N909DE

Part: CONNECTOR — DAMAGED (CABIN) · airframe 64,955 hrs · 50,679 cycles

28D EMERGENCY LIGHT INOP. REPAIRED CONNECTOR AT ROW 28D PER AMM 20-50 LIGHTS AT 28D CK GOOD. (LP4700680)

Part: PAN — CRACKED (CARGO DOOR) · airframe 64,631 hrs · 50,397 cycles

C2 DOOR PAN, CRACK FOUND ON LOWER CENTER AREA, SEEN FROM DOOR INTERIOR WITH INSULATION REMOVED. REMOVED AND REPLACED DOOR REF ND88 AMM 52-31-00. (LP0824299)

Part: WIRE — CHAFED (HYDRAULIC POWER) · airframe 64,624 hrs · 50,392 cycles

AUX HYDRAULIC PUMP POWER FEEDER WIRING WRAP HAS CHAFED SPOT NEAR HYDRAULIC HAND PUMP HANDLE. WRAPPED WIRE REF SWPM 20-10-01 AND ERA 467688-14MADD REV ORG.

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 64,624 hrs · 50,392 cycles

EXFOLIATION CORROSION FOUND AT FORWARD CARGO THRESHOLD NEAR LOWER AFT DOOR STOP- MARKED. REPAIRED, REF MD88 SRM 53-05 PARA 55A FIG 44A. REF. N/R 00103. (LP0812352)

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 64,434 hrs · 50,227 cycles

FOUND LT SLIDE PACK HAD BOTH PINS PULLED OUT OF EYELETS. R&R L1 SLIDE PACK PER AMDS W/C 2561-4964. A/C OK FOR SVC. (LP4489948)

Part: TURBINE — DAMAGED (RT ENGINE) · airframe 64,101 hrs · 49,921 cycles

PERFORMED AN AIR TURN BACK DUE TO A RIGHT ENGINE COMPRESSOR STALL. THE ENGINE WAS AT IDLE AT TOUCH DOWN. MAINTENANCE REPORTED TURBINE DAMAGE AND THE ENGINE WAS REPLACED.

Part: ATTACH ANGLE — BROKEN (CARGO DOOR) · airframe 63,783 hrs · 49,651 cycles

ON ARRIVAL ATL RAMP REPORTED INSULATION STICKING OUT OF UPPER SIDE OF AFT CARGO DOOR. ON FURTHER INSPECTION FOUND DOOR FRAME TO SKIN ATTACH ANGLE BROKEN WILL NEED REPAIR. REMOVED AFT CARGO DOOR AND BEGAN INST OF NEW DOOR PER AMM 52-31. COMPLETED INSTALLATION OF DOOR PER AMM 52-31.

Part: CLOSEOUT PANEL — MISSING (LT HORIZ STAB) · airframe 63,783 hrs · 49,651 cycles

ON WALKAROUND, FOUND SMALL CLOSEOUT PANEL MISSING FROM LEFT HORIZONTAL STAB NEAR FRONT SPAR INBD BOTTOM AT BARREL NUTS. ASSOCIATED ER/A 14-569512 ADDED FOR AC 9009 PER ERA 569512-14 REV ORIGINAL, SECT II, PERMANENT REPAIR, FABRICATED NEW FILLER PER DWG 5930603. INSTALLED AS REQ THIS IS BEING SDR REPORTED BECAUSE THE PART COULD HAVE POSSIBLY DEPARTED THE AIRCRAFT DURING OPERATION.

Part: BATTERY — INTERMITTENT (CABIN) · airframe 63,680 hrs · 49,562 cycles

SEVERAL OVHD EMER LIGHTS INOP SEAT ROWS 11-16. REMOVED SEVERAL CEILING PANELS TO ACCESS WIRING. FOUND BATTERY PACKS INTERMITTENT. NEEDS BATTERIES(907305). RPLD BATTERIES PER AMM 33-53. ALL EMER LIGHTS NOW CK GOOD. OK FOR SERVICE. REINSTALLED CEILING PANELS.

Part: AILERON — DELAMINATED (RT WING) · airframe 63,680 hrs · 49,562 cycles

RT AILERON LWR TRAILING EDGE DELAMINATION. RIGHT AILERON P/N 5955401-502, S/N 754 REMOVED REF W/C 2710-4124-RH. RIGHT AILERON P/N 5955401-502, S/N 409 INSTALLED PER W/C 2710-4124-RH.

Part: WIRE — BROKEN (CABIN) · airframe 63,680 hrs · 49,562 cycles

FOUND EMER LIGHTS AT SEAT ROWS 11,19,29 INOP. RELAMPED SEATS , NO HELP. FOUND SEAT ROWS 11 AND 29 WIRES BROKEN AT DISCONNECT. RETERMINATED SAME. SEAT HARNESS AT ROW 19 DAMAGED. REPLACED HARNESS. OPS CKS GOOD PER SWPM CHAP 20.

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 63,341 hrs · 49,299 cycles

LEFT ENGINE FIRE LOOP B LIGHT ILLUMINATED AFTER DEPARTURE. ALL OTHER INDICATIONS NORMAL. FOLLOWED QRH NOTIFIED ATL MTC OPS NORMAL REMAINDER OF FLIGHT. INSPECTED LT LOWER PYLON BURN THRU DETECTOR AND FOUND LOOPS RUBBING AGAINST FLUID PIPE. DETECTOR WORN THROUGH HALF WAY. R&R LT ENG PYLON BURN THRU LOWER DETECTOR IAW AMM 26-10. OPS TESTED GOOD.

Part: CONTROL ARM — OUT OF ADJUST (TAILCONE) · airframe 62,632 hrs · 48,738 cycles

TAILCONE DID NOT DEPLOY ON OPS CK. MADE ADJUSTMENT TO THE AFT FUSELAGE CONTROL ARM PER MD88 AMM 53-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,632 hrs · 48,738 cycles

TAILCONE MOUNT POINT PIN/CANTED FRAME IS CRACKED AT 10 OCLOCK POSITION AS VIEWED FROM AFT END. REMOVED DAMAGED LOCATION DRILLED NEW CANTED FRAME READY FOR INSTALL. INSTALLED NEW CANTED FRAME PER BAC DWG 9911843.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 62,632 hrs · 48,738 cycles

RUDDER PACK ROD END SUPPORT BRACKET CRACKED. REMOVED BRACKET AND DRILLED NEW BRACKET REF BAC DWG 9911875. INSTALLED SUPPORT BRACKET PER BAC DWG 9911875.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,559 hrs · 48,689 cycles

TAIL EMERGENCY LIGHTS IN CEILING NOT WORKING. TESTED POWER SUPPLY AND FOUND THE BATTERYS NOT TAKING A CHARGE. REPLACED THE BATTERIES, OPS CHECKED GOOD IAW AMM 33-50.

Part: SWITCH — FAILED · airframe 62,198 hrs · 48,403 cycles

WHEN MOVING THE VOLT/FREQ SELECTOR KNOB IT STARTED SMOKING. THE VOLTS AND FREQ METERS INCREASED A LITTLE THEN DROPPED TO ZERO. THE SMOKE STOPPED. COMPLIED WITH ODI CHECKLIST. INSPECTED ALL WIRING. REPLACED THE SELECTOR SWITCH AND FREQ INDICATOR. CHECKED GOOD IAW AMM 24-00. ACFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (ROW 14) · airframe 61,990 hrs · 48,227 cycles

SEAT ROW 14R EMERGENCY LIGHT DAMAGED. REPLACED THE EMERGENCY LIGHT ASSY. OPS NORMAL.

Part: BRACKET — BROKEN (DOOR OPEN SENSOR) · airframe 61,679 hrs · 47,975 cycles

AFTER TAKE OFF, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. ON APPROACH DOOR LIGHT REMAINED ILLUMINATED. RAN QRH AND SELECTED ALTERNATE GEAR. FOUND RIGHT MLG DOOR OPEN PROXIMITY SENSOR BRACKET BROKEN. REPLACED SENSOR BRACKET. ALL INDICATIONS NORMAL.

Part: SWITCH — NO TEST (TAILCONE) · airframe 60,873 hrs · 47,366 cycles

DURING TAIL CONE RELEASE FUNCTIONAL CHECK, TAIL CONE UNSAFE MESSAGE NOT FUNCTIONAL. HAD NO MESSAGE FROM UPPER SWITCH AND CONTINUES MESSAGE FROM LOWER SWITCH. FOUND BROKEN GROUND WIRE, REPAIRED WIRE IAW WDM 52-73-11. NEW SWITCH WAS INSTALLED ON LOWER BRACKET. OPS TESTED BOTH SWITCHES .

Part: HANDLE — UNKNOWN (TAILCONE) · airframe 60,873 hrs · 47,366 cycles

DURING TAIL CONE RELEASE SYSTEM FUNCTIONAL CHECK, UNABLE TO ROTATE EMERGENCY HANDLE TO THE UNLOCKED POSITION ON AFT ENTRANCE DOOR. INSPECTION COMPLETE.. ER/A 557676-14 REV 0 ISSUED AND COMPLETE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON CHANNEL STA Y= 1510 BTW 4 AND 8 HRS POSITION AT AFT ACC COMPARTMENT. FRAMES (2 EA'S) WERE REPLACED PER DWG 9911843-1 AND -6 AND SRM 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2L AND 3L AND CRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2R AND 3R. CRACKS OF .187" ON SKIN WERE REPAIRED PER ETI 88-16-364 REV 6 AND ER/A 550324-14AD REV ORIGINAL.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

SEVERE CORROSION AROUND LT AFT WINDOW CUTOUT. LT WINDOW RETAINER WAS REPLACED PER DDWG 5644161-1 REV M, SRM 51-10-4, SRM 51-30-5, ER/A 551732-14 REV ORIGINAL AND SRM 51-30-2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB DOUBLER REPAIR. PREVIOUS REPAIR DOUBLER WAS REPLACE PER DC9/MD80 SRM 53-05 FIGURE 123.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION AROUND CUTOUT OF AFT LAVATORY SERVICE ACCESS PANEL. CORROSION WAS FOUND OUT OF LIMITS AND WAS REPAIRED PER ER/A 550350-14 REV ORIGINAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON LONGERON END NR 2 LT/RT STA Y=1418 AT AFT ACC COMPARTMENT. LONGERONS SECTIONS WAS REPLACED PER SRM 53-02 FIGURE 18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON FRAME STA Y=1418 LONG 2 LT/RT SIDE AT AFT ACC. FRAME WAS REPLACED PER SRM 51-10-4, SRM 51-30-5.

Part: PLATE — CRACKED (CARGO DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACK WAS FOUND ON FORWARD CARGO DOOR (C1) AT THE UPPER FWD OF (0.120") STA Y=375". RIVETS WERE REMOVED PER SRM 51-30-2. DAMAGE WAS REMOVED PER SRM 53-05-FIG 105. HFEC WAS ACCOMPLISHED ON FORWARD CARGO DOOR (C1) AT THE UPPER FWD STA Y= 375". NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. PLATE WAS REMOVED PER SRM 51-30-5. REPAIR PARTS WERE FABRICATED PER SRM 53-05 FIG 105. PARTS REPAIR. PLATE AND CONICAL WASHER WERE INSTALLED PER SRM 51-30-5. PERFORM HFEC INSPECTION INITIAL 28,000 CYCLES AND REPETITIVE EVERY 20,000 CYCLES PER SRM 53-05 PARAGRAPH 120 GENERAL NOTE NUMBER 3, PAGE 683.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON CROSSBEAM LT SIDE BELOW TORQUE TUBE AT AFT ACC COMPARTMENT. CROSSBEAM BELOW TORQUE TUBE AT AFT ACC COMPARTMENT WAS REPLACED PER SRM 51-30-5 AND 51-30-2.

Part: SKIN — BENT (CARGO DOOR) · airframe 59,718 hrs · 46,553 cycles

BENT ON PREVIOUS DOUBLER REPAIR AT FWD CARGO DOOR FWD LOWER EDGE C1. THE SKIN WAS REPAIRED IAW ETI -88-16-377 REV 1 AND ERA 550347-14 REV ORIG.

Part: LONGERON SPLICE — CRACKED (BS 1463) · airframe 59,718 hrs · 46,553 cycles

CRACK ON THE LONGERON SPLICE 18L, BS 1463. REPAIRED IAW SRM 53-01 FI. 2 (SHEET 4).

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 59,718 hrs · 46,553 cycles

PUNCTURE ON SKIN RT WING INBOARD FLAP INBOARD VANE. REPAIRED IAW ERA 550339-14 REV.ORIG. AND ETI 88-16-371 REV.2.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 59,718 hrs · 46,553 cycles

CRACKED AND PUNCTURED SKIN AROUND OF FWD AND AFT HOLE XOVIF 53, RT WING INBOARD FLAP OUTBOARD VANE. REPAIRED IAW ERA 550344-14 REV. ORIG. AND ETI 88-16-375 REV. 2.

Part: SKIN — CRACKED (BS 1470) · airframe 59,718 hrs · 46,553 cycles

CRACKED SKIN AND PRODUCTION DOUBLER BS 1470, LONG 23 - 24R. REPAIRED IAW SRM 53-01 FIG 02 AND 53-34.

Part: CARGO TRACK — CORRODED (BS 1007-1225) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION FOUND ON THE LT CARGO TRACK, BS 1007 TO 1225 IN THE AFT CARGO BAY. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1,51-30-2 AND 51-30-5.

Part: FRAME SPLICE — CORRODED (BS 1309) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON FRAME SPLICE BS 1309 BETWEEN LONGERON 27L-27R. ANGLE AND PLATES WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR. 14 AND 21 ANGLE AND PLATES WERE INSTALLED IAW SRM 53-03 D FIG 2A.

Part: SKIN — BULGED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

PROTUBERANCE ON EXTERNAL FUSELAGE SKIN FROM STA Y= 1198 TO Y= 1200 BTW LONG 4 LT TO 5 LT 3EAS. PROTUBERANCE ON EXTERNAL FUSELAGE SKIN FROM STA Y= 1198 TO Y=1200 BTW LONG 4 LT TO 5 LT (3EAS), WAS REPAIRED PER SRM 53-04-3 FIGURE 11 SHEET 1. PERFORM GENERAL VISUAL INSPECTION INITIAL 8,000 CYCLES AND REPETITIVE EVERY 8,000 CYCLES PER SRM 53-04-3 PAG 8A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON LONG 3 STA Y=1437 AT AFT ACC COMPARTMENT RT SIDE. LONGERON WAS REPAIRED PER SRM 53-02 FIG 18.

Part: STRINGER — CRACKED (RT WING) · airframe 59,718 hrs · 46,553 cycles

CRACK OF 2.5"APROX ON STRINGER 17 RT INSIDE FUEL TANK AT XCW=12.0. STRINGER 17 WAS REPAIRED PER ER/A 550338-14 REV ORIGINAL AND ER/A 550337-14 REV ORIGINAL.

Part: STRINGER — CRACKED (LT WING) · airframe 59,718 hrs · 46,553 cycles

CRACK OF 0.500" WAS FOUND ON STRINGER 11, OUTBD SIDE AT THE OUTBD FLAP, INBD DRIVE HINGE AT STA XRS=164, LT WING. STRINGER WAS REPAIRED PER SERVICE REWORK (SR09570100 REVB) AND CARD 5712-01030-03 SECTION 03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON RT CUSP WEB BTW Y=845 TO Y=864, Y=864 TO Y =886, Y=886TO Y=905, X=44-X=60 AT CABIN FLOOR STRUCTURE UPPER AND LOWER FACE. CUSP WEB RT STA Y=845 TO Y=905 WAS REPLACED PER SRM 51-30-1, 51-30-2, 51-30-5, 53-05 FIG 131A-24 AND 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON LT CUSP WEB BTW Y=845 TO Y=864,Y=864 TO Y=886, Y=886 TO Y=905, X=44-X=60 AT CABIN FLOOR STRUCTURE, UPPER AND LOWER SURFACE. CUSP WEB WAS REPLACED PER SRM 53-05 FIG 131A-7.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 59,718 hrs · 46,553 cycles

DENTS AND SCRATCHES ON RT ANTI-FLOAT TAB SKIN P/N 5930497-502 53344. RT ANTI-FLOAT TAB SKIN WAS REPAIRED PER SRM 55-04 PAR 2 C3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACKED LONGERON 24R STA Y=200 AT E&E COMPARTMENT. LONGERON WAS REPAIRED PER SRM 53-02 FIGURE 18.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON LT AFT EMERGENCY EXIT DOOR JAMB UPPER AREA. CRACK (0.843") ON DOOR JAMB WAS REPAIRED PER SRM 53-05 FIG 32.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON RT CUSP WEB BTW Y=826 TO Y=845 X=44-X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A-10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACK ON WEB OF FRAME STA Y = 1437 RT SIDE 2 HRS POSITION AT AFT ACC COMPARTMENT. WEB WAS REPAIRED PER SRM 51-70-4 FIG1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

CRACKED LT CUSP WEB X=59 STA Y=816 AT PAX CABIN FLOOR STRUCTURE. WEB WAS REPAIRED PER SRM 53-05 FIG 131A.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON AFT BULKHEAD DOOR JAMB LOWER SECTION UPPER AND LOWER SURFACE. DOOR JAMB WAS REPAIRED PER SRM 53-05 PAR 45 FIGURE 34.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB FROM STA 1071 TO 1074 BTW X -54 AND -60. WEB WAS REPAIRED PER SRM 53-05 FIG 131A-13.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 59,718 hrs · 46,553 cycles

DELAMINATION ON UPPER SKIN APPROX STA XOVIF= 97 AT LT WING INBOARD FLAP OUTBOARD VANE. LT WING INBOARD FLAP OUTBOARD VANE WAS REPAIRED BY SRM 57-03D PAR 11.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

PUNCTURED LT CUSP WEB Y=1007 BTW X=44 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS FABRICATED AND REPLACED PER SRM 53-05 FIGURE 131A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON RT CUSP WEB BTW X= -54 TO X= -60 FROM Y= 503 TO Y= 598 AT PAX CABIN. CUSP WEB WAS REPLACED PER SRM 51-10-4, 51-30-1, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACKED INNER PAN ON FWD EDGE BTW BEAM 2 AND 3 AT FWD SERVICE DOOR INNER STRUCTURE. REPAIR DOUBLER WERE REPLACED PER ERA 487761-14 REV A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,718 hrs · 46,553 cycles

OUT OF LIMITS RT TIE TRACK FROM STA Y=1007 TO STA Y=1155 C3. NEW TIE TRACK WAS REPLACED PER SRM 51-10-4 2. HOLES TREATED AND PAINTED SRM 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 710-728) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB X -54 TO -60 BETWEEN BS 710 - 728. REPAIRED IAW SRM 51-30-2,51-30-3, 51-30-1,53-05 FIG. 131A-7 , 51-10-3 PAR. 21,14 AND 38.

Part: PAN — CRACKED (PAX DOORWAY) · airframe 59,718 hrs · 46,553 cycles

CRACKED INNER PAN ON FWD UPPER CORNER AREA AT MAIN ENTRANCE DOOR INNER STRUCTURE. THE PAN WAS REPAIRED IAW SRM 52-05 FIG. 18A.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 59,718 hrs · 46,553 cycles

CRACK ON INTERCOSTAL BS 1287 - 1307, X 0. THE INTERCOSTAL WAS REPAIRED IAW ER/A 380524-14 MA REV. ORIG. AND SRM 51-30-5.

Part: DOUBLER — CORRODED (BS 1174-1212) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON DOUBLERS BETWEEN BS 1174 AND 1212, X 54-60. REPLACED THE DOUBLERS IAW SRM 53-05 FIG.131A-8 AND SRM 51-30-5.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACKED AFT END OF BEAM 1 AT THE FWD SERVICE DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-2.

Part: SKIN — CRACKED (PAX DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACKED OUTER SKIN AT THE PAX DOOR. THE SKIN WAS REPAIRED IAW ERA 486216-14 MA REV A.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON PREVIOUS REPAIR PARTS OF LT CUSP WEB BETWEEN BS 598 - 617, X=44-X=60 . REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05 FIG 131A-24.

Part: BEAM — CRACKED (PAX DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON BEAM NR 8 ON THE INNER STRUCTURE OF THE PAX DOOR. REPAIRED IAW SRM DWG 9955759 REV. P.

Part: CUSP WEB — CORRODED (BS 598-610) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION OUT LIMITS ON RT CUSP WEB X -54 TO -60, BS 598 - 610. REPAIRED IAW SRM 53-05 FIG 131A-14.

Part: FLOOR SUPPORT — CRACKED (CABIN) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CRACK AND CORROSION ON FLOOR SUPPORT. REPAIRED IAW SRM 53-05 FIGURE 131 B.

Part: LONGERON — CRACKED (BS 1338) · airframe 59,718 hrs · 46,553 cycles

CRACKED LONGERON BS 1338, LONGERON 1. LONGERON REPLACED IAW SRM 53-14-3 FIGURE 4, 51-10-3 PAR 14,21, 51-30-5, 51-10-2A, AND 51-10-2.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,718 hrs · 46,553 cycles

FLOOR PANEL DAMAGED. REPLACED THE FLOOR PANEL IAW AMM 53-20- 01-201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,718 hrs · 46,553 cycles

FLOOR PANEL DAMAGED. REPAIRED IAW AMM 25-00-00-801

Part: LONGERON — CRACKED (BS 1437) · airframe 59,718 hrs · 46,553 cycles

CRACKED LONGERON 16R BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4 FIG 4, 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 59,718 hrs · 46,553 cycles

CRACK ON LONGERON 16L BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4 FIG 4,51-30-2 AND 51-30-5.

Part: DOOR FRAME — CRACKED (BS 200-210) · airframe 59,718 hrs · 46,553 cycles

CRACK ON WEB AT L1 DOOR FRAME STRUCTURE BTWEEN BS 200 AND 210, LONGERON 11L. WEB REPAIRED IAW SRM 53-05 FIG 143.

Part: CUSP WEB — CORRODED (BS 712-737) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON LT CUSP WEB BS 712 - 737, X 54 - 60. REPAIRED IAW SRM 53-05 FIG. 131A-13 (SHEET 1) AND 53-05 FIG. 131A-13 (SHEET 5).

Part: CUSP WEB — CORRODED (BS 503-522) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 503 TO 522 , X 44 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A.

Part: FLOOR PANEL — PUNCTURED · airframe 59,718 hrs · 46,553 cycles

FLOOR PANEL PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW AMM 53-20-01-201.

Part: ANGLE — CRACKED · airframe 59,718 hrs · 46,553 cycles

CRACKED ANGLE ON BEAM 1 AT FWD SERVICE DOOR INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9911581 REV. U.

Part: TEE FITTING — CORRODED (BS 1380) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION FOUND ON THE TEE ANGLE BS 1380 AND LONGERONS 24L TO 24R. THE TEE WAS REPLACED PER DC9/MD80 DWG 9912246-115. (LP2721089)

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,718 hrs · 46,553 cycles

CRACK ON PAN, AFT EDGE BETWEEN BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 52-05 FIG. 26A, SRM 51-30-2 AND SRM 51-30-5.

Part: LONGERON — CRACKED (BS 541) · airframe 59,718 hrs · 46,553 cycles

CRACKED LONGERON 4R BS 541. LONGERON WAS REPAIRED IAW SRM 53-02 FIGURE 18,51-30-5, 51-30-2, 51-10-3 PAR 14, 21,51-30-1.

Part: INTERCOSTAL — CRACKED (BS 1174) · airframe 59,718 hrs · 46,553 cycles

CRACKS ON INTERNAL STRUCTURE LOWER SECTION BS 1174 ON INTERCOSTAL, REPAIRED IAW SRM 52-03D FIG.8, 51-30-1, 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 59,718 hrs · 46,553 cycles

ELONGATED HOLES ON FUEL ACCESS PANEL 1436. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON PREVIOUS REPAIR OF LT CUSP WEB BTW BS 541 TO 560, X 44 - X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-7.

Part: FLOOR PANEL — BROKEN (COCKPIT) · airframe 59,718 hrs · 46,553 cycles

BROKEN COCKPIT FLOOR PANEL 120E. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — DAMAGED (RT WING) · airframe 59,718 hrs · 46,553 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT RT WING. REPAIRED IAW ER/A 550332-14AD REV.ORIGINAL.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON LT CUSP WEB BTW BS 446 - 465 BTW X 54-60 AT PAX CABIN. REPAIR INSTALLED SRM 53-05 FIG.131A-13.

Part: SPAR — DAMAGED (LT WING) · airframe 59,718 hrs · 46,553 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT L WING. REPAIRED IAW ER/A 550332-14AD REV.ORIGINAL.

Part: DOUBLER — WORN · airframe 59,718 hrs · 46,553 cycles

WEAR ON TITANIUM DOUBLER AT AFT LAV SERVICE PANEL AREA. TITANIUM DOUBLER WAS FABRICATED IAW DWG 5911423 REV. CD. 2, TITANIUM DOUBLER WAS PAINTED IAW SRM 51-10-3 PAR 14.

Part: PAN — CRACKED (BS 886-905) · airframe 59,718 hrs · 46,553 cycles

CRACKED RT WINDOW RING PAN AFT LOWER CORNER BETWEEN BS 886 TO 905. RING PAN WAS REPAIRED IAW SRM 53-05 FIG. 122.

Part: TAB — DENTED (LT ELEVATOR) · airframe 59,718 hrs · 46,553 cycles

SEVERAL DENTS ON LT ELEVATOR GEARED TAB UPPER SURFACE. GEARED TAB WAS REPLACED IAW SRM 55-04 PAR 2.

Part: TAB — DENTED (RT ELEVATOR) · airframe 59,718 hrs · 46,553 cycles

SEVERAL DENTS ALONG UPPER SURFACE OF THE RT ELEVATOR ANTI-FLOAT TAB. THE TAB WAS REPLACED IAW WORK CARD 2730-4832.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 59,718 hrs · 46,553 cycles

SEVERAL DENTS ALONG UPPER SURFACE OF RT ELEVATOR GEARED TAB. DENTS ON RH ELEVATOR GEARED TAB ARE OUT OF LIMITS FOR REPAIR IAW SRM 55-04 PAR 2. DUE TO SEVERAL DENTS THE RH ELEVATOR GEARED TAB WAS REPLACED IAW SRM 55-04 PAR 2 AND INSTALLATION IS ACCOMPLISHED UNDER CARD 2730-4832.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 59,718 hrs · 46,553 cycles

DELAMINATION ON LOWER SKIN BETWEEN XV2=214-226 AT LT WING OUTBOARD FLAP CENTER VANE. CENTER VANE REPLACED IAW SRM 57-03D PAR. 11.

Part: PAN — CRACKED (BS 807-826) · airframe 59,718 hrs · 46,553 cycles

CRACKED RT WINDOW RING PAN FWD/UPPER CORNER BTW BS 807 TO 826. PAN WAS REPAIRED IAW SRM 53-05 FIG122.

Part: PAN — CRACKED · airframe 59,718 hrs · 46,553 cycles

CRACK ON LT WINDOW RING PAN FWD UPPER CORNER BTW BS 674 & 693, 750 & 769, 1022 & 1041, 1041 & 1060. REPAIRED IAW SRM 53-05 FIGURE 122 AND ER/A 493648-14MA REV. A.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 59,718 hrs · 46,553 cycles

CORROSION ON ATTACH POINT INTERNAL STRUCTURE XV2=245 AT RT WING OUTBOARD FLAP CENTER VANE. REPLACED IAW AMM 27-51-03.

Part: TAB — DENTED (RT ELEVATOR) · airframe 59,718 hrs · 46,553 cycles

SEVERAL DENTS ALONG UPPER SURFACE OF RT ELEVATOR CONTROL TAB. DENTS OF ELEVATOR CONTROL TAB ARE OUT OF LIMITS FOR REPAIR IAW SRM 51-50-2. RT ELEVTOR CONTROL TAB WAS REPLACED AND INSTALLATION IS ACCOMPLISHED UNDER CARD 2730-4832 JOB 001-0234.

Part: TAB — DENTED (LT ELEVATOR) · airframe 59,718 hrs · 46,553 cycles

SEVERAL DENTS ALONG UPPER SURFACE OF LT ELEVATOR CONTROL TAB. THE CONTROL TAB WAS REPLACED.

Part: DOOR — DAMAGED (FUEL) · airframe 58,723 hrs · 45,760 cycles

FUELING DOOR FOUND OPEN AND RIPPED AT STRUT. R & R REFUEL DOOR. OK FOR SERVICE.

Part: CABLE — OBSTRUCTED (TAILCONE) · airframe 58,050 hrs · 45,267 cycles

MAINTENANCE FOUND THE TAILCONE FRAME INTERFERING WITH A RELEASE CAM. THE TAILCONE RING WAS ROUTED AND A DOUBLER WAS INSTALLED IAW DWG 991157.

Part: CABLE — WORN (TAILCONE) · airframe 58,050 hrs · 45,267 cycles

MAINTENANCE FOUND A TAILCONE CABLE WORN AT THE LOOP END. THE CABLE WAS REPLACED IAW AMM 53-53.

Part: SKIN — GOUGED (FUSELAGE) · airframe 60,486 hrs · 47,075 cycles

FUSELAGE SKIN L-1 PASSENGER DOOR DENT AND GOUGE. REPAIRED PER ERA 532474-14.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 57,719 hrs · 45,037 cycles

RT HORIZONTAL STABILIZER UPPER RT AFT SKIN PANEL SHOWS A CRACK INDICATION IAW NDTSPM 06-10-02.005 AND AMDS, AA 5510-01074-11. VERIFIED CRACK INDICATION IAW NDTSPM 06-00-07. INDICATION MEASURES APPROXIMATELY .5". ACCOMPLISHED SECTION 1 OF ERA 542476-14AD, REV "O". IDENTIFIED REPAIR AS TIME LIMITED IAW PS 900-5-1, NR 4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,246 hrs · 43,978 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE FWD OVERWING EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: SKIN — DENTED (BS 200) · airframe 55,287 hrs · 43,348 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AFT OF THE L1 PASSENGER DOOR CUTOUT BS 200 STRINGER 17L. REPAIRED IAW PRI 532474-14 REV.A REV 0,1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,620 hrs · 42,845 cycles

DURING CHECK, MAINTENANCE FOUND THE SEAT EMERGENCY LIGHT AT SEAT 11D WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMPS FOR BOTH SEAT EMERGENCY LIGHTS AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,620 hrs · 42,845 cycles

DURING CHECK, MAINTENANCE FOUND THE FIRST 3 ROWS OF CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN CHARGER B5-100 AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 31DE) · airframe 54,311 hrs · 42,616 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 31DE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: PAN — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 54,240 hrs · 42,556 cycles

AFT CARGO DOOR THRESHOLD LOWER PAN HAS CORROSION ON OTBD FACE. CORROSION AFT PIT SPACER FOUND TO BE OUT OF LIMITS IAW D88, SRM 53-01, FIG 1. REMOVED EXISTING SPACER IAW SRM 51-30-05. FABRICATED NEW SPACER 7075, T6, .071, PO ST00001251 DIM 2" X 53" LOCATED & DRILLED SPACER IAW MD-88 51-10-4. ALODINED SPACER IAW SRM 51-10-3, PAR 21. PRIMED SPACER IAW SRM 51-10-3, PAR 14 INSTALLED SPACER IAW 51-30-05 + 51-30-07, 53-05.

Part: DOOR FRAME — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 54,240 hrs · 42,556 cycles

FWD CARGO DOOR FRAME AFT WEB CORRODED, REMOVED CORROSION AND FOUND OUT OF LIMITS. CUT OUT DAMAGED, FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER AREA. INSTALLED DOUBLER IAW SRM 51-10-03, 53-01 FIG 1, 53-01 FIG 2, 53-10-2 FIG 2.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 53,877 hrs · 42,293 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATH LIGHT WAS OUT AT SEAT 28. MAINTENANCE FOUND A LOOSE HARNESS AND RECONNECTED THE HARNESS AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,566 hrs · 41,409 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 24 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPS CHECK WAS GOOD.

Part: CABLE — WORN (TAILCONE) · airframe 50,584 hrs · 39,965 cycles

DURING CHECK, KEVLAR CABLE ON TAILCONE FOUND WORN. R & R KEVLAR CABLE IAW MM 53-53-00.

Part: CABLE — OUT OF LIMITS (TAIL CONE) · airframe 50,584 hrs · 39,965 cycles

DURING CHECK, CABLE BLOCK FOUND OUT OF LIMITS ON TAILCONE. R & R CLAMPS AND ADJUSTED CLEARANCE BETWEEN BLOCK AND CONDUIT IAW MM 53-53-00.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 50,584 hrs · 39,965 cycles

DURING CHECK, MX FOUND TAILCONE LATCH RECEPTACLES WORN. R & R RT & LT RECEPTICLES IAW AMM 53-53-00.

Part: BRACKET — WORN (TAILCONE) · airframe 50,584 hrs · 39,965 cycles

DURING SERVICE CHECK, KEVLAR SPRING BRACKET WORN ON RT SIDE OF TAILCONE. R & R BOTH BRACKETS IAW SRM 51-30-02.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 50,434 hrs · 39,866 cycles

PIN RECEPTACLES WORN ON AFT FLANGE OF TAILCONE. R & R WORN PIN RECEPTACLES ON TAILCONE IAW SRM 51-30-02.

Part: BLOCK — WORN (TAILCONE) · airframe 50,458 hrs · 39,883 cycles

DURING CHECK, SLIDING BLOCK WORN. UPPER LT SIDE TAILCONE. R & R SLIDING BLOCK IAW AMM. RIG COMPLIED WITH.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,579 hrs · 39,300 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHT ON DROP DOWN PANEL FOR COALESCER BAGS INOPERATIVE. R & R BATTERY PACK IAW AMM. OPS CHECKED GOOD.

Part: GIRT BAR — DAMAGED (L2 DOOR SLIDE) · airframe 49,197 hrs · 39,017 cycles

GIRT BAR DOOR 2L DOES NOT STAY SECURED TO FLOOR. REPLACED GIRT BAR.

Part: RELEASE CABLE — OUT OF LIMITS (TAILCONE) · airframe 48,492 hrs · 38,526 cycles

WHILE PERFORMING INTERNAL RELEASE OF TAILCONE, PULL FORCE WAS LOW, 17LBS. ADJUSTED TAILCONE LATCHES PER AMM. PULL FORCE WITHIN LIMITS, 31 LBS. OPERATION CHECKS GOOD. OKAY FOR SERVICE.

Part: PIN — WORN (TAILCONE) · airframe 48,492 hrs · 38,526 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM FOUND EXCESSIVE WEAR ON PIN ASSEMBLY FITTING. REMOVED AND REPLACED PIN PER AMM. OPERATION CHECKS GOOD. OKAY FOR SERVICE.

Part: PIN — BACKED OUT (EMERGENCY LIGHT) · airframe 48,368 hrs · 38,446 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND SEAT 16DE EMERGENCY ESCAPE PATHWAY LIGHT INOPERATIVE. MAINTENANCE FOUND HARNESS PLUG WITH PUSHED BACK PIN. SECURED PIN. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 47,619 hrs · 37,959 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 14DE IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR IN THE SEAT TO WALL WIRE HARNESS BROKEN. MCO/PLC PER MEL 33-00-24.

Part: WIRE — BROKEN (CABIN) · airframe 45,493 hrs · 36,475 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE AT ROW 20 D/E. MAINTENANCE REPAIRED THE BROKEN WIRE AT THE UNDER-SEAT CONNECTOR. THE SYSTEM RETURNEDTO NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN) · airframe 45,383 hrs · 36,394 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE AT ROW 27D/E. MAINTENANCE REPAIRED THE BROKEN WIRE AT THE UNDER SEAT CONNECTOR. THE SYSTEM RETURNEDTO NORMAL OPERATION. (2011-D0140)

Part: SKIN — DENTED (BS 229 S18L) · airframe 45,382 hrs · 36,393 cycles

FOUND DENT DURING WALKAROUND, LOCATED AFT OF 6 INCHES AFT OF STA 229 AND 3 INCHES ABOVE STR 18L. COMPLETED REPAIR IAW ERA 475850-14, REV A.

Part: SKIN — DAMAGED (BS 218-227) · airframe 45,125 hrs · 36,224 cycles

IMPROPER RIVETS AND DOUBLER DAMGED ON FUSE SKIN REPAIR STA 218-227, L16L AND 18L. EXTERNAL AND INSTERNAL DOUBLERS WERE R & R IAW SRM 53-04D, FIG 12C.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 45,125 hrs · 36,224 cycles

ELONGATED HOLES ON MID CARGO COMPARTMENT LWR DOOR JAMB. DAMAGE CUTOUT AND REPAIRED IAW SRM53-05, FIG 12B.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 45,125 hrs · 36,224 cycles

CORROSION ON AFT CARGO LOWER DOOR JAMB BELOW PREVIOUS REPAIR DOUBLERS. CORROSION WAS REMOVED. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 123.

Part: SKIN — DENTED (BS 234-244) · airframe 45,125 hrs · 36,224 cycles

MISSING ID TAG ON PREVIOUS REPAIR DOUBLER STA Y-234-244, BTWN LONG 19R AND 22R. PORTUDING DENT ABOVE REPAIR DOUBLER. PREVIOUS REPAIR DOUBLER WAS R & R IAW SRM 53-04D, FIG 12B. DENT WAS ELIMINATED BY CUTOUT.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 45,125 hrs · 36,224 cycles

CORROSION ON RT MLG SUPPORT FITTING BORE. CORROSION WAS REMOVED AND BUSHING INSTALLED IAW ERA 487764-14AD.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 44,827 hrs · 36,017 cycles

VERTICAL STABILIZER/ LOWER FIXED L/E PANEL/ UPPER EDGE/ ZFS52/ HOLE DAMAGE. REPAIRED IAW ER/A 485868-14.

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 44,827 hrs · 36,017 cycles

C-3 THRESHOLD CORRODED. REPAIRED IAW SRM 53-05, FIG 123.

Part: LIGHT — MISSING (CABIN) · airframe 44,240 hrs · 35,660 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT ROW 3C MISSING. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OF LIGHT NOW CHECKS GOOD (2010-D0812)(DLM88101773).

Part: B-NUT — LEAKING (HYD LINE) · airframe 44,014 hrs · 35,493 cycles

DURING PHASE OF FLIGHT F/A'S NOTICED BURNED SMELL BY AFT GALLEY. CREW TURNED PACKS OFF AND ON TO DISSIPATE SMELL. ACTION DIDN'T MAKE DIFFERENCE IN SMELL. ONCE ON GROUND, MX INSPECTED AFT GALLEY AND AFT LAVATORIES NO TROUBLE FOUND. ON CONTROL NR C06050773, OPN 5088 TROUBLESHOT SMOKE IN CABIN, FOUND SMELL ORIGINATING FROM COFFEE MAKERS ALSO NOTICED HYD SMELL IN MID CABIN. FOUND B-NUT ON LT SIDE ACTUATOR LEAKING. A DUCT BURN OUT OPN 7904 AND COALESCER BAGS WERE REPLACED. (DLM88101447) (2010-D0659)

Part: COFFEEMAKER — ODOR (CABIN) · airframe 44,014 hrs · 35,493 cycles

DURING PHASE OF FLIGHT F/A'S NOTICED BURNED ODOR BY AFT GALLEY. CREW TURNED PACKS OFF AND ON TO DISSIPATE ODOR. ACTION DIDN'T MAKE DIFFERENCE IN ODOR ONCE ON GROUND MX INSPECTED AFT GALLEY AND AFT LAVATORIES NO TROUBLE FOUND. ON CONTROL NR C06050773, OPN 5088, TROUBLESHOT SMOKE IN CABIN FOUND ODOR ORIGINATING FROM COFFEE MAKERS ALSO NOTICED HYD ODOR IN MID CABIN. FOUND B-NUT ON LT SIDE ACTUATOR LEAKING. A DUCT BURNOUT OPN 7904 AND COALESCER BAGS WERE REPLACED. (DLM88101447)

Part: SKIN — DENTED (FUSELAGE) · airframe 41,743 hrs · 34,015 cycles

FUSELAGE SKIN FS 229-240 LONGERON 17L DENT AND PUNCTURE. PERFORMED REPAIR PER ERA 475850-14 REV 0 CODE 9-53-31-20.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 41,180 hrs · 33,651 cycles

LT HORIZONTAL STAB UPPER AFT SPAR CRACKED AT INBD END.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,479 hrs · 29,481 cycles

DURING LETTER CHECK, THE RHS HORIZONTAL STABILIZER UPPER AFT SKIN PANEL WAS FOUND CRACKED AT THE INBOARD AFT END. THE PART WAS REPLACED PER BOEING RECOMMENDATION AS NO FEASIBLE REPAIR CURRENTLY EXISTS. DOCUMENTED ON ER/A 460015-14.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 36,913 hrs · 28,792 cycles

DURING APPROACH INTO LGA 5000 FT SLOWING TO 170 KTS FLAPS 15THE NR 2 ENGINE RACED TO MAX EGT NEAR 660C, N1 OVER 102 PERCENT ALL PARAMETERS EXCEEDED. SHUTDOWN RT ENGINE. DID NOT PULL FIRE HANDLE. NORMAL SHUTDOWN AND DECLARED EMERGENCY. REPLACED NR 2 ENG IAW ROUTINE TRANSMITTAL.

Part: STARTER — FAILED (APU) · airframe 33,888 hrs · 25,939 cycles

WHILE WORKING AN MCO FOR AN APU REPORT TO NOT START, IT WAS FOUND THAT THE APU STARTER HAD EITHER BURNT, OVERHEATED OR CAUGHT FIRE. THE STARTER CABLES WERE BURNT, AS WERE THE GENERATOR CABLES. THE STARTER ITSELF WAS CHARRED AND DISCOLORED, AS WAS NUMEROUS WIRES AND WIRING HARNESSES. REPLACED STARTER, CABLES, BATTERY CONTACTOR, AND AUX POWER RELAYS

Part: SKIN — DENTED (FUSELAGE) · airframe 33,134 hrs · 25,416 cycles

FUSELAGE SKIN REPAIR DENTED AT STATION 229 AND LONGERON 17L. REPAIRED IAW ERA 385592-14 REV A.

Part: HEATER — INOPERATIVE (RUDDER PITOT) · airframe 32,852 hrs · 25,222 cycles

PITOT/STALL HEAT OFF LIGHT ON ANNC PANEL WITH NO CURRENT GOING TO RUDDER LIMITER. REPLACED PITOT TUBE.

Part: RACK — MALFUNCTIONED (BATTERY PACK) · airframe 31,719 hrs · 24,373 cycles

OVERWING EMERGENCY LIGHTS WOULD NOT SHUT OFF AFTER TEST.REPLACED BATTERY PACK RACK UNIT. OPS NORMAL

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,467 hrs · 23,509 cycles

INSPECTION OF A BLENDED GOUGE AND DENT AREA BETWEEN FS 1231 & FS 1265 AND BETWEEN STRINGERS 21R & 22R REVEALED A 6 INCH CRACK. THE CRACK AND BLENDED SKIN AREA WAS REMOVED WITH A 37 X 8.5 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER PER THE MD-88 SRM AND PER ER/A 087782-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,465 hrs · 23,508 cycles

A 6 INCH CRACK IN FUSELAGE SKIN AT PREVIOUS GOUGE BLEND REPAIR FS 1236 TO FS 1242 BETWEEN LONGERONS 22R AND 23R. REPAIRED SAME.

Part: POWER SUPPLY — DEFECTIVE (CARGO BAY) · airframe 29,907 hrs · 23,116 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHTS WILL NOT COME ON WHEN SELECTED FROM THE COCKPIT. OPS NORMAL FROM FLIGHT ATTENDANT PANEL. FOUND VOLTAGE BEING INDUCED ON TB 53-18 BLOCK 2. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY. SYSTEM OPS NORMAL.

Part: ANGLE — CRACKED (FS 1474) · airframe 28,424 hrs · 22,086 cycles

FUSELAGE / VERTICAL STAB TO FUSELAGE ATTACH ANGLE : CRACK REPAIR THE LH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN THE HORIZONTAL FLANGE AT CANT STA 1474. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384458-14, REV A.

Part: BRAKE ASSY — LOCKED (NR 2) · airframe 27,841 hrs · 21,655 cycles

NR 2 BRAKE LOCKED ON LANDING. REPLACED BRAKE

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 26,113 hrs · 20,412 cycles

APPROX 20 MINUTES INTO FLIGHT WHILE CRUISING FL290 MASTER CAUTION ILLUMINATED W/L HYD PRESS LOW LIGHT ON. ANNUNCIATOR PANEL HYDRAULIC PRESSURE WAS ZERO AND QTY WAS DOWN TO 2 QTS. RAN APPROPRIATE CHECKLISTS (SHUTTING OFF THE L ENG HYD PUMP), PRESSURE STAYED AT ZERO AND QTY CAME BACK TO 7 QTS. CHECKED LT ENG PUMP CASE DRAIN FILTER DUE LOW HYD QTY. FILTER CHECKS NORMAL. REPLACED LT ENG PUMP CASE DRAIN FILTER. REPLACED LINES AT LT PRESS/CASE RETURN MOD. PRESSURE CHECKS GOOD LEAK CHECK GOOD.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 24,713 hrs · 19,315 cycles

AFT GALLEY OUTBOARD COFFEEMAKER PRODUCED ELECTRICAL SMOKE. PULLED C/B. REPLACED DISPENSER. NEW UNIT CKS OK AND DOES NOT PRODUCE ANY ABNORMAL ODORS AFTER 30 MINS OPERATION.

Part: CLAMP — BROKEN (NR 1 ENGINE) · airframe 24,534 hrs · 19,187 cycles

ON INITIAL APPROACH THE LEFT ENGINE FIRE WARNING BOTH A AND B LOOPS ILLUMINATED. WARNING CEASED WHEN THROTTLE PULLED BACK TO IDLE. FOUND HIGH STAGE BLEED CLAMP BROKEN. REPLACED SAME.

Part: CONTROL VALVE — FAULTY (A/C BAY) · airframe 24,409 hrs · 19,094 cycles

AT 31,000 FT RT PACK AIR STUCK IN COLD POSITION, WOULD NOT MOVE. LEFT PACK SUPPLY PRESS DROPPED TO ZERO MOMENTARILY CAUSING CABIN ALT TO CLIMB. DESCEND TO 10,000 FT AND IT HAPPENED AGAIN. ATL MCC 2100Z. FOUND RT PACK MIX VALVE STICKING. REPLACED RT PACK TEMP CONTROL VALVE. RT PACK OPS AND LEAK CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,518 hrs · 17,753 cycles

AT 20 MINS OF CLIMB POWER WITH ENG ANTI-ICE IN USE FOR 10 MINS. THERE WAS REPORT OF FUMES IN CABIN. SMOKE ALARM SOUNDED FROM AFT LAV. FUMES CLEARED QUICKLY. PERFORM OPN 5088 AND DUCT BURN OUT.

Part: HOUSING — CRACKED (MEGAPHONE) · airframe 22,237 hrs · 17,546 cycles

MEGAPHONE BATTERY HOUSING CRACKED. REPLACED MEGAPHONE.

Part: FAN SEIZED (AFT)

ATL WORKING APU INOP FROM BURNING SMELL IN CABIN AT BTR. REF LOG C042035 ITEM 002. WHILE WORKING WRITEUP, FOUND AFT RECIRCULATION FAN BEARINGS GONE AND FAN SEIZED. SMELL CAME FROM FAN AT LIFTOFF IN BTR. AIR TURNBACK BTR. REPLACED FAN.

Part: TIRE — FAILED (MLG)

AT ROTATION SPEED, ENCOUNTERED AN UNSAFE GEAR INDICATION ON THE RIGHT MAIN LANDING GEAR. LEFT THE GEAR DOWN AND WENT THROUGH ALL APPLICABLE CHECKLISTS PER POM. NUMBER 3 TIRE SHED RETREAD AND DAMAGED PROX SWITCH AND CONDUIT. REPLACED SAME.

Part: PBE — PIN POPPED (CABIN)

PBE ON F/C BULKHEAD CAPTAIN'S SIDE INDICATOR PIN EXTENDED. REPLACED PBE.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AND RIGHT EMERGENCY EXIT LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK, SYSTEM CHECKS NORMAL.