N990DL

Part: BRACKET — CRACKED (RT MLG WW) · airframe 72,520 hrs · 53,011 cycles

RT WHEEL WELL FAIRING BRACKET CRACKED JUST LOWER OF PROXIMITY SENSOR. REPLACED RT WHEEL WELL FWD DOOR JAMB PER BAC DWG5930584. (LP5962266)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,424 hrs · 52,918 cycles

AFT CABIN EMERGENCY LIGHTS NOT ILLUMINATED WHEN TESTED ON SVC CHECK. REPLACED EMER LIGHT BATTERIES AND FUSE PER MD88 AMM 33-53. FOUND NORMAL OPERATION WHEN TESTED. (LP5587087)

Part: FUSE — BLOWN (BATTERY PACK) · airframe 72,157 hrs · 52,649 cycles

SEAT 31DEF THROUGH 36DEF SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED FUSE 1 IN BATTERY PACK B5-212 REF AMM 33-53 CHECKS GOOD. (LP6018365)

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 71,951 hrs · 52,461 cycles

LT AFT LAVATORY SMOKE DETECTOR CHIRPING. R/R SMOKE DETECTOR PER AMM 26-13. (LP1191067)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 71,641 hrs · 52,178 cycles

FOUND DOOR L1 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED L1 DOOR EMERGENCY LIGHT PER MD88 AMM 33-53. NO FIX. FOUND LIGHT ASSEMBLY DISCONNECTED BEHIND CEILING AND RECONNECTED IT. LIGHT OPERATIONAL CHECK IS OK PER MD88 AMM 33-53. (LP #5453557)

Part: WIRE — BURNED (CABIN) · airframe 71,564 hrs · 52,111 cycles

UPON ARRIVAL TO RAMP IN ATL AND APU SPOOL UP SMELLED ELEC BURNING, A/C CROSSTIE LOCKOUT, RIGHT GEN FELL OFF LINE, APU GEN PICKED UP LOAD, SPARK WAS SEEN IN FIRST CLASS SEAT 1 C/D OVERHEAD. RAN SMOKE/FIRE/FUME CHECKLIST. CABIN STAND BY LGTS C/B, (L) COND REG VALVE, OTHER R SIDE C/B POPPED AS WELL. REMOVED FIRST CLASS FLIGHT ATTENDANT SEAT AND FIRST CLASS FWD CEILING PANELS FOUND WIRING ABOVE SEAT 1 CD. COMPLETED SMOKE AND FUME QUESTIONNAIRE C/W W/C 2120-2367. SEVERAL WIRES ABOVE CEILING PANELS OVER SEATS 1 C AND D WERE BURNED AND REQUIRED REPAIR. REFERENCE LOG PAGES FOR INDIVIDUAL WIRE REPAIRS , 1098674, 1098735, 1098760, 1098765, 1098826, 1098627, 1098772, 1098788, 1098734, 1098727, 1098647, 1098667, 1098678, 1098657, 1098634, 1098622, 1098735, 1097692, 1098722, 1098826, 1098903, 1098714, 1098818, 1098675, 1098684, 1098694, 1098695, 1098751, 1098812, 1099395, 1098765, 1098723. (LP5453522

Part: WIRE — BURNED (CABIN) · airframe 71,563 hrs · 52,110 cycles

REF WDM 30-31-03 PG 2 WIRE F1551B20 FOUND BURNT THROUGH IN OVERHEAD F/C CABIN. RAN AND SPLICED WIRE F1551B20 IAW SWPM 20-10. TERMINATED AT R5-1201 IAW SWPM 20-31. 903393. WIRING CKS C/W IAW WDM 30-31-03. 399270. OPS CHECK PRIM STAM TRIM MOTOR HEATER PER AMM 27-40. CHECKS GOOD. (LP1097692)

Part: WIRE — DAMAGED (CABIN) · airframe 71,563 hrs · 52,110 cycles

REF WDM 35-24-01 WIRE W638CL20 HAS HEAT DAMAGE IN F/C CABIN OVER HEAD AREA. REMOVED AND REPLACED WIRE #W638CL20 FROM CONNECTOR R5-1200 PIN FF TO BUTT SPICE REPAIR ABOVE CEILING PANEL ROW 2CD PER SPWD 20-31. WIRING CKS IAW WDM 35-24-01. PERFORMED PAX O2 SYSTEM OPS CHECK PER AMM 35-20. CKS GOOD. (LP1097696 )

Part: LENS — MISSING (POSITION LIGHT) · airframe 71,443 hrs · 52,007 cycles

DURING WALKAROUND FOUND LEFT AFT POS LIGHT COVER MISSING. RPLCD LENS. (LP5564700)

Part: BRAKE — MALFUNCTIONED (RIGHT) · airframe 71,400 hrs · 51,970 cycles

FELT LIKE (R) BRAKE CAUGHT DURING T/O ROLL GSP . NOSE CAME RIGHT AND SOON AFTER BRAKE OVERTEMP LIGHT FLASHED ON + OFF. INSPECTED #3 BRAKE ,NO TROUBLE FOUND , OK FOR SVC. (LP5799880)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,235 hrs · 51,825 cycles

FOUND FLIGHT DECK AND CABIN EMERGENCY LIGHTS B523/P5 INOP. RELAMPED NO HELP. CHECKED AND FOUND ONE BATTERY WITH ZERO VOLTS. REPLACED BATTERY SET, CKS NML REF MD88 AMM 33-53. (LP5767472)

Part: COOLER — LEAKING (NR 1 FUEL/OIL) · airframe 70,906 hrs · 51,557 cycles

DURING PAX BOARDING APU STARTED AND A/C PACKS TURNED ON . AFTER APPROX. 5 MINUTES WE SMELLED JET EXHAUST/ JET A FUMES IN CABIN. SHUT DOWN APU AND SMELL/ FUMES DISSIPATED WITH GROUND AIR CONNECTED. FOUND FUEL LEAK AT NO 1 ENG. FUEL/OIL COOLER AFT SIDE. R/R O-RING ON FUEL LINE. RAN IDLE LEAK CHECK NO LEAKS. C/W NO GO ODI CHECK LIST 2172. C/W W/ 37, 7100-2619 NO ODORS PRESENT. (LP5548976)

Part: FUSE — BLOWN (BATTERY PACK) · airframe 70,351 hrs · 51,089 cycles

SEAT EMERGENCY LIGHTS ROW 1-12 AND L1 L2 DOOR EXIT SIGNS INOP. T/S PER WDM 33-51-14. FOUND FUSES BLOWN ON B5-211 BATTERY PACK ASSEMBLY. CHANGED FUSES AND OPS CHECKS GOOD. OK FOR SERVICE.

Part: SCHRADER VALVE — LEAKING (NLG) · airframe 70,146 hrs · 50,898 cycles

A/C RETURNED BACK TO SAV FOR NOSE GEAR UNABLE TO RETRACT. PILOTS FOLLOWED QRH PROCEDURES. FOUND SHRADER VALVE LEAKING, REPLACED SAME PER M/M 32-20. SERVICED NOSE STRUT PER W/C 3221-644 OK FOR SERVICE. REPORTED DUE TO DECLARED EMERGENCY. (LP4188484)

Part: PANEL — CRACKED (RT WING) · airframe 69,392 hrs · 50,268 cycles

PERFORM GVI OF RT WING UPPER SURFACE. DUE TO PASSENGER REPORT OF A CRACK ON THE RT WING UPPER SURFACE AS OBSERVED FROM THE CABIN, PLEASE SET- UP TO PERFORM A GVI OF THE RT WING UPPER SURFACE FOR ANY SIGNS OF A CRACK. WHILE WORKING MD LOG 0592224 FOR POSSIBLE UPPER WING CRACK, CONFIRMED CRACK ON UPPER WING PANEL TRAILING EDGE AFT OF HEATER BLANKET. REPAIRED UPPERWING CRACK PER SRM 51-90-0.

Part: DOOR — CRACKED (RTY MLG) · airframe 68,520 hrs · 49,602 cycles

CRACK ON LWR INNER SIDE AT RT STRUT DOOR. RIGHT MAIN DOOR OUTBOARD P/N 5936791-504 S/N:UNK WAS REMOVED AND SERVICEABLE RIGHT DOOR OUTBOARD P/N 5936791-504 S/N DL105 WAS INSTALLED PER AMM 32-12-01-201.

Part: INTERCOSTAL — CRACKED (RT MLG DOOR) · airframe 68,520 hrs · 49,602 cycles

CRACK INTERCOSTAL ON STA Y= 958 RT MLG DOOR. INTERCOSTAL ON STA Y= 958 RT MLG DOOR WAS REPLACED PER SRM 51-30-2, 51-30-5 AND DWG:5930583 REV DA.

Part: DOUBLER — CRACKED (STABILIZER) · airframe 68,520 hrs · 49,602 cycles

INITIAL INSPECTION : CRACK PRODUCTION DOUBLER LT SIDE ON STABILIZER JACKSCREW. PRODUCTION DOUBLER LT SIDE ON STABILIZER JACKSCREW WAS REPLACED PER SRM 51-30-5AND DWG 9911808 REV U.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,776 hrs · 49,051 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 17 AND 29. REPLACED THE BATTERY PACKS AT ROW 17 AND 29, OPS CHECKED GOOD IAW AMM 33-53.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,722 hrs · 49,001 cycles

THREE EMERGENCY LIGHTS INOPERATIVE. FOUND THE BATTERY DISCHARGED IN AFT RT LAVATORY. REPLACED THE BATTERIES IAW MM 33-53. EMERGENCY LIGHTS CHECKED OK.

Part: RHEOSTAT — FAILED (CHART LIGHT) · airframe 66,259 hrs · 47,939 cycles

CAPTAIN`S YOKE, CHART LIGHT SPARKED AND ARCED. REPLACED RHEOSTAT ON THE CHART HOLDER.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 64,319 hrs · 46,494 cycles

MAIN CABIN DOOR WAS OPENED WITHOUT SLIDE BEING DISARMED. SLIDE DID NOT DEPLOY, BUT IS OUT OF THE DOOR. RE-INSTALLED 1L SLIDE IAW AMM 25-62. CHECK NORMAL. NO FURTHER DISCREPANCIES NOTED. AC OK FOR SERVICE.

Part: HANDLE — MISINSTALLED (TAIL CONE) · airframe 63,496 hrs · 45,933 cycles

MAINTENANCE FOUND THE TAILCONE EXTERNAL RELEASE HANDLE IMPROPERLY INSTALLED. CABLE WAS REINSTALLED PROPERLY IAW AMM 53-53-00-501.

Part: FORMER — CRACKED · airframe 63,496 hrs · 45,933 cycles

CRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER LEADING EDGE INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW DC9/MD80 SRM 55-02D, FIG 27, PERFORM INSPECT FOR CRACKS ON L/E SKIN EVERY C-CHECK IAW SRM 55-02D, FIG 27 PAG 113, NOTE 3.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

ELONGED HOLES AT FWD AND AFT HINGES OF MID CARGO DOOR. HOLES OF HINGES WERE REPAIRED IAW ER/A 497387-14 MA, REV B, HOLE HINGE AFT ID 0.798" AND HOLE HINGE FWD ID 0.799.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FRAME CHANNEL IN BS 1307 BETWEEN LONGERON 27RT-LONGERON 27LT AT AFT CARGO COMPARTMENT. REPAIR WAS REPLACED IAW SRM 53-03D, FIG 2A.

Part: ANGLE — CRACKED (BS 991) · airframe 63,496 hrs · 45,933 cycles

CRACKED ANGLE ON BS 991 AND X=7 AT LT MLG WHEEL WELL. ANGLE WAS REPAIRED IAW ER/A413026-14 MA, REV ORIGINAL SRM 51-10-3, PAR 14, 21 AND 51-30-5.

Part: VANE — WORN (RT WING TE FLAP) · airframe 63,496 hrs · 45,933 cycles

WEAR ON RT WING, OTBD FLAP, OTBD VANE AT INBD AFT LWR EDGE. RT WING OTBD FLAP, OTBD VANE AT INBD AT LWR EDGE WAS REPAIRED IAW SRM 57-03, PAR 11, CARD 2000-8149-12 JOB 000-0052 AND ER/A 521199-14 MA, REV ORIGINAL.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,496 hrs · 45,933 cycles

DAMAGE METALLIZER ON RUDDER BOTH SIDE. METALIZER ON RUDDER BOTH SIDE WAS REPAIRED IAW SRM 51-70-1A PAR 23 AND CARD 2000-8149-01, JOB 000-0004.

Part: SKIN — CRACKED (RUDDER) · airframe 63,496 hrs · 45,933 cycles

CRACK ON RUDDER RT SKIN UPPER EDGE. RUDDER RT SKIN UPPER EDGE WAS REPAIRED IAW ER/A 541617-14, REV ORIGINAL AND CARD 2000-8149-06, JOB 000-0018.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 63,496 hrs · 45,933 cycles

DELAMINATION ON UPPER SKIN OF LT INBD FLAP OTBD GUIDE VANE. DELAMINATION ON UPPER SKIN OF LT INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW 57-03 PARR 11.

Part: STRUCTURE — CRACKED (RADIO RACK) · airframe 63,496 hrs · 45,933 cycles

CRACK RADIO RACK EXHAUST. RADIO RACK EXHAUST WAS REPAIRED IAW ER/A 464964-14 MA REV C.

Part: FRAME — CRACKED (BS 1510) · airframe 63,496 hrs · 45,933 cycles

CRACK ON FRAME 1510 CANT APPROXIMATELY 2 O`CLOCK POSITION. FRAME WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1220-1322 UPPER AND LOWER SURFACES AT AFT CARGO COMPARTMENT. LT CARGO TRACK WAS REPLACED IAW 51-30-1, 51-30-2, 51-10-4, 51-10-3 PAR 21 AND 14.

Part: DOUBLER — WORN (LT WING TE FLAP) · airframe 63,496 hrs · 45,933 cycles

WEAR ON DOUBLER LT WING OTBD FLAP INBD VANE BETWEEN BS XV1:159.5 AND XV1: 166 UPPER SKIN. LT WING OTBD FLAP INBD VANE BETWEEN BS XV1: 159.5 AND XV1: 166 UPPER SKIN WAS REPAIRED IAW SRM 57-03D, PAR. 11.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK FWD EDGE PAN WITH BEAM 1 OF MID CARGO DOOR. ACCOMPLISHED AROUND STOP DRILLS NO MORE CRACKS WERE FOUND IAW SRM 51-01, PAR 21, B, NEW DOUBLER WAS FABRICATED, PAINTED AND INSTALLED IAW ETI 88-16-041 AND 51-10-3, PAR 14 AND ER/A 543134-14 REV ORIGINAL.

Part: DOUBLER — NOT REPORTED (BS 370-381) · airframe 63,496 hrs · 45,933 cycles

DURING NDT INSPECTION, A DISCREPANT DOUBLER WAS FOUND ON UPPER FWD CORNER, FS 370 TO 381, IAW SRM 53-05, FIG 68. THESE NRC IS ATTENDED WITH ER/A NO 541596-14AD, REV ORIGINAL.

Part: INTERCOSTAL — BENT (BS 1227-1231) · airframe 63,496 hrs · 45,933 cycles

BENT INTERCOSTAL JUST ABOVE LONGERON 29 LT BS 1231 TO 1227 AT AFT CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21, 51-10-2 AND 53-01, FIG 2.

Part: CARGO TRACK — CORRODED (BS 1007-1220) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON LT TIE TRACK BETWEEN BS Y=1007-1220, UPPER AND LOWER SURFACES, AT AFT CARGO COMPARTMENT. DUE TO EXCCESIVE CORROSION TIE TRACK LT BS Y=1007-1220 AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-30-1 AND 51-10-4.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 7R WITH FRAME, BS 1380. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. LONGERON WAS TREATED AND PAINTED IAW, SRM 51-10-3, PAR 21, 14.

Part: DOOR FRAME — CRACKED (NLG DOORWAY) · airframe 63,496 hrs · 45,933 cycles

CRACK ON NLG DOOR FRAME BS 45 RBL 17 AT NOSE WHEELWELL. DOOR FRAME WAS REPAIRED IAW SRM 51-30-2, 51-30-3, 51-30-5, PAR 14 AND 21. 51-10-2, 51-10-4 AND 53-05, FIG 110.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1007-1155, UPPER AND LOWER SURFACES, IN AFT CARGO BAY. DUE TO EXCESIVE CORROSION THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 63,496 hrs · 45,933 cycles

CRACK AND CORROSION ON FLOOR PANEL COVER LT COCKPIT. REPAIR FABRICATED AND INSTALLED IAW SRM 53-01, FIG 4, SH 4.

Part: ANGLE — CRACKED (BS 1437) · airframe 63,496 hrs · 45,933 cycles

CRACK FRAME CLIP BETWEEN LONG 2L TO 4L AT FRAME BS 1437. FRAME CLIP WAS R & R IAW 51-30-5, 53-14-4, 51-10-3 PAR 14, 21.

Part: SKIN — DAMAGED (LT WING) · airframe 63,496 hrs · 45,933 cycles

ELONGATED SEVERAL ATTACHING HOLES ON LT WING TIP T/E UPPER SKIN SURFACE. LEFT WING TIP UPPER SKIN SURFACE WAS REPAIRED IAW EA 09-478904-14MA, REV ORIGINAL.

Part: SKIN — DAMAGED (LT WING) · airframe 63,496 hrs · 45,933 cycles

ELONGATED SEVERAL ATTACHING HOLES ON LT WING TIP LOWER SKIN SURFACE. LT WING TIP LOWER SKIN SURFACE WAS REPAIRED IAW EA 09-478904-14.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED FWD EDGE PAN WITH BEAM 5 OF MID CARGO DOOR. CRACKS WERE FOUND STOPPED IAW SRM 51-01, 21, A AND STEPS 1, 2 HFEC INSPECTION WAS ACCOMPLISHED AROUND STOP DRILLS NO MORE CRACKS WERE FOUND IAW SRM 51-01, PAR 21, B NEW DOUBLER WAS FABRICATED PAINTED AND INSTALLED IAW SRM 52-03D, FIG 8 AND 51-10-3, PAR 14.

Part: FRAME — CRACKED (BS 1418) · airframe 63,496 hrs · 45,933 cycles

CONTINUE CRACK AFTER STOP DRILL ON REPAIR FRAME 1418 WITH LONG 2R. CRACK WAS DRILLED, ANGLE WAS REMOVED, SUPPORT WAS REMOVED, NEW ANGLE WAS FABRICATED AND TREATED AND PAINTED. SUPPORT WAS INSTALLED IAW IAW SRM 53-03, FIG 31A. FRAME WAS REPLACED IAW SRM 53-03, FIG 31A.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED INNER PAN AFT EDGE WITHBEAM 1 OF MID CARGO DOOR. CRACK INNER PAN AFT EDGE WITH BEAM 1 WAS ACCOMPLISHED INSPECTION. 2 CRACKS WERE FOUND 1.843 AND 0.250" LENGTH IAW SRM 06-10-01-001. CRACK WAS STOPPED IAW SRM 51-01, 21, A AND STEPS 1, 2 HFEC INSPECTION WAS ACCOMPLISHED AROUND STOP DRILLS NO MORE CRACKS WERE FOUND IAW SRM 51-01 PAR 21, B NEW DOUBLER WAS FABRICATED, PAINTED AND INSTALLED IAW SRM 52-03D, FIG 8 AND 51-10-3 PAR 14.

Part: SKIN — CORRODED (ELEVATOR) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON AFT BARREL NUT HOLE 1 AND 2 AT LT SIDE UPPER PANEL REAR SPAR BS XH 26.625. AT LT SIDE WAS PERFORMED IAW ERA 541607-14, REV: A.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,496 hrs · 45,933 cycles

CRACK LONGERON 9R WITH FRAME, BS 1380. LONGERON 9 RT WAS REPAIRED IAW SRM 53-02, FIG 18, AND DRILLED AND ADJUSTED IAW 51-10-4 AND WAS TREATED AND PAINT IAW SRM 51-10-3, PAR 21 AND 14 AND WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1497-1510) · airframe 63,496 hrs · 45,933 cycles

CRACKED INTERCOSTAL BETWEEN BS 1497 CANT TO 1510 CANT APPROXIMATELY 7 HRS POSITION. INTERCOSTAL WAS R & R IAW SRM 51-30-2 AND D/DWG 9917701, REV ORG.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 3L WITH FRAME BS 1437 SECTION LONGERON WAS REPAIRED IAW SRM 51-30-5, 53-02, FIG 18, 51-10-4 AND 51-10-3.

Part: STIFFENER — CRACKED (BS 1463) · airframe 63,496 hrs · 45,933 cycles

CRACK STIFFENER AT FRAME BS 1463 CANT BETWEEN PROTECTION LONG 7L TO 8L. STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-10-3 PARA 14 AND 21, 51-30-3 AND DWG 9911839-29.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 65,524 hrs · 47,404 cycles

CORROSION ON INTERCOSTAL UPPER SURFACE BELOW OF LT TIE DOWN TRACK STA Y= 1307 TO Y= 1322. INTERCOSTAL WAS REPLACED.

Part: FAIRING — CRACKED (RT ELEVATOR) · airframe 63,496 hrs · 45,933 cycles

CRACK ON SETTLEMENT AREA OF ANTI-FLOAT FAIRING. RT ELEVATOR. REPAIR WAS ACCOMPLISHED IAW ET 88-16-030, REV 2 AND ER/A 541630-14, REV ORIGINAL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK PAN ON AFT EDGE BELOW STOP 5 AT MID CARGO DOOR. CRACKS WERE REWORKED IAW SRM 52-03D, FIG 10.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON CUSP WEB BS 503 TO BS 598 BETWEEN X=-54TO X= -60 AT CABIN PASSENGER. CUSP WEB WAS REPLACED DUE TO EXCESIVE DAMAGE IAW SRM 53-05, FIG 131A, 24.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTERSKIN AND SEATING AREA OF FUEL ACCESS PLATE NR 1311C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: FORMER — CRACKED (VERTICAL STAB) · airframe 63,496 hrs · 45,933 cycles

CRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER L/E INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW SRM 55-02D, FIG 27.

Part: CUSP WEB — CORRODED (BS 636-684) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X=-54 TO X=-60 FROM BS 636 TO 639 AND 682 TO 684. CUSP WEB IN STA 636 TO 639 WAS REPAIRED IAW SRM 53-05, FIG 131A-1. CUSP WEB IN STA 682 TU 684 WAS REPAIRED IAW SRM 53-05, FIG 131A-21.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON LT WING OTBD FLAP OTBD VANE LOWER SKIN AT BS XV2: 246 APPROXIMATELY CARD 122, ZONE 10. LT OTBD FLAP OTBD VANE WAS REPLACED IAW SRM 57-50-14, FIG 2A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,496 hrs · 45,933 cycles

DAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,496 hrs · 45,933 cycles

DAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 63,496 hrs · 45,933 cycles

DAMAGE METALLIZED ON RUDDER TAB, CARD 162, ZONE 100. DAMAGE METALLIZED WAS REPAIRED IAW SRM 51-70-1AD.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK AFT EDGE PAN WITH BEAM 5 OF MID CARGO DOOR. AFT EDGE PAN WITH BEAM 5 OF MID CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: DOUBLER — WORN (ELEVATOR) · airframe 63,496 hrs · 45,933 cycles

WEAR ON DOUBLER AT CUTOUT ELEVATOR ACCESS. DOUBLER WAS R & R IAW SRM 53-34-0, 51-30-2 AND 51-10-3 PAR 21, 14.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,496 hrs · 45,933 cycles

CRACK LONGERON 13R WITH FRAME BS 1380. LONGERON WAS REMOVED AND NEW SECTION LONGERON WAS DRILLED AND ADJUSTED TREATED AND PAINTED INSTALLED AND EXHAUST WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 51-10-4, 51-10-3, PAR 21, 14.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

DENTS ON OTBD SKIN BETWEEN BEAM 3 TO 4, 6 DENTS AND BEAM 4 TO 5, 5 DENTS AT MID CARGO DOOR. NEW SKIN WAS REPLACED IAW SRM 51-30-2 AND DWG 5910141, REV FE.

Part: LONGERON — CRACKED (BS 1309) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 8L AT BS 1309 AT FUSELAGE CABIN STRUCTURE. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5 AND 51-10-3, PARR 14, 21.

Part: FINGER DOUBLER — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON INTERNAL FINGER DOUBLER BETWEEN BS 1174-1193 BELOW LONGERON 26L AT AFT CARGO COMPARTMENT C3. FINGER DOUBLER WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 AND 38, AND 53-04-5, FIG 7.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

DENTS ON OTBD SKIN BETWEEN BEAM 1 AND 2, 1 DENTS BEAM 2 AND 3, 1 DENT BEAM 4 AND 5, 8 DENTS AND BEAM UPPER EDGE, 1 DENT AT AFT CARGO DOOR. SKIN WAS REPLACE IAW SRM 51-30-2, 51-30-5, DWG 5910141, REV. FE.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,496 hrs · 45,933 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FLOORBEAM — DAMAGED (BS 1309) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON REPAIR DOUBLER OF FLOORBEAM BETWEEN X=18 TO X=24, BS 1309 AT FLOOR STRUCTURE CAB. DOUBLER WAS REPLACED IAW SRM 51-10-3, PAR 14, 21 AND 38, 51-30-5 AND 53-05 FIG 20A.

Part: ISOLATOR — CORRODED (RT ENGINE) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON INNER SURFACE OF HOUSING BOLTS ON RT ENGINE AFT VIBRATION ISOLATOR. ON RT ENGINE AFT VIBRATION ISOLATOR WAS CLEANED AND CORROSION WAS FOUND. DUE TO CORROSION REPLACED AND INSTALLED IAW AMM 71-20-02-201 AND PS 900-1-2-1, NR 01.

Part: PAN — CRACKED (R1 DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK ON PAN FWD EDGE BEAM NR 4 AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03D, FIG 3, 51-01 PAR 21, 51-30-1, 51-30-4.

Part: LONGERON — CORRODED (BS 1287-1307) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON LONGERON 23L, BETWEEN BS 1287 - 1307. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 19, 51-30-2, 51-30-5, AND 51-10-3, PAR 26-21, 14.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FLOOR PANEL 160G IN PAX CABIN. THE FLOOR PANEL WAS REPLACED IAW SRM 51-30-2 AND DWG 9957828, REV AB.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED BEAM NR 4 FWD EDGE AT FWD SERVICE DOOR. NEW BEAM WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, 51-10-3 PAR 14/21 AND 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,496 hrs · 45,933 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK FWD EDGE PAN WITH BEAM NR 5 OF FWD CARGO DOOR. CRACK ON FWD EDGE PAN WITH BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: ANGLE — CRACKED (BS 1437 FRAME) · airframe 63,496 hrs · 45,933 cycles

CRACK FRAME CLIP ON BS 1437 BETWEEN LONGERON 16 - 17R. CLIP WAS REMOVED AND WAS FABRICATED IAW SRM 51-30-5 AND IAW DWG 9911840-75, REV DC AND NEW CLIP WAS INSTALLED IAW SRM 51-30-5.

Part: FITTING — CORRODED (BS 522) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FRAME FITTING BS 522. FITTING WAS REPLACED IAW SRM 51-10-8, 51-10-3 PAR 14, 21.

Part: RETAINER — CRACKED (CARGO DOOR SEAL) · airframe 63,496 hrs · 45,933 cycles

CRACK AND WEAR RETAINER SEAL AT FWD CARGO DOOR. RETAINERS WERE FABRICATED IAW SRM 52-33-0, FIG 1.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 63,496 hrs · 45,933 cycles

CRACK ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, 51-10-3, PAR 14 AND 21, 21-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK FWD EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. CRACK ON FWD EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. WAS REPAIRED IAW SRM 52-3D, FIG 8.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FRAME, BS 1380 BETWEEN LONGERON 24L TO 24R. FRAME BS 1380 WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21 AND DWG 9912246-115.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACK AFT EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. CRACK ON AFT EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG. 8.

Part: FLOOR SUPPORT — CRACKED (BS 1348) · airframe 63,496 hrs · 45,933 cycles

CRACKED FLOOR SUPPORT JUST NEXT TO 6 PULLEY BRACKET, 18 BS 1348. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21, 51-30-1, 51-30-2, 51-30-05A AND 53-01, FIG 2.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED BEAM NR 1 AFT EDGE AT FWD PASSENGER ENTRANCE DOOR L1. BEAM NR 1 AFT EDGE WAS REPAIR IAW SRM 52-05D, FIG 81, SHEET 3, 51-30-1, 51-10-3 PAR. 14 AND 21.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED FWD CLIP ON BEAM NR 1 AT FWD PASSENGER ENTRANCE DOOR L1. CLIP ON BEAM NR 1 AT FWD WAS REPLACE IAW DWG 9955752, REV K, 51-10-2 51-10-3 PARA 14 AND 21, 51-30-2.

Part: ATTACH ANGLE — CORRODED (BS 1350) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON ANGLE ATTACH LOWER DOOR JAMB OF VENTRAL STAIRWAY BETWEEN 18 TO 18, BS 1350. AREA WAS REPAIRED IAW SRM 53-05, FIG 34 AND 51-10-3 PAR 21 AND 14.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 63,496 hrs · 45,933 cycles

WEAR AND BEND FWD AND AFT LOWER EXTERNAL DOUBLERS AT FWD CARGO DOOR. DOUBLERS FWD AND AFT LOWER WERE REPLACED IAW ERA: 486624-14MA, REV ORIGINAL.

Part: DOOR FRAME — WORN (ACCESSORY BAY) · airframe 63,496 hrs · 45,933 cycles

WEAR ON FWD ACCESSORY COMPARMENT DOOR JAMB. WEAR WAS ATTENDED IAW SRM 51-10-3, 53-01, ER/A 527558-14, REV ORIG.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 63,496 hrs · 45,933 cycles

CRACKED INTERCOSTAL FROM BS 1287 TO BS 1307 X=0 AND 1271 TO 1287 X=5 AT PAX CABIN. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2 AND 51-10-3, PAR 21 AND 14 OTHER INTERCOSTAL WAS REPLACE ON BS 1287 TO 1307 X=0 WAS REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: SKIN — WORN (FUSELAGE) · airframe 63,496 hrs · 45,933 cycles

WORN PREVIOUS REPAIR DOUBLER ON HOLD OPEN HOOK AREA AT PASSENGER ENTRANCE DOOR L1. REPAIR DOUBLER WAS REPLACED IAW ERA 486216-14 MA, REV A.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED BEAM NR 8 AFT EDGE AT PASSENGER ENTRANCE DOOR L1. BEAM NR 8 AFT WAS REPAIR IAW SRM 52-05, D FIG 111, SHEET 3, 51-30-1, 51-30-2, AND 51-30-5.

Part: BEARING — CORRODED (RT MLG) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION AND WEAR ON RT MAIN GEAR SUPPORT FITTING BEARING. RT MAIN GEAR SUPPORT FITTING BEARING WAS REPLACED IAW CMM 57-40-02 AND CARD 5740-01139-04B, JOB 048-0001. (LP2322697)

Part: BEARING — CORRODED (LT MLG) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION AND WEAR ON LT MAIN GEAR SUPPORT FITTING BEARING. LT MAIN GEAR SUPPORT FITTING BEARING WAS REPLACED IAW CMM 57-40-02 AND CARD 5740-01139-04A, JOB 048-0001.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON INTERCOSTAL BETWEEN LOWER EDGE AND BEAM NR 1 BS 655 OF MID CARGO DOOR. DAMAGE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: STRUCTURE — CRACKED (BS 1338) · airframe 63,496 hrs · 45,933 cycles

CRACKED STR BS 1338 INTERSECTION LONGERON 1 AT PAX CABIN. STR WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FUEL ACCESS DOOR COUNTERSINK/SETTLEMENT AREA NR 1460C AT RT WING. FUEL ACCESS DOOR 1460C WAS FOUND OUT OF LIMITS THEN WAS REPLACED.

Part: LONGERON — CRACKED (BS 1309) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 5 LT BS 1309 AT FUSELAGE CABIN STRUCTURE. LONGERON 5 LT WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 605-617) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 605 AND 617 FROM X=60 AND X=54 FLOOR CABIN STRUCTURE. CUSP WEB FROM BS 598 TO BS 712 WAS REPLACED IAW SRM 51-30-5, 51-30-1, 51-30-2, 51-10-4, AND 51-10-3.

Part: SKIN — DAMAGED (BS 617-636) · airframe 63,496 hrs · 45,933 cycles

LIGHTNING STRIKES ON LT WINDOW BELT CUTOUT BETWEEN BS 617 TO 636. LIGHTNING STRIKE ON LT WINDOW BELT CUT OUT BS 617 TO 636 WAS REPAIRED BY BLEND OUT AND ITS WITHIN LIMITS IAW ER/A 541610-14, REV ORIGINAL AND ETI-88-16-012, REV 2.

Part: FLOOR SUPPORT — CRACKED (BS 1022-1041) · airframe 63,496 hrs · 45,933 cycles

CRACK ON INTERCOSTAL AFT SECTION BS X=0 BETWEEN 1022-1041 AT CABIN FLOOR STRUCTURE. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.

Part: FLOOR SUPPORT — CRACKED (BS 1348) · airframe 63,496 hrs · 45,933 cycles

CRACKED INTERCOSTAL JUST NEXT TO 6 PULLEY BRACKETS X=-24 BS 1348 AT FLOOR STRUCTURE CABIN. INTERCOSTAL WAS REPAIRED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21, AND 53-01, FIG 2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON RT WING HEATER BLANKET FUEL SECONDARY ACCESS PLATE NR 1409C. RT WING HEATER BLANKET FUEL SECONDARY ACCESS PLATE NR 1409C WAS REPLACED IAW IPC 57-30-00.

Part: ANGLE — CRACKED (BS 1338) · airframe 63,496 hrs · 45,933 cycles

CRACKED LOWER CLIP DEFORMED N.14 RT BS 1338 ON X-60 AT PAX CABIN. CLIP WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-14, 51-10-3, PAR 21 AND 14.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 63,496 hrs · 45,933 cycles

BENT PREVIOUS REPAIR DOUBLER FWD LOWER EDGE AT PASSENGER ENTRANCE DOOR L1. PREVIOUS REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-2 AND NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 52-05D, FIG 37, SHEET 1.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED BEAM NR 1 AFT EDGE AT FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5 AND DWG 9911579, REV "L".

Part: LONGERON — CRACKED (BS 1338) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 7L BS 1338 AT FUSELAGE CABIN STRUCTURE. LONGERON END 7 LT WAS REPLACED IAW DWG, REV H, SRM 51-10-3, PAR 14, 21, SRM 51-10-4 AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 772-776) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

OUT OF LIMITS CUSP WEB BETWEEN BS 739-743 AND BS 772-776 X=-54 TO X=-60 AT RT SIDE. CUSP WEB WAS REPAIRED ON BS 739-743 AND 772-776 BETWEEN X=-57 TO X=-60 AT RT SIDE. ON REF CARD 73, ACFT ZONE 201 IAW SRM 51-30-1, 51-30-5, 51-30-2, 53-05, FIG 131A-6, 53-05 FIG 131A-13 AND 51-10-3 PAR. 14 AND 21.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 63,496 hrs · 45,933 cycles

DAMAGED FLOOR PANEL 160C. FLOOR PANEL 160C WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,496 hrs · 45,933 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,496 hrs · 45,933 cycles

CRACK LONGERON 16R WITH FRAME BS 1437. SECTION LONGERON WAS REPLACED BS 1437 IAW SRM 53-14-4, 51-30-2, 51-30-05 51-10-3, PAR 21 AND 14 AND DWG 5910228, REV KH.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED INTERCOSTAL BETWEEN BEAMS NR 4 AND NR 5 AT PASSENGER ENTRANCE DOOR L1. INTERCOSTAL BETWEEN BEAM NR 4 AND 5 AT WAS REPLACED IAW DWG 9955763, REV:M AND 51-30-2, 51-10-3.

Part: CUSP WEB — CORRODED (BS 599-610) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X=-54 TO X=-60 FROM BS 599 TO BS 610 AND BS 600 TO BS 604, IN REF ORNRC 78, ZONE 201, SM, CARD 310, ZONE 201. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: WEB — CRACKED (ANTI ICE DUCT) · airframe 63,496 hrs · 45,933 cycles

CRACK ON INTERNAL WEB, ANTI-ICE DUCT HOUSING, APPROXIMATELY XOS=379 AT RT SLAT NR 3. INNER SKIN WAS REMOVED AND INTERNAL WEB WAS FABRICATED AND REPLACED THEN INNER SKIN WAS INSTALLED IAW SRM 51-30-2, 51-30-8 AND DWG 9922514-REV U.

Part: LONGERON — CRACKED (BS 522) · airframe 63,496 hrs · 45,933 cycles

CRACK ON LONGERON 4R BS 522 AT CABIN STRUCTURE. LONGERON SECTION WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-5, 51-30-2, AND 51-10-3, PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FUEL ACCESS DOOR COUNTERSINK/SETTLEMENT AREA NR 1361C AT LT WING. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A. ANGLE ON NEW FUEL ACCESS WAS INSTALLED IAW SRM 51-30-05.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,496 hrs · 45,933 cycles

CRACKED LONGERON 5L WITH FRAME BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTERSKIN AND SETTLEMENT AREA AT FUEL ACCESS NR 1456C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

ELONGED HOLES AND CORROSION ON COUNTER SINK AT FUEL ACCESS NR 1464C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTER SINK AND TOOL DAMAGE ON SKIN AT FUEL ACCESS NR 1363C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTER SINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1454C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FUEL ACCESS DOOR COUNTERSINK SETTLEMENT AREA NR 1436C AT RT WING. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTERSKIN AT FUEL ACCESS NR 1355C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTER SINK AND SEATING AREA OF FUEL ACCESS PLATE NR 13570. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTER SINK AND SETTLEMENT AREA AT FUEL ACCESS NR 1462C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — PUNCTURED (BS 758) · airframe 63,496 hrs · 45,933 cycles

PUNCTURED CUSP WEB AT BS 758 APPROXIMATELY AND X=-54 CABIN PASSENGER CUSP WEB WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21, 53-05 FIG 131A-2, 51-30-2, SEAT TRACK WILL BE INSTALLED WITH CARD NR 309, ZONE 201 AND CIC BE APPLYED WITH CARD 18, ZONE 201.

Part: CUSP WEB — CRACKED (BS 592-595) · airframe 63,496 hrs · 45,933 cycles

CRACK ON LT CUSP WEB BS 592-595, X=-54 AT FLOOR STRUCTURE IN REF CARD 56, ZONE 201. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,496 hrs · 45,933 cycles

CRACK LONGERON 11R WITH FRAME, BS 1380. CARD 07, ZONE 61. LONGERON WAS REPLACED IAW SRM 51-30-2, 53-14-4, 51-30-5, 51-10-4 AND 51-10-3, PAR 14 AND 21.

Part: RIB — CORRODED (RT SLAT) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FWD AND AFT HOLES OF RIB IN BS XOS=380 AT RT SLAT NR 3. CARD 14, ZONE 12. HOLES OF RIB WERE REWORKED, REAMED, MEASURED ID 1.123" ON HOLE FWD AND 1.1235" ON HOLE AFT, TREATED AND REPAIRED IAW SRM 57-02, PAR 9, 51-10-3, PAR 21 AND 51-30-10, PAR 7.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON FUEL ACCESS DOOR COUNTERSINK/SETTLEMENT AREA NR 1466C AT RT WING. CARD 323, ZONE 100. FUEL ACCESS 1466C WAS REMPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CRACKED (BS 994-996) · airframe 63,496 hrs · 45,933 cycles

CRACKED RT CUSP WEB X -54 TO X -60, BS 994 TO 996. REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-2 AND 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 1079) · airframe 63,496 hrs · 45,933 cycles

CRACKED RT CUSP WEB X -44 TO X -54, BS 1079. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-30-2.

Part: DOOR FRAME — CRACKED (E/E BAY DOORWAY) · airframe 63,496 hrs · 45,933 cycles

CRACK ON ELECTRONIC EQUIPMENT DOOR FRAME AT BS 146 AND LONG 27 LT. DOOR FRAME WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON T/E BUSHINGS AT RT WING HEATER BLANKET AREA. BUSHINGS WERE REPLACED IAW PS 900-9-1, NR 6 AND SRM 51-30-10.

Part: LONGERON — CRACKED (BS 541) · airframe 63,496 hrs · 45,933 cycles

CRACK ON LONGERON 4 LT BS 541 AT CABIN STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-10-3 PAR 14, 21.

Part: TAB — DENTED (LT ELEVATOR) · airframe 63,496 hrs · 45,933 cycles

SEVERAL DENTS ON GEAR TAB LT ELEVATOR. DENTS ON GEARED TAB WERE REPAIRED IAW SRM 55-04.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTERSKIN AND SEATING AREA OF FUEL ACCESS PLATE NR 1303C. FUEL ACCESS DOOR NR 1303 WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD 2800-0120 JOB 001-0451.

Part: CUSP WEB — CRACKED (BS 807) · airframe 63,496 hrs · 45,933 cycles

CRACKED RT CUSP WEB ON BS 807 BETWEEN X=-54 TO -60, CUSP WEB WAS REPAIRED IAW SRM 53-03, FIG 131A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

CORROSION ON COUNTER SINK AND SEATING AREA OF FUEL ACCESS PLATE NR 1409C. FUEL ACCESS DOOR NR 1407C WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CRACKED (BS 266) · airframe 63,496 hrs · 45,933 cycles

CRACKED LT CUSP WEB BS=266 AND X=58 AT PAX CABIN, REF: CARD 70 ZONE 201. CRACKED LT CUSP WEB BS=266 AND X=58 WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · corrosion level 2 · airframe 63,496 hrs · 45,933 cycles

ELONGATED HOLES 2 EA AND PUNCTURE ON COUNTER SINK HOLE AT FUEL ACCESS PLATE 2301C. FUEL ACCESS DOOR 2301C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD 5730-0655 JOB 001-0479.

Part: CUSP WEB — CRACKED (BS 218-229) · airframe 63,496 hrs · 45,933 cycles

CRACK ON CUSP WEB BS 218 TO BS 229 BETWEEN X=-54 TO X=-60 AT CABIN PASSENGER. CUSP WEB WAS REPLACED IAW SRM 51-10-3, PAR 14 & 21, 51-30-1, 51-30-2, 51-30-5.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 63,496 hrs · 45,933 cycles

DISBONDED MATERIAL AND PUNCTURE ON RT INBD FLAP INBD VANE. DAMAGE ON RT INBD FLAP INBD VANE EXCEED FOR REPAIR LIMITS IAW SRM 57-03D, PARR II THEREFORE WAS REPLACED WITH REPAIRED RT INBD FLAP INBD VANE.

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACK ON LT WINDOWS RING PAN AT LOWER FWD CORNER BETWEEN ST 1022-1041, ST 1041-1060. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, SRM 51-10-3 PAR 14, 21, SRM 51-30-2, 51-30-5, ER/A 487747-14MA, REV "A" AND 493648-14MA, REV "A".

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON LT WINDOWS RING PAN AT LWR AFT CORNER BETWEEN ST 731-712, 769-788, 807-826, ST 886-905. RING PANS WAS REPAIRED IAW SRM 53-05, FIG 122, SRM 51-10-3, PAR 14, 24, SRM 51-30-2, 51-30-5, ERAS 487747-14MA, REV "A" AND 493645-14MA, REV "A".

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON LT WINDOWS RING PAN AT UPPER AFT CORNER BETWEEN ST 1079-1098, ST 1231-1212. AREAS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14 AND 21, 51-30-2, 51-30-5, ER/A 487747-14MA, REV A AND 493648-14MA, REV A.

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON LT WINDOWS RING PAN AT UPPER FWD CORNER BETWEEN ST 579-598, ST 731-750, 1022-1041. AREAS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14C 21, 51-30-2, 51-30-5 AND ER/AS 487747-14MA, REV A, 493648-14MA, REV A.

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON RT WINDOW RING PAN AT LOWER AFT CORNER BETWEEN ST 1117-1136. WINDOWS RING PAN WAS REPAIRED IAW SRM 51-30-5, 51-30-2, 53-05 FIG 122, ER/AS 487747-14MA, REV A AND 493648-14MA, REV A.

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACK ON RT WINDOWS RING PAN AT UPPER AFT CORNER. WINDOWS RING PAN WERE REPAIRED IAW SRM 51-30-5, 51-30-2, 53-05, FIG 122 ER/AS 487747-14, REV A, 493648-14MA, REV A.

Part: PAN — CRACKED (WINDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON RT WINDOWS RING PAN AT LOWER FWD CORNER BETWEEN ST 1117-1136, ST 1097-1117, ST 984-1003. WINDOWS RING PAN WERE REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 ER/AS 487747-14MA AND 493648-14MA, REV A.

Part: PAN — CRACKED (WONDOW) · airframe 63,496 hrs · 45,933 cycles

CRACKS ON RT WINDOWS RING PAN AT UPPER FWD CORNER BETWEEN ST 1136-1155, ST 807-826. WINDOWS RING PAN WERE REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND ER/AS 487747-14 MA, REV A, 493648-14 MA, REV A.

Part: SEAT TRACK — CORRODED (BS 1130-1136) · airframe 63,496 hrs · 45,933 cycles

CORROSION ON PLUG AT RT SEAT TRACK, X=-22 FROM BS 1130 TO BS 1136. PLUG WAS REPLACED IAW SRM 51-30-1 AND 53-05, FIG 4A.

Part: ANGLE — CRACKED (DOOR) · airframe 63,496 hrs · 45,933 cycles

CRACKED ANGLE ON TOP REAR CHANNEL AT RT AFT OVERWING EMERGENCY EXIT DOOR. INNER SKIN AND ANGLE WERE REMOVED, NEW ANGLE WAS FABRICATED, TREATED, PAINTED, INNER SKIN AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 21 AND 14, DWG 9957735, REV G.

Part: SKIN — CRACKED (AIRSTAIR DOOR) · airframe 61,080 hrs · 44,276 cycles

SKIN CRACKED THRU RIVET AT LOWER AFT RADIUS OF AIRSTAIR DOOR BELOW L1 DOOR. NDT VERIFIED CRACK. REPAIRED IAW SRM 53-05, FIG 57A.

Part: FRAME — CRACKED (BS 1485) · airframe 59,907 hrs · 43,472 cycles

TAIL INTERIOR CRACKED BS 1485 CANTED FRAME WEB. CONFIRMED WITH HFEC. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-03D, FIG 48.

Part: BUSHING — WORN (TAILCONE) · airframe 59,834 hrs · 43,427 cycles

MAINTENANCE DISCOVERED THAT THE TEE PIN BUSHING WAS WORN BEYOND ALLOWABLE LIMITS AND REQUIRED REPLACEMENT.

Part: ANGLE — CORRODED (TAILCONE) · airframe 59,907 hrs · 43,472 cycles

ACFT FAILED FUNCTIONAL CHECK OF TAILCONE RELEASE SYS DUE TO THE TEE PIN ANGLES CORRODED AND TIGHT. THE ANGLES WERE REPLACED AND THE FUNCTIONAL CHECK WAS GOOD.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 59,834 hrs · 43,427 cycles

CORROSION ON FLOOR STRUCTURE LT AND RT OF FLOOR PANEL 160C AFT OF COCKPIT DOOR. REPAIRED IAW ER/A 527590-14.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 59,834 hrs · 43,427 cycles

MAINTENANCE DISCOVERED THAT THE RELEASE LATCH TEE PIN FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. TEE PINS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECKED SATISFACTORILY.

Part: CAM — WORN (TAILCONE) · airframe 59,834 hrs · 43,427 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 59,834 hrs · 43,427 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. CABLE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: SKIN — CRACKED (BS 1380) · airframe 59,834 hrs · 43,427 cycles

ACFT SKIN HAS A ONE INCH LONG CRACK AT BS 1380, ONE INCH ABOVE LONGERON 14L. REPAIR INSTALLED IAW PRI 527562-14, REV 0.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 59,834 hrs · 43,427 cycles

MAINTENANCE DISCOVERED THAT ONE OF THE TAILCONE RELEASE SYSTEM LATCH PIN RECEPTACLES WAS WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BOTTLE — EMPTY (R1 DOOR SLIDE) · airframe 59,664 hrs · 43,313 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE INFLATION BOTTLE AT R1 DOOR WAS DEPLETED. DOOR SLIDE WAS REPLACED.

Part: FILTER — CONTAMINATED (NR 2 ENGINE OIL) · airframe 59,458 hrs · 43,185 cycles

CREW REPORTED DURING APPROACH, THAT THE RT OIL STRAINER CLOG MESSAGE ILLUMINATED. CREW DECLARED AN EMERGENCY. MAINTENANCE FOUND HEAVY CONTAMINATION OF THE OIL FILTER. MAINTENANCE R & R THE NR 2 ENGINE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 58,579 hrs · 42,619 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 17-24 INOPERATIVE. FOUND A CONNECTOR DAMAGED, REPLACED CONNECTOR, AND CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,396 hrs · 42,512 cycles

DURING LINE CHECK, NOTED THE LEFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED NORMALLY.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 57,949 hrs · 42,212 cycles

F/A REPORTED THE L2 DOOR, FLOOR ATTACHMENT POINT FOR GIRT BAR LOOSE. MAINTENANCE SECURED BRACKET AND VERIFIED PROPER OPERATION OF THE GIRT BAR ATTACHMENT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,451 hrs · 41,839 cycles

DURING ROUTINE LINE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS FROM ROWS 16-30 WERE FOUND TO BE INOPERATIVE. BATTERY PACKS AT ROWS 17, 24 & 29 WERE REPLACED AND OPERATION CHECKED NORMALLY IAW AMM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,221 hrs · 41,678 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND THE GALLEY AT DOORS L1 & L2 WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CORRODED (BS 1320) · airframe 57,131 hrs · 41,621 cycles

DURING LINE INSPECTION, CORROSION WAS FOUND AT THE AFT LAV SERVICING POINT SKIN AT BS 1320 LONGERON 22L. REPAIRED IAW ER/A 516268-14.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,858 hrs · 41,423 cycles

UPON ARRIVAL, THE 1L DOOR SLIDE CAME OUT OF THE SLIDE PACK AND DID NOT INFLATE. IT WAS NOTED THAT THE GIRT BAR WAS NOT ENGAGED WHEN THE SLIDE CAME OUT OF THE PACK. THE 1L SLIDE WAS REPLACED IAW WC 2500-4484 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: THRESHOLD — CORRODED (BS 636-693) · airframe 56,270 hrs · 41,035 cycles

CORROSION ON MID CARGO DOOR THRESHOLD BS 636 TO 693. REPAIRED MID CARGO DOOR THRESHOLD STA 636 TO 693 IAW SRM 53-05. RII COMPLIED WITH.

Part: SKIN — CORRODED (BS 1190-1200) · airframe 56,270 hrs · 41,035 cycles

CORROSION AFT CARGO BAY NOTED BETWEEN SKIN LAYERS BS 1190 TO BS1200 DOOR THRESHOLD AREA. MRB 53-019-02. COMPLIED WITH ALL STEPS OF ER/A 508144-14, REV O.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 56,270 hrs · 41,035 cycles

CORROSION ON AFT CARGO BAY THRESHOLD JAMB FROM FORWARD END TO AFT END. MRB 53-019-02. FOUND TO BE OUT OF LIMITS, 100 PERCENT MATERIAL LOSS. R & R BEAM AT BS 1117 TO BS 1250, RBL 14 AT AFT CARGO BAY DOOR JAMB IAW SRM 51-30-05 AND SRM 51-30-02.

Part: FRAME — CORRODED (BS 1212) · airframe 56,267 hrs · 41,033 cycles

FOUND CORROSION ON S 1212 FRAME FROM LONGERON 26R TO LONGERON 28R AFT FACE. NO PREVIOUS BLEND OUT MRB 53-019-02. COMPLIED WITH STEPS OF DELTA PRI ER/A 508143-14, REV O.

Part: SKIN — DAMAGED (BS 727) · airframe 56,267 hrs · 41,033 cycles

ELONGATED FASTENER HOLE AT BS 727 BETWEEN LONGERON 30 AND 29R. COMPLIED WITH ER/A 508140-14, REV O.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,267 hrs · 41,033 cycles

TAILCONE UPPER MID EXTERIOR SKIN SURFACE IS GOUGED. REPAIRED IAW ER/A 508142.

Part: FRAME — CORRODED (BS 1155) · airframe 56,267 hrs · 41,033 cycles

FOUND CORROSION ON BS 1155 FRAME LONGERON 26R FORWARD FACE. COMPLIED WITH ALL STEPS OF PRI ER/A 508143-14 REV O.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 56,267 hrs · 41,033 cycles

PERFORMING TAILCONE FUNCTIONAL TEST, DOOR ARM PIN, PRESSURE BULKHEAD, AND FITTING DAMAGED. R & R EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM PIN AND FITTING IAW CMM RII COMPLETED.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 56,267 hrs · 41,033 cycles

INNER CARGO DOOR STRUCTURE FOUND TWO LOCATIONS OF CORROSION ON BEAMS. REMOVED CORROSION FROM AREAS, REPAIRED ONE AREA FOUND TO BE OUT OF LIMITS, RESTORED ALL REWORK AREAS, AND FINISH.

Part: THRESHOLD — CORRODED (BS 376) · airframe 56,267 hrs · 41,033 cycles

FORWARD CARGO DOOR THRESHOLD STA 376 CORRODED. REMOVED CORRODED DOOR SEAL DEPRESSOR SPLICE. INSTALLED NEW DOOR SEAL DEPRESSOR SPLICE IAW DWG 5910142, SRM 51-30-02.

Part: THRESHOLD — CORRODED (BS 420) · airframe 56,267 hrs · 41,033 cycles

FORWARD CARGO DOOR THRESHOLD BS 420, CORRODED. REMOVED, INSTALLED CORRODED/NEW DOOR SEAL DEPRESSOR SPLICE IAW SRM 51-30-02.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 56,267 hrs · 41,033 cycles

LEFT MLG WHEEL WELL FORWARD LOWER FRAME ATTACH ANGLE IS CRACKED 35: OTBD OF THE KEELBEAM. FABRICATED, HEAT TREATED, ALODINED, PRIMED, CIC'D AND INSTALLED ANGLE IAW SRM 51-30-02, 51-10-03, PARA 14, 21 AND 38 DAC DWG 5930584.

Part: LONGERON — CORRODED (BS 1287 L28R) · airframe 56,267 hrs · 41,033 cycles

LONGERON 28R 2 INCHES AFT OF FRAME BS 1287 CORRODED. BLENDED CORROSION. FOUND TO BE OUT LIMITS AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-02, STEP 13.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 56,033 hrs · 40,879 cycles

DURING SERVICE CHECK, MX FOUND SEAT MOUNTED EMERGENCY ESCAPE PATHWAY LIGHTS INOPERATIVE FROM ROW 18 TO 23. MX FOUND LOOSE SPLICE AT ROW 18, BELOW TRACK. SECURED SAME. OPS CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,308 hrs · 40,400 cycles

R1 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY B5-23. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,308 hrs · 40,400 cycles

UPPER TWO EMERGENCY TAIL CONE LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPLACED BATTERIES IN POWER SUPPLY B5-28. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,308 hrs · 40,400 cycles

FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY B5-100. REPLACED LAMPS. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,308 hrs · 40,400 cycles

L1 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY B5-23. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 55,308 hrs · 40,400 cycles

OVERHEAD AFT CATWALK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE DISCONNECTED. RECONNECTED PER WDM. OPS CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,308 hrs · 40,400 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY B5-23. OPS CHECKED GOOD.

Part: TAIL CONE — WORN · airframe 54,370 hrs · 39,792 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE INTERIOR RELEASE T-PIN SLOTS WORN. INSTALLED NEW RELEASE T-PIN PER AMM. FUNCTIONAL CHECK PER 6808AD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,450 hrs · 39,233 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND SEVERAL FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE BATTERY CHARGER PACK AND THE LIGHTS RETURNED TO NORMAL OPERATION.

Part: RELAY — DAMAGED (CABIN) · airframe 52,722 hrs · 38,731 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT EXIT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE FOUND RELAY, R2-271, DAMAGED AND REPLACED IT. OPERATIONAL CHECK OF LIGHTS WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,523 hrs · 37,307 cycles

DURING LINE CHECK MX FOUND EMERGENCY PATH LIGHT AT 3C INOPERATIVE. MX REPLACED LIGHT ASSEMBLY IAW AMM. OPS CHECK OF LIGHT NOW GOOD.

Part: SWITCH — DEFECTIVE (COCKPIT) · corrosion level 2 · airframe 49,960 hrs · 36,932 cycles

ON CLIMBOUT STRONG ELECTRICAL SMELL IN COCKPIT. RETURNED FOR LANDING. ONCE STOPPED, SMOKE AND SPARKS OBSERVED FROM UNDER CAPTAINS GLARESHIELD. FIRE PUT OUT WITH EXTINGUISHER. FOUND RT WING LANDING LIGHT CONTROL C/B POPPED. FOUND RT WING LANDING LIGHT BURNT. REPLACED SWITCH AND WIRE TERMINALS (2010-D0841) (DL88101903).

Part: FRAME — CORRODED (BS 1271 S26L-27R) · airframe 49,253 hrs · 36,504 cycles

AFT CARGO STA 1271, STR 26L-27R FRAME CORRODED/REPLACED FRAME SECTION AT HMV IAW SRM 53-03D, FIG 286 4A.

Part: SKIN — DENTED (BS 332 S19R) · airframe 49,253 hrs · 36,504 cycles

FUS DENT RT SIDE AT BS 332 BETWEEN LONG 19-20R APPROX 4" X 3". REPAIRED IAW SRM 53-04D, FIG 38.

Part: WEB — CORRODED (STA 1212-1220) · airframe 49,253 hrs · 36,504 cycles

WEB CORRODED AT STA 1212-1220 AFT CARGO DOOR CUT OUT AREA/ REPLACED WEB IAW SRM 51-30-5.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 49,253 hrs · 36,504 cycles

DURING HMV3 DHN (PEMCO) CAPT'S OTBD UPPER SEAT TRACK AT AFT END IS CRACKED. REMOVED DAMAGED TOP FLANGE OF SEAT TRACK IAW SRM 53-05, FIG 92 SHT 1 THRU 3, RECEIVED NEW SEAT TRACK "T" ANGLE PN SR09530111U11. LOCATED, DRILLED, DEBURRED IAW SRM 51-10-04 INSTALLED "T" ANGLE IAW SRM 51-30-05.

Part: FLOORBEAM — CORRODED (STA 241) · airframe 49,253 hrs · 36,504 cycles

MAIN PASS CABIN STA 241 LBL42 FLOOR SUPPORT CORRODED/ FABRICATED NEW FRAME SECTION USING EXT S2929169 IAW SRM 53-01 AND 51-10-03.

Part: INTERCOSTAL — CRACKED (STA 1295-1306) · airframe 49,253 hrs · 36,504 cycles

MAIN CABIN STA 1295 TO 1306, BL0 INTERCOSTAL BETWEEN BEAM CRACKED IN 4 PLACES.

Part: STRAP — CORRODED (BS1231-1271 L23L) · airframe 49,253 hrs · 36,504 cycles

DURING HMV3, AFT CARGO BETWEEN STATION 1231-1271, L23L STRAP IN CENTER OF LONGERON IS EXFOLIATED OUT OF LIMITS. REMOVED STRAP IAW SRM 51-30-02 MATERIAL USED FOR NEW STRAP 7075T6 .250, FAB OF -75 STRAP ACCOMPLISHED ON TRAVELER NR 1943N01202 IAW DWG 5911423. POSITIONED AND DRILLED -75 IAW SRM 51-10-04, TREATED AND PRIMED IAW SRM 51-10-03, INSTALLED IAW SRM 51-30-04.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 48,148 hrs · 35,848 cycles

IRR - DURING CLIMBOUT OF FL 290 A/C EXPERIENCED A LOUD BANG, SHUDDER LEFT ENGINE. SHUT DOWN INSTANTLY, COMPLETED ALL CHECKLISTS AND RETURNED TO KFLL. LANDING WEIGHT WAS 122,900LBS. REPLACED NR 1 ENGINE.

Part: SCHRADER VALVE — DAMAGED (NLG STRUT) · airframe 41,821 hrs · 31,861 cycles

AFTER GEAR RETRACTION A SEVERE VIBRATION CAME FROM NOSE GEAR AREA WITH NORMAL GEAR INDICATION/LIGHT IN COCKPIT. NOSE GEAR STRUT FLAT ON RETURN TO GATE. REMOVED AND REPLACED NLG STRUT SCHRADER VALVE AND COMPLETED SERVICING PER AMM 32-21-02. COMPLETED NLG T/S PER OPN 50006. CKS GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 41,240 hrs · 31,461 cycles

LEFT ENG OIL QTY DROPPED TO ZERO. THE ENG WAS SHUT DOWN WHEN THE OIL PRESS WAS AT 35 PSI. THE ENG WINDMILLED FOR 10 MINS AT ZERO OIL PRESS. REPLACED ENGINE NR 1 PER TRANSMITTAL 9T102.

Part: CYLINDER — CORRODED (RT MLG) · airframe 41,195 hrs · 31,436 cycles

RT MLG OUTER CYLINDER WAS FOUND WITH CORROSION. LOCALLY BLENDED TO REMOVE CORROSION PITTING AND REFINISHED.

Part: O-RING — CUT (APU OIL CAP) · airframe 40,934 hrs · 31,275 cycles

BOTH AFT SMOKE DETECTORS SOUNDED JUST AFTER TAKEOFF F/A REPORTED SMOKE AND FUME SMELL IN AFT CABIN. FOUND APU OIL CAP O-RING BAD. REPLACED OIL CAP PERFORMED. ALSO OPN 5089 DUCT BURNOUT. REPLACED COALESCER BAGS SYS NOW OK.

Part: A/C PACK — LEAKING (RIGHT) · airframe 38,885 hrs · 29,823 cycles

F/A REPORTED RT AFT LAV SMOKE DETECTOR SOUNDED ON T/O. SHUT DOWN RT PACK AND SMOKE DETECTOR QUIT. RESTARTED RT PACK AND SMOKE DETECTOR WENT OFF AGAIN. REPLACED NR 2 ENGINE FOR OIL CONTAMINATION IN A/C PACKS.

Part: CONNECTOR — LOOSE (SEAT ROW 17-18) · airframe 35,506 hrs · 27,355 cycles

ON PREFLIGHT EMERGENCY LIGHTS AT SEAT ROWS 18 TO 23 INOP. RESEATED CONNECTOR BETWEEN SEATS 17 AND 18. NOW OPERATES NORM.

Part: CLAMP — WORN (LT A/C PACK DUCT) · airframe 35,486 hrs · 27,339 cycles

FLOW CONTROL LIGHT CAME ON AT FL330 CABIN WOULD NOT HOLD PRESSURIZATION. CABIN ALT LIGHT CAME ON AS CABIN WENT ABOVE 10,000 FT. CABIN GOT AS HIGH AS 12,500 FT IN DESCENT. FLOW FROM AIR VENTS VERY LOW. FOUND LT PACK TURBINE OUTLET DUCT DISCONNECTED AT LOWER ATTACH POINT. REF: IPC 21-20-00-06B ITEM 300. REPLACED CLAMP AND SECURED DUCT. ALSO FOUND HOSE ITEM 45 WORN. REPLACED SAME. PRESSURIZED AIRCRAFT, ALL INDICATIONS NORM.

Part: SPLICE — BROKEN (EMERGENCY LIGHT) · airframe 34,685 hrs · 26,748 cycles

ON INSPECTION FOUND EMERGENCY PATH LIGHTS INOP FROM ROW 18-23. FOUND BAD SPLICE IN WIRES AT ROW 17 AND 18. REPAIRED WIRING AND LIGHTS NOW OPERATE NORMALLY.

Part: OVEN — MALFUNCTIONED (AFT GALLEY) · airframe 34,307 hrs · 26,492 cycles

AFT GALLEY - FUMES (ELECTRICAL) WERE DETECTED, NO SMOKE. ALL GALLEY CB'S WERE PULLED, ODOR DISAPPEARED. FOUND FWD OVENS IN AFT GALLEY AT FAULT. REPLACED SAME.

Part: BEARING — CORRODED (FLAP HINGE) · airframe 33,953 hrs · 26,261 cycles

DURING HMV IN ATL FOUND 3 FLAP HINGE BOLTS TO BE ROTATING AND WITH THE COTTER PINS SHEARED AT THE NUT. POSITIONS FOUND WERE THE RIGHT O/B FLAP I/B HINGE AT AFT ATTACH POINT, RIGHT O/B FLAP CENTER HINGE AT AFT ATTACH POINT, AND THE LEFT O/B FLAP CENTER HINGE AT THE AFT ATTACH POINT. TWO HINGE FITTINGS WERE REPLACED INCLUDING BEARINGS AND ONE HAD THE BEARING REPLACED ONLY.

Part: ATTACH ANGLE — CRACKED (STA 1474, RH) · airframe 30,737 hrs · 24,033 cycles

FUSELAGE / VERT STAB TO FUSELAGE ATTACH ANGLE / RH : CRACK REPAIR THE RH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FRAME STA. 1474. THE CRACK WAS .75" LONG IN THE HORIZONTAL FLANGE OF THE ANGLE AND WAS REMOVED WITH A TRIMOUT TO THE FLANGE. THE AREA WAS REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384165-14, REV A.

Part: ENGINE — UNSERVICEABLE (#1 ENGINE) · airframe 29,419 hrs · 23,068 cycles

ON CLIMB OUT VIBRATION FELT IN YOKE AND LOUD NOISE HEARD IN REAR OF A/C. WHEN LT THROTTLE RETARDED NOISE AND VIBRATION DECREASED. CA BOROSCOPED NO.1 ENG S/N 726047 FOUND 3 1ST STAGE FAN BLADES BENT FWD. REPLACED NO.1 ENG C-1FAN PER TRANS 9T133

Part: TRANSMITTER — FAILED (RT BRAKE) · airframe 26,102 hrs · 20,621 cycles

RIGHT BRAKE PRESSURE INDICATOR 200 PSI AT CRZ ALTITUDE. ALL OTHER PRESSURES AND QUANTITY NORMAL. ON LANDING BRAKES WORKED GOOD. IND REMAINED AT 200 PSI. REPLACED RT BRAKE PRESSURE TRANSMITTER. LEAK AND OPN CKS NORMAL.

Part: LAVATORY — LEAKING (AFT) · airframe 24,892 hrs · 19,721 cycles

AIR RETURN TO ATL DUE TO LAV FUMES IN CABIN. LEVEL AT FL290 FLT ATTENDANTS REPORT STRONG LAV FUMES THROUGHOUT CABIN. IN DESCENT FLT ATTENDANT REPORTED ODOR DISSIPATED SOMEWHAT BUT STILL STRONG IN REAR OF CABIN. FOUND LAV OVERFLOWED. CLEANED LAV AND SERVICED.

Part: UNKNOWN — SMOKE (COCKPIT)

SMALL AMOUNT OF SMOKE IN COCKPIT/CABIN DURING CLIMBOUT. CLEARED AFTER ENG ANTI-ICE OFF. RAN ENGINES WITH ANTI-ICE, UNABLE TO DUPLICATE.

Part: O RING — FAILED (RT HYD SYS)

ON APPROACH, RT HYD SYSTEM DROPPED TO 4 QTS. ACCOMPLISHED POM PROCEDURE. AFTER POM ACCOMPLISHED STABILIZED WITH 3 QUARTS. NORMAL PRESSURE. FOUND PLUG ON RUDDER SHUTOFF VALVE LEAKING. REPLACED O-RING.

Part: FRAME — CORRODED (BS 1307)

FS1307 FRAME WAS CORRODED FROM JUST INBD OF L29R TO BETWEEN L28L AND L29L. REPAIRED PER ERA 331842-14.

Part: SKIN — DENTED (BS 225)

A DENT WAS FOUND ON THE FUSELAGE SKIN JUST AFT OF THE L1 DOOR OPENING AT APPROX FS 225, BETWEEN LONGERONS 17L AND 18L. REPAIRED PER ERA 331827-14.

Part: SKIN — DENTED (BS 237)

A DENT WAS FOUND ON THE FUSELAGE SKIN JUST AFT OF THE L1 DOOR OPENING AT APPROX FS237, BETWEEN L18-20L. REPAIRED PER ERA 331828-14.

Part: FRAME — CRACKED (BS 1418)

MTC FOUND A CRACK AT L2L ON THE FS1418 FRAME WHICH IS A TYPICAL LOCATION. REPAIRED PER ERA 331832-14.

Part: CHIP DETECTOR — LEAKING (APU)

SMOKE IN CABIN IMMEDIATELY AFTER T/O. RTB FWD AND AFT SMOKE DETECTORS WENT OFF. FOUND APU CHIP DETECTOR LEAKING OIL. REPLACED PACKING, PERFORMED DUCT BURNOUT.

Part: HYD LINE — FAILED (RT PYLON)

SHORTLY AFTER LEVEL OFF, RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WAS LOST. ALL POM ABNORMAL PROCEDURES ACCOMPLISHED INCLUDING ALTERNATE GEAR EXTENSION. RETURNED TO ATL. REPLACED LINE IN RT ENG PYLON AREA CHAFED.

Part: PISTON — CRACKED (LT MLG)

FOUND ON E1 LTR CK, LT MLG PISTON CRACKED IN LOWER RADIUS REPAIR. REPLACED PISTON.

Part: PISTON — CRACKED (RT MLG)

FOUND ON E1 LTR CK, RT MLG CRACKED AT AFT LUG INBD END. REPLACED PISTON.

Part: RADAR — FAILED (NOSE)

WEATHER RADAR SYSTEM HAD AN ANTENNA FAULT, ENROUTE TO ATL. FLT DIVERTED TO MGM DUE TO WEATHER. REPLACED R/T UNIT AND ANTENNA.

Part: PAN — CRACKED (C-3 DOOR)

FOUND DURING D-1 LETTER CHECK, C3 DOOR FWD PAN CRACKED AT HOLD OPEN FITTING. REPAIRED PER SRM 52-05 FIG 26A.