N9615W

Part: DOOR SILL — CORRODED (BS 386-393) · corrosion level 2 · airframe 59,860 hrs · 29,908 cycles

CORROSION FOUND ON DOOR SILL BEAM, APPROXIMATELY 2 INCHES AFT OF BOTTOM FORWARD DOOR STOP. REPAIRED THE DOOR SILL IAW EA 287493.

Part: SPEED BRAKE — MALFUNCTIONED · airframe 59,380 hrs · 29,595 cycles

DURING A SECOND APPROACH, THE SPEED BRAKE DID NOT ARM FOR LANDING. A SECOND GO-AROUND WAS ACCOMPLISHED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT ON THIRD ATTEMPT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED TEST SPOILER AUTOMATIC SYSTEM LANDING MODE PER AMM 27-60-00. OPERATIONS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR) · airframe 59,380 hrs · 29,595 cycles

NO GEAR IN TRANSIT LIGHTS OR DOWN AND LOCKED LIGHTS ILLUMINATED ON GEAR EXTENSION. FOUND TWO CIRCUIT BREAKERS P-38 AND L-14 TRIPPED. RETRACTED AND EXTENDED THE LANDING GEAR, THE LIGHT INDICATIONS WERE NORMAL. CIRCIUT BREAKERS P-38 & L-14 DID NOT TRIP. THEAIRCRAFT WAS GROUNDED.

Part: DUCT — LEAKING (CABIN PRESSURE) · airframe 59,135 hrs · 29,427 cycles

ON TAKEOFF, PRESSURIZATION FLOW LIGHT ILLUMINATED, CAUSING INABILITY TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DELCARED AND RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. NO FAULTS NOTED ON BOTH PRESSURE CONTROLLERS. DECAY CHECKED GOOD IAW AMM 21-00-00. SEVERAL DUCT LEAKS WERE REPAIRED.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 58,651 hrs · 29,118 cycles

THE AIRCRAFT WAS NOT GROUNDED. EXTERIOR EMERGENCY LIGHT ON WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. INTERIOR EMERGENCY LIGHTS NORMAL. REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK AND TESTED PER AMM 33-53-00. LIGHTS CHECK GOOD.

Part: BATTERY — MISINSTALLED (EMERGENCY LIGHT) · airframe 58,368 hrs · 28,927 cycles

ROW 21 OVERWING EMERGENCY LIGHT INOPERABLE. FOUND THE BATTERY PACK INSTALLED IN THE WRONG DIRECTION. INSTALLED BATTERIES CORRECTLY IAW AMM 33-60-98.

Part: LIGHT — INOPERATIVE (SEAT 5E) · airframe 58,368 hrs · 28,927 cycles

SEAT 5E AFT EMERGENCY LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-60-95, AND PERFORMED SATISFACTORY OPS CHECK.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (NLG) · airframe 57,986 hrs · 28,699 cycles

NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE ON INITIAL GEAR EXTENSION. CYCLED GEAR, STILL NO NOSE GREEN INITIALLY, CAME ON AFTER ABOUT 30 SECONDS. ADJUSTED THE NOSE LANDING GEAR DOWN LOCK PROXIMITY SENSOR IAW AMM 32-60-05.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,966 hrs · 28,684 cycles

DURING PREFLIGHT, FOUND THE OVERWING EMERGENCY LIGHTS ILLUMINATED WITH EMERGENCY EXIT LIGHT SWITCH IN OFF OR ARM. REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-53-00.

Part: TIRE — FAILED (MLG) · airframe 57,826 hrs · 28,592 cycles

DURING LANDING, THE NR 3 MAIN LANDING GEAR TIRE BLEW OUT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE TIRE IAW AMM 32-40-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FRAME — CORRODED (BS 148) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON FRAME AND FITTING FORWARD OF FORWARD SERVICE DOOR AT BS 148.50, RIGHT CUSP LINE, STRINGER 18R. REPLACED THE FITTING, AND REPAIRED THE FRAME IAW EA 274437, DRAFT 1, DRAWING 9911541, AND SRM 51-60-00-001.

Part: FITTING — CORRODED (BS 148.5) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON FRAME AND FITTING FORWARD OF THE FORWARD SERVICE DOOR AT BS 148.50, RIGHT CUSP LINE, STRINGER 18R. REPLACED THE FITTING AND REPAIRED THE FRAME IAW EA274437, DRAFT 1, DRAWING 9911541, AND SRM 51-60-00-001.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,470 hrs · 28,362 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED FORWARD ENTRY DOOR AFT DOOR FRAME WEB BETWEEN FUSELAGE STATIONS 207 AND 208 AT L13L. REPAIRED WEB PER AARD 53-10-00-11.

Part: BEAM — CORRODED (BS 636-693) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION FOUND ON THE MID CARGO DOOR FRAME BEAM, FORWARD AND AFT OF DOUBLER BETWEEN BS 636 & 693. REPAIRED THE BEAM IAW SRM 53-10-00-3.

Part: CUSP WEB — CORRODED (BS 378-383) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON FORWARD CABIN RIGHT CUSP WEB BETWEEN BS 378 & 383. REPAIRED THE CUSP WEB IAW SRM 53-20-00-16.

Part: SEAT TRACK — CORRODED (BS 1100-1103) · airframe 57,470 hrs · 28,362 cycles

CORROSION WAS FOUND ON THE NR 2 SEAT TRACK BETWEEN BS 1100 & 1103. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-05-00 AND SRM 51-00-05.

Part: CARGO TRACK — CORRODED (BS 1098-1225) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON THE AFT LT CARGO TRACK UPPER AND LOWER SIDES BETWEEN BS 1098 AND 1225. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-00-01.

Part: CARGO TRACK — CORRODED (BS 1079-1155) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON THE AFT RT CARGO TRACK BETWEEN BS 1079 AND 1155. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-00-01.

Part: CARGO TRACK — CORRODED (BS 1220) · corrosion level 2 · airframe 57,470 hrs · 28,362 cycles

CORROSION ON THE AFT RT CARGO TRACK AT BS 1220, STRINGER 27R. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-00-01.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 57,470 hrs · 28,362 cycles

CRACKED SHEAR TIE AT BS 1380 BETWEEN LONGERONS 13R AND 14R. REPAIRED THE SHEAR TIE IAW SRM 53-10-00-20

Part: LONGERON — CRACKED (BS 1418) · airframe 57,470 hrs · 28,362 cycles

CRACKED LONGERON 2L AT INBOARD RADIUS AFT SIDE FRAME AT BS 1418. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: FRAME — WORN (BS 1380) · airframe 57,470 hrs · 28,362 cycles

WEAR ON FRAME FORWARD LEFT SIDE AT BS 1380. REPAIRED FRAME IAW SRM 53-10-00-28.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,112 hrs · 28,107 cycles

AFT GALLEY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00-401. ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 56,766 hrs · 27,884 cycles

RIGHT ENGINE INBOARD SIDE OTBD THRUST REVERSER HAS 10 ELONGATED HOLES WHERE THE RIVET HEADS ARE FLOATING AROUND. INSTALLED NEW RIVETS IAW SRM 51-30-08. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 56,766 hrs · 27,884 cycles

RIGHT ENGINE INBOARD SIDE INBOARD THRUST REVERSER FAIRING HAS 9 ELONGATED HOLES WHERE THE RIVET HEADS ARE FLOATING AROUND. INSTALLED NEW RIVETS IAW SRM 51-30-08. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 56,766 hrs · 27,884 cycles

AIRCRAFT WAS GROUNDED. RIGHT ENGINE INBOARD SIDE INBOARD THRUST REVERSER FAIRING IS MISSING ONE RIVET. INSTALLED NEW RIVET IAW SRM 51-30-08. OPERATIONAL CHECKED GOOD.

Part: FIRE BOTTLE — LEAKING (NR 2) · airframe 56,693 hrs · 27,834 cycles

DURING CRUISE ALTITUDE. AGENT 2 LOW LIGHT ILLUMINATED. NO INDICATION OF ABNORMAL ENGINE OPERATION NOTED. NO OTHER ASSOCIATED LIGHTS. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING FOUND ALL THE SQUIBS UNFIRED. BUT THE BOTTLE WAS EMPTY. REPLACED FIRE EXT BOTTLE IAW MM 26-20-01. OPS CHECKED FIRE BOTTLE SQUIBS IAW MM 26-20-03. CHECKED TAIL COMP FOR PNEUMATIC LEAKS. NONE FOUND. ALL CHECKS NORMAL. THE AIRCRAFT WAS GROUNDED.

Part: RETAINING CLIP — DETACHED (R1 DOOR) · airframe 55,770 hrs · 27,250 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE GIRT RETAINING CLIP DETACHED FROM SLIDE COVER. REATTACHED GIRT RETAINING CLIP. OPERATIONAL CHECK GOOD.

Part: WARNING MESSAGE — MALFUNCTIONED · airframe 54,855 hrs · 26,654 cycles

VREF 0/RET WAS BUGGED AT 228 KNOTS AND ALPHA SPEED ANNUNCIATION OCCURRED AT 240 KNOTS. DECLARED EMERGENCY. LANDING UNEVENTFUL. MAINTENANCE PERFORMED FAULT REVIEW ON DIGITAL FLIGHT GUIDANCE COMPUTERS 1 & 2 WITH NO FAULTS FOUND. PERFORMED FLIGHT MANAGEMENT COMPUTER OPS CHECKED IAW AMM 34-63-00 WITH NO FAULTS FOUND. SYSTEM CHECKED NORMAL.

Part: FILTER — CLOGGED (NR 1 ENGINE OIL) · airframe 54,807 hrs · 26,622 cycles

DURING FLIGHT, THE NR 1 ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED. ALL ENGINE PARAMETERS REMAINED NORMAL. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ACCOMPLISHED MCM CARD 71-91-14 AND 71-91-11. REMOVED AND REPLACED NR 1 ENGINE OIL FILTER IAW AMM 79-20-06. OPS AND LEAK CHECKED NORMAL. DEBRIS IN FILTER DETERMINED TO BE CARBON..

Part: FRAME — WORN (FUSELAGE) · airframe 54,484 hrs · 26,429 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CANT FRAME AT FUSELAGE STA 1510 IS WORN FROM TAIL CONE RUBBING. REPAIRED FRAME IAW SRM 51-70-05, FIGURE 1, EA 261574 AND EA 261591.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 54,484 hrs · 26,429 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR STOP, 2ND FROM TOP ON FORWARD END, IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1 AND DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 54,484 hrs · 26,429 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. MID CARGO DOOR UPPER AFT STOP FITTING AT APPROXIMATE FUSELAGE STA 427 IS CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1.

Part: HOSE — RUPTURED (AC BAY) · airframe 53,702 hrs · 25,975 cycles

AT 34,000 FT, GOT PRESSURIZATION FLOW LIGHT ON. DESCENDED TO 25,000 FT. AT 25,000 FT, THE CABIN DEPRESSURIZED. THE CREW DONNED OXYGEN MASKS & PERFORMED EMER DESCENT TO 10,000 FT. AN EMER WAS DECLARED. OXYGEN MASKS DEPLOYED IN THE CABIN WHEN CABIN ALTITUDE HIT 14,000 FT. THE FLIGHT CONTINUED & LANDED WITHOUT FURTHER INCIDENT. REPLACED LT PACK ACM EXIT HOSE IAW 21-51-01. THE ACFT WAS GNDED.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 53,582 hrs · 25,901 cycles

AIRCRAFT WAS NOT GNDED. EMER EVACUATION LIGHTING ON SEAT 32D IS INOPERATIVE. FOUND WIRING HARNESS DAMAGED. R & R EMER LIGHT ASSEMBLY WIRING HARNESS IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,157 hrs · 25,661 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS ROWS 3 - 6 FAILED TO TEST. R & R BATTERY PACK B5-100 IAW AMM 33-53-00. LIGHTS OPERATIONALLY CHECKED OK. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,157 hrs · 25,661 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS ROWS 12 - 17 FAILED TO TEST. REPLACED EMER LIGHT BATTERY PACK B5-102 IAW AMM 33-53-00, TESTED OK. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,157 hrs · 25,661 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS ROWS 7 - 11 FAILED TO TEST. REPLACED B5-101 EMER LIGHT BATTERY PACK IAW AMM 33-53-00, TESTED OK. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,992 hrs · 24,947 cycles

AFT OVERWING EMER EXIT LIGHTS FAILED FUNCTIONAL TEST. R & R BATTERY PACK B5-105. PERFORMED OPERATIONAL TEST IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: POWER SUPPLY — DIRTY (CABIN) · airframe 51,536 hrs · 24,680 cycles

LEFT & RIGHT FWD EMER OVERWING EXIT LIGHTS INOPERATIVE. CLEANED & ADJUSTED CONTACTS ON POWER SUPPLY WITH GOOD OPERATIONAL CHECKS.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,769 hrs · 24,255 cycles

AFT CARGO DOOR 2ND FROM TOP FWD DOOR STOP IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,769 hrs · 24,255 cycles

MID CARGO DOOR FWD LOWER STOP CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,769 hrs · 24,255 cycles

AFT CARGO DOOR FWD MIDDLE DOOR STOP IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK 2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,769 hrs · 24,255 cycles

AFT CARGO DOOR FWD UPPER DOOR STOP IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,769 hrs · 24,255 cycles

AFT CARGO DOOR AFT TOP DOOR STOP IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK 2345.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON SKIN UNDER RUB STRIP FOR FILLET PANEL FROM BS 750 TO 769 RT. INSTALLED DOUBLER REPAIR IAW SRM 53-04-00 FIGURE 57.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON FRAME STIFFENER AT BS 1171 & LONGERONS 20 TO 21 LT. ACCOMPLISHED SPLICE REPAIR IAW EA MD80-53-031576.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON SUBFLOOR AT BS 216 RT AT SEAT TRACK NR 6. INSTALLED SUBFLOOR DOUBLER FROM BS 210 TO 218 RT HAND IAW AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

RT HAND WW OVERWING LONGERON 20 RT IS CRACKED AT THE AFT OTBD SIDE OF THE WW ABOVE THE FLAP CABLES. ACCOMPLISHED REPAIR IAW AARD 53-10-00-18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

SEAT TRACK NR 1 CORRODED IN SEVERAL AREAS FROM STATIONS 613 TO 699. REPLACED SEAT TRACK SECTIONS IAW SRM 53-05-00 SECTION 4.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON GALLEY TIE DOWN FITTING NR 2 INBD STATION 210, 3 INCHES FROM CENTER LINE. INSTALLED NEW GALLEY MOUNT IAW SRM 51-30-01.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON GALLEY TIE DOWN FITTING NR 1 OTBD MOUNT. INSTALLED SERVICEABLE OTBD G-1 GALLEY MOUNT IAW AARD 51-00-05-1.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON GALLEY TIE DOWN FITTINGS NR 1 INBD & OTBD MOUNTS. INSTALLED INBD & OTBD G-1 GALLEY MOUNT FITTINGS IAW AARD 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CRACK IN LT FWD CORNER OF WINDOW PAN AT BS 845. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW FRAME) · airframe 47,307 hrs · 22,395 cycles

LOWER FWD TAB CRACKED AT RT HAND WINDOW FRAME AT STATION 1061. INSTALLED WINDOW RING PAN REPAIR DOUBLE IAW AARD 53-10-00-25.

Part: MOUNT — CORRODED (GIRT BAR) · corrosion level 3 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON AFT SERVICE DOOR GIRT BAR MOUNT FWD. INSTALLED NEW AFT SERVICE DOOR FWD GIRT BAR MOUNT IAW AARD 51-00-05-1 & DRAWING 9930612, CONFIGURATION -527.

Part: TAB — CRACKED (WINDOW FRAME) · airframe 47,307 hrs · 22,395 cycles

LOWER FWD TAB IS CRACKED AT RT HAND WINDOW FRAME AT STATION 1080. INSTALLED WINDOW RING PAN REPAIR DOUBLER IAW AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW FRAME) · airframe 47,307 hrs · 22,395 cycles

LOWER FWD TAB IS CRACKED AT RT HAND WINDOW FRAME AT STATION 1099. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW FRAME) · airframe 47,307 hrs · 22,395 cycles

TOP FWD TAB IS CRACKED AT RT HAND WINDOW FRAME AT STATION 947. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

SEAT TRACK NR 3 HAS TWO AREAS AT STATIONS 1276 & 1286 CORRODED. INSTALLED NEW SECTION OF TRACK FROM STATIONS 1090 TO 1309.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

SUBFLOOR CUSP CORROSION FOUND AROUND FWD SERVICE DOOR DURING MAINTENANCE CHECK. ACCOMPLISHED REPAIR IAW AARD 53-20-00-16.

Part: TAB — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

LOWER FWD TAB CRACKED AT RT HAND WINDOW FRAME, STATION 1118. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-10-00-25.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION AT STATION 1322 & LONGERON 30. ACCOMPLISHED DOUBLER REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

RT HAND FLOOR CUSP AT STATIONS 1159 CORRODED. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: TAB — CRACKED (WINDOW FRAME) · airframe 47,307 hrs · 22,395 cycles

TOP AFT TAB CRACK AT RT HAND WINDOW FRAME, STATION 1154. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-25 FIGURE 1.

Part: TAB — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

TOP AFT TAB CRACKED, RT HAND WINDOW FRAME AT STATION 1078. INSTALLED DOUBLER IAW AARD 53-10-00-25 FIGURE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CORROSION ON NR 1 SEAT TRACK FROM STATIONS 798 TO 921. REPLACED NR 1 SEAT TRACK FROM STATIONS 798 TO 1031 IAW SRM 53-05-00 FIGURE 4F & 4H.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CORROSION ON CUSP SHEET UNDER AFT GIRT BAR MOUNT AT AFT SERVICE DOOR. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

SEAT TRACK NR 3 CORRODED FROM STATIONS 1276 TO 1286. REPLACED SEAT TRACK NR 3 FROM STATIONS 1090 TO 1309.

Part: TAB — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

TOP AFT TAB CRACKED, RT HAND WINDOW FRAME AT STATION 1097. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-25 FIGURE 1.

Part: PAN — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

BIN CRACKED IN LT HAND TOP AFT CORNER OF WINDOW PAN, STATION 1041. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CORROSION ON SEAT TRACK NR 1 FROM STATIONS 243 TO 580. INSTALLED NEW SEAT TRACK FROM STATIONS 218 TO 588 IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

RT HAND CUSP HAS LIGHT CORROSION AT LIGHTNING HOLE STATION 507. REMOVED CORROSION & INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION AT STATION 1338 STIFFENER & LONGERON 29 LT. INSTALLED DOUBLER.

Part: FRAME — WORN (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

AFT ACCY, COCKPIT AIR VALVE AT 1380 FRAME HAS WEAR. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-28.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

FOUND CORROSION ON RT HAND CUSP SHEET FROM STATIONS 218 TO 237. INSTALLED SERVICEABLE CUSP SHEET IAW AARD 51-00-05-1.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

PUNCTURE IN THE LT HAND CUSP AT STATION 230 UNDER THE OTBD LEG OF THE NR 1 SEAT TRACK. INSTALLED DOUBLER IAW SRM 51-30 & AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

OVERWING LONGERON 20 LT IS CRACKED AT THE AFT OTBD SIDE OF THE WW ABOVE THE FLAP BUS CABLES. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-18.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON SHEAR TIE AT STATION 1231 & LONGERONS 30 TO 29 RT. REPLACED SHEAR TIE IAW AARD 51-00-05-1.

Part: TIE DOWN — CORRODED (CABIN) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

GALLEY NR 4 GALLEY TIE DOWN IN SEAT TRACK NR 1 AT STATION 1174 CORRODED. REMOVED & INSTALLED NEW SERVICEABLE NR 4 GALLEY TIE DOWN IN SEAT TRACK NR 1 AT STATION 1174 IAW AMM 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

SEAT TRACK NR 1 CORRODED FROM STATIONS 1174 TO 1309. REMOVED & INSTALLED NEW SERVICEABLE SEAT TRACK FROM STATIONS 1174 TO 1309 IAW AMM 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

MULTIPLE AREAS OF CORROSION ON NR 6 SEAT TRACK FORM STATIONS 207 TO 589. REPLACED SEAT TRACK IAW MM 53-40-01-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

CORROSION ON NR 6 SEAT TRACK FROM STATIONS 598 TO 788. REPLACED SEAT TRACK IAW AARD 51-00-05-1.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

RT CUSP HAS SMALL PUNCTURE UNDER NR 6 SEAT TRACK AT STATION 515. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,307 hrs · 22,395 cycles

NR 6 SEAT TRACK AT STATION 1185 CORRODED. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

LT CUSP CRACKED AT STATION 830. INSTALLED REPAIR DOUBLER IAW SRM 53-20-00 FIGURE 16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

LT CUSP IS CRACKED & PUNCTURED AT STATION 288. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 47,307 hrs · 22,395 cycles

CABIN CRACK IN LT TOP FWD CORNER OF WINDOW PAN STATION 946. ACCOMPLISHED NESTED ANGLE REPAIR IAW AARD 53-10-00-25.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 44,764 hrs · 21,105 cycles

ABQ - INFLIGHT DFW-RNO. CREW REPORTED LEFT ENGINE GENERATOR FAULT AND UNABLE TO START AUXILIARY POWER UNIT. EMERGENCY DECLARED FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,774 hrs · 20,614 cycles

CRACK IN FUSELAGE SKIN AT STATION 1474, AT APPROXIMATELY LONGERON 22 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01, FIGURE 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,774 hrs · 20,614 cycles

THE 1418 CANT FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER AND STRAP REPAIR PER SRM 53-03-00.

Part: LENS — BROKEN (CABIN) · airframe 43,552 hrs · 20,489 cycles

FORWARD AFT AIRSTAIRS EMERGENCY LIGHT LENS BROKE. REPLACED FORWARD AFT AIRSTAIRS EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: CIRCUIT BREAKER — DEFECTIVE (AUTOPILOT SYS) · airframe 42,422 hrs · 19,907 cycles

EWR - CREW REPORTED NUMBER 2 AUTO THROTTLES WOULD NOT ENGAGE. ONCE AIRBORNE SELECTED NUMBER 1 DFGS AND YAW DAMPER OFF LIGHT ILLUMINATED. FLIGHT RETURNED EWR LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 YAW DAMPER FAULTY CIRCUIT BREAKER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPAR CAP — CRACKED · airframe 41,778 hrs · 19,587 cycles

CRACK INDICATION WITH A HFEC HOLE PROBE, LEFT SIDE SIXTH HOLE DOWN FROM UPPER EDGE OF LOWER SKIN. DOUBLER AND TRIPLER INSTALLATION ON SPAR CAP PER EA MD80-55-019313.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,631 hrs · 18,537 cycles

CORROSION ON LEFT TIE DOWN TRACK STATIONS 1213 TO 1300. REMOVED AND REPLACED LEFT TIE DOWN TRACK PER SRM 53-01-00.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 39,626 hrs · 18,533 cycles

PDX - CREW REPORTED BATTERY CHARGER LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED PDX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CHARGER AND BATTERIES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — FAILED (APU BAY) · airframe 37,267 hrs · 17,410 cycles

SDF - INFLIGHT CMH-DFW. CREW REPORTED AUXILIARY POWER UNIT FAILED IN FLIGHT WITH RIGHT ENGINE DRIVEN GENERATOR PLACARD PER MEL REF 24-01B. EMERGENCY DECLARED DIVERTED SDF LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT CONSTANT SPEED DRIVE GENERATOR. THE APU WAS PLACARD PER MEL / REFERENCE 49-01. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: REGULATOR VALVE — FAILED (AC BAY) · airframe 36,304 hrs · 16,981 cycles

INFLIGHT SJD TO ORD. FLIGHT CREW REPORTED HEAVY SMELL OF ELECTRICAL FUMES IN AFT CABIN AFTER TURNING ON AIRFOIL ANTI ICE TO FULL. DIVERTED TO STL DUE TO CHANCE OF ICING IN ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED AIR CONDITIONING PACK BURNOUT AND REPLACED BOTH LEFT AND RIGHT PRESSURE REGULATING VALVES IN TAIL SECTION. NO FUMES DURING FUNCTIONAL FLIGHT CHECK.

Part: DUCT — LEAKING (CARGO BAY) · airframe 35,775 hrs · 16,754 cycles

ABQ - DFW - RETURNED ABQ SHORTLY AFTER TAKEOFF DUE TO THE AFT CARGO COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. CREW WAS ABLE TO EXTINGUISH THE LIGHT BUT ELECTED TO RETURN ABQ. AIRCRAFT REMOVED FROM SERVICE. FOUND SIX INCH DUCT WITH LARGE LEAK. REMOVED AND REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,719 hrs · 16,725 cycles

TUL - CORROSION IN AFT CARGO TIE DOWN TRACK. INSTALLED NEW TIE DOWN TRACK.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,541 hrs · 16,642 cycles

SHEAR TIE CRACKED AT LONGERON 2 LT. INSTALLED NEW SHEAR TIE CLIP PER STRUCTURE REPAIR MANUAL 51-10.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,541 hrs · 16,642 cycles

CORROSION ON BELLY SKIN UNDER RIGHT HAND FILLET NUMBER 2208. RREMOVED CORROSION ON BELLY SKIN UNDER FILLET PER SRM 51-10-3. CORROSION OUT OF LIMITS PER DT MAP AND SRM 53-04 FIGURE 30. INSTALLED DOUBLER FROM STATION 1077 TO 1087, LONGERON 29L TO 28R AND INSTALLED DOUBLER FROM STATION 1108 TO 1117, LONGERON 27L TO 28R PER EA MD80-53-006606 AND EA MD8-53-006631.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

SHEAR TIE CRACKED AT STATION 1437 INBOARD OF LONGERON 3R. REMOVED CRACKED SHEAR TIE INSTALLED SERVICEABLE SHEAR TIE IAW 51-30.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION ON RIGHT TIE DOWN TRACK, STATION 1211-1322. REPLACED RIGHT TIE DOWN TRACK.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION ON UPPER AND LOWER SIDE OF AFT LOWER FLANGE OF FRAME 1309, LONGERON 28 RIGHT TO LONGERON 28 LEFT. INSTALLED REPAIR DOUBLER ON UPPER AND LOWER SIDE OF AFT LOWER FLANGE 1309, LONGERON 28 RIGHT TO LONGERON 28 LEFT PER SRM 53-03-00 FIGURE 2A SHEET 2.

Part: VANE — WORN (TE FLAP) · airframe 35,531 hrs · 16,634 cycles

LEFT WING NR 4 FLAP VANE HAS HOLE WORN ON TOP FROM CONTACT WITH I/B SPOILER. PERFORMED HOT BOND REPAIR ON VANE PER SRM 57-03-00.

Part: CASTING — CRACKED (SPOILER) · airframe 35,531 hrs · 16,634 cycles

GROUND SPOILER MOUNT CASTING CRACKED AT FORWARD MOUNT, INBOARD SIDE. INSTALLED NEW SPOILER CASTING, LEFT, PER DRAWING 5936824 AND SRM 51-30-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

NR 3 SEAT TRACK CORRODED STATIONS 1130-1136. REPLACED SEAT TRACK SECTION STATIONS 1089-1222 PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION ON RIGHT CUSP AT STATION 845-864. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

INTERCOSTAL CRACKED BELOW CABIN FLOOR, STATION 1287-1309 AT CENTER LINE. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-01-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

INTERCOSTAL CRACKED BELOW CABIN FLOOR, STATION 1271-1287 AT CENTER LINE. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-01-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 35,531 hrs · 16,634 cycles

FORWARD CARGO DOOR FORWARD DOOR STOP SUPPORT FITTINGS (4) EACH CRACKED. REPLACED FITTINGS PER ESO 80174.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 35,531 hrs · 16,634 cycles

MID CARGO DOOR FITTING CRACKED. REPLACED MID CARGO DOOR FITTING PER ESO 80174.

Part: HOOK — CRACKED (SERVICE DOOR) · airframe 35,531 hrs · 16,634 cycles

AFT SERVICE DOOR OPEN HOOK CRACKED. REPLACED DOOR OPEN HOOK ON AFT SERVICE DOOR IN ACCORDANCE WITH ESO 80175.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION AT STATION 1285, SEAT TRACK NR 4. REMOVED CORROSION AND INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION BLENDED BEYOND LIMITS AT STATION 203. PLUG REPAIR ACCOMPLISHED PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION BLENDED OUT OF LIMITS AT STATION 935-940. PLUG REPAIR ACCOMPLISHED PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION IN SEAT TRACK NR 6. INSTALLED PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION IN SEAT TRACK NUMBER 6. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION BLENDED BEYOND LIMITS AT STATION 264. PLUG REPAIR ACCOMPLISHED PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION BLENDED BEYOND LIMITS AT STATION 400. PLUG REPAIR ACCOMPLISHED PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,531 hrs · 16,634 cycles

CORROSION BLENDED BEYOND LIMITS AT STATION 302. PLUG REPAIR ACCOMPLISHED PER AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

CRACK IN LOWER FORWARD CORNER OF WINDOW PAN. INSTALLED WINDOW PAN DOUBLER PER AARD 53-10-00-25.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

WEB CRACKED AT STATION 206 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

CRACK IN LOWER FORWARD CORNER OF WINDOW PAN STATION 1193 RIGHT. INSTALLED WINDOW PAN REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

CRACK IN UPPER AFT CORNER PAN STATION 1079 LEFT. TRIMMED AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,531 hrs · 16,634 cycles

CRACK IN UPPER CORNER OF WINDOW PAN STATION 1060 LEFT. TRIMMED, INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 34,966 hrs

SFO - AISLE SEAT 22D EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT 22D EMERGENCY LIGHT ASSEMBLY.

Part: CIRCUIT BREAKER — FAILED (ZONE 100) · airframe 34,361 hrs · 16,135 cycles

ORD INFLIGHT - DURING CLIMB CENTER TANK PRESSURE INDICATOR LIGHT ILLUMINATED ON OVERHEAD PANEL. LANDED ORD WITHOUT INCIDENT. FOUND THREE FUEL PUMP CIRCUIT BREAKERS POPPED. REPLACED LEFT AC PHASE C CIRCUIT BREAKER B1743. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (START VALVE) · airframe 34,161 hrs

IAD INFLIGHT LGA TO DFW - NR 2 ENGINE START VALVE OPEN INDICATION. LANDED IAD WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT STATOR CONNECTOR PL834. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 33,993 hrs

SFO - EMERGENCY LIGHTS AT FORWARD OVERWING LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,450 hrs

SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,450 hrs

SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 16B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BOOT — SPLIT (DUCT) · airframe 32,068 hrs

DFW INFLIGHT T852/09APR - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH AND DUCT PRESSURE ANOMALY. REDUCED POWER FOR DESCENT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION AND REPAIR. FOUND BLOWN DUCT BOOT ON RIGHT TEMPERATURE CONTROL DUCT. REPLACED DUCT BOOT ON RIGHT TEMPERATURE CONTROL DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RING — MISSING (MLG) · airframe 31,465 hrs

ORD INFLIGHT T1715/23JAN - RECEIVED RED NOSE GEAR UNSAFE LIGHT AFTER RETRACTING GEAR ACCOMPANIED BY LOUD AIR NOISE FROM NOSE WHEEL WELL. RECYCLED GEAR AND GEAR CAME DOWN NORMALLY BUT LIGHT WOULD ILLUMINATE AFTER RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND LOWER TWO SCRAPER RINGS MISSING FROM BOTTOM STRUT SEAL. ACCOMPLISHED NOSE GEAR STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 29 TO 32 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 29 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL SYSTEM)

DFW INFLIGHT T1760/10JAN - ON CLIMB-OUT, RIGHT HAND ENGINE STOPPED RESPONDING TO THROTTLE MOVEMENT. EXHAUST GAS TEMPERATURE AT CLIMB LIMIT AND ENGINE ENGINE PRESSURE RATIO AT 1.3. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IRU — INOPERATIVE

LAS - LOST BOTH INERTIAL REFERENCE UNITS EN ROUTE TO ORD. LANDED LAS WITHOUT INCIDENT. REPLACED BOTH INERTIAL REFERENCE UNITS AND CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACTOR — DIRTY (BATTERY)

AISLE EMERGENCY LIGHT AT ROWS 5, 7, 13 AND 16 INOPERATIVE. CLEANED ELECTRICAL CONTACTS IN FORWARD CABIN EMERGENCY LIGHT BATTERY PACK FOR ROWS 5, 7, 13, AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SNA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR LEFT AND RIGHT HAND EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

STL - CEILING EMERGENCY LIGHTS AT SEVERAL LOCATIONS THROUGHOUT CABIN AND FORWARD EXIT LIGHT AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FOR VARIOUS LOCATIONS THROUGHOUT CABIN AND FOR FORWARD EXIT LIGHT AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELAY — MISWIRED (NR 1 FIRE BOTTLE)

DFW INFLIGHT T1310/19 APPROACHING 14,000 FEET AFT CARGO FIRE INDICATION AND MASTER WARNING LIGHTS CAME ON. DISCHARGED NR 1 FIRE BOTTLE. NO INDICATION OF DISCHARGE. FOLLOWED QRH AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND ON R2-5 RELAY A GROUND CONTROL WIRE MIS-WIRED FROM CARGO SMOKE CONTROL PANEL. REPLACED R2-5 GROUND CONTROL RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW CEILING EMERGENCY LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR ROW 25 CEILING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CORROSION ON SEAT TRACK STATION 588-798. REPLACED NR 3 CHAIR TRACK STATION 588-798 PER SRM 53-05-00 FIG 4F. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

MCI - AFT LOWER SUPPORT BETWEEN MLG WHEEL WELL CRACKED, LEFT SIDE, FS 977. REPLACED CRACKED PART WITH NEW PART CPN NR 4057240. INSTALLED PER SRM 51-30-2, SRM 51-30-5, TREATED PART PER SRM 51-10-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

MCI - FOUND LEFT SIDE, INBOARD SET TRACK, INBOARD SIDE AT FS 1157 HAS EVIDENCE OF CORROSION. REMOVED DAMAGED CHAIR TRACK FROM STATION 1088-1220 AND INSTALLED NEW CHAIR TRACK AND SPLICE PER SRM 53-05-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

MCI - FOUND FLOOR TRACK AT LBL 23, FS 1166 HAS CORROSION GALLEY NR 3. REMOVED DAMAGED CHAIR TRACK FROM STATION 1088-1220, AND INSTALLED NEW CHAIR TRACK AND SPLICE PER SRM 53-05-00. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND FLOORBEAM FROM LBL 43 TO LBL 24, FLOOR SUPPORT CORRED FS 1155. FABRICATED NEW SUPPORT WITH EXTRUSION CRN4018034. TREATED PART AND INSTALLED PER SRM 51-10-35, 51-80-1. (M)

Part: BATTERY · airframe 16,556 hrs · 8,266 cycles

THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-7-02 STL. --CLOSED--

Part: TAIL CONE — DEPARTED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING TAKEOFF ON A TEST FLIGHT OUT OF A MAJOR CHECK, THE TAIL CONE UNSAFE LIGHT ILLUMINATED. CREW ELECTED TO GO AROUND AND LAND. DURING LANDING THE TAIL CONE DEPARTED FROM THE AIRCRAFT AND LANDED ON THE RUNWAY, AND THE TAIL CONE EVACUATION SLIDE DEPLOYED. RIGGED THE TAIL CONE LATCHES PER MM 53-53-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT AT THE AFT ACCESSORY COMPT FOUND A CRACK IN ANGLE ON SIDE, LT VENT BOX AT STA 1510. INSTALLED NEW ANGLE ON ACFT WITH RIVETS PER SRM 51-10-02, PAGE 2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON RT TIE DOWN TRACK, STA 1271 TO 1287 AND STA 1212 TO 1231. REMOVED OLD TRACK AND REPLACED WITH NEW. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-3. PRIMED AND PAINTED PER SRM 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LT TRACK, STA 1250 TO 1287. REPLACED TRACK FROM FACTORY SPLICE, STA 1216 TO AFT END PER SPM 6-70-01, SRM 51-30-2, AND SPM 6-30-07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT FOUND CORROSION ON UNDER SIDE OF LT TRACK SPLICE IN AFT CARGO COMPT, STA 1212 TO 1225. REMOVED SPLICE. CLEANED CORROSION PER SPM 6-80-01. OTBD SECTION REPLACED WITH NEW PART PER SPM 6-70-01. TREATED PARTS PER SRM 51-10-3. INSTALLED SPLICE USING SRM 51-30-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT FOUND CLASS 3 REPAIR INSTALLED AT STA 235, LONGERON 17L TO 18L. REMOVED OLD REPAIR. CUT OUT DAMAGED SKIN AND INSTALLED FLUSH CLASS 1 REPAIR PER SRM 53-10-107.

Part: SKIN — DENTED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT FOUND FUSELAGE DENT IN SKIN AT STA 229, LONGERON 19L, A 2 IN CLASS 3 REPAIR INSTALLED. REMOVED OLD REPAIR DOUBLER AND DAMAGED SKIN. INSTALLED REPAIR PER SRM 53-10-107. PLUGGED HOLES AND INSTALLED FASTENERS PER SRM 51-30. PAINTED ON WORK ORDER.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,676 hrs · 5,993 cycles

DURING CHECK-C MAINT FOUND FUSELAGE CRACK IN RT AFT ACCESS SECTION VENT BOX AT STA 1510. CRACK STOP DRILLED FOR INTERIM REPAIR PER ARA 13888. ACCOMPLISHED EDDY CURRENT PER NDT 53-00-03 PART AND CRACK CONTAINED. STOP DRILLED CRACK. REPAIRED PER SRM 53-01 FIG 2.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 12,316 hrs · 5,831 cycles

THE RT AFT OVERWING EXIT EGRESS RED LIGHT DID NOT ILLUMINATE. RECONNECTED EGRESS LIGHT AT THE AFT OVERWING EXIT. CHECK-C 7-14-00 STL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,282 hrs · 5,370 cycles

THE EGRESS LIGHTING WAS INOPERATIVE FROM ROWS 4 AND 9, 22 THRU 24, AND 28 TO 29. REPLACED BATTERY PACK AT ROW 4 PN 60-304-51, CLEANED AND RESEATED THE ELECTRICAL CONNECTOR AT ROW 22, AND REPLACED THE LIGHT MODULE AT ROW 28 PN LP7732-011. CHECK-C 7-14-00 STL.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 10,555 hrs · 5,003 cycles

THE LAST TWO EGRESS LIGHT LENSES WERE WHITE INSTEAD OF RED, AND THE FIRST LIGHT IN THE FWD GALLEY WAS INOPERATIVE. INSTALLED RED LENSES IN AFT CABIN (P/N 0105607-301), AND REPLACED THE LIGHT MODULE (P/N 0105606-004) FOR THE LIGHT MALFUNCTION.

Part: WIRE — WORN (ROWS 15 & 24)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 14 AND 15, ROWS 22 TO 24. REPLACED A CABLE WIRE MODULE AT BOTH LOCATIONS. CHECK-C 7-18-99 STL.

Part: WIRE — LOOSE (ROW 3)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 3. FOUND WIRE PULLED OUT AT THE LIGHT MODULE. REPLACED THE MODULE. CHECK-C 7-18-99 STL.

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINT CHECK, FOUND RED EGRESS LIGHT INOPERATIVE AT CABIN ROW 22. REPLACED MODULES, (P/N 0105606-002, 0105606-004).

Part: BULB — FAILED (CABIN)

DURING MAINT CHECK, FOUND THREE EGRESS LIGHTS INOPERATIVE BETWEEN CABIN ROWS 3 AND 5. REPLACED ALL THREE BULBS.

Part: SKIN — DENTED (CARGO DOOR)

MCI - DURING CHECK-C, MAINTENANCE FOUND FORWARD CARGO DOOR, OUTSIDE AT HANDLE, HAD DENT AND PRY MARK. DENT 2 INCHES ACROSS BY .75 INCH BY 0.187 INCH DEEP. REPAIRED DENT PER SRM 52-05, PAGE 159, INSTALLING CRES STEEL SCUFF PLATE TO HANDLE AREA USING HILOKS, WASHERS AND NUTS, AND SEALING. (X)