N9625W

Part: GIRT BAR — OBSTRUCTED (L1 DOOR SLIDE) · airframe 54,300 hrs · 26,835 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ESCAPE SLIDE WAS DIFFICULT TO ARM, RIGHT SIDE DIFFICULT TO INSERT. REMOVED DEBRIS FROM GIRT BAR INSERT AND ACCOMPLISHED SATISFACTORY OPERATIONS CHECK.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 54,234 hrs · 26,792 cycles

FLIGHT ATTENDANT FLASHLIGHT IS NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: DUCT — DAMAGED (RT ACM) · airframe 54,074 hrs · 26,680 cycles

INTERMITTENT FLUTTER IN THE AIR-CONDITIONING AND PRESSURIZATION SYSTEM FOLLOWED BY PRESSURIZATION FLOW LIGHT. EMERGENCY DECLARED, RETURNED TO DEPARTURE LANDING UNEVENTFUL. REMOVED AND REPLACED TURBINE COOLING OUTLET DUCT AND ADJACENT FORWARD BOOT ON THE RIGHT ACM IAW AMM 21-20-15. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BOOT — FAILED (RT ACM) · airframe 54,074 hrs · 26,680 cycles

INTERMITTENT FLUTTER IN THE AIR-CONDITIONING AND PRESSURIZATION SYSTEM FOLLOWED BY PRESSURIZATION FLOW LIGHT. EMERGENCY DECLARED, RETURNED TO DEPARTURE LANDING UNEVENTFUL. REMOVED AND REPLACED TURBINE COOLING OUTLET DUCT AND ADJACENT FORWARD BOOT ON THE RIGHT ACM IAW AMM 21-20-15. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: MEGAPHONE — BROKEN (CABIN) · airframe 53,861 hrs · 26,545 cycles

AIRCRAFT WAS NOT GROUNDED. AFT MEGAPHONE HAS A BROKEN HANDLE. REMOVED AND REPLACED MEGAPHONE. OPERATIONAL CHECK GOOD.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 53,805 hrs · 26,511 cycles

L2 DOOR SLIDE COVER IS LOOSE. STOWED LOWER DOOR LINING. OPS CHECKED GOOD.

Part: SLIDE — LOOSE (AFT GALLEY) · airframe 53,767 hrs · 26,490 cycles

AFT GALLEY SLIDE IS LOOSE. REPOSITIONED SLIDE. OPERATIONAL CHECKED GOOD.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,748 hrs · 26,480 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE Z FOLD WILL NOT LAY PROPERLY. REMOVED AND REPLACED SLIDE ASSEMBLY PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,582 hrs · 26,382 cycles

THE AIRCRAFT WAS NOT GROUNDED. OVERWING EMERGENCY EXIT LIGHTS WON’T STAY OFF WITH SWITCH IN ARMED POSITION AND POWER ON AIRCRAFT. REMOVED & REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-00. SYS OPS CKD GOOD.

Part: COALESCER BAG — SATURATED (AC BAY) · airframe 53,492 hrs · 26,328 cycles

THE AIRCRAFT WAS GROUNDED. VERY STRONG SMELL OF DIRTY GYM SOCKS DURING TAKEOFF ROLL, SMELL DISSIPATED DURING CLIMBOUT. R&R COALESCER BAG IAW AMM 21-20-02. ACCOMPLISHED MCM CARD 21-92-12. NO ODOR PRESENT AT THIS TIME.

Part: LANYARD — DETACHED (ZONE 800) · airframe 52,438 hrs · 25,669 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE LANYARD IS DETACHED. REATTACHED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 52,416 hrs · 25,654 cycles

L2 DOOR SLIDE COVER IS LOOSE ON THE AFT LOWER EDGE. ADJUSTED THE SLIDE COVER IAW AMM 25-62-01. OPS CHECKED GOOD.

Part: SWITCH — FAULTY (ZONE 100) · airframe 51,964 hrs · 25,354 cycles

AIRCRAFT WAS GROUNDED. APU EXPERIENCED HUNG START. NO EGT RISE OBSERVED. RIGHT PACK WAS OPERATING AT THE TIME. CABIN WAS INUNDATED WITH FUEL FUMES. REMOVED AND REPLACED CENTRIFUGAL SWITCH IAW AMM 49-60-01. OPERATIONAL CHECK GOOD.

Part: FAN — ODOR (ZONE 100) · airframe 51,853 hrs · 25,282 cycles

AIRCRAFT WAS GROUNDED. THE CREW REPORTED A STRONG ELECTRICAL BURNING SMELL THROUGHOUT THE AIRCRAFT WHEN PACKS TURNED ON WITH POWER TRANSFER FROM EXTERNAL POWER TO APU. MAINTENANCE ACCOMPLISHED MCM CARD 21-96-01 AND NOTED ODOR FROM RECIRCULATION FAN. REMOVED AND REPLACED THE RECIRCULATION FAN IAW AMM 21-20-12. OPERATIONAL CHECK NORMAL.

Part: FITTING — CRACKED (SPOILER) · airframe 51,644 hrs · 25,156 cycles

RIGHT WING GROUND SPOILER FITTING CRACKED AT FORWARD OUTBOARD CORNER. REMOVED AND REPLACED CASTING IAW SRM 51-30-01-001, SRM 51-30-05-001 AND SRM 51-30-02-001.

Part: PIN — SHEARED (TRANSDUCER) · airframe 51,097 hrs · 24,781 cycles

DURING TAKE OFF ROLL THE AMBER WHEEL NOT TURNING LIGHT ILLUMINATED. TAKE OFF ABORTED AT APPROXIMATELY 60 KNOTS. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE NR 1 WHEEL TRANSDUCER PINS SHEARED. REMOVED AND REPLACED TRANSDUCER IAW AMM 32-43-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,809 hrs · 24,607 cycles

AIRCRAFT WAS NOT GNDED. LT DORSAL FIN TO FUSELAGE ATTACH ANGLE IS CRACKED IN RADIUS AT APPROX FS 1463. ACCOMPLISHED INTERIM REPAIR IAW AARD 53-10-00-2 & EA 260689.

Part: CONNECTOR — FAULTY (OIL TEMPERATURE) · airframe 50,386 hrs · 24,358 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB RT ENG OIL TEMPERATURE INCREASED TO 200 DEGREES. FOUND LOOSE WIRE & BACK SHELL ON CONNECTOR FOR TEMPERATURE SENSOR. REPLACED OIL TEMPERATURE CONNECTOR P1-812 IAW CHP 205 20-31-15.

Part: FITTING — LEAKING (HYDRAULIC SYS) · airframe 50,239 hrs · 24,275 cycles

AIRCRAFT WAS NOT GNDED. FUMES FROM PACK SYS REPORTED. FOUND SOURCE TO BE APU INGESTION OF HYD FLUID, DUE TO A LEAKING PRESS BULKHEAD TO PYLON FIRE WALL UNION FITTING. ACCOMPLISHED REPAIR TO RT ENG PRESS LINE IAW AMM 200-12-04. LEAK CHECKED GOOD. .

Part: MOTOR — FAULTY (CABIN PRESSURE) · airframe 50,018 hrs · 24,149 cycles

FLIGHT ATTENDANT REPORTS LOUD AIR NOISE & WIND AT AFT GALLEY DOOR. ACFT WOULD NOT PRESSURIZE WITH AUTO 1 & AUTO 2 OR MANUAL. THE FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. REPAIRED LEAK AT AFT ENTRY DOOR. REPLACED PRESS CONTROL AC MOTORS IAW 21-32-05 & AMM 52-42-02. THE ACFT WAS GNDED.

Part: ACTUATOR — MALFUNCTIONED (OUTFLOW VALVE) · airframe 50,007 hrs · 24,142 cycles

AIRCRAFT WOULD NOT PRESSURIZE. LEVELED ACFT AT 8000 FT & AT THAT TIME THE AFT GALLEY DOOR WARNING CAME ON. AN EMER WAS DECLARED. RETURNED FOR LANDING WITHOUT FURTHER INCIDENT. AFT GALLEY DOOR LIGHT WENT AWAY AT 3000 FT. THE ACFT WAS GNDED. REPLACED & TESTED OUTFLOW VLV ACTUATOR IAW MM 21-32-05 PARAGRAPH G H. CONTROLLERS BITE NORMAL IAW MM 22-32-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 48,025 hrs · 22,944 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 8 - 10 REMAIN ON WITH ACFT POWER OFF. R & R EMERGENCY LIGHT BATTERY PACK B5-101 IAW AMM 33-53-00 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 48,025 hrs · 22,944 cycles

AFT OVERWING EMERGENCY LIGHTS REMAIN ON WITH ACFT POWER OFF. R & R EMERGENCY LIGHT BATTERY PACK B5-105 IAW AMM 33-53-00 WITH NORMAL OPERATIONS CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,962 hrs · 22,908 cycles

WITH EMER LIGHTS SWITCH IN OFF POSITION & ACFT COMPLETELY DEPOWERED, THE TWO AFT OVERWING EXIT LIGHTS COME ON ALONG WITH SOME OTHER LIGHTS AROUND ROW 9. RESET ACFT POWER & ALLOWED BATTERIES TO CHARGE FOR 6 HOURS. SYS CHECKED NORMAL IAW MM 33-53-00.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 47,889 hrs · 22,866 cycles

HOLE & DEEP SCRATCH ON LT ELEVATOR BOTTOM SKIN INBD & FWD EDGE. INSTALLED DOUBLER REPAIR IAW SRM 51-70-06-001 AND BLENDED SCRATCHES IAW 51-07-06-001 PG 12-14.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

CRACKED SHEAR TIE AT FS 1380 BETWEEN LONGERONS 14 RT & & 13 RT. REPAIRED SHEAR TIE IAW AARD 51-10-00-20.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

RIGHT CUSP SHEET HAS CORROSION OUT OF LIMITS FROM FS 216 TO 218. INSTALLED CUSP DOUBLER FROM FS 200 - 218 IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

SKIN CRACK AT FS 1380 & LONGERON 14 LT. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 53-01-00-001 & EA MD80-53-039159 DATED 3 25 2014.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

FLOOR GALLEY MOUNT AT FS 210 & APPROX RBL 10 IS CORRODED. R & R MOUNT IAW SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

RIGHT CUSP SHEET HAS CORROSION OUT OF LIMITS AT FS 239. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

RIGHT CUSP SHEET CORRODED BETWEEN FS 642 & 683. R & R CUSP SHEET BETWEEN FS 638 - 690 IAW SRM 53-05-00-001 FIG 131A-22 & DWG 9930538.

Part: SKIN — BENT (ENTRY DOOR) · airframe 47,836 hrs · 22,837 cycles

FORWARD ENTRY DOOR EXTERNAL SKIN BENT ALONG BOTTOM OF DOOR. PERFORMED DOUBLER REPAIR IAW SRM 52-05-00-001 FIG 37.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

LONGERON 30 CORRODED AFT OF FS 1287 FRAME. REPAIRED LONGERON IAW EA 53-039116.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

VERTICAL STIFFENER ON FWD CTR SIDE OF STATION 1338 BULKHEAD, ABOVE VAULT DOOR JAMB, IS CRACKED AT UPPER END. R & R STIFFENER IAW AARD 51-10-00-5 & DWG 9915562.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

RIGHT CUSP SHEET DAMAGED AT FS 389. PERFORMED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK CORRODED BETWEEN FS 1271 & 1287 AT LONGERON 17 LT. INSTALLED NEW TRACK IAW SRM 51-30-01.

Part: SEAL DEPRESSOR — WORN (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

FORWARD CARGO, FWD DOOR CUT OUT SEAL DEPRESSOR HAS DEEP WEAR AT FS 370 & APPROX LONGERON 24 RT. REPAIRED IAW AARD 53-20-00-5 & EA 53-039055.

Part: WEB — DAMAGED (NLG WW) · airframe 47,836 hrs · 22,837 cycles

NOSE GEAR WW SIDE WEB DAMAGED. REPAIRED WEB IAW SRM 53-05-00-001.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

AFT CARGO DOOR OPENING WEB AT LONGERON 27RT IS CORRODED BETWEEN FS 1200 & 1215. R & R SECTION OF WEB IAW AARD 53-10-00-24, SRM 51-30-05 & SRM 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK IS CORRODED BETWEEN STATIONS 1212 - 1319 AT LONGERON 27 RT. R & R TRACK SECTION IAW IPC 25-52-00-03L, AARD 51-00-05-1, SRM 51-30-01 & DWG 5956705.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

CORROSION ON FLOOR SUPPORT UNDER GALLEY MOUNT AT FS 218 & RBL 10 IS OUT OF MANUAL LIMITS. INSTALLED REPAIR DOUBLER IAW SRM 51-30-02 & AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

RIGHT CUSP SHEET HAS CORROSION OUT OF LIMITS FROM FS 227 - 229. R & R CUSP SHEET FROM STATION 218 - 237 IAW AARD 51-00-05-1, DWG EDK3190, SRM 53-14-02-001 FIG 4A & DWG 9930538.

Part: FORMER — CRACKED (RT WING) · airframe 47,836 hrs · 22,837 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED DOUBLER & HAT BUSHING IAW WC 57-98-06.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 47,836 hrs · 22,837 cycles

LEFT CUSP OTBD OF NR 1 SEAT TRACK AT FS 502 HAS DAMAGE AT MOUNT HOLE. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

G2 GALLEY MOUNT AT FORWARD END OF NR 6 SEAT TRACK IS CORRODED AT FS 216. REMOVED & REPLACED GALLEY MOUNT FITTING IAW AARD 51-00-05-1. DWG 3953059.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

SEAT TRACK NR 5 CORRODED OUT OF LIMITS AT FS 225. R & R SEAT TRACK FROM STATION 200 TO 315 IAW AMM 53-40-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

CABIN CUSP SHEET CORRODED BETWEEN FS 503 & 579. R & R CUSP SHEET IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

LEFT CUSP CORRODED FROM FS 932 - 942. R & R CUSP FROM FS 905 - 946 IAW SRM 53-14-03-001 FIG 10, DWG FDK3161, DWG 9910151 & DWG 53595.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,836 hrs · 22,837 cycles

CORROSION IN LT CUSP SHEET AT FS 1174 BETWEEN 1 & 2 SEAT TRACKS INSTALLED CUSP REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: COMPUTER — INOPERATIVE (NR 2) · airframe 44,951 hrs · 21,284 cycles

RDU INFLIGHT DFW ORF CREW REPORTED AUTOPILOT & AUTO THROTTLES WOULD NOT ENGAGE & ENG ANTI-ICE FAILED. FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. REPLACED NR 2 DIGITAL FLIGHT GUIDANCE COMPUTER. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,032 hrs · 17,725 cycles

BAGGAGE CART, BLOWN BY HIGH WINDS, PUNCHED HOLE IN FUSELAGE STATION 560 LONGERONS 22 TO 23 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SG09530002 DRAWING AND SRM 53-04-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,396 hrs · 16,921 cycles

RIGHT CUSP STATIONS 864 TO 886 CORROSION OUT OF LIMITS. REPAIRED CUSP SHEET AT STATIONS 870 TO 875 PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 36,396 hrs · 16,921 cycles

AFT CARGO HAS CORROSION ON RIGHT TIE DOWN TRACK BETWEEN STATIONS 1212 TO 1320. INSTALLED NEW TIE DOWN TRACK PER AARD 51-10-00-5.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

RIGHT CUSP STATIONS 984 TO 1003 ALL 3 LIGHTNING HOLES IN BAY HAVE TOOLING MARKS BEYOND LIMITS. REMOVED DAMAGE AT STATIONS 984 TO 1003 RIGHT AND INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

ELONGATED HOLE AT AFT OUTBOARD HOLE IN FORWARD CUSP SHEET STATION 845 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

AFT ACCS LONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED SPLICE REPAIR ON LONGERON 2 LEFT AT STATION 1418 PER SRM 53-02-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

AFT CARGO HAS CORROSION ON FRAME AT STATION 1271 NEAR LONGERON 30. INSTALLED J ANGLE DOUBLER PER AARD 53-10-00-14 FIGURE 1 SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,396 hrs · 16,921 cycles

SEAT TRACK NUMBER 5 HAS CORROSION OUT OF LIMITS AT STATIONS 237 TO 239. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

RIGHT CUSP STATIONS 984 TO 1003 ALL 3 LIGHTENING HOLES IN BAY HAVE TOOLING MARKS BEYOND LIMITS. REMOVED DAMAGE AT STATIONS 984 TO 1003 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,396 hrs · 16,921 cycles

FORWARD CARGO HAS CORROSION ON LOWER DOOR JAMB PAN BETWEEN STATIONS 370 TO 427. INSTALLED LOWER DOOR PAN PER SRM 53-05-00 FIGURE 44.

Part: BEAM — CORRODED (CARGO BAY) · airframe 36,396 hrs · 16,921 cycles

HEAVY CARGO/AFT- CORROSION ON DOOR CUTOUT LOWER BEAM SEVERAL PLACES FROM STATIONS 1155 TO 1212 RIGHT LONGERON 28 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 36,396 hrs · 16,921 cycles

LONGERON 2 LEFT CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-14-04.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,396 hrs · 16,921 cycles

LEFT CUSP STATIONS 598 TO 712 HAS AREAS OF BARE METAL AND CORROSION OUT OF LIMITS. REPLACED LEFT CUSP STATIONS 598 TO 712 PER SRM 51-01-00.

Part: PAN — CRACKED (WINDOW) · airframe 36,396 hrs · 16,921 cycles

LEFT STATION 1098 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 36,396 hrs · 16,921 cycles

LEFT STATION 1022 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 36,396 hrs · 16,921 cycles

RIGHT STATION 1098 FORWARD LOWER EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 36,396 hrs · 16,921 cycles

LEFT STATION 1041 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 35,108 hrs · 16,340 cycles

OMA - INFLIGHT ORD-DEN. CREW REPORTED O2 BOTTLE PRESSURE LOW. LANDED OMA WITHOUT INCIDENT. REPLACED CREW O2 BOTTLE PER MAINTENANCE MANUAL. PERFORMED SELF TEST OF FIRST OFFICER’S REGULATOR, NO DEFECTS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,188 hrs · 15,490 cycles

EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK.

Part: BEAM — CRACKED (VAULT DOOR) · airframe 32,112 hrs · 15,038 cycles

CRACK IN VAULT DOOR RIGHT BEAM AT UPPER HINGE AREA. INSTALLED DOUBLER (4090576) PER SRM 52-05-00 FIG 34 (E-58 6337696).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS)

LGA - FOUND EMERGENCY EGRESS LIGHTS FROM SEAT ROWS 1 TO 19 INOPERATIVE. REPLACED EMERGENCY LIGHT MODULE AT SEAT ROW 19 OVERHEAD BIN FOR SEAT ROWS 1 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OXYGEN BOTTLE — LEAKING (COCKPIT)

INFLIGHT - CREW OXYGEN PRESSURE LOW. LANDED MSY WITHOUT INCIDENT. FOUND LEAK AT CAPTAIN SIDE OXYGEN EMERGENCY SUPPLY. REPLACED CREW OXYGEN BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (OIL SYSTEM)

DFW - RIGHT ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY. ENGINE OIL QUANTITY WAS ZERO BUT PRESSURE INDICATION WAS STILL 36 PSI BUT DROPPING WHEN SHUTDOWN. OIL TEMPERATURE WAS ABOVE 100 DEGREES CELSIUS. ENGINE WINDMILLED FOR APPROXIMATELY 22 MINUTES WITH 12 PSI OIL PRESSURE. ENGINE SHUTDOWN WITHIN 5 MINUTES OF LOW PRESSURE WARNING. N1 WAS 17 PERCENT WINDMILL, N2 WAS 20 PERCENT WINDMILL. LANDED DFW WITHOUT INCIDENT. FOUND OIL LEAK AT THE OIL PRESSURE TRANSMITTER. REPLACED RIGHT HAND ENGINE OIL TRANSMITTER PRESSURE LINE. SERVICED ENGINE OIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

STL - EMERGENCY EGRESS LIGHTS AT AFT CABIN INOPERATIVE. REPAIRED QUICK DISCONNECT IN TAIL SIDEWALL LIGHT FOR EMERGENCY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT)

STL EMERGENCY EXIT LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. FOUND LOOSE TERMINAL ON POWER SUPPLY. SECURED LOOSE TERMINAL ON POWER SUPPLY FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHT BETWEEN ROWS 18-20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN)

TUL LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING ESCAPE HATCH EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,429 hrs · 6,375 cycles

THE CEILING EMERGENCY LIGHTS AT ROW 25 TO THE AFT CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,785 hrs · 5,986 cycles

CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE R5-205 AND R5-209 BATTERY PACKS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,523 hrs · 3,646 cycles

THE FWD OVERHEAD EMERGENCY LIGHTS AROUND THE LIFE RAFT CONTAINER WOULD NOT EXTINGUISH WITH POWER OFF THE AIRCRAFT. PLACED EMERGENCY LIGHT SWITCH TO ARM FOR A HALF HOUR THEN LIGHTS STAYED OFF. ON FOLLOW UP THE NEXT STATION REPLACED THE BATTERY PACK. CHECK-C 10-6-00 STL.

Part: TUBE — FRACTURED (NR 6 BEARING) · airframe 4,615 hrs · 2,310 cycles

THE RT ENGINE WAS SHUT DOWN DUE TO OIL LOSS. MADE AN UNSCHEDULED LANDING AT SAT. FOUND OIL IN THE TAIL PIPE. REPLACED THE ENGINE. CHECK-C 9-3-99. *S/D* FOUND THE NUMBER 4 1/2 AND NUMBER 6 BEARING INTERNAL PRESSURE TUBE ASSEMBLY HAD FRACTURED, LEAKING OIL INTO THE EXHAUST CASE. PRESSURE TUBE ASSEMBLY WAS REPLACED.

Part: SKIN — DAMAGED (PAX DOOR)

THE RT SIDE FORWARD CABIN DOOR WAS DAMAGED AT THE FORWARD LOWER CORNER OF DOOR. REWORKED LOWER EDGE OF DOOR AT FWD CORNERS PER SRM 53-02, PAGE 1. CHANGED HINGE ASSY AND TORQUE TUBE ASSY. OPS AND RIG OK REF MM 52-41-00 FIG 401, 405, 501, 513.

Part: SKIN — BENT (FUSELAGE)

THE FWD LOWER EDGE OF THE OUTER SKIN WAS BENT IN FOUR INCHES WIDE BY 1 IN HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03, PAGE 1, ITEM 1 PARAGRAPH A.

Part: SKIN — BENT (PASSENGER DOOR)

THE LT FWD PASSENGER ENTRY DOOR, FORWARD LOWER EDGE OF THE OUTER SKIN, WAS BENT IN 4 INCHES WIDE BY 1 INCH HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03, PAGE 1 ITEM 1 PARAGRAPH A.