IN FUSELAGE AT STATION 329 BELOW LONGERON 27 RIGHT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

FUSELAGE SKIN DENTED WITH A CREASE AT FRAME STATIONS 313 TO 332, BETWEEN LONGERON 27 TO 28 RIGHT. REMOVED DAMAGED SECTION OF SKIN, INSTALLED DOUBLER REPAIR PER SRM 53-04-00 FIGURE 12B.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

RIGHT CUSP CRACKED STATION 1300, LIGHTNING HOLE TO LIGHTNING HOLE. INSTALLED RIGHT CUSP AT STATIONS 1250 TO 1309 PER AARD 51-10-00-5 REPAIR 1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

AFT CARGO - CORROSION ON THE LEFT TIE DOWN TRACK UPPER AND LOWER SIDES BETWEEN BETWEEN STATIONS 1212 AND 1231. REMOVED AND REPLACED DAMAGED SPLICE PLATES PER SRM 51-30-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

TOOL DAMAGE ON CUSP UNDER NUMBER 1 SEAT TRACK STATION 824. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5 REPAIR 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

RIGHT CUSP SHEET STATIONS 598 TO 712 CORRODED. REMOVED AND REPLACED CUSP PER AARD 53-20-00-16.

Part: HINGE BRACKET — CORRODED (CARGO BAY) · airframe 56,772 hrs · 29,265 cycles

AFT CARGO DOOR CUTOUT-FORWARD HINGE BRACKET CORRODED. REMOVED AFT CARGO DOOR- FORWARD HINGE BRACKET ON THE AIRCRAFT. INSTALLED NEW HINGE BRACKET PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

CORROSION AT LEFT AFT SERVICE DOOR-UNDER AFT GIRT BAR BRACKET. REMOVED CORRODED CUSP SECTION, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

FRAME 1418 CRACKED ON AFT SIDE AT LONGERON 2 LEFT. STOP-DRILLED CRACK INSTALLED DOUBLER REPAIR PER SRM 53-10-00-15.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

AFT CARGO DOOR CUT OUT LOWER BEAM, CORROSION REMOVAL BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

RIGHT CUSP CORRODED STATIONS 1174 TO 1250. REPLACED CUSP SHEET PER SRM 51-30-01 AND SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

LEFT CUSP, STATIONS 1098 TO 1103 HAS CORROSION THAT IS OUT OF LIMITS. INSTALLED DOUBLER AND SPACER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

LEFT CUSP, STATIONS 712 TO 731 CORROSION OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 56,772 hrs · 29,265 cycles

RIGHT WING GROUND SPOILER FITTING CRACK IN OUTBOARD SIDE OF CASTING TRAILING EDGE OF WING. INSTALLED NEW SPOILER ATTACH FITTING PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

CORROSION UNDER AFT GIRT BAR BRACKET AT STATION 1166. INSTALLED .040" 6AL-4V TITANIUM REPAIR DOUBLER STATION 1166 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

LEFT CUSP STATIONS 1098 TO 1103 HAS CORROSION THAT IS OUT OF LIMITS. INSTALLED DOUBLER AND SPACER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

AFT CARGO - DOOR FRAME UPPER BOX TOP SIDE HAS CORROSION AT THE UPPER FORWARD END JUST FORWARD OF THE FORWARD HINGE MOUNT APPROXIMATELY STATION 1160. REMOVED AND REPLACED BEAM PER AARD 51-10-00-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

CORROSION UNDER FORWARD GIRT BAR BRACKET AT STATION 1140. INSTALLED .040" 6AL-4V TITANIUM REPAIR DOUBLER STATION 1140 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

LEFT CUSP STATIONS 636 TO 655 HAS CORROSION THAT IS OUT OF LIMITS. CUT OUT DAMAGE PER AARD 53-20-00-16 AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

NUMBER 1 GALLEY TIE DOWN FITTING CORRODED. REPLACED TIE DOWN FITTING PER 51-30-05.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

AFT VAULT DOOR JAMB, DOOR STOP CRACKED, LEFT SIDE MIDDLE STOP. REMOVED CRACKED FITTING, DRILLED UP NEW FITTING AND INSTALLED PER AARD 51-10-00-3.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 56,772 hrs · 29,265 cycles

SUBFLOOR HAS PUNCTURE AT STATION 198 FORWARD OF NUMBER 3 SEAT TRACK. REMOVED DAMAGE INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: PAN — DAMAGED (WINDOW) · airframe 56,772 hrs · 29,265 cycles

STATION 1098 UPPER AFT WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

CORROSION ON NUMBER 2 GALLEY TIE DOWN FITTING AT STATION 208 INBOARD OF NUMBER 4 SEAT TRACK. (MKD) INSTALLED NEW SERVICEABLE G-2 GALLEY TIE DOWN SUPPORT FITTING AT STATION 208 PER AARD 51-10-00-5.

Part: PAN — DAMAGED (WINDOW) · airframe 56,772 hrs · 29,265 cycles

STATION 946 LOWER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,772 hrs · 29,265 cycles

STATION 1060 LOWER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,772 hrs · 29,265 cycles

STATION 946 UPPER FORWARD WINDOW PAN CRACKED LEFT. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,772 hrs · 29,265 cycles

CORROSION ON NUMBER 2 GALLEY TIE DOWN FITTING AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. (MKD) INSTALLED NEW SERVICEABLE G-2 GALLEY TIE DOWN SUPPORT FITTING AT STATION 218 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,977 hrs · 27,114 cycles

RIGHT CUSP HAS CORROSION STATIONS 200-205. DAMAGED MATERIAL REMOVED, REPAIR DOUBLER INSTALLED PER EA MD-80-53-006501 AND AARD 53-20-00-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,975 hrs · 27,113 cycles

THE 1418 FRAME CRACKED LONGERON 2 LEFT AND 2 RIGHT. INSTALLED DOUBLER PER EA MD80-53-006493.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,067 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GUARD — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 17D LENS GUARD DAMAGED. REPLACED LENS GUARD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT AT AFT FORWARD POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (LT A/C PACK)

BUR - DURING DESCENT BOTH PACKS SHUTDOWN. PRIOR TO LEFT PACK RETURNING THE PASSENGER OXYGEN MASKS DEPLOYED. LANDED BUR WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED BOTH AIRCONDITIONING WATER SEPARATOR ASSEMBLIES. REPLACED LEFT AND RIGHT PACK ANTI-ICE VALVES. REPLACED RIGHT PACK PRESSURE REGULATOR OVER-RIDE VALVE S2-40. REPLACED BOTH CABIN DIFFERENTIAL PRESSURE SWITCHES S1-485 & 486 AND REPAIRED CHAFFED WIRE AT SINGLE ENGINE SECOND SEGMENT CLIMB PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — UNKNOWN (NLG)

NOSE GEAR WOULD NOT RETRACT. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT PER PATTERN CARD 4753. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

SFO - OVERHEAD EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT SEAT AND ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACKS AT B5 27 AND B5 102 FOR OVERHEAD EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT SEAT AND ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHTS AT TAIL COMPARTMENT SIDEWALL INOPERATIVE. REPLACED AFT VETICAL EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

BOS - EMERGENCY LIGHT AT FORWARD LEFT NUMBER 1 DOOR AND AISLE WAY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD LEFT NUMBER 1 DOOR AND AISLE WAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - FORWARD EMERGENCY ESCAPE PATH LIGHTING AND FORWARD EXIT SIGN AT LEFT ONE DOOR AND FORWARD GALLEY DOOR INOPERATIVE. REPLACED BATTERY PACK ON AB51 CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7DEF INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OIL SYSTEM — LEAKING (APU)

DFW - FLT 530 - DFW-RIC, ON CLIMB-OUT ABOVE 1000 FEET HAD BURNING SMELL IN THE COCKPIT WITH MODERATE SMOKE THROUGHOUT THE CABIN. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. INSPECTED ACM/PACK HEAT EXCHANGER DUCTING. NO DEFECTS NOTED. INSPECTED APU, FOUND OIL PRESENT IN THE APU PLENUM. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: REGULATOR VALVE — STICKING (A/C BAY)

DFW - FLT 1145 - EN ROUTE DFW-SFO, AIRCRAFT ON CLIMB-OUT, EMITTED SMOKE AND FUMES FROM AIRCRAFT GASPERS THROUGHOUT THE PLANE. SMOKE STOPPED AFTER APPROXIMATELY 5 MINUTES. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT AIR CONDITIONING PRESSURE REGULATOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL LINE — CRACKED (FUEL SYSTEM)

TUL - FOUND FUEL LINE CRACKS WHERE THE FUEL LINE CONTACTS THE UPPER WING STRUCTURE PANEL NUMBER 1409C, OUTBOARD OF STATION XCW 121.688. FUEL LINE WAS REPAIRED BY INSTALLING A DOUBLER AND ADJUSTING THE CLAMPS THAT HOLD THE LINE SO THAT IT HAS CLEARANCE AFTER INSTALLATION SHOP ESO FOR FUEL LINE REPAIR. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SHALLOW DENT ON FUSELAGE, STATION 316 BETWEEN L22L AND 23L. INSTALLED DOUBLER PER SRM 53-04, FIG 38. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DENT WITH 3 INCH GOUGE IN SKIN AT STATION 300, BETWEEN L20R AND L21R. INSTALLED INTERNAL DOUBLER AT STATION 300 BETWEEN LONGERON 20R AND L21R PER SRM 53-04, FIG 38 VIEW I. (M)

Part: WIRE — DAMAGED (CABIN)

PHL - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED WIRES ON BATTERY SUPPLY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

SAN - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT 8DEF INOPERATIVE. RE-SECURED EMERGENCY EXIT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CIRCUIT BREAKER — TRIPPED (TE FLAPS)

DFW - FLT 1392 - AFTER TAKEOFF AT ELP RIGHT FLPS STUCK AT 5 DEGREES WITH SLIGHT ROLL TO THE LEFT. ALSO HAD STALL FAILURE LIGHT. TESTED STALL SYSTEM AND RIGHT STALL SYSTEM WOULD NOT TEST. PULLED CIRCUIT BREAKER FOR RIGHT STALL SYSTEM AS PER CHECKLIST. FOUND C/B L9 RIGHT INSTRUMENT TRANSFORMER CIRCUIT BREAKER TRIPPED. AFTER CIRCUIT BREAKER REINSTATED SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (TAIL BAY)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT RAMP SIDEWALL EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE ON TAIL COMPARTMENT RAMP SIDEWALL EMERGENCY EXIT LIGHT, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS FORWARD OF FIRST CLASS INOPERATIVE. REPAIRED WIRE FOR EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS FORWARD OF FIRST CLASS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (SEAT 31)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 31 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 31. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (ROW 9D)

DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, MID CABIN FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS AT EXIT STICKERS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WATER HEATER — DEFECTIVE (FWD LAVATORY)

DFW - FLT 570 - EN ROUTE COS/DFW - DURING CRUISE, LOUD POP HEARD FROM FORWARD LAVATORY FOLLOWED BY SMOKE SMELL WHICH DISSIPATED QUICKLY. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. PLACARDED FORWARD LAVATORY HOT WATER HEATER INOPERATIVE. SUBSEQUENTLY REPLACED FORWARD LAVATORY HOT WATER HEATER AND CONNECTOR AT PHX/28 AND REMOVED PLACARD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (COCKPIT)

DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT OPERATION INTERMITTENT DURING TEST. REPLACED EMERGENCY FLOOR LIGHT COCKPIT OVERHEAD SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONDUCTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD END OF MAIN CABIN INOPERATIVE. REPLACED BROKEN/SHORTED FLAT CONDUCTOR WIRE BETWEEN FIRST CLASS CABIN AND MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)