N476AA

Part: BAYONET — DAMAGED (L2 DOOR) · airframe 75,544 hrs · 39,881 cycles

ACFT WOULD NOT PRESSURIZE. NO EMERGENCY DECLARED, RETURNED TO DEPARTURE. FOUND THE L2 DOOR BAYONET & BAYONET RECEIVER ON FRAME BENT & DAMAGED PREVENTING THE DOOR FROM SECURING PROPERLY. REMOVED AND REPLACED BAYONET RECEIVER AND RIGGED IAW AMM 52-40-00.

Part: WIRE — BROKEN (AC BAY) · airframe 74,554 hrs · 39,302 cycles

FOUND FWD OVERHEAD CEILING EMER LIGHT IN TAIL COMPARTMENT WIRE PULLED THROUGH. REPAIRED FWD OVERHEAD LIGHT TAIL COMPARTMENT WIRE. OPERATIONS CHECKED NORMAL.

Part: SENSE LINE — DISCONNECTED (AC PACK) · airframe 74,113 hrs · 39,033 cycles

CREW REPORTED BOTH AIR CONDITIONING PACKS INOPERATIVE. RT PACK WAS PLACARDED PRIOR TO DEPARTURE. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND LT PACK PRESS SENSING LINE LOOSE & DISCONNECTED DURING TROUBLESHOOTING IAW AMM 21-20-00-101. RE-INSTALLED SENSE LINE ON LT PACK & ACCOMPLISHED MPM & MEL IAW 21-01A ON RT PACK. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,333 hrs · 38,035 cycles

LT SIDE FUSELAGE CRACKED IN SKIN AT STATION 1437 BETWEEN LONGERONS 3 & 4. INSTALLED DOUBLER IAW EA MD80-53-032059 & SRM 53-04-00.

Part: RIB — CRACKED (R WING) · airframe 72,333 hrs · 38,035 cycles

RT WING NR 4 SLAT TRACK SUPPORT RIB CRACKED. STOP DRILLED CRACK & INSTALLED SLAT TRACK SUPPORT DOUBLER IAW EA MD80-57-032050.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 72,333 hrs · 38,035 cycles

RT WW PRESSURE PANEL IS CRACKED AT THE FUEL DRAIN SHROUD AFT ATTACH ANGLE. REPAIRED PRESSURE DECK IAW AARD 53-30-00-13.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 71,934 hrs · 37,792 cycles

DFW CREW REPORTED BIRD STRIKE TO NR 1 ENGINE. LT ENGINE WAS SHUTDOWN SINGLE ENGINE TIME 9 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. LT ENGINE FAN BLADES DAMAGED. REPLACED LT ENGINE AT DFW ON 08/23/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,575 hrs · 37,027 cycles

DAMAGED HOLE AT FRAME SPLICE FUSELAGE STATION 200 AT LONGERON 24 LEFT. INSTALLED FREEZE PLUG AND REINFORCING STRAP AT FRAME SPLICE FUSELAGE STATION 200 AND LONGERON 24 LEFT PER EA MD80-53-029731.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

FUSELAGE SKIN STATION 1380 LONGERON 14 RIGHT CRACKED. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIGURE 2 SHEET 3.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION UNDER G1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16 AND EA MD80-53-023501.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

CUT FROM LIGHTENING HOLE TO OUTBOARD EDGE OF CUSP SHEET, STATION 0687 FOR ELECTRICAL WIRING. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

LEFT STATION 674 HAS TOOLING MARK ON CUSP T-ANGLE. INSTALLED REPLACEMENT CUSP T-SECTION, FORWARD AND AFT SPLICE ANGLE PER SRM 53-05-00 FIGURE 25.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

SHEAR TIE CRACKED AFT SIDE OF 1437 ABOVE LONGERON 17 RIGHT. INSTALLED NEW SHEARTIE AFT SIDE OF STATION 1437 AND ABOVE LONGERON 17 RIGHT PER AARD 51-10-00-5.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

OBLONG HOLE IN DOOR BEAM STATION 1212 BETWEEN LONGERONS 25 AND 24 RIGHT. INSTALLED DOUBLER REPAIR PER EA MD80-53-023616.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION ON LEFT CUSP BETWEEN STATIONS 579 TO 598. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

RIGHT CUSP SHEET FROM STATIONS 446 TO 457 CORRODED. INSTALLED REPAIR DOUBLER FROM STATIONS 438 TO 454 RIGHT BUTTLINES 50 TO 60 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION ON LEFT CUSP FROM STATIONS 541 TO 560. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

RIGHT SUBFLOOR CORRODED AT STATION 216 RIGHT BUTTLINE 56. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

AFT SERVICE DOOR FORWARD GIRT BAR MOUNT BRACKET HAS CORROSION UNDER BRACKET ON SUB FLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION ON BOTTOM OF RIGHT CUSP AT STATION 522. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

DAMAGE ON RIGHT CUSP AT STATION 890 INBOARD OF SEAT TRACK 6. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

RIGHT CUSP SHEET FROM STATIONS 640 TO 650 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION ON LEFT CUSP OUTBOARD OF CENTER LIGHTNING HOLE BETWEEN STATIONS 522 TO 541. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

AFT SERVICE DOOR AFT GIRT BAR MOUNT BRACKET HAS CORROSION UNDER BRACKET ON SUB FLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,526 hrs · 35,887 cycles

CORROSION ON DIAPHRAM SHEET UNDER GALLEY TIEDOWN AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,526 hrs · 35,887 cycles

CRACK IN LEFT CUSP STATION 218 JUST OUTBOARD OF NUMBER 2 SEAT TRACK. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: UNLOCK SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 66,035 hrs · 34,510 cycles

DEN - INFLIGHT STL-LAX. CREW REPORTED LEFT TRUST REVERSER UNLOCK INDICATION LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. ADJUSTED LEFT ENGINE THRUST REVERSER UNLOCK SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CADC — MALFUNCTIONED (NR 1) · airframe 65,883 hrs · 34,425 cycles

AUS - CREW REPORTED CAPTAINS AIRSPEED INDICATOR BECAME UNRELIABLE. EMERGENCY DECLARED FLIGHT LANDED AUS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE CENTRAL AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TUBE — DIRTY (ACM) · airframe 65,581 hrs · 34,284 cycles

BWI - CREW REPORTED AFTER TAKEOFF PRESSURIZATION FLOW LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED BWI LANDED WITHOUT INCIDENT. CLEANED BOTH PACK AIR CYCLE MACHINE DE-ICE TUBES. PRESSURIZED AIRCRAFT AND NO FAULTS FOUND. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PROBE — INOPERATIVE (RUDDER) · airframe 64,580 hrs · 33,725 cycles

ORD - INFLIGHT DFW-MSP. CAPTAIN REPORTED RUDDER LIMITER LIGHT ILLUMINATED DURING CRUISE. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER LIMITER HEATER PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,570 hrs · 33,717 cycles

CANT FRAME 1474 IS CRACKED AT RIVETS AT LONGERON 18 RIGHT AREA AFT ACCESSORY COMPARTMENT. COMPLETED INSTALLATION OF DOUBLER PER EA MD-80-53-013941.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,570 hrs · 33,717 cycles

AFT CARGO DOOR JAM, STATION 1155, LOWER CORNER BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM 51-30-01.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 60,682 hrs · 31,611 cycles

3 EMERGENCY LIGHT BATTERY PACKS WEAK. REMOVED AND REPLACED BATTERY PACKS PER MM 33-53-00-6. OP`S CHECK GOOD.

Part: CASTING — CRACKED (RT WING SPOILER) · airframe 60,684 hrs · 31,612 cycles

RT WING GROUND SPOILER CASTING CRACKED. REPLACED SPOILER CASTING PER SRM 51-30-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,677 hrs · 31,607 cycles

AFT AISLE BATTERY PACK AB5-4 HAS LOW OUTPUT. REMOVED AND REPLACED BATTERY PER 33-60-98-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,677 hrs · 31,607 cycles

CANT FRAME 1474 CRACKED. INSTALLED DOUBLER ON CANT FRAME AT L18L PER ZAARD 53-10-00-15.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 60,677 hrs · 31,607 cycles

VERTICAL BRACKET CRACKED ON FWD WALL BELOW SLANT PANEL IN LT WHEEL WELL 21 INCHES FROM I/B CORNER. REPLACED SLANT PANEL BRACKET PER 51-30-00.

Part: ADC — INOPERATIVE (ZONE 200) · airframe 60,436 hrs · 31,472 cycles

STL CAPTAINS AIRSPEED FAILED ON TAKEOFF. RETURNED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE AIR DATA COMPUTER AND NUMBER THREE VERTICAL GYRO. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: SHROUD — BROKEN (LIGHT ASSY) · airframe 59,142 hrs

DFW - EMERGENCY LIGHT AT SEAT 14D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (LIGHT ASSY) · airframe 59,142 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (LIGHT ASSY) · airframe 59,142 hrs

DFW - EMERGENCY LIGHT AT SEAT 23D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT PASSENGER ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT PASSENGER ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (AIR CONDITIONING)

DFW INFLIGHT - LEFT AND RIGHT AIR CONDITION PACKS INOPERATIVE. UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED LEFT FLOW CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 27 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GYRO — FAILED (COCKPIT)

DFW T1052/09 EN ROUTE IAH-DFW ALL PRIMARY FLIGHT INSTRUMENTS INOPERATIVE. NR 2 GYRO IN 30 DEGREES TURN CONTINUED TO ROTATE AT ONE POINT NR 1, NR 2 AND STANDBY ALL SHOWED HEADINGS THAT WERE 30 DEGREES MINIMUM APART. LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER 1 AND 2 DIRECTIONAL GYROS AND CAPTAINS RADIO DIRECTION MAGNETIC INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: CONTACTOR — DIRTY (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT L2 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS OVER WALKWAY IN TAIL COMPARTMENT INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT BATTERY FOR TAILCONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — LOOSE (BATTERY PACK)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED TAIL CONE EMERGENCY EXIT LIGHT BATTERY PACK CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — RESTRICTED (EMER EXIT SYSTEM)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER TAIL CONE WALKWAY, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMER EXIT SYST)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER TAIL CONE WALKWAY, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROWS 19-22 INOPERATIVE. REPLACED EMEREGNCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (AFT AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

RDU - FLT 1176 - PRIOR TO GATE DEPARTURE DETECTED STRONG ELECTRICAL BURNING SMELL AT MID CABIN. TURNED OFF ALL POWER. REPLACED FLUORESCENT LAMP HOLDER AND BULB AT SEAT 10DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DENT WITH GOUGE IN FUSELAGE SKIN BETWEEN LONGERON 26L AND 27L AFT 1193 SKIN AROUND DENT HAS BEEN SCUFFED UP WITH ABRASIVE TOOL. BLENDED AREA REFOMRED DENT INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP PANEL STATION 1160 TO 1211. INSTALLED REPAIR TO CUSP PER AARD 53-00-00-02 AFTER DAMAGED AREAS REMOVED PER 51-10-3, DAMAGE REMOVAL. TREATED AND PRIMED AND INSTALLED PER 53-10-SRM. (M)

Part: SKIN — DENTED (TE FLAP)

TUL - FOUND OUTBOARD FLAP LOWER SIDE HAS 2 DENTS AT OUTBOARD END SCRATCH IN OUTBOARD FLAP LOWER OUTBOARD END. REPLACED DAMAGED PANEL WITH FABRICATED PANEL PER ESO 80559. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN SHEAR TIE AT STATION 1380, LEFT SIDE ABOVE NR 1 ENGINE PYLON. REMOVED AND REPLACED SHEAR TIE PER 53-10-00 PAGE 2. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP LEFT AT RIVET , STATION 1066-1073. INSTALLED DOUBLER PER SRM 53-01 AARD 53-00-02. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

NR 6 SEAT TRACK HAS GOUGE IN CENTER OF TRACK AT STATION 578. INSTALLED NEW SEAT TRACK FROM STATION 569-798 WITH SPLICE AT 569 PER SRM 53-05 PART 1 FIG 4F. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - TEMPORARY REPAIR RIVET INSTALLED AT STATION 310 BETWEEN LONGERON 27R AND 28R. CUT OUT 1 INCH HOLE TO CLEAR TEMPORARY REPAIR. INSTALLED FLUSH PATCH PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - NR 2 SEAT TRACK CORRODED FROM STATION 1212-1231. INSTALLED NEW NR 2 SEAT TRACK PER 51-01 AND 51-3. (M)

Part: STRUCTURE — CORRODED (VERTICAL STAB)

TUL - FOUND VERTICAL STAB HINGE PLATE CENTER SECTION, RIGHT INBOARD FACE AND LEFT INBOARD FACE CORRODED. MACHINED AND SPOT FACED RT INBOARD AND LEFT INBOARD SURFACE OF HINGE PLATE CENTER SECTION PER ESO 80559 DATED 2/11/00. LEFT MACHINED TO THICKNESS .631, RIGHT MACHINED TO THICKNESS .648 PER ESO. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED AT BS 1016.5 NR 2 SEAT TRACK. INSTALLED DOUBLER 4 INCH BY 5 INCH PER AARD 53-00-00-02. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FUSELAGE SKIN EMANATING FROM RIVET HOLE STATION 1309 LONGER 7L. CUT OUT CRACKED AREA AND INSTALLED FLUSH PATCH PER SRM 53-04 FIG 38. (M)

Part: STRUCTURE — CORRODED (VERTICAL STAB)

TUL - FOUR HINGE PLATES, FACES AND BORES CORRODED. REFACED INBOARD AND OUTBOARD FACES AND REBORED 1.435 INCH TO REMOVE CORROSION. INSTALLED NEW BUSHINGS AND HONED PER SRM 55-02 PAGE 68. (M)

Part: WEB — CRACKED (CUSP)

TUL - FOUND SEVERAL CRACKS AND CORROSION BETWEEN STATION 1250 AND STATION 1309. REPLACED LEFT CUSP PANEL FROM STATION 1250-1309 PER SRM 51-00. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED AT SMALL LIGHTNING HOLE, RIGHT TUNNEL STATION 223. INSTALLED NEW CUSP SHEET FROM STATION 218-220 PER SRM 51-00. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

TUL - G-2 GALLEY AFT INBOARD FLOOR TIE DOWN CORRODED AT BS 213. RE-INSTALLED LOWER GALLEY MOUNT, INSTALLED NEW UPPER GALLEY TIE DOWN INBOARD PER SRM 51-30. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

TUL - RIGHT FORWARD TIE DOWN TRACK HAS CORROSION AROUND SCREW ATTACH HOLES. REPLACED RIGHT FORWARD TIE DOWN TRACK SRM 51-01. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGE IN FUSELAGE STATION 1292, STRINGER 11R, ABOVE RIGHT PYLON. BLENDED AREA, ACID ETCHED, DYE CHECKED. NO CRACKS FOUND, FABRICATED DOUBLER 2024-T3 .032 INCH TREATED AND PRIMED. INSTALLED DOUBLER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - NR 6 SEAT TRACK WORN IN BOTTOM, STATION 1181. INSTALLED PLUG PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT ON RIGHT SIDE OF FUSELAGE, 1 FOOT DOWN 1 FOOT FORWARD A/C NUMB RS APPROX 4 INCH LONG. BLENDED DENT, ACID ETCHED, DYE CHECKED. NO CRACKS FOUND. FABRICATED DOUBLER .032 INCH 2024T3, COLD WORKED DENT BACK TO SHAPE. INSTALLED DOUBLER AT AREA NOTED PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND NR 4 SEAT TRACK WORN BS 764. REMOVED DAMAGE, INSTALLED TRACK PLUG PER 53-05 FIG 4A. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

TUL - FOUND DEEP WEAR IN NR 4 SEAT TRACK STATION 674. ROUTED OUT LIMITS AREA TREATED, PRIMED AND INSTALLED SEAT TRACK PLUG SRM 53-05 FIG 4A. (M)

Part: WEB — CORRODED (BS 1212-1219)

TUL - FOUND CORROSION ON WEB STATION 1212-1219 AROUND NUTPLATE. REMOVED WEB, INSTALLED WEB IAW MM 20-10-15-2 FIG 202 SRM 51-01. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND DEEP WEAR IN SEAT TRACK NR 4. REMOVED DAMAGE, INSTALLED PLUG PER 53-05 FIG 4. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND DOOR JAMB BEAM CORRODED. REPLACED DOOR JAMB BEAM PER AARD 53-10-00-03. (M)

Part: APU — LEAKING (AFT ACCESSORY)

MIA - FLT 1327 - DURING TAKEOFF, FLIGHT CREW NOTICED SMOKE IN THE CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. UPON LANDING, SMOKE DISSIPATED FOR THE CABIN. MAINTENANCE FOUND THE APU LEAKING OIL INTO THE AIR CONDITIONING SYSTEM. REPLACED APU AND RAN WITH PACKS ON WITH NO LEAKS OR SMELL NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — CHAFED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, STAIRWAY EMERGENCY LIGHTS WERE INOPERATIVE. REPAIRED CHAFED STAIRWAY EMERGENCY EXIT LIGHTING WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — SHORTED (CABIN)

BOS - FLT 630 - EN ROUTE DFW/BOS - DURING CRUISE, F/A NOTED ELECTRICAL ODOR BY PAX SEAT ROW 29DEFT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED BOS AND LANDED WITHOUT INCIDENT. PLACARDED WINDOW LIGHT LAMPHOULDER (SOCKET) ABOVE PAX SEAT ROW 28-29 DEF. SUBSEQUENTLY REPLACED LAMPHOLDER ABOVE PAX SEAT ROWS 28-29 DEF AT EWR. SYSTEM GROUND CHECKED NORMAL OPERATIONS WITH NO ELECTRICAL ODOR NOTED. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MAIN CABIN FORWARD OF PAX SEAT ROW 20 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT STRIP — MISSING (CABIN)

ATL - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 28 AND 32 MISSING. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 28 AND 32. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)