N962DL

Part: SKIN — CORRODED (BS 480) · airframe 74,891 hrs · 55,611 cycles

MD-88 FUSELAGE STA 480 & L-30 CORROSION - REQUIRED PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION LEVEL OF ER/A 563889-14 IS REV. A. RESULTS OF DTA/DTE HAVE BEEN INCORPORATED AT THIS REVISION LEVEL. ACCOMPLISH SECTION II: PERMANENT REPAIR AT OR PRIOR TO THE ACCRUEMENT OF 57,743 TOTAL AIRCRAFT FLIGHT CYCLES. ASSOCIATED ER/A 00-563889 ADDED FOR AC 0962. (LP0834471)

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 74,691 hrs · 55,441 cycles

EMERGENCY LIGHT AT 20 ED NOT ILLUMINATING. RESEATED CONNECTOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,691 hrs · 55,441 cycles

EMERGENCY LIGHT IN AFT VENTRAL STARS OVERHEAD PANEL NOT ILLUMINATING. REPLACED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY B5-28 IAW AMM 33-53.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,636 hrs · 55,400 cycles

ROW 16-20 ABC OVERHEAD E-LIGHTS INOP. R+R BATTERIES IN B5-102. OPS CK SAT. PER AMM 33-50. (LP4414850)

Part: SLIDE — NO TEST (TAILCONE) · airframe 74,268 hrs · 55,075 cycles

JETTISON TAIL CONE AND DEPLOY AFT SLIDE ROUTINE CARD 2562-7267 FAILED THE DEPLOYMENT TEST. CABLE IMPROPERLY ROUTED. ROUTED CABLE THE CORRECT WAY INSTALLED NEW SLIDE IAW AMDS ROUTINE CARD 2561-4001 AND LOG # 0697306 SCHEDULED PARTS CHANGE CARD JOB # 001-0001.(LP0697769)

Part: SMOKE DETECTOR — MALFUNCTIONED (AFT LAVATORY) · airframe 74,227 hrs · 55,041 cycles

RT AFT LAVATORY SMOKE DETECTOR WAS BEEPING. REPLACED THE SMOKE DETECTOR IAW AMM 26-13. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 73,331 hrs · 54,299 cycles

AFT LEFT SIDE LAVATORY SMOKE DETECTOR ACTIVATED DURING CRUISE. A/C PACKS AT 12 & 1 O'CLOCK IN AUTO MODE. COOLED PACKS AND SMOKE DETECTOR STOPPED. FOUND SMOKE DETECTOR DIRTY AND WET. CLEANED AND DRIED THE AREA. ALL FUNCTIONAL CHECKED GOOD.

Part: SLIDE — ABNORMAL (TAILCONE) · airframe 72,925 hrs · 53,972 cycles

LATE FINDING: UNFOLDING TAIL CONE SLIDE AT AFT ACCESORIES COMPARMENT. TAIL CONE SLIDE S/N:1586RP WAS REMOVED PER MD88 AMM 25-62-01 AND SERVICIABLE TAIL CONE SLIDE S/N:1082 WAS INSTALLED PER MD88 AMM 25-62-01.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

SEVERAL CORROSION POINTS AROUND FWD CARGO COMPARTMENT DOOR JAMB. CORROSION LEVEL 2 FWD CARGO COMPARTMENT DOOR JAMB WAS REPAIRED (PERMANENT REPAIR) PER ER/A 565444-14 REV ORIGINAL AND ETI-88-18-007 REV 1 REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL AIRFRAME FLIGHT CYCLES ONLY UNDER LOG PAGE 0404660 PER ER/A 565444-14 REV ORIGINAL.

Part: ANGLE — CRACKED (RT COWLING) · airframe 72,925 hrs · 53,972 cycles

CRACK IN ELBOW DUCT ANGLE AT RT NOSE COWLING YN= 19.430 AND 12 O'CLOCK POSITION, ALSO MISALIGNED MIXING TUBE AT RT NOSE COWLING 12 O'CLOCK POSITION. ELBOW DUCT ANGLE (P/N: 5938038-41) AT RT NOSE COWLING YN= 19.430 WAS REPLACED PER SRM 51-30-2, 51-30-5 AND DWG 5938038 REV "AL" AND MIXING TUBE AT RT NOSE COWLING 12 O'CLOCK POSITION WAS INSTALLED PER AMM 75-10-05.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 72,925 hrs · 53,972 cycles

CRACKS ( 2 EA ) ON DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER. DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER WAS REPAIRED (AS PERMANENT) PER ER/A 516509-14MA (SECTION I) REV 4 AND SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,925 hrs · 53,972 cycles

CRACKED FRAME ON STA Y=1510 CANT 5HRS POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME ON STA Y=1510 CANT 5 HRS. POSITION AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER DWG 9911843 REV "AC" AND SRM 51-30-2 AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

OUT OF LIMITS: CORROSION ON FRAME CLIP STA Y=1231 BTW LONG 29R TO 30 AT AFT CARGO COMPARTMENT. FRAME CLIP (EXTRUSION P/N: S2506195-12000) STA Y=1231 BTW LONG 29R TO 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 53-14-3 FIG 3, 51-30-5 AND SRM 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 72,925 hrs · 53,972 cycles

CRACK IN LONGERON 4L STA 200 AT PAX CABIN. DAMAGE LONGERON 4L STA 200 AT PAX CABIN WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-02 FIG 18.

Part: FRAME — CRACKED (FUSELAGE) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

OUT OF LIMITS: EXCESSIVE CORROSION ON FRAME STA=1287 BTW LONG 28R AND 28L AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER SRM 53-03D FIG 2A.

Part: SKIN — CORRODED (APU DOOR) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORROSION LEVEL 2.

Part: SKIN — CORRODED (APU DOOR) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORROSION LEVEL 2.

Part: SKIN — CORRODED (APU DOOR) · corrosion level 2 · airframe 72,925 hrs · 53,972 cycles

CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORROSION LEVEL 2.

Part: LANYARD — DAMAGED (EVAC SLIDE) · airframe 72,925 hrs · 53,972 cycles

INITIAL INSPECTION: DAMAGE LANYARD OF FWD PASSENGER ENTRANCE DOOR L1 SLIDE. L1 RELEASE LANYARD CABLE WAS REPLACED AND VERIFIED PER IPC 25-60-00-34.

Part: NOT REPORTED — CORRODED (BS 480) · airframe 72,624 hrs · 53,746 cycles

C/W PRI 563889-14 REV ORIGINAL. CORROSION FUSELAGE STATION 480 AND LONGERON L-30. C/W PRI 563889-14 REV 1. C/W 563889-14 REV 0. (LP0323707)

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,624 hrs · 53,746 cycles

ON WALKAROUND FOUND CORROSION WITH CRACK ON OUTER SKIN ON LOWER UHF ANTENNA. CUT OUT DAMAGE OND REMOVED INTERNAL PARTS FOR ACCESS. C/W ER/A 563889-14 REV 0 ON NRC4 SCEPTOR LOG 0323707. (LP3884696)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,548 hrs · 53,681 cycles

COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,370 hrs · 53,533 cycles

OVERHEAD TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERIES, OPS CHECKED LIGHTS AND BATTERY CHARGER IAW AMM 33-50.

Part: TIRE — FAILED (NR 1) · airframe 71,744 hrs · 53,025 cycles

NR 1 MAIN TIRE, LEFT TIRE MAIN CORD SHREDDED. TIRE DAMAGED AFTER USING MAX AUTO BRAKE AND THEN ACFT CAME TO ABRUPT STOP. SMOKE FROM TIRE WAS NOTED BY TOWER. REPLACED THE NR 1 MAIN WHEEL ASSY IAW AMM 32-40. INSPECTED UNDERSIDE OF LT WING NO DAMAGE NOTED. BITE TEST OF ANTISKID SYSTEM IAW AMM 32-43, CHECKED OK, NO FAULTS ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 29) · airframe 71,637 hrs · 52,945 cycles

SEAT 29 MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-53. OPS CHECKED OK.

Part: ANGLE — CRACKED (BS 1463) · airframe 70,751 hrs · 52,260 cycles

LEFT LOUVER PANEL FOUND A CRACKED ANGLE, BS 1463. REPLACED THE ANGLE IAW DWG 9911839.

Part: SUPPORT — CRACKED (BS 1463) · airframe 70,751 hrs · 52,260 cycles

BS 1463 FOUND BRIDGE SUPPORT ROD BRACKET CRACKED. REMOVED BRIDGE SUPPORT. FABRICATED AND REPLACED IAW DWG 5930556.

Part: CONNECTOR — DAMAGED (OIL TEMP) · airframe 69,902 hrs · 51,725 cycles

RIGHT ENGINE OIL TEMPERATURE ERRATIC AND HIGH. FOLLOWED QRH PROCEDURES AND SHUT ENGINE DOWN. POSITIVE OIL PRESSURE WAS MAINTAINED DURING WINDMILLING TIME. MAINTENANCE FOUND CONNECTOR P1-812 WITH A PUSHED BACK PIN. REPLACED AND RE PINNED THE CONNECTOR. ALSO REPLACED TEMP BULB AND RE-TERMINATED THE GROUND TERMINAL 906. RAN BOTH ENGINES OIL TEMP NORMAL A/C RTS.

Part: COFFEEMAKER — MALFUNCTIONED (LAVATORY) · airframe 69,042 hrs · 51,087 cycles

COFFEEMAKER, F303, NR 1 TURNED ON. IN FLT, SMELLED ELECTRICAL BURNING. SECURED, ODOR DISSIPATED IMMEDIATELY. DEFERRED IAW NEF 253602. COFFEEMAKER REPLACED ON 08JUL16.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 67,938 hrs · 50,277 cycles

LOWER CARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AND EDGE SEAL DETERIORATED. REPAIRED IAW PRI 543287-14 ALL REVISIONS AND COMPLIED WITH ERA 543287-14, REV ORIGINAL.

Part: HEATER — FAILED (CARGO BAY) · airframe 67,713 hrs · 50,127 cycles

ACFT HAD SLIGHT ODOR, HAZE IN CABIN AND COCKPIT. FLIGHT CREW NOTED 1 PHASE OF CARGO HEAT C/B POPPED. PULLED REMAINING C/BS AND ALL DISSIPATED. MAINTENANCE FOUND THE FORWARD CARGO HEAT INTERNAL ELEMENT FAILED AND REPLACED THE FORWARD CARGO HEATER. MAINTENANCE ALSO COMPLIED WITH THE PNEUMATIC TROUBLESHOOTING TASK CARD WITH NO OTHER DEFECTS NOTED. THE ACFT HAS RETURNED TO SERVICE.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 67,525 hrs · 49,974 cycles

ER/A 519139-14, REV A,VERTICAL STABILIZER REAR SPAR CAP, CRACK REPAIRED IAW ER/A 519139-14, REV A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,095 hrs · 49,633 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FOUND EMERGENCY LIGHTS IN CEILING FORWARD OF AFT CABIN DOOR INOPERATIVE. BATTERIES AT B5-27 AND B5-28 WERE REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,747 hrs · 48,702 cycles

MAINTENANCE FOUND 3 CEILING EMERGENCY LIGHTS INOPERATIVE IN THE FWD CABIN AREA. MSP MAINTENANCE R & R THE EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-00. OPS CHECKED NORMAL. LP6972433.

Part: WIRE — DAMAGED · airframe 65,671 hrs · 48,655 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE FLOOR MOUNTED EMERGENCY PATHWAY LIGHTING FOR ROWS 1-12 AND THE OVERHEAD LIGHTS AT DOORS L1 & R1 WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT ROW 11E WAS SHORTING TO GROUND. WIRE WAS REPAIRED WITH A SPLICE AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,902 hrs · 51,725 cycles

CORROSION ON RT CUSP WEB X=-54 TO X=-60 BETWEEN STA Y=793 TO STA Y=800, FLOOR CABIN STRUCTURE. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, TRIMMED, DRILLED, TREATED, PAINTED, AND INSTALLED.

Part: CAM — MISINSTALLED (TAILCONE) · airframe 62,840 hrs · 46,648 cycles

DURING ZONE FINAL CHECK, NOTED MISINSTALLED RELEASE MECHANISM CAM OF TAILCONE. INSTALLED RELEASE MECHANISM CAM CORRECTLY IAW AMM 53-53-02-201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,840 hrs · 46,648 cycles

DURING CHECK, CORROSION FOUND ON RT WING HEATER BLANKET AROUND FUEL ACCESS PANEL. REPLACED ACCESS PANEL IAW AMM 30-80-02.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,840 hrs · 46,648 cycles

DURING CHECK, CORROSION FOUND ON LT WING HEATER BLANKET AROUND FUEL ACCESS PANEL. REPAIRED IAW ER/A 519147-14.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 62,840 hrs · 46,648 cycles

DURING CHECK, A CRACK FOUND ON RT HORIZONTAL STABILIZER REAR SPAR CAP APPROXIMATELY STA XE 14.525. SPAR CAP REPLACED IAW DWG SR09550030, REV "C" CONFIG. 7006.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION FOUND ON FRAME BS 1380 L25LT & RT AT AFT ACCESSORY COMPARTMENT. LOWER FRAME TEE AT BS 1380 WAS REPLACED IAW ER/A 521172-14 REV ORIGINAL AND DWG 9912246, REV DE & SRM 51-30-2 AND 51-30-5 AND ER/A N.- 521175-14, REV ORIG ORIGINAL.

Part: WEB — DAMAGED (HORIZONTAL STAB) · airframe 62,840 hrs · 46,647 cycles

ELONGATED HOLES ON WEB, ANGLES AND FITTING BETWEEN XH=27 AND XHS=97 ALSO ON PRODUCTION DOUBLER BETWEEN XH=27 AND XHS=41 AT RT HORIZONTAL STABILIZER REAR SPAR. DAMAGED WEB , ANGLES AND FITTING AND DOUBLER REMOVED IAW SRM 51-30-1, 51-30-2 AND 51-30-5, FABRICATED IAW DWG 9918401, REV "DC" AND TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. NEW WEB, DOUBLER , ANGLES AND FITTING WERE INSTALLED IAW DWG 9918401, REV "DC" AND SRM 51-30-1, 51-30-2, AND 51-30-5 G.

Part: SKIN — CRACKED (BS 1437) · airframe 62,840 hrs · 46,647 cycles

CRACKS ON FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3&4R. DAMAGE REMOVED, REPAIR FABRICATED, TREATED, PAINTED AND REPAIR INSTALLED IAW SRM 51-30-2, 53-04 FIG. 27, 51-10-3.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,840 hrs · 46,647 cycles

LIGHTING STRIKE AT LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 522 - 541. BLENDED IAW SRM 53-05, FIG III,

Part: PLATE — DAMAGED (RUDDER) · airframe 62,840 hrs · 46,647 cycles

EXPOSED COMPOSITE MATERIAL ON RUDDER PLATE. RUDDER REPAIRED IAW SRM 51-70-1AD, PAR.7.

Part: INTERCOSTAL — CORRODED (BS 1183-1193) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION OUT OF LIMITS ON INTERCOSTAL BELOW DOOR FRAME WEB, BS 1183 AND 1193 AT AFT CARGO BAY. INTERCOSTALS REMOVED IAW SRM 51-30-2-51-30-5. NEW INTERCOSTALS INSTALLED IAW SRM 51-30-2 - 51-30-5.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 62,840 hrs · 46,647 cycles

DAMAGE FLAME SPRAY ON RUDDER. FLAME SPRAY ON RUDDER WAS REPAIRED IAW CARD 2000-8149-07.

Part: SEAT TRACK — CORRODED (BS 1258-1261) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION FOUND ON RT SEAT TRACK, REPAIR PLUG LBL 22 BETWEEN BS 1258-1261. REPAIRED IAW SRM 51-30-1, 53-05, FIG 4A , 51-10-3 PAR 14,21,38.

Part: LONGERON SPLICE — DAMAGED (BS 1401-1418) · airframe 62,840 hrs · 46,647 cycles

LONGERON SPLICE 8R BETWEEN BS 1401 - 1418 DAMAGED. INSTALLED NEW LONGERON SPLICE IAW SRM 53-02 FIG 18, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5, 51-20-0.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION FOUND ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1409C ON RT WING. REPLACED ACCESS PANEL.

Part: SEAT TRACK — CORRODED (BS 1084-1087) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING CHECK, CORROSION FOUND ON LT SEAT TRACK RBL 54, BS 1084 - 1087. REPAIRED IAW SRM 53-05-10-3, PAR 14, 21, 38 ERA 485415-14MA, REV ORIG. AND SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 610-614) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION ON RT CUSP WEB BS 610-614, LBL 54 - 60. REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 1141) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB LBL 54-60 BS 1141-1144. REPAIRED IAW SRM 51-10-3, PAR 14, 21, 38, 53-05, FIG 131A-5 AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 446-449) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION ON RT SEAT TRACK LBL 54. BS 446-449. INSTALLED NEW REPAIR IAW SRM 51-30-1.

Part: LONGERON SPLICE — DAMAGED (BS 1401-1418) · airframe 62,840 hrs · 46,647 cycles

NOTED WEAR ON LONGERON 8R REPAIR SPLICE BS 1401 - 1418 AT AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 , 51-10-4 , 53-02 FIG. 18, 51-20-0 AND PS 900-5-1, NR 04.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

CORROSION ON FRAME BS 1309 L27L-27R AT AFT CARGO BAY. REPAIRED IAW SRM 53-03 "D" FIG 2-A.

Part: INTERCOSTAL — CRACKED (BS 1271-1287) · airframe 62,840 hrs · 46,647 cycles

CRACK ON INTERCOSTAL BS 1271-1287, LBL 22 - RBL 22. INTERCOSTAL REPAIRED IAW ERA 380524-14MA.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING SCHEDULED CHECK, NOTED CORROSION ON CARGO DOOR FRAME FITTING BS 1155. REPLACED CARGO DOOR FRAME FITTING AND INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1358) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING CHECK, NOTED CORROSION ON LT FLOORBEAM, BS 1338 BETWEEN RBL 54 AT FLOOR CABIN STRUCTURE. FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIG. 20A AND 51-30-2 AND 51-30-5 AND TREATED WITH 51-10-3, PAR 21 AND 14.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING SCHHEDULED CHECK, NOTED CORROSION ON RT FLOORBEAM AT BS 200 BETWEEN LBL 10 - 44. REPAIRED IAW SRM 53-14-1.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING SCHEDULED CHECK, CORROSION FOUND ON COUNTERSUNK AND SEATTLEMENT AREA OF FUEL ACCESS PLATE NR 1303C AT LT WING. NO BLEND OUT ALLOWED. REPLACED PLATE IAW SRM 51-22-2A, PAR 6B.

Part: BEAM — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING SCHEDULED CHECK, CORROSION ON AFT CARGO BAY DOOR FRAME LOWER BEAM, BS 1155 - 1212.

Part: CUSP WEB — CRACKED (BS 1293) · corrosion level 2 · airframe 62,840 hrs · 46,647 cycles

DURING CHECK, A CRACK FOUND ON CUSP WEB BS 1293 X=-54 AND X=-60. REPAIRED IAW SRM 53-05 FIG 131A.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 62,546 hrs · 46,429 cycles

MX DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE INFLATION BOTTLE AT L2 DOOR DEPLETED. T THE DOOR SLIDE INFLATION BOTTLE WAS REPLACED.

Part: SPRING — INOPERATIVE (TAILCONE LATCH) · airframe 60,671 hrs · 45,078 cycles

BOTH THE UPPER RT AND THE UPPER LT TAILCONE RELEASE LATCH SPRINGS ARE NOT FUNCTIONING, ARE WEAK, AND HAVE GOUGED INTO THE TAILCONE FLANGE. BOTH UPPER RT AND LT LATCH ASSEMBLIES WERE REPLACED IAW AMM 53-53-00. THE TAILCONE FUNCTIONAL CHECK WILL BE ACCOMPLISHED ON AMDS 5350-01077-0101.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 59,764 hrs · 44,420 cycles

IN FLIGHT LT OIL QTY WENT TO ZERO. SHUTDOWN ENGINE PER QRH. NO DAMAGE NOTED AFTER LANDING. LT OIL QTY AND PRESSURE WENT TO 0, LOW OIL PRESSURE ON EOAP PLUS AMBER AND RED OIL PRESS CAUTION AND WARNING LIGHTS ILLUMINATED ON EDP WITH ZERO PRESSURE TWO MINUTES ELAPSED FROM INITIAL INDICATIONS TO SHUTDOWN, TEN MINUTES ELAPSED ON WINDMILL. ENGINE DID OPERATE ABOVE IDLE POWER WITH OIL PRESSURE BELOW 34 PSI BEFORE THROTTLE WAS IDLED AND ENGINE SHUTDOWN.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,378 hrs · 44,177 cycles

DURING SERVICE CHECK, FOUND EMERGENCY OVERHEAD LIGHTS ROW 12AND EMERGENCY ENTRY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND 8 LEDS AT SEAT 2AC. OPS CHECKED NORMAL.

Part: OIL CAP — MISINSTALLED (APU) · airframe 54,323 hrs · 40,732 cycles

DURING CLIMB PASSING THROUGH 8000 FT, THE CABIN CREW REPORTED A BURNING OIL SMELL FOLLOWED BY THE AFT LAVATORY SMOKE DETECTORS SOUNDING. SMELL DISSIPATED AND FLIGHT CONTINUED TO ATL. UPON ARRIVAL MAINTENANCE FOUND THE APU OIL CAP IMPROPERLY INSTALLED. REPLACED APU AND ACCOMPLISHED OPERATION 5089 - PACK BURNOUT (2010-D0829)(DLM88101854).

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 53,542 hrs · 40,157 cycles

SEAT 34ED, RED SEAT ROW EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. RE-TERMINATED PLUG MALE END. OPS CHECK OF LIGHTS NOW OK.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,518 hrs · 40,143 cycles

3C EMERGENCY LIGHT INOP, REPLACED LIGHT SOCKET ASSY AT 3C. CKS OK.

Part: SKIN — DENTED (RT ELEVATOR TAB) · airframe 48,476 hrs · 36,954 cycles

DURING HMV, DENTS WERE FOUND ON LOWER AND UPPER SKIN OF RT ELEVATOR GEARED TAB. TAB WAS REPAIRED IAW SRM 51-70-2D.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 48,476 hrs · 36,954 cycles

DURING HMV A DENT WAS FOUND ON LOWER SKIN OF OUTBD GUIDE VANE LT OUTBD FLAP. VANE WAS REPAIRED IAW SRM 51-70-2D.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 35,492 hrs · 28,040 cycles

RT ENG WITH NORMAL PWR T/O AT ROTATION HAD A COMPRESSOR STALL. THE ENG ROLLED BACK AND EGT 500 DEGS RISING. REPLACED ENGINE.

Part: SENSOR — FAILED (NLG) · airframe 32,104 hrs · 25,541 cycles

ON DEPARTURE THE NOSE GEAR DID NOT RETRACT. RED LIGHT WAS ON AND BOTH MAIN LIGHTS WERE EXTINGUISHED. REPLACED LOCK SENSOR.

Part: DUCT — CRACKED (A/C BAY) · airframe 31,674 hrs · 25,221 cycles

TAIL COMPARTMENT HIGH MESSAGE DURING CLIMB. FOUND CRACKED BLEED DUCT AT RIGHT ACM. REPLACED SAME. LEAK CHECKS GOOD.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 31,543 hrs · 25,121 cycles

SHORTLY AFTER TAKEOFF AC CROSSTIE LOCKOUT MESSAGE ILLUMINATED. APPROXIMATELY 5 MINUTES LATER, RIGHT GEN OFF, RT AC BUS OFF AND RT DC OFF. REPLACED GENERATOR.

Part: PISTON — FLAKING (NLG) · airframe 30,601 hrs · 24,398 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF DESPITE NUMEROUS ATTEMPTS. WHILE SERVICING NOSE STRUT FOUND CHROME FLAKING FROM STRUT CYL. REPLACED NOSE PISTON PER M/M, SWUNG GEAR AND OPS CKS OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 30,493 hrs · 24,310 cycles

ACFT LOST HYD PRESS AND QTY ON RT SYS, MADE EMERGENCY LANDING GEAR DOORS WERE UP AND RT SYS HYD QTY DID NOT GO TO ZERO. FOUND RT ENG HYD RETURN LINE IN 48 SECTION TO HAVE A HOLE IN IT. REPLACED LINE. SERVICED SYS, LK CKS GOOD.

Part: BEARING — FAILED (RECIRC FAN)

IRREG// ON VECTORING TO FINAL AT CVG FLT ATT REPORTED STRONGSMOKEY, ACRED ODOR IN CABIN. LANDED UNEVENTFULLY AT CVG. SMELL WENT AWAY AFTER LANDING, SMELLED ELEC FROM FWD GALLEY AREA. NO SMOKE DETECTORS WENT OFF. NO SMOKE DETECTED, JUST STRONG SMELL. INSPECTED CABIN AREA FOR VISUAL ODORS FROM LIGHTS OR ELEC COMPONENTS, NONE FOUND. FOUND CABIN AIR RECIRCULATION FAN TO BE VIBRATING EXCESSIVELY. REMOVED AND REPLACED AIR RECIRCULATION FAN. OPS CKS OK. CLOSED AFT BAG BIN. RAN BOTH ENGINES AND OPERATED BOTH PACKS, NO SMELL.

Part: SWITCH — FAILED (NR 1 ENGINE)

L OIL STRAINER CLOG MSG AFTER T/O WOULD NOT EXTINGUISH L ENG SHUT DOWN IAW POW 140000 LBS LANDING NORMAL. REPLACED DIFF PRESS SWITCH. REMOVED AND REPLACED MAIN OIL SCREEN RAN ENG CKD GOOD. NO MSG AND NO LEAKS.

Part: DOOR — OPEN (ACCESS COMPT)

AFTER TAKEOFF, ACCESS COMPARTMENT DOOR CAME OPEN AND AIRCRAFT WOULD NOT PRESSURIZE. DOOR LT EXTINGUISHED AFTER LANDING. UPON ARRIVAL, NO DOORS WERE FOUND TO BE OPEN. AIRCRAFT WAS PRESSURIZED AND NO LEAKS WERE DETECTED. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. NO PRESSURIZATION PROBLEMS WERE NOTED.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR UNSAFE (RED) INDICATION WHEN GEAR HANDLE WAS RAISED AFTER TAKEOFF. CYCLED HANDLE SAME RESULTS. LEFT GEAR DOWN AND RETURNED TO ATL. FOUND NOSE STRUT FLAT. SERVICED STRUT.

Part: AUGMENTATION VLV — MALFUNCTIONED (RT ENGINE)

DURING CLIMBOUT, F/A CALLED WITH STRONG BURNING SMELL INBACK. GOT RT ICE PROT HI-LIGHT. BOTH XFEEDS CLOSED. REDUCED PWR ON RT ENG AND SELECTED HP BLEED OFF ON RT PACK. LIGHT WENT OUT. ADVANCED RT THROTTLE, LIGHT CAME BACK ON. REDUCED PWR LIGHT WENT OUT. REPLACED ANTICIPATOR AND THERMO, AUG VALVE CHECK TESTS GOOD.

Part: BOLT — LOOSE (BRAKE PEDALS)

AFTER LANDING, BRAKES ARE SPONGY AND INEFFECTIVE AND PARKING BRAKE WILL NOT SET. SECURED LOOSE BOLT ON BRAKE SWITCH BRACKET TO ALLOW FULL TRAVEL OF BRAKE PEDAL AND OPERATION NORMAL.

Part: HYD LINE — CHAFED (NR 2 ENGINE)

LOST RIGHT HYD PRESSURE IN FLIGHT, THEN QTY SYSTEM TURNED OFF AND ALT GEAR EXT USED. FOUND RIGHT ENGINE HYD PRESSURE LINE CHAFED AT PLYON ATTACH ANGLE. REPLACED SAME.

Part: FRAME — CRACKED (LT MLG WW)

FOUND DURING E-2 LETTER CHECK, 2.5 INCH CRACK FWD UPPER LEFT WHEEL WELL FRAME. REPAIRED PER SRM 53-05 FIG 78A.

Part: FRAME — CRACKED (RT MLG WW)

FOUND DURING E-2 LETTER CHECK, 2 INCH CRACK IN RIGHT WHEEL WELL FORWARD UPPER FRAME. REPAIRED PER SRM 53-05 FIG 78A.