N913DL

Part: TERMINAL — BURNED (GENERATOR) · airframe 82,874 hrs · 63,832 cycles

SDR REPORTED DUE TO EMERGENCY DECLARED PER MCC NOTIFICATION - ON DESCENT / APPROACH A/P AND A/T DISCONNECTED WITH MULTIPLE OAP LIGHTS AND LOTS OF CA / FO FLT / NAV INSTRUMENTATION - LT GEN OFF AND LT AC BUS MULTIPLE ASSOCIATED LIGHTS - RAN QRH GEN OFF PROCEDURES WITH SUCCESSFUL RESET. THEN SAME ISSUE REOCCURRED WITH IN 3 MINS. T/S PER MD88 AMM 2421 CHECKED FOR PYLON PLUG SECURITY CHECKS OK. FOUND POSSIBLE SHORT ON LOCKOUT SWITCH. REPLACED SAME. RAN ENGINES COULD NOT DUPLICATE. FOUND TERMINAL T3 & TERMINAL END BURNED AT GENERATOR. REPLACED LT ENG GENERATOR & FEEDER CABLE HARNESS PER MD88 AMM 24-20. NEEDS ENG RUN. RAN ENGINE & LOADED GENERATOR. OPS NORMAL WITH GOOD VOLTS AND FREQS. REMOVED MCO AND PLACARD. (LP6658092)

Part: GCU — FAILED (LT GENERATOR) · airframe 82,874 hrs · 63,832 cycles

DURING DESCENT PASSING 9000 FT, LOST THE LEFT GENERATOR, NO FURTHER ACTION TAKEN. REMOVED AND REPLACED THE LT GEN CONTROL IAW AMM 24-20. OPS CHECKS GOOD .

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,398 hrs · 63,373 cycles

ROW 25 OVERWING EMERGENCY EXIT SIGNS INOP. REPL BATTERY PACK PER AMM 33-53. OPS CHECK GOOD. (LP5597571)

Part: GAUGE — FAILED (NR 1) · airframe 82,266 hrs · 63,266 cycles

CREW LOST THE LT GENERATOR WHILE THE RT GENERATOR WAS ALREADY ON MEL. REPLACED LT ENG. GENERATOR, CSD, AND OIL COOLER. FLUSHED OIL LINES AND SERVICED CSD. FOUND # 1 PMG C/B POPPED ON # 1 GCU. REPLACED GCU. OPN CKS AND LEAK CKS OK. (LP5595378)

Part: TERMINAL BLOCK — BURNED (COCKPIT) · airframe 81,250 hrs · 62,372 cycles

BEFORE PUSHBACK EXT. PWR WAS PULLED. ALL ELECT POWER REMOVED FROM JET. RESTORED EXT PER. AFTER PUSH, BEGINNING TAXI, GALLEY PER SHREDDED. STRONG ELECTRICAL SMELL OBSERVED FROM CB PANEL BEHIND CAPTAINS SEAT. NO SMOKE OBSERVED. FOUND TERMINAL BLOCK S3-263 BURNED. REMOVED S3-263. REMOVED CROSSFIRE RELAY R2-45. REMOVED WIRES 1X151B4A, 1X15ZB4B, AND 1X153B4C. REMOVED WIRES 1X151A4A, 1X152A4B AND 1X153A4C. REPLACED WIRES PER SWPM 20-00-16 AND WDM 24-51-01. R/R R2-45, F1-7,F1-5,F1-3 AND T/B S3-263 PER AIM 24-20. OPS CHECK GOOD. C/W NO GO ODE ATA 24-72 OK FOR SERVICE. (LP5834316)

Part: SKIN — TORN (FUSELAGE) · airframe 82,897 hrs · 63,857 cycles

FUSELAGE/ SKIN/ C-3 DOOR CUTOUT/ AFT EDGE: REPAIR OF EDGE TEAR - PERMANENT REPAIR ACCOMPLISHMENT. ACCOMPLISHED SECTION III OF ERA 271005-14 REV E NO FURTHER DAMAGE NOTED. REF LOG PG 1386582 AS TRACKING SECTION IV PERMANENT REPAIR REQ PER ERA 2710050-14 REV E. OK TO CLOSE LOG. (LP0984540)

Part: WIRE — SHORTED (COCKPIT) · airframe 81,179 hrs · 62,311 cycles

SUSPECTED SHORT IN CAPT'S OVERHEAD MAP LT. POPPED CB AFTER RESETTING. ELECTRICAL SMELL. TURNED OFF, SMELL GONE. INSP. OVHD MAP LIGHT ASSY. FOUND EVIDENCE OF SHORTED WIRE AT POS TERM. R/R LIGHT ASSY PER AMM CH 33-10. OPS CK GOOD. OK FOR SVC. (LP5759160)

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 81,124 hrs · 62,265 cycles

TWO CRACKS WERE FOUND ON INTERNAL DOUBLER AT LOWER AFT CORNER OF FORWARD CARGO DOOR JAMB. PERMANENT REPAIR SECTION I WAS PERFORMED AT LOWER AFT CORNER OF FORWARD CARGO DOOR JAMB PER ER/A 575828-14AD REV. ORIGINAL AND ETI-88-19-016 REV.4. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER. DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. AND WILL BE MONITORING UNDER LOG PAGE #0962938 (LP0964394)

Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 81,124 hrs · 62,265 cycles

DENTS ON LOWER SKIN ON MID AND INBD FLAPS VANES OF OUTBD FLAP AT RT WING (AD). DUE TO DELAMINATION ON DENT AT MID VANE PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-03D-PAR. 11B PERFORM A TAP TEST INSPECTION FOR POSSIBLE DISBOND EVERY C CHECK ON DENTED AREA, LOWER SKIN OF INBOARD FALP VANE AT OUTBOARD FLAP RT WING PER SRM 51-50-2 PAR. 2B FOR VISUAL INSPECTION PLEASE SEE LP 0962552. (LP0962563)

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,124 hrs · 62,265 cycles

CRACK ON AFT. ACC. COMP. WEB FRAME FWD FACE STA Y=1463 CANT PROYECTION LONG 9R. WEB FRAME FWD FACE STA Y=1463 CANT PROYECTION LONG 9R.ON AFT. ACC. COMP. WAS REPLACED PER DWG 9953015 REV AH AND SRM 51-30-2 AND SRM 51-30-5. (LP0962285)

Part: SKIN — DENTED (TE FLAP VANE) · airframe 81,124 hrs · 62,265 cycles

DENTS ON LOWER SKIN ON MID AND INBD FLAPS VANES OF OUTBD FLAP AT RT WING (AD). DUE TO DELAMINATION ON DENT AT MID VANE PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-03D-PAR. 11B. PERFORM A DETAIL VISUAL INSPECTION EVERY C CHECK ON DENTED AREA, LOWER SKIN OF INBOARD FLAP VANE AT OUTBOARD FLAP RT WING PER SRM 51-50-2 PAR. 2B. (LP0962552)

Part: RELEASE MECH — SHEARED (TAILCONE) · airframe 81,124 hrs · 62,265 cycles

AWR. MTC REQUEST. DURING TORQUE TEST VERIFICATION IN REF AMDS 5350-4287 STEP 1, SHAFT OF TAILCONE RELEASE MECHANISM CAM WAS SHEARED. CAM ASSY P/N: 5961568-501 WAS REMOVED PER MD-88 AMM 53-53-02-201 1 STEP 3(A) AND SERVICIABLE CAM ASSY P/N: 5961568-501 WAS INSTALLED AND TEST WAS PERFORMED OK. PER MD-88 AMM 53-53-02-201 TOOOL USED: P/N QD2R1000 S/N 116503952 D/D 29-MAY-19. (LP0959816)

Part: ACCESS PANEL — WORN (WING) · airframe 81,124 hrs · 62,265 cycles

AFTER REMOTION OF FUEL ACCES PANEL NBR: 1361C WAS FOUND WEAR ON CONTERSINK IN REF NRC 006. FUEL ACCESS PANEL NBR: 1361C WAS REPLACED FOR A SERVICEABLE ACCESS PANEL P/N: NARB0975-519 PER MD-88 AMM 28-00-00-201. (LP0958359)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,106 hrs · 62,251 cycles

2ND ROW OVERWING EXIT EMERGENCY LIGHTS INOP. R/R BATTERY PACK FOR 2ND ROW OVERWING EXIT SIGNS. PER MD88 AMM 33-53. OK FOR SVC. (LP3759170)

Part: SKIN — DELAMINATED (RUDDER) · airframe 81,067 hrs · 62,223 cycles

DURING PAINT VISIT FOUND RUDDER DELAMINATED. REPLACED RUDDER WITH SERVICEABLE RUDDER PER WORKCARD 2720-4421 RUDDER, MAIN TA OFF 00000 ON 88-5554-9-0001 00550. (LP3759132)

Part: TAB — DAMAGED (RUDDER) · airframe 81,067 hrs · 62,223 cycles

REMOVE RUDDER TAB DUE TO MISSING AND DAMAGED FLAME SPRAY. REMOVE ON NRC 20 IAC/AMA PER AMM 27-20-02. REPLACED RUDDER TAB WITH SERVICEABLE RUDDER TAB PER WORKCARD 2720-4921 TAB, RUDDER W/C OFF 00000 ON 88-5554-9-0003 00350. (LP3759131)

Part: RELAY — STUCK (ELECTRICAL SYS) · airframe 81,046 hrs · 62,210 cycles

AFTER LNDG WITH APU GEN ON - WITH RIGHT ENGINE SHUTDOWN, R BUS FAILED. ELEC SMELL STARTED. C/W NO GO ODI 21-72 AND W/C 2120-2367. FOUND RT AUX POWER RELAY STUCK. R/R RT AUX POWER RELAY PER WDM 24-21-03. OPS CK GOOD. A/C OK FOR SVC. (LP3759108)

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,412 hrs · 61,645 cycles

EMRG EXIT ROW LIGHTS INOP AT 19/20. REPLACED EMRG LIGHT WIRE HARNESS PER MD88 AMM 32-51 OK FOR SVC. (LP4359437)

Part: FRAME — CRACKED (LT MLG WW) · airframe 80,351 hrs · 61,592 cycles

THE LEFT WHEEL WELL FORWARD FRAME HAS A CRACK. REPLACED LEFT FORWARD WHEEL WELL FRAME PER BAC DWG #5930584. (LP #4765882)

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 79,981 hrs · 61,280 cycles

WASTE WATER SERVICE DOOR AFT. AFT LAV SVC DOOR CORRODED. RMVD DOOR AND PLACED IN FWD CARGO MCO POUCH. INSTALLED NEW AFT LAV SERVICE DOOR OPS CHECK GOOD REF AMM 52-40 P/N ON 5914792-61.

Part: CABLE — DETERIORATED · airframe 79,516 hrs · 60,888 cycles

KEVLAR CABLE FOUND DETERIORATED BE LT GROMMET. R/I KEVLAR CABLE PER MD88 AMM 53-53 & WORKCARD 5350-01077-0101 STEP 14. (LP4247373)

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 79,493 hrs · 60,872 cycles

EMERGENCY LIGHTS FROM SEAT 31 AFT INOPERATIVE. REPLACED FUSES IN CHARGER PER CMM 25-60-03. OPS CHECK GOOD PER MD88 AMM 33-53.

Part: APU — SHUTDOWN (APU BAY) · airframe 79,626 hrs · 60,982 cycles

ON APU START, APU STARTED AND THEN SHUT DOWN. NO FAULT LIGHT RPM DROPPED IMMEDIATELY TO ZERO. GRN CREW REPORTED FLAME OUT THE EXHAUST. COMPARTMENT NO EXTERNAL DAMAGE FOUND. FWD APU TO MCO AND PLACARD PER MEL 49-00-01A M PROC C/W. R&R APU ASSY OPS + LK CK GOOD PER AIM 49-10-00. M PROCEDURES REVERSED PLACARDS REMOVED.

Part: LONGERON — CRACKED (BS 294 L24L) · airframe 78,367 hrs · 59,976 cycles

FUSELAGE CRACK AT FASTEN HOLE STA 294 L24L. REMOVED DAMAGE SECTION 54 3/4 OF LONGERON 24 LEFT @ STA 294 AND REPAIRED LONGERON IAW MD88 SRM 53-02 FIG 18. (LP0342699)

Part: SKIN — DENTED (BS 291-307) · airframe 78,360 hrs · 59,970 cycles

FUSELAGE / SKIN / FS STA 291 - 307 / LONG. 23L - 25L / DENT REPAIR - DTA-INFORM ENGINEERING. ERA273604-14 REV B FS STA 291-307/LONG, 23L-25L/DENT REPAIR TIME LIMITED. THIS LP IS TO BE TERMINATED. THE DTA HAS BEEN ACCOMPLISHED AND REQUIRES REPAIR REPLACEMENT PRIOR TO THE ACCUMULATION OF 60,000 TOTAL AIRFRAME FLIGHT CYCLES, AS INSTRUCTED IN THE PERMANENT REPAIR INSTRUCTIONS IN SECTION III OF REVISION C. THIS IS NOW TRACKED VIA LP 0309235. (LP0562053)

Part: FIRE LOOP — FALSE INDICATION (RT ENGINE) · airframe 78,146 hrs · 59,802 cycles

FIRE LOOP A, ON THE RIGHT ENGINE ILLUMINATED WITH NO FIRE WARNING. LOOP B OPS CHECKED GOOD. INSPECTED THE FIRE LOOP ELEMENTS AND CONNECTIONS. NO PROBLEMS NOTED. OPS CHECKED THE RT ENGINE FIRE LOOP A, CHECKED NORMAL IAW AMM 26-10-00. NO 30 DAY HISTORY. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 78,024 hrs · 59,700 cycles

LEFT AFT LAVATORY SMOKE DETECTOR SOUNDED IN FLIGHT. NO SMOKE OR FIRE PRESENT. NO TROUBLE FOUND. SMOKE DETECTOR TESTS OK.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 77,148 hrs · 58,994 cycles

DUAL RED EMERGENCY LIGHTS AT ROW 24 INOPERATIVE. CONNECTED WIRES TO CONNECTOR. LIGHTS OPERATED NORMALLY IAW AMM 33-53.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 77,148 hrs · 58,994 cycles

AISLE EMERGENCY LIGHT AT ROW 26 INOPERATIVE. RECONNECTED WIRES TO CONNECTOR. LIGHT OPERATES NORMALLY IAW AMM 33-53.

Part: FEEDER CABLE — BURNED (APU GENERATOR) · airframe 76,577 hrs · 58,537 cycles

WHILE PERFORMING DUAL PACK CONFIDENCE CHECK FOUND APU GENERATOR FEEDER CABLES SCOTCHED AND BLACKENED. PULLED AND COLLARD APU CNTR/APU DOOR CNTL/AND APU GEN CNTL C/BS. RMVD L/H AFT STAIR SIDEWALL FOR ACCESS. RMVD APU INLET SCREEN FOR ACCESS. RMVD JUMPER BETWEEN TB S3-282 AND R5-1109. RPLD TB S3-282 AND RETERMINATED WIRES 3X1B00AL, 3X2B00AL, AND 3X3V00CAL. ALL WORK C/W PER BSWPM CHAPT 20. REMOVED AND REPLACED APU FEED CABELS 3X2A0AAL, 3X2A0BAL, AND 3X3A0CAL IAW BSWPM 20-10 AND 20-20. C/W ERA 5772778-14 REV O. ALL C/B'S GND OPS CHECKES APU GEN NO DEFECTS NOTED INSTLD L/H AFT STAIR SIDEWALL PANEL. (LP9088475)

Part: INDICATOR — MISSING (HYDRAULIC SYS) · airframe 76,482 hrs · 58,463 cycles

RIGHT HYDRAULIC SYSTEM PRESSURE/QUANTITY LOSS REQUIRED USE OF ALTERNATE GEAR EXTEND PER QRH. MAINTENANCE FOUND THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SIDE FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR (DPI) MISSING. RETAINING SCREWS SHEARED FROM MODULE. REPLACED FILTER MODULE ASSEMBLY, ALL FILTERS (NO CONTAMINATION FOUND), ENGINE DRIVEN PUMP AND ELECTRIC PUMP.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 76,266 hrs · 58,323 cycles

CRACKED INNER SKIN ON RT ELEVATOR. REPAIRED IAW ET/I-88-17-044 REV 4 AND ER/A 554132-14 SECCION 1 REV ORIGINAL .

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 76,266 hrs · 58,323 cycles

DELAMINATION ON LOWER SURFACE OF CENTER GUIDE VANE, LT OTBD FLAP. THE GUIDE VANE WAS REMOVED AND REPLACED IAW AMM 27-51-03.

Part: DOUBLER — DENTED (BS 227) · airframe 76,266 hrs · 58,323 cycles

DENT FOUND ON FUSELAGE SKIN REPAIR DOUBLER BS 227, LONGERON 16 - 18L. REPAIRED IAW ETI-88-17-042 REVISION 4, AND ER/A 554130-14 REVISION ORIGINAL.

Part: SKIN — CRACKED (BS 1406) · airframe 76,266 hrs · 58,323 cycles

CRACK ON FUSELAGE SKIN AT BS 1406 NEAR LONGERON 2R BESIDE DORSAL FIN ATTACH ANGLE. REPAIRED IAW ETI-88-17-016 REVISION 3 AND ER/A 541702-14AD SECTION II.

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON UPPER SKIN BELOW STATIC DISCHARGE BASE AT LT AILERON . THE SKIN WAS REPAIRED IAW SRM 51-70-1A, PAR. 12.

Part: SKIN — NICKED (WINDOW BELT) · airframe 76,266 hrs · 58,323 cycles

NICK ON FWD LOWER EDGE LT WINDOW BELT IAW ER/A 554127-14 REV,ORIG. THE NICKS WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21, AND ER/A. 554136-14 REV. ORIGINAL,

Part: SKIN — NICKED (LT WINDOW BELT) · airframe 76,266 hrs · 58,323 cycles

NICK ON FWD LWR EDGE LT WINDOW BELT. THE NICKS BS 658 - 714 WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21 AND ERA 554135-14 REV. ORIGINAL.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

AFT CARGO COMPARTMENT, CORROSION ON LT TIE TRACK FROM Y=1003 TO Y=1322. NEWS TIE TRACK LT Y=1003 TO Y=1220 AND TIE TRACK LT Y=1220 TO Y=1322 WERE INSTALLED PER SRM 51-30-1 AND 51-30-2 HOLES WERE TREATED AND PAINTED PER SRM 51-10-3 PAR 14 AND 21.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

AFT CARGO COMPARTMENT, ELONGATED HOLE ON FLOOR SUPPORT ABOVE LONG 28R BTW STA Y = 1117 TO 1155. SUPPORT "Z" WAS REMOVED AND INSTALLED PER SRM 51-30-1 AND 51-30-2 NEW SUPPORT "Z" WAS DRILLED PER SRM 51-10-4. NEW SUPPORT "Z" WAS TREATED AND PAINTED PER SRM 51-10-3 PAR 14 AND 21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

CRACKED ANGLE ON FLOOR SUPPORT AT STA Y=1361 X=-22 Z=0. INTERCOSTAL WAS REPAIRED PER SRM, 53-01 FIG 1 51-10-2, 51-30-5.

Part: SKIN — NICKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

FUSELAGE, NICKS ON AFT LWR EDGE LT WINDOW BELT STA Y=748. REF ERA 554116-14 REV ORIG SEC II.

Part: INSERT — MISSING (FLOOR PANEL) · airframe 76,266 hrs · 58,323 cycles

MISSING INSERTS AND CRACK ON AFT CARGO COMPARTMENT CENTER FLOOR PANEL 181DF. FLOOR PANEL WAS REPLACED PER AMM 25-52-01-801.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

AFT CARGO COMPARTMENT, CORROSION ON RT TIE TRACK FROM Y=1003 TO Y=1155, Y=1212 TO Y=1322. DUE TO EXCESIVE CORROSION WERE REPLACE TIE TRACKS. NEWS TIE TRACKS WERE DRILLED PER SRM. 51-10-4. NEWS TIE TRACK RT Y=1212 TO Y=1322 AND TIE TRACK RT Y=1103 TO Y=1155 WERE INSTALLED PER SRM 51-30-1 AND 51-30-2 HOLES WERE TREATED AND PAINTED PER SRM 51-10-3 PAR 14 AND 21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

CRACKED 2 INTERCOSTALS AND PLATE AT KEEL BEAM STA 937 BETWEEN X=7 AND X=-7. INTERCOSTALS (2 E/A) AND PLATE WAS REMOVED, FABRICATED AND INSTALLED PER DWG 9936368 REV AW SRM 51-30-5 AND 53-14-3.

Part: STRUCTURE — CORRODED (LT MLG) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON BUSHING BORE OF LT MLG. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW DWG SR 09570087 REV. BB.

Part: FRAME — CRACKED (BS 1497) · airframe 76,266 hrs · 58,323 cycles

AFT ACCESSORY COMPARTMENT. CRACKED FRAME BS 1497. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 2.`

Part: FRAME — CRACKED (BS 1485) · airframe 76,266 hrs · 58,323 cycles

AFT ACCESSORY COMPARTMENT. CRACKED FRAME BS 1485, LONGERON 16L. THE FRAME WAS REPARED IAW SRM 53-01 FIG 2 (SHEET 3), 51-10-3 PAR 14, 21 AND 51-30-2.

Part: RELIEF VALVE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

FWD CARGO BAY CORRODED ON AFT POSITIVE PRESSURE RELIEF VALVE AT FWD CARGO BAY. REPLACED FOR A NEW VALVE IAW AMM 21-32-07-201.

Part: INTERCOSTAL — CRACKED (BS 1407) · airframe 76,266 hrs · 58,323 cycles

AFT ACCESSORY COMPARTMENT. CRACKED INTERCOSTAL BS 1407, LONGERON 25R. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01 FIG.2 SHEET 4.

Part: FRAME — CRACKED (BS 1452) · airframe 76,266 hrs · 58,323 cycles

AFT ACCESSORY COMPARTMENT HAD A CRACKED FRAME BS 1452, LONGERON 1. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG 2 AND 51-30-5.

Part: FRAME — CRACKED (BS 1380) · airframe 76,266 hrs · 58,323 cycles

AFT ACCESSORY COMPARTMENT HAD A CRACKED FRAME ANGLE BS 1380 BETWEEN LONGERONS 13 & 18R. THE FRAME ANGLE WAS FABRICATED AND REPLACED IAW SRM 53-14-4,51-30-2, AND 51-30-5.

Part: SUPPORT FITTING — DAMAGED (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

ELONGATED VERTICAL ADJUSTMENT PIN HOLE ON FWD CARGO DOOR AFT HINGE. FITTING SUPPORT ON FWD CARGO DOOR AFT HINGE WAS REPLACED PER MD88 AMM 52-31-02-201. (LP2867655)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON ACCESS PANEL 1414C. THE ACCESS PANEL WAS REPLACED.

Part: SKIN — CRACKED (BS 161-188) · airframe 76,266 hrs · 58,323 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON THE FUSELAGE SKIN, DOUBLER AND TRIPLER REPAIR BTW BS 161.5 - 188.25 AND LONGERONS 11 TO 14R.

Part: FINGER DOUBLER — CORRODED (BS 1193-1250) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

AFT CARGO COMPARTMENT, CORROSION WAS FOUND ON FINGER DOUBLER FROM BS 1193 TO 1250 AND LONGERON 26L. THE FINGER DOUBLER WAS FABRICATED IAW DWG 5911423 REV CD, THE FINGER DOUBLER WAS REMOVED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

CRACK ON OUTER PAN BELOW STOP FITTING NR 4 AT AFT EDGE FROM AFT CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05 FIG.50.

Part: MOUNT — CORRODED (ENGINE) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON UPPER HOUSING FWD ENGINE MOUNT. THE PYLON FRONT SPAR BEAVER TAIL FITTING HOLE WAS REPAIRED IAW SRM 54-04D PAR 15.

Part: BEAM — CRACKED (L1 DOOR) · airframe 76,266 hrs · 58,323 cycles

L1 DOOR BEAM NR 1 CRACKED. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG 81, 82.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 76,266 hrs · 58,323 cycles

CRACKED RT HORIZONTAL STABILIZER REAR UPPER SPAR CAP. DRILLED TO NOMINAL SIZE IAW SR09550032 REVISION B.

Part: BEAM — CRACKED (L1 DOOR) · airframe 76,266 hrs · 58,323 cycles

CRACKED BEAM NR 1 ON THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG 81,82.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 76,266 hrs · 58,323 cycles

CRACKED ANGLE ON AFT SERVICE DOOR MID ZONE. THE ANGLE WAS REPLACED IAW DWG 5937918 REV Z AND SRM 51-30-1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

CRACKED INNER PAN ON FWD EDGE BEAM NR 1 AND 5 IN AFT CARGO DOOR. REPAIRED IAW SRM 52-03 FIG. 8.

Part: CUSP WEB — CORRODED (BS 1199-1201) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON RT CUSP WEB RBL 54 TO 60 BETWEEN BS 1199 TO 1201. REPAIRED IAW SRM 53-05 FIG 131A-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

CRACKED INNER PAN ON AFT EDGE BEAM NR 1 AND 5 ON AFT CARGO DOOR. REPAIRED IAW SRM 52-03 FIG. 8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON SECONDARY ACCESS PANELS 1409C AND 1303C. THE ACCESS PLATES WERE REPLACED PER.ER/A 530866-14AD MA.

Part: INTERCOSTAL — CRACKED (BS 786) · airframe 76,266 hrs · 58,323 cycles

CRACKED INTERCOSTAL BS 786 AND BL 0. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG.2 (SHEET 4).

Part: SKIN — WORN (VERTICAL STAB) · airframe 76,266 hrs · 58,323 cycles

VERTICAL STABILIZER, WEAR ON LT AND RT OUTER SKIN BTW YV=256 AND YV=221 AT VERTICAL STABILIZER REMOVABLE TIP FAIRING. AREAS WERE BLEND OUT PER SRM 55-01 FIG 1 AND MEASURED WITH ULTRASONIC TEST PER NDT SPM 04-00-07 FIG3 SHEET 2, AS FOLLOW: UPPER RT SKIN, ORIGINAL THICKNESS IS 0.050" AND MINIMUM REMAINING IS 0.042" THEREFORE ITS WITHIN LIMITS AND THE OTHERS SKINS,(RT LOWER, LT LOWER, AND LT UPPER) DUE TO EXCESSIVE DAMAGE ARE OUT OF LIMITS, BECAUSE ORIGINAL THICKNESS IS 0.050" AND MINIMUM REMAINING IS 0.020"ON RT LOWER SKIN, 0.029"ON LT UPPER SKIN AND 0.005"ON LT LOWER SKIN. PER SRM 55-01 FIG 1. SKINS OUT OF LIMITS WERE REPLACED PER ER/A 551728-14MA REV ORIGINAL, DWG:5912166 REV.

Part: ANGLE — CORRODED (BS 503-522) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORRODED UPPER AND LOWER THE RT ANGLE CUSP BETWEEN BS 503 TO 522. CORROSION WAS REMOVED,TREATED AND PAINTED IAW SRM 51-10-3 PARS. 26, 21 AND 14. THE ANGLE WAS REPLACED IAW SRM 51-10-2;51-10-4 AND DWG 9930538-31.

Part: SKIN — DAMAGED (RUDDER) · airframe 76,266 hrs · 58,323 cycles

DAMAGE METALIZED SKIN ON RUDDER. REPAIRED ERA 092613-14MA REV.A.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 503 - 598 AND BETWEEN RBL 44 TO 60. THE CUSP WEB WAS REPLACED IAW SRM 53-14-4.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 76,266 hrs · 58,323 cycles

CRACKED CHANNEL ON FLOOR PANEL 826D AT MID PAX CABIN. THE CHANNEL WAS REPLACED IAW DWG 9936639 REV.P AND SRM 51-30-1.

Part: SLAT TRACK — CRACKED · airframe 76,266 hrs · 58,323 cycles

CRACK ON SLAT PANEL NR 2 TRACK 7 XRS207. THE TRACK WAS REPAIRED IAW SRM 57-01 FIG 3 SHEET 2.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

WORN PREVIOUS REPAIR DOUBLER ON AFT CARGO DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-2.

Part: PAN — WORN (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

CARGO DOOR WORN FWD OUTER PAN BETWEEN BEAMS 1 AND 2. THE PAN WAS REPAIRED IAW ETI-88-17-014 REV 1 AND ERA 554088-14 REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 522-598) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON LEFT CUSP WEB FROM BS 522 TO 598 BETWEEN LBL 54 AND 60. THE CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2,- 51-30-5, 51-10-3 PAR 14, 21, AND 51-10-4.

Part: LONGERON — CRACKED (BS 1003) · airframe 76,266 hrs · 58,323 cycles

CRACKED LONGERON 6L, BS 1003. THE LONGERONS WAS REPAIRED IAW SRM. 53-02 FIG. 18, 51-30-2, 51-30-5, AND 51-30-1.

Part: CUSP WEB — CRACKED (BS 720) · airframe 76,266 hrs · 58,323 cycles

CRACKED LEFT CUSP WEB AT BS 720 BETWEEN LBL 54 AND 60. THE SEAT TRACK WAS REMOVED AND REPAIRED IAW SRM 53-05 FIF 131A-6 AND 51-30-1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,266 hrs · 58,323 cycles

DELAMINATION ON FLOOR PANEL. REPLACED IAW AMM 53-20-01-201.

Part: DOUBLER — CORRODED (BS 1060-1098) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON RT PREVIOUS REPAIR DOUBLER BETWEEN BS 1060 TO 1098 AND BETWEEN RBL 54 TO 60. THE REPAIR DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-05, FIG 131A-7.

Part: BEAM — CRACKED (NOT REPORTED) · airframe 76,266 hrs · 58,323 cycles

CRACK ON PAN AFT BEAM NR 1. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG 18A.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON LT CUSP WEB FROM BS 598 TO 712 BTW LBL 54 AND 60. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG 131A-24, 51-30-1, 51-30-2, AND 51-30-5.

Part: BEAM — CORRODED (BS 636-683) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

MID CARGO BAY, FOUND CORROSION ON LOWER BEAM FRAME BETWEEN BS 636 TO 683. REWORKED IAW 53-05 FIG 123 SHEET 2 AND DWG 5936038 REV. A.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 76,266 hrs · 58,323 cycles

CRACKED FLOOR PANEL 256E IN THE PAX CABIN. REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 76,266 hrs · 58,323 cycles

CRACKED FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9957828 REV:AB AND SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 185-200) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

FWD WET AREA. CORROSION ON FLOOR SUPPORT BS 185 TO 200, LBL 54. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON FUEL TANK ACCESS PANEL 1303C. THE ACCESS PANEL WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 76,266 hrs · 58,323 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 484 TO 503, RBL 54 TO 60. DAMAGE WAS REPAIRED IAW SRM 53-05 FIG 131A-6.

Part: LONGERON — CRACKED (BS 160) · airframe 76,266 hrs · 58,323 cycles

CRACK ON LONGERON 4L, BS 160. THE LONGERON WAS REPAIRED IAW SRM 53-02-FIG 18 SHEET 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,266 hrs · 58,323 cycles

DELAMINATION ON FLOOR PANEL IN THE FWD PAX CABIN. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01-201.

Part: DOUBLER — CRACKED (BS 1380) · airframe 76,266 hrs · 58,323 cycles

CRACK ON PREVIOUS REPAIR DOUBLER ON BS 1380 NEAR LONGERON 15L. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-04 FIG 18 AND 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,266 hrs · 58,323 cycles

DELAMINATION ON FLOOR PANEL IN PAX CABIN. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01-201.

Part: CUSP WEB — CRACKED (BS 218-225) · airframe 76,266 hrs · 58,323 cycles

FWD WET AREA, CRACKS WERE FOUND ON THE CUSP WEB BS 225 AND 218 BETWEEN LBL 55 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG.131A-13.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 76,266 hrs · 58,323 cycles

CRACKS ON LOWER CORNER NEAR STOPS NR 5 AND 10 INTERNAL STRUCT ON AFT RT OVERWING EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9957735 REV G.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

CRACKED LONGERON 16R ON STA Y=370. LONGERON WAS REPAIRED PER SRM 53-02 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

CRACKED LONGERON 16R ON STA Y=427. LONGERON WAS REPAIRED PER SRM 53-02 FIGURE 18.

Part: PAN — CRACKED (BS 905) · airframe 76,266 hrs · 58,323 cycles

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

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,266 hrs · 58,323 cycles

CARGO DOOR: WORN FWD LOWER CORNER DOUBLER AT FWD CARGO COMPARTMENT DOOR. DAMAGE FWD LOWER CORNER DOUBLER AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER ERA 486624-14MA REV. ORIGINAL. (LP2846170)

Part: TAB — GOUGED (RT ELEVATOR) · airframe 76,266 hrs · 58,323 cycles

GOUGES ON RT ELEVATOR ANTIFLOAT TAB LOWER SKIN. REPLACED IAW SRM 55-04 PAR 2.

Part: TAB — DENTED (HORIZONTAL STAB) · airframe 76,266 hrs · 58,323 cycles

HORIZONTAL STABILIZER: DENTED ON LT GEARED TAB UPPER SKIN. REPLACED IAW SRM 55-04 PAR 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,266 hrs · 58,323 cycles

FUSELAGE SKIN STA 1418 L-2L TO L-2R CRACK DAMAGE SECTION II PERMANENT REPAIR. ER/A 541702-14AD, REV C ACCOMPLISH SECTION II PERMANENT REPAIR INSTRUCTIONS WITHIN 24 MONTHS OF SECTION I. RECOMMEND ACCOMPLISHING AT NEXT H CHECK FROM REVISION C.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 75,140 hrs · 57,475 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 35 AFT. FOUND PUSHED PIN IN QUICK DISCONNECT. REPAIRED THE CONNECTOR AND CHECKED GOOD.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 73,895 hrs · 56,603 cycles

DURING CLIMBOUT PASSING 5000 FT, THE FLOW LIGHT, ILLUMINATED. THE RT PACK HAD SHUTDOWN. ACCOMPLISED QRH PROCEDURE WITH NO POSITIVE RESULT. RT PACK WOULD NOT RECOVER AND LT PACK WOULD MANAGE THE CABIN ALTITUDE KEPT CLIMBING. RETURNED TO DEPARTURE. REPLACED RT PACK PRESSURE REGULATOR AND FLOW CONTROL VALVE. LEAK CHECK OK. INSPECTED LT PACK AND FOUND ORANGE BOOT BLOWN OFF AFT SIDE OF ACM. RE-INSTALLED SAME. ALSO FOUND ORANGE BOOT BLOWN AT LOWER SIDE OF ICE SCREEN. REPLACED BOOT. PERFORMED FUSELAGE LEAK CHECK AND SINGLE PACK CONFIDENCE CHECKS. OPERATION AND LEAK CHECKS, OK IAW AMM 21-00.

Part: FORMER — CRACKED (LT WING) · airframe 73,377 hrs · 56,246 cycles

FOUND LT WING L/E, XRS 80, FORMER CRACKED & DAMAGED WHERE UPPER SLAT CABLES PASS THROUGH. -M-. NR FOR ADDITIONAL INFORMATION 001-0249:5700-2633/025 00264, COMPLETED ER/A 541749-14 REV A.

Part: SKIN — CRACKED (BS 1418) · airframe 73,377 hrs · 56,246 cycles

AIRCRAFT SKIN IS CRACKED AT BS 1418 FROM SKIN EDGE AT LAP ON LONGERON 1 CTR EXTENDING & APPROXIMATELY 3" RBL. ACCOMPLISHED REPAIR IAW PRI 541702-14AD, REV 0 AND 1 AND COMPLIED WITH ER/A 541702-14AD, REV B.

Part: FRAME — CRACKED (BS 1437) · airframe 73,377 hrs · 56,246 cycles

TAIL INTERIOR, BS 1437, CANTED FRAME LOWER CHORD FROM APPROXIMATELY 5"-7" LT FROM LONGERON 1 HAS CRACK. FOR ADDITIONAL INFORMATION NR 001-0280:5300-2957/006, 00216. REPAIRED BY TRIMOUT AND REPAIR ANGLE INSTALLATIONS. ALL WORK RECORDED AND COMPLIED WITH ON PRI 540985-14, REV 0 AND VERIFIED COINCIDES WITH FINAL ER/A 540985-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1437) · airframe 73,377 hrs · 56,246 cycles

TAIL INTERIOR, BS 1437, CANTED FRAME LOWER CHORD FROM APPROXIMATELY 6"-8" RT FROM LONGERON 1 HAS CRACK. FOR ADDITIONAL INFORMATION NR 001-0280:5300-2957/007, 00217. REPAIRED BY TRIMOUT AND REPAIR ANGLE INSTALLATIONS. ALL WORK RECORDED AND COMPLIED WITH ON PRI 540985-14, REV 0 AND VERIFIED COINCIDES WITH FINAL ER/A 540985-14, REV ORIGINAL.

Part: FITTING — CRACKED (BS 1437) · airframe 73,377 hrs · 56,246 cycles

CRACKED UPPER CAP STRIP BS 1437 FWD SIDE OF FITTING AT LONGERON LBL2. IAW DWG 9911840.

Part: SKIN — DAMAGED (BS 170) · airframe 75,858 hrs · 58,036 cycles

SKIN DAMAGED. REPAIRED IAW ER/A 533202-14 SECTION II. MAJOR REPAIR.

Part: WEB — DAMAGED (FUSELAGE) · airframe 77,005 hrs · 58,879 cycles

ERA 540979-14 SECTION I ISSUED FOR STA 1437 WEB REPAIR BETWEEN L2L AND L2R.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 73,377 hrs · 56,246 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT L1 DOOR HAD A NON-SERVICEABLE FRAYED LANYARD. THIS COULD 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: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,312 hrs · 54,862 cycles

MAINTENANCE FOUND SEAT 34D EMERGENCY EXIT LIGHT WIRE BROKEN. MAINTENANCE REPLACED HARNESS AT SEAT 34D.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,312 hrs · 54,862 cycles

MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM 31DE BACK INCLUDING AFT LT EMERGENCY EXIT DOOR SIGN. MAINTENANCE FOUND BAD FUSE IN BATTERY PACK AT OVERHEAD OF SEAT 35DE. REPLACED FUSE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,260 hrs · 54,831 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 10E WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 70,878 hrs · 54,584 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 11 AND 17 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE HARNESS AT 11 AND RE-PINNED THE CONNECTOR AT 17. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,753 hrs · 54,497 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHT FROM DOOR L2 TO ROW 26 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 69,576 hrs · 53,619 cycles

DUE TO A REPORT OF SMOKE IN THE CABIN THAT WAS IDENTIFIED AS BEING CAUSED BY AN OVEN IN THE GALLEY. CREW DECLARED AN EMERGENCY AND REPORTED THAT THE SMOKE DISSIPATED. MAINTENANCE PERFORMED CABIN SMOKE/ODOR WC 2120-2367. THE FWD GALLEY OVEN WAS FOUND WITH GREASE BUILD-UP. THE OVEN AND GALLEY AREA WAS CLEANED AND THE OVEN DEFFERED AS IT WAS NIS.

Part: RELAY — FAILED (CABIN PRESSURE) · airframe 68,647 hrs · 52,989 cycles

DURING CRUISE AT FL280, RED CABIN ALTITUDE WARNING LIGHT ILLUMINATED. PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET AND CONTINUED TO SCHEDULED DESTINATION. CABIN PRESSURE CLIMBED TO 12,000 FEET BEFORE CREW COULD MANUALLY STABILIZE. NO OTHER FAULT LIGHTS AND PASSENGER MASKS WERE NOT DEPLOYED. MAINTENANCE VERIFIED THAT THE LT AND RT PACKS OPERATE NORMALLY AND THAT THE OUTFLOW VALVE MANUALLY OPERATED NORMALLY. REPLACED CABIN PRESSURE POWER TRANSFER RELAY R2-258. OPS CHECKED NORMAL.

Part: LANYARD — DETACHED (R1 DOOR SLIDE) · airframe 68,534 hrs · 52,918 cycles

A PILOT REPORTED THE THE SLIDE COVER LANYARD ON R1 DOOR HAD BECOME DETACHED. NO DAMAGE WAS NOTED AND THE R1 DOOR SLIDE LANYARD WAS REATTACHED.

Part: FRAME — CRACKED (BS 1510) · airframe 68,249 hrs · 52,710 cycles

FRAME BS 1510 CRACKED AT TAIL CONE GUIDE LUG 2 OCLOCK POSITION. HFEC INSPECTED IAW NDT SPM 06-10-01.001. TWO CRACKS FOUND. TOP CRACK .6" LONG BOTTOM CRACK .9" LONG . 5/16 FROM GUIDE HOLE MADE 1 INCH HOLE ACCOMPLISHED HFEC INSPECTION PER NDT SPM 06-10-01.001 OF CUT-OUT, NO CRACKS NOTED. FABRICATION AND REPAIR INSTALL PER PRI INSTRUCTIONS OF ER/A 520646-14 REV. O.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,303 hrs · 49,147 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 62,332 hrs · 48,473 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE AT ROWS 22D AND 23D. MAINTENANCE REPLACED HARNESS AT 22D AND LIGHT ASSEMBLY AT 23D PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: DOUBLER — CORRODED (STA 393-417) · airframe 61,374 hrs · 47,842 cycles

CORROSION ON INTERNAL DOUBLER SKIN BTWN STA Y393 AND 417 L29R-28L. REPAIR PARTS WERE R & R IAW ERA 266459-14, REV H.

Part: SKIN — DENTED (BS 324-363 S20R) · airframe 61,374 hrs · 47,842 cycles

TRANS CN C10080766. DUE ERA 266920-14, REV G PERMANENT REPAIR TO DENT RT STA 324-363, STR 20. SECTION OF SKIN REPLACED STA 324-404 IAW SRM 53-04, FIG 12C.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 61,374 hrs · 47,842 cycles

DUE ERA 372747-14, REV A, PERMANENT REPAIR TO RT INBD FLAP LWR SKIN DAMAGE. ACCOMPLISHED PERMANENT REPAIR SKIN SECTION REPLACMENT IAW ERA 372747-14, REV B.

Part: SKIN — DENTED (BS 408 L29R-29L) · airframe 61,374 hrs · 47,842 cycles

DUE ERA 266459-14, REV G INSPECT DENT STA 408, STR29L-20R. INTERNAL DOUBLER AND FILLER AND EXTERNAL DOUBLER INSTALLED IAW SRM 51-30-2 AND ERA 266459-14, REV H.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 61,374 hrs · 47,842 cycles

CORROSION ON BARREL NUT HOLE FWD SKIN PANEL, LT HORISONTAL STAB, STA XH 28 AND 9 INCHES FWD SPAR. CORROSION REMOVED AND REPAIR BUSHING INSTALLED IAW ERA 487769-14, REV ORIG.

Part: LONGERON — CRACKED (STA 993 L20R) · airframe 61,374 hrs · 47,842 cycles

CRACK ON LONG 20RT, STA Y=993. REPAIR ANGLES INSTALLED IAW ERA 487786, REV ORIG.

Part: SKIN — CORRODED (BS 240-255) · airframe 61,374 hrs · 47,842 cycles

CORROSION BTW TCAS PLATE AND FUSE SKIN STA Y240-255, BTW L28L AND 29R. REPAIR DOUBLERS WERE INSTALL IAW ERA 488845-14, REV ORIG.

Part: WIRE — DISCONNECTED (CABIN) · airframe 59,480 hrs · 46,569 cycles

SEATS 22 AND 23 THE EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT ASSY AT SEAT 22 AND 23, NO HELP. FOUND LIGHT ASSY WIRE HARDNESS UNDER SEAT 23 DE, DISCONNECTED. RECONNECTED AND OPS CHECK GOOD.

Part: SOCKET — MELTED (CABIN LIGHT) · airframe 57,100 hrs · 44,984 cycles

ELECTRICAL BURNING SMELL AT FWD FLIGHT ATTENDANT JUMPSEAT. FOUND 3RD LEFT OVERHEAD CABIN FLUORESCENT FWD LIGHT SOCKET SHORTED/MELTED. REPLACED SOCKET PER AMM OPS CHECKS NORMAL.

Part: LINK — DAMAGED (LT NOSE DOOR) · airframe 50,439 hrs · 40,655 cycles

LT FWD NOSE LANDING GEAR DOOR DID NOT STOW ON GEAR RETRACTION.FOUND LT FWD DOOR LINK BAD. REPLACED DOOR LINK AND ADJUSTED IAW MM. PERFORMED GEAR SWING SEVERAL TIMES-CKS OK.

Part: LANYARD — STRETCHED (TAILCONE SLIDE) · airframe 47,488 hrs · 38,469 cycles

OPS AGENT WALKED DOWN THE CATWALK AND MISTAKENLY PULLED THE RED DEPLOY HANDLE FOR TAILCONE AND SLIDE DEPLOYMENT. THE TAILCONE RELEASED BUT DID NOT FULLY DROP. IT WAS STILL HANGING ABOUT A FT ABOVE THE GND BY THE KEVLAR CABLE. THE SLIDE NEVER DEPLOYED. REINSTALLED TAILCONE AND REPLACED STRETCHED LANYARD.

Part: DUCT — BIRD INGESTION (A/C BAY) · airframe 47,088 hrs · 38,184 cycles

ATB DUE TO OVER POWERING STENCH OF ROASTED BIRD AFTER TAKEOFF, OUT OF LGA. PERFORMED DUCT BURNOUT.

Part: STRUT — LOW (NLG) · airframe 46,189 hrs · 37,549 cycles

NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. SERVICED NOSE STRUT AND CYCLED GEAR.

Part: SWITCH — FAILED (TAIL CONE) · airframe 44,531 hrs · 36,385 cycles

FOUND DURING L/O CHECK WHILE LOOKING IN TAIL COMPARTMENT FOUND CABLE FREE FOR TAIL CONE DEPLOYMENT SYSTEM WITH NO LIGHT INDICATION IN COCKPIT OF TAIL CONE DEPLOYMENT. FOUND SWITCH S1-537 NOT ACTUATING / COMPLETING CIRCUIT. REPLACED SWITCH PER M/M, NOW LIGHT ILLUMINATES NORMALLY.

Part: BATTERY — OVERHEATED (E/E COMPARTMENT) · airframe 44,105 hrs · 36,087 cycles

SMOKE OBSERVED COMING FROM BATTERY VENTS JUST AFT OF NOSEWHEEL AT GATE. REPLACED ACFT BATTERIES AND CHARGER AND BATTERY THERMAL SENSORS PER M/M.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 41,446 hrs · 34,243 cycles

POWER OFF EMERGENCY LIGHTS STAY ON AT L-1, R-1 AND COCKPIT. REPLACED POWER SUPPLY.

Part: WIRE HARNESS — DAMAGED (TRIM ACTUATOR) · airframe 40,890 hrs · 33,852 cycles

PRIMARY TRIM CAUSED A/P AND A/T TO KICK OFF WHEN ACTUATED.CPTS PFD AND NAV DISPLAY BLANKED OUT AND ALL COCKPIT LIGHS DIMMED WHEN TRIM ACTUATED. UPON INSPECTION FOUND WIRE BUNDLE AT PRIMARY AND ALTERNATE TRIM BURNT. SUSPECT WIRES CHAFED DUE TO CONTACT WITH ONE OF PRIMARY ACTUATOR MOUNTING BOLTS.

Part: APU — LEAKING (APU BAY) · airframe 40,368 hrs · 33,508 cycles

DURING TAKEOFF AFT F/A REPORTED ODOR IN CABIN. PERFORMED OP 5088 FOUND OIL LEAK AT APU OIL FILLER NECK. REPLACED APU PER M/M PERFORMED OP 5089 DUCY BURNOUT A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,695 hrs · 32,984 cycles

15C MOUNTED EMERGENCY LIGHT INOP. RELAMPED LIGHT.

Part: BLEED VALVE — LEAKING (BLEED AIR) · airframe 37,168 hrs · 31,057 cycles

ON T/O AFTER PASSING 1000 FT AGL TAIL COMPARTMENT TEMP HIGH MESSAGE ILLUMINATED ON AOP. FOLLOWED ABNORMAL PROCEDURE IN POM AND ISLOATED RT PACK OFF AND MSG WENT OUT. MESSAGE RE-ILLUMINATED WITH PWR UP AND CLIMBING THUR 240. REPLACED RIGHT CROSS-BLEED VALVE AND CLAMPS. RAN ENGINE TO TAKEOFF POWER AND CHECKS OK PER PFHB. PRESSURIZED AIRCRAFT, LEAK CK''D DUCTING, OPERATED PACKS AND ALL CKS OK.

Part: REGULATOR — FAILED (CABIN PRESSURE) · airframe 36,484 hrs · 30,532 cycles

BURNING SMELL THROUGHOUT A/C AFTER T/O. AFT LAV SMOKE DETECTOR SOUNDED. ENGS AT T/O ENG A/I ON, AIRFOIL A/I OFF CROSSFEEDS CLOSED APU OFF. REPLACED LT PRESS REG, C/W DUCT BURNOUT PROCEDURE PER OPN 5088 AND M/M 21-20-02-2 ITEM 7C.

Part: RELAY — INOPERATIVE (RECIRC FAN) · airframe 36,394 hrs · 30,473 cycles

AIRCRAFT OUT AND OFF AND RETURNED TO PHX DUE TO AN ODOR COMING FROM AIR CONDITIONING VENTS IN THE BACK CABIN. FOUND AIR CONDITIONING RECIRCULATING FAN INOP. FOUND FAN RELAY R2-278 BAD. REPLACED RELAY, FAN NOW OPERATES NORMALLY. ALSO NOTED FLUID ACCUMULATION NEAR APU INLET. PERFORMED DUCT BURNOUT PROCEDURE PER OP 5088. CLEANED INLET SCREEN.

Part: OVEN — SMOKE (FWD GALLEY) · airframe 35,990 hrs · 30,193 cycles

IR/ FWD GALLEY OVEN C/B POPPED ACCOMPANIED BY AN ELECTRICAL BURNING ODOR. OVEN SECURED AND NOT USED. REPLACED OVEN. CHECKS GOOD. NO SMELL NOTED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,683 hrs · 29,964 cycles

THE FS 1446 CANTED FRAME WAS FOUND WITH TYPICAL CRACKS IN THE OUTER CHORD AT STRINGERS 3L-6L AND AT STRINGERS 3R-4R. THE CRACKS WERE LOCATED AT THE FRAME TO STRINGER ATTACH POINTS AND WERE .25 INCH LONG TO A MAX OF 3 INCHES LONG. THE CRACKS WERE REPAIRED WITH ALUMINUM REPAIR CHANNELS PER ER/A 378976-14, REV A.

Part: SKIN — DENTED (BS 484)

THE FUSELAGE SKIN HAD A DENT AT FS 484 BELOW STRINGER 20R. THIS DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333456-14.

Part: SKIN — DENT (BS 655)

DURING HMV, A DENT WAS FOUND IN THE FUSELAGE SKIN AT FS 655 AND STRINGER 30L. THE DAMAGE WAS REPAIRED PER ERA 333458-14.

Part: SKIN — DENTED (BS 237)

DURING HMV, DENTS WERE FOUND IN THE FUSELAGE SKIN AT FS 237 BETWEEN STRINGERS 17L AND 18L. THE DAMAGE WAS REPAIRED BY ERA 333441-14.

Part: BATTERY — DISCHARGED (CABIN)

AFT CABIN FLASHLIGHT NOT FLICKERING. REPLACED BATT AND BULB, OP CKS GOOD.

Part: SOCKET — MISSING (CABIN)

EMERGENCY TRACK LIGHTING MISSING LENS AND SOCKET ON MCO. REPLACED LENS AND SOCKET CKS NML.

Part: COALESCER BAG — DIRTY (CABIN)

AFTER TAKEOFF, HAD STRONG ODOR OF SMOKE FILL THE CABIN AND FLIGHT DECK, THIS OCCURRED AFTER FULL POWER APPLICATION, AFTER WIND SHEAR ALERT. RETURNED ATL. RAN ENGINES AT T/O POWER, NO SMOKE OR ODOR NOTED. PERFORMED DUCT BURNOUT, AND CHANGED WATER SEPARATOR BAGS.