N948TW

Part: SENSOR — FAULTY (LE SLAT) · airframe 70,505 hrs · 36,915 cycles

STL CREW REPORTED SLAT DISAGREE LIGHT INTERMITTENT IN FLIGHT. "SLAT OVERSPEED" AUDIO WARNING CONTINUOUS ABOVE 280 KTS. FLIGHT LANDED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT SLAT A SENSOR. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: ENGINE — SHUTDOWN (LEFT) · airframe 69,650 hrs · 36,474 cycles

LIT INFLIGHT CLT-DFW CREW REPORTED LT ENGINE SHUTDOWN WITH NO ABNORMAL INDICATIONS OR WARNINGS, SINGLE ENGINE TIME 15 MINUTES. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE AT LIT ON 08/26/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: DUCT — LEAKING (AC BAY) · airframe 68,956 hrs · 36,098 cycles

CREW REPORTED TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LEAKING RT DUCT. SYS GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK IN SKIN ON RIGHT INBOARD SIDE OF RADOME HINGE CUTOUT. INSTALLED DOUBLER AND FILLERS PER SRM 53-05-00 FIGURE 77 SHEETS 1 AND 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CORROSION ON CUSP FROM STATIONS 364 TO 365. INSTALLED DOUBLER FROM STATIONS 360 TO 367 PER AARD 53-20-00-16.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 68,303 hrs · 35,773 cycles

LEFT AFT OVERWING EXIT DOOR IS CRACKED ON THE UPPER LEFT SIDE OF THE INNER SKIN. INSTALLED DOUBLER PER EA COMP-52-029017.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CORROSION ON SEAT TRACK NUMBER 6 FROM STATIONS 1024 TO 1030. REPLACED NUMBER 6 SEAT TRACK FROM STATIONS 797 TO 1030 RIGHT PER MM 53-40-20-01-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CORROSION ON SEAT TRACK NUMBER 6 AT STATIONS 790 TO 791. INSTALLED SEAT TRACK PLUG AND SPLICE STRAP AT SEAT TRACK NUMBER 6 RIGHT, FROM STATIONS 789 TO 792 PER SRM 53-05-00 FIGURE 4A.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

LEFT UPPER CUSP FROM STATIONS 978 TO 980 HAS DEEP CORROSION. INSTALLED DOUBLER CUSP FROM STATIONS 978 TO 980 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

AFT SERVICE DOOR AREA, CORROSION ON NUMBER 1 SEAT TRACK GALLEY MOUNT HOLE AT STATION 1176. INSTALLED NEW SEAT TRACK FROM STATIONS 1174 TO 1309 LEFT SIDE PER AMM 53-40-01-2 AND SRM 51-30-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

THE 1485 CANT FRAME CRACKED BELOW STAIR RET ACTUATOR. INSTALLED CANT FRAME SPLICE REPAIR AND FRAME STIFFENER AT STATION 1485 PER AARD 53-10-00-33.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CROWN AREA, STATION 465 AND LONGERON 4 RIGHT, INBOARD LONGERON LEG CRACKED. INSTALLED LONGERON SECTION AND SPLICE FROM STATIONS 438 TO 474 PER SRM 53-02-00 FIGURE 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK IN SKIN AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04-02 FIGURE 2 SHEET 29.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

SHEAR TIE CRACKED AFT SIDE OF 1437 ABOVE LONGERON 17 LEFT. INSTALLED SHEAR TIE AT STATION 1437 ABOVE LONGERON 17 LEFT PER AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CORROSION ON SUBFLOOR UNDER AFT INBOARD G-2 GALLEY MOUNT FITTING AT STATION 217 RIGHT AND RIGHT BUTTLINE 11. INSTALLED SUBFLOOR DOUBLER AT STATION 217 RIGHT UNDER AFT INBOARD G-2 GALLEY MOUNT FITTING PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,303 hrs · 35,773 cycles

HEAVY CORROSION ON RIGHT CUSP AT STATION 881. INSTALLED DOUBLER AT STATION 881 PER AARD 53-20-00-16.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 68,303 hrs · 35,773 cycles

FORWARD SERVICE DOOR CRACKED AT FORWARD END OF TOP DOOR BEAM. REPLACED BEAM PER ESO 80177.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,303 hrs · 35,773 cycles

CORROSION ON THE FITTING AT THE LOWER FORWARD CORNER OF THE DOOR CUTOUT AT STATION 636. INSTALLED SUPPORT BRACKET PER AARD 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER AFT CLIP AT STATION 902. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN TOP AFT CLIP AT STATION 1021. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN TOP AFT CLIP AT STATION 1040. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER FORWARD CLIP AT STATION 1175. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

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

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER AFT CLIP, STATION 1211. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER AFT CLIP, STATION 1230. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER, FORWARD CLIP AT STATION 1099. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT HAND WINDOW PAN LOWER AFT CLIP STATION 902. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN TOP AFT CLIP STATION 1021. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN TOP AFT CLIP STATION 1040. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,303 hrs · 35,773 cycles

CRACK AT RIGHT WINDOW PAN LOWER AFT CLIP STATION 1097. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 68,303 hrs · 35,773 cycles

COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. RESEATED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECKS NORMAL.

Part: GENERATOR — FAILED (RIGHT) · airframe 67,602 hrs · 35,442 cycles

SHV - INFLIGHT ATL-DFW. CREW REPORTED RIGHT GENERATOR FAILED AND AUXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT DIVERTED SHV LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARD RIGHT GENERATOR PER MEL. REPLACED RIGHT GENERATOR AND CONSTANT SPEED DRIVE AT DFW ON 11/06/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: O-RING — DEFECTIVE (CSD) · airframe 63,922 hrs · 33,557 cycles

BNA - INFLIGHT EWR-DFW. CREW REPORTED RIGHT CONSTANT SPEED DRIVE OIL QUANTITY LOW. SHUTDOWN RIGHT CSD WITH LEFT CSD ON MEL EMERGENCY WAS DECLARED. FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BAD O-RING ON CSD FILL PORT. REPLACED RIGHT CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 63,315 hrs · 33,251 cycles

BNA - CREW REPORTED NEAR START OF DESCENT CABIN ALTITUDE CLIMBING. EMERGENCY DECLARED FLIGHT LANDED BNA WITHOUT INCIDENT. REPLACED NUMBER 2 PRESSURE CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,585 hrs · 32,907 cycles

ACCESSORY TAIL COMPARTMENT LIGHTS INOPERATIVE. RE-SEATED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT ACCESSORY TAIL COMPARTMENT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,585 hrs · 32,907 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 THRU 16 INOPERATIVE. RE-SEATED BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 62,585 hrs · 32,907 cycles

EMERGENCY EXIT LIGHT AT SEAT 32D INOPERATIVE. REPLACED BROKEN CONNECTOR AT SEAT 32D. OPS CHECK NORMAL.

Part: ACTUATOR — FAULTY (NLG) · airframe 61,039 hrs · 32,176 cycles

LAS - CREW REPORTED BUFFETING AND VIBRATION COMING FROM NOSE GEAR AREA. EMERGENCY DECLARED RETURNED LAS LANDED WITHOUT INCIDENT. UPON ARRIVAL AT GATE MAINTENANCE FOUND RIGHT FORWARD NOSE GEAR DOOR DOWN AND OPEN. REPLACED RIGHT NOSE GEAR DOOR LINKAGE ACTUATOR AND PERFORMED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 60,764 hrs · 32,054 cycles

VERTICAL SUPPORT CRACKED AT BOTTOM SIDE STATION 1322 AFT RIGHT CORNER. INSTALLED REPAIR DOUBLER AND RE-INSTALLED SUPPORT STRUT PER SRM 51-30-5 AND EA MD80-53-011122.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,764 hrs · 32,054 cycles

AFT ACCS SHEAR TIE CRACKED AFT SIDE OF 1437 BETWEEN LONGERONS 16 AND 17 RIGHT. INSTALLED NEW SHEAR TIE PER SRM 51-30-05.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,531 hrs · 31,937 cycles

EMERGENCY LIGHT BY SEAT 15D INOPERATIVE. SECURED EMERGENCY ESCAPE PATH CONNECTOR ON OUTBOARD SIDE OF SEAT 15D. OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 60,531 hrs · 31,937 cycles

EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. RECONNECTED EMERGENCY PATH LIGHT CONNECTOR AT SEAT 23D. OPS CHECKED NORMAL.

Part: O-RING — FAILED (AIR VALVE) · airframe 56,674 hrs

ORD INFLIGHT - CREW REPORTED AFTER GEAR RETRACTION RED LIGHT REMAINED ON FOR NOSE LANDING GEAR. ALSO REPORTED ADDITIONAL NOISE. IN COCKPIT, CYCLED GEAR BUT UNABLE TO EXTINGUISH RED LIGHT. EXTENDED GEAR WITH THREE GREEN LIGHTS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED O-RING ON AIR VALVE AND ACCOMPLISHED COMPLETE NOSE STRUT SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BEAM — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CARGO DOOR TOP BEAM HAS A CRACK. REMOVED AND REPLACED BEAM ASSEMBLY.

Part: WEB — CRACKED (ZONE 200) · airframe 56,388 hrs · 30,136 cycles

WEB CRACKED IN CANT FRAME LEFT SIDE, (AFT ACCESSORY) STATION 1463. INSTALLED REPLACEMENT WEB SECTION IN CANT FRAME PER SRM 51-02-00.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, CRACK IN INTERCOSTAL BETWEEN STATIONS 1287 AND 1309. REMOVED AND REPLACED INTERCOSTAL WITH SERVICEABLE PER SRM 53-14-3.

Part: BRACKET — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO TIE DOWN TRACK ATTACHED BRACKET BROKEN STATION 1287 LEFT SIDE AT LONGERON 28L. INSTALLED A SERVICEABLE BRACKET PER SRM 51-10-1.

Part: FRAME — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, CORROSION ON STATION 1309 FRAME. INSTALLED FRAME SPLICE PER SRM 53-03-00

Part: WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON LOWER WEB STATION 363-434 (FORWARD CARGO). REPLACED LOWER WEB WITH SERVICEABLE PER SRM 51-02-00.

Part: PAN — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

FORWARD CARGO DOOR PAN CORRODED. REMOVED AND REPLACED CARGO DOOR PAN WITH SERVICEABLE PER SRM 51-10-3.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, CORROSION ON SHEAR TIE STATION 1287. REMOVED AND REPLACED SHEAR TIE.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

MID CARGO, CORROSION AT CLIP NUT ATTACH HOLES ON RIGHT TIE DOWN TRACK FROM STATION 693 TO 788. REMOVED AND REPLACED CARGO TIE DOWN TRACK WITH SERVICEABLE PER SRM 51-10-3.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, CORROSION ON LIP OF LEFT TIE DOWN TRACK. REMOVED AND REPLACED SECTION OF TRACK FROM STATION 1090 TO 1212.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, INTERCOSTAL CORRODED AT LONGERON 29L BETWEEN STATION 1212 AND 1231. REMOVED AND REPLACED INTERCOSTAL WITH SERVICEABLE PER SRM 51-10-3

Part: LONGERON — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO, CORROSION ON LONGERON UNDER FRAME FROM STATION 1277 TO 1297. REPLACED SECTION OF LONGERON FROM 1277 TO 1297.

Part: BEAM — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

MID CARGO DOOR BEAM AND DOUBLERS BETWEEN STATION 636 AND STATION 693 ARE CORRODED, OUT OF LIMITS. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: FRAME — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION IN FRAME 1287 BETWEEN LONGERON 25 LEFT AND LONGERON 29 RIGHT. INSTALLED JAY ANGLE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON ANGLE ABOVE BOTTOM FORWARD CORNER OF AFT CARGO DOOR CUT-OUT, STATION 1155 BETWEEN LONGERON 28 RIGHT AND LONGERON 27 RIGHT. CORROSION ADDRESS CORRECTED BY REPLACING WITH SERVICEABLE COMPONENT PER SRM 51-10-1.

Part: LONGERON — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON LONGERON 30 BETWEEN STATIONS 446 AND 484 (FORWARD CARGO). REPAIRED PER SRM 53-02-00.

Part: SKIN — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION INTERIOR SIDE OF FUSELAGE SKIN FORWARD OF STATION 731 BETWEEN LONGERON 30 AND LONGERON 29 RIGHT. SPLICED IN SECTION OF SKIN PER SRM 53-04-00 12C SHEET 3.

Part: ANGLE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON ANGLE IN AFT CARGO AT STATION 1155 LONGERON 28 RIGHT. REPLACED CORRODED ANGLE WITH SERVICEABLE ONE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

SHEAR TIE CORRODED AT STATION 674 FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. INSTALLED NEW SHEAR TIE AND SPLICE AT STATION 674, FROM LONGERON 29 LEFT AND LONGERON 29 RIGHT PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: SKIN — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

NOSE LANDING GEAR LEFT AFT STRUT DOOR AFT HINGE CUT-OUT CRACKED. INSTALLED DOUBLER PER SRM 53-05-00 SHEETS 1 AND 2.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED UNDER CO-PILOTS BRIEF CASE HOLD AT STATION 120 LONGERON 19 RIGHT. REMOVED AND REPLACED ANGLE.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

AFT CARGO FLOOR SUPPORT CRACKED AT LONGERON 28 LEFT AT STATION 1174. REMOVED DAMAGED SUPPORT AND REPLACED WITH NEW SUPPORT PER SRM 51-30-5.

Part: FRAME — DAMAGED (ZONE 200) · airframe 56,388 hrs · 30,136 cycles

AFT SIDE OF FRAME HAS DEEP WEAR MARK FROM CONTACT WITH G1 GALLEY STATION 148 LONGERON 4 RIGHT. INSTALLED DOUBLER PER ESO 80559 DATED 11-18-08.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION IN AFT CARGO ON INTERCOSTAL ABOVE LONGERON 27 LEFT BETWEEN FRAME STATION 1271 TO STATION 1250. INSTALLED DOUBLER PER 51-10-3.

Part: FRAME — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION IN FRAME STATION 1231 LONGERON 29 RIGHT TO LONGERON 24 LEFT IN AFT CARGO. REMOVED AND REPLACED WITH NEW SECTION OF FRAME AND SPLICE STATION 1231 LONGERON 28 RIGHT TO LONGERON 29 LEFT.

Part: BRACKET — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION IN LOWER BRACKET AT INBOARD AFT CORNER OF AFT CARGO DOOR JAMB OPENING STATION 1212. INSTALLED SERVICEABLE BRACKET PER SRM 51-30-2.

Part: ANGLE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

TEE ANGLE FROM BELOW LEFT CUSP STATION 1140 HAS CORROSION. INSTALLED NEW TEE ANGLE PER SRM 51-01.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

SUPPORT ANGLE CRACKED IN FORWARD CARGO AT STATION 237. REMOVED AND REPLACED SUPPORT ANGLE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON FLOORBOARD SUPPORT DIRECTLY FORWARD OF NR 6 SEAT TRACK. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-01.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED AT STATION 237 BETWEEN LONGERON 28 RIGHT AND LONGERON 27 RIGHT. INSTALLED INTERCOSTAL SUPPORT ANGLE AT STATION 237 BETWEEN LONGERON 28 RIGHT AND LONGERON 27 RIGHT PER SRM 51-30-5.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

INTERCOSTAL SUPPORT ANGLE IN FORWARD CARGO CRACKED AT STATION 237 BETWEEN LONGERON 27 RIGHT AND LONGERON 28 RIGHT. REPLACED SUPPORT ANGLE PER SRM 51-01.

Part: MOUNT — CORRODED (LIGHT) · airframe 56,388 hrs · 30,136 cycles

HOLE FROM CORROSION IN MOUNTING FLANGE FOR UPPER ANTI-COLLISION LIGHT. DOUBLER INSTALLED PER 53-04 PAGE 145.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON LOWER SIDE OF CUSP, STATION 1136 TO STATION 1155. REMOVED CORROSION BY REMOVING DAMAGED DOUBLER AND REPLACING WITH NEW DOUBLER PER AARD 53-20-00-16 AND ESO 80559 DATED 11/11/2008.

Part: FRAME — CRACKED (ZONE 300) · airframe 56,388 hrs · 30,136 cycles

LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER LEFT STATION ZFS 36.500. INSTALLED REPAIR DOUBLER PER AARD 55-30-00-2.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

RIGHT CUSP CORRODED STATION 564 TO STATION 575. INSTALLED CUSP REPAIR PER AARD 53-20-00-16, STATION 564 TO STATION 575.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON NR 6 SEAT TRACK OUT OF LIMITS STATION 1031 TO STATION 1307. REPLACED SEAT TRACK FROM SPLICE AT STATION 1031 TO STATION 1307 PER 51-01 SRM.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 56,388 hrs · 30,136 cycles

VERTICAL STABILIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 49.625. REPAIRED PER AARD 55-30-00-2.

Part: FLOORBOARD — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION ON INBOARD SIDE STATION 1174. INSTALLED 8 INCH BY 14 INCH DOUBLER PER AARD 53-20-00-23.

Part: FRAME — CRACKED (ZONE 300) · airframe 56,388 hrs · 30,136 cycles

VERTICAL STABLIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 30.00. REPAIRED PER AARD 55-30-00-2.

Part: ANGLE — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CORROSION OUT OF LIMITS ON ANGLE STATION 1338, LONGERON 28 LEFT TO LONGERON 29 LEFT. REPLACED ANGLE STATION 1338, LONGERON 28 LEFT TO LONGERON 29 LEFT PER 51-01 SRM.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON NUMBER 3 SEAT TRACK AT STATION 1174. REPAIRED PER AARD 53-20-00-10.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, FLOORBOARD SUPPORT CRACKED AT STATION 180 LEFT BODY LINE 32. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE SUPPORT.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON BOTTOM SIDE OF RIGHT CUSP AT STATION 1079 TO 1098. INSTALLED SERVICEABLE CUSP SHEET FROM STATION 1022 TO 1098 PER SRM 51-01.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON BOTTOM SIDE OF RIGHT CUSP AT STATION 1098 TO 1117. INSTALLED SERVICEABLE CUSP SHEET FROM 1098 TO 1074 PER SRM 51-01.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

FLOORBOARD SUPPORT CRACKED AT STATION 845. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-01.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

RIGHT CUSP MEMBRANE HAS CORROSION STATION 939 TO STATION 941. INSTALLED NEW CUSP SHEET RIGHT STATION 905 TO STATION 946 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, RIGHT SIDE CUSP IS CORRODED AT STATION 170. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON RIGHT CUSP AT STATION 1287 TO 1309. REMOVED DAMAGED CUSP SHEET AND INSTALLED A SERVICEABLE CUSP SHEET FROM STATION 1250 TO 1309.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, LEFT CUSP CORRODED AT STATION 390. REMOVED CORROSION AND INSTALLED REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON NUMBER 3 SEAT TRACK AT STATION 1200. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON LEFT CUSP AT STATION 602. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON RIGHT CUSP AT STATION 1011. REPAIRED PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,388 hrs · 30,136 cycles

CABIN, CORROSION ON SEAT TRACK STATION 1130. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: CASTING — CRACKED (ZONE 200) · airframe 56,388 hrs · 30,136 cycles

AFT ENTRY DOOR JAMB STATION 1338, RIGHT MID STOP CASTING CRACKED. INSTALLED SERVICEABLE CASTING PER SRM 51-01.

Part: RIB — CRACKED (ZONE 400) · airframe 56,388 hrs · 30,136 cycles

LEFT ENGINE PYLON, CRACK IN LOWER FORWARD END OF THE INBOARD RIB JUST ABOVE PANEL NUMBER 8111C. REPAIRED PER SRM 54-21-00 FIGURE 2 SHEET 1 AND 2, 54-01-00 FIGURE 2 SHEET 2 AND 51-60-00 FIGURE 1 SHEET 1.

Part: WIRE HARNESS — LOOSE (CABIN)

EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. SECURED WIRE HARNESS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (K)

Part: STRUT — INOPERATIVE (NLG)

ORD INFLIGHT T1426 - AFTER GEAR RETRACTION RED NOSE GEAR DOOR LIGHTS REMAINED ILLUMINATED. RECYCLED GEAR WITH NO HELP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING HEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SERVO — INOPERATIVE (YAW DAMPER)

DFW INFLIGHT T2265/23APR ORD TO PVR - AT FLIGHT LEVEL 320 BOTH AUTOPILOTS AND YAW DAMPER INOPERATIVE. LANDED DFW WITHOUT INCIDENT. REPLACED ELEVATOR SERVO. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,193 hrs · 23,287 cycles

THE AFT EGRESS TRACK LIGHTING WOULD NOT ILLUMINATE. REPLACED THE BATERY PACK AND SECURED CONNECTOR ON THE TRACK LIGHTING.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,413 hrs · 22,810 cycles

THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE FROM ROW 18 TO 26, THE EGRESS FLOOR LIGHTS WERE INOPERATIVE IN FIRST CLASS, AND THE LEFT SIDE NUMBER 1 AND RH SIDE NUMBER 1 CABIN DOOR EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERIES PN 408822-101 FOR THE CEILING EMERGENCY LIGHTS AND FOR THE EGRESS LIGHTS. REPLACED THE POWER SUPPLY PN 60-0304-51LB FOR THE EXIT SIGNS. CHECK-C 1-21-02 STL.

Part: BATTERY · airframe 8,373 hrs · 4,739 cycles

THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE FROM ROW 12 THRU 17. REPLACED THE BATTERIES IN THE B5-102 BATTERY PACK. CHECK-C 12-17-2002 STL. --CLOSED--

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C FOUND CORROSION ON HORIZONTAL ANGLE ATTACHED TO TRAPEZOIDAL PANEL RBL 58, 7 INCHES AFT OF CENTER SECTION UPPER SPAR CAP; JUST AFT OF LT MLG SIDE STRUT UPPER MOUNT, 9 INCHES BELOW PRESSURE DECK. REMOVED AND REPLACED ANGLE PER SRM 6-7-01 PG 3, AND BOEING DRAWING 5930516.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT FRAME AT STA 1322, FOUND HEAVY CORROSION AT LONGERON 30 ON AFT SIDE. SPLICED IN NEW SECTION OF FRAME PER SRM 53-03 FIGURE 2A. INSTALLED RIVETS IN BULKHEAD SUPPORT FRAME PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT, RT SIDE AT STATION 1212 TO 1308, FOUND RT TIE DOWN TRACK CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF TRACK FROM STATION 1202 TO 1322, PER SPM 6-70-01 PAGES 1-3.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT LT SIDE, TIE DOWN TRACK FROM STATION 1220 TO 1308 IS CORRODED BEYOND LIMITS. NEW SECTION OF TRACK WAS INSTALLED PER SRM 51-30-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT AT STATION 1079 TO 1155 RT SIDE, TIE DOWN TRACK WAS FOUND CORRODED BEYOND LIMITS. NEW SECTION OF TRACK WAS INSTALLED FROM STATION 1079 TO 1155 PER SRM 53-05 PG 10.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT RT SIDE, TIE DOWN TRACK FROM STATION 1212 TO 1322 WAS FOUND CORRODED BEYOND LIMITS. NEW SECTION OF TRACK WAS INSTALLED FROM STATION 1212 TO 1322 PER SRM 51-30-02/05.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

IN THE ELECTRONIC COMPARTMENT FOUND CORROSION ON LONGERON 30 FROM STA 110 TO 130. REMOVED LONGERON 30 FROM STA 110 TO 130. INSTALLED REPAIR PER SRM 53-02, FIG 18, SHEET 1 PAGE 48.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE FWD CARGO COMPARTMENT FOUND CORROSION ON THE RT CARGO TIE DOWN TRACK, SEVERAL PLACES FROM STA 427 TO 522. REPLACED DAMAGED AREA OF TIE DOWN TRACK PER SRM 53-05, FIG 4G, PAGE 10R.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT FOUND CORROSION AT PANEL ATTACH HOLES IN LT TIE DOWN TRACK, STA 644 TO 787 AND IN TIE DOWN TRACK ABOVE LONGERON 27L. FOUND TRACK CORRODED BEYOND LIMITS. FABRICATED NEW TRACK AND INSTALLED REPAIR PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT FOUR UPPER TIE CLIPS WERE CRACKED ON LOWER VENT AFT OF CANTED FORMER RING, STA 1463, LBL 19 INCHES TO LBL 32. FABRICATED 4 EACH TIE CLIPS PER SPM 6-70-01, PAGE 2 AND 3, AND DOUGLAS DRAWING 5920838. INSTALLED 4 EACH TIE CLIPS PER SPM 6-70-01, PAGE 3 AND DOUGLAS DRAWING 5920838, AND SRM 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION IN RT OUTBOARD CHAIR TRACK AT STA 217. REPLACED TRACK SECTION PER SRM 53-05-4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN CABIN AT STA 1136 TO 1212, THE NUMBER 2 CHAIR TRACK HAD CORROSION AROUND FLOOR PANEL ATTACH HOLES. REPAIRED SEAT TRACK PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT A CABIN FLOOR MEMBRANE PANEL HAD LIGHT CORROSION ON THREE AREAS, STA 160 TO 200, LBL 5 INCHES. REPLACED FLOOR MEMBRANE FROM STA 200 TO 160, LBL 9 INCHES TO RBL 32. INSTALLED PER SRM 51-30-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FORMER AT STA 1308 HAD CORROSION AT LONGERON 30, ON THE AFT SIDE. REMOVED CORRODED SECTION OF FRAME AND INSTALLED NEW PIECE WITH SPLICES PER SRM 53-03 FIG 2A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION ON FLOOR SUPPORT BEAM AT RBL 9 TO RBL 46, AT STATION 200. REPLACED FLOOR SUPPORT PER SRM 51-30-02.

Part: SKIN — CORRODED (RT WING) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT ON THE RT WING LOWER SURFACE, CORROSION WAS FOUND AROUND THE FASTENER AT WING STATION 511, TR LOWER MID SPAR SKIN. ACCOMPLISHED UT INSPECTION PER NDT 51-00-03 AND FOUND 47 PERCENT MATERIAL LOSS. INSTALLED FILLER AND DOUBLER PER SRM 57-03, FIG 24A, SHEETS 1 THROUGH 6.

Part: WEB — BROKEN (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN TAIL COMPT RT SIDE BETWEEN STA 1474 AND 1486 STRUCTURAL WEB WAS BROKEN OUTBOARD OF STAIR HYD ACTUATOR. INSTALLED NEW STANDARD STRUCTURAL WEB PER SPM 6-70-01 AND DOUGLAS DRAWING 9911946.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK BETWEEN STA 1136 THROUGH 1155 AT LONGERON 28R. REMOVED SURFACE CORROSION PER SPM 6-80-01. REMOVED AND REPLACED 2 ANGLES PER SRM 6-70-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT ON FUSELAGE EXTERIOR, STA 1293, FOUND DENT BETWEEN LONGERON 16L AND 15L. ACCOMP INSP PER NDT 51-00-03 AND NO CRACK. UT INSPECTION INDICATED 50 PERCENT MATERIAL LOSS. CUT OUT PLUG TO REMOVE DAMAGED AREA AND INSTALLED AN EXTERIOR AND INTERNAL DOUBLER SHIM AS REQUIRED PER SRM 53-04, FIG 38, PAGE 218.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT AT LONGERON 25L, THE STIFFENER HAD DOUBLER WITH CORROSION AT STA 1271, STA 1283, 1250, 1240 AND 1231. THE DOUBLERS WERE ON TOP OF THE STIFFENERS AND FORMERS. REMOVED CORROSION PER SRM 51-10-3. MADE NEW DOUBLER AS NEEDED PER SPM 6-70-01. INSTALLED PER SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT ON THE FUSELAGE EXTERIOR, STA 1293, FOUND BULGE IN SKIN AT LONGERON 16L. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM BETWEEN SKIN AND STRINGER TO REMOVE BULGING IN, PER SRM 51-09.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,926 hrs · 21,312 cycles

DURING CHECK-C MAINT THE FUSELAGE EXTERIOR HAD A BULGE IN THE SKIN AT LONGERON 17L, STA 1293. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM BETWEEN SKIN AND STRINGER TO REMOVE BULGING IN, PER SRM 51-10-9. INSTALLED HI-LOKS PER SRM 51-60-0, PAGE 36.

Part: DUCT (LH PACK) · airframe 37,762 hrs · 21,223 cycles

AFTER TAKEOFF SMOKE APPEARED IN THE COCKPIT. CREW SHUT OFF THE LH PACK AND RETURNED TO STL. FOUND Y DUCT WITH HOLE WORN IN IT. WELDED THE DUCT. CHECK-C 3-1-01 JFK. --CLOSED--