N977DL

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 72,165 hrs · 53,394 cycles

DURING SVC, FOUND L1 DOOR SLIDE BOTTLE PRESSURE IN RED ''NO GO'' STATUS. R/R L1 DOOR SLIDE PER W/C 2561-4964. ACFT OK FOR SVC. (LP5055352)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,900 hrs · 53,155 cycles

FOUND LT OVERWING EXIT UPPER EMERGENCY LIGHT INOP. RELAMPED OVERWING EXIT EMERGENCY LIGHT IAW AMM 33-50. OPS CK NML. (LP3740096)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,517 hrs · 52,812 cycles

AFT CABIN EMERGENCY LIGHT ON THE CEILING FROM ROW 32 AND BACK WERE INOPERATIVE. FOUND THE CHARGER NOT CHARGING THE BATTERY PACK. REPLACED THE CHARGER IAW AMM 33-51. LIGHTS TESTED GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,989 hrs · 51,585 cycles

FLT CREW REPORTS SOFT SPOT IN GALLEY FLOOR BETWEEN G1 AND G3. FLOOR PANEL REF IPC 53-21-00-02J AND REPLACED NICKEL MAT. OK FOR SVC.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 68,568 hrs · 50,434 cycles

ON TAKEOFF ROLL CENTER FUEL PRESS LO LIGHT ILLUMINATED. CB J21 AND J23 WERE FOUND POPPED ON CLIMBOUT. T/S PER MM REF 28-20-07-101 THRU STEP 4 - WIRING CK AT TERMINAL STRIP S3-10 CKS OK. REF WDM 28-21-00 RANG LT AND RT BOOST PUMPS PHASES A B C TO GRD AND PHASE TO PHASE. ALL CKD GOOD. RANG CENTER BOOST PUMPS FROM TERMINAL BLOCK 53-10 TO PUMP. CKS GOOD. REPLACED TERMINAL BLOCK B7-8. ALL OPS CKD GOOD. REPLACED CENTER TANK AFT BOOST PUMP PER AMM 28-20-07 PB201. REPLACED LT WING FWD BOOST PUMP PER AMM 28-20-07. PERFORMED OPERATIONAL CKS AND COMPLIED WITH SFAR 88 - CDDCL REQUIREMENTS PER MD88 AMM 28-20 AND 28-00-00 PB201. ALL CBS RESET- LEAK CKS COMPLETED.

Part: WIRE — ARCED (COCKPIT) · airframe 68,364 hrs · 50,273 cycles

ON DESCENT INTO ATL TURNED ON W/S ANTI-FOG SWITCH. RECEIVED A QUICK FLASH IN COCKPIT, POPPING SOUND, EFIS FLICKERED MOMENTARILY. HAD ELECTRICAL BURNING SMELL FOR ABOUT 10 SECONDS, NO SMOKE, DISSIPATED QUICKLY. EVERYTHING NORMAL AFTER INCIDENT. PERFORMED 2120-2367. FOUND LEFT SLIDING WINDOW ANTI-FOG WIRES ARCED. REPL CB B1-339 AND SPLICED IN NEW SECTIONS OF WIRING ON H629E18, H643A18N, H645A18N PER SWPM CH 20-00. ALL CKS GOOD. NOTIFIED OCC. C/W NO GO ODI PROGRAM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 68,206 hrs · 50,151 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 31 AB. REPLACED A BROKEN CONNECTOR IAW SWPM 20. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (AFT CABIN) · airframe 67,990 hrs · 49,992 cycles

AFT EMERGENCY LIGHTS ILLUMINATED WITH POWER REMOVED FROM ACFT. PERFORMED EMERGENCY LIGHT CHECK IAW AMM 33-53. RECYCLED ARM SWITCH WITH POWER OFF, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1451) · airframe 67,813 hrs · 49,853 cycles

FRAME BS 1451 CRACKED AT LONGERON 1. . REPAIRED IAW ERA 554841-14 REV ORIG.

Part: BULKHEAD — DAMAGED · airframe 67,813 hrs · 49,853 cycles

LEFT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW PRI 554877-14 REV 0 AND COMPLIED WITH ERA 554877-14 REV ORIG.

Part: BULKHEAD — DAMAGED · airframe 67,813 hrs · 49,853 cycles

RIGHT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW ERA 554877-14 REV ORIG.

Part: FRAME — CRACKED (BS 1437) · airframe 67,813 hrs · 49,853 cycles

FRAME BS 1437, FWD SIDE HAS A 2 INCH LONG CRACK, LBL 7. REPAIRED IAW PRI 554290-14, REVISIONS 1, 2, AND 3 AND COMPLIED WITH ERA 554290-14 REVISION ORIGINAL.

Part: FRAME — CRACKED (BS 1437) · airframe 67,813 hrs · 49,853 cycles

FRAME BS 1437 FWD SIDE HAS A 2 INCH LONG CRACK THRU THREE FASTENER HOLES, RBL 7. REPAIRED IAW PRI 554290-14 REVISIONS 1, 2, AND 3 AND COMPLY WITH ERA 554290-14 REVISION ORIGINAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,813 hrs · 49,853 cycles

TAIL INTERIOR, CROWN SHEAR TIE HAS 2 CRACKS, BS 1437, RBL 8. REPAIR PER DWG 9953016.

Part: SKIN — CRACKED (BS 1437) · airframe 67,813 hrs · 49,853 cycles

TAIL SKIN HAS A CRACK BETWEEN TWO RIVETS AT BS 1437, LONGERON 4 & 5L. REPAIRED IAW PRI 554872-14 REV 0RIGINAL AND COMPLIED WITH ERA 554872-14 REV ORIGINAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 67,539 hrs · 49,689 cycles

FOUND EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRES AT SEAT 31ED IAW SWPM. OK FOR SERVICE.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 67,042 hrs · 49,320 cycles

HOLE IN INBD FIXED VANE, OTBD SECTION OF RT WING TE FLAP. REMOVED AND REPLACED THE VANE IAW AMM 27-51-03 P 201.

Part: TAB — DAMAGED (RUDDER) · airframe 67,040 hrs · 49,318 cycles

RUDDER CONTROL TAB HAS FLAME SPRAY MISSING IN CRITICAL AREAS. REMOVED & REPLACED RUDDER CONTROL TAB IAW WORK CARD 2720-4321. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 65,899 hrs · 48,473 cycles

MSP MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 17DE, 22DE, AND 33DE. BROKEN WIRES WERE FOUND AND REPAIRED UNDER 17R, 22E AND 33E. ALL LIGHTS CHECKED OK.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 65,795 hrs · 48,396 cycles

LEFT ELEVATOR ANTI-FLOAT TAB HAS LIGHTNING STRIKE. REPLACED TAB IAW AMDS CARD 2730-4382.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 64,600 hrs · 47,537 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 12D WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: DOUBLER — CORRODED · airframe 62,888 hrs · 46,355 cycles

THE AFT LAV CUTOUT DOUBLER WAS CORRODED AND REPAIRED, 532435-14.

Part: NONE — NONE · airframe 62,888 hrs · 46,355 cycles

INADECUATE RIVETS ON STA 435 AND BETWEEN LONGERON 20 TO 24RT. FASTENERS WERE REMOVED. AREA WAS TREATED AND PAINTED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21. REPAIR WAS ACCOMPLISHED IAW ER/A 532510-14, REV ORIGINAL AND ETI-88-15-057, REV 2.

Part: PANEL — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION WAS FOUND ON INTERNAL DOUBLER AT FWD LAVATORY SERVICE PANEL BTW STA Y= 282 TO 287 AND LONGS 20LH TO 22LH. REPAIR WAS PERFORMED WITH ER/A 473507-14 REV "A". (LP1836669)

Part: ACCESS PANEL — CRACKED · airframe 62,888 hrs · 46,355 cycles

CRACKED SETTLEMENT AREA, BOTH SIDES OF ACCESS PANEL 6301B AT DORSAL FIN L/E. DORSAL ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PARA 14 & 21, AND DWG 5912188 REV BD.

Part: DOOR FRAME — CRACKED · airframe 62,888 hrs · 46,355 cycles

CONTINUED CRACK ON AFTER TO PREVIOUS REPAIR AT DOOR JAMB AT STA Y=46, X=29 AT NOSE WHEEL WELL STRUCTURE. DOOR JAMB WAS REPAIRED IAW ETI-88-15-033, REV 4 AND ER/A 531399-14, REV ORIGINAL.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON CUSP ANGLE IN STA Y=646, Y=655 AND Y=674 ON X=-60 RT SIDE AT PAX CABIN STRUCTURE. REPAIR WAS PERFORMED WITH ER/A 532529-14, REV ORIG.

Part: SLAT TRACK — CRACKED · airframe 62,888 hrs · 46,355 cycles

CRACKED LOWER EDGE CUT OUT SLAT TRACK NR 7 LT WING. L/E OUTER WING SKIN WAS REPAIRED IAW ETI-88-15-063, REV 3 AND ER/A 532516-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1311C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LOWER DOOR JAMB, BETWEEN STA Y=638 TO Y=893 ON LONGERON 28 AT CTR CARGO COMPARTMENT. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A.

Part: FRAME — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

SEVERAL CORROSION POINTS ON FRAME AT STA Y=1250 BETWEEN LONGS 27L TO 27R AFT CARGO COMPT CORROSION WAS REMOVED; MEASURED AND FOUND OUT OF LIMITS IAW SRM 51-10-3 PAR 26 AND 53-01, FIG 1, BETWEEN L-28 TO L-28R. UT WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.063" AND REMAINING IS BETWEEN L-27-28 LT AND L-27- L-28 RT 0.056", THEREFORE WITHIN LIMITS. BUT MINIMUN REMAINING BETWEEN L-28L-28R IS 0.45", THEREFORE THIS SECTION IS OUT OF LIMITS IAW SRM 53-01, FIG 1. FRAME SECTION BETWEEN L-28L TO 28R WAS REPAIRED IAW SRM 53-03, FIG 2A.

Part: TRACK — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

SEVERAL CORROSION POINTS ON RT TIE TRACK FROM STA Y=1212 TO 1320 AFT CARGO COMPARTMENT THE TRACK WAS REPLACED IAW 51-30-1 AND DWG 5936660, REV BZ.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1335C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: TRACK — CORRODED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

SEVERAL CORROSION POINTS ON LT TIE TRACK FROM STA Y=1174 TO 1320 AFT CARGO COMPT. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 593666, REV BZ.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,888 hrs · 46,355 cycles

CRACKED RIBS AT VERTICAL STABILIZER L/E. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.

Part: WEB — CRACKED · airframe 62,888 hrs · 46,355 cycles

CRACKED LOWER DOOR JAMB WEB AT STA Y=1217 APPROXIMATELY BETWEEN PROJECTION LONGERONS 28R AND 27R AFT CARGO COMPT WEB WAS REMOVED. NEW WEB WAS DRILLED, TREAT AND PAINTED AND WAS INSTALLED IAW DWG 5936442, REV "A" SRM 51-10-3, PAR 21 AND 14; 51-10-4, 51-30-1, 51-30-2, 51- 30-5.

Part: STRUCTURE — WORN · airframe 62,888 hrs · 46,355 cycles

WEAR ON UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING. UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING WERE REPAIRED IAW ER/A 521199-14MA REV ORIGINAL AND SRM 57-03D.

Part: FLOOR SUPPORT — CRACKED · airframe 62,888 hrs · 46,355 cycles

CRACKED FLOOR SUPPORT AT STA Y=1136 BETWEEN LONGERONS 27L TO 26L AFT CARGO COMPT. FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2 AND ER/A 413029-14MA, REV "D".

Part: FLOOR PANEL — UNKNOWN · airframe 62,888 hrs · 46,355 cycles

INITIAL REPAIR AS REQUIRED PAX CABIN FLOOR PANELS FROM STA Y=120 TO 1338 BETWEEN X=- 44 TO X= 44. FLOOR PANELS NRS 160A, 160E, 160F, 148A, 148B, 148D, 148C, 200C, 160D, 160B, 200E, 826C, 826F, 927B, 927D, 617E, 389F, 769E, 160C, 200D, 826D, 886C, 120E, 617C, 465C, 769D, 769C, 313C, 1307B, 769B AND 769F WERE FABRICATED IAW 53-20-01-201. FROM AMM THE CHANNELS ON FLOOR PLANEL 826D AND 886C SIDE LT WERE REPLACED IAW DWG 9936639, REV A.

Part: RIB — CRACKED · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CRACKED RIBS AT VERTICAL STABILIZER L/E STA ZFS 23.500 AND STA ZFS 17.656. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.

Part: TAB — DAMAGED (RUDDER) · airframe 62,888 hrs · 46,355 cycles

DAMAGE PAINT COAT AND METALIZED ON BOTH SIDES OF RUDDER CONTROL TAB SKIN. RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: CUSP WEB — CORRODED (BS 395-484) · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 395-484, X 54 TO X 60. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 14, 38.

Part: SKIN — WORN (BS 1485-1510) · airframe 62,888 hrs · 46,355 cycles

WEAR ON INTERNAL FUSELAGE SKIN BETWEEN BS 1485 - 1510 AND LONGERONSS 21-23R. SKIN REPAIRED IAW SRM 53-01, FIG 1, FIG 2, 51-10-3 PAR 14 AND 21 AND 51-30-2.

Part: WINDOW FRAME — SCRATCHED (EMERGENCY EXIT) · airframe 62,888 hrs · 46,355 cycles

SCRATCHED WINDOW CUTOUT OF LT FWD EMERGENCY EXIT DOOR AROUND. SCRATCHES WERE BLENDED OUT IAW SRM 53-05, FIG 111.

Part: COVER — DAMAGED (RT ELEVATOR) · airframe 62,888 hrs · 46,355 cycles

DAMAGED DUST COVER ON BEARING OF ANTI-FLOAT TAB ROD AT RT ELEVATOR. DAMAGED PUSHROD OF ANTI-FLOAT TAB WAS REPLACED FOR A SERVICEABLE ONE IAW AMM 27-30-14.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

SEVERAL CORROSION POINTS ON LOWER DOOR JAMB GUSSETS AT BS 1155 TO 1212 AND LONGERON 28R. REPAIRED IAW SRM 51-30-2, SRM 53-14-3. SRM 51-10-3 PAR 14 AND 21, SRM 51-30-5.

Part: TORSION BAR — CORRODED (RT WING SPOILER) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

RUSTED TORSION BAR OF OTBD FLIGHT SPOILER RT WING. TORSION BAR OF OTBD FLIGHT SPOILER RT WING WAS REPLACED IAW AMM 27-61-06-201.

Part: FITTING — DAMAGED (NACELLE) · airframe 62,888 hrs · 46,355 cycles

ELONGATED HOLES UPPER FITTING STA YN=154 AND YN=214 AT LT APRON. DAMAGES ON UPPER FITTINGS STA YN=154 AND YN=214 WERE REWORKED AND MEASURED: YN=154 ID=0.5155", 4 EAS, Y=214, ID= 0.4985, 4 EAS AND BUSHINGS WERE FABRICATED AND INSTALLED IAW ER/A 228793-14 AND 266727-14.

Part: ANGLE — CORRODED (BS 1307 FRAME) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON CLIP FRAME AFT AND FWD FACE AT BS 1307 BETWEEN LONGERONS 28R - 28L. CORROSION WAS REMOVED BUT REWORKED AREA WAS OUT OF LIMITS. DAMAGE AREA WAS R & R WITH NEW REPAIR PARTS IAW SRM 53-03D, FIG 3, 51-10-3 PAR 14,21 AND 38, 51-30-2.

Part: ANGLE — CRACKED (BS 788) · airframe 62,888 hrs · 46,355 cycles

CRACKED ANGLE ON FRAME BS 788 BETWEEN LONGERONS 23 - 24L. FABRICATED A NEW ANGLE IAW DWG 5936628, REV "B" AND INSTALLED IAW SRM 51-30-2 AND 5.

Part: WEB — CRACKED (NLG WW) · airframe 62,888 hrs · 46,355 cycles

CRACKED REPAIR DOUBLER BELOW TO WEB 7 STA Y=37, X=-10 AND X=10 AT NOSE WHEEL WELL STRUCTURE. REPAIR DOUBLERS WAS REPLACED IAW SRM 51-30-2, SRM 53-01, FIG 2, SRM 51-10-2, NDT SPM 06-10-01.001, SRM 51-10-3 PAR 14 & 21.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT LT MAIN FUEL TANK ACCESS PLATE NR 1303 C. REWORKED IAW SRM 51-22-2A AND WAS TREATED IAW SRM 51-10-3, PAR. 21 AND BUSHING WERE FABRICATED IAW SRM 51-22-2A, PAR 6 AND WERE TREATED IAW SRM 51-10-3, PAR. 21 AND WERE INSTALLED IAW SRM 51-22-2A. ACCESS PLATE WAS TREATED IAW SRM 51-10-3 AND WAS PAINTED IAW PS 900-3-6, NR 36 AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0386.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1456C. ACCESS PLATE WAS REPLACED FOR EXCESSIVE DAMAGE AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0392.

Part: PAN — CRACKED (L1 DOOR) · airframe 62,888 hrs · 46,355 cycles

CRACK ON PAN ON FWD UPPER CORNER AT LT FWD ENTRY DOOR INTERNAL STRUCTURE (L1). DAMAGE PAN WAS REMOVED IAW SRM 51-30-2 AND 51-30-3. NEW PAN WAS DRILLING IAW SRM 51-10-4. HOLES WERE TREATED AND PAINTED IAW SRM 51-10-3. NEW PAN WAS INSTALLED IAW SRM 51-30-2 AND 51-30-3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATES NR 1466 C OUT OF LIMITS. ACCESS PLATE WAS REPLACED. DRIPLESS FUEL WAS REMOVED AND INSTALLED IAW AMM 28-40-02. ACCESS PLATE 1466 WAS INSTALLED IAW AMM 28-00-00.

Part: ANGLE — BROKEN (BS 218-237) · airframe 62,888 hrs · 46,355 cycles

BROKEN RT ANGLE BS 218 - 237 BETWEEN LONGERON 9-10R. REPAIRED IAW ETI-88-15-070, REV ORIGINAL AND ER/A 532525-14, REV ORIGINAL.

Part: CUSP WEB — CRACKED (BS 845) · airframe 62,888 hrs · 46,355 cycles

CRACKED LT CUSP WEB BS 845 BETWEEN X 44-54. THE CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-14, DWG 9910151, REV AL.

Part: CUSP WEB — CORRODED (BS 946-965) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION AND WEAR ON RT CUSP WEB BS 946 - 965 X 44 TO X 60. CORROSION AND WEAR ON CUSP WEB WAS REMOVED IAW SRM 51-10-3 P. 26, 14, 21 AND 38, 53-05, FIG 131A-21 51-30-2.

Part: CUSP WEB — CORRODED (BS 1054) · airframe 62,888 hrs · 46,355 cycles

CRACKED LT CUSP WEB BS 1054 BETWEEN X 54-60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: CUSP WEB — CORRODED (BS 905-910) · airframe 62,888 hrs · 46,355 cycles

CRACKED LT CUSP WEB BETWEEN X-60, BS 905-910. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: CUSP WEB — CORRODED (BS 150-160) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON WEB BS 150-160 X -44 TO -54. REPAIRED IAW ETI-88-15-060, REV 1, ER/A 532514-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 1028-1032) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT CUSP WEB BS 1028 - 1032 AND X -54 TO X- 60. CUSP WEB REPLACED IAW SRM 53-05, SRM 51-10-3, PAR 14 AND 21.

Part: LONGERON CLIP — BROKEN (BS 1174-1193) · airframe 62,888 hrs · 46,355 cycles

BROKEN LONGERON CLIPS BS 1174 - 1193 BETWEEN LONGERON 7 - 8L . REPAIRED IAW ETI 88-15-070, REV ORIG AND ER/A 532525-14, REV ORIG.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FITTING RIB, ON INNER SURFACE XOS 580 AT RT SLAT PANEL NR 5. NEW RIB ON STA XOS=580 LWR SKIN AND INTERNAL STRUCTURE WERE INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-8.

Part: CUSP WEB — CORRODED (BS 990-992) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT CUSP WEB X 54 TO X 60 BETWEEN BS 990 - 992. THE CUSP WEB WAS REPLACED, IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 846-858) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB FROM BS 846 - 858 BETWEEN X 54 AND X 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-1 AND 51-10-3.

Part: CUSP WEB — CORRODED (BS 1160-1163) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT CUSP WEB FROM BS 1160 - 1163 X -54 AND X -60. REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT LT MAIN FUEL TANK ACCESS PLATE NR 1367C OUT OF LIMITS. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0386.

Part: CUSP WEB — CRACKED (BS 1022-1026) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 1022 - 1026 FROM X 54 TO X 60. CUSP WEB REPLACED IAW SRM 53-05, FIG 131A-4.

Part: CUSP WEB — CRACKED (BS 883-886) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CRACKED LT CUSP WEB BETWEEN BS 883-886, X 44-54. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-16 AND 51-10-3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1470 C. ACCESS PLATE WAS REPLACED FOR NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: CUSP WEB — CORRODED (BS 1174-1187) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT CUSP WEB FROM BS 1174 - 1187 AND BETWEEN X -54 AND X -60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131, A-1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1464 C. OUT OF LIMITS IAW SRM 52-22-2A. ACCESS PLATE NR 1464C WAS REPLACED.

Part: CUSP WEB — CRACKED (BS 1230) · airframe 62,888 hrs · 46,355 cycles

CUSP WEB WAS FOUND CRACKED IN BS 1230 AND BETWEEN X -44 AND X -54. CUSP WEB REPAIRED IAW SRM 51-30-2, SRM 53-05, FIG 131 A -17 AND SRM 51-10-3 PAR 14, 21 & 38.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE 1409C. ACCESS DOOR WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 061-0392.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1410C. OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PLATE NR 1410C WAS REPLACED AND WILL BE INSTALLED UNDERCARD 2800-0390 JOB 001-0392.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1462C. OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PLATE 14626 WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0386.

Part: PAN — CRACKED (RT OVERWING EXIT) · airframe 62,888 hrs · 46,355 cycles

CRACKED DOOR PAN INNER STRUCTURE AT INTERSECTION WITH ZEE CHANNEL ON FWD RT OVERWING EMERGENCY EXIT. INNER SKIN, STOP FITTING AND CLIP WERE REMOVED IAW SRM 51-30-2, SRM 51-30-1 AND 51-30-5. CRACK WAS STOP DRILLED IAW SRM 51-01, PAR 21. HFEC INSPECTION WAS ACCOMPLISHED ON DOOR PANEL INNER AT INTERSECTION WITH ZEE CHANNEL. NO CRACK WERE FOUND AFTER STOP DRILLED IAW SRM 51-01, PAR 21B NDT SRM 06-10-01-001. CRACK WAS STOP HOLE .0625 DIAMETER LARGE TO REMOVE ANY FATIGUE DAMAGE MATERIAL IAW SRM 51-01 PAR 21 (2). DOUBLER WAS FABRICATE IAW SRM 52-05D, FIG 51. DOUBLER WAS PAINTED IAW SRM 51-10-3, PAR 14. NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND INNER SKIN STOP FITTING AND CLIP WERE INSTALLED IAW SRM 51-30-2, 51-30-1.

Part: INTERCOSTAL — CRACKED (BS 769-788) · airframe 62,888 hrs · 46,355 cycles

CRACKED INTERCOSTAL X 0 BETWEEN BS 769 - 788. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. CRACK WAS STOPPED IAW SRM 51-01, P21. DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2 DOUBLER AND INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3 P21 AND 14. INSTALLED IAW SRM 51-30-2.

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 63,309 hrs · 46,618 cycles

THE AFT LAV CUTOUT DOUBLER WAS CORRODED AND REPAIRED, IAW ER/A 532435-14.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 465 - 484 X 54 TO X 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-A AND 51-10-3, PAR 21, 14, 38.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,888 hrs · 46,355 cycles

CRACK ON LONGERON 16R BS 1437. LONGERON REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21, 53-14-4.

Part: LONGERON — CORRODED (BS 1287-1338) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1338. NEW LONGERON WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. THE LONGERON WAS REPLACED IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,888 hrs · 46,355 cycles

DAMAGED PAINT COAT AND METALIZED ON BOTH SIDES OF RUDDER SKIN. BOTH SIDES OF RUDDER SKIN WAS REPAIRED FLAME SPRAY AND PAINTED IAW PS 900-3-6. N 36.

Part: CUSP WEB — CORRODED (BS 846-974) · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB BETWEEN STA Y846-851, 964-966, 970-974 AT PASSENGER CABIN STRUCTURE. CORROSION WAS REMOVED, TREATED, PAINTED IAW SRM 51-10-3 P 14, 21, 26 (UT) IAW NDT SRM 04-00-07, PAR 5, FIG 3, SH 1 AND 2 WAS ACCOMPLISHED: ORIGINAL THICKNESS IS BETWEEN Y=964 TO 974 0.040" AND REMAINING IS 0.038" FOR Y=964-966 AND 970-974, THEREFORE IT`S WITHIN LIMITS IAW DAL ER/A 511165-14MA, REV B; BUT BETWEEN 846 TO 851 REMAINING THICKNESS IS 0.013", ORIGINAL IS 0.020"; THEREFORE IT`S OUT OF LIMITS AND WILL BE ATTENDED WITH CARD 342, ZONE 201, REF NRC 20000045279.

Part: FLOORBEAM — CORRODED (BS 160) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOORBEAM BS 160 AND X 8. FLOORBEAM REPLACED IAW SRM 51-30-5, SRM 51-30-1, SRM 51-10-4, SRM 51-10-3 PAR. 14, 21 Y 38.

Part: FRAME — CRACKED (BS 1380) · airframe 62,888 hrs · 46,355 cycles

CRACKED FRAME ANGLE BS 1380 LONGERON 14L. FRAME ANGLE WAS FABRICATED AND INTALLED IAW SRM 53-14-4, FIG 1 AND 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 723-728) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT CUSP WEB FROM BS 723-728 AND X 54 TO 60. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-10-3 P.14-21 AND 51-30-2.

Part: LONGERON SPLICE — WORN (BS 1401-1418) · airframe 62,888 hrs · 46,355 cycles

WEAR ON LONGERON SPLICE 8L BETWEEN BS 1401 - 1418. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3 PAF 14 AND 21 AND 53-02 AND SRM 53-02, FIG 18.

Part: SEAT TRACK — CORRODED (BS 484) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON SEAT TRACK 22, BS 484. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FRAME AFT FACE AT BS 1287 BETWEEN LONGERONS 29R TO 28L. FRAME ANGLE WAS REPLACED IAW SRM 53-03D, FIG 3, 51-30-2, 51-10-3 PAR 14,21 AND 38.

Part: CUSP WEB — CORRODED (BS 560-563) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB FROM BS 560 TO 563 X 54 AND X 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,888 hrs · 46,355 cycles

CRACK PAN OF RT AFT EMERGENCY EXIT DOOR AT ZEE CHANNEL AFT EDGE. INER SKIN CLIP AND STOP FITTING WERE REMOVED IAW SRM 51-30-2. CRACK WAS STOP DRILLED IAW SRM 51-01, PARAF 21, ANOTHER .0625 LARGER TO REMOVE ANY FATIGUED DAMAGE MATERIAL. HFEC WAS ACCOMPLISHED IAW NDT SPM PARA F06-10-01-001. NO CRACKD WERE FOUND AFTER STOP DRILLED. DOUBLER WAS FABRICATED IAW SRM 52-05, FIG 51, SHEET 2 AND SRM 51-10-2. DOUBLER WAS PAINTED IAW SRM 51-10-3 PARA F14. DOUBLER WAS INSTALLED IAW SRM 52-05 D FIG 51.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,888 hrs · 46,355 cycles

CRACKED ANGLE OF RT AFT EMERGENCY EXIT DOOR AT ZEE CHANNEL AFT EDGE. ANGLE REMOVED AND REPLACED IAW SRM 51-30-2, DWG 995773, REV G, SRM 51-10-3, AND SRM 51-30-2.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,888 hrs · 46,355 cycles

LIGHTNING STRIKE ON FWD EDGE OF WINDOW BELT BS 360 - 379 ON FUSELAGE SKIN. LIGHTNING STRIKE WAS BLENDED OUT IAW SRM 53-05, FIG 121.

Part: LONGERON — CRACKED (BS 1307) · airframe 62,888 hrs · 46,355 cycles

CRACK ON LONGERON 17L AND BS 1307. LONGERON SECTION REMOVED AND REPLACED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT CENTRAL FUEL TANK ACCESS PLATE NR 2301C. PLATE NR 2301C WAS REMOVED IAW SRM 51-10-3 COUNTERSINKS WERE MEASURED. THE ALLOWED MAXIMUM DIAMETER IS 0.660". THE PLATE IS 0.660" THE PLATE HAVE 3 HOLES DAMAGE ADJACENT 0.698, 0.698 AND 0.675 THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2. THEREFORE FUEL TANK ACCESS PLATE NR 2301C WAS REPLACED IN REF TO IPC 57-30-00 AND WILL BE INSTALLED WITH CARD 5730-0655, JOB 001-0414.

Part: FLOORBEAM — CORRODED (BS 522) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOORBEAM BS 522 BETWEEN LONGERONS 24L TO 24R. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREA TREATED AND PAINTED IAW SRM 51-10-3 PAR 21, 14, 38. FOUND WITHIN LIMITS IAW ER/A 511165-14MA, REV "B".

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,888 hrs · 46,355 cycles

LIGHTNING STRIKE ON AFT EDGE OF WINDOW BELT FRAME ON BS 256-408. L BLENDED IAW SRM 53-05, FIG 111.

Part: BEAM — CRACKED (PAX DOOR) · airframe 62,888 hrs · 46,355 cycles

CRACK ON BEAM ENDS NR 1 AT LT FWD ENTRY DOOR INTERNAL STRUCTURE. FASTENER ON INNER SKIN WERE REMOVED IAW SRM 51-30-1 AND 51-30-2. DOUBLER WERE REMOVED IAW SRM 51-30-1. CRACKED WERE STOP DRILLED IAW SRM 52-05 D NOTES 14. REPAIR DOUBLER WERE FABRICATED IAW SRM 52-05 D, FIG 97 AND 98. DOUBLER WERE PAINTED IAW SRM 51-10-3, PAR 14. NEW DOUBLER WERE INSTALLED IAW SRM 51-30-1 AND 51-30-2. INNER SKIN WAS INSTALLED IAW SRM 51-30-2.

Part: ARM — CORRODED (FLT SPOILER) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON CAM ARM, REACTION ARM, AND INBD AND OTBD BEARINGS SUPPORTS OF TORSION BARS AT INBD FLIGHT SPOILER LT WING. CAM ARM REATION ARM, AND INBD AND OTBD BEARINGS SUPPORTS OF TORSION BAR AT INBD FLIGHT SPOILER LT WING WERE REPLACED IAW JAMB AMM 20-10-01 AND 27-61-06 AND WILL BE INSTALLED WITH CARD 61, ZONE 10. (LP1817186)

Part: SEAT TRACK — CORRODED (BS 612) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT SEAT TRACK, 22, BS 612 APPROXIMATELY AT PAX CABIN. CORROSION WAS REMOVED IAW SRM 51-10-3, SEAT TRACK REPAIRED WITH PLUG IAW SRM 53-05, FIG 4.

Part: SEAT TRACK — CORRODED (BS 579) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT SEAT TRACK 54, BS 579. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, AMD 53-05IG 4B1.

Part: SEAT TRACK — CORRODED (BS 1257-1293) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

SEAT TRACK REPAIR PLUG X 22 BETWEEN BS 1257-1293 . REPLACED IAW SRM 53-05, FIG 4A, SHEET 1.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW SRM 51-30-2, DWG 9957828, REV AB, SRM 51-10-4 AND SRM. 51-10-3, PAR. 14, 21 & 38.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,888 hrs · 46,355 cycles

CRACK ON LONGERON 5L AT BS 1437. LONGERON AND SPLICE REMOVED AND REPLACED IAW SRM 53-02, FIG 18, SRM 51-10-4 AND SRM 51-30-5.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOORBEAM ANGLE BS 180, X-10 TO -54. FLOOR SUPPORT REPLACED IAW SRM 53-14-1, 51-30-2, 51-10-4, 51-10-3, PAR 14, 21, 26, 38.

Part: CUSP WEB — CORRODED (BS 619-623) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT CUSP WEB BS 619-623 AND BETWEEN X 54 AND X 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 395-484) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON CUSP WEB BETWEEN BS 395-484 X 54 TO X 60. THE CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 14, 21, 26, 38. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07. FOUND OUT OF LIMITS.

Part: BEAM — CRACKED (NR 3) · airframe 62,888 hrs · 46,355 cycles

CRACK ON REPAIR FOR BEAM NR 6 AT LT FWD ENTRY DOOR INTERNAL STRUCTURE. REPAIRED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT CENTRAL FUEL TANK ACCESS PLATE NR 2302C. COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2 ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 5730-0655.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT RT MAIN FUEL TANK ACCESS PLATE NR 1436C. COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW 1 AND WILL BE INSTALLED UNDER CARD 2200-0390OB, 001-0392.

Part: DOUBLER — WORN (RT MLG DOOR) · airframe 62,888 hrs · 46,355 cycles

WEAR ON UPPER AFT PRODUCTION DOUBLER OF STA Y=995 AT RT MLG DOOR. DOUBLER DAMAGE WAS REMOVED. NEW DOUBLER WAS INSTALLED IAW CMM 32-17-05, SRM 51-10-3, PARA 14 AND 21.

Part: FLOORBEAM — CORRODED (BS 150) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOORBEAM BS 150 AND X-54. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-2, SRM 53-14-1, FIG 11, SRM 51-10-2 ,SRM 51-10-3 PAR 14,21,38 AND SRM 51-10-4.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LT MLG ACTUATOR SUPPORT FITTING. THE LT MLG ACTUATOR SUPPORT WAS REPLACED IAW SOPM-20-10-7.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 62,888 hrs · 46,355 cycles

CRACK ON BEAM NR 4 CLOSE TO LOWER HINGE AT RT FWD SERVICE DOOR INTERNAL STRUCTURE. NEW BEAM WAS INSTALLED IAW SRM 51-30-2, 51-30-4, 51-30-5.

Part: FITTING — CORRODED (BS 465) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION FOUND ON FRAME FITTING X 58, BS 465. THE FRAME FITTING WAS REPLACED IAW SRM 51-30-5,51-30-1 AND DWG 4911383, REV L.

Part: SEAT TRACK — CORRODED (BS 270) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON RT SEAT TRACK X=54 BS 270. FOUND OUT LIMITS IAW SRM 53-05, FIG 4B-1. AREA DAMAGE WAS REMOVED IAW SRM 53-05, FIG 4A. PLUG WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. PLUG WAS INSTALLED IAW SRM 53-05, FIG 4A. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON MAIN GEAR SUPPORT FITTING. THE MLG ACTUATOR SUPPORT WAS REPLACED IAW SOPM 20-10-7.

Part: SUPPORT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON EVACUATION SLIDE LATCH SUPPORT BS 1142, X 54. SUPPORT REPLACED IAW 51-30-5, DWG 9930612, REV.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1307 C. CORROSION ON COUNTERSINKS WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDERCARD 2800-0120.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT RT MAIN FUEL TANK ACCESS PLATE NR 1454C. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT LT MAIN FUEL TANK ACCESS PLATE NR 1357 C. CORROSION ON COUNTERSINKS WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1361C AND 1363C. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WERE REPLCED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1355C. CORROSION ON COUNTERSINKS WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDERCARD 2800-0120.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINKS AT LT MAIN FUEL TANK ACCESS PLATE NR 1371 C. CORROSION ON COUNTERSINKS WAS REMOVED IAW IAW SRM 51-10-3 AND COUNTER SINKS HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 160-200 AND X -44 TO -54. THE FLOOR SUPPORT WAS REPLACED IAW SRM 57-14-1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT RT MAIN FUEL TANK ACCESS PLATE NR 1414C. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED UNDER CARD 2800-0340 JOB 001-0392.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1365 C. CORROSION ON COUNTERSINKS WAS REMOVED IAW SRM 51-10-3 AND COUNTERSINK HOLES WERE FOUND OUT OF LIMITS IAW SRM 51-22-2. ACCESS PLATE WAS REPLACED FOR A NEW 1 AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: SKIN — DAMAGED (BS 695.5) · airframe 62,888 hrs · 46,355 cycles

LIGHTING STRIKE ON FUSELAGE SKIN ON BS 695.5 BETWEEN LONGERON PROYECTION 21 AND 22 LT LIGHTNING STRIKE WAS ATTENDED IAW SRM 53-04-1, PAR 6.C. AND 6.D CONDITION 1 AND SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 168-200) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON THE FLOOR SUPPORT BS 168-200 AND X -8. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5, SRM 51-30-1, SRM 51-10-4 AND SRM 51-10-3 PAR 14 & 21.

Part: BRACKET — DAMAGED (ELEVATOR BEARING) · airframe 62,888 hrs · 46,355 cycles

ELONGATED HOLES ON LT/RT INBD BEARING BRACKETS AT ELEVATORS SECTOR BEARINGS. RT INBD BEARING BRACKET AT ELEVATORS SECTOR BEARINGS WERE REPLACED AND WILL BE INSTALLED UNDER CARD 2730-4231, JOB 001-0301.

Part: STIFFENER — CRACKED (BS 1338 BULKHEAD) · airframe 62,888 hrs · 46,355 cycles

CRACKED STIFFENER ON UPPER FWD PRESSURE DOME BETWEEN BS 1338 LONGERON 1. THE STIFFENER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 P.21 AND 14.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 62,888 hrs · 46,355 cycles

PUNCTURED FLAP NOSE SKIN OF LT OTBD FLAP ON NOSE ASSY OF STA XFLS=235. FLAP NOSE SKIN WAS REPAIRED IAW SRM 57-01, FIG 3.

Part: DOUBLER — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON INTERNAL DOUBLER, CUT OUT, AT ELEVATOR ACCUMULATOR ACCESS DOOR. DAMAGED CUTOUT WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. NEW CUT OUT WAS FABRICATED IAW DWG 5917686, REV AA. NEW CUTOUT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: CONDUIT — WORN (TAILCONE) · airframe 62,888 hrs · 46,355 cycles

MAINTENANCE FOUND WEAR ON CONDUIT OF TAIL CONE CONTROL CABLE BETWEEN STA Y=1485 CANT TO 1497 CANT AT 7 O'CLOCK POSITION. MAINTENANCE REPLACED THE CONDUIT IAW AMM 20-10-11-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,888 hrs · 46,355 cycles

CRACK ON LONGERON 3R BS 1437. LONGERON SECTION WAS REPLACED IAW SRM 53-02, FIG 18.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION WAS FOUND ON THE FLOORBEAM TEE LBL 14 - RBL 5 BS 200. THE FLOORBEAM WAS REPLACED IAW 53-14-1.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 62,888 hrs · 46,355 cycles

PUNCTURED ON LOWER SKIN AT OTBD FLAP, MID VANE LT WING MID VANE LOWER WAS REMOVED IAW 27-51-03-201 AMM. DUE TO SEVERAL DAMAGE AT MID VANE LT WAS REPLACED.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,888 hrs · 46,355 cycles

CRACK ON LONGERON 2R BS 1418. THE LONGERON WAS REPAIRED IAW SRM 53-14-4, FIG 2.

Part: INTERCOSTAL — CRACKED (BS 948-953) · airframe 62,888 hrs · 46,355 cycles

SEVERAL CRACKS WERE FOUND ON THE LOWER INTERCOSTAL BETWEEN BS 948- 953 AT THE LT MLG DOOR. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND DWG 5930583, REV DA.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON REPAIR DOUBLER AT LT CUSP WEB BETWEEN BS 598-617, X 54-60 AT PASSENGER CABIN STRUCTURE. PREVIOUS REPAIR DOUBLER WAS REPLACED ON LT CUSP WEB IAW SRM 53-05, FIG 131 A-2.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON FLOORBEAM FROM RBL 44 - 7, BS 200 AT PAX CABIN. REPLACED IAW SRM 53-14-1 AND 51-30-2.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,888 hrs · 46,355 cycles

CORROSION ON LOWER DOOR BEAM FROM BS 1155 - 1212 AND LONGERON 28R. SPACER WAS REMOVED IAW SRM 51-30-5. NEW SPACER WAS FABRICATED IAW SRM 53-05, FIG 123. NEW SPACER WAS TREATED, PAINTED IAW SRM 51-10-3 PAR 14 AND 21. NEW SPACER WAS INSTALLED IAW SRM 53-05, FIG 123. CIC WAS APPLIED IAW PS 900-2 NR 9.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 62,888 hrs · 46,355 cycles

CRACK ON UPPER SKIN AT OTBD FLAP/INBD VANE RT WING. DUE TO SEVERAL DAMAGE OTBD FLAP/INBD VANE RT WING WAS REPLACED WITH REPAIRED OTBD FLAP/INBD VANE.

Part: PAN — CRACKED (BS 731) · airframe 62,888 hrs · 46,355 cycles

CRACKED RING PAN AT BS 731 AND LONGERON 11R. RING PAN WAS REPAIRED IAW SRM. 53-05 AND 51-30-2.

Part: PAN — CRACKED (BS 946-1250) · airframe 62,888 hrs · 46,355 cycles

CRACKED RING PAN AT BS 946 - 1250 AND LONGERON 11L. RING PAN WAS REPAIRED IAW SRM 53-05 AND 51-30-2.

Part: PAN — CRACKED (BS 1022) · airframe 62,888 hrs · 46,355 cycles

CRACKED RING PAN AT BS 1022 AND LONGERON 14R. THE RING PAN WAS REPAIRED IAW SRM 53-05 AND 51-30-2.

Part: ANGLE — CRACKED (BS 1003) · airframe 62,888 hrs · 46,355 cycles

CRACKED ANGLE AT BS 1003 AND LONGERON 11R. ANGLE WAS REPAIRED IAW SRM. 53-05 AND 51-30-2.

Part: PAN — CRACKED (BS 218-237) · airframe 62,888 hrs · 46,355 cycles

CRACK ON RT AFT UPPER CORNER RING PAN SKIN PANEL BETWEEN STA Y= 218-237. DAMAGE AREA WAS REMOVED IAW SRM FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122.

Part: FRAME — CRACKED (BS 1510) · airframe 62,888 hrs · 46,355 cycles

CRACKED FRAME WEB BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-2, 51-10-4 51-10-3 PAR 14 AND 21 AND DWG 9911843-5, REV AC.

Part: DOOR — DAMAGED (CARGO DOOR) · airframe 60,126 hrs · 44,349 cycles

FWD, MID, AFT CARGO DOORS DAMAGED. REPAIRED IAW AA 5230-01159.

Part: SKIN — CRACKED (BS 1380 L13R) · airframe 59,487 hrs · 43,864 cycles

SKIN CRACKED AT FASTENER HOLE 1.7500" ABOVE LONGERON 13R BS 1380. ACCOMPLISHED DOUBLER REPAIR IAW ERA 518137-14, REV ORIG, SEC 1.

Part: FRAME — CRACKED (BS 1485) · airframe 59,476 hrs · 43,859 cycles

BELT FRAME WEB CRACKED AT CANTED BS 1485, NEAR 8 O`CLOCK POSITION, AT TAIL INTERIOR, TAIL CONE RELEASE HANDLE STRUCTURE ATTACHMENT. REPAIRED IAW ERA 518140-14, REV ORIG.

Part: SKIN — CRACKED (BS 1380) · airframe 59,476 hrs · 43,859 cycles

SKIN CRACKED AT LONGERON 14L, APPROX .5 INCHES ABOVE BS 1380. REPAIRED CRACK IAW ERA 518138-14, REV O, SEC I.

Part: STRUCTURE — CORRODED (BS 1212) · corrosion level 2 · airframe 59,476 hrs · 43,859 cycles

CORROSION FOUND AT THE AFT CARGO DOOR SILL L28R, BS 1212 FRAME AND FITTING. REPAIRED IAW SRM 53-01, 51-01.

Part: BUSHING — WORN (TAILCONE RELEASE) · airframe 59,476 hrs · 43,859 cycles

THE TAILCONE RELEASE CABLE T-PIN BUSHINGS WERE FOUND TO BE WORN IN THE RT AFT ACCESSORY COMPARTMENT. THE T-PIN BUSHINGS WERE REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED ON WC 5350-01077-0101.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 59,476 hrs · 43,859 cycles

THE TAIL CONE RELEASE CABLE T-PIN WAS FOUND TO BE WORN. THE T-PIN WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CABLE — CHAFED (TAILCONE RELEASE) · airframe 59,476 hrs · 43,859 cycles

THE TAILCONE RELEASE LOCK CABLE HAS CHAFED THRU THE PROTECTIVE SLEEVE. THE RELEASE CABLE WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SLIDER — WORN (TAILCONE RELEASE) · airframe 59,476 hrs · 43,859 cycles

THE TAILCONE RELEASE CABLE BLOCK/SLIDER AT UPPER LT SIDE IS WORN. REPLACED CABLE BLOCK/SLIDER AT UPPER LT SIDE IAW AMM 53-53.

Part: SLIDER — WORN (TAILCONE RELEASE) · airframe 59,476 hrs · 43,859 cycles

THE TAILCONE RELEASE CABLE BLOCK/SLIDER AT UPPER RT SIDE WAS FOUND TO BE WORN. REPLACED CABLE BLOCK/SLIDER AT UPPER RT SIDE IAW AMM 53-53.

Part: STRUCTURE — DAMAGED (TAILCONE) · airframe 58,071 hrs · 42,865 cycles

DURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY WAS DAMAGED AND JAMMING. THE MOVEABLE CEILING (CATWALK) WAS REPAIRED, ADJUSTED, AND RIGGED. IT NO LONGER BINDS DURING OPERATION AND MEETS PUBLISHED SPECIFICATIONS.

Part: AIRSTAIR — OUT OF SEQUENCE (AFT) · airframe 57,792 hrs · 42,657 cycles

THE REAR STAIRWAY HAD BEEN EXTENDED AT SOME POINT WHEN THE ACFT WAS PARKED. WHEN THE STAIRS WERE RETRACTED THE CATWALK REMAINED STUCK IN THE UP POSITION BLOCKING THE EMERGENCY PATH, AND WAS LATER JOLTED OUT OF THAT STUCK POSITION DURING TAXI FOR TAKEOFF. MX SEQUENCED THE STAIRS CORRECTLY AND THE PROBLEM DID NOT REPEAT.

Part: SPAR — CRACKED (WING) · airframe 57,569 hrs · 42,499 cycles

WING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.

Part: SPAR — DAMAGED (RT WING) · airframe 57,577 hrs · 42,503 cycles

DURING ACCOMPLISHMENT OF RT WING LOWER SPAR CAP INSPECTION FOUND CRACK IN LOWER SPAR CAP EMANATING FROM INBD LOWER FLAP FITTING HOLE AT XRS=164.00. REF WC NR 5710-01110-0502. STOP DRILLED BOTH ENDS OF CRACK IAW DWG J060271. PERFORMED HFEC INSPECTION AT BOTH ENDS OF STOP DRILLED IAW DWG J060271. REPAIRED CRACK IAW AMDS WORK CARD 5710-01110-0601 AND NR CARD 013.

Part: LANYARD — MISINSTALLED (DOOR SLIDE) · airframe 56,245 hrs · 41,568 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE DOOR SLIDE LANYARDS TO BE INSTALLED INCORRECTLY. MAINTENANCE REINSTALLED THE LANYARDS AND RETURNED THE AIRCRAFT TO SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,245 hrs · 41,568 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING AT 10D TO BE INOPERATIVE. MAINTENANCE REPLACED THE SEAT HARNESS AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 55,808 hrs · 41,240 cycles

DURING PSV CRACK WAS FOUND IN FUSELAGE SKIN AT STA 1437 BETWEEN LONGERONS 2R AND 3R, ADDITIONAL CRACKS WERE ALSO FOUND AT SURROUNDING FASTENER HOLES. REPAIRED PER ERA 500857-14 REV A.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 55,808 hrs · 41,240 cycles

HORIZONTAL STAB UPPER CENTER SKIN PANEL IS DAMAGED. REPAIRED IAW AA 5510-01086.

Part: BEARING — DAMAGED (HORIZONTAL STAB) · airframe 55,808 hrs · 41,240 cycles

HORIZONTAL STAB HINGE RIB PIVOT BEARING LUG DAMAGED. REPAIRED IAW AA 5500-01011.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 55,060 hrs · 40,683 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 34D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SOCKET — SPARKS (CABIN LIGHTS) · airframe 54,550 hrs · 40,309 cycles

STRONG ELECTRICAL SMELL DURING THE APU START UP AND F/A STATED THE ODOR WAS STRONGEST OVER THE WING. CREW STATED ALL COCKPIT INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENTS. PAX STATED THE OVERHEAD FLUORESCENT LIGHT AT ROW 18 WAS SPARKING AND FLASHING. MX FOUND BULB HOLDER SPARKING ABOVE 18 ABC. MAINTENANCE INSTALLED LIGHT SOCKETS AT ROW 17/18 PER IAW SWPM 20-11-03. OPERATION OF LIGHTS NOW CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,697 hrs · 39,002 cycles

DURING THROUGH, FLIGHT MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 12D INOPERATIVE AND DAMAGED. MAINTENANCE REPLACED LIGHT ASSEMBLY PER MM 33-53-01. OPERATION CHECK OF LIGHT NOW CHECKS GOOD. (2010-D1370) (DLM88103198)

Part: OIL SYSTEM — LEAKING (APU) · airframe 52,050 hrs · 38,559 cycles

ON CLIMB OUT, F/A REPORTED SMOKE IN THE CABIN WITH AFT LAVATORY SMOKE DETECTORS SOUNDING. MX ACCOMPLISHED OPS, 5088 SMOKE IN CABIN TROUBLESHOOTING. FOUND APU LEAKING OIL, CORRECTED OIL LEAK AND ACCOMPLISHED SEVERAL DUCT BURN OUTS IAW OPS 5089. REPLACED H2O SEPARATOR BAGS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,826 hrs · 37,690 cycles

EMERGENCY LIGHT INOP AT SEAT SHROUD 1CD AND EXIT SIGNS ABOVE AFT OVERWING EXITS. RELAMPED EXIT SIGNS AND REPLACED LIGHT ASSY AT SEAT 1CD. ALL CHECKS GOOD.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 50,736 hrs · 37,635 cycles

ON L/O FOUND SEAT ROWS 23DE AND 26 DE INOP EMERGENCY LIGHTS. FOUND SEAT WIRE HARNESSES BROKEN AT BOTH 23ED AND 26ED. R & R WIRE HARNESS AT BOTH, CKS GOOD.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 48,483 hrs · 36,202 cycles

THE LT WING INBD FLAP INBD GUIDE VANE EXTERNAL LOWER SKIN WAS FOUND WITH A 10 INCH MAXIMUM DIAMETER DELAMINATED AREA. A PUNCTURE WAS ALSO FOUND NEARBY. DAMAGE WAS BETWEEN XIVIF 35.557 AND 6.2364. THE DAMAGE WAS REMOVED AND AN EXTERNAL REPAIR DOUBLER WAS HOT BONDED ONTO THE VANE SKIN PER THE SRM.

Part: SKIN — CRACKED (STA 172-193) · airframe 48,483 hrs · 36,202 cycles

DURING HMV, THREE CRACKS WAS FOUND BTW STA Y=172 TO 193 LONGERON 22 LT. CRACKS WERE REPAIRED IAW EA 09-069085-12AD REV D.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 48,483 hrs · 36,202 cycles

DURING HMV CORROSION WAS FOUND ON LOWER DOOR JAMB BTW STA Y=636 TO 693. LOWER DOOR BEAM WAS REPAIRED IAW SRM 53-05 FIG 123.

Part: GUIDE — WORN (TAILCONE CABLE) · airframe 48,483 hrs · 36,202 cycles

DURING HMV WEAR WAS FOUND ON CABLE GUIDE TUBE OF TAIL CONE RELEASE SYSTEM. CABLE GUIDE TUBE WAS REPLACE IAW AMM 20-12-01-201.

Part: DOOR FRAME — DAMAGED (R1 DOOR) · airframe 48,483 hrs · 36,202 cycles

DURING HMV A PUNCTURE WAS FOUND ON LOWER DOOR JAMB OF R1 AT STA Y=171 AND TOOLING MARKS. LOWER DOOR JAMB WAS REPAIRED IAW SRM 53-05 FIG 55.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 48,483 hrs · 36,202 cycles

DURING HMV CORROSION WAS FOUND ON HORIZONTAL STAB ATTACH PLATES ON BOTH SIDES. PLATES WAS REPAIRED IAW SRM 55-02 FIG 28 PARAGRAPH 24.

Part: PRESSURE BLKHD — CORRODED (FUSELAGE) · airframe 48,483 hrs · 36,202 cycles

DURING HMV CORROSION WAS FOUND ON TEE PRESSURE BULKHEAD STA Y=1339 BTW PROJECTION LONGERON 29 LT AND 29 RT. THE TEE AT PRESSURE BULKHEAD WAS REPAIRED IAW EO 09-086680-12 REV E.

Part: MECHANISM — CORRODED (TAILCONE) · airframe 48,483 hrs · 36,202 cycles

DURING HMV RUSTED HARDWARE WAS FOUND ON TAIL RELEASE MECHANISM. REPLACE HARDWARE IAW AMM 20-30-01-201.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 48,483 hrs · 36,202 cycles

VERTICAL STABILIZER LEADING EDGE SKIN AT ZFS=136.803 UPPER PANEL RIGHT SIDE AFT CORNER ATTACH TANG WAS FOUND CRACKED APPROXIMATELY 0.281 INCH. THE CRACK WAS TRIMMED OUT APPROXIMATELY 1 INCH BY 1 INCH AND REPAIRED WITH AN EXTERNAL DOUBLER.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 48,483 hrs · 36,202 cycles

RUST ON HORIZ STAB ATTACH PLATES BOTH SIDES. RUST REPAIRED IAW SRM'S 51-10-3D AND 55-02.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 48,483 hrs · 36,202 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB BTW STA Y=636 TO Y=693. DOORJAMB REPAIRED IAW SRM 53-05 FIG 123.

Part: SKIN — DAMAGED (RUDDER) · airframe 48,483 hrs · 36,202 cycles

DAMAGED METALIZED COATING ON RUDDER CONTROL TAB ROD FAIRING. REPAIRED FAIRING IAW SRM 51-70-1AD.

Part: PRESSURE BLKHD — CORRODED (FUSELAGE) · airframe 48,483 hrs · 36,202 cycles

EXFOLIATION CORROSION ON "T"CAP P-DOME STA Y=1339 BETWEEN LONG 29 LT AND RT. REPAIR ACCOMPLISHED IAW EA 09-086680-12 REV E ME 06 OPN 0603.

Part: SKIN — ERODED (LT TE FLAP) · airframe 48,483 hrs · 36,202 cycles

EROSION ON LOWER SKIN OF LT WING INBD FLAP INBD VANE. THIS NRC WAS ACOOMPLISHED IAW OPN 1031 CARD 1251-1254.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 48,483 hrs · 36,202 cycles

WEAR ON CABLE GUIDE TUBE OF TAILCONE RELEASE SYSTEM STA Y=1510. CABLE REPLACED IAW AMM 20-12-01-201.

Part: ROD END — CORRODED (TAILCONE RELEASE) · airframe 48,483 hrs · 36,202 cycles

RUSTED CABLE ROD ENDS ON CABLE RELEASE MECHANISM. CABLE REPLACED IAW AMM 53-53-00-501 AND OPS CHECKED ON OPN 8908AD CARD 1141.

Part: TAB — DEBONDED (RT ELEVATOR) · airframe 48,483 hrs · 36,202 cycles

DISBONDED DOUBLER REPAIR ON RT ELEVATOR GEARED TAB. THIS N/R WAS ACCOMPLISHED IAW OPN 1031 CARD 1317-1325 AND SRM 55-04D PAR 3A.

Part: SKIN — DAMAGED (RUDDER) · airframe 48,483 hrs · 36,202 cycles

DAMAGED METALIZED COAT OF RUDDER. DAMAGED METALLIZED COAT OF RUDDER REPAIRED IAW SRM 51-70-1AD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 48,483 hrs · 36,202 cycles

CRACK ON UPPER SKIN DOUBLER AT VERTICAL STABILIZER. REPAIR WAS ACCOMPLISHED IAW ERA 473511-14 REV ORIG.

Part: DOOR FRAME — PUNCTURED (R1 DOOR) · airframe 48,483 hrs · 36,202 cycles

PUNCTURE ON LOWER DOORJAMB OF R1 STA Y=171 AND TOOLING MARK ON LOWER DOORJAMB OF R1 FROM Y=172-200. PUNCTURES REPAIRED IAW SRM'S 53-01 FIG 1 AND 53-05 FIG 5S.

Part: MECHANISM — CORRODED (TAILCONE RELEASE) · airframe 48,483 hrs · 36,202 cycles

RUSTED HARDWARE OF TAILCONE RELEASE MECHANISM STA Y=1510. REPLACED HARDWARE IAW AMM 20-30-01-201.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,483 hrs · 36,202 cycles

TRANSFERED FROM OMI, RT HORIZ STAB UPPER SKIN INBD PANEL CRACKED. CRACKED SKIN WAS REMOVED AND REPLACED IAW ERA 461288-14D REV B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,483 hrs · 36,202 cycles

THREE CRACKS AT STA Y=172 OF .125", STA Y=191 OF .0625, AND STA Y=193 OF .0625 INCH AT LONGERON 22L. DOUBLER REPAIRED IAW EA 09-069085-12AD REV D ME02 OPN 0203.

Part: CSD — MAKING METAL (NR 1 ENG) · airframe 47,660 hrs · 35,648 cycles

ON CLIMB-OUT MULTIPLE GEN RELAY TRANSFERS FOLLOWED BY LEFT CSD OIL PRESSURE LOW MESSAGE QRH FOLLOWED LEFT CSD WOULD NOT DISCONNECT. RTN TO ATL. FOUND CSD FULL OF METAL, REMOVED AND REPLACED TRANSMISSION AND GENERATOR WET SPLINE SERVICED NEEDS LINE TO OIL COOL HOOK U AFTER COOLER REPLACEMENT SEE ITEM 003, ALSO NEED SERVICED. CONNECTED OIL COOLER LINES SERVICED CSD. INSTALLED PER M/M 24-10-01, GENERATOR INSTALLED PER MM 24-20-01 PG 401. OPS AND CKS OK.

Part: ACTUATOR — BROKEN (TRIM MOTOR) · airframe 47,520 hrs · 35,553 cycles

HOUSING FOUND CRACKED AND BROKEN PIECE HANGING ON WIRES. ALT TRIM INOP. REMOVED AND REPLACED ALT TRIM MOTOR ACTUATOR PER M/M CKS OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 46,338 hrs · 34,717 cycles

FOUND SEAT 26CD EMERGENCY LIGHT INOP. SECURED PIN INTO CONNECTOR OF LIGHT ASSY, OPS OK.

Part: STRUT — UNDERSERVICED (NLG) · airframe 45,875 hrs · 34,426 cycles

NOSE GEAR UNSAFE LIGHT ON GEAR RETRACTION. NOISE INDICATED DOOR DID NOT SEQUENCE FULLY CLOSED. AUTOSPOILER INOP MESSAGE ALSO ILLUMINATED BUT EXTINGUISHED AFTER LANDING. QRH PROCEDURES COMPLETED TROUBLESHOT NOSE GEAR STRUT C/W OPN5006. FOUND NOSE STRUT UNDER SVCD. C/W OPN4703 NOSE STRUT SVC. MCC SET FOR RECHECK. CYCLED GEAR NUMEROUS TIMES TEST GOOD.

Part: HYDRAULIC SYSTEM — LOW PRESSURE · airframe 45,442 hrs · 34,156 cycles

AFTER EXTENDING SLATS BOTH LT AND RT HYD PRESS DROPPED TO ZERO. AFTER RESETTING C/B H17 PRESS RETURNED TO NML. FOUND AIR IN BOTH LT AND RT SYS BED AIR. SERVICED TO FULL. FOUND A 4 ACCUM LOW LT T/R LEAKING. NO BYPASS PINS POPPED. SERV LT/RT BRAKE ACCUM AND RT THRUST REV ACCUM TO PLACARD. RAN ENG PRESS CKS GOOD. ECLECTIC PUMPS CKS GOOD. PRESS CK GOOD. CHECK SYS AGAIN FOR AIR. NO SYS HYD LEAKS NOTED. PRECAUTION CHANGED BOTH ENG HYD PUMPS. ALSO CHANGED LT THRUST REV ACCUM LEAKING. REPLACED LT THRUST REV ACCUM. ALSO, REPLACED BOTH CASE DRAIN FILTERS AND NR 1 GARLOCK SEAL.

Part: WIRE — BURNED (WINDSHEILD) · airframe 44,188 hrs · 33,328 cycles

WIRE CABLE ON CAPT SIDE BLEW, OCCURED IMMEDIATELY AFTER TURNING WINDSHEILD ANTI FOG ON. REMOVED DAMAGED ANTI FOG WIRING TO CAPT CLEARVIEW SLIDING WINDOW AND CAPPED OFF ENDS AND SECURED WIRES. PULLED AND COLLARED CBS FOR WINDOW ANT FOG SYS X-26 Z-26 Z-25 VERIFIED WINDSHEILD ANTI ICE SYS. OPERATIONAL FWD ANTI FOG SYS TO MCO AND PLACARDED PER MEL 30-00-20B. REPLACED WIRE SPLICES CKS NML MCO/PLAC REMOVED.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,756 hrs · 33,037 cycles

THE RT HORIZONTAL STABILIZER UPPER INBD SKIN PANEL FOUND CRACKED - 1.25 IN LONG. THE CRACK WAS CUT OUT OF THE SKIN AND INSPECTED. THE PANEL WILL BE REPLACED AT WITHIN 2000 FLIGHT HOURS.

Part: BATTERY — OVERHEATED (FWD E/E) · airframe 35,110 hrs · 27,113 cycles

FOUND BATTERIES OVERHEATING AT GATE WITH WHITE SMOKE. REPLACED BATTERIES AND CHARGER.

Part: SWITCH — SHORTED (NR 2 ENGINE) · airframe 34,542 hrs · 26,707 cycles

AIR TURNBACK, RIGHT ENGINE OIL FILTER CLOGGED MESSAGE ON EOAP. T/S--SHOOK DOWN WIRING AT ENGINE -NTF. CHECKED AND REPLACED MAIN ENGINE OIL FILTER AND DETECTOR--NTF. REPLACED BAD OIL DIFF PRESSURE SWITCH. LEAK AND OPERATIONAL CHECKS OK.

Part: A/C PACK — ODOR (AFT) · airframe 33,286 hrs · 25,800 cycles

ON TAKEOFF FROM SDF FLIGHT ATTENDANTS IN AFT CABIN SAID THEY SMELLED FUMES. NO FUMES IN FWD CABIN OR FLIGHT DECK ALL INDICATIONS NORM. LINE CHECK PILOT IN AFT CABIN SAID FUMES SMELLED LIKE RESIDUE BURNING OFF OF PNEUMATIC DUCTS. ODOR DISAPPATED QUICKLY WHEN CLIMB POWER SELECTED. REMAINDER OF FLIGHT UNEVENTFUL. CORR. PERFORMED OPN 5088 AND 5099 DUCT BURNOUT

Part: LIGHT — BROKEN (CABIN) · airframe 33,000 hrs · 25,576 cycles

ON INSPECTION FOUND EMERGENCY LIGHT IN FWD AREA OF AFT AIRSTAIR INOPERATIVE. FOUND WIRING TO LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY AND QUICK DISCONNECT SPLICES. OPERATION OF LIGHT NORMAL.

Part: LIGHT — INOPERATIVE (CABIN ROW 19D) · airframe 32,196 hrs · 25,056 cycles

EMERGENCY TRACK LIGHT AT 19D INOPERATIVE. REPLACED SEAT MOUNTED LIGHT ASSY

Part: CYLINDER — FAULTY (NLG) · airframe 31,152 hrs · 24,293 cycles

NOSE GEAR WOULD NOT RETRACT ON T/O NOR DURING CHECKLIST. REPLACED NOSE GEAR PISTON AND INNER CYLINDER.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 31,107 hrs · 24,255 cycles

IN FLIGHT RIGHT HYD PRESS LOW LIGHT ILLUM AND RT PRESS INDICATED ZERO. QUANTITY INDICATED 19 QTS. FOLLOWED POM PROCEDURES AND RESTORED HYD PRESS. NORMAL INDICATIONS FOR THE REST OF FLIGHT. REPLACED RT ENGINE HYD PUMP PER M/M. LEAK CHECK AND TEST NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,024 hrs · 23,406 cycles

FWD ENGINE FLASHLIGHT INOP. REPLACED LIGHT ASSY, OPS NORMAL.

Part: TRIM MOTOR — FAULTY (AUTOPILOT SYS) · airframe 29,336 hrs · 22,918 cycles

A/P C/BS POPPED. A/P TRIM LIGHT ILLUM. A/P TRIM INOP. RESET C/BS. D11 POPPED 2ND TIME. PRIMARY TRIM FUNCTIONED ENTIRE TIME. REPLACED ALTERNATE STABILIZER TRIM MOTOR PER M/M. PERFORM RTS TEST ON BOTH DFGCS. BOTH PASS/GO. STAB TRIM NOW OPS NORMAL.

Part: ROD — CORRODED (RUDDER) · airframe 28,221 hrs · 22,098 cycles

DURING T/S OF AUTOPILOT INOP. FOUND RUDDER INPUT CRANK LOOSE, .065 UP AND DOWN MOTION AND CORROSION COMING OUT ENDS OF CRANK. REPLACING RUDDER CRANK, RUDDER INPUT TORQUE TUBE, RUDDER INPUT SECTOR BELLCRANK, RUDDER TRIM ACTUATOR, YAW DAMP ACTUATOR, RUDDER POWERPACK.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 27,943 hrs · 21,910 cycles

LEFT ENGINE FIRE INDICATION ON CLIMBOUT. RETARDED THROTTLE LIGHT WENT OUT. FOUND LEFT ENGINE ANTI ICE DUCT BLOWN, DUCT FROM ENG BLEED TO ANT ICE VALVE. REPLACED DUCT. RAN ENGINE. FIRE DETECTION AND LEAK CHECK GOOD.

Part: LIGHT — BURNED OUT (COCKPIT) · airframe 27,500 hrs · 21,598 cycles

AFTER MLG EXTENDED LT MLG HAD NO LIGHTS ILLUM. CKD DOWN AND LOCKED VISUALLY THRU PERISCOPE. LANDED NORMALLY. FOUND LEFT MLG IND LAMPS BURNED OUT. RELAMPED LIGHTS, OP NML.

Part: FITTING — DENTED (TRUNNION) · airframe 26,346 hrs · 20,730 cycles

AN INTEGRAL STIFFENER ON THE LT NOSE LANDING GEAR TRUNNION SUPPORT FITTING WAS FOUND DENTED JUST AFT OF THE MAIN LUG. THE DENTED STIFFENER WAS REFORMED, HFEC INSPECTED TO ENSURE NO CRACKING, AND REINFORCED WITH TWO ALUMINUM REPAIR ANGLES PER ER/A 377424-14, REV A.

Part: AHRS — MALFUNCTIONED (E/E COMPT)

AT APPROX 100 KTS ON T/O ROLL, GOT HORIZON, NO AUTO LAND AND MONITOR LIGHTS ON FMA. F/O'S ATTITUDE DISPLAY INDICATED FAILURE (NO HORIZON). ABORT SPEED 120 KTS, MAX BRAKE TEMP 250 DEG CELSIUS. REMOVED AND REPLACED NR 2 AHRS UNIT PER M/M 34-21-10, ALL CKS OK.

Part: CLAMP — BROKEN (LT PACK)

CLIMBING THROUGH FL 310, CABIN ALTITUDE ROSE RAPIDLY, FLOW LT ON PRESS PNL ILLUM. DURING SUBSEQUENT EMERGENCY DESCENT CABIN PRESS COULD NOT BE CONTROLLED. OUTFLOW VALVE COULD NOT BE MANUALLY CLOSED, AS IT WOULD BIND. WHEEL COULD NOT BE MOVED TO A MORE CLOSED POSITION BUT COULD BE MOVED TO FULL OPEN. FOUND INPUT DUCT TO LEFT A/C PACK WATER SEPARATOR DISCONNECTED. FOUND CLAMP ON SAME TO BE DEFECTIVE. REPLACED CLAMP AND CONNECTED DUCT, PRESSURIZED A/C TO 6.0 PSI AND PRESSURIZATION SYSTEM CKS OK.

Part: INTERCOSTAL — CRACKED (L1 DOOR)

FOUND ON HMV ITEM: L-1 DOOR INTERCOSTAL CRACKED AT SKIN ATTCH POINT LOC JUST ABOVE DOOR HOLD OPEN HOOK MECHANISM. REPLACED INTERCOSTAL.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLASHLIGHT IN AFT CABIN INOP. REPLACED BATTERY PACK AND BULB.

Part: COALESCER BAGS — DIRTY (CABIN)

ON T/O AND CLIMBOUT, A HOT SMELL WAS NOTICED IN THE COCKPIT. SMELL WENT AWAY WITH POWER REDUCTION TO CRUISE. RAN BOTH ENGINES TO T/O POWER PER PFHB FOR PNEUMATIC BURNOUT. CKD AUG VALVES PER PFHB, NO SMELL NOTED. CHANGED COALESCER BAGS.

Part: PLUG — LEAKING (RT WHEEL WELL)

ON APPROACH, THE RT HYD SYSTEM QTY WENT TO ZERO. ALTERNATE GEAR EXTENSION WAS USED FOR LANDING. A/C WAS TOWED OFF RUNWAY. CONTRACT MTC FOUND THE A-PLUG IPC REF 29-10-00 FIG 01S ITEM 325 HAD BACK OFF. TIGHTENED PLUG AND SAFTIED, SERVICED RESERVIOR AND LEAK CHECKED THE PLUG. NO DAMAGE TO WHEEL WELL DOORS CAUSED BY LANDING.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

DURING CRUISE, CAPTAINS WINDSHIELD STARTED TO ARC, THEN CRACKED. A/C DIVERTED TO ATL. REPLACED WINDSHIELD.

Part: PACK — ODOR (CABIN)

ON CLIMBOUT, FLT ATTENDANT REPORTED BURNING ODOR COMING FROM AIR CONDITIONING SYSTEM, NO SMOKE WAS VISIBLE. RT PACK WAS SHUTDOWN, ODOR DISSIPATED. INSPECTED PACK, ALL NORMAL. PERFORMED DUCT BURNOUT, RETURNED TO SERVICE.

Part: HYD PUMP — FAILED (NR 1/2 ENGINE)

AT TOP OF DESCENT, WITH POWER BACK LT HYD PRESS LOW MSG ILL. LT HYD PRESS READ 0, LT HDY QTY WENT FROM 5 TO 17-C/W HYD PRESS LOW ABNORMAL. AS SOON AS AUX/TRANSFER PUMPS WERE TURNED ON. RT HYD PRESS WENT TO 0, RT HYD QTY READ 14, TURNED OFF AUX/TRANSFER PUMPS. CA-FOUND LEFT REVERSER LINE LEAKING. REPLACED SAME AND REPLACED NR 1 AND NR 2 ENG DRIVEN HYD PUMPS AND REPLACED ASSOCIATED FILTERS.

Part: LINK — FAILED (NLG DOOR)

AFTER TAKEOFF, HEARD LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA AFTER GEAR RETRACTION. RETURNED TPA, FOUND RT NOSE GEAR DOOR OPEN. REPLACED RIGHT DOOR LINK DUE TO NOT LOCKING.