N967DL

Part: LINE — LOOSE (NR 1 PYLON) · airframe 73,192 hrs · 55,019 cycles

NR 1 ENGINE PYLON FIRE SUPPRESSION LINE LOOSE @ PYLON. TIGHTENED FIRE SUPPRESSION LINE @ PYLON PER AMM 20-30. (LP1275066)

Part: VALVE — FAILED (FUEL HEAT) · airframe 73,059 hrs · 54,890 cycles

DIVERTED DUE TO RIGHT ENGINE HIGH OIL TEMPERATURE. AFTER TAKEOFF OIL TEMP STEADILY CLIMBED TO 135DEG. FLT CREW SHUT DOWN ENGINE PER QRH. MAX OIL TEMP REACHED WAS 157 AFTER SHUT DOWN. MTC FOUND FUEL HEAT VALVE FAILED OPEN. DRAINED AND RE-SERVICED OIL TANK, REPLACED OIL FILTER PER AMM FOR HIGH OIL TEMP. REPLACED FUEL HEAT VALVE. RAN ENGINE OIL TEMP NORMAL, A/C RTS.

Part: DISPLAY — FAILED (WX RADAR) · airframe 72,971 hrs · 54,811 cycles

IN ROUTE DURING CRUISE, ELECTRICALLY STARTING GETTING STRONG WX/TCAS DISPLAY STARTED BLANKING OUT. TURNED DISPLAY TO OFF FUMES SUBSIDED. R & R WX TCAS RADAR CENTER DISPLAY DUE TO ODI IN RIC FOR SMOKE ODOR IAW MD-88 AMM 34-41. OPS CHK GOOD.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 72,589 hrs · 54,480 cycles

DAMAGED SLIDE TAIL CONE. HORIZONTAL STABILIZER P/N: 55-0130-501 S/N: UNK7Q1JRB WAS REMOVED PER MD88 AMM 55-10-00 AND A SERVICEABLE HORIZONTAL STABILIZER P/N: 55-0130-501 S/N: 53423 MUST BE INSTALLED WITH AMDS 5510-4135. STABILIZER, ASS OFF 88-5510-9-0001 00967 ON 88-5510-9-0001 53423. (LP1108056)

Part: CABLE — TORN (SLIDE) · airframe 72,589 hrs · 54,480 cycles

RII, DURING CONNECTION OF SLIDE DEPLOYMENT LANYARD TO TAILCONE KEVLAR CABLE, WAS FOUND TORN KEVLAR CABLE IN REF AMDS 5350-4287 STEP 5 AND AMDS 5350-01077-0101 AT AFT ACCESSORIES COMPARTMENT. KEVLAR CABLE OF TAILCONE SLIDE WAS REPLACED PER MD88 AMM 53-53-00-401. (LP1108997)

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 72,589 hrs · 54,480 cycles

CRACK OF 0.343" WAS FOUND ON RH HORIZONTAL STABILIZER UPPER REAR SPAR AT AFT BARREL NUT HOLE. HORIZONTAL STABILIZER P/N: 55-0130-501 S/N: UNK7Q1JRB WAS REMOVED PER MD88 AMM 55-10-00 AND A SERVICEABLE HORIZONTAL STABILIZER P/N: 55-0130-501 S/N: 53423 MUST BE INSTALLED WITH AMDS 5510-4135. STABILIZER, ASS OFF 88-5510-9-0001 00967 ON 88-5510-9-0001 53423. (LP1108084)

Part: SLIDE — DAMAGED (TAILCONE) · airframe 72,589 hrs · 54,480 cycles

DAMAGED SLIDE TAIL CONE. TAILCONE SLIDE P/N: D29984-213 S/N: 1437 WAS REPLACED WITH SERVICEABLE SLIDE P/N: D29984-213 S/N: 0873 AND APLICABILITY WAS VERIFIED PER MD88 AIPC 25-60-00-09C ITEM 266. SLIDE, ASSEMBLY OFF 88-2561-9-0006 01437 ON 88-2561-9-0006 00873. (LP1108117)

Part: UNKNOWN — HAZE (CABIN) · airframe 71,464 hrs · 53,507 cycles

ON FIRST FLIGHT OF DAY AFTER APU START, PACK WENT FULL HOT AND AFT PORTION OF THE CABIN FILLED WITH HEAVY HAZE. C/W NO GO ODI 2172. MCC NOTIFIED. R/R WATER SEPARATOR BAGS IAW MD88 AMM 21-20. FOUND NOTHING ABNORMAL. INSPECTED TAIL SECTION OF PNEUMATIC DUCTS . SUSPECTED CREW OVERTEMPED PNEUMATIC SYSTEM. (899852) RAN BOTH ENGINES WITH PAX ON HIGH WITH NO DISCREPS FOUND. (LP5058600)

Part: SPRING — MISSING (TAILCONE) · airframe 70,950 hrs · 53,051 cycles

SPRINGS MISSING FROM T-FITTING ON AFT ENTRY DOOR CABLE RELEASE FOR TAILCONE. INSTALLED MISSING SPRINGS, MPN: 4934469-1, AMM 53-53. FUNCTIONAL CHECK TO BE ACCOMPLISHED ON AMI-TASK 5350-01077-0101.

Part: FASTENER — MISSING (ACCESS DOOR) · airframe 70,944 hrs · 53,045 cycles

NOSE FORWARD LEFT HINGE FASTENER MISSING ON OVAL PLUG ACCESS DOOR. INSTALLED NEW FASTENER AND SECURED HINGE. REFERENCE IPC 52-40-02-01A. PN ON 4002-15W. SDR REPORTED BECAUSE THE CAMLOC FASTENER COULD HAVE POSSIBLY DEPARTED THE AIRCRAFT DURING FLIGHT.

Part: UNKNOWN — ODOR (CABIN) · airframe 70,754 hrs · 52,884 cycles

DURING DECENT, AFT FA CALLED ABOUT AN ELECTRICAL ODOR COMING FROM FWD GALLEY AND FIRST CABIN. RAN QRH, TURNED OFF GALLEY POWER, ODOR SUBSIDED. CALLED BACK FEW MINS LATER, THE ODOR WAS STARTING AGAIN. CONTINUED QRH UNTIL LANDING. TROUBLESHOT THE ACFT AFTER SMELLING THE ELECTRICAL ODOR. CHECKED SEAT 2AB WHERE THE ODOR WAS NOTICED. FOUND NO INDICATION. FWD OF THE ACFT WAS AN ODOR OUTSIDE. CHECKED THE E & E FWD NOSE, AFT TAIL SECTION, COULD NOT DUPLICATE THE ODOR OR FIND ANY INDICATION OF BURNING. RAN THE APU AND BOTH ENGINES AND FOUND NO BURNING OR ODOR. COMPLIED WITH PNEUEMATIC DIS CABIN SMOKE/ODOR TS FLOW CHART JIC 2120-2367. NO ODORS DETECTED. PERFORMED HIGH POWER ENG RUN W/ LT AND RT AC BUSSES ISOLATED DURING TAXI. REMOVED ALL FWD GALLEY COFFEE DISPENSERS AND INSPECTED ELEC CONNECTORS AND WIRING. REMOVED THE OVEN AND INSPECTED THE ELECT CONNECTORS AND WIRING. ALL OK. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 70,651 hrs · 52,797 cycles

L2 ENTRY LIGHT INOP. FOUND BAD BATTERY PACK. REMOVED AND REPLACED BATTERY PACK IN F/C OPS CHECK GOOD IAW AMM 33-50.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,116 hrs · 52,357 cycles

OVHD EMERGENCY LIGHTS INOP IN FIRST CLASS. RPLD BATTERIES PER AMM 33-53. OP CKS GOOD.

Part: MOUNT — DEFECTIVE (EVAC SLIDE) · airframe 70,069 hrs · 52,320 cycles

FWD ENTRY DOOR EVACUATION SLIDE FOUND PIN NOT ENGAGE. R&R DOOR SLIDE MOUNT REF. W/C 2561-4964.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,498 hrs · 51,870 cycles

EMERGENCY ESCAPE CEILING LIGHTS INOP ON TEST BETWEEN ROWS 27-31. REPL BATTERIES ABOVE SEAT ROW 29DE PER AMM 33-53. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,214 hrs · 51,650 cycles

EMERGENCY LIGHTS INOP FWD DOOR'S. REPLACED BATT, OPS NOW OK PER AMM 33-53.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 68,855 hrs · 51,373 cycles

L1 DOOR SLIDE PINS NOT ENGAGED IN FRONT COVER. REPLACED L1 DOOR SLIDE, IAW AMM 25-62-00-201.

Part: ANNUNCIATOR — LOOSE (COCKPIT) · airframe 68,086 hrs · 50,748 cycles

WITH AIRCRAFT ON GROUND SERVICE POWER TURNED BATT PWR SW ON AND POWERED AIRCRAFT WITH GROUND POWER. WITHIN 5 MINUTES STRONG ELECTRICAL BURNING SMELL IN COCKPIT. DEPOWERED AIRCRAFT. T/S AND FOUND PILOTS FMA AT FAULT/ FMA LOOSE IN HOUSING/ FORWARD PANEL. CAPTAINS PANEL PULLED BACK FOR MAINT REF AMM 22-17. REPLACED CAPTAINS FMA PER AMM 22-17. PERFORMED RTS PER AMM -22-10 SYSTEM CKS GOOD.

Part: LIGHT — INOPERATIVE (CATWALK) · airframe 68,007 hrs · 50,687 cycles

EMERGENCY LIGHTS ON CATWALK NEED RELAMPED SEVERAL LOCATIONS. RELAMPED CATWALK EMERGENCY LIGHTS SEVERAL LOCATIONS PER AMM 33-52. CKS GOOD.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 68,007 hrs · 50,687 cycles

EMERGENCY LIGHT AT SEAT 31D INOP. REPLACED SEAT HARNESS AND PIG TAIL PER AMM 33-52.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 67,483 hrs · 50,283 cycles

LOOSE ON TWO ROWS FASTENERS ABOVE THE SPLICE (9E/A) AND TWO ROWS FASTENERS BELOW THE SPLICE (28E/A) STA ZFS= 52.26 AT LE VERTICAL STABILIZER. WORK WITH CARD 5530-01045-08. COUNTERSINKS AND HOLES WERE EVALUATED AND WAS FOND 34 WITHIN LIMITS AND 3 OUT OF LIMITS. OUT LIMITS HOLES WERE REPAIR PER DWG SG09550004 REV D AND CARD 5530-01045-08.

Part: SUPPORT — CORRODED (BS 160) · corrosion level 2 · airframe 67,483 hrs · 50,283 cycles

CORROSION ON LOWER SUPPORT OF EPC PANEL AFT FACE AT BS 160. THE SUPPORT WAS REPLACED IAW SRM 51-30-2, 51-30-1, 51-30-5, AND DWG 9955780-7, REV LA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,215 hrs · 50,072 cycles

COCKPIT AND GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERIES IAW AMM 33-53-00.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 66,664 hrs · 49,700 cycles

RUDDER HAS FLAME SPRAY PEELING AND DAMAGED. RUDDER WAS REPLACED.

Part: SUPPORT FRAME — CRACKED (TAILCONE) · airframe 66,345 hrs · 49,427 cycles

TAIL CONE SUPPORT FRAME BS 1510 CRACKED. REPLACED THE FRAME IAW DWG 9911843. (LP2726274)

Part: SUPPORT FRAME — CRACKED (TAIL CONE) · airframe 66,345 hrs · 49,427 cycles

TAILCONE SUPPORT FRAME BS 1510 CRACKED. REPLACED THE SUPPORT FRAME IAW DWG 9911843.

Part: HANDLE — LOOSE (TAILCONE RELEASE) · airframe 66,345 hrs · 49,427 cycles

TAILCONE INTERIOR RELEASE HANDLE. FOUND THE HANDLE FWD RETENTION CLIP DAMAGED. REMOVED AND REPLACED INTERIOR RELEASE HANDLE IAW AMM 25-62.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,845 hrs · 48,288 cycles

THE 1L DOOR EMERGENCY ESCAPE SLIDE FELL OFF OF THE DOOR. MAINTENANCE INSPECTED THE SLIDE AND REINSTALLED IT. THE GIRT BAR WAS FOUND MIS-ALIGNED AND WAS THEN RE-ALIGNED PRIOR TO INSTALLATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 64,150 hrs · 47,793 cycles

MEM MAINTENANCE FOUND LT FORWARD EMERGENCY OVERWING SIGN INOPERATIVE. A DAMAGED WIRE WAS FOUND AT THE EMERGENCY EXIT ROW AND WAS REPAIRED. LIGHT CHECKED OK.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,481 hrs · 49,551 cycles

CORROSION ON SETTLEMENT AREA FUEL ACCESS PANEL 1434C. THE ACCESS PANEL WAS REPLACED IAW CMM 28-40-36.

Part: DOOR FRAME — CRACKED · airframe 62,544 hrs · 46,649 cycles

2 CRACKS WERE FOUND OF, 0.187 AND 0.093 OF LENGTH, AT THE SAME FASTENER HOLE ON UPPER FWD DOOR JAMB CORNER STA Y=173 AT FWD SERVICE DOOR, R1. AREA WAS REPAIRED IAW ER/A 534329-14, AD REV ORIG. LP 1926236.

Part: BEAM — CORRODED (FUSELAGE) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON MID CARGO COMP LWR DOOR JAMB BEAM BTW STA Y=636-645, Y=654-679, ALSO ON PREVIOUS REPAIR DOUBLERS BTW Y=645-654 AND Y=679-690. LOWER DOOR JAMB BEAM WAS REPAIRED IAW ER/A AND SRM.

Part: FRAME — CRACKED (BS 1485) · airframe 62,542 hrs · 46,648 cycles

CRACKED FRAME BS 1485 CANT AND 1 HR POSITION. CRACKED FRAME WAS REPAIRED IAW SRM 53-03D, FIG.49. LP 1922656.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1472C. FUEL ACCESS 1472C WAS REPLACED DUE TO EXCESSIVE DAMAGE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1367C. FUEL ACCESS 1367C WAS REPLACED DUE TO EXCESSIVE DAMAGE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NBR1460C. CORROSION FOUND OUT OF LIMITS IAW SRM. ACCESS PLATE WAS REPLACED.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON THE RT CARGO TRACK BETWEEN BS 1212 - 1320. THE CARGO TRACK WAS REPLACED IAW SRM.

Part: FRAME SPLICE — CORRODED (BS 1231) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON SPLICE BS 1231 BETWEEN LONGERONS 28 - 30R. THE SPLICE WAS REPLACED IAW SRM.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · airframe 66,604 hrs · 49,654 cycles

SEVERAL POINTS OF CORROSION ON THE LT CARGO TRACK BETWEEN BS 1212 - 1320. THE CARGO TRACK WAS REPLACED IAW SRM.

Part: FRAME — CORRODED (BS 1308) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON FRAME BS 1308, LONGERONS 28L - 28R. THE REPAIR DOUBLER WAS REPLACED IAW SRM.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF THE ACCCES PANEL 1371C. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-22-2A AND THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORRSOION ON COUNTERSINK AND SETTLEMENT AREA OF ACCESS PANEL 1365C. CORROSION OUT OF LIMITS IAW SRM. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,604 hrs · 49,654 cycles

CORRSOION ON COUNTERSINK AND SETTLEMENT AREA OF THE ACCESS PANEL 1377C. THE ACCESS PANEL WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,542 hrs · 46,648 cycles

CRACKED LONGERON 12L BS 1437. LONGERON 12L WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: INTERCOSTAL — CORRODED (BS 1308-1320) · airframe 66,604 hrs · 49,654 cycles

CORROSION ON LEFT INTERCOSTAL BS 1308 - 1320. THE INTERCOSTAL WAS REPLACED IAW SRM.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,489 hrs · 49,557 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA AND DEGRADED SEALANT ON ANCHOR NUT AT FUEL ACCESS PANEL 1414C. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: INTERCOSTAL — CORRODED (BS 1308-1320) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON INTERCOSTAL OVER LONGERON 28R BETWEEN BS 1308-1320 . THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1046-1079) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB BS 1046-1049 AND 1060-1079, RBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-7 AND 53-05 FIG 131A-14.

Part: LONGERON — CRACKED (BS 984) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LONGERON 3R AT BS 984. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 845) · airframe 62,542 hrs · 46,648 cycles

CRACKED LONGERON 2 RT BS 845 AT CABIN STRUCTURE. REPAIR WAS INSTALLED IAW SRM 53-02, FIG 18. LP 1909457.

Part: DOUBLER — CORRODED (BS 1338) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON DOUBLER ON DOME BETWEEN LONGERON 29L AND 29R BS 1338. THE DOUBLER WAS REPLACED IAW SRM 53-14-3 FIG. 7 ITEM 59 , 51-30-2 , 51-30-5 , 51-10-3 PARAGRAPH 21 AND 14.

Part: FRAME SPLICE — CORRODED (BS 1338) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON SPLICE BETWEEN LONGERON PROJECTION 26 AND 27R, BS 1338 AT AFT CARGO COMPARTMENT. SPLICE WAS REPLACED IAW SRM 53-03, FIG 37, 51-10-3 PARA 14 AND 21, 51-30-5. LP 1909271.

Part: SUPPORT FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON RT MLG SUPPORT FITTING BUSHING BORE, ALSO CORROSION AND TOOL MARKS ON BUSHING BORE BOTTOM. DAMAGE ON BUSHING BORE WAS REPAIRED IAW DWG SR 09570087. NOTE II, REV B AND DAMAGE ON BUSHING BORE BOTTOM WAS REPAIRED WITH FINAL LENGTH:1.202" SO IT WAS OUT OF LIMITS IAW DWG SR09570087, REV B AND DWG 5935812, REV BB ; THEREFORE IT WAS PERFORMED IAW ER/A 534336-14AD, REV ORIG. LP 1913313.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE, ALSO CORROSION AND TOOL MARKS ON BUSHING BORE BOTTOM. DAMAGE ON BUSHING BORE WAS REPAIRED IAW SR DWG SR09570087. NOTE II, REV B AND DAMAGE ON BUSHING BORE BOTTOM WAS REPAIRED WITH FINAL LENGTH: 1.218" SO IT WAS OUT OF LIMITS, THEREFORE WAS PERFORMED IAW 534336-14AD, REV ORIGINAL LP 1913307.

Part: DOUBLER — CORRODED (BS 1338) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON DOUBLER BS 1338 BETWEEN LONGERONS 28L - 28R AT AFT PRESSURE BULKHEAD AREA. THE DOUBLER WAS REPLACED IAW SRM 51-10-4 , 51- 30-2 , 51-30-5 , 51-10-3 PARAGRAPH 14 AND 21.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1454C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1464C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1456C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1476C. THE ACCESS PANEL WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,542 hrs · 46,648 cycles

CRACKED LONGERON 15R BS 1437. LONGERON REPAIRED IAW SRM 53-02.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF THE ACCESS PANEL 1478C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1470C. THE ACCESS PANEL WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 1189-1193) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON LT SEAT TRACK LBL 44, BS 1189 - 1193. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1 , 51-30-5 , 51-10-4 , 51-10-3 PARAGRAP 21 , 14 , 38.

Part: TAB — DAMAGED (RUDDER) · airframe 62,542 hrs · 46,648 cycles

DAMAGE METALIZED COVER ON RUDDER TAB LT SIDE. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1A PAR. 23. LP 1904665.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,574 hrs · 49,628 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1466C. THE ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1183-1187) · airframe 66,534 hrs · 49,594 cycles

CUSP WEB CORRODED OUT OF LIMITS, BS 1183-1187 LBL 54-60. REPAIRED THE CUSP WEB.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1311C CORRODED OUT OF LIMITS, REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1410C CORRODED OUT OF LIMITS, REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 1250-1271) · airframe 66,534 hrs · 49,594 cycles

PREVIOUS CUSP WEB REPAIR DOUBLER CORRODED OUT OF LIMITS, BS 1250-1271 BETWEEN RBL 54 TO 60, A NEW REPAIR WAS INSTALLED.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,542 hrs · 46,648 cycles

DAMAGED METALLIZED COAT ON RT SIDE OF RUDDER. METALLIZED COAT ON RT SIDE OF RUDDER WAS REPAIR IAW SRM 51-70-1A, PAR 23. LP 1904856.

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 62,542 hrs · 46,648 cycles

DURING CHECK, MAINTENANCE FOUND THAT THE EXTERNAL TAIL RELEASE CABLE WAS WORN. MAINTENANCE R & R THE WORN CABLE AND A FUNCTIONAL TEST WAS SATISFACTORY. LP 1901103.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,542 hrs · 46,648 cycles

CRACKED PAN ON STOP 1 AT RT FWD EMERGENCY EXIT DOOR. CRACK WITH 0.590" LONG WAS STOPPED IAW SRM 52-05. REPAIR PARTS WERE INSTALLED IAW SRM 52-05.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,542 hrs · 46,648 cycles

DAMAGED METALLIZED COAT ON LT SIDE OF RUDDER. METALLIZED COAT ON LT SIDE OF RUDDER WAS REPAIR IAW SRM 51-70-1A, PAR 23. LP 1904812.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1436C CORRODED OUT OF LIMITS, THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1335C CORRODED OUT OF LIMITS, REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1462C CORRODED. REPAIRED THE ACCESS PANEL.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,542 hrs · 46,648 cycles

CRACKED LONGERON 2RT ON FS Y=1418. CARD 45, ZONE 61. LONGERON WAS REPLACED IAW SRM 53-02, FIG. 18. LP 1900908.

Part: CUSP WEB — CORRODED (BS 1201-1207) · airframe 66,534 hrs · 49,594 cycles

LEFT CUSP WEB CORRODED OUT OF LIMITS, BS 1201, 1206-1207 BETWEEN LBL 54-60. DAMAGE REMOVED AND A REPAIR INSTALLED.

Part: LANYARD — CORRODED (TAILCON SLIDE) · airframe 62,542 hrs · 46,648 cycles

RUSTED DEPLAY LANYARD ON SLIDE AFT INFLATABLE AT TAIL CONE. LANYARD WAS REPLACED IAW AMM 26-60-01.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON FLOOR PANEL 160G, W1. FLOOR PANEL WAS REPLACED IAW DWG 9957828, REV AB AND 51-10-3, PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 844) · airframe 62,542 hrs · 46,648 cycles

CRACK ON RT CUSP WEB STA Y=844 BETWEEN X=-54 TO X=-60 AT PAX CABIN. IN REF OR NRC 102 AC ZONE 201. DAMAGE WAS REMOVED, FABRICATED DOUBLER, DOUBLER AND FILLER TREATED AND PAINTED ALSO INSTALLED REPAIR PARTS IAW SRM 53-05, FIG 131A-14 AND SRM 51-10-3, PAR 14 AND 21 ALSO SRM 51-30-2. LP 1896328.

Part: CUSP WEB — CORRODED (BS 484-729) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON DOUBLER REPAIR ON RT CUSP WEB BETWEEN X=-54 AND X=-60 STA Y=484-496, Y=720-729 AT PAX CABIN. MRB 53-037-02. DOUBLERS WERE REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-30-3, PAR 14, 21 & 38, 53-05, FIG 131A-6. LP 1896262.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 62,542 hrs · 46,648 cycles

DISBONDED FIRST LAYER ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-01-201.

Part: LONGERON — CRACKED (BS 160) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LONG 3 LT FS Y=160 AT PAX CABIN, CARD 10. DAMAGE SECTION ON LONGERON NR 3 LT WAS REMOVED. NEW SECTION LONGERON NR 3 LT WAS AJUSTED, AND DRILLED ALSO TREATED AND PAINTED NEW SECTION LONGERON AND SPLICE WAS INSTALLED IAW SRM 51-10-3, PAR 14 AND 21, ALSO SRM 51-30-2 AND 51-30-5 AND SRM 53-02, FIG 18, LP 1895247.

Part: CUSP WEB — CRACKED (BS 278) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LT CUSP WEB E FS Y 278 BETWEEN X=54 TO X=60 AT PAX CABIN. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-10-3 PAR. 14, 21, 51-30-2. LP 1894794.

Part: LONGERON — CRACKED (BS 160) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LONGERON 2 LT AT FS Y=160 CABIN PASSENGER, SM, CARD 334 ZONE. SECTION ON LONGERON NR 2 LT DAMAGE WAS REMOVED. NEW SECTION ON LONGERON 2 LT WAS AJUSTED, DRILLED ALSO TREATED AND PAINTED NEW SECTION OF LONGERON AND SPLICE, WAS INSTALLED IAW SRM 51-10-3, PAR 14 AND 21, ALSO SRM 51-3-2 AND 51-30-5 AND SRM 53-2, FIG 18. LP 1895250.

Part: CUSP WEB — CRACKED (BS 574-575) · airframe 62,542 hrs · 46,648 cycles

CRACK ON RT CUSP WEB, FS Y=574-575 BETWEEN X=-54 TO X=-60 AT PAX CABIN. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-10-3, PAR 14, 21. LP 1895259.

Part: CUSP WEB — CORRODED (BS 788-807) · airframe 66,534 hrs · 49,594 cycles

LEFT CUSP WEB CORROSION, BS 788-807, LBL 54 - 60. DAMAGE REMOVED, REPAIR INSTALLED.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 AND X=60 STA Y=598-712 AT PAX CABIN, SM. DAMAGE CUSP WEB WAS REMOVED AND NEW CUSP WEB WAS DRILLED, HOLES WERE TREATED AND PAINTED AND NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4 , 51-30-2 AND 51-10-3, PAR 21 AND 14.

Part: FRAME — CRACKED (BS 1338 BULKHEAD) · airframe 62,542 hrs · 46,648 cycles

CRACKED FORMER ON AFT PRESSURE BULKHEAD FS Y=1338 PROJECTION LONGERON 7R. FORMER WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5. LP 1896855.

Part: CUSP WEB — CORRODED (BS 604-606) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON RT CUSP WEB STA Y=604-606, BETWEEN X=-54 TO X=-60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND SRM 51-10-3, PAR 14, 21, 38, SRM 51-30-2.

Part: FLOOR PANEL — CRACKED · airframe 62,542 hrs · 46,648 cycles

CRACKED STIFFENERS OF FLOOR PANEL. STIFFENERS OF FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOORBEAM — CORRODED (BS 1380) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON FRAME TEE BS Y=1380 BETWEEN X=15 TO X=-15 AT A/A. TEE FRAME WAS REPLACED IAW D. DWG 9912246, REV DE AND SRM 51-10-3/51-30-2/51-30-5/51-30-1 AND 51-10-4.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 62,542 hrs · 46,648 cycles

CRACKS ON CHANNEL STA Y=953 AT LT MLG INBD DOOR. FASTENERS WAS REMOVED, CRACK WAS STOP DRILL AND DOUBLER REPAIR WAS FABRICATED, TREATED AND PAINTED IAW SRM 51-30-2, 52-05, FIG 6, 51-10-3, PAR 14/21 AND INSTALLED IAW SRM 52-05, FIG 60. LP 1896870.

Part: DOOR FRAME — WORN (RT MLG) · airframe 62,542 hrs · 46,648 cycles

WEAR ON ANGLE TEE AND SETTLEMENT STRIP OF RT AFT MLG DOOR JAMB STA XCW=60. ANGLE "T" AND RUBSTRIP WERE REPLACED BY NEW ANGLE AND STIP IAW SRM 51-30-2 , 51-30-5 , 53-14-3. LP 1893020

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,542 hrs · 46,648 cycles

CRACKED PAN BELOW FWD STOP NR 3 AT FWD CARGO BAY DOOR, C1. CRACK WAS STOPPED, DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 52-05, FIG 50, 51-10-2 , 51-10-3, PAR 21 AND 14 , 51-30-1 , 51-30-2. CRACK LONG: 750". LP 1894575.

Part: BULKHEAD — CRACKED (BS 1437) · airframe 62,542 hrs · 46,648 cycles

CRACKED BULKHEAD BS 1437 AND 10 HRS POSITION. BULKHEAD WAS REPAIRED IAW ERA 519146-14MA, REV A.

Part: CUSP WEB — CORRODED (BS 522-747) · airframe 66,534 hrs · 49,594 cycles

LEFT CUSP WEB CORROSION BS 522-533, 541-560, 737-747, LBL 54 TO 60. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 62,542 hrs · 46,648 cycles

CRACKED FITTING STOPS 2, 3, 5 ON FWD FRAME CUTOUT OF C2 DOOR. STOP FITTINGS WERE REMOVED IAW SRM 51-30-1 AND 51-30-5 , STOPS FITTINGS WERE DRILLED IAW SRM 51-10-4, NEW STOP FITTINGS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14 , NEW STOP FITTINGS WERE INSTALLED IAW SRM 51-30-1 AND 51-30-5. LP 1890527

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1361C. FUEL ACCESS 1361C WAS REPLACED. LP 1889493.

Part: LONGERON — CRACKED (BS 160-200) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LONGERON 4L BS 160 AND 200 AT PAX CABIN. LONGERON REPLACED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-30-5.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 62,542 hrs · 46,648 cycles

CRACKED FITTINGS STOPS 2, 4, 5 ON AFT FRAME CUTOUT OF C2 DOOR. SUMMARY:STOPS FITTING WERE REMOVED IAW SRM 51-30-1 AND 51-30-5 , STOP FITTINGS WERE DRILLED IAW SRM 51-10-4 , STOPS FITTING WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14 , STOP FITTINGS WERE INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 62,542 hrs · 46,648 cycles

WEAR LOWER FWD AND AFT EXTERNAL DOUBLER AT FWD CARGO COMPARTMENT DOOR. NEW DOUBLER WERE INSTALED IAW SRM 51-30-2.

Part: WINDOW FRAME — CRACKED (BS 598-946) · airframe 62,542 hrs · 46,648 cycles

CRACK ON RT FWD/UPPER CORNER OF WINDOW RING PAN BETWEEN STA 598-617, 750-769 AND 927-946 AT PAX CABIN. AREA WAS REPAIR IAW SRM 53-05, PAR 139, FIG 122, SRM 51-36-2 AND 51-30-5 AND ER/A 487747-14MA.

Part: ACCESS PANEL — CORRODED (WING) · airframe 66,534 hrs · 49,594 cycles

FUEL TANK ACCESS PANEL 1303C COUNTERSINKS CORRODED, REPLACED THE ACCESS PANEL.

Part: LANYARD — DAMAGED (DOOR SLIDE) · airframe 62,542 hrs · 46,648 cycles

QRO MAINTENANCE FOUND BROKEN WIRES ON LANYARD ASSY AT R1 AND L1 SLIDE. LANYARD ASSEMBLIES AT R1 AND L1 WERE REPLACED.

Part: CUSP WEB — CORRODED (BS 218-237) · airframe 62,542 hrs · 46,648 cycles

CRACKED CUSP WEB BETWEEN STA Y=218 TO Y=237, 2 EAS, AND X=54 TO X=60 LT SIDE. CRACKED CUSP WEB BETWEEN STA Y=218 TO Y=237 AND X=54 TO X= 60 WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 2301C. FUEL ACCESS 2301C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1409C, AYP, CARD 132 ZONE 00, FUEL ACCESS DOOR NR 1409C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1373C. FUEL ACCESS 1373C WAS REPLACED DUE EXCESSIVE CORROSION.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 2302C, PART RACKS, AYP, CARD 198, ZONE 00. FUEL ACCESS 2302C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR SUMMARY: FUEL ACCESS 1307C WAS REPLACED DUE EXCESSIVE CORROSION.

Part: WINDOW FRAME — CRACKED (BS 408-655) · airframe 62,542 hrs · 46,648 cycles

CRACK ON LT FWD/UPPER CORNER OF WINDOW RING PAN BETWEEN STAY=408-427, 503-522, 560-579, 617-636 AND 636-655 AT PAX CABIN. AREA WAS REPAIRED IAW SRM 53-05, PAR 139, 51-10-2, 51-10-3 PAR 14 & 21, 51-30-2, 51-30-5, ER/A 487747-14 MA, REV ORIGINAL.

Part: WINDOW FRAME — CRACKED (BS 1079) · airframe 62,542 hrs · 46,648 cycles

CRACK ON FWD LOWER CORNER OF WINDOW RING PAN STA Y= 1079 CABIN PASSENGER LT SIDE. AREA WAS REPAIR IAW SRM 53-05 PAR 139 SRM 51-30-2 AND 51-30-5 AND ERA 487747-14 MA REV ORIGINAL SRM 51-10-3, PAR 14-21.

Part: WINDOW FRAME — CRACKED (BS 845-927) · airframe 62,542 hrs · 46,648 cycles

CRACK ON FWD UPPER CORNER OF WINDOW RING PAN, STA Y= 845 AND Y=927 CABIN PAX LT SIDE. AREA WAS REPAIRED IAW SRM 53-05 PAR 139, 51-10-2, 51-10-3 PAR 14 & 21, 51-30-2, 51-30-5 & ER/A 487747-14MA, REV ORIGINAL.

Part: WINDOW FRAME — CRACKED (BS 788) · airframe 62,542 hrs · 46,648 cycles

CRACK ON FWD UPPER AND LOWER CORNERS AF WINDOW RING PAN STA Y=788 CABIN PAX LT SIDE. AREA WAS REPAIRED IAW SRM 53-05, PAR 139, SRM 51-30-2 AND 51-30-5 AND ER/A 487747-14MA REV ORIGINAL, SRM 51-10-3, PAR 14-21.

Part: WINDOW FRAME — CRACKED (BS 845-894) · airframe 62,542 hrs · 46,648 cycles

CRACK ON RT AFT/LWR CORNER OF WINDOW RING PAN BETWEEN STA Y=845-894 AT PAX CABIN. AREA WAS REPAIR IAW SRM 51-30-2, 51-30-5, AND 53-05, PAR 139, FIG 122 AND ERA 487747-14MA REV ORIGINAL.

Part: WINDOW FRAME — CRACKED (BS 598-946) · airframe 62,542 hrs · 46,648 cycles

CRACK ON RT FWD/UPPER CORNER OF WINDOW RING PAN BETWEEN STA 598-617, 750-769 AND 927-946 AT PAX CABIN. AREA WAS REPAIRED IAW SRM 53-05, PAR 139, 51-10-3, 51-10-2, 51-30-2 AND 51-30-5 AND ERA 487747-14, MA REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 323-434) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON RT SEAT TRACK REPAIR PLUG X=-54 BETWEEN STA Y= 323-328 AND Y=429-434, SM, CARD 48 ZONE 201, SUMMARY: PLUGS WERE REMPLACE IAW SRM 53-05, FIG 4A 51-10-3 PARR. 14, 21, 38.

Part: LANDING GEAR — CORRODED (NOSE) · corrosion level 2 · airframe 62,542 hrs · 46,648 cycles

CORROSION ON NOSE LANDING GEAR BEARING SETTLEMENT AREA. CYLINDER ASSY ON NOSE LANDING GEAR WAS REMOVED IAW AMM 32-21-02.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 62,328 hrs · 46,506 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE SEAT 12DE EMERGENCY LIGHT HARNESS DAMAGED. MAINTENANCE REPLACED THE HARNESS AND THE OPS CHECK WAS SATISFACTORY.

Part: FLOOR PANEL — BUCKLED (CABIN) · airframe 62,180 hrs · 46,395 cycles

FLOOR AT FWD BOARDING DOOR IS BUCKING WHEN WALKED ON. REMOVED FLOOR PANEL & BEGAN REINSTALLING REPLACEMENT PANEL. INSTALL FLT ATT SEAT (LI) SEALED PANEL AND INSTALLED FLT COMPARTMENT THRESHOLD PLATE IAW AMM 25-20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,683 hrs · 46,045 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT BAY TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: BEAM — CRACKED (DOOR TORQUE TUBE) · airframe 60,760 hrs · 45,334 cycles

AFT AIRSTAIR TORQUE TUBE SUPPORT BEAM CRACKED. LOCATED BELOW RT AFT CORNER OF WALKING BRIDGE. FABRICATED NEW BRACKET. FABRICATED -5 AND -6 STRAPS IAW DWG 5920986. INSTALLED IAW SRM VOL 1 51-00-00 AND ERA 526846.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 59,802 hrs · 44,674 cycles

CREW REPORTED ODOR IN COCKPIT AND THEN IN CABIN DURING CRUISE AT FL270. IDENTIFIED AS A BURNING PLASTIC ODOR AND COMING FROM THE GASPERS. CREW SECURED THE LT PACK AND PULLED THE CIRCUIT BREAKERS FOR THE RECIRCULATION FAN. ODOR SOON DISSIPATED AND THE ACFT CONTINUED TO SCHEDULED DESTINATION. MAINTENANCE DISCOVERED A LEAKING HYDRAULIC LINE, FROM THE THRUST REVERSER CONTROL VALVE FILTER HOUSING, CONTAMINATING THE APU INLET. THE FAULTY HYDRAULIC LINE WAS REPLACED, THE RESIDUAL FLUID WAS CLEANED UP, A PACK BURNOUT WAS ACCOMPLISHED, AND THE COALESCER BAGS WERE REPLACED. THE ACFT HAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (SENSOR TARGET) · airframe 59,506 hrs · 44,470 cycles

DURING CRUISE AT FL330, "GEAR DOOR OPEN" LIGHT ILLUMINATED. LIGHT STAYED ON AFTER GEAR WAS LOWERED AND SLOWED TO APPROACH SPEED. DECLARED EMERGENCY. QRH PROCEDURE ACCOMPLISHED AND LANDED WITH EMERGENCY GEAR EXTENSION HANDLE EXTENDED. MAINTENANCE FOUND THE LT GEAR DOOR PROXIMITY SENSOR TARGET BRACKET TO BE CRACKED. BOTH THE LT GEAR TARGET BRACKET AND THE PROXIMITY SENSOR WERE REPLACED AND ADJUSTED. DURING TROUBLESHOOTING THE RT DOOR CLOSED PROXIMITY SENSOR RESISTANCE VALUE WAS FOUND READING HIGH AND SO IT WAS REPLACED AS WELL. REPLACED BUMPER AND SKID ON LT DOOR AND SKID ON RT DOOR. GEAR SWING AND PSEU TEST GOOD.

Part: DOOR — DAMAGED (CARGO) · airframe 59,401 hrs · 44,407 cycles

CARGO DOOR DAMAGED. REPAIRED IAW AA 5230-01159.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 59,034 hrs · 44,139 cycles

EMERGENCY PATH LIGHTING WIRING IS LOOSE AT SEAT 25E. THE WIRING WAS SECURED.

Part: LOCK FASTENER — SHEARED (BS 1463) · airframe 58,843 hrs · 44,001 cycles

FOUND TWO LOCK FASTENERS WITH HEADS SHEARED. RT SIDE OF FUSELAGE BS 1463 RT WHERE VERTTCAL STABILIZER MEETS THE FUSELAGE, R & R THE LOCK FASTENER IAW SRM 51-30-5.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,305 hrs · 43,601 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 14DE IN THE CABIN WAS INOPERATIVE. MX FOUND A BROKEN WIRE IN THE HARNESS UNDER THE SEAT. THE WIRE BUNDLE WAS REPLACED AND THE SYS RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,177 hrs · 43,508 cycles

DURING LINE MX INSPECTION, BOTH FWD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. BATTERIES REPLACED IAW AMM 33-50 AND OPERATION CHECKED NORMAL.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 57,219 hrs · 42,869 cycles

CARGO DOOR BEAM, L28R CORROSION ON VERTICAL FLANGE OF BEAM BETWEEN STA 1155-1212---CORROSION VARIOUS AREAS BETWEEN STA 1155-1212. SUMMARY OF NR 170: REMOVED CORROSION IAW AMM 53-05 AND INSTALLATION OF FILLERS AND DOUBLERS. WORKED WITH NR 25 AND ER/A 499523-14MA REF LOG 0729485. CLASS 2, CORROSION LEVEL CHANGED FROM: N TO: 2.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 57,219 hrs · 42,869 cycles

AFT CARGO COMPARTMENT LONGERON 28R BEAM LOWER FLANGE UPPER SURFACE, CORROSION BETWEEN BARRIER DOOR BAYONET GUIDE FITTINGS. REPAIRED C3 CARGO DOOR BEAM IAW ER/A 499523-14MA BY REMOVING CORROSION, INSTALLING FILLERS, AND DOUBLERS IAW ER/A 499523-14MA AND SRM 53-05, FIG 123. REF ALSO NR 170. CLASS 2 CORROSION LEVEL CHANGED FROM: N TO: 2.

Part: RIVET — MISSING (BS 1418) · airframe 57,206 hrs · 42,861 cycles

RIVET MISSING AT BS 1418 STRINGER 2L. INSTALLED FASTENERS IAW ER/A 511211-14AD, REV 1.

Part: SKIN — DENTED (BS 1418 S2L) · airframe 57,206 hrs · 42,861 cycles

FUSELAGE SKIN DENTED AT BS 1418 INBD OF STR 2 LT, DAMAGE REMOVED IAW ER/A 511211-14AD, REV 1.

Part: FRAME — DAMAGED (BS 1485) · airframe 57,206 hrs · 42,861 cycles

CANTED FRAME RT SIDE, BS 1485 DAMAGED. REPAIRED IAW ERA 511292-14.

Part: SKIN — CRACKED (BS 1418 S2-3L) · airframe 57,206 hrs · 42,861 cycles

FUSELAGE SKIN CRACKED AT BS 1418 BETWEEN STRINGERS 2 & 3 LT. PERFORMED HFEC IAW NTM SPM 06-10-01. 001. REMOVED DAMAGE AREAS IAW SRM 53-04, FIG 40. DAMAGE CONTAINED. SPLICED FITTING & END FITTING IAW ER/A 511211-14AD.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 57,206 hrs · 42,861 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: ANGLE — CRACKED (TAILCONE) · airframe 57,206 hrs · 42,861 cycles

TAILCONE UPPER RT L ANGLE INTERCOSTAL IS CRACKED. REMOVED UPPER L ANGLE, DRILLED NEW , PRIMED AND INSTALLED IAW SRM 51-30.

Part: ATTACH FITTING — DAMAGED (HORIZONTAL STAB) · airframe 57,206 hrs · 42,861 cycles

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

Part: SKIN — CRACKED (BS 1401) · airframe 57,206 hrs · 42,861 cycles

FUSELAGE SKIN CRACKED AT STA 1401, 12" ABOVE RT PYLON. PERFORMED REPAIRS IAW ER/A 511207-14, REV ORIG.

Part: SKIN — CRACKED (BS 1401) · airframe 57,206 hrs · 42,861 cycles

FUSELAGE SKIN CRACKED AT STA 1401 12" ABOVE LT PYLON. REPAIRS ACCOMPLISHED IAW ER/A 511206-14, REV ORIG.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 55,576 hrs · 41,712 cycles

REPORT OF STRONG ELECTRICAL BURNING ODOR IN THE MIDDLE TO AFT CABIN AREAS. MAINTENANCE REPLACED A CABIN LIGHTING BALLAST AND BULB.

Part: ENGINE — FAILED (NR 2) · airframe 55,545 hrs · 41,689 cycles

CREW DIVERTED TO IAD FOLLOWING THE FAILURE OF THE RIGHT ENGINE DURING CLIMB TO FL30. THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND THEN EXPERIENCED FEELING A JOLT & SHUDDER CULMINATING WITH THE LOSS OF POWER IN THE RIGHT ENGINE. MAINTENANCE FOUND METAL IN TAIL PIPE ALONG WITH TURBINE DAMAGE. THE NR 2 ENGINE WAS SUBSEQUENTLY REPLACED.

Part: SPAR — CRACKED (WING) · airframe 53,768 hrs · 40,457 cycles

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

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 53,757 hrs · 40,448 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,318 hrs · 39,475 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS BETWEEN ROW 34-36 AND LIGHTS ABOVE L2 DOOR INOPERATIVE. MX REPLACED BATTERIES AT POWER SUPPLY B5-107. OPERATION OF LIGHTS NOW CHECKS OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,207 hrs · 37,987 cycles

EMERGENCY EXIT SIGN AT AFT F/A SEAT INOP. FOUND BROKEN WIRE AT QUICK DISCONNECT FWD OF AFT FLT ATTEN SEAT, REPINED WIRE IN NEW CONNECTOR IAW WEM. OPS CHK NML.

Part: SKIN — DAMAGED (BS 235) · airframe 49,991 hrs · 37,843 cycles

DAMAGE TO FUSELAGE SKIN AT BS 235 +18. REPAIRED IAW SRM 53-04-5.

Part: FLOOR SUPPORT — CORRODED (FS 160-200) · airframe 48,111 hrs · 36,628 cycles

FLOOR SUPPORT CORRODED FS 160-200 AT FASTENER HOLES TOP AND BOTTOM. REMOVED AND REPLACED PER SRM 51-30-01/05.

Part: SKIN — DAMAGED (FS 521 L21R) · airframe 48,111 hrs · 36,628 cycles

SKIN DAMAGED, COMPLIED WITH ER/A 234607-14 REV B. MAJOR REPAIR PERMANENT.

Part: PAN — CORRODED (FS 826-845) · airframe 48,111 hrs · 36,628 cycles

MAIN CABIN STA 826-845 AT LBL 60 FLOOR PAN CORRODED. REPAIRED IAW ER/A 398191-14 MA.

Part: WEB — CRACKED (FS 1474-1485) · airframe 48,111 hrs · 36,628 cycles

CANTED FRAME ATTACHMENT FS 1474-1485 WEB CRACKED IN AFT CORNER RADIUS.

Part: CUSP WEB — CRACKED (FS 218 L18R) · airframe 48,111 hrs · 36,628 cycles

CUSP WEB CRACKED AT ATTACH POINT STA 218 LONGERON 18R. REMOVED AND REPLACED CUSP WEB.

Part: ATTACH ANGLE — CRACKED (FS 1498 L22L) · airframe 48,111 hrs · 36,628 cycles

FS 1498, LONG 22L ATTACH ANGLE CRACKED AT PREVIOUS REPAIR BELOW VENTRAL STAIR TORQUE TUBE. REPLACED ANGLE IAW SRM 51-10-2, 51-10-4, 51-10-3.

Part: FLOORBEAM — CORRODED (FS 254) · airframe 48,111 hrs · 36,628 cycles

FLOOR SUPPORT LBL 35 FS 254 HAS CORROSION AROUND NUTPLATE HOLES. REPLACED FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FS 200 RBL 44) · airframe 48,111 hrs · 36,628 cycles

SEAT TRACK RBL 44 FS 200-245 HAS CORROSION AT NUTPLATE HOLES REPLACED SEAT TRACK.

Part: FLOORBEAM — CORRODED (FS 180 RBL 10-44) · airframe 48,111 hrs · 36,628 cycles

FLOORBEAM FS 180 RBL 10 TO RBL 44 HAS CORROSION AROUND FASTENER HOLES. REPLACED SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FS 164 LBL15) · airframe 48,111 hrs · 36,628 cycles

FLOOR SUPPORT AT STA 164 LBL 15 HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FS 160-200) · airframe 48,111 hrs · 36,628 cycles

FLOOR SUPPORT RBL 7 FROM FS 180-200 HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SKIN PANEL — DAMAGED (FS 1380-1401) · airframe 48,111 hrs · 36,628 cycles

SKIN CREASED BETWEEN FS 1380-1401 BETWEEN LONGERON 21R AND 22R. REPAIRED PER SRM 53-04D FIG 12B.

Part: FAIRING — DAMAGED (AILERON) · airframe 47,074 hrs · 35,913 cycles

LT AILERON TRIM TAB ACTUATOR ROD MISSING A PORTION OF FAIRING. DRILLED AND INSTALLED PANEL O/B OF AILERON TRIM SURFACE NEED PAINTED. REMOVED PNL PAINTED AND REINSTALLED. LEFT ALL CONT TAB AND LEFT AILERON PER JIC OPERATION NR 7037 7038 7039. REQUIRED INSPECTION COVERED.

Part: CSD — INOPERATIVE (NR 2 ENGINE) · airframe 44,610 hrs · 34,327 cycles

ON T/O OUT OF MIA, RT ENGINE CSD OIL TEMP HIGH AND RT GENERATOR FAILED, STARTED APU AND COVERED RT BUSS AND THEN GOT APU GEN FAILED 3 MINUTES LATER. FOUND RT CSD OVER SERVICED AND METAL ON CSD CHIP DETECTOR. REMOVED AND REPLACED NR 2 CSD/GEN/AND CSD OIL COOLER AND FLUSHED COOLER LINES. R/R AND CHECKED GOOD PER MM. ALSO, REMOVED AND REPLACED CSD DRIVE SEAL.

Part: SMOKE — DETECTED (COCKPIT) · airframe 41,990 hrs · 32,503 cycles

SHIPPED DIVERTED TPA SMOKE IN COCKPIT/CABIN. PERFORMED OPN 5088 AND 5089 NO REOCCURRENCE.

Part: PRESSURE PANEL — LEAKING (RT MLG WW) · airframe 38,122 hrs · 29,682 cycles

MLG WHEEL WELL SLANT PRESSURE PANEL REPAIRED IAW 09-085387-12.

Part: SCHRADER VALVE — MALFUNCTIONED (NLG) · airframe 36,509 hrs · 28,553 cycles

ON TAKEOFF ROLL, NOSE GEAR BOTTOMING OUT. TRIED TO RAISE GEAR NOSE, GEAR DISAGREEMENT AND AUDIO NOISE INDICATED PARTIALLY DOWN OR DOORS OPEN. RAN CHECKLIST, LOWERED GEAR TO 3 GREEN, LANDING UNEVENTFUL AT 136,000 LBS, TOUCHDOWN AT LESS THAN 300 FPM. FOUND SHRADER VALVE O-RING LEAKING. REPLACED SHRADER VALVE AND SERVICED NOSE STRUT PER M/M. SWUNG NOSE GEAR SEVERAL TIMES. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (SAFETY EQUIPMENT) · airframe 36,267 hrs · 28,386 cycles

AFT CABIN MEGAPHONE INOP. REPLACED MEGAPHONE.

Part: SWITCH — INTERMITTENT (NLG) · airframe 35,868 hrs · 28,073 cycles

ON TAKEOFF CREW NOTICED EXCESSIVE NOSE GEAR VIBRATION. AFTER GEAR RETRACTION, HAD RED NOSE GEAR UNSAFE LIGHT. COMPLIED WITH POM GOT THREE GREEN LIGHTS. FOUND SWITCH S1-412 OPERATING INTERMITTENTLY. REPLACED SAME.

Part: SENSOR — INTERMITTENT (NLG) · airframe 35,863 hrs · 28,069 cycles

AT CRUISE ALTITUDE NOSE GEAR UNSAFE LIGHT ILLUMINATED. FLT CREW REPORTED NO ABNORMAL FLIGHT CHARACTERISTICS. REPLACED UP AND DOWN LOCK PROX SENSORS PER M/M, OPS CHECKS OKAY.

Part: CONNECTOR — SHORTED (NR 2 ENGINE) · airframe 34,524 hrs · 27,094 cycles

DURING FLIGHT 269 ATL OMA RIGHT ENGINE FIRE WARNING BOTH LOOPS ENGINE WAS SHUTDOWN BOTH FIRE BOTTLES DISCHARGED. A/C DIVERTED TO LIT. REPAIRED LOOPS A AND B FOR SHORTED CONNECTORS.

Part: PROXIMITY SWITCH — FAILED (MLG UPLOCK) · airframe 32,954 hrs · 26,032 cycles

ON DEPARTURE GEAR RETRACTED NORMALLY HOWEVER DURING ACCELERATION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. REPLACED NOSE GEAR UPLOCK PROXIMITY SWITCH. CYCLED GEAR CHECKS OK.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 32,819 hrs · 25,935 cycles

DURING HMV-2, LIGHTNING STRIKE DAMAGE ON WINDOW BELTS WAS FOUND AT FS 674-693 AND FS 712-731. A TIME LIMITED BLEND REPAIR WAS PERFORMED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 31,232 hrs · 24,754 cycles

FIRST CLASS EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE UNDER SEAT 1C AND REPLACED POWER SUPPLY AND BATTERY PACK.

Part: CONTROLLER — STUCK (CABIN PRESSURE) · airframe 30,234 hrs · 24,015 cycles

AUTO PRESSURIZATION 1 AND 2 INP ON T/O. MANUAL PRESSURE CONTROLLER JAMMED IN MIDWAY POSITION. REPLACED PRESSURIZATION CONTROLLER.

Part: APU — LEAKING (APU BAY) · airframe 29,732 hrs · 23,642 cycles

FLT ATTENDANTS SMELLED AN ELECTRICAL BURNING ODOR, A LITE HAZE ALSO APPEARED. AFT LAV SMOKE DETECTORS WERE INTERMITTENTLY SOUNDING FOR APPROX 2 MINUTES THEN WENT OFF COMPLETELY. PERFORMED OPN 5088. NO ELECTRICAL SMELL NOTED. REPLACED APU DUE TO OIL LEAK REF ITEM 3. PERFORMED DUCT BURNOUT. REPLACED WATER SEPARATOR BAGS. RAN ENGS TO TAKEOFF POWER. NO SMELL OR HAZE NOTED.

Part: SKIN — LIGHTNING STRIKE (WINDOW BELT) · airframe 28,773 hrs · 22,915 cycles

THE WINDOW BELT SKIN SUFFERED A LIGHTNING STRIKE ON THE LWR FWD CORNER OF THE WINDOW OPENING BETWEEN FS 598 & 617. THE DAMAGED WAS BLENDED OUT AND AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER MD-88 SRM 53-05, FIG 111A AND PER ER/A 379838-14.

Part: SKIN — LIGHTNING STRIKE (WINDOW BELT) · airframe 28,773 hrs · 22,915 cycles

THE LT WINDOW BELT SKIN WAS STRUCK BY LIGHTNING AT TWO WINDOW CUTOUTS BETWEEN FS 767 AND 807. THE STRIKES WERE AT THE EDGES OF THE CUTOUTS. EACH LOCATION WAS BLENDED TO REMOVE THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 379840-14.

Part: FILTER — CONTAMINATED (NR 1 ENGINE)

ON DESCENT INTO GRR, GOT LEFT ENG OIL STRAINER CLOG MSG. PERFORMED POM PROCEDURES, LIGHT DID NOT EXTINGUISH. PERFORMED POM PROCEDURES AND SHUT LEFT ENG DOWN AND DECLARED EMERGENCY. FOUND CARBON IN FILTER. REPLACED AND PERFORMED ENGINE RUN-UP, NO ADDITIONAL CARBON FOUND.

Part: ENGINE — DAMAGED (NR 2)

AFTER TAKEOFF, HEARD LOUD NOISE, LOSS OF AIR CONDITIONING AND A FLOW LIGHT ILLUMINATED. RECEIVED FIRE WARNING ON THE NR 2 ENGINE. FOLLOWED ENGINE FIRE PROCEDURES. THE FIRE WARNING WENT OUT AT IDLE THRUST. TESTED THE FIRE WARNING SYSTEM AND TESTED GOOD. RETURNED TO ATL. REPLACED DAMAGED ENGINE COWL AND APRON.

Part: LUBRICATION — OVERSERVICED (NR 2 ENGINE)

ON CLIMBOUT, NR 2 ENG OIL TEMP REACHED 165 DEG AND PRESS WAS 55 PSI. TEMP FLUX FROM 155 TO 165 DEG UNTIL DESCENT PWR RETARDED. GRADUAL DECREASE TO NML ON TAXI IN. OIL TANK OVER SERVICED. DRAINED TANK TO PROPER LEVEL, RAN ENG PRESS AND TEMP NORMAL.

Part: PRESSURIZATION — MALFUNCTIONED (COCKPIT)

AUTO 1 AND 2 INOP LOST PRESURIZATION. UNABLE TO CONTROL CABIN IN MANUAL MODE AT 27000. AUTO 1 AND 2 INOP ILLUMINATED. CABIN WAS IN DESCENT AT 1500 FPM AND REMAINED IN DESCENT. FOLLOWED PROCEDURES PER POM. WEMT TO MANUAL MODE, THEN CABIN WOULD NOT CONTROL. UNABLE TO CONTROL OUTFLOW VALVE. CABIN BEGAN TO CLIMB. TESTED CONTROLLERS AND OUTFLOW VALVE, UNABLE TO DUPLICATE.

Part: SKIN — DENTED (AFT SERVICE DOOR)

THE AFT SERVICE DOOR OUTER SKIN WAS DAMAGED DUE TO CONTACT WITH GROUND SUPPORT EQUIPMENT. THE SKIN HAS AN APPROXIMATE 1.0 INCH DIAMETER DENT THAT WAS 0.120 INCH DEEP AND IS CRACK FREE. THIS HAS A TIME LIMITED REPAIR OF DYE PENETRANT INSPECTION AND A PERMANENT REPAIR IN WHICH A DOUBLER WILL BE INSTALLED. THIS REPAIR HAS BEEN APPROVED BY FAA/ DER FORM 8110-3, DER DESIGNATION SO-867, DATED 3-7-97.

Part: SKIN — DAMAGED (BS 408)

THERE IS A CUT-OUT IN THE FUSELAGE SKIN AT F.S. 408, BETWEEN STR 17R AND 18R. AN EXISTING TIME-LIMITED REPAIR HAS BEEN REMOVED. THE CUT-OUT MEASURES APPROXIMATELY 6 INCHES FORWARD/AFT AND 6 INCHES UP/DOWN. THE MD-88 SRM REPAIR CALLS FOR AN EXTERNAL DOUBLER AS WELL AS SEVERAL FINGER DOUBLERS. THE ADDITION OF THE LOWER FINGER DOUBLER IS NOT POSSIBLE. ER/A 304927-14 PROVIDES PERMANENT INSTRUCTIONS FOLLOWING THE SRM WITH THE EXCLUSION OF THE AFOREMENTIONED FINGER DOUBLER.

Part: SKIN — DENTED (BS 227-237)

THE FUSELAGE SKIN WAS FOUND TO BE DENTED FROM F.S. 227 TO F.S. 237 BETWEEN STRINGERS 18L AND 19L. DAMAGE WILL BE REPAIRED PER ER/A 304919-14.

Part: SUBFLOOR — CRACKED (BS 1260)

FOUND DURING HMV-1, AFT RT CABIN SUBFLOOR AT STA 1260, 1281 AND 1295 MEMBRANE CRACKED. REPLACED MEMBRANE PER SRM 53-05 FIG 100.

Part: SUBFLOOR — CRACKED (CABIN)

FOUND DURING HMV-1 AFT LT CABIN SUBFLOOR MEMBRANE CRACKED AT STA 1295. INSTALLED NEW MEMBRANE PER SRM 53-05 FIG 100.

Part: DRIVE ARM — BROKEN (LT TE FLAP)

LEFT TRAILING EDGE FLAP REPORTED WITH EXCESSIVE DROOP. FOUND BROKEN LINK ON LT FLAP ACTUATOR. REMOVED LINK AND ACTUATOR. INSTALLED AFT END OF ARM ASSEMBLY, LINK AND ROD. INSTALLED ACTUATOR AND RECONNECTED LINKS, OPERATION NORMAL.

Part: AIR COND — ODOR (TAIL COMP)

DURING TAKEOFF, CABIN FILLED WITH SMOKE ODOR AND CONTINUED AFTER ATTEMPTING TO SWAP PACKS. RETURNED TO TYS AND PERFORMED GROUND RUN, COULD NOT DUPLICATE. PERFORMED DUCT BURNOUT, REPLACED WATER SEPARATOR BAGS AND RETURNED TO SERVICE.

Part: FRAME — CRACKED (L/H W/W)

CRACK IN W/W AFT JAMB AFT ANGLE. FOUND DURING E-1 LETTER CHECK. REPAIRED PER SRM 53-05 FIG 101.