N575AM

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,163 hrs · 34,429 cycles

FOUND ONE INCH FUSELAGE CRACK ON THE LT SIDE AT STATION 1474, NEAR THE TAIL CONE JETTISON HANDLE. ACCOMPLISHED A SHEETMETAL REPAIR WITH A DOUBLER PATCH IAW SRM 53-01-00.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 64,707 hrs · 33,602 cycles

UPPER SIDE OF THE GEAR DOOR ACTUATOR, THE GREEN SHELF BRACKET IS CRACKED AT THE AFT INBD RADIUS. INSTALLED DOUBLER & SHIM IAW AARD 53-10-00-38.

Part: RIB — CRACKED (RT WING) · airframe 64,707 hrs · 33,602 cycles

RT HAND WING LE CRACKED IN INBD NR 4 SLAT TRACK FITTING AT AFT UPPER CABLE BRACKET LUG. INSTALLED DOUBLER IAW CARD 57-98-06 & EA MD80-57-033572.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,707 hrs · 33,602 cycles

CRACK AT STATION 1418 & LONGERON 2 LT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,125 hrs · 33,286 cycles

EMERGENCY EXIT SIGNS WERE AT ROW 21 BOTH SIDES INOPERATIVE. REPLACED BATTERY PACKS FOR EXIT SIGNS. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,960 hrs · 33,198 cycles

TAIL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 62,810 hrs · 32,511 cycles

LEFT NR 1 DOOR PORTABLE EMERGENCY LIGHT VERY DIM. REPLACED LT NR 1 DOOR PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL

Part: WIRE — PULLED (CABIN) · airframe 62,810 hrs · 32,511 cycles

FORWARD AND AFT ESCAPE PATH LIGHTING AT SEAT 19D INOPERATIVE. WIRES PULLED FROM CONNECTOR. RECONNECTED WIRES AT SEAT 19D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 62,810 hrs · 32,511 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL

Part: CHECK VALVE — DEFECTIVE (AC BAY) · airframe 58,588 hrs · 30,124 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AIR CHECK VALVE THAT WAS DEFECTIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — CRACKED (CABIN) · airframe 58,049 hrs · 29,815 cycles

EMERGENCY LIGHT LENS SHROUD AT ROW 10D CRACKED. REPLACED EMERGENCY LIGHT LENS SHROUD AT ROWS 10D AND 12D. OPS CHECK NORMAL.

Part: LENS — CRACKED (CABIN) · airframe 58,049 hrs · 29,815 cycles

EMERGENCY LIGHT LENS SHROUD CRACKED AT ROW 12D. REPLACED LENS SHROUD FOR EMERGENCY LIGHT AT ROW 12D. OPS CHECK NORMAL.

Part: SPRING — BROKEN (ZONE 500) · airframe 57,420 hrs · 29,463 cycles

CREW REPORTED LEFT ENGINE LOST THRUST POWER. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT FUEL SHUT-OFF LEVER SPRING BROKEN. REPLACED SPRING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

FUSELAGE DENTED STATION 236 LONGERONS 16 AND 17. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

DENT IN FUSELAGE STATION 58.75 LONGERON 18 RIGHT. INSTALLED DOUBLER PER SRM 53-04-03.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION IN G1 GALLEY OUTBOARD FLOOR MOUNT STATION 160. REMOVED OLD CENTER FLOOR G1 GALLEY MOUNT AND REPLACED PER AARD 51-10-00-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION IN CUSP TEE STATIONS 265 TO 168. INSTALLED NEW CUSP TEE PER SRM 53-05-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

SHEAR TIE STATION 1307 LONGERONS 19 TO 26 LEFT CORRODED BEYOND LIMITS. INSTALLED SHEAR TIE PER SRM 51-30-05 AND 51-30-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

LEFT CUSP CRACKED AT LIGHTNING HOLE STATION 316. INSTALLED REPAIR DOUBLER AT LEFT CUSP STATION 316 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION OUT OF LIMITS RIGHT CUSP STATION 540. INSTALLED DOUBLER AT RIGHT CUSP STATION 540 PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION IN SUBFLOOR DIAPHRAGM RIGHT SIDE FORWARD OF FIBER GLASS HAT CHANNEL STATION 166. INSTALLED REPAIR DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 44 TO 57 PER AARD 53-20-00-16 AND FACTOR DOUBLER AT STATIONS 160 TO 180 RIGHT BUTTLINES 45 TO 57 PER AARD 51-10-00-5.

Part: DIAPHRAGM — GOUGED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

GOUGE IN SUB-FLOOR DIAPHRAGM APPROXIMATELY 22 INCHES LEFT OF CENTER LINE STATION 198. INSTALLED REPAIR DOUBLER REF AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

CRACK IN LONGERON 2 LEFT STATION 160. INSTALLED LONGERON 2 LEFT AND SPLICE STATION 148 TO 180 SRM 53-02-00 FIGURE 18.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION IN SUBFLOOR DIAPHRAGM STATION 180 APPROXIMATELY 14 INCHES INBOARD OF FORWARD SERVICE DOOR CUTOUT. INSTALLED REPAIR DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 44 TO 57 PER AARD 53-20-00-16 AND FACTOR DOUBLER AT STATIONS 160 TO 180 RIGHT BUTTLINES 45 TO 57 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION IN CUSP TEE RIGHT SIDE STATION 208 SEEN THROUGH WEB HOLE. INSTALLED NEW RIGHT CUSP ANGLE FROM STATIONS 185 TO 228 PER SRM 53-05-00 FIGURE 55 AND INSTALLED REPAIR SPLICE ANGLES AT STATION 185 PER SRM 53-05-00 FIGURE 55.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CORROSION ON LEFT CUSP STATIONS 990 TO 1000. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

RIGHT CUSP SHEET STATIONS 218 TO 237 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

CORROSION IN SUBFLOOR DIAPHRAGM RIGHT SIDE BETWEEN 5 AND 6 SEAT TRACK STATION 200. INSTALLED CUSP REPAIR PER AARD 53-20-00-16.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

CORROSION ON AFT CARGO DOOR BEAM STATIONS 1167 TO 1212. INSTALLED FULL LENGTH DOOR BEAM REPAIR DOUBLER PER AARD 53-10-00-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

FUSELAGE SKIN CRACKED BEYOND STOP DRILL AT NOSE GEAR RIGHT AFT DOOR, AFT HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05-00 FIGURE 62 AND EA MD80-015952.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

THREE EACH CRACKS FOUND AT ATTACHMENT HOLES, ENDS MARKED. ONE CRACK IS APPROXIMATELY 1.5 INCHES LONG ANTENNA POSITION STATION 402. INSTALLED DOUBLER PER EA MD80-53-015958, SRM 53-04 FIGURE 12B AND DRAWING SG09530002.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

LEFT CUSP CRACKED AT STATION 218. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

CARGO AFT CORROSION FRAME 1271 AFT SIDE LONGERON 29 RIGHT TO LONGERON 28 LEFT. INSTALLED NEW "J" ANGLE REPAIR DOUBLER PER AARD 53-10-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,386 cycles

LEFT CUSP SHEET OUT OF LIMITS AT STATIONS 1174 TO 1250. INSTALLED NEW CUSP FROM STATIONS 1174 TO 1250 ON LEFT SIDE PER AARD 51-10-00-5 AND EA MD80-51-015900 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

SKIN BULGED AND SHAVED AT PREVIOUS STATIC BURN REPAIR (NACA RIVET) STATION 254 LONGERON 25 RIGHT. INSTALLED DOUBLER PER BOEING DRAWING SG09530001, SRM53-04-02, SRM 51-30-05 AND SRM 51-10-4.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

CARGO AFT CORROSION FRAME 1271 AFT SIDE LONGERON 29 RIGHT TO LONGERON 28 LEFT. INSTALL NEW "J" ANGLE PER AARD 53-10-00-14.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

FLOORBEAM DAMAGED FROM CARGO DOOR AT STATION 389 RIGHT OF CENTER. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-21.

Part: TRACK — CORRODED (FUSELAGE) · airframe 57,290 hrs · 29,386 cycles

CORROSION RIGHT TIE-DOWN TRACK STATIONS 1212 TO 1271 AT MOUNT SCREWS AND TABS. INSTALLED NEW TIE DOWN TRACK PER AARD 51-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,386 cycles

CRACKED WINDOW PAN STATIONS 1079 TO 1089 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 56,672 hrs · 29,039 cycles

SEAT 4E EGRESS LIGHT INOPERATIVE. RE-SEATED SEAT CONNECTOR FOR 4E EGRESS LIGHT. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,753 hrs · 27,400 cycles

FRAME 1418 CRACKED AT LONGERON 2 LEFT. REPAIRED FRAME PER 53-03 FIG 31A WITH DEVIATIONS PER EA MD80-53-008121.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 51,478 hrs

LGA- LEFT EMERGENCY LIGHT AT ROW 19 INOPERATIVE. SECURED CONNECTOR FOR LEFT EMERGENCY LIGHT AT ROW 19

Part: LENS — MISSING (CABIN) · airframe 49,469 hrs

ORD EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG) · airframe 48,750 hrs

ORD INFLIGHT T1145/02FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER NOSE GEAR RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPACKED NOSE STRUT ASSEMBLY AND REPLACED METERING PIN SEALS AND LOWER TURNING TUBE BEARING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHTS AT SEAT ROWS 3DEF TO 20DEF INOPERATIVE. REPAIRED HARNESS AT SEAT ROWS 19DEF AND 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS FROM SEAT ROWS 13 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM SEAT ROWS 13 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: LIGHT — BROKEN (SEAT 7D)

DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 7D IS BROKEN. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY FOR SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 24D)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 24D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (RIGHT)

FLT 1237 - MCO-STL, UPON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLS AND VIBRATIONS. RETURNED MCO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL CONE AREA INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTOR ON BOTTOM CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE)

LAX - FLT 237 - EN ROUTE LAX-SJD, DURING CLIMB-OUT, LEFT START VALVE OPEN LIGHT ILLUMINATED. CREW PREPARED TO SHUT DOWN ENGINE WHEN LEFT ENGINE FLAMED OUT. RETURNED LAX AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL AND ENGINE FUEL PUMP. ACCOMPLISHED ENGINE RUN AND POWER ASSURANCE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WEB — CRACKED (FUSELAGE)

TUL - TWO CRACK FOUND IN LEFT CUSP STATION 1261. STOP DRILLED CRACKS INSTALLED DOUBLER PER SRM 53-05-00. (M)

Part: DOOR — CORRODED (LAV SERVICE)

TUL - AFT LAV ACCESS DOOR FLANGE HAS CORROSION AT INBOARD SIDE OF FLANGE AT AFT LOWER CORNER, FS 1309-1322. REPAIRED PER ESO 80559 DATED 12/5/02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP MEMBRANE BETWEEN STATION 655 TO 636 OUTBOARD OF NR 6 SEAT TRACK. REMOVED AND REPLACED CUSP MEMBRANE BETWEEN STATION 598 TO 712 PER DRAWING FDK5972. REINSTALLED SEAT TRACK NR 6 FROM STATION 560 TO 788. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW ATTACH FRAME CRACKED AT RIVET LEFT SIDE STATION 1022 UPPER LEFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK AT FASTENER HOLE STRINGER 14L STATION 1401 ABOVE NR 1 ENGINE PYLON. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 APPROX 4 INCHES BY 5 INCHES EXTERNAL PATCH DOUBLER. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK AT FS 218. INSTALLED SEAT TRACK AND SPLICE REPAIR STATION 207-260 RIGHT, IAW SRM 53-05-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP CORRODED UNDER AFT GIRT BAR FITTING SUPPORT ANGLE AT AFT SERVICE DOOR. INSTALLED DOUBLER IN CUSP UNDER AFT GIRT BAR FITTING SUPPORT ANGLE PER SRM 53-00-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND TRACK CORRODED BEYOND LIMITS UNDER GALLEY ATTACH POINTS, FS 1174-1320. SEAT TRACK REPLACED PER AMM 53-40-00-2. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN AIRCRAFT SKIN, L10L AT CANT STATION 1510. INSTALLED DOUBLER PER SRM 53-01-00. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN SKIN L10L CANT 1497. INSTALLED DOUBLER PER SRM 53-10-00. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP STATION 598 RIGHT. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL INOPERATIVE. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROW 7 THROUGH 10 INOPERATIVE. ADJUSTED OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CATWALK)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT CATWALK INOPERATIVE. TIGHTENED WIRE ON EMERGENCY EXIT LIGHT AT CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (AFT STAIR)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR FORWARD EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: ENGINE — BIRD STRIKE (LEFT)

DFW - FLT 459 - ON DEPARTURE AIRCRAFT SUSTAINED BIRD STRIKE WHICH APPEARED TO BE INGESTED INTO LEFT ENGINE. RETURNED AND LANDED DFW WITHOUT INCIDENT. ENGINE BOROSCOPED AND INSPECTED FOR BIRD STRIKE. NO DAMAGE NOTED. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: VALVE — FAILED (FUSELAGE)

LGA - FLT 1911 - ON CLIMB-OUT WITH POWER IN CLIMB AND WING AND ENGINE ANTI-ICE SELECTED THE AIRFOIL ICE PROTECTION, ABNORMAL LIGHT ILLUMINATED WITH LEFT/RIGHT ICE PROTECTION LOW AND LEFT AIRCRAFT SUPPLY TEMPERATURE HIGH LIGHTS ILLUMINATED. ACCOMPLISHED PROCEDURE FOR AIRCRAFT SUPPLY HIGH LIGHT AND THIS LIGHT WENT OUT. ICE PROTECTION LIGHTS WENT OUT BUT AIRFOIL ICE PROTECTION ABNORMAL LIGHT EXTINGUISHED. REPLACED WING ANTI-ICE VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — FAILED (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING IN TAIL COMPARTMENT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (BS 1260)

TUL - FOUND SEAT TRACK NR 2 HAS CORROSION ON FLOORBOARD OUTBOARD LANDING STATION 1260. BLENDED AREA, REMOVED CORROSION AND INSTALLED STRAP PER AARD 53-20-00-13 PAGE 1-2. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN FIRST CLASS AND COACH CABIN WERE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT JUMPER STRIP BETWEEN FIRST CLASS AND COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT STAIR)

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

Part: WIRE — OUT OF POSITION (AFT FUSELAGE)

OMA - FLT 1501 - EN ROUTE ORD-DEN - DURING CRUISE, RIGHT AC GENERATOR TRIPPED WITH CROSSTIE LOCKOUT AND MULTIPLE ELECTRICAL ANNUNCIATOR LIGHTS. VOLTAGE AND FREQUENCIES CHECKED GOOD. RESET AC GENERATOR AND TRIPPED AGAIN. STARTED APU AND PLACED APU GENERATOR ON-LINE AND APU GENERATOR TRIPPED. AIRCRAFT DIVERTED TO OMA AND LANDED WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRY OMA/TUL, CORRECTED WIRES H736D8B AND H738D8A FOUND CONNECTED TO INCORRECT TRANSFORMERS. ACCOMPLISHED GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — OUT OF POSITION (AFT FUSELAGE)

OMA - FLT 1501 - EN ROUTE ORD-DEN - DURING CRUISE, RIGHT AC GENERATOR TRIPPED WITH CROSSTIE LOCKOUT AND MULTIPLE ELECTRICAL ANNUNCIATOR LIGHTS. VOLTAGE AND FREQUENCIES CHECKED GOOD. RESET AC GENERATOR AND TRIPPED AGAIN. STARTED APU AND PLACED APU GENERATOR ON-LINE AND APU GENERATOR TRIPPED. AIRCRAFT DIVERTED TO OMA AND LANDED WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRY OMA/TUL, CORRECTED WIRES H736D8B AND H738D8A FOUND CONNECTED TO INCORRECT TRANSFORMERS. ACCOMPLISHED GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. REFERENCE NR AALA951638.