N248AA

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 71,950 hrs · 38,586 cycles

LOWER FORWARD TEE FITTING CRACKED. REMOVED AND REPLACED CRACKED TEE FITTING.

Part: PUMP — FAILED (FUEL BOOST)

ORD INFLIGHT T1493/13SEP - AFT CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AFT CENTER TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT ON ANNUNCIATOR PANEL INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON ANNUNCIATOR PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT AFT SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MANIFOLD — INOPERATIVE (LT ENGINE)

LAX - LEFT ENGINE LOOP-A LIGHT FOLLOWED BY LEFT ENGINE FIRE WARNING DURING CLIMBOUT AT APPROXIMATELY 6000 FEET. THROTTLES TO IDLE AND LIGHTS AND WARNING WENT OUT. LEFT EXHAUST GAS TEMPERATURE AT TAKEOFF IN YELLOW ZONE. RIGHT ENGINE EXHAUST GAS TEMPERATURE NORMAL. CONTINUED OPERATION AT IDLE FOR 20 MINUTES. LANDED LAX WITHOUT INCIDENT. FOUND 13TH STAGE MANIFOLD INNER CASE BLOWN APART. CHANGED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, CEILING AISLE EMERGENCY EXIT LIGHTS FROM ROWS 8 THROUGHT 11 INOPERATIVE. INSTALLED NEW EMERGENCY EXIT LIGHT BATTERY GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED AT FASTENER HOLE, RIGHT SIDE OF L2R. REPLACED WITH SERVICEABLE SHEAR TIE PER SRM 51-30. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED STATION 1437, RIGHT SIDE OF LONGERON 1R AFT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FUSELAGE SKIN .375 INCH LONGERON FROM RIVET HEAD AT STATION 1380 L13R. STOP DRILLED CRACK, DYE CHECKED AND INSTALLED DOUBLER PER SRM 53-01-00. (M)

Part: FRAME — DAMAGED (FUSELAGE)

TUL - FOUND DAMAGE ON FORMER AT STATION 522 BETWEEN L20R AND L21R. INSTALLED FORMER REPAIR SPLICE PER SRM 53-03-00 FIG 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACKED .375 INCH IN FUSELAGE SKIN FROM RIVET HEAD STATION 1380 L14L. INSTALLED DOUBLER PER AARD 53-30-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BOTTOM SIDE OF CLIP NUT TABS, BEYOND MANUAL LIMITS. SPLICE IN NEW SECTION OF NR 2 SEAT TRACK PER SRM 53-05. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND STATION 636 FORWARD SIDE OF DOOR JAMB DAMAGE TO STRUCTURE FROM TO LONGERON SCREW BEING INSTALLED IN FLOORBOARD. INSTALLATION OF DOUBLER PER AARD 53-10-00-24. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION BEYOND MANUAL LIMITS. SPLICE NEW SECTION OF SEAT TRACK NR 6 SRM PER SRM 53-05. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN FUSELAGE SKIN INBOARD AREA OF FORWARD LAVATORY DRAIN ACCESS AREA BEYOND MANUAL LIMITS. INSTALLED DOUBLER PER ESO 80559, DATED 11-18-2002. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 17L CRACKED WHERE IT INTERSECTS FRAME 237. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIG 18. (M)

Part: BELTFRAME — CRACKED (FUSELAGE)

TUL - FOUND TWO CRACKS ON BELL FRAME STATION 1174, L6L. INSTALLED DOUBLER, STOP DRILLED CRACKS PER 53-10-00-30. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 17L CRACKED AT STATION 332. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIG 18. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 17L IS CRACKED AT STATION 408. CUT OUT DAMAGED SECTION OF LONGERON. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02-00. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND TWO DAMAGED HOLES IN FORWARD EDGE OF CUSP AT STATION 984. INSTALLED CUSP DOUBLER AT STATION 984 PER SRM 53-01 FIG 4. (M)

Part: WEB — TORN (FUSELAGE)

TUL - FOUND RIGHT CUSP TORN AT STATION 1000. REPLACED CUSP, RIGHT SIDE, STATION 1000 PER SRM 53-01. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON HORIZONTAL AND VERTICAL SURFACES OF MID CARGO DOOR BEAM. REMOVED CORROSION PER SRM 51-10-03. INSTALLED DOUBLER ON DOOR BEAM WHERE CORROSION REMOVAL WAS BEYOND MANUAL LIMITS PER AARD 53-10-00-8. (M)

Part: SKIN — WRINKLED (FUSELAGE)

TUL - FOUND 3 INCH WRINKLE ON EXTERNAL SKIN STATION 109, FORWARD OF LONGERON 25R. INSTALLED FILLER A DOUBLER PER SRM 53-01-00 FIG 2 SHEET 3. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROW 8 THROUGH 11 DIM. RESEATED CEILING EMEREGNCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — MISSING (ANTI-ICE SYS)

AMA- FLT 717 - EN ROUTE DFW-OAK, AT 31,000 FEET FLIGHT ATTENDANTS REPORTED FUMES AND SMOKE IN REAR OF AIRCRAFT. PASSENGER IN SEAT 24B REPORTED TO FLIGHT ATTENDANT THAT FLOOR WAS HOT AND GETTING HOTTER. AIR CONDITION SMOKE/FUMES CHECKLIST ACCOMPLISHED. CABIN SMOKE FUMES CHECKLIST ACCOMPLISHED. FLIGHT ATTENDANTS STILL REPORTED STRONG FUMES. AIRCRAFT AS DEPRESSURIZED AT 4.000 FEET. DIVERTED AND LANDED AMA WITHOUT INCIDENT. AIRCRAFT INSPECTED AND FOUND TO BE IN CONDITION FOR SAFE FLIGHT FROM AMA TO DFW FOR REPAIR OF WING ANTI-ICE DUCT. REPLACED DEFECTIVE AND MISSING SEALS IN WING ANTI-ICE DUCTING FORWARD LEFT SIDEWALL AREA OF AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

SAN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTORS — DEFECTIVE (LT ENGINE)

MIA - FLT 1479 - DURING CLIMB-OUT FROM FLL AT APPROX 15,000-18,000 FT, THE MASTER CAUTION AND FIRE DETECTION LIGHTS ILLUMINATED, ALONG WITH LOOP 'B' LIGHT FOR THE LEFT ENGINE. PERFORMED APPROPRIATE CHECKLIST AND THE LEFT ENGINE FIRE LIGHT ILLUMINATED ALONG WITH THE AURAL FIRE WARNING. ALL ENGINE INDICATIONS WERE NORMAL FOR CLIMB SETTINGS. THE FIRE HANDLE WAS PULLED AND BOTH FIRE BOTTLES WERE FIRED. FIRE LIGHT REMAINED ILLUMINATED THROUGHOUT FLIGHT. LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED LOWER LOOP 'A' AND 'B' CONNECTORS, GROUND TERMINAL AND LOWER LOOP SUPPORT ASSEMBLY. ACCOMPLISHED FULL POWER RUN, FIRE TEST OPERATIONS CHECK NORMAL. NO FIRE DETECTION LIGHT NOTED. NO LEAK NOTED. REPLACED FIRED BO

Part: CONDUCTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS FOUND INOPERATIVE FROM FIRST CLASS BULKHEAD TO FORWARD OVERWING EXIT. REPLACED FLAT CONDUCTOR AT FIRST CLASS BULKHEAD AND REPAIRED FLAT CONDUCTOR FORWARD OF FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MAIN CABIN FROM PAX SEAT ROW 21 FORWARD INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)

SFO - FLT 1308 - DURING CLIMB-OUT, RIGHT ENGINE SURGED TO 95 PERCENT N1 FOLLOWED BY FLAME OUT. ACCOMPLISHED ENGINE SHUTDOWN PROCEDURES AND AIRCRAFT DIVERTED TO SFO, LANDING WITHOUT INCIDENT. CHECKED RIGHT ENGINE INLET AND EXHAUST WITH NO DAMAGE OR DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND ENGINE OPERATION CHECKED NORMAL. ACCOMPLISHED BORESCOPE OF RIGHT ENGINE WITH NO DAMAGE OR DEFECTS FOUND. REPLACED RIGHT ENGINE FUEL CONTROL. ALSO, REPLACED RIGHT ENGINE FUEL PUMP AND FILTER. ACCOMPLISHED GROUND ENGINE RUN AND TRIM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)