N979DL

Part: ACM — SEIZED (LEFT) · airframe 74,794 hrs · 55,306 cycles

ATB DUE TO UNABLE TO PRESSURIZE. FOUND LEFT ACM SEIZED AND REPLACED IT.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 73,593 hrs · 54,193 cycles

LEFT AFT LAVATORY SMOKE DETECTOR SOUNDING CONSTANTLY/NO SMOKE OR ODORS PRESENT. THE SMOKE DETECTOR WAS REPLACED. (LP1089857)

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 73,332 hrs · 53,961 cycles

MISSING EMERGENCY EXIT SIGN BTW EMERGENCY EXIT DOORS AT CABIN PAX. EXIT SIGNAL BTW EMERGENCY EXIT DOORS AT CABIN PAX WAS INSTALLED PER AMM 33-51-00.

Part: SPACER — CORRODED (MID CARGO) · corrosion level 2 · airframe 73,329 hrs · 53,960 cycles

CORROSION AT DOUBLER REPAIR SPACER OF THE MID CARGO. (CORROSION LEVEL 2): SPACER OF THE MID CARGO WAS REPLACED PER DC-9 / MD-80 SRM 53-05 FIG. 123. (LP1012114)

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,833 hrs · 53,543 cycles

ON SVC FOUND 1ST CLASS EMERGENCY CEILING LIGHTS INOP. REPLACED BATTERYS ON 1ST CLASS CEILING EMERGENCY LIGHTS PER AMM 33-53. OPS CHK GOOD. OK FOR SVC. (LP5205676)

Part: SKIN — DAMAGED (FUEL TANK) · airframe 70,795 hrs · 51,852 cycles

DURING CENTER TANK LOWER SKIN INSPECTION, FOUND DAMAGE ON TANK SKIN FROM HYDRAULIC LINE RIGHT SIDE. C/W ERA 566705-14.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 70,504 hrs · 51,622 cycles

AFTER PUTTING DOWN LANDING GEAR, NOSE GEAR GREEN DOWN AND LOCKED DID NOT ILLUMINATE. PUSH TO TEST BULBS (GREEN) DID NOT ILLUMINATE BUT PEDESTAL INDICATOR WAS OUT, INDICATING DOWN AND LOCKED. COMPLIED WITH QRH. DECLARED EMERGENCY AND LANDED WITH NO ISSUES. REPLACED NOSE GEAR INTERLOCK S1-412 AND LANDING GEAR INTERLOCK R2-262, REPLACED B5-75 WARNING LIGHT DIM AND TEST UNIT 2, REPLACED PROXIMITY SENSOR D1-31 AND REPLACED PSEU IAW AMM 32-60. PERFORMED A NLG SENSOR INTEGRITY CHECK IAW WORK CARD 3262-01015-0401. JACKED NOSE AND PERFORMED A GEAR SWING OF NOSE LANDING GEAR IAW AMM 07-12. ALL INDICATIONS NORMAL. PROXIMITY SENSOR D1-31 REPLACED IAW SWPM 20.

Part: LIGHT — SHORTED (CABIN) · airframe 70,338 hrs · 51,488 cycles

CALL SYSTEM CIRCUIT BREAKER POPPED, WILL NOT RESET. T/S PER WDM 33-21. FOUND DEBRIS SHORTING PSU AT ROW 28ABC. REMOVED DEBRIS. RESET C/B, SYSTEM OPS NRML.

Part: STRUCTURE — DAMAGED (BS 1338) · airframe 68,269 hrs · 49,845 cycles

OUT OF LIMITS DRAIN HOLE IN LOWER TEE AFT FLANGE BS 1338. REPAIRED IAW ER/A 555650-14, REV ORIGINAL & ETI-88-17-082, REV. 2.

Part: FRAME — CRACKED (BS 1451) · airframe 68,269 hrs · 49,845 cycles

AFT ACCESSORY BAY, CRACKED FRAME BS 1451, LONGERON 3L - 3R. REPAIRED IAW ETI-88-17-080, REVISION 4, AND ER/A 555642-14, REV ORIGINAL.

Part: ANGLE — CRACKED (BS 1463) · airframe 68,269 hrs · 49,845 cycles

CRACKED ANGLE ON FRAME BS 1463, LONGERON 18L. REPAIRED IAW ETI-88-17-081 REV. ORIGINAL, & ER/A 555643-14 REV. ORIGINAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,662 hrs · 49,443 cycles

RIGHT WING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51. OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 67,616 hrs · 49,409 cycles

CABIN PRESSURE AUTO INOPERATIVE, AUTO 1 INOPERATIVE, AUTO 2 INOPERATIVE, ALL ILLUMINATED COMPLIED WITH QRH. AN EMERGENCY WAS DECLARED. PERFORMED BITE OF AUTO PRESSURE CONTROLLER NR 1 AND 2. BITE SHOWS A/C MOTOR. PERFORMED RESET OF CONTROLLER NR 2 FWD.

Part: INTERCOSTAL — CRACKED (TAILCONE) · airframe 66,670 hrs · 48,663 cycles

INTERCOSTAL CRACKED AT TAIL CONE CABLE ATTACH. REPLACED CRACKED INTERCOSTAL IAW SRM 51-00.

Part: WIRE HARNESS — FAILED (EMERGENCY LIGHT) · airframe 66,260 hrs · 48,347 cycles

EMERGENCY LIGHT AT 14DE INOPERATIVE. REPLACED HARNESS AT SEAT 14DE IW AMM 33-52.

Part: CUSP WEB — CORRODED (BS 1054) · airframe 63,014 hrs · 46,082 cycles

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

Part: LATCH — CORRODED (TAILCONE) · airframe 62,927 hrs · 46,023 cycles

MAINTENANCE FOUND RUSTED LATCH PINS OF TAIL CONE SLIDE. MAINTENANCE REPLACED HARNESS ASSY IAW AMM 25-62-01-201.

Part: ANGLE — CORRODED (BS 193) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP ANGLE BS 193 AND X=59 AT R1. REPAIRED IAW SRM 53-05, FIG 55 AND ELONGATED HOLES WITH ER/A 531375-14AD, REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CARGO TRACK BS 1007 - 1155. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR. 26. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, DWG 5936660, REV BZ.

Part: CUSP WEB — CORRODED (BS 865-905) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB BETWEEN X -44 AND -60 AND BS 865 - 905. THE CUSP WEB WAS REPLACED IAW SRM 53-057 AND 131A SHEET 1 AND DWG N 9910151, REV H AND 51-30-2, 51-30-5.

Part: RIB — CORRODED (SLAT) · corrosion level 2 · airframe 62,916 hrs · 46,016 cycles

CORROSION ON RIB FWD AND AFT LOWER BORES STA XIS 186 AT SLAT PANEL NR 1 RT. DAMAGES ON LOWER BORES WERE REWORKED IAW ETI-88-14-35, REV 1 AND ER/A 531360-14 REV ORIGINAL.

Part: RETAINER — CRACKED (NACELLE) · airframe 62,914 hrs · 46,015 cycles

CRACKED PYLON T/E RT RETAINER. THE RETAINER WAS REPLACED IAW SRM 54-31-0, FIG 2B AND 51-30-1.

Part: BAR — CORRODED (TE FLAPS) · airframe 67,484 hrs · 49,320 cycles

CORROSION ON LOWER BAR AND LINK OF THE LT FLAP FLEX JOINT. THE LOWER BAR WAS REWORKED AND REPAIRED IAW ER/A.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,916 hrs · 46,016 cycles

CRACKED REPAIR DOUBLER ON HORIZONTAL STABILIZER FAIRING 3705A. SKIN WAS TRIM OUT. FABRICATED DOUBLER AND FILLER IAW ER/A 464895-14 MA. PARTS REPAIR WERE INSTALLED IAW SRM 55-03.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT HORIZONTAL STABILIZER REAR SPAR HINGE HOLES NR 6. DAMAGE REPAIRED IAW ERA 531383-14, REV.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 62,914 hrs · 46,015 cycles

CUT OUT AND WEAR ON OTBD TIP OF RT HORIZONTAL STABILIZER REAR SPAR LOWER CAP. DAMAGE REPAIRED IAW ER/A 531383-14, REV ORIG.

Part: LONGERON — CORRODED (BS 995) · corrosion level 2 · airframe 62,916 hrs · 46,016 cycles

CORROSION ON REPAIR OF LONGERON 20L BS 995. REPAIRED IAW ER/A 531391-14 REV ORIG.

Part: BEAM — CORRODED (BS 1159-1210) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON AFT CARGO DOOR FRAME LOWER BEAM BS 1159-1210. BEAM REPLACED IAW DWG NR 5930483, REV.

Part: ANGLE — CRACKED (BS 825) · airframe 62,914 hrs · 46,015 cycles

CRACKED ANGLE AT LOWER INTERCOSTAL ATTACH BS 825 X -45 AND Z=-9. . ANGLE WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: CARGO TRACK — CORRODED (BS 522-788) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 522-788 AND LONGERONS 27 - 28L. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 1485-1497) · airframe 62,914 hrs · 46,015 cycles

CRACKED ANGLE BETWEEN STA Y=1497 CANT AND Y=1485 LONGERON 23LT AT AFT ACCESORY COMPARTMENT. ANGLE WAS REMOVED IAW SRM 51-30-2 AND 51-30-5 AND DAMAGE WAS REMOVED IAW SRM 51-70-5 AND ANGLE AND DOUBLERS WERE FABRICATED IAW SRM 51-07, FIG 2 AND REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-70-3, PAR 14,21 AND REPAIR ANGLE AND ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,914 hrs · 46,015 cycles

CRACKED PAN AT FWD CARGO DOOR BETWEEN BEAM 5 AND AFT EDGE. REPAIRED IAW ER/A 531392-14, REV ORIGINAL AND ETI-88-15-024, REV. 1.

Part: FITTING — CORRODED (MLG) · corrosion level 2 · airframe 62,916 hrs · 46,016 cycles

CORROSION ON RT MLG FITTING AT INBD LOWER HOLE FACE. REPAIRED IAW ER/A 531381-14, REV ORIGINAL.

Part: RETAINER — CRACKED (RT PYLON) · airframe 62,914 hrs · 46,015 cycles

CRACKED PYLON T/E RT RETAINER. THE RETAINER WAS REPLACED IAW SRM 54-31-0, FIG 2B AND 51-31-1.

Part: FINGER DOUBLER — CRACKED (BS 1180-1213) · airframe 62,914 hrs · 46,015 cycles

CRACKS ON FINGER DOUBLER FROM BS 1180 - 1213 BETWEEN LONGERONS 25 - 26L. FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E.

Part: FRAME — CRACKED (BS 1510) · airframe 62,914 hrs · 46,015 cycles

CRACKS ON FRAME BS 1510. FRAME REPLACED IAW DWG 9911843, ITEMS 3 & 5, REV AC SRM 51-10-4 AND SRM 51-30-2.

Part: SKIN — CORRODED (BS 807) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN BS 807 BETWEEN LONGERONS 29-30L. CORROSION REMOVED IAW SRM AND DWG 5936046 AND SRM 53-04, PAR 57.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 62,914 hrs · 46,015 cycles

CRACK ON INTERNAL DOUBLER BS 1429-1431, APPROXIMATELY 10 INCHES FROM LT DORSAL ANGLE AT SETTLEMENT AREA OF ACCESS PLATE 6301A AT VERTICAL STABILIZER FIXED L/E. INTERNAL DOUBLER WAS REPLACED IAW DWG 59140242, REV BV AND SRM 51-70-4 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CARGO TRACK BS 1007 - 1155. CORROSION REMOVED IAW SRM 51-10-3, PAR. 26. THE CARGO TRACK IAW SRM 51-30-2 DWG 5936660 REV BZ.

Part: CARGO TRACK — CORRODED (BS 1007-1218) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION WAS FOUND ON LT CARGO TRACK BS 1007 - 1218. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2, FIG 4C, SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 693) · airframe 62,914 hrs · 46,015 cycles

CRACKED LONGERON 4R BS 693. LONGERON WAS REPAIR IAW ER/A NR 531369-14.

Part: VANE — PUNCTURED (LT WING TE FLAP) · airframe 62,914 hrs · 46,015 cycles

PUNCTURE ON LT WING OTBD FLAP MID GUIDE VANE L/E. REPAIRED IAW SRM 57-03D, PAR 11 AND OPEN 1031.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,914 hrs · 46,015 cycles

DAMAGE COAT PAINT AND FLAME SPRAY ON RUDDER. RUDDER WAS REPAIRED IAW 51-70-1AD, PAR 23.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,914 hrs · 46,015 cycles

CRACK ON VERTICAL STABILIZER L/E RT SIDE BS 1401 BESIDE TO DORSAL ANGLE. CRACK WAS STOP DRILLED, DOUBLER WAS FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 55-01.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 62,914 hrs · 46,015 cycles

PUNCTURE ON LOWER SKIN OF INBD FLAP XFLS=27 AT LT WING. PUNCTURE WAS REPAIRED IAW SRM 57-01, FIG 1, SH 2.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,914 hrs · 46,015 cycles

CRACKED LONGERON 2RT STA Y=1418 AT AFT ACCESSORY COMPARTMENT. LONGERON 2RT WAS REPAIR IAW SRM 53-02, FIG 18 AND WAS INSTALLED IAW ER/A 531352-14AD, REV ORIG.

Part: STIFFENER — CRACKED (BS 1418) · airframe 62,914 hrs · 46,015 cycles

CRACKED STIFFENER OF FRAME BS 1418 BETWEEN LONG 2 LT- 2 RT AT AFT ACCESSORY COMPARTMENT. STIFFENER WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,914 hrs · 46,015 cycles

CRACKED PAN AT FWD CARGO DOOR BETWEEN BEAM 5 AND AFT EDGE. CRACKED ON PAN WAS STOPPED AND DRILLED IAW SRM 51-01, PAR 21. HFEC WAS ACCOMPLISHED. NO CRACKS WERE FOUND NDT SRM 06-10-01. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-03, FIG 8. REPAIR DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10- 3 PARS 1 AND 14. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5 AND 51-30-1.

Part: SKIN — DAMAGED (BS 294-313) · airframe 62,914 hrs · 46,015 cycles

LIGHTNING STRIKE ON RT WINDOW FRAME FWD/MID SECTION AND AFT/UPPER CORNER BETWEEN BS 294-313. LIGHTNING STRIKE WAS REPAIRED IAW ETI 88-15-004 AND ER/A 531372-14 REVISION ORIGINAL.

Part: CUSP WEB — CORRODED (BS 865-905) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-44 AND X=-60 AND BETWEEN Y= 865 TO 905. CUSP WEB WAS REPLACED IAW SRM 53-057 AND 131A SHEET 1 AND DWG N. 9910151.

Part: SEAT TRACK — CORRODED (BS 721-1031) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON SEAT TRACK BETWEEN BS 721 - 1031 AT X -54. THE SEAT TRACK REPLACED IAW SRM 53-05, FIG 4F.

Part: SKIN — CORRODED (BS 785) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN, BS 785 BETWEEN LONGERONS 29-30R. CORROSION WAS REMOVED IAW SRM AND DWG 5936046 AND SRM 53-04, PAR 57.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,914 hrs · 46,015 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME FWD/UPPER CORNER AND UPPER/MID SECTION STA Y:313 TO 332. LIGHTNING STRIKE WAS REPAIRED IAW ETI 88-15-004 AND ER/A 53-137214, REV ORIG.

Part: SKIN — DAMAGED (BS 256-275) · airframe 62,914 hrs · 46,015 cycles

LIGHTNING STRIKE ON RT WINDOW FRAME FWD/LWR CORNER AND AFT/LWR CORNER BETWEEN BS 256-275. LIGHTNING STRIKE WAS REPAIRED IAW ETI 88-15-004 AND ER/A 531372-14, REVISION ORIGINAL.

Part: CUSP WEB — DAMAGED (BS 731-750) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

REWORK OUT OF LIMITS CORROSION ON RT CUSP WEB BETWEEN X -54 TO -60 AND BS 731 - 750. AREA OUT OF LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-10-3 PAR 14, 21, AND 38 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 221) · airframe 62,914 hrs · 46,015 cycles

CRACK ON RT CUSP WEB BS 221 BETWEEN X -54 TO X -60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131 A.

Part: CUSP WEB — CORRODED (BS 503-579) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

RT CUSP WEB CORRODED BETWEEN X -54 AND X -60 BS 503 - 579. CUSP WEB WAS REPLACED IAW SRM 51-30-1, FIG 1 AND 51-30-2.

Part: WEB — CRACKED (BS 200-218) · airframe 62,914 hrs · 46,015 cycles

CRACKED WEB BETWEEN BS 200 - 218. WEB REPLACED IAW SRM 53-14-1, FIG 11.

Part: INTERCOSTAL — CRACKED (BS 988) · airframe 62,914 hrs · 46,015 cycles

CRACKED INTERCOSTAL BETWEEN X -6 AND X 6, BS 988. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS INDICATIONS WERE FOUND IAW NDT SPM 06 -10-01.001. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-30-2 AND SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 214-216) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT SEAT TRACK FITTING X -55, BS 214-216. FITTING WAS REPLACED IAW SRM 51-30-5 AND DWG 3953059, REV "H".

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,914 hrs · 46,015 cycles

CRACKED CHANNEL. CRACK STOP DRILLED IAW SRM 53-05 REPAIRED IAW SRM 53-05, FIG 131C.

Part: STRIP — CORRODED (BS 1148-1218) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON AFT CARGO LOWER DOOR FRAME NUT STRIP, BS 1148 - 1218. NUT STRIP REMOVED IAW SRM 51-30-2, AND REPLACED IAW DWG 590483, REV AND SRM 51-30-2.

Part: SKIN — CORRODED (BS 1315) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

THE AFT LAVATORY CUTOUT SKIN & INTERNAL DOUBLER, BS 1315, L22L, CORRODED. REPAIRED IAW ER/A 515200-14, REV B.

Part: CUSP WEB — CORRODED (BS 782-785) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CUSP WEB X 57 TO X 59 BS 782-785. REMOVE DAMAGE, FABRICATED REPAIR, TREATED, PAINTED REPAIR AND INSTALLED IAW SRM 51-30-2 AND 53-05, FIG 131 A-13 AND 51-10-3 PAR 21 AND 14.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 62,914 hrs · 46,015 cycles

CRACKED FLOOR PANEL 826A. DAMAGE WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND WAS TREATED, PAINTED AND WAS INSTALLED AND RUB STRIP WAS BONDED IAW SRM 51-70-4 AND 51-20-0.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,914 hrs · 46,015 cycles

CRACKED LONGERON 3R BS 1437 AFT ACCESORY COMPARTMENT. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: WEB — CORRODED (BS 1338) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON VERTICAL WEB BS 1338 BETWEEN LONGERONS 26-30L. CORROSION WAS REMOVED AND MEASURE IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2 AND FOUND WITHIN LIMITS. AREAS TREATED AND PAINTED IAW SRM 53-01, FIG 1, SRM 51-10-3, PAR 14,21,26, 38, SRM 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 62,914 hrs · 46,015 cycles

CRACKED CHANNEL . CHANNEL STOP DRILLED, REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, PAR 145, 51-10-3, PAR 21, 14, 51-30-2, AND 51-30-5.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 62,914 hrs · 46,015 cycles

CRACKED FLOOR PANEL. CRACK STOP DRILLED, REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05 PAR 145 51-10-3 PAR 21,14 AND SRM 51-30-2.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 62,914 hrs · 46,015 cycles

CRACKED FITTING ON MID CARGO DOOR, BS 654 BETWEEN BEAM 5 AND UPPER EDGE. FITTING WAS REMOVED IAW SRM 51-30-02 AND 51-30-1. FITTING WAS FABRICATED AND DRILLED AJUSTED IAW DWG 3926046, REV B. FITTING WAS TREATED AND PAINTED IAW SRM 51-30-03 PAR 14/21. NEW FITTING WAS INSTALLED IAW SRM 51-30-1.

Part: CUSP WEB — CRACKED (BS 769-788) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CRACK AND CORROSION ON RT CUSP WEB BETWEEN STA Y= 769 TO 788, FROM X =-54 TO X=-60 AT PAX CABIN FLOOR STRUCTURE. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 26. ORIGINAL THCKNESS IS 0.020" REMAINING IS 0.019" WITHIN LIMITS IAW ER/A 511165-14MA, REV B. AREA WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14-21. CRACK WILL BE ATTENDED WITH CARD NR 250 ZONE 201.

Part: STRUCTURE — CORRODED (BS 662-669) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON REPAIR DOUBLER X 56 TO X 60, BS 662-669. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-14, 51-30-5, AND 51-10-3.

Part: CUSP WEB — CRACKED (BS 769-788) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CRACK RT CUSP WEB BETWEEN STA Y=769 TO Y=788 FROM X=-54 TO X=- 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: TEE FITTING — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACKED TEE FITTING BETWEEN BEAM 5 AND UPPER EDGE BS 654 AT MID CARGO DOOR. THE TEE FITTING WAS REMOVED IAW SRM 51-30-2, FORMER WAS FABRICATED IAW SRM 51-10-2 AND DWG 9957664, REV N, NEW FORMER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21 NEW FORMER WAS INSTALLED IAW SRM 51-30-20 AND 51-30-01.

Part: CARGO TRACK — CORRODED (BS 1221-1322) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CARGO TRACK BS 1221 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 62,914 hrs · 46,015 cycles

CRACK ON CHANNEL AND SPACER OF WING BOX FLOOR PANELS 826D AND 886C. THE CHANNELS AND SPACER WERE REPLACED ON FLOOR PANEL 826D AND 886C. REMOVED SRM 51-30-1 DRILLED SRM 51-10-4 INSTALLED DWG 9936639, REV -"P".

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RIBS XOS 380 AND 286 FWD BORES AT RT SLAT PANEL NR 3. DAMAGES ON BORES WERE REWORKED IAW ETI-88-14-298, REV 1 AND ER/A 531354-14, REV ORIG.

Part: FITTING — CRACKED (BS 927) · airframe 62,914 hrs · 46,015 cycles

CRACK ON FITTING ON BS 927, X -43 AND Z -11. CRACKED FITTING WAS REMOVED, NEW FITTING WAS DRILLED, TREATED AND PAINTED AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5/51-30-2/51-30-1 AND 51-10-3 PAR 14, 21.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 62,914 hrs · 46,015 cycles

WEAR ON FWD/AFT LOWER EDGE PRODUCTION DOUBLERS ON AFT CARGO DOOR SKIN. DOUBLERS WERE BLEND OUT IAW SRM 52-01, FIG 1. ORIGINAL THICKNESS ON FWD DOUBLER IS .160 AND REMAINING IS .154 WITHIN LIMITS IAW SRM 52-01, FIG 1 FWD DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21 AFT DOUBLER WAS REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1185-1237) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT ANGLES BETWEEN X 54 TO X 60, BS 1237, 1234, 1228, 1215, 1188, AND 1185. ANGLES WERE REMOVED IAW SRM 51-30-2 CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, CLIPS WERE TREATED PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14,21 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 628-655) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 AND X=-60 AND Y=628 AND Y=655. CUSP WEB WAS REMOVED, FITTING WERE REMOVED, SPARS WERE REMOVED, NEW CUSP WEB WAS ADJUSTED AND DRILLED, NEW CUSP WEB WAS TREATED AND PAINTED, NEW CUSP WEB WAS INSTALLED, FITTINGS AND SPARS WERE INSTALLED IAW SRM 51-30-2, 51-30-1,51-30-5, 51-10-4,51-10-3, PAR 14 AND 21. Y=598, Y=617, Y=629, Y=636, Y=655,Y=674,Y=693,Y=701. MEASURE: NDT SPM 04-00-07 PAR 5, FIG 3, SHEET 1 AND 2 ORIGINAL THICK .020" REM .013IN ON ALL AREAS FROM STA 598 TO 701 IAW ER/A 511165-14 MA REV B. .

Part: CUSP WEB — DAMAGED (S 1065-1066) · airframe 62,914 hrs · 46,015 cycles

CRACK CUSP WEB BETWEEN X=-54 TO X=-60, Y=1065-1066 AND Y=1074-1075. SECTION DAMAGE WAS REMOVED, NEW PARTS WERE FABRICATED. REPAIR PARTS WERE TREATED AND PAINTED. REPAIR PARTS WAS INSTALLED IAW SRM 53-05, FIG 131 A-14 51-10-3, PAR 14 AND 21 SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 608-614) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CUSP WEB X=57 TO X=60, STA Y=608-614 AT FLOOR STRUCTURE. DAMAGE WAS REPAIRED WITH SRM 53-05, FIG. 131A-13.

Part: CUSP WEB — CORRODED (BS 1193-1212) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION FOUND ON RT CUSP WEB REPAIR DOUBLER BETWEEN X -54 AND X -60 BS 1193 - 1212. REPAIR DOUBLER WAS REMOVED. A NEW DOUBLER WAS FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 53-05, FIG 131A, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1098-1117) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB BETWEEN X -54 AND X -60 BS 1098 - 1117. REMOVED FASTENERS AND FOUND TO BE OUT OF LIMITS. AREA WAS REPAIRED WITH SRM 53-05, FIG 131A-8, AND SRM 51-30-2.

Part: LONGERON — CRACKED (BS 1336) · airframe 62,914 hrs · 46,015 cycles

CRACK ON LONGERON 14R END BS 1336. LONGERON END WAS REPLACED IAW SRM 53-14-3, FIG 4, 51-30-5 AND 51-10-3, PAR 21 AND 14.

Part: FLOOR PANEL — DELAMINATED · airframe 62,914 hrs · 46,015 cycles

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

Part: SKIN — DAMAGED (BS 446-465) · airframe 62,914 hrs · 46,015 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN LONGERON 9R BETWEEN BS 446-465. REPAIRED IAW SRM 53-04-2, FIG 2, SHEET 15.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 62,914 hrs · 46,015 cycles

CRACK ON SHEAR TIE BS 1380 BETWEEN LONGERON 12 - 13R. SHEAR TIE WAS REMOVED, A NEW SHEAR TIE WAS FABRICATED TREATED AND PAINTED. THE NEW SHEAR TIE WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 P.14 AND 21 AND DWG 5913596, REV AN.

Part: DOUBLER — CORRODED (BS 1338 BULKHEAD) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON BULKHEAD DOUBLER BS 1338 LONGERON 30. DOUBLER WAS REPLACED WITH SRM 51-10 -4, SRM 51-30-2 & SRM 51-30-5 & DWG REV.

Part: DOUBLER — CORRODED (BS 1338) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON DOME PRODUCTION DOUBLER STA Y=1338 LONG PROTECTION 30 AFT CARGO COMPARTMENT. PRODUCTION DOUBLER WAS REPLACED WITH SRM 51-10-4, SRM 51-30-2 & SRM 51-30-5 & DWG 9915561, REV CARGO.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON FRAME BS 1380 BETWEEN LONGERONS 28RT - 28LT IN AFT ACCESORY COMPARTMENT. FRAME WAS REPLACED IAW DWG 9912246 REV DE AND SRM 51-30-2 , 51-30-5, AND 51-30-1.

Part: SKIN — CRACKED (SLAT) · airframe 62,914 hrs · 46,015 cycles

CRACK ON LOWER SKIN AT MID SECTION AT SLAT PANEL 0 LT. FASTENER WERE REMOVED IAW SRM 51-30-02 AND 51-30-08 DAMAGE AREA WAS CUTOUT IAW SRM 57-01, FIG 5. DOUBLER AND FILLER WERE FABRICATED IAW SRM 57-01, FIG 5 DWG 5937421. DOUBLER AND FILLER WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-02 AND 51-30-02 AND 51-30-08.

Part: PAN — CRACKED (BS 1155) · airframe 62,914 hrs · 46,015 cycles

CRACK ON PAN BELOW STOP FITTING 4 BS 1155 IN AFT CARGO BAY. FASTENER WERE REMOVED IAW SRM 51-30-2. CRACK ON PAN WAS STOPPED DRILLED IAW SRM 52-05D, SHEET 1. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-05D, SHEET 2, DOUBLER WAS PAINTED IAW SRM 51-10-3, PAR 14. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 484-495) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION RT CUSP WEB X -54 TO X -60 FROM BS 484 - 495. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A.

Part: SKIN — CORRODED (BS 541-560) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON INNER FUSELAGE SKIN BETWEEN BS 541-560 LONGERONS 29 - 30L. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, (UT) WAS ACCOMPLISHED AND FOUND OUT LIMITS IAW SRM 53-04 COND. 2 AND NDT SRM 04-00-07, PAR 5, FIG 3, SHEET 1-2. A DOUBLER WAS FABRICATED IAW SRM 53-04-02, FIG 2, THE DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 21 AND 14, AND INSTALLED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON COUNTERSINK HOLES AT FUEL ACCESS PANEL 1414C AND 1436C ON RT WING. CORROSION WAS REMOVED IAW SRM 51-22-2A. AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON BORE OF PLATES, ZRS=173 AND XH=5 LT SIDE LOCATED ON VERTICAL STAB REAR. BORE OF PLATES WAS REMOVED. HOLD WAS REWORKED WITH MEASURED HOLE LT OTBD: O 1.435 AND HOLE. LT INBD: O 1.435, THEREFORE WITHIN LIMIT. REPAIR AND BUSHING WAS FABRICATED, AREA WAS PAINTED, BUSHINGS WERE INSTALLED AND BORE PLATES WAS INSTALLED IAW SRM 55-02D FIG. 28. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 622-630) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CUSP WEB BETWEEN STA Y= 630 TO 622 AND STA X= 57 TO 60 AT PAX CABIN. DAMAGE WAS REMOVED, NEW PARTS WERE FABRICATED, REPAIR PARTS WERE TREATED AND PAINTED, REPAIR PARTS WERE INSTALLED AND CIC WAS APPLIED IAW SRM 53-05, FIG 131A-13, 51-10-3, PARR 21 AND 14, 51-30-5 AND 51-10-3 PARR.38.

Part: RIB — CORRODED (RT WING SLAT) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RIB FWD BORE STA XOS 380 AT RT SLAT PANEL NR 4. DAMAGE ON BORE RIB STA XOS 380 WAS REWORKED IAW ER/A 531353-14, REV ORIG.

Part: FRAME — DAMAGED (BS 1322) · airframe 62,914 hrs · 46,015 cycles

TOOL DAMAGE ON FRAME BS 1322 BETWEEN LONGERON 21 AND 22L . THE FRAME WS REPLACED IAW SRM 53-03, FIG 2A,

Part: HINGE FITTING — CORRODED (CARGO DOOR) · airframe 67,484 hrs · 49,320 cycles

CORROSION ON FWD HINGE ASSEMBLY OF AFT CARGO DOOR. THE FITTING WAS REMOVED, A NEW FITTING WAS DRILLED, TREATED, AND PAINTED. A NEW FITTING WAS INSTALLED.

Part: FLOOR SUPPORT — CRACKED (BS 788) · airframe 62,914 hrs · 46,015 cycles

CRACKED FLOOR SUPPORT AT BS 788 AND X -33 AT PAX CABIN. REPLACED IAW SRM 51-14-2, 51-10-4, 51-103, PAR 14 AND 21, 51-30-5.

Part: RIB — CORRODED (WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RIBS XOS 380 AND 286 FWD BORES AT RT SLAT PANEL NR 3. DAMAGES ON BORES WERE REWORKED IAW ETI-88-14-298, REV 1 AND ER/A 531354-14, REV ORIGINAL.

Part: CUSP WEB — WORN (BS 284) · airframe 63,214 hrs · 46,196 cycles

WORN LT CUSP WEB X=53 STA Y=284 AT FLOOR STRUCTURE. DAMAGE WAS DRILLED, TREATED, PAINTED, AND REPAIR PLUG WAS INSTALLED IAW SRM 51-10-3, PAGE N 14, 21, 53-01 FIG 1, SHEET 2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON COUNTERSINK HOLES IN FUEL ACCESS PANEL OF RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON ACCESS PANEL 1303C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,914 hrs · 46,015 cycles

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

Part: ATTACH FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON INBD, MID AND OTBD ATTACH FITTING FWD AND AFT BORES AT SLAT PANEL 3LT. CORROSION WERE REMOVED OF STA OUTB AND INBD HOLES WERE MEASURED 4EAS 0.1.126 THEREFORE OUT LIMIT MAXIMUM REWORK BUSHINGS WERE FABRICATED AND INSTALLED IAW ERA 531359-14, REV ORIG CORROSION WERE REMOVED STA MID, HOLES WERE MEASURED 4 EAS 0.938 BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,914 hrs · 46,015 cycles

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

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON COUNTERSINK AT FUEL ACCESS PANEL 1464C AND 1466C RT WING. CORROSION ON COUNTERSINKS ON ACCESS PLATES 1464C AND 1466C WAS REMOVED IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR SUPPORT — BROKEN (BS 370) · airframe 62,914 hrs · 46,015 cycles

BROKEN FLOOR SUPPORT, BS 370 BETWEEN LONG=22L TO LONG=23L AT FWD CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPLACED IAW ER/A 413029-14MA, REV C.

Part: ATTACH ANGLE — CRACKED (BS 769-788) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CRACKED ATTACH ANGLE BETWEEN BS 769 - 788 AND LONGERON 27 - 28L. THE ATTACH ANGLE REMOVED AND REPLACED IAW SRM 51-30-2, 51-0-5, 51-10-4, 51-10-3, PAR 21,14, 38.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION FOUND ON COUNTERSINK OF FUEL ACCESS PANEL 1355C. DAMAGE WAS REWORKED IAW SRM 51-22-2A CONDITION II AND FOUND OUT OF LIMITS IAW SRM 51-22-2A COND. II FIG. 8. BUSHINGS WERE FABRICATED, AND TREATED IAW SRM 51-22-2A COND. II AND 51-10-3 PAR. 21. THE REPAIR BUSHING WERE INSTALLED IAW SRM 51-22-2A. AND REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 829-858) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT CUSP WEB X 56 TO X 60, BS 829-858. CORROSION WAS REMOVED IAW SRM 51-30-3 PAR 26. AREA WAS MEASURED IAW ER/A 511165-14MA, CRACK WAS FOUND BS 831-854. DAMAGE WAS REMOVED IAW SRM 53-05, FIG. 131A-1. REPAIR FABRICATED IAW SRM 53-05, FIG 131A-1, AND INSTALLED IAW SRM 53-05, FIG. 131A-1.

Part: SKIN — CORRODED (BS 805-807) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 805-807 LONGERONS 29-30L. CORROSION REMOVED AND FOUND WITHIN LIMITS. TREATED PAINTED AND APPLIED CIC IAW SRM 51-10-3, 53-04, PAR 57.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON COUNTERSINK HOLES AT FUEL ACCESS PANEL 1365C AND 1367C LT WINGS. CORROSION WAS REMOVED IAW SRM 51-22-2A. ON ACCESS PANEL 1367C WAS FOUND WITHIN LIMITS IAW SRM 51-22-2A AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. ACCESS PANEL 1365C WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON INTERCOSTAL FROM BS 769 - 788 LONGERONS 27 - 28L. CORROSION WAS REMOVED AND FOUND OUT OF LIMIT. A NEW INTERCOSTAL WAS FARICATED, TREATED PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 26, 53-01 FIG , 51-10-2, 51-10-3 PAR 21,14, 38 51-30-5 AND DWG 9915554, REV J.

Part: LONGERON — CRACKED (BS 1307) · airframe 62,914 hrs · 46,015 cycles

CRACKED LONGERON 8R BS 1307. LONGERON REPAIRED IAW SRM 53-02 FIG 18 AND 51-302 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 247-256) · airframe 62,914 hrs · 46,015 cycles

CRACK ON CUSP WEB AT BS 247 - 256 BETWEEN X 44 TO X 54 . CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 5, 53-05, FIG 131-A 24, 51-10-3 PART 21, 14, AND 51-30-2.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 62,914 hrs · 46,015 cycles

CRACKED FITTING TO ATTACH HORIZONTAL STABILIZER AND FORCE FIXURE AT VERTICAL STABILIZER UPPER EDGE, CARD 10, ZONE 65. DAMAGED FITTING WAS REMOVED NEW FITTING WAS DRILLED TREATED PAINTED AND INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21 AND 51-30-1.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT WING ACCESS PANEL 1303C. ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON COUNTERSINK HOLES AT FUEL ACCESS PANEL ON RIGHT WING. REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON ACCESS PANEL 1303C. REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: CUSP WEB — CRACKED (BS 208) · airframe 62,914 hrs · 46,015 cycles

CRACKED CUSP WEB AT BS 208 BETWEEN X 44 TO X 54. DAMAGE WAS REMOVED AND AREA WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: FLOOR SUPPORT — CORRODED (BS 159-200) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON FLOOR SUPPORT X=8, BETWEEN BS 159 - 200. CORROSION AND FLOOR SUPPORT WERE REMOVED IAW SRM 51-10-3 PAR 26, 51-30-1 AREA WAS MEASURED IAW SRM 53-01, FIG. 1. NEW SUPPORT WAS DRILLED AND ADJUST IAW SRM 51-10-4. NEW SUPPORT WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: SEAT TRACK — CORRODED (BS 369-371) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON REPAIR PLUG OF SEAT TRACK, X 22 BETWEEN BS 369 - 371. REMOVED AND REPLACED THE REPAIR PLUG IAW SRM 51-30-1.

Part: SKIN — CRACKED (BS 1437) · airframe 62,914 hrs · 46,015 cycles

CRACKS ON FUSELAGE SKIN BS 1437 BETWEEN LONGERONS 4 - 5R. DAMAGE REMOVED, REPAIR FABRICATED. AREA AND REPAIR TREATED AND PAINTED, REPAIR INSTALLED IAW SRM 53-04, FIG 27.

Part: FLOOR SUPPORT — CORRODED (BS 255) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION FOUND ON FLOOR SUPPORT AT BS 255 X34 AT PAX CABIN. FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-4, 51-10-3, PAR 21, AND 14 AND IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,914 hrs · 46,015 cycles

CRACKED LONGERON 16R BS 1437 . LONGERON WAS REMOVED AND REPLACED IAW AMM 54-20-00 AND SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 P. 14-21.

Part: DUCT — CORRODED (RT A/C) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT AIR CONDITIONING EXTERNAL EXHAUST DUCT. EXHAUST DUCT WAS REMOVED, DAMAGE WAS REMOVED, EXHAUST AND WAS REPAIR AND INSTALLED IAW SRM 53-04, PAR 56, 51-30-2.

Part: DOOR FRAME — CORRODED (BS 1185-1201) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON REPAIR DOUBLER ON AFT CARGO BAY LOWER DOOR FRAME BS 1185-1201. DOUBLER REMOVED, AND A NEW DOUBLER WAS FABRICATED,TREATED, PAINTED, AND INSTALLED IAW SRM 53-05, FIG 123.

Part: RECEPTACLE — CORRODED (EXTERNAL POWER) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION AND CRACKS ON EXTERNAL POWER RECEPTACLE. EXTERNAL POWER RECEPTACLE WAS REPLACED IAW DWG 5957232, REV.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RIBS AFT BORES XIS 40 AND 12.2 AT RT SLAT PANEL NR 0, CORROSION ON RIBS AFT BORES REMOVED, AND FOUND OUT OF LIMITS, REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9C.

Part: CUSP WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB DOUBLER REPAIR, X -60 BETWEEN BS 826 - 845. REPAIR REMOVED IAW SRM 51-30-2 AND A NEW REPAIR WAS FABRICATED IAW SRM 53-05, FIG 131A-6. REPAIR TREATED, AND PAINTED IAW SRM 51-10-3 PAR 21, 14. REPAIR WAS INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1041-1060) · airframe 62,914 hrs · 46,015 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER X -60 BS 1041 - 1060. NEW WEB DOUBLER WAS INSTALLED IAW SRM 53-05, FIG. 131A-6 AND 51-30-53.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 62,914 hrs · 46,015 cycles

CRACKS ON ACCESS PANEL 6404A OF VERTICAL STABILIZER. (SM) (CARD 56 - ZONE 00). CRACK WAS STOPPED IAW SRM 55-01, FIG 2 AND 51-01, PAR 21. FABRICATED AND INSTALLED NEW DOUBLERS IAW SRM 55-01, FIG 2, 51-30-2, INSP WAS ACCOMPLISHED AFTER STOP DRILL AND NO CRACKS WERE FOUND IAW SRM 51-01, STEP 86 B AND NDC SPM 06-10-01. 001, NEW DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14.

Part: SEAT TRACK — CORRODED (BS 453-456) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT REPAIR ON SEAT TRACK X 54, BS 453-456. REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3 PAR 38.

Part: BEAM — CORRODED (BS 1185-1201) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION FOUND ON REPAIR DOUBLER IN THE AFT CARGO BAY, LOWER DOOR FRAME BEAM BS 1185-1201. DOUBLER WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05, FIG 123.

Part: ANGLE — CRACKED (BS 110 BULKHEAD) · airframe 62,914 hrs · 46,015 cycles

CRACKED ANGLE ON FWD BULKHEAD, STA Y=110 AT ELETRONIC COMPARTMENT. (SM) (ZONE 100) (CARD 232). ANGLE WAS REPLACED IAW SRM 51-30-2, DWG 9915600, REV V, SRM 51-10-4, 51-10-2, 51-10-3, PAR 21 AND 14, 51-30-5.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACKED FWD LOWER CORNER OF RT RING PAN STA Y=1117-1136 AT INTERNAL FUSELAGE STRUCTURE. RING PAN FWD LOWER CORNER DAMAGE WAS REPAIRED WITH SRM 53-05, FIG 112 AND ERA 493648-14MA, REV ORIGINAL.

Part: FRAME — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN FWD UPPER CORNER STA Y= 674-693 AT INTERNAL FUSELAGE STRUCTURE. REMOVE FASTENERS AND DAMAGE, REPAIR PARTS WERE FABRICATED, TREATED PAIN PAINTED, NDT CHECKED, REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-5, 51-30-2, 51-10-3 PAR 21, 14 ERA 493648-14MA, REV ORIGINAL.

Part: ANGLE — CRACKED (LT WING) · airframe 62,914 hrs · 46,015 cycles

CRACKED ANGLE ON LT WING REAR SPAR XW=536. ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED AND INSTALLED IAW DWG 9910010, REV 65 AND SRM 51-30-3, 51-10-3 PAR 21/14 AND 51-30-5.

Part: ANGLE — CRACKED (BS 1463) · airframe 62,914 hrs · 46,015 cycles

CRACKED ANGLE ON FRAME BS 1463 LONGERONS 19L. ANGLE REMOVED AND REPLACED IAW SRM 51-30-5, IAW DWG 9915634-5, AND SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 422-425) · corrosion level 2 · airframe 62,914 hrs · 46,015 cycles

CORROSION ON LT REPAIR ON SEAT TRACK X 22, BS 422-425. REPAIRED WAS REMOVED AND REPLACED IAW SRM 53-05, FIG 4A, 51-10-3 PAR 38.

Part: FRAME — CRACKED (BS 769-788) · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN FWD UPPER CORNER STA Y=769-788 AT INTERNAL FUSELAGE STRUCTURE. FASTENERS WERE REMOVED, DAMAGE AREA WAS REMOVED REPAIR PARTS WERE FABRICATED, NDT CHECKED, REPAIR PARTS WERE TREATED/ PAINTED AND WERE INSTALLED IAW SRM 51-10-3 PAR 21,14, 51- 30-5 51-30-2 AND 53-05, FIG 122 AND ERA 493648-14MA REV ORIG.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN FWD UPPER CORNER STA Y=788-877 AT INTERNAL FUSELAGE STRUCTURE. FASTENERS WERE REMOVED DAMAGE WAS REMOVED REPAIR ANGLE WAS FABRICATED SHIM AND REPAIR WASHER WERE FABRICATED PARTS REPAIR WERE TREATED AND PAINTED. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, E/RA 493648-14MA, REV ORIG.

Part: FRAME — CRACKED (BS 541-560) · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN FWD UPPER CORNER STA Y= 541-560 AT INTERNAL FUSELAGE STRUCTURE. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED, TREATED/PAINTED, NDT CHECKED, AND WERE INSTALLED IAW SRM 51-10-3, PAR 21,14, 53-05, FIG 122, 51-30-5,51-30-2 ERA 493648-14MA, REV ORIG.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN AFT LOWER CORNER STA Y= 1231-1250 AT INTERNAL FUSELAGE STRUCTURE. SUMMARY RING PAN AFT LOWER CORNER DAMAGE WAS REPAIRED WITH SRM 53-05 FIG 122, FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, TREATED/PAINTED, NDT CHECK AND WERE INSTALLED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21,14, 51-30-5, 51-30-2 ERA 493648-14MA ORIG REV.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACKED FWD UPPER CORNER OF RT RING PAN STA Y=788-807 AT INTERNAL FUSELAGE STRUCTURE. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, NDT CHECKED, REPAIR PARTS WERE TREATED/ PAINTED IAW SRM 53-05, FIG 122, 51-30-5, 51-30-2,51-10-3 PAR. 21,14.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING PAN FWD LOWER CORNER STA Y= 1060-1079 AT INTERNAL FUSELAGE STRUCTURE. DAMAGE WAS REPAIRED WITH SRM 53-05, FIG 122. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, TREATED PAINTED AND INSTALLED IAW SRM 53-05 FIG 122, 51-10-3, PAR 21, 14, 51-30-2, 51-30-5 AND ERA 493648-14MA REV.

Part: PAN — CRACKED · airframe 62,914 hrs · 46,015 cycles

CRACK ON LT RING, PAN FWD UPPER CORNER STA Y= 927-946 AT INTERNAL FUSELAGE STRUCTURE. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21, 14, 51-30-2, 51-30-5 ER/A 493648-14MA, REV.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,474 hrs · 45,722 cycles

OVERHEAD EMERGENCY LIGHTS ROW 1 AND 13 INOPERATIVE. REPLACED THE LAMPS AND OPS CHECKED NORMAL.

Part: STRUCTURE — DAMAGED (BS 1418) · airframe 62,358 hrs · 45,627 cycles

DURING CHECK, CRACK AND GOUGES IN SKIN WAS FOUND BS 1418 STRINGER 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,140 hrs · 45,449 cycles

DURING CHECK, MAINTENANCE FOUND THE FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPS CHECK WAS GOOD.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 62,061 hrs · 45,397 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A BROKEN LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR SLIDE LANYARD WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,642 hrs · 45,083 cycles

CREW FOUND THAT THE EMERGENCY LIGHT AT 27DE WAS LOOSE AND INOPERATIVE. MAINTENANCE SECURED THE LIGHT AT 27DE. LIGHTS OPS OK.

Part: POWER SUPPLY — BURNED (EMERGENCY LIGHTS) · airframe 60,106 hrs · 44,007 cycles

BATTERY POWER SUPPLY B5-23 HAS BURNED CASE IN GALLEY OVERHEAD. REPLACED BATTERY POWER SUPPLY B5-23 IAW AMM 33-53.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 59,862 hrs · 43,818 cycles

VERTICAL STAB L/E SKIN CRACKED ON LT SIDE JUST ABOVE LOWER EDGE OF REMOVEABLE PANEL. REPAIRED IAW SG09550004, REV D.

Part: SLIDE — OUT OF POSITION (TAILCONE) · airframe 59,862 hrs · 43,818 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE COVER FOR TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. AN OUT OF POSITION, MISRIGGED, POOR CONDITION, OR ILL-ARRANGED SLIDE ASSEMBLY COULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYS AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAILCONE SLIDE WAS REPLACED AND AN RII WAS COMPLETED SATISFACTORILY.

Part: SKIN — CRACKED (BS 1418) · airframe 59,862 hrs · 43,818 cycles

CROWN SKIN CRACKED AT BS 1418, S1 & 2R, CUT OUT DAMMAGE AREA. PREFORMED HFEC IAW NDT SPM 06-10-01 . NO CRACKS FOUND. SKIN CRACK AND GOUGE IN SKIN CONTAINED & REPAIR ACCOMPLISHED ON ER/A 518899-14, REV O.

Part: SKIN — CRACKED (BS 1380) · airframe 59,855 hrs · 43,815 cycles

FUSELAGE SKIN CRACKED TWO AREAS AT BS 1380 + 10" ABOVE LT PYLON. CUT OUT CRACKS. HFEC IAW NDTSPM 06-10-01.001. NO FINDINGS COMPLIED WITH PRI ER/A 518877-14 REV O.

Part: SKIN — CRACKED (BS 1439) · airframe 59,855 hrs · 43,815 cycles

CROWN SKIN CRACKED IN TWO AREAS AT BS 1439 BETWEEN S2-3L, CUT OUT DAMAGED AREAS. DAMAGE CONTAINED. HFEC IAW NDTSPM 06-10-01. 001, NO FINDINGS. REPAIRED IAW ER/A 518875-14, REV ORIG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,283 hrs · 43,404 cycles

DURING ROUTINE LINE CHECK, THE AFT STAIR LIGHTS WERE FOUND TO BE INOPERATIVE. THE WRITEUP IS UNCLEAR WHCIH SPECIFIC LIGHTS WERE INOPERATIVE, SERVICE OR ESCAPE PATH. THE LIGHTS WERE REPLACED LAMPS AND OPERATION CHECKED NORMAL.

Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 59,024 hrs · 43,193 cycles

DURING ROUTINE INSPECTION, THE INSPECTOR NOTED DURING PRE-FLIGHT THAT THE NR 1 LT DOOR SLIDE PINS WERE OUT. THE DOCUMENTED COMMENTS ARE NOT SUFFICIENT TO VERIFY THE SPECIFIC PINS IDENTIFIED. THE SLIDE WAS REPLACED ON AMDS WC 2500-4484 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: STRUCTURE — CORRODED (LAV SERVICE DOOR) · airframe 59,016 hrs · 43,186 cycles

DURING SCHEDULED PAINT VISIT, CORROSION WAS FOUND AT THE AFT LAV SERVICE DOOR. PERMANENT REPAIR ACCOMPLISHED IAW ER/A 515200-14.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,873 hrs · 43,096 cycles

DURING OVERNIGHT MX CHECKS, EMERGENCY EXIT ROW LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LAMPS AND OPS CHECKED NORMALLY.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 58,202 hrs · 42,670 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 25D IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED. AFTER RESECURING IT, THE SYSTEM CHECKED FUNCTIONAL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 57,365 hrs · 42,080 cycles

FLIGHT CREW REPORTED SMOKE IN THE CABIN, DECLARED AN EMERGENCY, AND RETURNED BACK TO MCO, LANDING WITHOUT INCIDENT. THE SMOKE DID CLEAR AFTER CREW COMPLETED QRH PROCEDURES. MAINTENANCE REPLACED THE LEFT COOLING TURBINE, REPLACED THE LEFT AND RIGHT COALESCER BAGS, AND PERFORMED A DUCT BURNOUT PER AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,052 hrs · 41,881 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE 1R EMERGENCY FLOOR LIGHTING TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY CONNECTOR AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: GIRT BAR — INOPERATIVE (L1 DOOR) · airframe 56,796 hrs · 41,685 cycles

PILOT FOUND 1L DOOR GIRT BAR TO BE INOPERATIVE. MAINTENANCE INSTALLED THE COVER LATCH AND RETURNED THE AIRCRAFT TO SERVICE.

Part: STRUCTURE — CRACKED (RAM AIR OUTLET) · airframe 56,581 hrs · 41,528 cycles

RIGHT RAM AIR PACK DISCHARGE OUTLET HAS A 5.5 INCH CRACK. MAINTENANCE CUT OUT DAMAGED AREA PER SRM 53-01. HFEC INSPECTED PER NDT SRM 06-10-01, NO OTHER DEFECTS NOTED. FABRICATED DOUBLER AND FILLER. TREATED AND INSTALLED PER SRM 53- 01 FIG 2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,530 hrs · 41,497 cycles

DURING LINE CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY EXIT IDENTIFIER SIGN LAMPS TO BE INOPERATIVE. MAINTENANCE LAMPED SIGNS AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,163 hrs · 41,229 cycles

AFT CARGO COMP AFTER REMOVED ACCESS PANEL STA 1322 FOUND TRACK WITH CORROSION. REMOVED CORROSION FROM AFT CARGO COMP RT TRACK TIEDOWN STA 1322 FOUND OUT OF LIMITS IAW DC9/MD80 53-05 PG 29 FIG 4C. REMOVED AFT CARGO COMP TIEDOWN TRACK RT FROM STA 1212 TO 1322 IAW DC9/MD80 SRM 51-30-2. INSTALLED NEW TRACK ON AFT CARGO COMPARTMENT AT STA 1212 TO 1322 IAW DC9/MD80 SRM 51-30-1 PG 1. AT SAA DURING PSV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,163 hrs · 41,229 cycles

FWD ENTRY AREA STA 168 TRACK WITH CORROSION. REMOVED CORROSION ON FWD ENTRY AREA TRACK STA 168 RBL 10. FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 PG 6 FIG 1. REMOVED FWD ENTRY AREA TRACK STA 168 RBL 10 IAW DC9/MD80 MM20-30-01-201 PG 1. INSTALLED TRACK ON FWD ENTRY AERA STA 148 TO 200 RBL 10 IAW DC9/MD80 MM 20-30-01 PG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,163 hrs · 41,229 cycles

CORROSION ON SEAT TRACK LOCATED AT STA 207 LBL 22. REMOVED CORROSION ON SEAT TRACK LOCATED AT STA 207 LBL 22, FOUND OUT OF LIMITS IAW DC9/MD80 SRM 53-05 FIG 4B PG 24. REMOVED AND CUT OUT SEAT TRACK LOCATED AT STA 200 TO 256 LBL 22 IAW DC9/MD80 SRM 51-30-0 PG 1 AND DC9/MD80 SRM 53-05 FIG 4F PG 32. INSTALLED PARTS FABRICATED SEAT TRACK, SPLICE AND PLATE ON STA 200 TOM 256 LBL 22 IAW DC9/MD80 SRM 53-05 FIG 4F PG 32. AT SAA DURING PSV.

Part: BARRIER — CORRODED (SERVICE DOOR) · airframe 56,163 hrs · 41,229 cycles

FWD SERVICE DOOR STA 168 TO 200 BARRIER WITH CORROSION. REMOVED BARRIER, REMOVED FILLER DAMAGE AT BARRIER STA 168 TO 200. REMOVED CORROSION ON FILLER STA 168 TO STA 200, FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 PG 8. FABBED FILLER IAW MD88 DRW 9957828 AND DC9/MD80 SRM 51-10-4 PG 1. INSTALLED FILLER TO BARRIER IAW DC9/MD80 SRM 51-30-2 PG 1. INSTALLED BARRIER ON FWD SERVICE DOOR STA 168 TO 200 IAW DC9/MD80 SRM 51-30-0 PG 1 ITEM A.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,163 hrs · 41,229 cycles

CORROSION ON THRESHOLD LOCATED AT STA 636 AND 693 L28R MID CARGO COMPARTMENT. REMOVED EXISTING REPAIR SPACER ON THRESHOLD LOCATED AT STA 655.5 TO 681 L28R IAW DC9/MD80 SRM 51-30-5 PG 29. REMOVED CORROSION ON THRESHOLD IAW DC9/MD80 SRM 53-01 FIG 1 PG 6. SPACER REMOVED ON THRESHOLD, FOUND TO BE OUT LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 PG 8. HFEC INSP PER NDTSPM 06-10-01.001 NO CRACKS NOTED AT BLENDED AREAS. NDT INSP FOUND WITHIN LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 SH 3. FABBED NEW SPACER AND INSTALLED NEW SPACER IAW DC9/MD80 SRM 53-05 FIG 123 SH 12 PG 876. AT SAA DURING PSV.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,163 hrs · 41,229 cycles

CORROSION ON AFT CARGO COMP THRESHOLD BETWEEN STA 1155 AND 1211 L28R. RMVD SPACER ON AFT CARGO COMP THRESHOLD BETWEEN STA 1185 AND 1198 L28R. REMOVED CORROSION ON AFT CARGO COMP THRESHOLD BETWEEN STA 1155 AND 1211 L28R IAW DC9/MD80 SRM 53-01 FIG 1 PG 6. RMVD SPACER AT STA 1185 AND 1198 L28R FOUND OUT OF LIMITS IAW SRM DC9/MD80 53-01 FIG 1 PG 8. UT THICKNESS INSP FOUND WITHIN LIMITS IAW DC9/MD80 SRM 53-05 PG 866. HFEC INSP NO CRACKS NOTED IAW NDTSPM 06-10-01.001. FABBED SPACER. INSTALLED NEW SPACER IAW DC9/MD80 SRM 53-03 FIG 123 PG 876. AT SAA DURING PSV.

Part: SLIDE — MISRIGGED (DOOR R1) · airframe 53,275 hrs · 39,261 cycles

DURING LINE CHECK, MX FOUND DOOR R1 SLIDE LANYARD INSTALLED IMPROPERLY AND NOT ATTACHED TO THE GIRT BAR. MX INSTALLED BOTH DOOR SLIDE LANYARDS IAW AMM 25-62-00. CHECKS OK.

Part: SLIDE — MALFUNCTIONED (GALLEY DOOR) · airframe 52,881 hrs · 39,013 cycles

PILOT REPORTED AFT GALLEY DOOR WAS OPENED AFTER DOOR WAS ARMED. SLIDE DID NOT DEPLOY. MAINTENANCE INSTALLED SLIDE PACK PER IAW AMM 25-62-00-201. OK FOR SERVICE. (2010-D1361) (DLM88103191)

Part: CONNECTOR — MALFUNCTIONED (CABIN) · airframe 51,449 hrs · 38,055 cycles

THE EMERGENCY FLOOR LIGHT AT SEAT 11D WAS FOUND TO BE DAMAGED. MAINTENANCE RELAMPED THE LIGHT, WHICH WAS NO HELP. MAINTENANCE THEN RESET THE CONNECTOR, AND THE LIGHT CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,454 hrs · 37,447 cycles

EMERGENCY EXIT LIGHTS INOP ABOVE R1 DOOR, L1 DOOR, COCKPIT DOOR. RELAMPED LIGHT ASSY ABOVE L1 DOOR. REPLACED BATTERY PACK BATTERIES OPS CHK GOOD. PART CHANGED: BATTERY - PN: AD4002P DELTA PN: 339201836, 33-50-00-12D ITEM 30.

Part: TAB — CRACKED (RUDDER) · airframe 48,814 hrs · 36,348 cycles

DAMAGED METALIZED AND CRACKED SKIN OF RUDDER CONTROL TAB. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1AD. TAB WAS BALANCE CHECKED IAW SRM 55-40-1D PAR 25.

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 47,928 hrs · 35,788 cycles

C1 DOOR JAMB PAN WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED PER SRM 53-05D FIG 804D.

Part: HYDRAULIC SYSTEM — CONTAMINATED (LEFT) · airframe 39,640 hrs · 30,220 cycles

LEFT HYD PRESS WENT TO 0 QUANTITY, NORMAL ON DESCENT INTO BDL. RECOVERED PRESS WITH TRANS PUMP ON. DECLARED EMERGENCY AND LANDED UNEVENTFULLY. BLED AIR FROM LEFT HYD RESERVIOR, RAN LEFT ENGINE, CYCLED ALL FLT CONTROLS THRU SEVERAL TIMES. SERVICED AND BLED AIR AGAIN. HYD PRESSURE NOW NORMAL WITH LEFT ENGINE OR TRANSFER PUMP.

Part: CONTROL HANDLE — DIRTY (COCKPIT) · airframe 38,826 hrs · 29,635 cycles

THREE RED GEAR UNSAFE LIGHTS AFTER GEAR EXTENSION. CLEANED LANDING GEAR HANDLE AND SWITCH ASSEMBLY.

Part: POSITION SWITCH — FAILED (COCKPIT) · airframe 36,323 hrs · 27,841 cycles

PUT LANDING GEAR HANDLE DOWN, 3 RED BELOW 1500 FT, GEAR UNSAFE AURAL WARNING. ACCOMPLISHED CHECKLIST. EMERGENCY GEAR HANDLE PULLED 3 GREEN. EMERGENCY GEAR STOWED, 3 RED. COMPLETED CHECKLIST, STOPPED STRAIGHT AHEAD. REPLACED GEAR HANDLE POSITION SWITCH 21-89. JACKED A/C AND CYCLED GEAR THRU SEVERAL TIMES, ALL INDICATIONS NORMAL. A/C OK FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 35,823 hrs · 27,498 cycles

SMOKE IN CABIN FROM PACKS WHEN FIRST APPLIED FROM APU ON TAKEOFF. NORMAL POWER WITH EGT QUITE HIGH, ABOUT 585 DEG, GOT A BURNING ODOR THAT SET OFF SMOKE DETECTORS IN AFT LAV LASTED ONLY A SHORT TIME. REPLACED APU PERFORMED DUCT BURNOUT AND REPLACED WATER BAGS.

Part: BOOT — TORN (TEMP CON VALVE) · airframe 32,688 hrs · 25,317 cycles

TAIL COMPTARTMENT TEMP HIGH ON CLIMB AT 20,000 FT. LIGHT GOES OUT WHEN REDUCING LT ENGINE POWER. REPLACED TORN BOOT AT RT TEMP CONTROL VALVE AND REPLACED CRACKED DUCT IN TAIL COMPTARTMENT

Part: O-RING — FAILED (MLG) · airframe 31,947 hrs · 24,777 cycles

AFTER TAKE OFF, NOSE GEAR SHOWED UNSAFE IN UP POSTION. RECYCLED LANDING GEAR IAW POM PROCEDUCRES. NO HELP RETURNED TO ATL. NOSE GEAR STRUT SHRADER VALVE O-RING DETERIORATED. REPLACED SHRADER VALVE AND O-RING AND SERVICED STRUT PER MM LEAK CHECK OK. NO SPOILER FAIL STALL INDICATION FAIL OR AUTO PRESSURE FAIL MSG. PERFORMED NOSE GEAR SWING. GEAR INDICATIONS NORMAL

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,595 hrs · 24,518 cycles

FWD FLASHLIGHT IN AFT CABIN INOP. REMOVED AND REPLACED BATTERY, OPS GOOD.

Part: RELAY — UNSERVICEABLE (STA 110) · airframe 30,562 hrs · 23,749 cycles

ON GEAR EXTENSION HAD ALL 3 UNSAFE RED LIGHTS AND GEAR DOOR OPEN LIGHT.PERFORMED LANDING GEAR UNSAFE GEAR HANDLE DOWN CKLIST.HYDRAULIC QTY AND PRESS NORMAL.LANDED WITH EMERGENCY GEAR EXTENSION HANDLE PULLED, THREE GREEN LIGHTS AND GEAR DOOR OPEN LIGHT ON. CA-T/S PER MM.BITE CK PSEU OK.JACKED A/C.CYCLED GEAR SEVERAL TIMES.ALL INDICATIONS NORMAL. REPLACED RELAY R2-28 PRECAUTIONARY.ALL CKS NORMAL.

Part: VALVE — LEAKING (MLG) · airframe 28,455 hrs · 22,223 cycles

STRONG SMELL REPORTED BY FLIGHT ATTENDANTS AND NOTICED ALL THE WAY IN THE COCKPIT. SMELLED LIKE RUBBER FROM TIRES. THIS OCCURED RIGHT AFTER GEAR RETRACTION AND VERY QUICKLY DISSAPATED. REPLACED LANDING GEAR CONTROL VALVE. LEAK CHECKS GOOD. PERFORMED OPERATION 5088 DUCT BURNOUT

Part: DUCT — CRACKED (TAIL) · airframe 26,508 hrs · 20,798 cycles

ON CLIMBOUT THUR 1200 FT, TAIL COMPARTMENT TEMP HI LIGHT CAME ON EVEN WITH BOTH A/C SUPPLY SWITCHES IN HP BLEED OFF. LIGHT ILLUMINATES WHEN CLIMB THRUST APPLIED. FOUND A/C WATER SEPARATOR TO CHECK VALVE DUCT CRACKED. REMOVED DUCT WELDED CRACK PER ERA 377908-14, INSTALLED DUCT, LEAK CKS OK. REPLACED RIGHT AND LEFT COMPARTMENT HI TEMP SENSORS, RAN ENGINES, SYS OPS CHECKS OK.

Part: STRUT — DISCHARGED (NLG)

AFTER TAKEOFF WHEN GEAR HANDLE RAISED, NLG WOULD NOT RETRACT. AUTO SPLR FAIL, STALL IND FAIL, NO ACARS OFF TIMES. SERVICED NOSE STRUT.

Part: TIRE — FAILED (LT MLG)

NR 2 MAIN TIRE RECAP SEPARATED FROM CASING. REPLACED NR 2 MAIN WHEEL ASSY. INSPECTED NR 1 ENG INTAKE, NO DAMAGE. REPLACED LEFT GEAR FLYING DOOR STRUT, NO OTHER DAMAGE NOTED.

Part: LONGERON — CRACKED (BS 1418)

CRACKS FOUND AT FS 1418 ON L2L AND L2R AT TYPICAL LOCATIONS PER EO9-63538-03 AND SB53-184. REPAIRED PER ERA 330915-14.

Part: PACK — MALFUNCTIONED (LEFT)

SMELL AND SMOKE IN CABIN WITH LEFT PACK RUNNING. LEFT PACK INOP FWD TO MCO/PLACARD PER MEL 21-00-30B.

Part: PANEL — SHORTED (COCKPIT)

AFTER LIGHT CHECK ON PREFLIGHT, F/O TRP PANEL UPPER RIGHT CORNER BEGAN TO SMOKE WITH ACRID ELECTRICAL ODOR. SECURED ALL ELECTRICS, REPLACED TRP PANEL, ALL CHECKS NORMAL.

Part: LANYARD — BROKEN (DOOR SLIDE)

ON PREFLIGHT, FWD GALLEY DOOR SLIDE LANYARD FOUND BROKEN. REPLACED LANYARD.