N9621A

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 55,477 hrs · 27,559 cycles

AIRCRAFT WAS GROUNDED. ON TAKE OFF FROM SAT NR 1 ENGINE GENERATOR DROPPED OFFLINE. CHECKLIST RAN AND RESET ATTEMPTED BUT UNSUCCESSFUL. EMERGENCY DECLARED AND AC DIVERTED TO AUS. LANDED WITHOUT INCIDENT, FLIGHT CHANGED EQUIPMENT AND CONTINUED. REPLACED LEFT ENGINE GENERATOR PER AMM 24-20-01. (SEE ALSO SDR'S: AALA201806299005 & AALA201806299009).

Part: GCU — FAILED (ZONE 100) · airframe 55,477 hrs · 27,559 cycles

AIRCRAFT WAS GROUNDED. ON TAKE OFF FROM SAT NR 1 ENGINE GENERATOR DROPPED OFFLINE. CHECKLIST RAN AND RESET ATTEMPTED BUT UNSUCCESSFUL. EMERGENCY DECLARED AND AC DIVERTED TO AUS. LANDED WITHOUT INCIDENT, FLIGHT CHANGED EQUIPMENT AND CONTINUED. REPLACED LEFT ENGINE GENERATOR CONTROL UNIT PER AMM 24-20-07. (SEE ALSO SDR #'S: AALA20180628017 & AALA201899009)

Part: GCU — FAILED (ZONE 100) · airframe 55,477 hrs · 27,559 cycles

AIRCRAFT WAS GROUNDED. AFTER STARTING APU INFLIGHT 5 MINUTES IN, THE APU GENERATOR TRIPPED OFFLINE. COUPLED WITH THE LEFT GENERATOR FAILURE IN MIC# 34440469 - WE DECLARED EMERGENCY AND LANDED IN AUS. LANDED WITHOUT INCIDENT, FLIGHT CHANGED EQUIPMENT AND CONTINUED. REPLACED APU GENERATOR CONTROL UNIT PER AMM 24-20-07. (SEE ALSO SDR #'S: AALA20180628017 & AALA201806299005)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,144 hrs · 27,343 cycles

EMERGENCY LIGHTS NEAR SEATS 28 THROUGH 30, AND AFT GALLEY REMAIN ILLUMINATED AFTER POWER IS REMOVED FROM AIRCRAFT. OPERATIONS TEST OF EMERGENCY LIGHTS SHOWS ROWS 8, 13, 20 AND 28 OVERHEAD AISLE LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-55-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,144 hrs · 27,343 cycles

EMERGENCY LIGHTS NEAR SEATS 28 THROUGH 30, AND AFT GALLEY REMAIN ILLUMINATED AFTER POWER IS REMOVED FROM AIRCRAFT. OPERATIONS TEST OF EMERGENCY LIGHTS SHOWS ROWS 8, 13, 20 AND 28 OVERHEAD AISLE LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-55-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,144 hrs · 27,343 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS NEAR SEATS 28 THROUGH 30, AND AFT GALLEY REMAIN ILLUMINATED AFTER POWER IS REMOVED FROM AIRCRAFT. OPERATIONS TEST OF EMERGENCY LIGHTS SHOWS ROWS 8, 13, 20 AND 28 OVERHEAD AISLE LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-55-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,144 hrs · 27,343 cycles

EMERGENCY LIGHTS NEAR SEATS 28 THROUGH 30, AND AFT GALLEY REMAIN ILLUMINATED AFTER POWER IS REMOVED FROM AIRCRAFT. OPS TESTED THE EMERGENCY LIGHTS SHOWS ROWS 8, 13, 20 AND 28 OVERHEAD AISLE LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS IAW AMM 33-55-00.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 55,012 hrs · 27,246 cycles

CAPTAIN`S L1 WINDOW DELAMINATED AND OBSCURES VISION. REPLACED THE L1 WINDOW IAW AMM 56-10-02 LK. AIRCRAFT WAS GROUNDED.

Part: WINDOW — DELAMINATED (R1) · airframe 55,012 hrs · 27,246 cycles

FIRST OFFICER`S WINDOW R1 DELAMINATED AND OBSCURES VISION. REMOVED AND REPLACED THE R1 WINDOW IAW AMM 56-10-02-201. LEAK AND OPS CHECKED OK.

Part: OIL COOLER — FAULTED · airframe 54,990 hrs · 27,231 cycles

ENROUTE, LEFT ENGINE OUTLET AND RISE WENT TO FULL SCALE HIGH. DISCONNECTED CONSTANT SPEED DRIVE. NR 1 GENERATOR FAILURE AND APU WOULD NOT START. EMERGENCY WAS DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CENTRIFUGAL SWITCH ON APU AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 49-60-01. REPLACED THE CONSTANT SPEED DRIVE, OIL COOLER, AND GENERATOR IAW AMM 24-10-01, 24-10-03, AND PERFORMED SATISFACTORY OPS CHECK. AIRCRAFT WAS GROUNDED

Part: SWITCH — FAULTED · airframe 54,990 hrs · 27,231 cycles

ENROUTE TO CLE, LEFT ENGINE OUTLET AND RISE WENT TO FULL SCALE HIGH. DISCONNECTED THE CONSTANT SPEED DRIVE. NR 1 GENERATOR FAILURE AND APU WOULD NOT START. EMERGENCY WAS DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CENTRIFUGAL SWITCH ON APU AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 49-60-01. REPLACED CONSTANT SPEED DRIVE, OIL COOLER, AND GENERATOR IAW AMM 24-10-01, 24-10-03, AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: GENERATOR — FAILED (NR 1) · airframe 54,990 hrs · 27,231 cycles

ENROUTE, LEFT ENGINE OUTLET AND RISE WENT TO FULL SCALE HIGH-DISCONNECTED CONSTANT SPEED DRIVE. NR 1 GENERATOR FAILURE AND APU WOULD NOT START. EMERGENCY WAS DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CENTRIFUGAL SWITCH ON APU AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 49-60-01. REPLACED THE CONSTANT SPEED DRIVE, OIL COOLER, AND GENERATOR IAW AMM 24-10-01, 24-10-03, AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: STRAP — BROKEN (AFT FLASHLIGHT) · airframe 54,949 hrs · 27,207 cycles

FLASHLIGHT IN THE AFT CABIN BY L4 DOOR WILL NOT STAY MOUNTED. STRAP IS BROKEN. REPLACED THE AFT FLASHLIGHT HOLDER AND LIGHT ASSEMBLY IAW AMM 25-60-00.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 54,550 hrs · 26,960 cycles

R1 DOOR SLIDE GIRT FLAP IS NOT FOLDED CORRECTLY. REPLACED R1 DOOR SLIDE IAW MCM 25-94-20.

Part: GUST LOCK — BENT (L2 DOOR) · airframe 54,427 hrs · 26,888 cycles

FORWARD ENTRY DOOR GUST LOCK FOUND BENT, AND WILL NOT LOCK INTO SLOT. HITS FUSELAGE. REPLACED GUST LOCK IAW AMM 52-11-00.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 54,067 hrs · 26,650 cycles

AIRCRAFT NOT GROUNDED. REAR GALLEY SERVICE DOOR ESCAPE SLIDE DIFFICULT TO ARM. THERE IS RESISTANCE BETWEEN GIRT BAR AND SLIDE ACTUATION LANYARD. LANYARD IS NOT FULLY STOWED. REPLACED L2 SERVICE DOOR SLIDE PER AMM 25-62-00.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 54,062 hrs · 26,647 cycles

AIRCRAFT WAS GROUNDED. FIRST OFFICER'S SLIDING WINDOW IS DIFFICULT TO LOCK AND UNLOCK WHEN OPEN. ADJUSTED CLEARVIEW WINDOW PER AMM 56-10-03 AND PERFORMED LUBRICATION PER AMM 12-21-03. OPERATIONAL CHECK GOOD.

Part: CHANNEL — CRACKED (MLG DOOR FRAME) · airframe 53,531 hrs · 26,302 cycles

CRACK IN MAIN LANDING GEAR DOOR FRAME IN LEFT WHEEL WELL FORWARD PORTION OF WHALE BONE, EXTENDING UNDER A HYDRAULIC SERVICE LINE BRACKET. REPAIRED THE FORWARD CHANNEL IAW EA 272680A. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,258 hrs · 25,498 cycles

AIRCRAFT WAS GROUNDED. DURING PRE-TAXI WALK AROUND, MAINTENANCE NOTICED A 2 INCH CRACK ON THE LEFT AFT TAIL SECTION SKIN FUSELAGE STATION 1474 JUST LEFT OF AFT AIRSTAIRS. REPAIRED IAW SRM 53-01-00-001 AND AARD 53-30-00-4. OPERATIONAL CHECK GOOD.

Part: CABLE — DETACHED (L2 DOOR SLIDE) · airframe 52,057 hrs · 25,381 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE CABLE IS DETACHED. REMOVED AND REPLACED SLIDE IAW AMM 25-94-17. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 52,002 hrs · 25,349 cycles

AIRCRAFT NOT GROUNDED. R1 EMERGENCY EVACUATION SLIDE PACK IS DETACHED. REINSTALLED SLIDE PACK IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,812 hrs · 25,230 cycles

AIRCRAFT NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS AT ROWS 18 THROUGH 21 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY B5-104 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,812 hrs · 25,230 cycles

AIRCRAFT NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS AT ROWS 27 THROUGH 30 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY B5-107 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,812 hrs · 25,230 cycles

AIRCRAFT GROUNDED. FIRST CLASS CEILING EMERGENCY EXIT LIGHTS AT ROWS 3 THROUGH 6 STAY ON AFTER POWER DOWN SWITCH WAS IN OFF POSITION. REMOVED AND REPLACED BATTERY ASSEMBLY B5-100 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LANYARD — DETACHED (EVAC SLIDE) · airframe 51,766 hrs · 25,202 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EVACUATION SLIDE GIRT BAR LANYARD IS DETACHED. SECURED LANYARD AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 51,689 hrs · 25,158 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE LANYARD LOOSE. REINSTALLED SLIDE LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,705 hrs · 24,551 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS IN FORWARD ENTRANCE AREA ARE INOPERATIVE. R & R THE FORWARD EMERGENCY BATTERY ASSY IAW AMM 33-53-00. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,705 hrs · 24,551 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY ESCAPE PATH LIGHTING IS INOPERATIVE. EMERGENCY PATH MARKING SYS FAILS DUAL FEED TEST IN AFT PORTION OF CABIN. R & R POWER SUPPLY AND BATTERY PACK AT FUSELAGE STA 1260 IAW AMM 33-60-98. OPS CHECK GOOD, ALSO, AALA20160627002.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 50,705 hrs · 24,551 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY ESCAPE PATH LIGHTING IS INOPERATIVE. EMERGENCY PATH MARKING SYS FAILS DUAL FEED TEST IN AFT PORTION OF CABIN. R & R POWER SUPPLY AND BATTERY PACK AT FUSELAGE STA 1260 IAW AMM 33-60-98. OPS CHECK GOOD. ALSO AALA20160627003.

Part: PUMP — INOPERATIVE (FWD BOOST)

DURING CLIMB, THE CENTER TANK AFT BOOST PUMP BECAME INOPERATIVE. EMERGENCY WAS DECLARED. LANDING UNEVENTFUL. REMOVED AND REPLACED THE CENTER TANK FORWARD FUEL BOOST PUMP AND AFT FUEL BOOST PUMP IAW AMM 28-20-07-201. OPERATIONAL CHECKED GOOD.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 50,411 hrs · 24,380 cycles

DURING CLIMB THE CTR TANK AFT BOOST PUMP BECAME INOPERATIVE. EMERGENCY WAS DECLARED, LANDING UNEVENTFUL. REMOVED AND REPLACED THE CENTER TANK FORWARD FUEL BOOST PUMP AND AFT FUEL BOOST PUMP IAW AMM 28-20-07-201. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,252 hrs · 24,279 cycles

AIRCRAFT WAS NOT GNDED. OVERHEAD EMER LIGHT IN FIRST CLASS ARE INOPERATIVE. R & R EMER BATTERY ASSEMBLY IAW AMM 33-53-00.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 50,081 hrs · 24,177 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO COMPARTMENT DOOR STOP PAD SUPPORT FITTING, 3RD FROM TOP ON FWD EDGE, IS CRACKED. R & R FITTING IAW AARD 51-00-05-1 & DWGS CDK2345 & 5910141.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,081 hrs · 24,177 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED AT STATION 1380 & LONGERON 14R. REPAIRED SKIN IAW SRM 53-01-00-001 & AARD 53-30-00-02;.

Part: FITTING — CRACKED (RT SPOILER) · airframe 50,081 hrs · 24,177 cycles

AIRCRAFT WAS IN BASE MX. RT GND SPOILER ACTUATOR FITTING IS CRACKED AT FWD INBD & OTBD END. R & R ACTUATOR FITTING IAW SRM 51-01-00-001.

Part: ENGINE — LEAKING (NR 1) · airframe 47,834 hrs · 22,866 cycles

DURING CLIMB OUT AT FL 300, FLIGHT ATTENDANTS & PILOTS SMELLED BURNING FUMES. FLIGHT ATTENDANTS REPORTED FUMES WERE STRONGEST FROM ROW 23 FWD. FOUND OIL ON NR 1 ENGINE 6TH STAGE FAN BLADES. R & R NR 1 ENGINE IAW MCM 71-91-9.

Part: TRIM MOTOR — FAULTY (ZONE 300) · airframe 47,323 hrs · 22,568 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CREW REPORTED STABILIZER TRIM WOULD NOT WORK WITH THUMB OR LONG TRIM HANDLE. STABILIZER TRIM WORKED IN ALTERNATE & ALSO WITH AUTO PILOT. R & R MAIN STABILIZER TRIM MOTOR IAW CARD 27-94-15 17472.

Part: FMC — INOPERATIVE (ZONE 100) · airframe 46,938 hrs · 22,365 cycles

AIR INTERRUPT, RETURNED FOR LOST HEADING & NAVIGATION DATA. EMER NOT DECLARED, LANDED UNEVENTFULLY & WAS NOT OVERWEIGHT. REPLACED FMC & ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. PERFORMED REQUIRED TEST IAW AMM 34-63-03. ACCOMPLISHED MCDU OPERATIONS TEST IAW AMM 34-63-04. ALL TEST PASSED.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

CRACKED WEB FASTENER HOLE, UPPER LT SIDE OF STATION 1485 CANT IN THE AFT ACCESSORY COMPARTMENT. INSTALLED REPAIR DOUBLER ON WEB AT STATION 1485 CANT IN THE AFT ACCESSORY COMPARTMENT IAW AARD51-10-00-32.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

NUMBER 6 SEAT TRACK CORRODED BETWEEN FS 934 & 938. REPAIRED SEAT TRACK IAW SRM 53-05-00-001.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

LEFT SHELF BRACKET ON AFT SIDE OF FS 37 BULKHEAD IS CRACKED. R & R SHELF BRACKET IAW AARD 51-00-05-1 & DWG 9911500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

NUMBER 6 SEAT TRACK CORRODED BETWEEN FS 216 & 588. R & R SEAT TRACK IAW AMM 53-40-01-2 & SRM 51-30-01.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK SPLICE PART 5936660-91AT FS 1220 IS CORRODED. R & R SPLICE PART IAW AARD 51-00-05-1 & IPC 25-52-00-03L.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

CORROSION ON RT CUSP BETWEEN FUSELAGE STATIONS 313 & 389 UNDER SEAT TRACK NR 6. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK SPLICE PART 5936660-93 AT FS 1220 IS CORRODED. R & R SPLICE PART IAW AARD 51-00-05-1 & IPC 25-52-00-03L.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK SPLICE PART 5936660-95 AT FS 1220 IS CORRODED. R & R SPLICE PART IAW AARD 51-00-05-1 & IPC 25-52-00-03L.

Part: SKIN — GOUGED (APU BAY) · airframe 46,735 hrs · 22,245 cycles

APU ENCLOSURE HAS DEEP GOUGE IN UPPER SKIN 6 INCHES FROM OTBD END. REPAIR ENCLOSURE IAW AARD 53-20-00-11 REPAIR 11.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 46,735 hrs · 22,245 cycles

AFT CARGO DOOR HAS PITTING ON SKIN LOWER FOOT ALL THE WAY ACROSS. R & R AFT CARGO DOOR SKIN IAW ESO 0174601E.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CRACKED BETWEEN FUSELAGE STATIONS 1287 & 1309 AT BL 0. R & R INTERCOSTAL IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

CORROSION ON RT CUSP BETWEEN FUSELAGE STATIONS 256 & 275. REPAIRED CUSP IAW AARD 53-20-00-16 FROM STATION 256 TO 275.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

LEFT AFT CARGO TIE DOWN TRACK CORRODED BETWEEN FUSELAGE STATIONS 1212 & 1322 AT STRINGER 27 LT. R & R TRACK IAW AARD 51-00-05-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

SHEAR TIE CRACKED AT FUSELAGE STATION 1437 & LONGERON 3 RT. R & R SHEAR TIE IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

CORROSION ON NR 4 SEAT TRACK BETWEEN FUSELAGE STATION 1260 & 1309. REMOVED TRACK SECTION FROM STATION 1260 TO 1309. INSTALLED NEW SERVICEABLE SEAT TRACK SECTION IAW SRM 53-05-00-001 FIG 4F & AMM 53-40-01-2.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

DAMAGE TO RT CUSP AT FUSELAGE STATION 237. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

SHEAR TIE CRACKED AT FUSELAGE STATION 1437 & LONGERON 3 LT. R & R SHEAR TIE IAW AARD 51-00-05-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

CRACKED SHEAR TIE AT FUSELAGE STATION 1451 & LONGERON 3 LT. R & R SHEAR TIE IAW AARD 51-00-05-1 & SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

SEAT TRACK NR 6 REWORK AREA BETWEEN FUSELAGE STATIONS 893 & 897 IS OUT OF LIMITS. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

SEAT TRACK NR 6 REWORK AREA BETWEEN FUSELAGE STATIONS 855 & 858 IS OUT OF LIMITS. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

SEAT TRACK NR 4 AT FUSELAGE STATION 946 WORN BEYOND LIMITS. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

AFT CARGO COMPARTMENT LT TIE DOWN TRACK CORRODED BETWEEN FS 1136 & 1212. R & R TRACK IAW EA MD 80-53-037439 DATED 11/17/2014.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

FIRST OFFICER`S OTBD SEAT TRACK IS CORRODED BETWEEN FS 142.55 & 147.55. REPAIRED TRACK IAW SRM 51-70-05 FIG 2.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

G1 GALLEY OTBD MOUNT AT FWD END OF NR 6 SEAT TRACK IS CORRODED OUT OF LIMITS. R & R MOUNT IAW AARD 51-00-05-1.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 46,735 hrs · 22,245 cycles

FORWARD AIRSTAIRS SUPPORT ANGLE IS CRACKED AT THE TOP FASTENER, FUSELAGE STATION 160 LT JUST INSIDE STAIR ACCESS DOOR. CRACK IS 3 INCHES LONG FROM BOTTOM OF FASTENER HOLE. R & R SUPPORT ANGLE IAW SRM 51-00-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,735 hrs · 22,245 cycles

G2 GALLEY TIE DOWN MOUNT, SUPPORT, CORRODED 10 INCHES INBD OF NR 4 SEAT TRACK AT FUSELAGE STATION 210. R & R MOUNT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,193 hrs · 21,466 cycles

EMERGENCY PATH LIGHT ON SEAT 25D INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT ON SEAT 25D. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 44,334 hrs · 21,028 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FAILED TO TEST. REPLACED LT NR 1 DOOR PORTABLE EMERGENCY FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 44,075 hrs · 20,885 cycles

DFW CREW REPORTED MID CARGO FIRE ALARM & MID CARGO FAULT INTERMITTENTLY CAME ON & OFF. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED A & B CARGO SMOKE DETECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: COUPLING — DETACHED (ANTI-SKID SYS) · airframe 43,519 hrs · 20,556 cycles

DFW CREW REPORTED WHEEL NOT TURNING LIGHT ILLUMINATED. TAKEOFF ROLL WAS DISCONTINUED & AIRCRAFT RETURNED TO GATE. FOUND NR 2 MAIN ANTI-SKID TRANSDUCER DRIVE COUPLING PINS DETACHED. REATTACHED & SECURED ANTISKID DRIVE COUPLING PINS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 41,904 hrs · 19,675 cycles

PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (ZONE 200) · airframe 41,904 hrs · 19,675 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOP. RESEATED BATTERY, OPS CHECK GOOD.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 41,904 hrs · 19,675 cycles

RIGHT AND CENTER EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERY PACK FOR RIGHT AND CENTER EMERGENCY LIGHTS. OPS CHECK NORMA.L

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,091 hrs · 19,282 cycles

TWO OVERWING EXIT EMERGENCY LIGHT SIGNS INOPERATIVE. REPLACED BATTERY PACK AT ROW 21. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,974 hrs · 19,219 cycles

EMERGENCY LIGHT L245 FAILED TO ILLUMINATE. REPLACED LAMP FOR EMERGENCY LIGHT L245. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,974 hrs · 19,219 cycles

EMERGENCY LIGHT L246 FAILED TO ILLUMINATE. REPLACED LAMP FOR EMERGENCY LIGHT L246. OPS CHECK NORMAL.

Part: CSD — FAILED (LT ENGINE) · airframe 37,335 hrs · 17,351 cycles

LAS - CREW REPORTED LEFT ENGINE CONSTANT SPEED DRIVE TEMPERATURE ROSE INTO RED ZONE. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,505 hrs · 16,476 cycles

EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,505 hrs · 16,476 cycles

EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,505 hrs · 16,476 cycles

EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

DENT OVER SHEAR TIE AT STATION 1309, BETWEEN LONGERON 23 AND LONGERON 24, LEFT SIDE OF FUSELAGE. INSTALLED INTERNAL DOUBLER AS PER SRM 53-04-00 AND EA MD80-53-012815 AND THE SHEAR TIE REPAIR WAS DONE AS PER SRM 53-03 FIGURE 45 AND EA MD80-53-012815.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

AFT ACCESSORY STATION 1418 FRAME CRACKED LONGERON 2 RIGHT. INSTALLED REPAIR DOUBLER ON FORWARD SIDE OF FRAME STATION 1418 LONGERON 2 RIGHT PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

LEFT CUSP SHEET STATION 1098 TO STATION 1174 HAS CORROSION. INSTALLED NEW LEFT CUSP SHEET STATION 1098 TO STATION 1174 PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

AFT ACCESSORY LONGERON 2 RIGHT CRACKED AFT OF STA 1418. INSTALLED SPLICE REPAIR AT STATION 1418 LONGERON 2 RIGHT PER AARD 53-30-00-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

CORROSION ON SUBFLOOR AT STATION 200 BELOW FORWARD END OF FIBERGLASS SUPPORT NUMBER 6 SEAT TRACK. INSTALLED CUSP DOUBLER FROM STATION 200 TO STATION 218 PER AARD53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

AFT ACCESSORY LONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED LONGERON REPAIR SPLICE AT STATION 1418 LONGERON 2 LEFT PER ARRD 53-30-00-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

AFT ACCESSORY FRAME CRACKED AT STATION 1418 LONGERON 2 LEFT. INSTALLED DOUBLER REPAIRS ON FORWARD AND AFT SIDE OF FRAME 1418 AT LONGERON 2 LEFT PER AARD 53-10-00-15 AND SRM 53-03-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

CORROSION REMOVAL AT SEAT TRACK NUMBER 2 IS OUT OF LIMITS. INSTALLED NEW SECTION OF NUMBER 2 SEAT TRACK STATION 1089 TO 1184 PER AARD 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

CORROSION OUT OF LIMITS AT STATIONS 680 TO 690 ON RIGHT CUSP. INSTALLED DOUBLER ON RIGHT CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

RIGHT CUSP STATION 683 HAS TOOLING MARKS. INSTALLED DOUBLER PER EA MD8053-012663.

Part: STRAP — GOUGED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

FRAME STRAP AT LEFT CUSP STATION 1136 GOUGED OUT OF LIMITS. REPLACED STRAP PER SRM 51-30-05.

Part: STRAP — GOUGED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

FRAME STRAP AT LEFT CUSP STATION 1127 FOUND GOUGED OUT OF LIMITS. REPLACED STRAP PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,857 hrs · 16,170 cycles

CORROSION BEYOND LIMIT RIGHT CUSP AT STATION 488 TO 489. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

FORWARD CARGO RIGHT TIE DOWN TRACK HAS CORROSION AROUND FLOOR AND SIDEWALL PANEL ATTACH HOLES AFT OF DOOR OPENING. TIE DOWN TRACK BLENDED BEYOND MANUAL LIMITS AT STATIONS 434 TO 446 PER SRM 53-01-00. INSTALLED REPAIR STRAP PER AARD 53-20-00-13.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

CORROSION FOUND OUT OF LIMITS LEFT CUSP AT STATIONS 454 TO 462 OUTBOARD LIGHTENING HOLES. CUT OUT DAMAGE AND INSTALLED DOUBLER ON CUSP PER AARD53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

INBOARD OF NUMBER 5 SEAT TRACK AT STATION 200 CORROSION ON SUBFLOOR. CUT OUT DAMAGED AREA OF CUSP AND INSTALLED NEW CUSP DOUBLER PER AARD53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 34,857 hrs · 16,170 cycles

NUMBER 5 SLAT 2ND FROM OUTBOARD END SLAT RIB IS CRACKED. REPLACED DAMAGED NUMBER 14 2ND FROM OUTBOARD RIB PER IAW ESO 89117 27-80-1.

Part: RIB — CRACKED (LE SLAT) · airframe 34,857 hrs · 16,170 cycles

NUMBER 5 SLAT OUTBOARD SLAT RIB IS CRACKED. REPLACED NUMBER 15 OUTBOARD RIGHT RIB PER IAW ESO 80117 27-80-01.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,857 hrs · 16,170 cycles

STATION 207, 12 INCHES OF NUMBER 4 SEAT TRACK MOUNT IS CORRODED. INSTALLED NEW MOUNT SRM 51-01-00.

Part: TEE FITTING — LEAKING (HYDRAULIC SYS) · airframe 34,514 hrs · 16,001 cycles

SEA - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT. EMERGENCY DECLARED RETURNED SEA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND TEE FITTING IN TAIL COMPARTMENT LEAKING. REPLACED TEE FITTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRACKET — CRACKED (DOOR) · airframe 30,656 hrs · 14,206 cycles

CRACK AT MIDDLE STOP PAD BRACKET FORWARD SIDE. REPLACED BRACKET PER ESO 80174.

Part: BRACKET — CRACKED (DOOR) · airframe 30,656 hrs · 14,206 cycles

CRACK AT STOP PAD BRACKET TOP, FORWARD SIDE. REPLACED BRACKET PER ESO 80174.

Part: FORMER — DAMAGED (FUSELAGE) · airframe 30,539 hrs

LGA - FORMER AT STATION 485 DAMAGED. REPLACED FORMER AT LOCATION 485. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: START VALVE — FAILED (NR 2 ENGINE) · airframe 29,791 hrs

INFLIGHT ORD TO LAX - RIGHT START VALVE OPEN INDICATION ILLUMINATED AT FL300. REDUCED NUMBER TWO ENGINE TO IDLE. LIGHT FLICKERED ON AND OFF THROUGH DESCENT AND LANDING. LANDED MCI WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE START VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CSD — FAILED (NR 2 ENGINE) · 29,383 cycles

INFLIGHT T870/30SEP. BUR TO DFW. CREW REPORTED DISCONNECTION OF NR 2 ENGINE GENERATOR DUE TO HIGH CONSTANT SPEED DRIVE OIL PRESSURE. AUXILIARY POWER UNIT ALSO HAD TO BE SHUT DOWN DUE TO LOW OIL PRESSURE. LANDED LAS WITHOUT INCIDENT. REPLACED NR 2 ENGINE CONSTANT SPEED DRIVE CSD, GENERATOR AND OIL COOLER. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,846 hrs

AUX OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT BS 106 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,846 hrs

AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 103 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,846 hrs

AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 102 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,846 hrs

AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,846 hrs

AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 105 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,846 hrs

AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 104 FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,047 hrs

LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ELECTRONIC BAY FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 27,912 hrs

SFO - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE)

DURING CRUISE EXPERIENCED CABIN PRESSURE LOSS AND MASKS DEPLOYED. LANDED ELP WITHOUT INCIDENT. REPLACED AFT CABIN PRESSURE SAFETY VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (L2 DOOR)

LGA LEFT 2 DOOR SLIDE WAS NOT DISARMED AND CATERING OPENED DOOR. SLIDE EXTENDED BUT DID NOT INFLATE. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — BROKEN (EMERGENCY LIGHT)

AUS - B5-27 BATTERY PACK HAS A BROKEN CIRCUIT BOARD WHITE PLASTIC MOUNT ARM. REPLACED B5-27 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (LEFT)

DFW T1357/26 EN ROUTE DFW-TUS LEFT HAND ENGINE LOW OIL PRESSURE. CREW REDUCED POWER OF ENGINE TO IDLE. LANDED ELP WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD OVERHEAD EMERGENCY AISLE LIGHT INOPERATIVE ON AFT AISLE GANGWAY. REPAIRED QUICK DISCONNECT ASSEMBLY FOR FORWARD OVERHEAD EMERGENCY AISLE LIGHT IN AFT AISLE GANGWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,999 hrs · 6,494 cycles

THE EMERGENCY EXIT SIGNS ABOVE BOTH AFT OVERWING DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 12,165 hrs · 5,980 cycles

DURING CHECK-C MAINT THE FWD SUPPORT STRUCTURE FOR THE LT MAIN GEAR WELL DOOR SEAL WAS CRACKED APPROXIMATELY 36 INCHES FROM KEEL BEAM. INSTALLED NEW CHANNEL PER PRINT 5930584 AND SRM 51-30-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,165 hrs · 5,980 cycles

DURING CHECK-C MAINT THE FWD SUPPORT STRUCTURE FOR LT MAIN GEAR WELL DOOR SEAL WAS CRACKED AT INBD KEEL BEAM END, STA 946. INSTALLED NEW ANGLE PER SRM 51-30-0.

Part: LONGERON — SEVERED (FUSELAGE) · airframe 12,165 hrs · 5,980 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT, LONGERON 30 WAS FOUND SEVERED AT STA 1219. REPLACED LONGERON PER SPM 6-70-01.

Part: CAP — LEAKING (APU) · airframe 12,110 hrs · 5,942 cycles

FUEL SMELL IN AIRCRAFT CABIN. REMOVED AND REPLACED LEAKING RUBBER CAP ON ATOMIZER IN APU COMBUSTION CHAMBER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,865 hrs · 5,788 cycles

THE FORWARD OVERWING EMERGENCY EXIT LIGHTS, EGRESS LIGHTS AT ROW 17 TO 20, AND FIVE OTHER INDIVIDUAL EGRESS LIGHTS, WERE INOPERATIVE. REPLACED THE BATTERY PACK (P/N 5822-2) FOR THE EMERGENCY LIGHTS, REPLACED THE WIRE HARNESS (P/N 0105606-003SMI) BETWEEN ROW 17 AND 18 AND INSTALLED FIVE LAMPS (P/N 7732) THAT HAD FALLEN OUT.

Part: MODULE — MISSING (CABIN) · airframe 9,072 hrs · 4,350 cycles

AT CABIN ROW 22 TWO RED EGRESS LIGHT LENSES AND A LIGHT MODULE WERE MISSING. REPLACED THE LENSES P/N 0105607-310, AND THE LIGHT MODULE. CHECK-C 6-3-00 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,303 hrs · 3,486 cycles

THE PORTABLE HANDHELD EMERGENCY LIGHT WAS INOPERATIVE AT THE LT SIDE MOST FORWARD CABIN DOOR. REPLACED THE LIGHT ASSEMBLY. CHECK-C 6-3-00 STL.

Part: LENS — CRACKED (CABIN) · airframe 6,993 hrs · 3,348 cycles

RED- CLEAR LENS COVER ON EGRESS LIGHTING IS CRACKED. AC 6-30-00 STL - CLOSED 7-27-2000 STL.

Part: SKIN — SCRATCHED (BS 439)

ON LT FUSELAGE FOUND DENT AND SCRATCH AT LONGERON 21, STA 439 TO 470, 1.5 INCH WIDE BY 36 INCH LONG AND .070 DEEP, PARALLEL TO LONGERON. FABRICATED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-04, FIG 12B, PG 39. ENGR CONCURRENCE A3250800082 AND A3250800087. ----CLOSED-----