N954U

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,788 hrs · 43,608 cycles

AIRCRAFT GROUNDED. COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 79,560 hrs · 43,466 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH MARKING BATTERY PACK AB5-3 FAILED TEST. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 79,046 hrs · 43,125 cycles

DURING FLIGHT THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. TRANSFER PUMP WAS TURNED OFF. QUANTITY IN LEFT SYSTEM 3 QUARTS, PUMP PRESSURE WENT TO 3000 PSI FOR 5 SECONDS THEN DROPPED TO 1000 PSI. PUMP TURNED OFF. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND A LOOSE B-NUT ON THE LEFT THRUST REVERSER FILTERS MOUNT BLOCK. RETORQUED B-NUT IAW AMM 20-30-02. OPS AND LEAK CHECKED NORMAL.

Part: CLAMP — OUT OF POSITION (ACM) · airframe 79,000 hrs · 43,096 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATUR HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE AIR CYCLE MACHINE DUCT CLAMP ON THE RIGHT HAND PACK DISPLACED. REPOSITIONED CLAMP AND DUCT, ACCOMPLISHED OPERATIONAL CHECK IAW AMM 21-20-00. SYSTEM CHECKS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 75,777 hrs · 41,156 cycles

DURING TAKEOFF & CLIMB, FLIGHT ATTENDANTS REPORTED SMOKE ODOR IN AFT CABIN, SOURCE UNIDENTIFIED. RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING CARD MCM 21-96-01 & PACK BURN CARD MCM21-91-12. NO ODORS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,911 hrs · 40,642 cycles

AFT EMER PATH LIGHTS FAILED TEST ON MCM 5403. R & R AFT BATTERY PACK FOR EMER PATH LIGHTS. SYS CHECKED NORMAL.

Part: RIB — CRACKED (LT WING) · airframe 74,072 hrs · 40,095 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR FITTING.

Part: RIB — CRACKED (RT WING) · airframe 74,072 hrs · 40,095 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR FITTING.

Part: CONNECTOR — LOOSE (CABIN) · airframe 73,902 hrs · 39,993 cycles

ROW 16 & 17 SIDE SEAT EMER EGRESS LIGHTS INOPERATIVE. FOUND SEAT TO WALL CONNECTOR KNOCKED LOOSE. RECONNECTED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 73,362 hrs · 39,665 cycles

PRIMARY STAB TRIM INOPERATIVE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED STAB TRIM MOTOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,858 hrs · 39,372 cycles

EGRESS LIGHTS FAILED AT AB5 1. REPLACED BATTERY PACK, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,724 hrs · 39,283 cycles

ROW 21 OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK & LAMPS IN LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 71,211 hrs · 38,443 cycles

LT HAND GENERATOR FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED LT HAND ENGINE CONSTANT SPEED DRIVE & GENERATOR. SYSTEM GROUND CHECKED NORMAL.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CORROSION TOP OF SUBFLOOR AT STATION 200 UNDER FORWARD END OF NUMBER 4 SEAT TRACK. INSTALLED DIAPHRAGM REPAIR DOUBLER FROM STATIONS 200 TO 218 AND RIGHT BUTTLINES 17 TO 26 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

SHEAR-TIE AT STATION 1437 RIGHT SIDE OF LONGERON IS CRACKED. REPLACED SHEAR-TIE AT STATION 1437 BETWEEN LONGERONS 1 AND 2 PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN LONGERON 3 LEFT. SPLICED IN NEW SECTION OF LONGRON FROM STATIONS 150 TO 170 PER SRM 53-02-00.

Part: LONGERON CLIP — DAMAGED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

LEFT LONGERON 4 END CLIP AT STATION 148 HAS ELONGATED HOLES WHERE CLIP ATTACHES TO LONGERON. INSTALLED NEW LONGERON 4 LEFT END CLIP AT STATION 148 PER AARD 51-00-05-1 AND BOEING DRAWING 5911405.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN LONGERON 3 LAFT AT STATION 160. REMOVED CRACKED SECTION AND INSTALLED NEW SECTION OF LONGERON 3 LEFT FROM STATIONS 150 TO 170 PER SRM 53-14-01 FIGURE 3. INSTALLED LONGERON SPLICE AT STATION 170 PER SRM 51-30-05.

Part: LONGERON CLIP — DAMAGED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

LEFT LONGERON 3 END CLIP AT STATION 148 HAS ELONGATED HOLES WHERE CLIP ATTACHES TO LONGERON. INSTALLED NEW LONGERON 3 END CLIP AT STATION 148 PER AARD 51-00-05-1 AND BOEING DRAWING 5911405.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

RIGHT SIDE OF FUSELAGE HAS CRACK IN SKIN AT FASTENER HOLE AT STATION 1418 BELOW LONGERON 2 RIGHT. INSTALLED INTERNAL AND EXTERNAL DOUBLER AND FILLER PER SRM 53-04-00 FIGURE 40.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

LEFT TIE DOWN TRACK SPLICE FROM STATIONS 1212 TO 1227 CORRODED. INSTALLED NEW LEFT TIE DOWN TRACK SPLICE FROM STATIONS 1212 TO 1227 PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

STATION 1437 LONGERON 2 RIGHT HAS CRACK UNDER FRAME. REMOVED CRACKED PORTION OF LONGERON AND INSTALLED SERVICEABLE LONGERON AND LONGERON SPLICE AT STATION 1437 PER SRMS 53-02-00, 53-14-04, 51-60-00 AND AARD 53-00-00-05.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

CORROSION ON THE DOOR BEAM FROM STATIONS 1160 TO 1202. REMOVED CORROSION AND INSTALLED DOOR BEAM DOUBLER AS PER AARD 53-10-00-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN CUSP BETWEEN STATIONS 415 AND 419 RIGHT. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN LONGERON 4 LEFT AT STATION 160. INSTALLED NEW SECTION OF LONGERON AND RE-INSTALLED ORIGINAL SPLICES.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN LONGERON 4 LEFT AT STATION 160. INSTALLED LONGERON REPAIR PER SRM 53-02-00 AND BOEING DRAWING 5911406.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

FITTING CRACKED UNDER SEAT TRACK NUMBER 4 AT STATION 845. INSTALLED NEW FITTING PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

BOTTOM OF LEFT CUSP HAS CORROSION AT STATION 1143. INSTALLED CUSP SUPPORT AT STATION 1143 PER BOEING DRAWING 9930612 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

BOTTOM OF LEFT CUSP HAS CORROSION AT STATION 1175. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN CUSP FROM STATIONS 307 TO 310 RIGHT. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

RIGHT CUSP FROM STATIONS 1223 TO 1226 CORRODED. REMOVED CORROSION AND INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,498 hrs · 38,033 cycles

CORROSION ON CUSP RIGHT SIDE AT FUSELAGE STATIONS 1197 TO 1206. INSTALLED DOUBLER PER AARD.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 70,498 hrs · 38,033 cycles

FORWARD SERVICE DOOR HAS CRACK ON DOOR PAN AT DOOR HINGE LOWER CUTOUT. INSTALLED DOUBLER PER ESO 80177 AND EA MD80-52-028790.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

CRACK IN FASTENER HOLE AT FORWARD ENTRY DOOR SUB FLOOR, STATION 170 LEFT BUTTLINE 54. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 70,498 hrs · 38,033 cycles

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

Part: RIB — CRACKED (LE SLAT) · airframe 70,498 hrs · 38,033 cycles

LEFT NUMBER 5 SLAT SECOND FROM OUTBOARD END CRACK INDICATION. INSTALLED NEW ATTACH RIB PER ESO 80117.

Part: SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 68,907 hrs · 37,137 cycles

AUS - INFLIGHT DFW-LGA. CREW REPORTED BOTH PACKS CYCLED ON AND OFF 2 TIMES AND PRESSURIZATION FLOW LIGHT ILLUMINATED. FLIGHT DIVERTED AUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT SINGLE ENGINE SECOND CLIMB PRESSURE SWITCHES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,311 hrs · 36,225 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR-TIE PER AARD 51-10-11-5.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,369 hrs · 35,098 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO ROW 30 INOPERATIVE. REPLACED AND SECURED LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 65,369 hrs · 35,098 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 27D INOP. WIRE PULLED OUT OF CONNECTOR BELOW SEAT 27F. REPLACED PIN & SECURED CONNECTOR. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,369 hrs · 35,098 cycles

CEILING EMERGENCY LIGHTS FROM ROW 7 TO ROW 21 INOPERATIVE. REPLACED BATTERY AT ROW 20. OPS CHECK NORMAL.

Part: SENSOR — FAULTY (AC BAY) · airframe 64,171 hrs · 34,395 cycles

DFW - CREW REPORTED ON CLIMB OUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMP SENSOR BAD. REPLACED TEMPERATURE SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — FAILED (APU BAY) · airframe 63,919 hrs · 34,242 cycles

DFW - CREW REPORTED AUXILIARY POWER UNIT FAILED AND LEFT ENGINE GENERATOR ON PLACARD. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CHAFED (CABIN PRESSURE) · airframe 63,794 hrs · 34,169 cycles

DFW - CREW REPORTED DURING CLIMBOUT CABIN ALTITUDE WARNING ALERT SOUNDED AND MASTER WARNING LIGHT. BOTH PRESSURE CONTROLLERS FAILED. ALSO HAD MULTIPLE ALERTS DURING DESCENT AND CABIN CHIMES COMING ON. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WIRE V129A10 AT TOP LEFT SIDE OF 110 RELAY PANEL CHAFED CAUSING DAMAGED TO WIRE BUNDLE. REPLACED WIRES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — SEIZED (LEFT) · airframe 63,550 hrs · 34,034 cycles

EWR - INFLIGHT LGA-ORD. LEFT ENGINE FAILED ON TAKEOFF (SINGLE ENGINE TIME 5 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED EWR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON 05/06/2010 AT EWR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — BROKEN (CABIN) · airframe 62,123 hrs · 33,226 cycles

EMERGENCY LIGHT AT SEAT 4E HAS BROKEN LENS. REPLACED LENS AT SEAT 4E.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,123 hrs · 33,226 cycles

EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP AT SEAT 7D.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,953 hrs · 33,130 cycles

FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED BATTERY AND OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,725 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROWS 31 TO 32 INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHTS FROM ROWS 31 TO 32.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,725 hrs

LGA - LEFT AND RIGHT AFT EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT AFT CARGO COMPARTMENT.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 58,558 hrs · 31,696 cycles

GALLEY MOUNT FITTING CORRODED STATION 218 OUTBOARD OF NR 5 SEAT TRACK. INSTALLED NEW GALLEY MOUNT FITTING.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON OUTFLOW VALVE SUPPORT STRUCTURE AT STATION 1275 NEAR LONGERON 21 LEFT. REMOVED AND REPLACED INTERCOSTAL FROM STATION 1271-1287 PER SRM 51-30-05.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

LONGERON 30 CORRODED AT STATION 446-465. INSTALLED LONGERON "U" CHANNEL SPLICE IN LONGERON 30 PER SRM 53-02-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON RIGHT CUSP MEMBRANE STATION 560-579. INSTALLED NEW CUSP MEMBRANE STATION 503-598.

Part: FRAME — CRACKED (ZONE 200) · airframe 59,558 hrs · 31,696 cycles

FRAME AT STA 1418 L-2L TO L-2R HAS CRACKS. INSTALLED DOUBLER AND RADIUS BLOCK PER AARD 53-10-00-17.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 59,558 hrs · 31,696 cycles

RIGHT CARGO TIE DOWN TRACK CORRODED STATION 1231-1271. REPLACED TIE DOWN TRACK FORM STATION 1212 TO 1322.

Part: STRINGER — CORRODED (ZONE 100) · airframe 59,558 hrs · 31,696 cycles

LONGERON 30 CORRODED FROM STATION 465-494. INSTALLED LONGERON REPAIR AT STATION 465-494 PER ESO 80559 DATED 11/04/2008.

Part: STRINGER — CORRODED (ZONE 100) · airframe 59,558 hrs · 5,244 cycles

LONGERON 29 LEFT CORRODED FROM STATION 484 TO 494. INSTALLED LONGERON REPAIR PER ESO 80559 DATED 11/04/2008.

Part: WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON SUBFLOOR, STATION 200 TO 218 BETWEEN NUMBER 4 AND NUMBER 5 SEAT TRACKS. REPAIRED PER AARD 53-20-00-16, INSTALLED DOUBLER.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON CUSP BETWEEN STATION 256 TO 275 LEFT SIDE. INSTALLED NEW CUSP MEMBRANE FROM STATION 237 TO 313.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON SKIN SPLICE FINGER DOUBLER STATION 1245 TO 1310 AT LONGERON 26L. REMOVED AND REPLACED SKIN SPLICE FINGER DOUBLER AND INSTALLED LONGERON SPLICES AT STATION 1240 AND 1310 PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON CUSP AT STATION 503 TO 617. REPLACED CUSP PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

SEAT TRACK NR 2 CORRODED STATION 1221 TO 1307. REPLACED SEAT TRACK SECTION FROM STATION 1031 TO 1309 PER AARD 51-010-00-012.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

WEB CRACKED AT NUTPLATE, STATION 1215 LONGERON 28R. STOP DRILLED CRACK AND REPAIRED PER ESO 80559 DATED 11-06-08.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,588 hrs · 31,696 cycles

AFT CARGO, CRACK IN INTERCOSTAL AT STATION 1271 TO 1287. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CABIN FLOOR SUPPORT, INTERCOSTAL CRACKED AT STATION 1287 TO 1209. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

VERTICAL ANGLE ABOVE VAULT DOOR JAMB FORWARD SIDE OF AFT PRESSURE BULKHEAD CRACKED AT STATION 1338. REMOVED AND REPLACED ANGLE PER SRM 53-30-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON T-ANGLE AT STATION 1155 AT LONGERON 28R. REMOVED AND REPLACED T-ANGLE PER SRM 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,588 hrs · 31,696 cycles

CORROSION ON CUSP AT STATION 598 TO 617 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

SEAT TRACK NR 2 CORRODED FROM STATION 1031-1221. REPLACED SEAT TRACK.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

CRACK IN CUSP MEMBRANE STATION 219 UNDER SEAT TRACK NUMBER 5. FABRICATED AND INSTALLED DOUBLER.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

LONGERON 4 LEFT CRACKED AT STATION 180 AND 200. SPLICED IN A NEW SECTION OF LONGERON.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 316,996 cycles

LEFT CUSP MEMBRANE CORRODED STATION 1022. INSTALLED NEW CUSP SHEET PER AARD 51-00-00-12.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 59,558 hrs · 31,696 cycles

CORROSION ON RIGHT CUSP AT STATION 1281 TO 1309. REMOVED AND REPLACED CUSP FROM STATION 1250 TO 1309 RIGHT SIDE PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · airframe 59,588 hrs · 31,696 cycles

CORROSION ON FORWARD CARGO DOOR PAN STATION 370-427. SPLICED IN NEW SECTION OF PAN STATION 370-427.

Part: SKIN — SEPARATED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

FUSELAGE SKIN SEPARATED AT BOTTOM FORWARD CORNER OF THE AFT LAVATORY SERVICE PANEL. INSTALLED DOUBLER ON BOTTOM HALF OF SKIN AT AFT LAVATORY SERVICE PANEL CUT-OUT PER ESO 80559 DATED 11/05/2008.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 59,558 hrs · 31,690 cycles

CORROSION ON CUSP T AT RIGHT SIDE AT STATION 598. INSTALLED SPAR SECTION OF TEE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

MID CARGO DOOR BEAM CORRODED STATION 637-693. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

SUB FLOOR WEB CORRODED, STATION 160-200, JUST INBOARD OF THE FORWARD SERVICE DOOR. INSTALLED DOUBLER STATION 160-200 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,558 hrs · 31,969 cycles

LEFT CUSP MEMBRANE CRACKED AT STATION 1250 BELOW THE NUMBER 2 SEAT TRACK. INSTALLED NEW SECTION OF CUSP FROM STATION 1174-1250 PER AARD 53-20-00-16.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 59,558 hrs · 5,094 cycles

BROKEN TANG ON SEAT TRACK NUMBER 3 AT STATION 1060. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: STRAP — CRACKED (FUSELAGE)

TEE STRAP CRACKED STATION 207 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-011.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,588 hrs · 31,696 cycles

CRACKED TANG ON WEB AFT OF THE FWD ENTRY DOOR STATION 208 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

RIGHT CUSP MEMBRANE CORRODED STATION 886-905. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

RIGHT CUSP MEMBRANE CORRODED AT STATION 1197 - 1200. INSTALLED CUSP DOUBLER STATION 1197-1200 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

RIGHT CUSP MEMBRANE CORRODED STATION 655-674. INSTALLED CUSP DOUBLER STATION 654-670.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,558 hrs · 31,696 cycles

RIGHT CUSP MEMBRANE CORRODED FROM STATION 1174 TO 1193. INSTALLED NEW CUSP MEMBRANE.

Part: DUCT — LEAKING (A/C PACK) · airframe 58,413 hrs

ORD INFLIGHT T564/30MAY. AT FLIGHT LEVEL 310 PRESSURIZATION FLOW LIGHT ILLUMINATED AND THE CABIN ALTITUDE WAS CLIMBING AT 300 TO 500 FEET PER MINUTE. DECLARED AN EMERGENCY AND BEGAN A DESCENT. DURING DESCENT CREW TURNED ON ANTI ICE TO THE TAIL AND THE PRESSURIZATION RETURNED TO NORMAL. LANDED ORD WITHOUT INCIDENT. REPLACED BLOWN DUCT IN RIGHT AIR CONDITIONING PACK SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY OVERWING EXIT LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERWING EXIT LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 46,803 hrs · 24,532 cycles

THE AFT EXIT DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPAIRED BROKEN WIRES IN CEILING. CHECK-C 6-17-03 STL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,316 hrs · 23,625 cycles

THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 45,060 hrs · 23,479 cycles

HYDRAULIC FLUID LEAK FROM B-NUT ON LT ANTI-SKID CONTROL VALVE. TIGHTENED B-NUT AND RESERVICED HYDRAULIC SYSTEM. LAST CHECK C PERFORMED 07/31/2002 IN STL -- CLOSED--

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,475 hrs · 21,301 cycles

FOUND 2 HI-LOKS PULLED THRU FUSELAGE SKIN AT LONGERON 24L, AFT AND BELOW THE LAV SERVICE DOOR. CUT OUT DAMAGED LONGERON. SPLICED IN NEW SECTION PER SRM 53-02, FIG 18. CHECK-C 10-20-00 MCI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND DENT WITH CRACK IN SKIN ON RT SIDE AT CANTED STA 1500, ABOVE TAIL CONE WARNING STENCIL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2 PAGE 69.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND ANGLE CRACKED AT FWD INBD CORNER OF LT MAIN GEAR WELL. REMOVED CRACKED CHANNEL. INSTALLED NEW CHANNEL PER SPM 6-70-01 PAGE 3, SRM 51-6-00, SRM 51-30-2, SRM 51-30-5, AND DOUGLAS DRAWING 5930584.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FRAME AT STA 1308 BETWEEN STRINGER 23L AND 23R. REMOVED CORROSION PER SPM 6-80-01. PRIMED AND PAINTED PER SRM 51-10-03. REPLACED FRAME PER SRM 53-03-2A.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE AFT CARGO DOOR FRAME WAS CRACKED ON FWD SIDE AT TORQUE TUBE. REPAIRED PER SRM 52-05, FIG 26A.

Part: STRUCTURE — CORRODED (LAV PANEL) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON LAV SERVICE PANEL BACK SIDE, AROUND FILL LINES AT STATION 1320L. REMOVED CORROSION PER SPM 80-01 AND REPLACED PANEL. TREATED WITH PAINT. INSTALLED PER ARA 17160 AND SRM 51-30-3 HI-LOKS. LONGERON SPLICE PER 53-02 FIG 18.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE RT CARGO TIE DOWN TRACK WAS CORRODED AT STA 1212 TO 1308. REMOVED AND REPLACED TRACK PER SPM 6-70-01. INSTALLED PER SRM 51-30-1.

Part: FLANGE — CRACKED (CARGO DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND FLANGE CRACKED IN FORWARD LOWER CARGO COMPT DOOR AT AFT LATCH. REPAIRED PER SRM 52-05, FIG 26A.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT THE AFT CARGO DOOR FRAME WAS CRACKED AT TORQUE TUBE, AFT SIDE OF DOOR. STOP DRILLED CRACK. APPLIED SEALER AND INSTALLED DOUBLER WITH HI-LOKS PER SRM 52-05, FIG 26A, 1 AND 2, AND SRM 51-30-5. HIGH FREQ EDDY CURRENT INSP PER NDT MANUAL PART 6, 51-00-03 CRACK CONTAINED.

Part: FLANGE — CRACKED (CARGO DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND FLANGE CRACKED AT FWD LOWER DOOR AT FWD LATCH. ACCOMP HIGH FREQ EDDY CURRENT INSPECTION PER NDT MANUAL PART 6, 51-00-03 FOR CRACK CONTAINMENT. INSTALLED DOUBLER PER SRM 52-05, PAGE 110A.

Part: FLANGE — CRACKED (CARGO DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND FLANGE CRACKED AT FWD LOWER DOOR AT FWD LATCH. ACCOMP HIGH FREQ EDDY CURRENT INSPECTION PER NDT MANUAL PART 6, 51-00-03 FOR CRACK CONTAINMENT. INSTALLED DOUBLER PER SRM 52-05, PAGE 110A.

Part: FRAME — CORRODED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN AFT CARGO BIN CORROSION WAS FOUND ON FORMER AND REPAIR ANGLE AT STA 1322, STRINGER 28L TO 30, AND FASTENERS WERE RUSTY. REMOVED FRAME AND REPAIR ANGLE FOR CORROSION REMOVAL. RE-INSTALLED FRAME AND REPAIR ANGLE PER SRM 53-03 FIG 2A. INSTALLED HI-LOK PER SRM 51-30-5. INSTALLED RIVETS PER 51-30-2. TREATED PER 51-10-3 PAGE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT THE CABIN FLOOR TRACK WAS DAMAGED AND CORRODED AT STA 200 TO 332, RBL 44 IN, NUMBER 4 TRACK. REPLACED NUMBER 4 TRACK FROM STA 200 TO 341 PER SPM 6-70-01 PAGE 2 AND 3 ITEM 4, SRM 53-05 FIG 4F, SRM 51-60-0. TREATED TRACK PER SRM 51-10-3.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR TRACK AT STA 1031 TO 1308, LBL 44 INCHES. REMOVED NUMBER 2 CHAIR TRACK STA 1031 TO 1306. INSTALLED NEW SECTION OF TRACK. SPLICE REPAIR PER SRM 53-05 FIG 4 AND 5. TRACK INSTALLED WITH NUTS, WASHERS, BOLTS, AND TRACK TO WEB WITH RIVETS PER SRM 51-30-1 AND SRO 51-103 AND SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT AT STA 160 TO 200, RBL 7, 40 INCHES OF FLOOR SUPPORT WAS CORRODED, C2 GALLEY AREA. REMOVED FLOOR SUPPORTS FROM STA 148 TO 200. MADE NEW AND INSTALLED WITH BOLTS PER SRM 51-30-1.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT AT STA 148 TO 200, RBL 58, A 51 INCH SECTION OF THRESHOLD COVER PLATE WAS CORRODED. INSTALLED NEW SECTION OF THRESHOLD COVER PLATE AFTER CORROSION WAS REMOVED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED AT CLIP NUT HOLE STA 1212 TO 1320. INSTALLED NEW TRACK PER SPM 6-70-01.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN AFT CARGO BIN THE AFT DOOR JAM BEAM AT STA 1155 TO 1212 WAS CORRODED AND GROUND BEYOND LIMITS PER SRM 53-05 PAGE 174 FIG 63. REPLACED BEAM PER MDD 5930483 AND SRM 51-60-0.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, AT STA 200, RBL 58 INCHES, THE LOWER CORNER OF DOOR JAMB AREA WAS CORRODED. REMOVED AND REPLACED CORRODED CUSP FROM STA 170 TO 218, PER REPAIR DRAWING J060288. INSTALLED RIVETS PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE LT ELEVATOR HAD STATIC BURN ON UPPER AND LOWER SURFACE OF ELEVATOR AT LOWER T/E OTBD END. ACCOMP NDT PER NDT MANUAL PART 6, 51-00-06, AND NO CRACKS FOUND. REPAIRED PER SRM 51-01, FIG 2. WT AND BALANCE RECALCULATED PER SRM 55-20-02. MATERIAL LIST 43 GRAMS REMOVED, 82 GRAMS ADDED. TOTAL WEIGHT ADDED 39 GRAMS. INSTALLED NEW PLACARD.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND FUSELAGE DENT BETWEEN LONGERON 29L AND 29R, STA 389. A 5 IN BY 0.375 IN BY 0.050 DEEP. CUT OUT DAMAGE AND REPAIRED PER SRM 53-04 FIG 35 AND SEALED PER SRM 51-20-0.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND CORROSION AND CRACK IN MEMBRANE AT STA 200 TO 208, RBL 55. MADE AND INSTALLED NEW MEMBRANE WITH RIVETS PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND 9 INCH SECTION OF FLOOR SUPPORT CORRODED AT STA 160, BETWEEN RBL 44 AND 53. REMOVED OLD FLOOR SUPPPORT, MADE NEW AND INSTALLED WITH HI-LOKS PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND A 12 INCH SECTION OF FLOOR SUPPORT CORRODED BETWEEN STA 148 AND 160, RBL 44. REMOVED CORROSION PER SPM 6-80-1 AND TREATED AREA PER SRM 51-10-3. REINSTALLED FLOOR SUPPORT WITH RIVETS PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND DENT IN SIDE OF FUSELAGE AFT OF THE RT FWD DOOR AT CUSP LINE, LONGERON 18L, STA 213. CUT OUT DAMAGED SKIN. REMOVED OLD FINGER DOUBLER AND MADE NEW FINGER DOUBLER. REPAIRED PER SRM 53-04 FIG 38 SHEET 33.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND 40 INCHES OF FLOOR SUPORT CORRODED AT STA 160 TO 200, RBL 7. REMOVED FLOOR SUPPORT FROM STA 148 TO 200, MADE NEW AND INSTALLED WITH BOLTS PER 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND 34 INCH SECTION OF FLOOR SUPPORT CORRODED AT STA 180, BETWEEN RBL 7 TO RBL 44. MADE NEW FLOOR SUPPORT WITH TWA S/N 56-2789. INSTALLED WITH RIVETS PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FLOOR WEB WAS CORRODED IN SEVERAL LOCATIONS AT STA 200 TO 218, RBL 44 TO RBL 56. INSTALLED NEW MEMBRANE WITH RIVETS, PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND 37 INCH SECTION OF FLOOR SUPPORT CORRODED AT STA 200, FROM RBL 7 TO RBL 44. INSTALLED NEW FLOOR SUPPORT FROM TWA S/N 56-2789 AND INSTALLED WITH RIVETS PER SRM 51-30-2 AND HI-LOKS PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT AT STA 160 TO 200, RBL 44, A 38 INCH SECTION OF FLOOR SUPPORT WAS CORRODED. REMOVED OLD FLOOR SUPPORT AT STA 160 TO 200. MADE NEW AND INSTALLED WITH RIVETS PER SRM 51-30-7 AND HI-LOKS PER SRM 51-30-5.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT AT STA 160 TO 180, BETWEEN RBL 7 AND RBL 42, HAD FLOOR WEB CORRODED IN NUMEROUS LOCATIONS. REMOVED CORROSION PER SPM 6-80-1 AND TREATED AREA PER SRM 51-10-3. REINSTALLED RIVETS PER SRM 51-30-2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT THE AFT LOWER FUSELAGE REPAIR AT STA 1322 BETWEEN LONGERON 30 AND 29L HAD ONLY SINGLE ROW OF FASTENERS, 7 INCHES AFT OF LT FWD CORNER OF REPAIR. REMOVED PREVIOUS REPAIR AND REINSTALLED NEW REPAIR PER SRM 53-04, FIG 12B PAGE 43 SHEET 6. TREATED PER SRM 51-10-02. SEALED PER SRM 51-20-0.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT THE FWD LT PASSENGER DOOR INTERCOSTAL WAS CRACKED APPROX 1 INCH, MID AREA OF DOOR HANDLE PAN, OUTBOARD EDGE. REPLACED INTERCOSTAL PER DRAWING 5910081, (P/N 9955763-11).

Part: SKIN — DENTED (RT WING SLAT) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT ON THE RT WING FOUND 2 DENTS TOGETHER 16 INCHES TO 18 INCHES OUTBOARD OF THE INBOARD END OF THE NR 2 L/E SLAT, .5 IN BY .75 IN BY 0.050, AND .75 BY .75 BY 0.020. ACCOMP HFEC OF AREA PER NDT 51-00-03 PART 6 AND NO DEFECT FOUND. REPAIRED PER SRM 57-09-10A AND ARA 17153.

Part: STRUCTURE — DAMAGED (RT WING SLAT) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT ON THE RT WING L/E OUTBOARD END OF NUMBER 1 L/E SLAT HAD A PREVIOUS DENT IN L/E WITH FILLER COMING OUT. ACCOMP HIGH FREQ EDDY CURRENT OF DENT PER 51-00-03, PART 6 OF NDT MANUAL AND NO CRACKS. MEASURED DENT 0.140 IN DEEP. REPAIRED PER SRM 57-09 FIG 10A.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT AT STA 200 TO 247, RBL 22 INCHES, A 47 INCH SECTION OF NUMBER 3 FLOOR TRACK WAS CORRODED. REMOVED CORRODED TRACK SECTION FROM STA 200 TO 247. SPLICED NEW TRACK SECTION PER SRM 53-05.

Part: WEB — CORRODED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN THE MID CARGO COMPT, CORROSION WAS FOUND ON MEMBRANE AREA OF CEILING AT LONGERON 18R, STA 522 THRU 579. REMOVED CORRODED MEMBRANE FROM STA 503 TO 579. SHOP FABRICATED MEMBRANE. INSTALLED WITH RIVETS PER SRM 51-30-2, HI-LOKS PER 51-30-5; NUTS, BOLTS WASHERS PER TWA SPM 6-30-07.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND SKIN DENTED AT STA 275 TO 313 AT LONGERON 23 TO 26. CUT OUT DAMAGE AND REPAIRED PER 53-04-12C. LONGERON REPAIR SPLICE MOVED PER 53-02 FIG 18 PER EMLR 71329.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE FWD RT SERVICE DOOR ANGLE WAS CRACKED AT LOWER HINGE OF DOOR, BOTTOM SIDE OF HINGE INSIDE DOOR. INSTALLED NEW RIB, INSTALLED RIVETS AND HI-LOKS PER SRM 51-30-3 AND 51-30-5.

Part: FITTING — CRACKED (LT WING SPOILER) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, LT WING GROUND SPOILER AFT ACTUATOR ATTACH FITTING HAD A 1.5 INCH LONG CRACK ON I/B SIDE OF FITTING. CRACK CONTAINED STOP DRILLED CRACK PER MD80 80-57-180. INSTALLED DOUBLER FILLER AND STIFFENER PER 80-57-180.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR TRACK AT LBL 55 INCHES, STA 1250 TO 1275, 1231 TO 1250, AND 1172 TO 1193. REMOVED CHAIR TRACK AT ALL THREE LOCATIONS AND REPLACED WITH NEW PER SPM 6-70-01. INSTALLED CHAIR TRACK PER SRM 51-30-1.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE FWD CARGO FLOOR ATTACH ANGLE WAS CORRODED AT BOTTOM OF FASTENER HOLE ABOVE LONGERON 30, STA 427. INSTALLED NEW ANGLE WITH AD RIVETS 6-6. INSTALLED ANGLE TO BEAM WITH HI-LOK''S TWA (P/N 72-5019) PER SRM 51-30-5.

Part: SKIN — DENTED (CARGO DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE AFT EDGE OF THE MID CARGO DOOR HAD A DENT TO THE DOOR, 2.5 BY .375 BY 0.062. ACCOMP HIGH FREQ EDDY CURRENT PER 51-00-03 PARAGRAPH 6 OF NDT MANUAL AND NO CRACKS. REPAIRED DOOR EDGE PER SRM 52-05, PAGE 1 AND SRM 52-04.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FRAME FOOT AT STA 1287, BETWEEN LONGERON 28R AND 29R, AND BETWEEN LONGERON 25L AND 26L. INSTALLED NEW FORMER FOOT AT BOTH LOCATIONS PER DRAWING 9957739. INSTALLED HI-LOKS PER SRM 51-30-5. INSTALLED RIVETS PER SRM 51-30-2.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, CORROSION WAS FOUND ON LONGERON 25L, AT STA 1322 TO 1332. REPLACED LONGERON TIE FITTING WITH NEW PER SRM 6-70-01. REPLACED HI-LOKS PER SRM 51-30-5. REPLACED RIVETS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON THE LOWER LIP OF CABIN CHAIR TRACK AT CLIP NUT AREA, STA 1224, LBL 23. REMOVED OLD CHAIR TRACK AND INSTALLED NEW TRACK FROM STA 1085 TO 1309, WITH SPLICE AT STA 1085, PER SRM 53-05, FIG 4F.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CHAIR TRACK BEYOND REPAIR AT LBL 22, STA 1088 TO 1309. INSTALLED NEW TRACK FROM STA 1088 TO 1309 PER SRM 53-05, FIG 4F AND 51-30-1.

Part: STOP — CRACKED (PAX DOOR) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CRACK AT DOOR STOP CASTING, LT SIDE OF REAR BULKHEAD DOOR JAM, 18 INCHES ABOVE FLOOR AND ANOTHER CRACK 36 INCHES ABOVE THE FLOOR. REMOVED AND INSTALLED NEW CASTINGS AT BOTH LOCATIONS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND I/B FLANGE OF CHAIR TRACK WITH CORROSION AT CLIP NUT AREAS, STA 1195 TO 1305, LBL 22. INSTALLED NEW TRACK FROM STA 1088 TO 1309 PER SRM 53-05 AND 51-301.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON O/B CHAIR TRACK, STA 746, RBL 44. REMOVED CORROSION PER SPM 6-80-01. TREATED METAL PER SRM 51-10-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON MAIN FRAME AT STA 1250, BETWEEN LONGERON 29R AND 29L. REMOVED CORROSION PER SPM 6-80-01. PRIMED PER SRM 51-10-3. INSTALLED RIVETS PER 51-30-02.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, THE CABIN FLOORBEAM CAP FLOOR SUPPORT WAS CORRODED AT STA 1250, LBL 22 TO LBL 44, WL 200. REPLACED FLOOR SUPPORT (P/N 5930544-97). INSTALLED PER SPM 6-70-01 AND DRAWING 5930544 AND SRM 53-01.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT FOUND IN CABIN, CORROSION ON FLOORBEAM CAP AT STA 1155, LBL 22 INCHES TO 44 IN. REPLACED FLOOR SUPPORT (P/N 5930544-97). INSTALLED PER SPM 6-70-01 AND DRAWING 5930544 AND SRM 53-01.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON INTERCOSTAL BETWEEN STA 1271 AND STA 1250, LONGERON 25L. REMOVED CORROSION PER SPM 6-80-01. PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-3.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON LONGERON 30 BETWEEN STA 1312 AND 1306, LONGERON 27L AT STA 1298, AND LONGERON 22L AT STA 1300. CLEANED AND TREATED PER SRM 51-10-03 AND INSTALLED FASTENERS PER SRM 51-30-05.

Part: SEAL — CRACKED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CRACK AT FWD END OF UPPER SLIDING SEAL. REMOVED CRACKED DOUBLER AND FABRICATED AND INSTALLED NEW DOUBLER AND INSTALLED MISSING SHIM PER SRM 55-03 FIG 17, SHEET 1 TO 7 PAGES 34 TO 40, AND DOUGLAS DRAWING SR09550008.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FRAME FOOT AT STA 1308, BETWEEN LONGERON 26L AND 27L. TREATER PER SRM 51-70-03 AND INSTALLED FASTENERS PER 51-30-02.

Part: DOUBLER — CORRODED (CARGO BAY) · airframe 39,476 hrs · 20,182 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON FUSELAGE DOUBLER AT STA 1300 BETWEEN LONGERONS 26L AND 27L. REMOVED CORROSION PER SPM 6-80-01. PRIMED PER SRM 51-05-3. FASTENERS INSTALLED PER 51-30-2.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 38,871 hrs · 19,834 cycles

DURING CRUISE, THE FIRST OFFICERS WINDSHIELD CRACKED. REPLACED WINDSHIELD (P/N 5912290-506) AND TEMP CONTROLLER (P/N 617-2). 0004 5-4-00 JFK.

Part: LIGHT — INOPERATIVE (ROW 12 - 20)

THE EGRESS TRACK LIGHTS WERE INOPERATIVE FROM ROWS 12 THRU 20, AND BOTH FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY (P/N 60-0304-51) EGRESS LIGHTS, AND FOR THE EMERGENCY LIGHTS REPLACED POWER SUPPLY (P/N 803900-1). CHECK-C 8-9-99 MCI.

Part: BATTERIES — DISCHARGED (CABIN)

FOUND EMERGENCY CEILING LIGHTS INOPERATIVE AT ROWS 12,15, 17, 19, 21, 23, 24, 26, AND 28. THE EMERGENCY EXIT LIGHTS BY ROW 22 OVER THE WING, AND THE TAIL CONE EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERIES AT STATIONS 170, 480, 580, 880, 1050, AND 1350. CHECK-C 8-9-99 MCI.

Part: CSD — WORN (LT ENGINE)

FLIGHT LEFT STL WITH LT GENERATOR PLACARDED INOPERATIVE PER MEL. IN FLIGHT THE APU GENERATOR WENT OFF LINE AND AC CROSSTIE LOCKOUT LIGHT CAME ON. UNABLE TO RESET. MADE UNSCHEDULED LANDING AT MCI. REPLACED THE LT ENG CSD. PLACARDED THE APU GENERATOR INOPERATIVE PER MEL. CHECK-C 8-2-98 STL. *S/D* RESTORED THE APU BY REPLACING THE FUEL CONTROL, (P/N 3608000-10), AND THE GENERATOR, (P/N 976J252-8).

Part: OIL SYST — OVERSERVICED (APU)

IN CLIMB EXPERIENCED HEAVY BURNING SMELL IN ACFT. TURNED OFF RT PACK. SMELL RETURNED WHEN WAITING FOR A GATE ON THE GROUND. FOUND OIL LEAKING ON INLET SIDE OF APU DUCT. PLACARDED APU INOP. LATER CLEANED APU COMPT AND SURROUNDING AREA. RAN APU FOR 2 HOURS AND NO LEAKS OR ODOR. POSSIBLE SERVICING PROBLEM. CHECK-C 8-2-98 STL.

Part: SENSOR — FAILED (RT MLG)

SAN - FLT 203 - AT GEAR EXTENSION, THE RT MAIN GEAR RED LIGHT ILLLUMINATED AND THE UNSAFE HORN SOUNDED. PERFORMED PROXIMITY BOX SELF-TEST AND CHECKED DOWNLOCK PROXIMITY SENSOR AND TARGET. OP-15 3-6-97 JFK. (X)

Part: DUCT — CRACKED (NR 2 ENGINE)

PHX - FLT 179 - DURING CRUISE, TAIL CONE AND DUCT SEPARATED FROM NR 2 ENGINE, SN 1212, DUE TO FATIGUE CRACKS. REPLACED DUCT, MFG PN 809127-01, MANUFACTURED BY PRATT AND WHITNEY, AND CONE, MFG PN HA8809128-01, MANUFACTURED BY JET AVION CORP. OPERATIONAL CHECK NORMAL. ENGINE TOTAL HOURS, 24,060 HOURS; 12,155 CYCLES. OP-16 - 8-5-96 - MCI. (X)

Part: FRAME — CORRODED (BS 1174)

MCI - DURING OP-16, FOUND CORROSION ON AFT SIDE OF FS 1174 FRAME WEB BETWEEN STRINGERS 29L AND 30L. REMOVED CORROSION PER SRM 51-10-03 AND REPAIRED FRAME PER SRM 53-01, PAGE 3. (M)

Part: LONGERON — CORRODED (BS 1309)

MCI - DURING OP-16, FOUND CORROSION ON LONGERON 5-30 TOP LEFT FLANGE, AFT OF FORMER BS 1309. REPAIRED PER SRM 51-01. (M)

Part: FRAME — CORRODED (BS 1309)

MCI - DURING OP-16, FOUND CORROSION ON LOWER SIDE OF FRAME, STATION 1309, LONGERON 25R TO 26R. REPAIRED PER SRM 53-03, FIGURE 2A AND TWA STANDARD PRACTICES. (M)

Part: SEAT TRACK — CORRODED (BS 1211-1320)

MCI - DURING OP-16, FOUND CORROSION AT FLOOR TRACK, STATION 1211 TO 1320, RIGHT SIDE. REPLACED FLOOR TRACK PER SRM 51-01, PAGE 1 AND TWA STANDARD PRACTICES. (M)

Part: SUPPORT — CORRODED (BS 200)

MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT AND STRUCTURE, FS 200, RBL 6 TO RBL 42. REPAIRED BY INSTALLING NEW FLOOR SUPPORT ANGLE PER SRM 57-01.

Part: LONGERON — CORRODED (BS 1300-1322)

MCI - DURING OP-16, FOUND CORROSION ON LONGERON 25R INBOARD FLANGE AT FASTENER HOLES, STATION 1309. REPLACED TRACK STATION 1300 TO 1322 PER SRM 51-01, PAGE 1, ITEM C AND INSTALLED SPLICE PER SRM 53-03, FIGURE 5. (M)

Part: SEAT TRACK — CORRODED (BS 1311-1320)

MCI - DURING OP-16, FOUND CORROSION AT RIGHT FLOOR TRACK, STATION 1311 TO STATION 1320. REMOVED AND REPLACED FLOOR TRACK PER SRM 51-01 AND TWA STANDARD PRACTICES. (M)

Part: SEAT TRACK — CORRODED (CABIN)

MCI - DURING OP-16, FOUND CORROSION AT LBL 44 CHAIR TRACK FLANGE, FS 1212, 1250, 1257, 1296. REPLACED PART PER SRM 51-10-01 AND TWA STANDARD PRACTICES. (M)

Part: INTERCOSTAL — CORRODED (BS 1250-1271)

MCI - DURING OP-16, FOUND CORROSION ON INTERCOSTAL TOP SURFACE, FS 1250 TO FS 1271, STRINGER 25L. REMOVED CORROSION PER SRM 51-10-03 AND REPLACED INTERCOSTAL PER SRM 51-01, PAGE 1, ITEM C. (M)

Part: BYPASS VALVE — OUT OF POSITION (LANDING GEAR)

JFK - FLT 253 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT AND LANDING GEAR UNSAFE LIGHTS ILLUMINATED. PLACED LANDING GEAR SELECTOR TO DOWN AND ALL DOWN, AND LOCKED INDICATION ILLUMINATED. VERIFIED LANDING GEAR DOWN. FOUND LANDING GEAR BYPASS VALVE IN THE BYPASS POSITION. STOWED AND LATCHED LANDING GEAR BYPASS VALVE. GROUND CHECKS OF LANDING GEAR CHECKED NORMAL. CHECK C-1D - 11-14-94 - MCI.