N912DL

Part: CONTROL CABLE — BROKEN (SPOILER) · airframe 81,606 hrs · 63,133 cycles

AIRPLANE ROLLED LEFT WITH SPOILER DEPLOYMENT WITH AUTOPILOT ON OR OFF ALL SPEEDS. ALSO FELT IT WHEN ACTUATING AILERONS WHILE FLYING MANUALLY (SOME LEFT ROLL PRESSURE WHEN AILERONS NEUTRAL). GND SPOILER F/D CHECK IS OK. DID FLIGHT AND GROUND SPOILER VISUAL CHECK. 2 PANELS ON LEFT WING. 1 PANEL ON RIGHT BOTH GROUND & FLIGHT SPOILERS AIRPLANE WAS TRIMMED RIGHT (TO THE RIGHT). FOUND SPOILER CABLE 15A BROKEN IN RT WING JUST OUTBD OF RT LANDING GEAR. REPLACED CBLE PER AMM 27-60-00 AND ADJUSTED PER AMM 27-60-00. PERFORMED OPERATIONAL CHECK PER WORKCARD 2760-7293 OPS CHECK GOOD ALL. (LP5846732)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 81,195 hrs · 62,771 cycles

VERTICAL STABILIZER LT SIDE LEADING EDGE SPAR CHORD CRACK REPAIR / AMOC 17-088ER/A 557950-14AD REV A SUPPLEMENTAL INSPECTION RESTRICTION: ACCOMPLISH SECTION II: SUPPLEMENTAL INSPECTIONS, AT ACCRUEMENT OF 63,615 TOTAL AIRCRAFT FLIGHT CYCLES, AND EVERY 4,500 FLIGHT CYCLES THEREAFTER. (LP1003568)

Part: TAB — DAMAGED (RT WING AILERON) · airframe 80,619 hrs · 62,275 cycles

RT WING AILERON CONTROL TAB TRAILING EDGE EXPOSED COMPOSITE. PAINTED RIGHT WING AILERON CONTROL TAB PER MD-88 SRM-51-10-3B. PERFORMED RIGHT WING AILERON CONTROL TAB SATISFACTORY WEIGHT AND BALANCE PER MD-88 SRM 57-50-1 . REMOVAL AND INSTALLATION OF RIGHT WING AILERON CONTROL TAB WAS ACCOMPLISHED ON AMDS 2710-4376-RH NEW WEIGHT 7.97 NEW MOMENT -3.87 ASSET 0022617. (LP0873579)

Part: SKIN — DELAMINATED (NR 2 NACELLE) · airframe 80,619 hrs · 62,275 cycles

#2 ENGINE INLET COWL INTERIOR HAS DELAMINATED AREA AT AFT END OF COWL , 7 OCLOCK POSITION. REPLACED #2 ENG INLET COWL IAW MD-88-AMM-71-10-01 LEAK CHECKED SATISFACTORY ANTI-ICE CONNECTION ON #2 ENG INLET COWL IAW MD-88-AMM-71-10-01. (LP0872635)

Part: TAB — DAMAGED (LT AILERON) · airframe 80,619 hrs · 62,275 cycles

LT WING AILERON CONTROL TAB TRAILING EDGE EXPOSED COMPOSITE. PAINTED LEFT WING AILERON CONTROL TAB PER MD-88 SRM 51-10-3B. PERFORMED LEFT WING AILERON CONTROL TAB SATISFACTORY WEIGHT AND BALANCE PER MD-88 SRM 57-50-1 . REMOVAL AND INSTALLATION OF LEFT WING AILERON CONTROL TAB WAS ACCOMPLISHED ON AMDS 2710-4376-LH. NEW WEIGHT 7.90 NEW MOMENT -3.66 ASSET 0022617. (LP0873569)

Part: SKIN — CRACKED (L1 DOOR) · airframe 80,619 hrs · 62,275 cycles

TASKCARD 5211-2537 - L1 DOOR FUSELAGE SKIN AFT #5 DOORSTOP ADJUST HOLE, STA Y=200, CRACKED APROX 0.125" LONG 37-001. REPAIRED FUSELAGE SKIN AT L1 DOOR JAMB AFT #15 DOOR STOP HOLE. CUT OUT DIM 1.7"X3.7" IAW MD88 SRM 53-05 FIG 114 PAR 131. THIS IS A CATEGORY B REPAIR AND REQUIRES REPETITIVE INSPECTION STARTING AT 28,000 CYCLES FROM TIME OF REPAIR INSTALLATION AND EVERY 20,000 CYCLES THERE AFTER. INSPECTION METHOD EDDY CURRENT PER MD88 SRM 51-10-5C. (LP0872634)

Part: TAB — DEBONDED (HORIZONTAL STAB) · airframe 80,619 hrs · 62,275 cycles

RT HORIZ STAB CENTER GEARED TAB HAS DISBANDED COMPOSITE REPAIR ON TE DOT 003/96. REMOVED & INSTALLED OF RIGHT HORIZ. STAB GEAR TAB IAW DELTA 2730-4130-RH REPAIRED RIGHT HORIZ. STAB GEAR TAB IAW -MD-88-SRM- 51-70-02D PARA E(7,8,13,15) WEIGHED RIGHT HORIZ. STAB GEAR TAB, 5.784 LBS IAW MD-88-55-20-02 WEIGHT WITHIN LIMITS. (LP0871185)

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,695 hrs · 61,458 cycles

EMERERGENCY CELLING LIGHTS ARE INOPERATIVE ROW 31 TO THE TAIL. B5-107 BATTERIES DEAD. THE BATTERIES WERE REPLACED PER AMM 33-53. OPERATIONAL CHECK WAS GOOD.

Part: LANYARD — BROKEN (GIRT BAR) · airframe 79,484 hrs · 61,275 cycles

FOUND 1L DOOR SLIDE GIRT BAR LANYARD BROKEN. REPLACED 1L DOOR LANYARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,285 hrs · 61,117 cycles

DOOR R1 EMERGENCY LIGHT INOP. RELAMPED OPS CHECK GOOD IAW AMM 33-51.

Part: ENGINE — FAILED (RIGHT) · airframe 79,161 hrs · 61,014 cycles

ATB/IFSD TO RIC DUE TO A RIGHT ENGINE FAILURE. CREW REPORTED AT 900 FT HEARD A BANG ENGINE ROLLED BACK AND EGT SPIKED. PER QRH SHUT DOWN ENGINE AND RETURNED. FIREBALL REPORTED BY WITNESS ON GROUND. SUBSEQUENT FIRE IN FIELD OFF OF DEPARTURE END OF RUNWAY. MTC FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGED.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,059 hrs · 60,929 cycles

CLIMBING THROUGH FL90, FLIGHT ATTENDANT REPORTED STRONG SMOKEY ODOR IN THE MID CABIN. CREW RAN QRH AND ODOR DISSIPATED. ON RESUMPTION OF CLIMB POWER ODOR RETURNED. RETURNED TO DEPARTURE. MAINTENANCE PERFORMED THE NO GO ODI PREVENTION WORK CARDS 2120-2367 AND 2120-2368 AND A FULL DUCT BURNOUT. NO ODOR WAS PRESENT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: B-NUT — LEAKING (HYD FILTER) · airframe 77,965 hrs · 60,082 cycles

FLIGHT ATTENDANTS REPORTED FUMES IN CABIN AFTER TAKEOFF. FOUND THE LT A/C COMPARTMENT B-NUT ON A HYD FUSE LEAKING NEAR FILTER PACK. TIGHTENED THE B-NUT.

Part: SKIN — CRACKED (BS 1474) · airframe 77,907 hrs · 60,031 cycles

CRACK IN SKIN, ONE INCH FWD OF THE LT CANT BS 1474 AT VENTRAL STAIR CUTOUT. COMPLIED WITH ERA 562986-14, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,876 hrs · 60,005 cycles

FWD UPPER EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES IAW AMM 33-53-00. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,257 hrs · 59,505 cycles

DURING A SERVICE CHECK, FOUND SEAT ROWS 1-3, 10-12 AND FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 77,238 hrs · 59,489 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. SECURED EMER EXIT SIGN. OPN CKS NORM.

Part: LIGHT — ILLUMINATED (COCKPIT) · airframe 77,019 hrs · 59,314 cycles

GEAR DOOR OPEN LIGHT ILLUMINATED IN CRUISE. PER QRH, ALTERNATE GEAR EXTEND USED FOR LANDING. REPLACED L1-122 MAIN GEAR OPEN LIGHT ASSEMBLY. JACKED A/C AND COMPLETED MULTIPLE GEAR SWINGS WHILE COMPLYING WITH POSITION AND WARNING INDICATION TEST. POSITIVE RESULTS FOR ALL TESTS. REPLACED L/R GEAR DOOR SKIDS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,989 hrs · 59,292 cycles

LEFT & RIGHT AFT OVERWING EXIT IDENTIFIER LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM IAW 33-53. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 76,829 hrs · 59,159 cycles

DURING CLIMB AT FL 260, THE AUTOTHROTTLES DISCONNECTED WITH ERRONEOUS EPR READINGS ON THE RIGHT ENGINE. FLIGHT ATTENDANTS ADVISED ELECTRICAL, PLASTIC BURNING ODOR IN THE FORWARD GALLEY AND FAINT ODOR NOTICED IN COCKPIT. COMPLIED WITH WORK CARD 2120-2367. COULD NOT ISOLATE ANY PROBLEMS. COMPLIED WITH WORK CARD 7100-2619 FULL DUCT BURNOUT. NO ODOR NOTICED. NO EPR FLUCTUATIONS WHILE ENGINE RUN WAS ACCOMPLISHED DURING DUCT BURN.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 81,206 hrs · 62,784 cycles

VERTICAL STABILIZER LT SIDE LEADING EDGE SPAR CHORD CRACK REPAIR AMOC 17-088. ER/A 557950-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, LOGPAGE TERMINATED. (LP2989956)

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 76,637 hrs · 59,015 cycles

CRACK INDICATION ON BOLT HOLE FOR THE LT SIDE OF THE VERTICAL STAB L/E ZFS 52.267. REPAIRED IAW DWG SG 09550005-7001.

Part: HEATER — FAILED (SLIDING WINDOW) · airframe 75,988 hrs · 58,522 cycles

WITH ANTI FOG SWITCH ON, CAPTAINS SLIDING WINDOW GOT EXCESSIVELY HOT. WINDOW STARTED WARPING, AND BECAME SOFT. ALSO HAD A SMALL BURNING ODOR. WITH ANTI FOG OFF, THE BURNING ODOR WENT AWAY. R & R CAPTAINS SLIDING WINDOW IAW AMM 56-10. OPS CHECKED GOOD, NO BURNING ODOR NOTED.

Part: SUPPORT — CORRODED (RT MLG) · corrosion level 2 · airframe 75,797 hrs · 58,396 cycles

MAIN LANDING GEAR/WHEEL WELL, CORROSION AND SCRATCHES ON BEARING OF RT MLG RETRACT ACTUATOR UPPER SUPPORT. BEARING WAS REPLACED PER CMM 20-10-17 AND ER/A 552856-14 AD REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

EXTERNAL FUSELAGE SKIN: WAVY PREVIOUS REPAIR FROM STA Y=181 TO Y=228 BTW LONG 22R TO 26R. DAMAGE PREVIOUS REPAIR WAS REMOVED AND REPLACED FOR NEW ONE CORRECT REPAIR PER SRM 53-04 FIGURE 12C. PERFORM EXTERNAL VISUAL INSPECTION THRESHOLD 8000 LANDINGS AND REPETITIVE INTERVAL 8000 LANDINGS PER SRM 53-04 FIG.12C SHEET 12 GENERAL NOTE 31.

Part: RELEASE MECH — DEFECTIVE (TAILCONE) · airframe 75,795 hrs · 58,395 cycles

DURING "OK TO INSTALL EVACUATION SLIDE" WERE FOUND SEVERAL DISCREPANCIES: ACTIVATED POSITION OF TAIL CONE RELEASE CAM, OVER TENSIONED TAIL CONE RELEASE MECHANISM CONTROL CABLES AND MISSING LUBE SAME CONTROL CABLES/PADS GUIDE PIN. TAILCONE WAS REMOVED PER AMM 53-53-00-401, RELEASE MECHANISM CAM WAS INSTALLED PROPERLY PER AMM 53-53-02-201, PADS GUIDE PIN AND LATCHES WERE LUBRICATED PER AMM 53-53-00-401, TAIL CONE RELEASE MECHANISM WAS ADJUSTMENT PER AMM 53-53-00-501, RELEASE MECHANISM CONTROL CABLES WAS LUBRICATED PER AMM 20-10-17 AND TAILCONE WAS INSTALLED PER AMM 53-53-00-401.

Part: SKIN — DAMAGED · airframe 76,047 hrs · 58,559 cycles

SKIN DAMAGED AROUND AFT LH LAV SERVICE. REPAIRED IAW ERA 551757-14.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON RT WING HEATER BLANKET CUT OUT OF ACCESS PANEL. REPLACED IAW AMM 30-80-02, PAGE 401, PAR 2.A.

Part: SKIN — CORRODED (BS 1170) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON INNER SKIN BS 1170, LONGERON 18 - 19L. REPAIRED IAW ETI-88-16-453 REV. 2 AND ER/A 552819-14 REV. ORIG.

Part: FRAME — CRACKED (BS 1510) · airframe 75,795 hrs · 58,395 cycles

AFT ACCESORY COMPARTMENT, HAS A CRACK ON FRAME BS 1510. REPLACED IAW SRM 51-30-2 AND DWG 9911843-5 REV AC.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 75,795 hrs · 58,395 cycles

HIDDEN DAMAGE. AFTER NUT REMOVAL ON RT MLG SUPPORT FITTING INBD LOWER STUD CORROSION WAS FOUND. LOWER STUD ON RT MLG SUPPORT FITTING WAS REMOVED AND INSTALLED PER AMM 20-30-01 AND 20-10-14, AFTER STUD REMOVAL CORROSION WAS FOUND ON FITTING BORE AND WAS ATTENDED UNDER ERA 552830-14 REV ORIGINAL AND ETI-88-16-458 REV 5. FUEL LEAK CHECKS WAS PERFORMED AND LEAKS NOT WAS FOUND PER AMM 28-10-01/601.

Part: LATCH — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION AROUND OF INTERNAL SIDE ON LATCHES AND CLIP AT AFT SERVICE PANEL DOOR AMDS 5300-2960. SERVICE PANEL DOOR WAS REPLACED PER SRM 51-30-5.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

AFT CARGO COMPARTMENT, CORROSION ON DOOR JAMB WEB BTW STA Y=1150 TO Y=1270 BTW LONG 30 TO 24R. FITTINGS STA-Y: 1255, Y: 1212, STRAPS STA Y: 1220, Y: 1245 AND WEB WERE REMOVED AND INSTALL NEW WEB PER SRM 51-30-2, 51-30-5 AND DWG 5936442 REV A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON UPPER AND LOWER CUSP WEBS FROM STA Y=1150 TO Y=1174 BTW X= 60 TO X=44. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A-21.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

AFT CARGO COMPARTMENT, CORROSION ON DOOR JAMB BEAM BTW STA Y=1155 TO 1212 LONG 27R TO 28R. DOOR JAMB BEAM BTW STA Y=1155 TO 1212 LONG 27R TO 28R WAS REPAIRED PER SRM 51-30-5 AND SRM 53-05 FIG 123.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB AT RT OVERWING FRAME STA Y=864 STA: 00441. FRAME WAS REPLACED PER SRM 51-10-4, SRM 51-30-5, SRM 51-30-2 AND CARD REPLACE SECTION OVERWING FRAME 5310-01415-0302.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON THE RT HORIZONTAL STABILIZER SKIN BARREL NUT HOLE 14 AND 16. REPAIRED IAW ETI-88-16-438 REV. 1 AND ER/A 551763-14 REV ORIG.

Part: LONGERON — CRACKED (BS 1437) · airframe 75,795 hrs · 58,395 cycles

AFT ACCESORY BAY HAS A CRACKED LONGERON 5R BS 1437. THE LONGERON WAS REPAIRD IAW SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 75,795 hrs · 58,395 cycles

CRACKED LONGERON 3L, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.

Part: SKIN — DELAMINATED (RT WING) · airframe 75,795 hrs · 58,395 cycles

RIGHT WING HAD A DELAMINATED OTBD TE PANEL XA=429-434. REPAIRED IAW ERA 551768-14 REV ORIGINAL.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON THE LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 15,14, AND 13. REPAIRED IAW ETI 88-16-437 REV 1 AND ER/A 551718-14 REV ORIG.

Part: LONGERON — CORRODED (BS 1319) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON LONGERON 22L, BS 1319 AT AFT CARGO BAY. THE LONGERON WAS REPLACED IAW SRM 53-02 FIGURE 18.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

AFT WET AREA HAD CORROSION ON THE FLOORBEAM BS 1338 BETWEEN RBL 60 TO LBL 60. THE FLOORBEAM WAS REPLACED IAW SRM 51-70-5 FIG 1 (SHEET 2).

Part: INTERCOSTAL — CORRODED (BS 1308-1361) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON INTERCOSTAL BS 1308 - 1361 BETWEEN RBL 17 AND LBL 17. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1 AND DWG 9936656 REV. AM.

Part: DOOR FRAME — CRACKED (SERVICE DOORWAY) · airframe 75,795 hrs · 58,395 cycles

DURING NDT INSPECTION WAS FOUND WITH DISCREPANT AREA AT FWD SERVICE DOOR FRAME UPPER FWD CORNER. REPAIRED IAW ERA 551775-14AD REV. ORIGINAL SECTION II.

Part: FRAME — CRACKED (BS 1322) · airframe 75,795 hrs · 58,395 cycles

AFT WET AREA HAS A CRACKED FRAME BS 1322 AND LONGERON 17R. REPAIRED THE FRAME IAW ER/A 493697-14MA REV.B.

Part: FRAME — CRACKED (BS 1322) · airframe 75,795 hrs · 58,395 cycles

AFT WET AREA HAS A CRACKED FRAME BS 1322 AND LONGERON 17L. REPAIRED THE FRAME IAW ER/A 493697-14MA REV.B.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON BULKHEAD OF WALKING BRIDGE STA Y=1485 CANT. BULKHEAD WAS REPLACED PER SRM 51-30-2 AND DWG 9911993 REV CJ.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

CRACKED RT CUSP WEB STA Y= 997 BTW X=-54 TO -60 AT PAX CABIN FLOOR STRUCTURE. DAMAGE WAS REPAIRED PER SRM 53-05 FIG 131A-14.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON INTERCOSTALS OF WALKING BRIDGE FROM STA Y=1361 TO Y=1485 CANT INTERCOSTAL ON STA 1427, STA 1449 AND STA 1339 WERE REPLACED PER DWG: 9911993 REV CJ.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

MID CARGO COMPARTMENT, CORROSION ON PRODUCTION DOUBLER STA Y=750-760 BETWEEN LONGERONS 28R AND 28L. PRODUCTION DOUBLER WAS REPLACED PER SRM 53-34-0 FIG2A 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

HIDDEN DAMAGE, CRACKED LONGERON 25 AND 22 RT STA Y=218 AT E&E COMPARTMENT. LONGERONS WERE REPAIRED PER SRM 53-02 FIGURE 18.

Part: PAN — CRACKED (CARGO DOOR) · airframe 75,795 hrs · 58,395 cycles

FWD CARGO COMPARTMENT. CRACKED INNER PAN ON BEAM 5 STA Y= 370 AND 426 AT FWD CARGO DOOR INNER STRUCTURE. CRACK ON PAN STA Y=426 WAS REPAIRED PER SRM 52-03 D FIG 8 AND CRACK ON PAN STA Y=370 WAS REPAIRED PER ETI-88-16-444 REV ORIGINAL AND ERA 551769-14 REV ORIGINAL.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

HIDDEN DAMAGE, CORROSION ON WEB STA Y=210 BTW X=-44 TO X=-60 AT PAX CABIN. DIAPHRAGM WAS REPLACED PER SRM 53-14-1 FIG 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

AFT ACCESSORY COMPARTMENT, CRACKED TITANIUM FRAME ON STA Y=1346 BTW X=14L TO 14R. TITANIUM FRAME ON STA Y=1346 BTW X=14L TO X=14R WAS REPAIRED PER ER/A 094719-14 MA REV A STEPS 6, AND 7.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

FWD WET AREA, CORROSION ON CUSP ANGLE STA Y=160 TO Y=200 X=-60 RIGHT SIDE. CUSP ANGLE WAS REPAIRED PER SRM 53-05 FIG 55.

Part: PAN — CRACKED (BS 905) · airframe 75,795 hrs · 58,395 cycles

CRACKED PAN ON RT FWD OVERWING EMERGENCY DOOR FRAME BS 905, LONGERON 16R. REPAIRED IAW SRM 51-70-4 FIG 2 SHEET 1.

Part: CUSP WEB — CRACKED (BS 845-905) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON THE CUSP WEB LOWER AND UPPER SURFACE, BS 845 - 905, RBL 44 - 60. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG 131A-24, 51-10-3 PAR 14 -21, AND 51-30-2.

Part: DOOR FRAME — CRACKED (LT OVERWING) · airframe 75,795 hrs · 58,395 cycles

CRACKED PAN ON THE LT AFT OVERWING EMERGENCY DOOR FRAME BS 905 LONGERON 16L. REPAIRED IAW SRM 53-01 FIG 2 SHEET 3.

Part: CUSP WEB — CRACKED (BS 997) · airframe 75,795 hrs · 58,395 cycles

CRACK ON CUSP WEB BS 997, LBL 57. REPAIRED IAW SRM 53-05 FIG 131A-4.

Part: STEP — CORRODED (VENTRAL STAIR) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON VENTRAL STAIR STEPS 2, 3, 4, 5, 10, AND 12. ALSO A BROKEN RETAINERS ON STEPS 3 AND 4. STEPS 3 AND 12 WERE REPLACED DUE TO CORROSION. CORROSION ON STEPS 2, 4, AND 5 WERE REMOVED, THE RETAINERS ON STEPS 3 AND 4 WERE REPLACED.

Part: BRACKET — CORRODED (LAVATORY) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION FOUND ON AFT BRACKET SUPPORT OF PREMIER LAVATORY. BRACKET WAS FABRICATED IAW DWG MD081101 ECO NO A-3.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 75,795 hrs · 58,395 cycles

CARGO DOOR DOUBLER REPAIR HAS WEAR REPLACED PER ER/A 486624-14MA REV.ORIGINAL.

Part: FITTING — CRACKED (BS 1193) · airframe 75,795 hrs · 58,395 cycles

CRACKED FITTING ON UPPER AND LWR EDGE OF DOOR BS 1193 AT AFT CARGO DOOR INNER STRUCTURE. FITTINGS ON UPPER AND LWR EDGE WERE REPLACED IAW SRM 51-30-2 , 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 446-1212) · airframe 75,795 hrs · 58,395 cycles

CRACK ON BS 446 LONGERON 4L, BS 522 LONGERON 4R AND BS 1212 LONGERON 5L. LONGERON REPAIRED IAW 53-02 FIG. 18.

Part: DOUBLER — CORRODED (BS 826-845) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON RT PREVIOUS REPAIR BS 826-845 RBL 54 TO 60. DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR. 38 AND 53-05 FIG.131A-14.

Part: SKIN — DAMAGED (LT WING) · airframe 75,795 hrs · 58,395 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR XRS=163 TO 168 AT LT WING. REPAIRED IAW ER/A NO. 551774-14AD REV. ORIGINAL .

Part: SKIN — DAMAGED (RT WING) · airframe 75,795 hrs · 58,395 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR XRS=163 TO 168 AT RT WING. REPAIRED IAW ER/A NO. 551774-14AD REV. ORIGINAL .

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 75,795 hrs · 58,395 cycles

CRACK ON RT CUSP WEB BS 218 - 237. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-24.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 75,795 hrs · 58,395 cycles

FWD CARGO BAY CRACKED FWD AND AFT STOP FITTING NR 5 AT FWD CARGO DOOR. CRACKED FWD AND AFT STOP FITTING NR 5 WERE REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: TEE FITTING — CRACKED (BS 370) · airframe 75,795 hrs · 58,395 cycles

FWD CARGO BAY CRACKED TEE FITTING ON BEAM 5 BS 370 AT FWD CARGO DOOR INNER STRUCTURE. CRACKED TEE FITTING WAS REPLACED IAW SRM 51-30-4 AND 51-30-5.

Part: CUSP WEB — PUNCTURED (BS 769) · airframe 75,795 hrs · 58,395 cycles

PUCNTURE ON CUSP WEB BS 769, LBL 54 TO 44. REPAIRED IAW SRM 53-01 FIGURE 1 SHEET 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

CRACKED LONG 3 LT STA Y= 160. REPAIRED PER SRM 53-02 FIG 18.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON FLOOR SUPPORT STA Y= 1309 BTW X= -17 TO X=17. FLOOR SUPPORT WAS REPLACED PER SRM 51-30-5.

Part: WEB — DAMAGED (FUSELAGE) · airframe 75,795 hrs · 58,395 cycles

PUNCTURE AND CRACK ON WEB STA Y= 190, Y=214 AND Y=250 BTW X=44 AND X=60 LT SIDE. REPAIRED PER SRM 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 470) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON CUSP WEB BS 470 BETWEEN LBL 54 - 60. REPAIRED IAW SRM 51-30-5, 51-30-2, 53-05 FIG. 131A-13, 51-10-3 PAR. 38.

Part: CAM — WORN (TAILCONE) · airframe 75,795 hrs · 58,395 cycles

WORN TAILCONE RELEASE CAM. TAILCONE RELEASE CAM WAS REPLACED IAW AMM 20-30-01.

Part: LINK — CORRODED (HORIZONTAL STAB) · airframe 75,795 hrs · 58,395 cycles

LEFT HORIZONTAL STAB FREEPLAY AND RUSTED CONTROL LINK 9F GARED TAB ON LH ELEVATOR. CONTROL LINK OF GEARED TAB AT LT ELEVATOR WAS REPLACED PER MD88 CMM 27-30-1 ADJUSTMENT IS ACCOMPLISHED UNDER CARD 2730-4831 JOB 001-0234. (LP# 2779489)

Part: TORSION BAR — CORRODED (SPOILER) · airframe 75,795 hrs · 58,395 cycles

RUSTED TORSION BAR AT LT WING INBD FLIGHT SPOILER PANEL. DAMAGED TORSION BAR, CAM ARM AND LEVER WERE REPLACED AND INSTALLED IAW AMM 27-61-06

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 160 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-1, 51-10-4, AND 53-14-2.

Part: TORQUE TUBE — CORRODED (ELEVATORS) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON RT AND LT ELEVATORS TORQUE TUBE ENDS. THE TORQUE TUBE ENDS WERE REPLACED IAW AMDS 2730-4234.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 503 TO 598 RBL 44 TO 60. THE CUSP WEB WAS REPLACED IAW 51-30-1,51-30-2,51-30-5 AND 51-10-4.

Part: CUSP WEB — CRACKED (BS 519) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CRACK ON LT CUSP WEB LBL 54, BS 519. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-12.

Part: PIN — CORRODED (ELEVATOR) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORRODED ELEVATORS SECTOR PIN. THE PIN WAS REPLACED IAW AMDS 2730-4234.

Part: TORSION BAR — CORRODED (RT WING) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

RIGHT WING.CORROSION ON TORSION BAR OF INBD FLIGHT SPOILER AT RH WING. DAMAGED TORSION BAR, CAM ARM AND LEVER AT RH INBD FLIGHT SPOILER WERE REPLACED AND INSTALLED IAW AMM 27-61-02.

Part: BEAM — CRACKED (PAX DOOR) · airframe 75,795 hrs · 58,395 cycles

CRACKED RT BEAM BELOW UPPER HINGE ON AFT ENTRY DOOR. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG. 34. ( SHEET 1 ).

Part: FLOOR PANEL — DELAMINATED · airframe 75,795 hrs · 58,395 cycles

DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: VANE — WORN (LT WING TE FLAP) · airframe 75,795 hrs · 58,395 cycles

LEFT WING HAS A WORN DOUBLER ON THE LT GUIDE VANE, OUTBOARD FLAP. VANE WAS REPAIRED IAW SRM 57-03D PAR.11.

Part: TORSION BAR — CORRODED (LT WING) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

LEFT WING RUSTED TORSION BAR ON LT WING OUTBD SPOILER PANEL. DAMAGED TORSION BAR, CAM ARM AND LEVER AT LT OUTBD FLIGHT SPOILER WERE REPLACED AND INSTALLED IAW AMM 27-61-06. (LP2774203)

Part: CLEVIS — CORRODED (LT WING SPOILER) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

LEFT WING HAS CORROSION ON REACTION BOLT AND CLEVIS OF LT OUTBD FLIGHT SPOILER. REACTION BOLT AND CLEVIS WERE REPLACED IAW AMM 27-61-08.

Part: CUSP WEB — CRACKED (BS 296) · airframe 75,795 hrs · 58,395 cycles

CRACK ON CUSP WEB BS 296 AND CORROSION ON BS 312 BETWEEN RBL 44 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-13,51-30-2,51-30-5,51-10-3 PARR 14 AND 21.

Part: DOUBLER — CRACKED (SERVICE DOOR) · airframe 75,795 hrs · 58,395 cycles

CRACK ON PREVIOUS REPAIR BETWEEN LOWER ARM HINGE AT FWD SERVICE DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-03 D FIG. 3.

Part: CUSP WEB — CORRODED (BS 546-589) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON CUSP WEB BS 589 AND 546 BETWEEN LBL 54 - 60. REPAIRED IAW SRM 53-05 FIGURE 131A.

Part: LONGERON — CRACKED (BS 389) · airframe 75,795 hrs · 58,395 cycles

CRACK ON LONGERON 16L BS 389. REPAIRED IAW SRM 53-02 FIG 18.

Part: VANE — WORN (LT WING TE FLAP) · airframe 75,795 hrs · 58,395 cycles

LEFT WING WORN DOUBLER ON GUIDE VANE, OUTBOARD FLAP REPAIRED IAW SRM 57-03D PAR. 11.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 75,795 hrs · 58,395 cycles

DURING NDT INSPECTION WAS FOUND WITH DISCREPANT AREA AT LOWER AFT CARGO DOOR FRAME. REPAIRED IAW ER/A 487137-14AD.

Part: HOUSING — WORN (CARGO DOOR) · airframe 75,795 hrs · 58,395 cycles

WEAR ON HOUSING BELOW EXTERNAL HANDLE AT AFT CARGO DOOR (C3). DAMAGE HOUSING WAS REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: DOOR FRAME — DAMAGED · airframe 75,795 hrs · 58,395 cycles

DURING NDT INSPECTION WAS FOUND WITH DISCREPANT AREA AT UPPER FORWARD DOOR FRAME. REPAIRED IAW ER/A 487144-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON FUEL TANK ACCESS PANEL COUNTERSINKS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A COND II.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 75,795 hrs · 58,395 cycles

CRACKED FITTING ON UPPER EDGE STA Y= 647 AT MID CARGO DOOR INNER STRUCTURE. FITTING WAS REPLACED PER SRM 51-30-1 AND 51-30-5 AND DWG 3926046 REV B.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 75,795 hrs · 58,395 cycles

CORROSION ON RIGHT WING TE FLAP GUIDE VANE. THE VANE WAS REPLACED IAW SRM 57-03D PAR 11.

Part: FRAME — CRACKED (BS 1463) · airframe 72,596 hrs · 55,974 cycles

CRACKED AT THE BS 1463 FRAME 1:00 POSITION. REPAIRED IAW ER/A 535920-14, REV ORIGINAL.

Part: STIFFENER — DAMAGED (BS 1463) · corrosion level 2 · airframe 72,596 hrs · 55,974 cycles

AT BS 1463 WEB, FOUND STIFFNER, HAS FOUR HOLES MISALIGNED, DUE TO OIL CANNING OF WEB. DAMAGE REMOVED AND THE .1875" HOLES ARE NOW .390-.400 DIAMETER. REPAIRED IAW ER/A 535920-14, REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,751 hrs · 56,072 cycles

AFT FUSELAGE SKIN CORRODED ALONG LOWER EDGE OF LAV PANEL. COMPLY WITH ERA 537873-14, REV O.

Part: FRAME — CRACKED (BS 1418) · airframe 72,596 hrs · 55,974 cycles

TAIL INTERIOR, LOWER AFT FLANGE AT OF FRAME, BS 1418 IS CRACKED AT L2L. REPAIRED IAW ER/A 538118-14, REV 0.

Part: FRAME — CRACKED (BS 1463) · airframe 72,596 hrs · 55,974 cycles

FRAME BS 1463, CRACKED AT THE 1:00 POSITION. REPAIRED IAW ER/A 535920-14, REV ORIGINAL.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 71,283 hrs · 55,107 cycles

AT DEPARTURE, THE L1 DOOR SLIDE CAME OFF. MAINTENANCE REPLACED THE L1 DOOR SLIDE.

Part: LIGHT — MISSING (SEAT 24DE) · airframe 69,912 hrs · 54,100 cycles

DURING PREFLIGHT CHECK, PILOT NOTICED THAT THE EMERGENCY LIGHT AT SEAT 24DE IN THE CABIN WAS MISSING. MAINTENANCE REPLACED THE MISSING LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,292 hrs · 53,671 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROW 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 67,820 hrs · 52,651 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24DE IN THE CABIN WAS INOPERATIVE. MX FOUND A PROBLEM WITH THE EEPL WIRE HARNESS AT AND REPLACED THE HARNESS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,718 hrs · 52,567 cycles

DURING LINE CHECK, FLIGHT DECK EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. POWER SUPPLY BATTERY PACK REPLACED AND OPS CHECKED NORMAL.

Part: DISPLAY — BURNED (FMA) · airframe 67,250 hrs · 52,216 cycles

FLIGHT CREW EXECUTED AN AIRBORNE RETURN DUE TO A BURNING ODOR IN THE COCKPIT. CREW REPORTED THE LOSS OF THE F/O'S FD ALONG WITH E8 CIRCUIT BREAKER TRIPPED. MX COMPLIED WITH CABIN SMOKE/ODOR TROUBLESHOOTING CARD 2120-2367. FOUND F/O'S FMA WITH BURNED ODOR. REPLACED F/O'S FMA, PERFORMED RTS DFGC 1 AND 2 BOTH CHECKED GO.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,007 hrs · 52,030 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE ROWS FROM MID-CABIN AND AFT WERE INOPERATIVE. MX REPLACED THE BATTERIES AT 03CDE. OPS CHECK WAS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,889 hrs · 51,946 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,367 hrs · 51,562 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 28D IN THE CABIN WAS INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT.

Part: WARNING LIGHT — FALSE ACTIVATION (TAIL CONE) · airframe 66,161 hrs · 51,411 cycles

AFTER LEVEL OFF IN CRUISE, "TAILCONE UNSAFE" WARNING ILLUMINATED. QHR PROCEDURES WERE COMPLIED WITH BUT HAD NO IMMEDIATE EFFECT. FLIGHT DESCENDED AND THE LIGHT REMAINED EXTINGUISHED. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED TAILCONE, HANDLE CABLE, AND SWITCH AND ALL WAS FOUND TO BE NORMAL WITH NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,081 hrs · 51,364 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROWS 28DE AND 35DE WERE INOPERATIVE. MX REPAIRED THE EMERGENCY PATH LIGHTS IAW THE SWPM 20-90-03 AND THE OPS CHECK WAS GOOD.

Part: ATTACH FITTING — OUT OF POSITION (DOOR R1) · airframe 65,163 hrs · 50,685 cycles

R1 DOOR WOULD NOT OPEN. MAINTENANCE REPOSITIONED THE DOOR SEAL ATTACH PLATE. DOOR NOW FUNCTIONS NORMALLY.

Part: PANEL — WORN (VERTICAL STAB) · airframe 64,464 hrs · 50,218 cycles

DURING PSV VISIT IN MSP FOUND WORN FASTENER HOLES FOR VERTICAL L/E. BUSHED 16 HOLES AND FABRICATED DOUBLER FROM 7075-T6 .125". WORK ACCOMPLISHED PER DWG SG 09550004.

Part: BUSHING — WORN (TAILCONE) · airframe 64,464 hrs · 50,218 cycles

DURING PSV "P" IN MSP WHILE PERFORMING OPN 6908 FOR THE TAIL CONE FUNCTIONAL CHECK AFT PASSENGER DOOR PULL TEST FAILED. PULL TEST SHOWED 28 LBS VERSUS THE REQUIRED 10 TO 20 LBS. THE "T" PIN AND BUSHINGS WERE REPLACED ON N/R #137, TAIL CONE FUNCTIONAL RE-PERFORMED PER OPN 6908 AND PULL TEST PASSED AT 18LBS.

Part: SPAR CAP — CRACKED (LT HORIZ STAB) · airframe 64,416 hrs · 50,187 cycles

DURING OPN 8903 DISCOVERED CRACK ON LT HORIZ STAB SPAR CAP. ACCOMPLISHED ME-15 EA 09-460214-12AD.

Part: SPAR CAP — CRACKED (RT HORIZ STAB) · airframe 64,416 hrs · 50,187 cycles

DURING OPN 8904 DISCOVERED CRACK ON RT HORIZ STAB SPAR CAP. ACCOMPLISHED ME-16 EA 09-460214-12AD

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,195 hrs · 50,033 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT BOTH AFT OVERWING EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERIES PER AMM AND THE LIGHTS RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 64,148 hrs · 49,997 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS ABOVE THE AFT OVERWING EXIT DOORS INOPERATIVE. MAINTENANCE FOUND BATTERIES NOT HOLDING CHARGE AND REMOVED AND REPLACED. OPS CHECKED GOOD.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 63,599 hrs · 49,612 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,923 hrs · 49,095 cycles

DURING SERVICE CHECK MAINTENANCE FOUND BOTH EMERGENCY EXIT SIGNS ABOVE BOTH AFT OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY PER AMM 33-53. OPERATION OF LIGHTS NOW CHECKS OK.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 62,052 hrs · 48,490 cycles

FLIGHT CREW NOTIFIED MCC THAT EMERGENCY PATHWAY LIGHTS FOR ROWS 2C AND 15D ARE INOPERATIVE. ITEM WAS FORWARDED TO MEL 33-00-24. ON 04/26/11 ATL, MAINTENANCE FOUND WIRE HARNESS CONNECTOR BROKEN. REMOVED AND REPLACED WIRE HARNESS FOR 2C. OPERATION CHECKS GOOD, 15D NO FAULT FOUND. AIRCRAFT IS OKAY FOR SERVICE. MCO/PLACARD WAS REMOVED.

Part: WIRE — BROKEN (CABIN) · airframe 61,722 hrs · 48,277 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 5C WITH BROKEN WIRES. MAINTENANCE REPLACED SEAT HARNESS AT SEAT 5C. OPERATION OF LIGHTS NOW CHECKS OK.

Part: FAN — BURNED (RECIRCULATION) · airframe 61,613 hrs · 48,215 cycles

ON SHORT FINAL, FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR THROUGHOUT THE CABIN. NO SMOKE REPORTED. BURNING ODOR DISSIPATED AFTER 3 MINUTES ON GROUND. RT ENGINE WAS SHUTDOWN UPON CLEARING RUNWAY. APU WAS OFF. MAINTENANCE PERFORMED OPERATION 5088. FOUND RECIRCULATION FAN THE CAUSE OF THE ELECTRICAL BURNING ODOR. REMOVED AND REPLACED FAN PER MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,537 hrs · 48,174 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS AT LT AND RT OVERWING EXITS INOPERATIVE. MX REPLACED BATTERIES AT B5-105 IAW MM. OPS OF LIGHTS NOW CHECK GOOD.

Part: LANYARD — MISRIGGED (L2 DOOR SLIDE) · airframe 61,378 hrs · 48,075 cycles

DURING LINE CHECK, MX FOUND L2 DOOR GIRT BAR LANYARD ROUTED WRONG. MX REROUTED GIRT BAR LANYARD ON L2 DOOR. OK FOR SERVICE. (2011-D0093)

Part: SKIN — CORRODED (FS 242 L29-30L) · airframe 61,110 hrs · 47,901 cycles

DURING HMV CORROSION WAS FOUND ON LWR FUSELAGE SKIN AT LOWER TCAS ANTENNA STA Y=242 BTW LONGERONS 30 AND 29LT. FUSELAGE SKIN WAS REPAIRED IAW ERA 487766-14, REV A.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 61,110 hrs · 47,901 cycles

DURING HMV A CRACK WAS FOUND OF .500" ON FUSELAGE SKIN AT UPPER FWD DOORJAMB CORNER OF THE FWD CARGO COMPARTMENT BTW LONG 20 AND 21 RT AT STA Y=374. FUSELAGE SKIN WAS REPAIRED IAW ERA 487144-14 REV ORIG.

Part: DOUBLER — CRACKED (BS 427 L26-27R) · airframe 61,109 hrs · 47,900 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLER ON STA Y=427 BTW LONGERON PROLONGATION 27-26RT. REPAIR FUSELAGE SKIN IAW ERA 487137-14, REV ORIG.

Part: SKIN — CRACKED (BS 427) · airframe 61,109 hrs · 47,900 cycles

DURING HMV A CRACK WAS FOUND OF 1.531" LENGTH ON LOWER AFT CORNER FS Y=427 OF FWD CARGO COMPARTMENT. REPAIR FUSELAGE SKIN IAW ERA 487137-14, REV ORIG.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 61,109 hrs · 47,900 cycles

DURING HMV CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LOWER BEAM BELOW REPAIR DOUBLER BETWEEN STA Y=1155-1212. REPLACE BEAM IAW SRM 51-30-5.

Part: SKIN — CORRODED (FS 591 L29-30R) · airframe 61,109 hrs · 47,900 cycles

DURING HMV CORROSION WAS FOUND ON EXTERIOR FUSELAGE SKIN FROM STA Y=591 TOY=597 BETWEEN LONGERONS 29-30 RT SKIN WAS REPAIRED IAW ERA 487752-14, REV ORIG.

Part: SUPPORT CHANNEL — DAMAGED (RT MLG) · airframe 61,109 hrs · 47,900 cycles

DURING HMV TOOLING MARKS WAS FOUND ON WALL BETWEEN BUSHING AND BEARING BORES AT RT MLG SUPPORT FITTING. REPAIRED SUPPORT FITTING IAW EO 09-093855-03AD REV B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,109 hrs · 47,900 cycles

DURING HMV TOOLING MARKS WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLER BETWEEN STA Y=638 TO 642,Y=658 TO 662,Y=668 TO 673 AND Y=681 TO 688 AND LONGERON PROLONGATION 27 TO 28RT BELOW MID CARGO COMPARTMENT DOORJAMB LOWER BEAM DOUBLER WAS REPAIRED IAW ERA 487149-14, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,691 hrs · 47,593 cycles

MX FOUND THAT THE UPPER AFT EMERGENCY EXIT SIGNS DID NOT ILLUMINATE. MX REPLACED THE BATTERY PACK. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,660 hrs · 47,575 cycles

MX FOUND THE AFT LT AND RT OVERWING EXIT UPPER EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE BATTERIES FOR B5-105. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (MASTER) · airframe 52,000 hrs · 41,819 cycles

ON TAXI IN RAMP REPORTED SMOKE/STEAM COMING FROM UNDER A/C. CALLED MTC TO INVESTIGATE SAME. FOUND SHIPS BATTERIES OVERHEATED. NO DAMAGE TO A/C, BATTERIES OR CHARGER. REPLACED MAIN BATTERIES AND CHARGER. OP AND SYSTEM TESTS OK.

Part: INLET — DAMAGED (ENGINE) · airframe 51,615 hrs · 41,596 cycles

DURING SHOP VISIT EROSION AND DAMAGE FOUND TO INLET COWL OUTER COMPOSITE SKIN. REPAIRED PER ERA 095803-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,493 hrs · 37,878 cycles

FUSELAGE OVERWING FRAME AT STATION 886 FOUND CRACKED AT LONGERON 18L. FRAME REPLACED I/A/W ERA 096171-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,493 hrs · 37,878 cycles

FUSELAGE SKIN BUSHED ADJACENT TO THE AIRSTAIR DOOR CUTOUT AT TWO LOCATIONS BETWEEN LONGERONS 21L AND 22L. REPAIRED I/A/W ERA 096251-14.

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE) · airframe 46,445 hrs · 37,844 cycles

SHUT DOWN RT ENGINE IN FLIGHT AFTER T/O AND CLEANUP. THE RT ENG STARTED SURGING, RT GEN DROP OFF AND ON. SHUT DOWN RT ENG IAW MANUAL. ENGINE WINDMILL FOR APPROX 10-12 MIN, TOTAL TIME FROM OFF TO ON WAS 20 MIN. WINDMILL OIL PRESS >10 PSI. PERFORMED WINDMILL INSP AND REPLACED ENG OIL FILTER PER M/M. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL. PERFORMED IDLE CHECK, PART PWR CHECK, AND T/O POWER CHECK PER PFHB. ALL TEST ARE GOOD.

Part: WATER HEATER — FAILED (AFT LEFT LAV) · airframe 45,548 hrs · 37,185 cycles

AFT LT LAV SMOKE DET BEEPING IN FLT. WATER HEATER WAS VERY HOT INITIALLY OPENED DETECTOR AND DISCONNECTED BATTERY NO ODOR DETECTED. PULLED CB'S FOR AFT LT LAV MIRROR, FLUSH MOTOR AND WATER HEATER. RAN HOT WATER UNTIL COOL. AFT F/A INTERPHONE PANEL WAS WARM BUT BECAME COOL. RE-ATTACHED SMOKE DET BATTERY RED LIGHT OUT, NO BEEPING. RESET ALL CB'S, INSPECTED AFT LT LAV FOUND WATER HEATER OVERHEATING. PULLED AND COLLARED C/B FOR WATER HEATER. FWD TO MCO AND PLAC PER MEL 25-00-12D. ALSO FOUND WATER IN SMOKE DETECTOR. REPLACED SMOKE DETECTOR, NO WATER LEAKS FOUND.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 44,333 hrs · 36,330 cycles

ROW 1D & FWD GALLEY EMERGENCY LIGHT BURNED OUT. FOUND BAD WIRE TO GALLEY LIGHT HAD TO REWIRE.

Part: STRUT — LEAKING (NLG) · airframe 42,755 hrs · 35,280 cycles

ON TAKEOFF NOSE LANDING GEAR REMAINED EXTENDED, RED NOSE GEAR LIGHT ON. CA:REPLACING NOSE GEAR STRUT ASSY. REPLACED NOSE GEAR INNER CYLINDER AND PACKINGS.

Part: ENGINE — LEAKING (NR 1) · airframe 42,236 hrs · 34,904 cycles

PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL QTY..WIND- MILL TIME 15 MIN...MIN OIL PRESS 8 PSI...MAX OIL TEMP 162- FOR LESS THAN 5 MIN. REPLACED NR 1 ENGINE PER TRANSMITTAL 9T102 ...

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 42,236 hrs · 34,904 cycles

PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL QUANTITY WINDMILL TIME 15 MIN, MINIMUM OIL PRESSURE 8 PSI. MAX OIL TEMP 162 FOR LESS THEN 5 MIN. REPLACED NR 1 ENGINE ASSY.

Part: POWER SUPPLY — INOPERATIVE (CABIN ROW 31) · airframe 40,667 hrs · 33,791 cycles

EMERGENCY EXIT LIGHT INOPERATIVE ROW 24 THRU 36. REPLACED POWER SUPPLY AND REPAIR WIRE AT SEAT B25 LIGHTS CHECK GOOD.

Part: RACK — UNSERVICEABLE (B5-12) · airframe 40,026 hrs · 33,333 cycles

ALL AFT SECTION EMERGENCY LIGHTS INOP. REPLACED BATTERY AND RACK...NOW OPS NML

Part: BATTERY — UNSERVICEABLE (MID CABIN) · airframe 40,019 hrs · 33,327 cycles

FWD OVERHEAD OVERWING EMERGENCY LIGHTS INOP...RPLD BATTERIES NOW OPS NML

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,467 hrs · 32,954 cycles

FWD AUX EXIT LIGHTS FAILED TO OPERATE DURING LAYOVER CHECK. REPLACED POWER SUPPLY B5-103, OPS NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 39,348 hrs · 32,857 cycles

AFTER PUSH BACK EMERGENCY LIGHTS IN F/C FAIL TO COMES ON. REPLACED FUSE IN F/C BATT PACK BETWEEN WINDOWS 7 AND 8, FOUND SHORT IN LIGHT ASSY FOR SEAT 4DC. REPLACED SAME, CHECKS GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 38,175 hrs · 31,970 cycles

AT 1000 FT AGL CREW EXPERIENCED SMOKE/HAZE IN CABIN. ANTI ICE SYSTEM NOT IN USE. REPLACED NR 1 ENGINE FOR INTERNAL OIL LEAK.

Part: SCREEN — CLOGGED (LT ACM) · airframe 38,071 hrs · 31,895 cycles

UNABLE TO PRESSURIZE A/C WITH LEFT PACK. CLEARED CLOGGED SCREEN FROM ACM TO ACM ANTI ICE VALVE.

Part: ACM — LEAKING (ACM BAY) · airframe 36,415 hrs · 30,662 cycles

ON APPROACH TO KBOS WITH ENGINE WING ANTI-ICE X BLEEDS OPEN AND APU RUNNING. PAX AND F/AS COMPLAINED OF SMOKE IN CABIN AND BOTH FORE AND AFT SMOKE DETECTORS WENT OFF. FOUND RT ACM LEAKING OIL. REPLACED SAME. PERFORMED DUCT BURNOUT.

Part: PANEL — FAILED (E/E BAY) · airframe 36,050 hrs · 30,399 cycles

EN ROUTE CVG, LEFT AC BUS OFF, DC BUS OFF, EMER AC BUS OFF, AC CROSSTIE LOCKOUT LIGHTS ILLUMINATED, REF POM PROCEDURE: EMER POWER ON, RECOVERED EMER AC BUS. DIVERTED KIAH, EMERGENCY DECLARED. REMOVED AND REPLACED THE APU GCU WHICH HAD A DIST SYS FAULT. RAN APU NR 1 AND 2 ENG''S PER PFHB AND TRANSFERRED POWER SOURCES, ALL INDICATIONS NORMAL.

Part: COALESCER BAG — CONTAMINATED (ACM BAY) · airframe 35,992 hrs · 30,359 cycles

ON SHORT FINAL 500 AGL, CABIN REPORTED STRONG ELECTRICAL SMELL (BURNING ODOR). INSPECTED CABIN, EXTERIOR, BAG BINS, CABIN RECIRC FAN. NO DISCREPANCIES. INSP AIR COND DUCTS DOWNSTREAM OF ACMS. REPLACED COALESCER BAGS. NO EVIDENCE OF CONTAMINATION FROM ENGS OR APU. RAN ENGS AT HIGH POWER WITH PACKS FULL HOT. NO UNUSUAL ODORS. ALL DUCTS REMOVED FOR INSP LEAK CK GOOD. OPN 5008 COMPLIED WITH.

Part: APU — LEAKING (AFT) · airframe 35,664 hrs · 30,113 cycles

AFTER TAKEOFF FROM PWM, NORMAL POWER TAKEOFF WITH ENGINE ANTI ICE ON, GOT A STRANGE OIL ODOR THROUGH OUT CABIN. ODOR CLEARED UP SHORTLY DURING CLIMB. PERFORMED DUCT BURNOUT.

Part: UNKNOWN — SMOKE (TAIL)

ON SHORT FINAL WITH ENG AND AIRFOIL ANTI ICE ON, A BURNING SMELL WAS NOTICED THRU OUT A/C. SMOKE DETECTOR IN AFT LT LAV WENT OFF. F/A CHECKED LAV AND TRASH BIN, ALL WAS NORMAL. PERFORMED DUCT BURNOUT AND PNEU SYS CK OUT PER M/M, OPS NORMAL. NO SMELL NOTED.

Part: BATTERY — DISCHARGED (COCKPIT)

EMERGENCY LIGHTS INOP IN COCKPIT OVER ENTRY DOOR AND UNDER GLARESHIELD. REPLACED BATTERIES IN BATTERY PACK, CKS GOOD.

Part: APU — CONTAMINATED (APU BAY)

ON FINAL INTO CLE ON FLT 1156/17 AT 1000 FT, THE AFT FLT ATTN REPORTED AN OILY ODOR AND HAZE INDICATIONS IN CABIN. TAIL ANTI ICE WAS ON, LAV SMOKE ALARMS SOUNDED. ENG ANTI ICE WAS ALSO ON. INSPECTED ENG PNEU DUCTS, CHECKED GOOD. INSPECTED A/C FOR HYD LEAK, NONE FOUND. REPLACED WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT PROCEDURE, CHECKS GOOD. FOUND OIL IN APU INLET DEACTIVATED APU PER MEL 49-00-01A.

Part: SWITCH — INOP (PEDESTAL)

SLAT DISAGREE LIGHT FLICKERED DURING APPROACH THROUGH ALL FLAP SETTINGS. NO ROLLING TENDENCY. REPLACED FLAP/SLAT HANDLE POSITION SWITCH ASSY, ADJUSTED AND TESTED PER M/M 27-80-07-2. OK FOR SERVICE.

Part: SKIN — DENTED (BS 218)

FUSELAGE SKIN WAS FOUND DENTED AT APPROX FS 218 AND L19L. CUTOUT DIMENSIONS ARE APPROX 16 BY 17. REPAIRED PER ERA 333366-14, REV A.

Part: SKIN — DENTED (BS 232)

FUSELAGE SKIN DENTED BETWEEN FS 229 AND 234 BETWEEN L17L AND L18L. CUTOUT DIMENSIONS ARE APPROX 5 BY 11. REPAIRED PER ERA 333371-14, REV A.

Part: SWITCH — OUT OF ADJUST (NLG)

AFTER T/O GEAR RETRACTED, NOSE GEAR INDICATION UNSAFE LIGHT RED ILLUMINATED ABOUT 12 TO 15 TIMES FOR ONE TO THREE SECONDS. THIS HAPPENED FOR ABOUT 5 MINUTES AFTER GEAR RETRACTION. ADJUSTED NOSE GEAR LOCK SWITCH. SWUNG NOSE GEAR, OPERATES NORMALLY.

Part: CONNECTOR — DAMAGED (TAIL COMPT)

EMERGENCY LIGHTING ON WALL IN TAIL COMPARTMENT INOP. REMOVED LIGHT ASSY, FOUND WIRING PULLED FROM CONNECTORS. INSTALLED NEW CONNECTORS AND REINSTALLED LIGHT ASSY, LIGHT OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

FWD FLASHLIGHT AT THE AFT FLIGHT ATTENDANT STATION INOP. REPLACED FLASHLIGHT ASSY AND BATTERY.

Part: COALESCER BAG — DIRTY (LT/RT)

ON FINAL AT APPROX 4000 FT GOT A BURNING SMELL IN COCKPIT AND THE CABIN. BOTH AFT LAV SMOKE ALARMS SOUNDED. ORDER CLEARED AND SMOKE ALARMS STOPPED JUST AFTER LANDING. INSPECTION A/C FOR FLUID LEAKS. FOUND RESIDUAL DE-ICE FLUID. REPLACED BOTH A/C WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT. ODOR DISSIPATED. RUNUP NORMAL.

Part: HYD LINE — BROKEN (TAIL CONE)

AT FLT LEVEL 330 RT HYD QTY WAS 8 (11 IN CHOCKS) AFTER 2 MIN QTY WENT TO 6. SHUTOFF RT SIDE WENT TO 19. TURNED BACK ON TO LAND WENT DOWN TO 4 WITH AMBER LIGHT. AFTER SHUTDOWN QTY STEADY AT 6 WITH AMBER LIGHT ON. REPAIRED BROKEN HYDRAULIC LINE LOCATED ABOVE THE RIGHT THRUST REVERSER CONTROL VALVE.

Part: FILTER — DAMAGED (RT HYD SYST)

RT HYD QUANTITY AT ONE QUART, PRESURE OK AT TOP OF DESCENT. THROTTLES TO IDLE HYD RT PRESURE WENT TO ZERO. ACCOMPLISHED RT HYD FAILURE CHECKLIST. INDICATION NORMAL LANDING GEAR ALT EXTENSION USED. FOUND RIGHT HYD FILTER HOUSING ASSEMBLY POP UP FILTER BROKEN OUT. REPLACED FILTER HOUSING ASSEMBLY.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOOR)

LOUD NOSE GEAR DOOR AFTER GEAR RETRACTION ON TAKEOFF. FOUND ON ARRIVAL LEFT NOSE GEAR DOOR OPEN. CLOSED DOOR, CK DOOR LOCK MECH. DOOR CKS OK PER MM CHAPT 32 AND 52.

Part: DOOR — UNLATCHED (E/E COMPT)

NOSE AREA VIBRATION AFTER T/O. FOUND LATCH ON UPPER FRONT E/E DOOR UNLATCHED, RELATCHED.

Part: MEDICAL KIT — DEFECTIVE (CABIN)

EMERGENCY MEDICAL KIT USED. REPLACED EMERGENCY MEDICAL KIT.

Part: BUNGEE CYLINDER — FAILED (NOSE GEAR)

LANDING GEAR WOULD NOT EXTEND, (NOSE GEAR) RECYCLED, NO NOSE GEAR. USED EMERGENCY EXTENSION, NOSE GEAR EXTENDED. REPLACED NLG BUNGEE CYLINDER AND LUBED NLG. CYCLED NLG SEVERAL TIMES. OPS CKS NORMAL.

Part: TURBINE — OIL LEAK (APU)

CLIMBING THROUGH 11.0 TURNED ENG A/I ON, SMOKE IN CABIN AND COCKPIT. APU NOTICED TO HAVE EXCESSIVE OIL LEAKAGE. PUT APU ON MCO, BURNED BOTH PACKS OUT.

Part: COALESCER BAGS — DIRTY (CABIN)

ON DESCENT, AT 1,200 WITH WING/ENG ANTI-ICE ON, CABIN FILLED WITH STRONG ODOR AND HAZE, SETTING OFF ALL 3 SMOKE DETECTORS. TURNED WING ANTI-ICE AND PACKS S/W TO HP BLEEDS OFF, WHICH BEGAN TO CLEAR CABIN BY LANDING. REPLACED WATER SEPARATOR BAGS, RAN APU AND BOTH ENGINES WITH PACKS ON. AIRFLOW ANTI-ICE ON, OPS CHECK NORMAL.

Part: AIR DISTR — SMOKE (CABIN)

AFTER T/O, SMOKE APPEARED IN CABIN. SMOKE DETECTORS LT AND RT WENT OFF. ACCOMPLISHED CHECKLIST AND SMOKE DISAPPEARED WITH REDUCED POWER. COULD NOT ISOLATE PROBLEM PACK AND SMOKE REAPPEARED ON FINAL. PERFORMED SMOKE BURNOUT, REPLACED BOTH PACK COALESCER BAGS, RAN BOTH ENGINES TO T/O POWER WITH PACKS AND NO SMOKE WAS NOTED.