N258AA

Part: LONGERON — CRACKED (BS 1003 S20L) · airframe 73,488 hrs · 39,296 cycles

LONGERON 20 LEFT AT STATION 1003 IS CRACKED AFT OF WHEEL WELL. INSTALLED DOUBLER PER AARD 53-10-00-18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,488 hrs · 39,296 cycles

LONGERON 20 RIGHT AT STATION 1003 IS CRACKED AFT OF WHEEL WELL. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-18.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,347 hrs · 39,216 cycles

EMERGENCY EXIT LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK.

Part: WIRE — BROKEN (NR 1 ENGINE) · airframe 72,224 hrs · 38,586 cycles

DFW - LEFT ENGINE SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMPERATURE. SINGLE ENGINE TIME 29 MINUTES. EMERGENCY DECLARED RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BROKEN WIRE TO LEFT ENGINE TEMPERATURE LAMP AND LOOSE PNEUMATIC LINES. REPAIRED WIRE TO NUMBER ONE ENGINE TEMPERATURE LAMP AND LOOSE PNEUMATIC LINES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS) · airframe 68,839 hrs

DFW - EMERGENCY LIGHT AT SEAT 12D HAS SHROUD MISSING. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 68,504 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT GALLEY CHARGE LIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DAMAGED (L1 DOOR)

RDU - EMERGENCY EVACUATION SLIDE AT LEFT NUMBER ONE DOOR HAD INFLATION CABLE PULLED FROM PINS. REPLACED EMERGENCY EVACUATION SLIDE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LGA - AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 20 INOPERATIVE. RESEATED PUSH BACK PIN IN CONNECTOR FOR AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LGA - AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 28 INOPERATIVE. RESET PUSH BACK PIN IN CONNECTOR FOR AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHX - EMERGENCY EXIT SIGN LIGHT AT STATION 909 RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT STATION 909 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL CABLE — FRAYED (TAIL CONE)

TUL - DURING SCHEDULED MAINTENANCE, FOUND TAIL CONE JETTISON HOIST CONTROL CABLE FRAYED. REPLACED TAIL CONE JETTISON HOIST CONTROL CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — LACK OF LUBE

ORD - INFLIGHT AFTER TAKEOFF NOSE WHEEL WOULD NOT RETRACT. PERFORMED FULL NOSE STRUT SERVICE AND LUBED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINK — INOPERATIVE (NLG DOOR)

LGA - UPON GEAR RETRACTION SEVERE VIBRATION FELT IN NOSE OF AIRCRAFT. CONTINUED THROUGH FLIGHT. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR DOOR FOUND OPEN ON ARRIVAL. REPLACED FAULTY LINK ON LEFT HAND NOSE GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 9D AND 18D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 9D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHX - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — SHUTDOWN (LEFT)

DURING CRUISE WITH NO WARNING CREW HEARD A BOOM & LT ENGINE STARTED TO ROLL BACK ACCOMPANIED BY SEVERE VIBRATION & SMOKE IN COCKPIT & CABIN. SMOKE DISSIPATED RAPIDLY, SEVERE VIBRATION CONTINUED TO LANDING, ENGINE CONTINUED TO ROTATE. LANDED WITHOUT INCIDENT. FIRE PERSONNEL REPORTED A LARGE FUEL LEAK. BOTH FIRE HANDLE AND ENGINE FUEL WERE OFF. LEAK STOPPED AFTER APPROX 20 MIN. VISUAL INSPECTION ON GROUND INDICATED MAJOR DAMAGE TO COMPRESSOR BLADES. ENGINE TIME APPROX 12 MINUTES. REPLACED LT ENGINE. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING PER MAINTENANCE MANUAL WORKCARD 21-92-12. REMOVED AND REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 5E INOPERATIVE. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT ARM INDICATOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

STL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR UNDER SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND LEFT CUSP CRACKED. REPAIRED CRACKED CUSP, STOP DRILLED AND DOUBLER PER SRM 53-01 FIG 4. (M)

Part: STRAP — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN FRAME STRAP STATION 1147 ABOVE L28R. INSTALLED NEW STRAP PER SRM 53-01-00. (M)

Part: PAN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FORWARD CX PAN STATION 370 TO 427. REMOVED AND REPLACED PAN PER SRM 53-05 FIG NR 44. (M)

Part: BATTERY PACK — INOPERATIVE (AFT ASSY)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE LOWER EMERGENCY ESCAPE SLIDE LIGHT AND EMERGENCY ESCAPE LIGHTS ABOVE AFT FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RETRACT MECH — MALFUNCTIONED (MLG)

TUL - DURING AIRCRAFT 'RCF' AFTER HEAVY C-CHECK, THE MAIN LANDING GEAR EMERGENCY EXTENSION SYSTEM WAS ACTUATED BUT DID NOT OPERATE PROPERLY. MAIN LANDING GEAR DID NOT EXTEND, COULD NOT RELEASE MECHANISM. CHECK AND RE-RIGGED EMERGENCY EXTEND CABLES. PERFORMED GEAR SWING WITH EMPHASIS ON EMERGENCY EXTEND SYSTEM. (M)

Part: ANGLE — CRACKED (BS 1474)

TUL - VERTICAL TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED AT STATION 1474. INSTALLED DOUBLER ON LEFT ATTACH ANGLE VERTICAL TO FUSELAGE PER AARD 53-10-00-2. (M)

Part: BELL FRAME — CORRODED (BS 1271)

TUL - BELL FRAME CORRODED AT STA 1271, LONGERON 30. INSTALLED DOUBLER ON ANGLE PER MD80 AARD 53-10-00-17. TST: 37,496.23 HOURS. CYCLES, 21,140. (X)

Part: FLOOR CUSP — CORRODED (FS 179-200)

TUL - FOUND CORROSION ON FLOOR CUSP INSIDE FORWARD RIGHT SERVICE DOOR BETWEEN STATION 179 TO STATION 200. INSTALLED NEW SECTION OF CUSP AND DOUBLER PER SRM 51-01 FIG 2. (M)

Part: FLOOR CUSP — CORRODED (BS 167-179)

TUL - FOUND CORROSION ON FLOOR CUSP INSIDE FORWARD RIGHT SERVICE DOOR BETWEEN STATION 167 TO 179. INSTALLED NEW SECTION OF CUSP AND DOUBLER PER SRM 53-01 FIG 2. (M)

Part: ANGLE — CORRODED (BS 1212)

TULE - FOUND CORROSION ON FLOOR BOARD ATTACH ANGLE FRAME STATION 1212, LONGERON 28L TO LONGERON 29R. REPLACED WITH NEW ANGLE. (M)

Part: SKIN — DAMAGED (BS 1271)

TULE - FOUND TEMPORARY DOUBLER INSTALLED AT STATION 1271 LONGERON 28L. INSTALLED FLASH REPAIR AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND ESO NR 80559 DATED 1-18-96. (M)

Part: GUSSET — CORRODED (BS 1212)

TUL - FOUND CORROSION ON GUSSET AT DOOR JAMB STATION 1212. REPLACED GUSSET (SUPPORT) AT AFT CORNER OF DOOR JAMB STATION 1212. (M)

Part: CARGO TRACK — CORRODED (BS 1007-1231)

TUL - FOUND LEFT TIEDOWN TRACK CORRODED FROM STATION 1079 TO STATION 1212 WHERE IT MOUNTS TO BELL FRAMES. INSTALLED NEW TIEDOWN TRACK. (M)

Part: LONGERON — CORRODED (BS 1212-1231)

TUL - FOUND CORROSION STATION 1212 TO STATION 1231 LONGERON 26R AND LONGERON END FITTING. INSTALLED LONGERON SECTION AND SPLICED PER ESO 80559 DATED 1-18-96. (M)

Part: ANGLE — CORRODED (BS 1155-1212)

TUL - FOUND FLOOR BOARD ATTACH ANGLE CORRODED, STATION 1155 - STATION 1212. INSTALLED NEW FLOOR BOARD ATTACH ANGLE, STATION 1136 - 1212. (M)

Part: SEAT TRACK — CORRODED (BS 256-797)

TULE - FOUND CORROSION AT SEAT TRACK NR 6, STATION 256 TO STATION 797. REMOVED AND REPLACED SEAT TRACK NR 6 BETWEEN STATION 256 AND STATION 797. (M)

Part: GUSSETT — CORRODED (BS 1155)

TUL - FOUND CORROSION ON GUSSET AT FORWARD CORNER OF DOOR JAMB STATION 1155. REPLACED GUSSET (SUPPORT) AT FORWARD CORNER OF DOOR JAMB STATION 1155. (M)

Part: ANGLE — CORRODED (BS 190)

TULE - FOUND CORROSION UNDER SCUFF PLATE OF FORWARD SERVICE DOOR OF CUSP ANGLE BEYOND REPAIR LIMITS. INSTALLED DOOR JAMB PAN AND CUSP REPAIR PER SRM 53-05 FIG 55 PG 139-145 REFER TO E58 1484568. (M)

Part: CARGO TRACK — CORRODED (BS 1022-1155)

TULE - FOUND RIGHT TIEDOWN TRACK CORRODED AT EACH MOUNT SCREW HEAD. REMOVED CORRODED RIGHT TIEDOWN TRACK AND INSTALLED NEW TRACK FROM STATION 1022-1155. (M)

Part: INTERCOSTAL — CORRODED (BS 1184)

TULE - FOUND INTERCOSTAL CORROSION BEYOND REPAIR LIMITS BELOW AFT CARGO DOOR SILL. REPLACED INTERCOSTAL AT STATION 1184 OF DOOR JAMB UNDER PLATE. (M)

Part: INTERCOSTAL — CORRODED (BS 1193)

TULE - INTERCOSTAL CORROSION BEYOND REPAIR LIMITS BELOW AFT CARGO DOOR SILL. REPLACED INTERCOSTAL AT STATION 1193 OF DOOR JAMB UNDR PLATE. (M)

Part: SEAT TRACK — CORRODED (BS 1200)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK AT STATION 1200. INSTALLED NEW SEAT TRACK PER SRM 53-05 FIG 43, STATION 1185 TO STATION 1305. (M)

Part: LONGERON — CORRODED (BS 1212-1231)

TUL - FOUND LONGERON 25R IS CORRODED FROM STATION 1212-1231. CUT OUT 19 INCHES OF CORRODED LONGERON. INSTALLED NEW PIECE OF LONGERON AND LONGERON SPLICE PER SRM 53-02 FIG 5. (M)

Part: BRACKET — CORRODED (BS 636)

TUL - FOUND ANGLE FORWARD BOTTOM CORNER HAS CORROSION MID CARGO DOOR CUTOUT. INSTALLED NEW CORNER BRACKET IN FORWARD BOTTOM CORNER OF MID CARGO DOOR CUTOUT. (M0

Part: DOOR JAMB — CORRODED (BS 1155-1212)

TUL - FOUND CORROSION LOWER DOOR JAMB, STATION 1155 TO STATION 1212. REPAIRED PER ESO 80559, DATED 1-11-96 AND AARD 53-10-00-3. (M)

Part: BLKHD DOUBLER — CORRODED (BS 1338)

TUL - FOUND CORROSION ON SPADE PLATE, FORWARD FACE OF PRESSURE BULKHEAD STRINGER 1338 LONGERON 30. INSTALLED NEW SPADE PLATE ON FORWARD FACE OF AFT PRESSURE BULKHEAD. (M)

Part: FRAME — CORRODED (BS 1320)

TULE - FOUND BELT FRAME AT STATION 1320 HAS CORROSION AT L30 LOWER ATTACH POINT. INSTALLED REPAIR PER SRM 53-03 FIG 2A. (M)