N7548A

Part: FRAME — CRACKED (BS 1510) · airframe 74,783 hrs · 39,505 cycles

CRACK FOUND ON THE FRAME ON THE LEFT BS 1510 AROUND THE 6TH TAIL CONE ALIGNMENT PIN FROM THE TOP IN THE TAIL CONE COMPARTMENT . REPAIRED IAW SRM 53-01-00-001.

Part: LONGERON — CRACKED (BS 160) · airframe 74,633 hrs · 39,388 cycles

CRACK INDICATIONS ON LONGERON 24L AT THE FASTENER HOLE, BS 160. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (BS 200) · airframe 74,633 hrs · 39,388 cycles

CRACK INDICATIONS ON LONGERON 23L AT THE FASTENER HOLE, BS 200. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (BS 200) · airframe 74,633 hrs · 39,388 cycles

CRACK INDICATIONS ON LONGERON 24L AT THE FASTENER HOLE, BS 200. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: STIFFENER — CRACKED (BS 218 BULKHEAD) · airframe 74,633 hrs · 39,388 cycles

CRACK INDICATION ON THE STIFFENER LOWER END AT BS 218 BULKHEAD BETWEEN LONGERONS 23L AND 24L. REPAIRED THE STIFFENER IAW SRM 53-01-00-001, SRM 53-14-01-001, AND D 53-10-00-15.

Part: BATTERY — WEAK (MEGAPHONE) · airframe 74,538 hrs · 39,315 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD MEGAPHONE IS WEAK. REMOVED AND REPLACED MEGAPHONE BATTERIES PER AMM 23-34-00. OPERATIONAL CHECK GOOD.

Part: MOUNT — UNSECURE (EMERGENC LIGHT) · airframe 74,452 hrs · 39,256 cycles

RED EMERGENCY LIGHT IN THE AISLE FLOOR ADJACENT TO SEAT 19D IS COMING OUT OF MOUNT. SECURED THE MOUNT IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD.

Part: FRAME — CRACKED (RT MLG WW) · airframe 73,979 hrs · 38,973 cycles

THREE WAY CRACK IN THE RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD FRAME. REPAIRED IAW DWG 53-10-00-12. AIRCRAFT WAS GROUNDED.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 73,491 hrs · 38,662 cycles

AT FL250 PRESSURIZATION FLOW LIGHT CAME ON. UNABLE TO REGAIN CONTROL OF CABIN, LEFT PACK ZERO FLOW. THE FLIGHT WAS OPERATING SINGLE PACK WITH THE RIGHT HAND PACK PREVIOUSLY PLACARDED. CREW DECLARED EMERGENCY AND INITIATED AN EMERGENCY DESCENT. THE CABIN PRESSURE REACHED 12,500. THE MASKS DID NOT DEPLOY. THE FLIGHT DIVERTED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WATER SEPARATOR TEMP CONTROL VALVE IAW AMM 21-20-03. ALSO REPLACED BOTH COALESCER BAGS IAW 21-20-02. THE RIGHT PACK CONTINUED ON MEL. THE AIRCRAFT WAS GROUNDED.

Part: DOOR — OPEN (NLG) · airframe 72,970 hrs · 38,303 cycles

AIRCRAFT NOT GROUNDED. TPA-DFW FLIGHT RETURNED TO TPA ACCOUNT VIBRATIONS FROM NOSE LANDING GEAR DURING RETRACTION. LANDING UNEVENTFUL. RIGHT NOSE GEAR DOOR REPORTED TO BE OPEN UPON GATE ARRIVAL. ACCOMPLISHED INSPECTION IAW AMM 32-96-14. NO FAULTS NOTED. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,931 hrs · 38,271 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT AFT VAULT DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW 25-60-00. OPERATIONAL CHECK GOOD.

Part: SENSOR — FAULTY (CABIN TEMP) · airframe 72,921 hrs · 38,265 cycles

AIRCRAFT WAS GROUNDED. WHILE ADVANCING THROTTLES, THE LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED. TAKEOFF WAS ABORTED, AIRSPEED ATTAINED WAS 0. REMOVED AND REPLACED LEFT PNEUMATIC AIR CONDITIONING CONTROL THERMOSTAT IAW AMM 21-61-07 (AALA20170104024) AND LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH SENSOR IAW AMM 21-61-04. OPERATIONAL CHECK GOOD.

Part: THERMOSTAT — FAULTY (CABIN TEMP) · airframe 72,921 hrs · 38,265 cycles

AIRCRAFT WAS GROUNDED. WHILE ADVANCING THROTTLES, THE LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED. TAKEOFF WAS ABORTED, AIRSPEED ATTAINED WAS 0. REMOVED AND REPLACED LEFT PNEUMATIC AIR CONDITIONING CONTROL THERMOSTAT IAW AMM 21-61-07 AND LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH SENSOR IAW AMM 21-61-04(AALA20170104025). OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 72,787 hrs · 38,186 cycles

AIRCRAFT NOT GROUNDED. 2 EMERGENCY EXIT LIGHTS ON THE WALL OF THE TAIL AIR STAIR EXIT ARE INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHTS. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMEGENCY LIGHT) · airframe 72,700 hrs · 38,126 cycles

SEAT MOUNTED ESCAPE LIGHT CONNECTOR AT SEAT 16DEF IS DISCONNECTED. SECURED CONNECTOR. OPERATIONAL CHECK GOOD.

Part: FRAME — WORN (FUSELAGE) · airframe 72,084 hrs · 37,755 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT SIDE OF FRAME AT FUSELAGE STA 1510 BETWEEN L24L AND L30. REPAIRED FRAME IAW SRM 51-70-05 FIGURE 1 AND EA 262610

Part: SKIN — CRACKED (ZONE 200) · airframe 72,084 hrs · 37,755 cycles

FUSELAGE SKIN IS CRACKED AT BS 1418 AND LONGERON 2R. REPAIRED SKIN IAW SRM 53-04-00 FIGURE 40.

Part: FRAME — WORN (BS 1510) · airframe 72,084 hrs · 37,755 cycles

AFT SIDE OF FRAME AT BS 1510 BETWE LONGERONS 24 AND 27R. REPAIRED FRAME IAW SRM 53-01-00-001 AND EA 262608.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,084 hrs · 37,755 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR STOP FITTING, AFT SIDE BOTTOM STOP IS CRACKED. REMOVED AND REPLACED THE DOOR STOP FITTING IAW AARD 51-00-05-1 AND DRAWINGS CDK2345 & 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,084 hrs · 37,755 cycles

FORWARD CARGO COMPARTMENT MID CARGO DOOR STOP FITTING ON DOOR, FORWARD SIDE, SECOND STOP FROM TOP IS CRACKED. REMOVED AND REPLACED DOOR STOP FITTING IAW AARD 51-00-05-1 AND DRAWINGS CDK2345 & 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,084 hrs · 37,755 cycles

FORWARD CARGO BAY MID CARGO DOOR STOP FITTING ON DOOR, AFT SIDE, THIRD STOP FROM TOP, IS CRACKED. REMOVED AND REPLACED DOOR STOP FITTING IAW AARD 51-00-05-1 AND DRAWINGS CDK2345 & 5910141.

Part: SKIN — CRACKED (BS 1380) · airframe 72,084 hrs · 37,755 cycles

FUSELAGE SKIN AT BS 1380 AND LONGERON 14R IS CRACKED. REPAIRED SKIN IAW SRM 53-01-00 FIGURE 2 AND 53-30-00-02.

Part: BALLAST — BURNED (CABIN) · airframe 71,702 hrs · 37,523 cycles

AIRCRAFT WAS GROUNDED. BURNING ODOR REPORTED IN AFT CABIN OF AIRCRAFT. MAINTENANCE FOUND LIGHTING BALLAST BURNED OUT. R & R BALLAST IAW AMM 33-21-03.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,386 hrs · 37,333 cycles

AIRCRAFT WAS NOT GNDED. CABIN EMER FROM FWD MOST OVERWING EMER EXIT ROW ARE DIM. R & R BATTERY PACKS & POWER SUPPLIES AT LOCATION AB5-1 & AB5-2 IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160506002, AALA 20160506003 & AALA 20160506005.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,386 hrs · 37,333 cycles

AIRCRAFT WAS NOT GNDED. CABIN EMER FROM FWD MOST OVERWING EMER EXIT ROW ARE DIM. R & R BATTERY PACKS & POWER SUPPLIES AT LOCATION AB5-1 & AB5-2 IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160506003, AALA 20160506004 & AALA 20160506005.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,386 hrs · 37,333 cycles

AIRCRAFT WAS NOT GNDED. CABIN EMER FROM FWD MOST OVERWING EMER EXIT ROW ARE DIME. R & R BATTERY PACKS & POWER SUPPLIES AT LOCATION AB5-1 & AB5-2 IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160506002, AALA 20160506003 & AALA 20160506004.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,386 hrs · 37,333 cycles

AIRCRAFT WAS NOT GNDED. CABIN EMER FROM FWD MOST OVERWING EMER EXIT ROW ARE DIM. R & R BATTERY PACKS & POWER SUPPLIES AT LOCATION AB5-1 & AB5-2 IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160506002, AALA 20160506004 & AALA 20160506005.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 70,912 hrs · 37,049 cycles

WHILE THE ACFT WAS BEING CATERED. DOOR SLIDE AT THE FWD GALLEY FELL OUT & WAS LAYING ON THE RAMP. IT DID NOT DEPLOY. REPLACED THE R1 FWD RT SERVICE DOOR ESCAPE SLIDE IAW MCM 25-94-20 & REFERENCE EA 258524. THE ACFT WAS NOT GNDED.

Part: SEAL — LEAKING (APU) · airframe 70,836 hrs · 37,998 cycles

AIRCRAFT WAS GNDED. DURING CLIMB SLIGHT SMELL & HAZE NOTICED. RECIRCULATION FAN & ENG HEAT TURNED OFF. SMELL & HAZE DISSIPATED. AT TOP OF DESCENT RECIRCULATION FAN TURNED BACK ON & SMELL REOCCURRED. FOUND BAD SEAL ON APU OIL CAP. R & R SEAL & ACCOMPLISHED PACK BURN IAW MCM 21-96-01, MCM 21-92-12, & AMM 21-20-02. GND OPERATIONAL CHECKED GOOD.

Part: SENSOR — FAILED (COCKPIT) · airframe 70,575 hrs · 36,822 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB PRESSURIZATION FLOW CAME ON. RT PACK FLOW INDICATOR WENT TO ZERO. ACFT WOULD NOT PRESSURIZE. CABIN PRESS TRANSFER LOCKOUT & STANDBY LIGHT ON. R & R FLIGHT COMPARTMENT TEMPERATURE LIMITER SENSOR IAW AMM 21-21-61-05. PERFORMED ACFT PRESSURIZATION IAW AMM 21-32-00. OPERATIONAL CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,425 hrs · 36,742 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS IN AFT ACCESSORY AREA ARE INOPERATIVE. R & R EMER LIGHT BATTERY AT STATION 1338 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: SLIDE — FAULTY (TAILCONE) · airframe 69,499 hrs · 36,204 cycles

AS CREW CLOSED DOORS THE FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN. SLIDES WERE DEPLOYED & AIRCRAFT EVACUATED. THE TAIL CONE SLIDE FAILED TO DEPLOY.

Part: APU — SMOKE (CABIN) · airframe 69,499 hrs · 36,204 cycles

AS CREW CLOSED DOORS THE FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN. SLIDES WERE DEPLOYED & AIRCRAFT EVACUATED. THE TAIL CONE SLIDE FAILED TO DEPLOY. R & R APU IAW MCM 49-96-82. ACCOMPLISHED PACK BURN OUT IAW MCM 21-92-12. APU OPERATIONAL & LEAK CHECKED GOOD. APU ENGINEERING REPORTS OIL FILL SCUPPER SEPARATED FROM HOUSING.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,251 hrs · 36,057 cycles

AFT GALLEY EMER LIGHT WILL NOT TEST. REPLACED POWER SUPPLY.

Part: MODULE — INOPERATIVE (CABIN) · airframe 69,251 hrs · 36,057 cycles

FORWARD EGRESS LIGHT INOPERATIVE. REPLACED MODULE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,251 hrs · 36,057 cycles

CABIN ROWS 17 - 24 EMER LIGHTS WILL NOT TEST. REPLACED BATTERY POWER SUPPLY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,251 hrs · 36,057 cycles

FIRST CLASS CABIN ROWS 3 TO 7, EMER LIGHT WILL NOT TEST. REPLACED BATTERY POWER SUPPLY.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

RIGHT CUSP TO FRAME T FITTING AT FS 1287 IS CORRODED. R & R FITTING IAW SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

RIGHT CUSP SHEET CRACKED BETWEEN FS 993 & 1003. R & R CUSP SHEET IAW AARD 51-00-05-1, AARD 53-20-00-16, AARD 51-00-00-03, AMM 53-20-01 & SRM 51-10-03.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

RIGHT CUSP SHEET CRACKED IN SEVERAL LOCATIONS BETWEEN FS 1271 & 1303. R & R CUSP SHEET IAW SRM 51-30-02, SRM 51-30-05 & DWG 9930612.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

AFT CARGO COMPARTMENT LOWER DOOR FRAME WEB STRAP AT FS 1174 IS CORRODED. R & R STRAP IAW AARD 51-00-05-1, DWG 5936442 & SRM 51-30-02. 8.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

LONGERON 29 RT END FITTING IS CORRODED AT FS 1335. R & R FITTING IAW AARD 51-00-05-1 & IPC 53-3-00-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

AFT CARGO COMPARTMENT LOWER DOOR FRAME WEB STRAP AT FS 1193 IS CORRODED. R & R STRAP IAW AARD 51-00-05-1, DWG 5936442 & SRM 51-30-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

AFT CARGO LOWER DOOR FRAME WEB UPPER & LOWER SURFACES ARE CORRODED AT SEVERAL AREAS BETWEEN FS 1155 & 1220. REPAIRED WEB IAW SRM 51-30-05 & SRM 51-30-02.8.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

FUSELAGE FRAME AT STATION 1250 IS CORRODED BETWEEN LONGERON 28 LT & 28 RT. REPAIRED FRAME IAW AARD 53-10-00-17.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

FLOORBOARD SUPPORT CORRODED. R & R FLOORBOARD SUPPORT IAW AARD 51-00-05-1 & DWG 9936656.

Part: STRAP — GOUGED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

GOUGE IN FRAME STRAP RT TIE DOWN TRACK. R & R STRAP IAW SRM 51-30-05.

Part: SKIN — BENT (CARGO DOOR) · airframe 68,666 hrs · 35,712 cycles

MID CARGO DOOR UPPER EDGE SKIN BENT TO RIVET ROW. REPAIRED IAW ESO 80174 PINK PAGE 601 F FIGURE 1 & SRM 51-10-03-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

CARGO MID CX CORROSION ON BOTTOM OF CUSP BETWEEN STATIONS 563 & 565 AT LONGERON 18 RT. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

CORROSION AT FOOT FITTING, AFT SIDE OF FRAME 1136, TOP RT CUSP. R & R FOOT FITTING IAW AARD 51-00-05-1, SRM 53-14-03-001 & DWG 9911524.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

LEFT CUSP CRACKED AT FS 226 OTBD OF SEAT TRACK NR 1. R & R CUSP SHEET IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

NUMBER 6 SEAT TRACK CORRODED BETWEEN FS 216 & 797. R & R SEAT TRACK & SPLICE IAW SRM 53-05-00-001 FIG 4F.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

FLOOR SUPPORT UNDER SEAT TRACK 3 IS CRACKED AT FS 864. R & R FLOOR SUPPORT IAW AARD 51-00-05-1.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

FORWARD CARGO DOOR SILL PAN CORRODED BETWEEN FS 397 & 399 AT LONGERON 28 RT. REPAIRED IAW EA 53-038696 DATED 2-20-15.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

RIGHT CUSP SHEET CRACKED AT LIGHTNING HOLE AT FS 282. REPAIRED IAW AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

INTERCOSTAL WEB CRACKED AT FS 206 & LONGERON 11 LT. REPAIRED WEB IAW AARD 53-10-00-11.

Part: STRUCTURE — PUNCTURED (APU BAY) · airframe 68,666 hrs · 35,712 cycles

APU ENCLOSURE HAS PUNCTURE DAMAGE ON AFT RT INTERIOR SIDE BETWEEN FS 1338 - 1380. REPAIRED IAW AARD 53-20-00-11 FIG 1 REPAIR 11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,666 hrs · 35,712 cycles

CORROSION ON BOTTOM AFT LIP OF FRAME AT FS 1271 BETWEEN LONGERON 29 RT & 29 LT. R & R LOWER J COMPLETE IAW AARD 51-10-00-01.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

RIGHT FWD UPPER CORNER WINDOW RING PAN CRACKED AT FS 927. REPAIRED IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,666 hrs · 35,712 cycles

CRACK IN LT SIDE WINDOW PAN FWD UPPER CORNER. DAMAGE REMOVED & DOUBLER INSTALLED IAW AARD 51-10-00-25.

Part: SENSOR — FAULTY (NLG) · airframe 67,444 hrs · 34,978 cycles

NOSE LANDING GEAR UNSAFE INDICATION. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED D1-32 SENSOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CSD — FAILED (RT ENGINE) · airframe 66,169 hrs · 34,227 cycles

STL CREW REPORTED RT ENG CONSTANT SPEED DRIVE OIL PRESS LOW LIGHT CAME ON & RT GEN TRIPPED OFF. EMERGENCY DECLARED FLIGHT RETURNED STL LANDED WITHOUT INCIDENT. DEFERRED RT ENG GEN INOPERATIVE IAW MEL 24-01A. FLIGHT CONTINUED TO DESTINATION. REPLACED RT CONSTANT SPEED DRIVE AT DFW ON 03/20/2014. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SHUTOFF VALVE — LEAKING (LT SPOILER) · airframe 63,135 hrs · 32,516 cycles

DFW - CREW REPORTED LEFT HYDRAULIC FLUID WENT TO ZERO QUANTITY DURING CRUISE. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT SPOILER SHUTOFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — FAILED (NLG) · airframe 63,135 hrs · 32,516 cycles

DFW - CREW REPORTED NOSE GEAR UNSAFE LIGHT ILLUMINATED AND GEAR UNSAFE AURAL WARNING SOUNDED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED D1-32 GEAR LOCKED SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PIN — LOOSE (EMERGENCY LIGHT) · airframe 62,654 hrs · 32,235 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 17D INOPERATIVE. FOUND LOOSE PIN IN CONNECTOR INSTALLED AND SECURED PIN ON CONNECTOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 62,654 hrs · 32,235 cycles

RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: GENERATOR — FAILED (RIGHT) · airframe 61,591 hrs · 31,630 cycles

ORD - CREW REPORTED DURING CLIMBOUT THE ENTIRE ELECTRICAL SYSTEM AC BEGAN CYCLING ON AND OFF VERY RAPIDLY (PINBALL EFFECT). OPENED AC CROSSTIE IN AN EFFORT TO STABLIZE THE SYSTEM WITH NO EFFECT. TURNED THE GENERATOR SWITCHES OFF ONE AT TIME, SYSTEM DID NOT STABLIZE UNTIL BOTH GENERATOR SWITCHES OFF. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR CONTROL UNIT AND LEFT CONSTANT SPEED DIRVE AND GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 61,577 hrs · 31,620 cycles

DFW - CREW REPORTED LEFT ENGINE GENERATOR FAILED ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. PLACARD LEFT ENGINE GENERATOR PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED LEFT HAND ENGINE GENERATOR AND GENERATOR CONTROL UNIT AT AUS ON 07/19/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PROBE — LEAKING (RT ENGINE) · airframe 60,101 hrs · 30,788 cycles

DFW - CREW REPORTED RIGHT THROTTLE 3 KNOBS FORWARD OF LEFT WITH EPR MATCHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PT2 ON RIGHT ENGINE THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — INOPERATIVE (LT ENGINE) · airframe 58,588 hrs · 29,941 cycles

DFW - CREW REPORTED LEFT FUEL HEAT INDICATION DURING CLIMBOUT. HAD TO PUSH LEFT ENGINE THROTTLE UP TO KEEP OIL TEMP LESS THAN 135 DEGREES AND FUEL HEAT WOULD NOT GO OFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL HEAT VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 58,556 hrs · 29,922 cycles

DFW - CREW REPORTED MULTI BIRD STRIKES TO RADOME, WINGS AND POSSIBLE ENGINE INGESTION. NO VIBRATIONS OR ENGINE INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED DFE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SEVRICE. REPLACED RADOME. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — FAULTY (FUEL HEAT) · airframe 58,030 hrs · 29,641 cycles

DFW - CREW REPORTED BOTH FUEL HEAT LIGHTS FLICKERED MULTIPLE TIMES AND FUEL TEMPERATURE KEPT RISING TO 55C. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AND LEFT ENGINE FUEL HEAT VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

DENT IN FUSELAGE SKIN 1 INCH BY 1.5 INCH BY .063 AT STATION 210 STRINGER 15 LEFT WITHIN SRM 53-04-00 LIMITS. INSTALLED DOUBLER PER AARD 53-30-00-9 AND SRM 53-04-00 FIGURE 12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

FIRST OFFICERS OUTBOARD SEAT TRACK IS CORRODED. INSTALLED FIRST OFFICERS OUTBOARD AFT SEAT TRACK PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

FORWARD CARGO - BOTTOM SURFACE OF RIGHT CUSP IS CORRODED STATIONS 503 TO 513. INSTALLED NEW DOUBLER AT RIGHT STATIONS 503 TO 522 CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

CABIN HAS CORROSION IN SUB FLOOR WEBBING OUTBOARD OF AFT SERVICE DOOR AFT GIRT BAR SUPPORT BRACKET. INSTALLED CUSP SPLICE REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

FORWARD CARGO - BOTTOM SURFACE OF RIGHT CUSP IS CORRODED STATIONS 503 TO 513. INSTALLED NEW DOUBLER REPAIR AT RIGHT STATIONS 503 TO 522 CUSP PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

INTERCOSTAL CRACKED JUST RIGHT OF CENTER STATIONS 1287 TO 1309 BETWEEN CABIN FLOORBEAMS. INSTALLED NEW INTERCOSTAL AT STATIONS 1287 TO 1309 PER SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

DOOR BEAM HAS CORROSION STATIONS 1155 TO 1211. INSTALLED DOUBLERS ON AFT CARGO DOOR BEAM PER AARD 53-10-00-3 AND EA MD80-013913.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

CRACKED INTERCOSTAL STATIONS 1322 TO 1309 BETWEEN LONGERONS 28 LEFT AND 27 LEFT. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-02 AND SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

FORWARD SERVICE DOOR AREA: CRACKS IN CUSP SHEET UNDER SEAT TRACK NUMBER 6 AT STATION 219 (MARKED). INSTALLED RIGHT CUSP SHEET STATIONS 218 TO 237 PER AARD 51-10-00-5 AND BOEING DRAWING 9930538.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

LEFT SIDE CABIN UPPER CUSP IS CRACKED AT STATION 1263. INSTALLED NEW CUSP SHEET STATIONS 1250 TO 1309 LEFT SIDE PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

RIGHT SIDE CUSP SHEET CORROSION OUT OF LIMITS STATIONS 598 TO 712. INSTALLED NEW CUSP SHEET STATIONS 598 TO 712 RIGHT SIDE AS PER BOEING DRAWING NUMBER 9930538 AND AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

FORWARD OUTBOARD G1 GALLEY MOUNT IS CORRODED. REMOVED AND REPLACED FORWARD OUTBOARD G1 GALLEY MOUNT PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

LEFT CUSP CORRODED AT STATIONS 877 TO 878. INSTALLED CUSP DOUBLER PER AARD 53-20- 00-16.

Part: SKIN — PUNCTURED (RUDDER) · airframe 57,198 hrs · 29,168 cycles

RUDDER HAS SMALL PUNCTURE IN RIGHT SKIN AT TOP NEAR LEADING EDGE. TRIMMED OUT DAMAGED AREA AND APPLIED A WET LAYUP PERMANENT REPAIR PER SRM 51-70-01A.

Part: FITTING — CORRODED (DOOR) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

AFT LOWER CORNER DOOR FITTING AT STATION 1212 CORRODED. REMOVED AND REPLACED AFT LOWER DOOR FITTING PER SRM 51-30-05.

Part: SKIN — DENTED (CARGO DOOR) · airframe 57,198 hrs · 29,168 cycles

AFT CARGO DOOR OUTER SKIN HAS 3 EACH DENTS WITH LESS THAN 3 INCHES BETWEEN THEM, LOCATED CENTER OF UPPER DOOR BETWEEN NUMBER 40 BEAMS. FABRICATED AND INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38.

Part: SKIN — DAMAGED (TE FLAP) · airframe 57,198 hrs · 29,168 cycles

A 3 BY 3 BY .095 DEPTH DENT ON LOWER SURFACE OF INBOARD RIGHT FLAP 20 INCHES FORWARD OF TRAILING EDGE AND 31 INCHES OUTBOARD OF INBOARD EDGE. INBOARD RIGHT FLAP REPLACED DAMAGED LOWER SKIN WITH NEW SKIN AS PER ESO 80095 IAW SRM 57-50-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,198 hrs · 29,168 cycles

CABIN NUMBER 4 SEAT TRACK CORRODED STATIONS 1275 TO 1280. ROUTED OUT DAMAGED AREA PER SRM 53-05-00,AARD 53-20-00. VERIFIED MATERIAL PLUG DDK2704-7, CHANNEL 7452952-7 PER SRM 53-05-00, AARD 53-20-00 AND INSTALLED SEAT TRACK PLUG PER SRM 53-05-00.

Part: PAN — CRACKED (WINDOW) · airframe 57,198 hrs · 29,168 cycles

STATION 788 RIGHT SIDE WINDOW PAN CRACKED AT FORWARD LOWER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,198 hrs · 29,168 cycles

STATION 1022 RIGHT SIDE WINDOW PAN CRACKED AFT UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,198 hrs · 29,168 cycles

STATION 886 RIGHT SIDE WINDOW PAN CRACKED AT FORWARD UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,198 hrs · 29,168 cycles

WINDOW PAN CRACKED FORWARD TOP CORNER LEFTSIDE STATION 845. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,198 hrs · 29,168 cycles

SEAT TRACK NR 6 DAMAGED. REMOVED DAMAGE AND INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: PAN — CRACKED (WINDOW) · airframe 57,198 hrs · 29,168 cycles

WINDOW PAN CRACKED FORWARD OF CORNER LEFT SIDE OF AIR CONDITIONING STATION 886. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,907 hrs · 28,992 cycles

EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. OPS CHECK NORMAL.

Part: GCU — INOPERATIVE (RIGHT) · airframe 56,676 hrs · 28,871 cycles

MEM - CREW REPORTED RIGHT GENERATOR FAILED ALONG WITH CROSS TIE LOCK-OUT DURING APPROACH. EMERGENCY DECLARED LANDED MEM WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,016 hrs · 28,519 cycles

EMERGENCY LIGHTS AT ROW 32 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 32. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,016 hrs · 28,519 cycles

CEILING EGRESS LIGHTS AT ROWS 22 TO 25 INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AT ROW 25DEF. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,825 hrs · 28,428 cycles

LEFT AND RIGHT OVERWING INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING INTERIOR EMERGENCY EXIT LIGHTS. OPS CHECKED NORMAL.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 54,428 hrs · 27,687 cycles

INFLIGHT DFW TO MEX. CREW REPORTED CABIN ALTITUDE CLIMBED TO 10,000 FEET. PASSENGER OXYGEN MASKS DID NOT DEPLOY. INITIATED RAPID DESCENT PROCEDURES. LANDED AUS WITHOUT INCIDENT. BITE CHECK OF NUMBER 2 AUTO PRESSURE CONTROLLER INDICATED FAILURE OF THE OUTFLOW VALVE ACTUATOR. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — FAILED (CABIN) · airframe 54,185 hrs · 27,547 cycles

EMERGENCY LIGHT CHARGER FAILED TEST AT OVERHEAD BIN 20. REMOVED AND REPLACED CHARGER AT BIN 20. OPS NORMAL.

Part: BATTERY — LOOSE (CABIN) · airframe 54,185 hrs · 27,547 cycles

EMERGENCY LIGHTS OVER THE TWO REAR OVERWING EXIT ARE INOPERATIVE. RESEATED BATTERY AND OPS IS NORMAL.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,185 hrs · 27,547 cycles

EMERGENCY LIGHT BATTERY PACK AT BIN 20 FAILED TEST. REMOVED AND REPLACED LOWER BATTERY AT BIN 20. OPS NORMAL.

Part: SILL — DIRTY (FUSELAGE) · airframe 54,106 hrs · 27,507 cycles

DFW - CREW REPORTED AIRCRAFT UNABLE TO PRESSURIZE AND A LOUD RUSH OF AIR WAS HEARD NEAR AFT GALLEY DOOR. RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED DEBRIS AND CLEANED AND LUBED ALL DOOR SILLS. PRESSURIZED AIRCRAFT AND NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,628 hrs · 27,253 cycles

FORWARD LEFT AND RIGHT EMERGENCY LIGHTS WILL NOT ILLUMINATE.

Part: SENSE LINE — LOOSE (A/C PACKS) · airframe 53,547 hrs · 27,204 cycles

AMA - INFLIGHT ABQ-DFW. AIRCRAFT LOST PRESSURIZATION, MASKS DID NOT DROP. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AIR CONDITIONING PILOT PRESSURE REGULATOR SENSE LINE LOOSE AT RIGHT A/C PACK. RE-SECURED SENSE LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (ZONE 200)

DFW - THE FORWARD CABIN PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY FOR THE FORWARD CABIN PORTABLE EMERGENCY LIGHT.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 24D CRACKED. REPLACED SHROUD AT SEAT 24D.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 25D CRACKED. REPLACED SHROUD AT SEAT 25D.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - BOTTOM LAMP IN THE FORWARD SEAT EMERGENCY PATH LIGHTING AT SEAT 28D INOPERATIVE. REPLACED LAMP AT THE BOTTOM POSITION IN THE FORWARD SEAT EMERGENCY PATH LIGHTING AT SEAT 28D.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - SEAT EMERGENCY PATH LIGHTING AT SEAT 13D INOPERATIVE. REPLACED LAMP AT BOTTOM POSITION IN SEAT EMERGENCY PATH LIGHTING AT SEAT 13D.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 7D CRACKED. REPLACED SHROUD AT SEAT 7D.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 27D CRACKED. REPLACED SHROUD AT SEAT 27D.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - THE FORWARD CABIN EXIT MARKERS AND SEAT EMERGENCY PATH LIGHTING FROM FRONT TO ROW 19 INOPERATIVE. REPLACED THE BATTERY PACK FOR THE AB5-1 CHARGING MODULE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER LIGHT FORWARD OF RIGHT NUMBER ONE DOOR IS BROKEN. REPLACED THE LAMP AT EMERGENCY EXIT MARKER FORWARD OF RIGHT NUMBER ONE DOOR.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 28D CRACKED. REPLACED SHROUD AT SEAT 28D.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - BOTTOM LAMP IN THE FORWARD SEAT EMERGENCY PATH LIGHTING AT SEAT 21D INOPERATIVE. REPLACED LAMP AT THE BOTTOM POSITION IN THE FORWARD SEAT EMERGENCY PATH LIGHTING AT SEAT 21D.

Part: LIGHT — BROKEN (ZONE 200)

DFW - SEAT EMERGENCY PATH LIGHTING AT 10D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 10D.

Part: SHROUD — CRACKED (EMERGENCY LIGHTS)

DFW - SHROUD FOR EMERGENCY PATH LIGHTING AT SEAT 23D CRACKED. REPLACED SHROUD AT SEAT 23D.

Part: PIN — BROKEN (GALLEY DOOR)

GDL FOUND BROKEN SCREW AT AFT GALLEY DOOR LEVER MECHANISM. REPLACED PIN AT AFT GALLEY DOOR MECHANISM. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 15D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — MISROUTED (CABIN)

DFW - AFT CABIN CEILING EMERGENCY LIGHT L2 615 INOPERATIVE. FOUND POWER WIRE FOR LIGHT ASSEMBLY WIRED TO GROUND. CORRECTED POSITION OF WIRE L2615. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - AFT SEAT EMERGENCY PATH LIGHTS ON SEATS 7D, 27 AND 30 INOPERATIVE. REPLACED AFT SEAT EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHTS ON SEATS 7D, 27 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - CEILING EMERGENCY LIGHTS AT FORWARD ENTRY GALLEY AND ROWS 11 TO 17 IN CABIN INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY BS023 FOR CEILING EMERGENCY LIGHTS AT FORWARD ENTRY GALLEY AND ROWS 11 TO 17 IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

RDU FORWARD GALLEY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN BUTT SPLICE FOR WIRE TO FORWARD GALLEY SIDEWALL EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: COVER — LEAKING (BOOST PUMP)

RDU - INFLIGHT T1886/31 DURING FLIGHT FUEL SEEPING FROM LEFT INBOARD BOOST PUMP ACCESS PANEL. LANDED WITHOUT INCIDENT AT RDU. CLEANED, SEALED AND RETORQUED LEFT INBOARD BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - CEILING EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE IDENTIFIER BETWEEN FORWARD GALLEY AND FIRST CLASS ARROWS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (CABIN)

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

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UPPER BEAM OF AFT CARGO DOOR CUTOUT AT STATION 1184. REPAIRED UPPER DOOR CUTOUT BEAM PER ESO 80559. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR BEAM CORRODED STATION 1174. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-03. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP HAS CORROSION AT STATION 1261. INSTALLED REPAIR DOUBLER PER SRM 53-0 FIG 4. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

TUL - FOUND CRACK AROUND FASTENER HOLE UNDER FLOORBOARD SUPPORT STATION 170-200. REMOVED CRACK DAMAGE. INSTALLED REPAIR PER SRM 53-01 FIG 4. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND 1452 FRAME CRACKED INBOARD SIDE OF STRINGER 3R, SMALL STRAIGHT FRAME BETWEEN 1437 AND 1388. STOP DRILLED CRACK. INSTALLED DOUBLER PER AARD 53-10-00-1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AT RIGHT CUSP AREA AROUND LIGHTING HOLE BETWEEN STA 731-739. INSTALLED CUSP REPAIR AS PER AARD 53-00-00-02. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND UPPER AFT WINDOW FLANGE SHOWS EVIDENCE OF CRACK INBOARD OF FASTENER AT RADIUS STATION 1060. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 1 STATION 1234 HAS CORROSION IN BOTTOM OF TRACK. REPAIRED PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK 1 STATION 1208 HAS CORROSION IN BOTTOM OF TRACK. REPAIRED PER SRM 53-05 FIG 4A. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND RIGHT SIDE OF A/C STATION 1060 UPPER AFT OF WINDOW FRAME CRACKED. TRIMMED OUT CRACK. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — DAMAGED (AIRSTAIRS)

ORD - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT CONNECTOR. REPAIRED EMERGENCY EXIT WIRE AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — BROKEN (AFT STAIRWAY)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE AT AFT STAIRWAY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)