N973DL

Part: BULB — BURNED OUT (LAVATORY LIGHT) · airframe 74,948 hrs · 55,858 cycles

AFTER FLIGHT F/A REPORTED LEFT AFT LAV SMOKE DETECTOR WENT OFF IN FLIGHT. ONE PAX REPORTED SMELLING SOMETHING. IN FLIGHT F/A REPORTED WHAT PAX SAID I ASKED FOR DETAILS, SHE SAID SHE SMELLED NOTHING; AND NO REPORT OF ALARM. ONLY AFTER WE DEPLANED DID SHE TELL ME ABOUT THE ALARM. COMPLIED WITH NO GO ODI PREVENTION ATA 2172. COMPLIED WITH PNEUMATIC DIST. CABIN SMOKE/ODOR WORKCARD 2120-2367. NO DEFECTS NOTED. COMPLIED WITH WORKCARD 7100-2619 - PNEUMATIC SYSTEM DUCT BURNOUT. REMOVED AND REPLACED LEFT AFT LAV MIRROR LIGHT BULBS PER MD88 33-22. OPS CHECK GOOD. INSPECTED LEFT AFT + RIGHT AFT LAV TRASH BINS. NO DEFECTS NOTED. AFT LAV SMOKE DETECTORS OPS CHECK GOOD IN REFERENCE TO MD88 AMM 26-13. OK FOR SERVICE. (LP6544408)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 74,918 hrs · 55,826 cycles

AFT LEFT LAV SMOKE DETECTOR WENT OFF FOR SEVERAL SECONDS ENROUTE . NO SMOKE OR FIRE PRESENT. R/R AFT LEFT LAV SMOKE DECTECTOR PER MD 88 AMM 26-13. OPS CHECK GOOD.

Part: SMOKE DETECTOR — MISSING (FWD LAVATORY) · airframe 73,713 hrs · 54,693 cycles

FWD LAV SMOKE DETECTOR IS MISSING. RPLCD FWD LAV SMOKE DETECTOR PER MD88 AMM 26-13. ALL CHKS GOOD. (LP5675132)

Part: TAB — DAMAGED (RUDDER) · airframe 73,298 hrs · 54,328 cycles

RUDDER TAB HAS PAINT CHIPPING INTO COMPOSITE. REPLACED WITH SERVICEABLE RUDDER TAB IAW DELTA WORK CARDS 2720-4438 AND 2720-4321 TAB, RUDDER OFF 88-5554-9-0002 00094 ON 88-5554-9-0002 00542. (LP0959946)

Part: CAM — OUT OF POSITION (TAIL CONE) · airframe 73,301 hrs · 54,331 cycles

TAIL CONE CAM ARM FOR SLIDE LANYARD IS NOT POSITIONED CORRECTLY. ADJUSTED CAM PER MD88 AMM 53-53-02. (LP0960759)

Part: RUDDER — DAMAGED · airframe 73,298 hrs · 54,328 cycles

DURING PAINT VISIT -RUDDER MISSING DAMAGED FLAME SPRAY. REMOVED AND REPLACED RUDDER PER MD88 AMM 27-20-01. REMOVE & INSTALL MISTAKENLY ACCOMPLISHED ON LOG 5318866. (LP5318867)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 73,289 hrs · 54,324 cycles

INITIAL INSPECTION: CRACK ON VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65. VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65 WAS REPAIRED PER ER/A 575282-14 REV. ORIG. AND ETI-88-19-008 REV.1. PERFORM GENERAL VISUAL INSPECTION EVERY "C" CHECK, NOT TO EXCEED 24 MONTHS PER ER/A 575282-14 REV. ORIGINAL SEC II . REPETITIVE INSPECTION WILL BE FOLLOWED UNDER LOG NBR 0936865. (LP0938410)

Part: ACCESS PANEL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 73,289 hrs · 54,324 cycles

INITIAL INSPECTION: CORROSION ON AFT LAVATORY ACCESS PANEL BTW STA Y 1309 -1322 AND BTW LOG 20LH -21LH FUS. CORROSION LEVEL 2. AFT LAVATORY ACCESS PANEL,SKIN AND INTERNAL DOUBLER WERE REPAIRED PER ER/A 473500-14 REV. A SECTION II AND ETI-88-19-009 REV.3. PERFORM AN EXTERNAL GENERAL VISUAL INSPECTION WITHIN EVERY 8000 CYCLES PER ER/A 473500-14 REV. A SEC. III. REPETITIVE INSPECTION WILL BE FOLLOWED UNDER LOG NBR 0937432. (LP0938403)

Part: LONGERON — CORRODED (BS 1270-1290) · corrosion level 2 · airframe 73,289 hrs · 54,324 cycles

INITIAL INSPECTION: CORROSION AT LONGERON 29RH BTW STA Y=1270 TO Y=1290.(C3). SECTION OF LONGERON 29RH BTW STA Y=1270 TO Y=1290. WAS REPAIRED AND REPLACED PER DC9/MD80, SRM 53-02 FIG. 18. CORROSION LEVEL 2. PERMANENT REPAIR. (LP0936794)

Part: JACKSCREW — CORRODED (HORIZONTAL STAB) · airframe 73,289 hrs · 54,324 cycles

INITIAL INSPECTION: AD. RII. AA WORKCARD. CORROSION ON HORIZONTAL STABILIZER ACTUATOR JACKSCREW UPPER SIDE. HORIZONTAL STABILIZER JACKSCREW ASSEMBLY P/N 5910962-71 S/N: DCA2042 WAS REPLACED FOR SERVICEABLE P/N 5910962-57 S/N: DCA1689 UNDER AMDS 2742-4540. JACKSCREW, STAB OFF 03-2740-9-0007 02042 ON 03-2740-9-0007 01689(LP0936140)

Part: DOOR FRAME — CRACKED (BS 946) · airframe 73,289 hrs · 54,324 cycles

INITIAL INSPECTION: CRACK ON FWD OUTBD DOORJAMB STA 946 AT RH MLG WHEEL WELL. FWD OUTBD DOORJAMB STA 946 AT RH MLG WHEEL WELL WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG 113. (LP0933140)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,450 hrs · 53,591 cycles

RED EMERGENCY FLOOR LIGHT INOP FWD OF F/C COAT CLOSET. RELAMPED PER AMM 33-53. OPS CHECK GOOD.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 71,974 hrs · 53,185 cycles

AFTER LANDING AND STARTING THE APU, SMELLED FUMES COMING FROM THE COCKPIT EYE BALL VENTS. WE IMMEDIATELY SHUT THE AIR OFF. APU AND INLET DRY NO SIGNS OF FUEL CONTAMINATION. OPENED APU DOORS VERIFIED NOT CONTAMINATED. CKD FUEL DRAINS, NO FUEL. PRESSURIZED FUEL SYSTEM FOR EXTENDED TIME AND STARTED APU. NO ODOR DETECTED IN CABIN OR COCKPIT. APU NO LEAK. SHUTDOWN. MADE SEVERAL NMI STARTS, NO ODOR AND NO LEAKS. FOLLOWING PILOT AIRCRAFT AND SMOKE AND FUME QUESTIONNAIRE AND CARD 2120-2367 THRU FIG 6. C/W PNEUMATIC SYSTEM DUCT BURNOUT WC 7100-2619. C/W COELESCER BAG R&R 2170-4139. C/W NO GO ODI PREVENTION SMOKE FUME OF UNKNOWN SOURCE.

Part: TAB — MISSING (LT ELEVATOR) · airframe 70,884 hrs · 52,325 cycles

WHILE INSPECTING FLIGHT CONTROLS, FOUND LEFT ELEVATOR INBD TAB OTBD EDGE REPAIR MISSING. REMOVED AND REPLACED LEFT ELEVATOR CONTROL TAB IAW JIC 2730-4634-LH.

Part: ROLLER — MISSING (UP LATCH) · airframe 69,333 hrs · 51,095 cycles

DURING GEAR EXTENSION, THE GEAR DOOR LIGHT REMAINED ILLUMINATED. IAW QRH 14.3, THE ALTERNATE GEAR EXTEND PROCEDURE WAS PERFORMED FOR LANDING. MAINTENANCE FOUND THE LEFT GEAR DOOR UP LATCH ROLLER AND ATTACHING HARDWARE MISSING. THE ROLLER AND HARDWARE WAS REPLACED. THE ADJUSTMENT OF THE UP LATCH AND DOOR WAS CHECKED IAW AMM. A GEAR SWING WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 69,032 hrs · 50,883 cycles

AT FL250, TURNED ON THE WING ANTI-ICE DUE TO RIME ICE BUILD UP, IMMEDIATELY SMELLED A STRONG CHEMICAL ODOR . THE FLIGHT ATTENDANTS DETECTED THE ODOR. LASTED CONTINUOUSLY FOR THE 10 MINUTES OR SO THE WING ANTI-ICE WAS ACTIVE. ONCE TURNED OFF, THE ODOR QUICKLY WENT AWAY. TROUBLESHOT IAW WORKCARD 21202367 FOR PNEU DUCT SMOKE/ODOR, INSPECTED THE CROSSOVER DUCT FOR OIL CONTAMINATION WITH BORESCOPE. NO EVIDENCE FOUND, CONTINUING TO FOLLOW THE WORKCARD. ACCOMPLISHED DUCT BURN OUT PROCEDURES IAW WC 7100-2619 AND WC 2120-2367. NO ODOR PRESENT AT THIS TIME. OK FOR SERVICE.

Part: SEAT — DETACHED (ROW 13 ABC) · airframe 68,481 hrs · 50,491 cycles

ROW 13ABC SEATS CAME DETACHED AT THE FLOOR ON THE FRONT. ENTIRE ROW TIPPED BACK ON TAKEOFF. ADJUSTED AND SECURED SEAT ROW IAW AMM 25-23. ALL OPS NORMAL.

Part: STRAP — CRACKED (ESCAPE SLIDE) · airframe 68,370 hrs · 50,425 cycles

EVACUATION SLIDE OF TAILCONE THE CONTAINER FORWARD HOLD-DOWN STRAPS WERE FOUND CRACKED DUE TO CORROSION. HOLD DOWN STRAPS WERE REPLACED IAW AMM 25-62-01.

Part: FRAME — CRACKED (BS 1485) · airframe 68,370 hrs · 50,425 cycles

CRACKED FRAME BS 1485 BETWEEN LONGERONS 15 AND 16L. THE FRAME WAS REPAIRED IAW ERA 552911-14 REV. ORIGINAL AND ETI-88-17-004 REV.2.

Part: FRAME — DAMAGED (BS 1361) · airframe 68,370 hrs · 50,425 cycles

ELONGATED HOLES AT FRAME BS 1361 LONGERON 9 AND 10L. REPAIRED IAW SRM 53-03 FIG. 4 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 845) · airframe 68,370 hrs · 50,425 cycles

CRACK ON CUSP WEB BS 845 AND BTW LBL 54 AND 58. THE CUSP WEB WAS REPARIED IAW SRM 53-05 FIG 131A-13.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 65,267 hrs · 48,088 cycles

LEFT OTBD HORIZONTAL STABILIZER ATTATCH FITTING HAS WEAR ON OTBD FACE AND PITTING IN BORE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 032-0001, 5510-01074-16/001, 00008. REPLACED PLATES REF ER/A 540306-14, REV ORIGINAL.

Part: ATTACH FITTING — WORN (HORIZONTAL STAB) · airframe 65,253 hrs · 48,073 cycles

RIGHT OTBD HORIZONTAL STABILIZER ATTATCH FITTING HAS WEAR ON OTBD FACE AND PITTING IN BORE. REPLACED PLATES, REF ERA 540306-14, REV O.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 65,253 hrs · 48,073 cycles

BOTH INBD ATTACH FITTINGS FOR HORIZONTAL STABILIZER HAVE PITTED BORES. REPACED PLATES REF ERA 540306-14, REV O.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 65,253 hrs · 48,073 cycles

RT HORIZONTAL STABILIZER AFT UPPER SPAR CAP CRACKED AT AFT BARREL NUT HOLE (MKD) . REF NOTES AMDS 5510-01098-01B, ITEM 7. FOR DETAILS SEE JOB 00 - WORK PACKAGE. REPLACE HORIZONTAL STAB ASSY ON TASK CARDS: 5510-4135, 2730-4182, 2730-4831, 2730-4590-LT, 2730-4590-RT, 2730-4001-LT, AND 7. 2730-4001-RT.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 64,403 hrs · 47,494 cycles

FLIGHT RETURNED TO DEPARTURE FOLLOWING A COMPRESSOR STALL AND RESULTING HIGH EGT IN THE NR 2 ENGINE. THE CREW SHUTDOWN THE NR 2 ENGINE AND LANDED UNEVENTFULLY ON 1 ENGINE. MAINTENANCE HAS REPLACED THE ENGINE.

Part: SKIN — DENTED (BS 402-403) · airframe 63,120 hrs · 46,615 cycles

DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BS 402-403 BETWEEN LONGERONS 25 -26L. AREA REPAIRED IAW ER/A 365087-14, REV C.

Part: SLIDE — UNSERVICEABLE (TAILCONE) · airframe 63,114 hrs · 46,612 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EVACUATION SLIDE WAS INADEQUATELY WRAPPED. MAINTENANCE INSTALLED A SERVICABLE TAILCONE EVACUATION SLIDE. RII WAS SATISFACTORY.

Part: SKIN — DENTED (BS 402-403) · airframe 63,114 hrs · 46,612 cycles

DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BS 402-403 BETWEEN LONGERONS 25 -26L. REPAIRED IAW ER/A 365087-14, REV C.

Part: RELEASE MECH — DAMAGED (TAILCONE) · airframe 63,114 hrs · 46,612 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM TO BE DAMAGED. MAINTENANCE REPLACED THE RELEASE MECHANISM FITTING AND CRANK ASSY.

Part: FLOORBEAM — CORRODED (BS 1322) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FLOORBEAM BS 1322, X 18, X 26L. DAMAGE REPAIRED IAW SRM 53-05, FIG 79A, SH 1.

Part: FRAME — CRACKED (BS 1485) · airframe 63,114 hrs · 46,612 cycles

CANTED FRAME BS 1485 CRACKED AT LT AFT SIDE OTBD OF LIGHT ASSY. DAMAGE WAS REMOVED IAW SRM 53-030, FIG 48. REPAIR FABRICATED IAW SRM 53-030, FIG 8 AND INSTALLED IAW SRM 53-030, FIG 48.

Part: STRUCTURE — CRACKED (DOOR FRAME) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION AND CRACK AROUND OF SETTLEMENT AREA OF LT APU DOOR. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. FASTENERS WERE REMOVED IAW SRM 51-30-2, NEW REPAIR DOUBLERS WERE FABRICATED IAW SRM 52-05D, FIG 9 NEW REPAIR DOUBLERS WERE TREATED AND PAINTED IAW SRM 51-10-03, PAR 14/21 REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (LT WING) · airframe 63,114 hrs · 46,612 cycles

CRACKED REPAIR DOUBLER AND ELONGATED HOLES ON INTERNAL STRUCTURE AT LT WING INBD BUTE DOOR AFT EDGE. REPAIR WAS REMOVED, AND A NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2 AND 51-30-5, 57-01, FIG 3 AND 51-10-3, PAR 14 AND 21. HOLES WERE REPAIRED IAW ER/A 530160-14, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1287) · airframe 67,999 hrs · 50,157 cycles

CORROSION ON FRAME BS 1287, BETWEEN LONGERONS 29 TO 30L. THE FRAME WAS REPAIRED IAW SRM 53-03 D FIG 2A,

Part: PAN — CRACKED (PAX DOOR) · airframe 63,114 hrs · 46,612 cycles

CRACK BEYOND PREVIOUS STOP DRILL ON FWD UPPER CORNER AT DOOR PAN OF FWD PASSENGER DOOR. DOOR PAN WAS REPLACED IAW SRM 52-05D, 51-30-1, 51-30-2, 51-30-4.

Part: INTERCOSTAL — CORRODED (BS 1271-1287) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

INTERCOSTAL CORRODED BETWEEN BS 1271-1287 BL 0. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-10-3, PAR 21,14, 26, 38; 51-30-2, 51-30-5, ER/A 511165-14, REV B, AMM 20-30-01-201, DWG 9936580.

Part: SKIN — DAMAGED (BS 1079-1117) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

DAMAGE ON FUSELAGE SKIN BELOW RUB STRIPS AREA FROM BS 1117 - 1079 BETWEEN LONGERONS 25-30. . CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREAS WITHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21.

Part: FLOORBEAM — CORRODED (BS 1307) · airframe 67,999 hrs · 50,157 cycles

FLOORBEAM CORRODED BS 1307, X 22. REPAIRED THE FLOORBEAM.

Part: FRAME — CRACKED (BS 1485) · airframe 63,114 hrs · 46,612 cycles

CANT FRAME BS 1485 CRACKED AT LT AFT SIDE OF OTBD LIGHT ASSY. DAMAGE WAS REMOVED IAW SRM 53-03, FIG 48. REPAIR FABRICATED IAW SRM 53-03, PAR 48. REPAIR DRILLED AND TRIMED IAW SRM 53-03, FIG 48. REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. REPAIR INSTALLED IAW SRM 53-03 PAR 48.

Part: INTERCOSTAL — CORRODED (BS 1145-1155) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1145-1155 AND L28-29R. THE INTERCOSTAL WAS R&R IAW SRM 51-30-2, 51-30- 5, 51-10-3 PAR 14, 21, 26, 38 ER/A 511165-14 MA, REV B, 51-10-4.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON RT CARGO TRACK BS 1212-1322. THE CARGO TRACK WAS REMOVED, AND CORROSION WAS REMOVED. A NEW CARGO TRACK WAS DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-1, 51-10-3, PAR 26,14,21 AND 38, SRM 53-05, FIG 4C, SRM 51-10-4, 51-30-1 AND NDT SPM 04 -00-07, PAR 5, FIG 3 SHEET 1 AND 2.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FRAME BS 1380 BETWEEN LONGERONS 26 - 30R. FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9912246-REV DE.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FRAME, BS 1287 BETWEEN LONGERONS 29 - 30L. FRAME REPAIRED IAW SRM 53-03 D, FIG 2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON RT FUEL TANK ACCESS PANEL COUNTERSINK AND SETTLEMENT AREAS. THE CORROSION WAS REMOVED, AND AREAS FOUND WITHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-22-2A. AREAS OUT OF LIMITS WERE REPLACED IAW SRM 51-22-2A, CONDITION II FIG 8.

Part: FLOORBEAM — CORRODED (BS 1322) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON LT FLOORBEAM BS 1322, X 18, X 26. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 79A, SH 1.

Part: SPACER — CORRODED (BS 636-693) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON LOWER CARGO DOOR FRAME BS 636-693 LONGERON 28R. SPACER WAS REMOVED IAW SRM 51-30-2, 51-30- 4, A NEW SPACER WAS FABRICATED IAW SRM 53-05, FIG 123, OPT 1, TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21, AND INSTALLED IAW SRM 53-05, FIG 123, 51-20-0 AND 51-30-04.

Part: CARGO TRACK — CORRODED (BS 1222-1322) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON CARGO TRACK BS 1222-1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, 38 AND 51-30-1.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON RT CUSP WEB AND REPAIRS DOUBLES BS 465 - 484. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26 AND FOUND OUT OF LIMITS. DAMAGE WAS REMOVED, REPAIR FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 51-10-3, 53-05 FIG 131 AG, 51-30-2 AND 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1003-1222) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON OF THE CARGO TRACK BETWEEN BS 1003-1222. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-10-3, 51-10-4, SRM 51-10-3, AND INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON CARGO TRACK BETWEEN BS 1003-1155. THE CARGO TRACK WAS REMOVED IAW SRM 51-30-1, 51-30-2, AND A NEW CARGO TRACK WAS DRILLED IAW SRM 51-10-4, SRM 51-10-3, PAR 14, 21, AND INSTALLED IAW SRM 51- 30-2, 51-30-1.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FRAME BS 1307 BETWEEN LONGERONS 29L & 29R. SECTION OF FRAME WAS REMOVED, A NEW SECTION OF FRAME AND REPAIR WERE FABRICATED, DRILLED, TREATED PAINTED AND INSTALLED IAW SRM 53-03D, FIG 2-A.

Part: SKIN — CORRODED (BS 1096-1100) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FUSELAGE SKIN BS 1096 - 1100 BETWEEN LONGERONS 25 - 30L. REPAIRED IAW SRM 53-04, FIG 57.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON RT FUEL TANK ACCESS PANEL. CORROSION WAS REMOVED IAW SRM 51-22-2A, REPLACED IAW SRM 51-22-2A COND II.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FLOORBEAM BS 1338 X 18 AND X -18. THE FLOORBEAM WAS REPLACED IAW DWG 9912243, REV.

Part: DOUBLER — CORRODED (BS 826-830) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 826-830 X 54 - 60. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-13.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,114 hrs · 46,612 cycles

DAMAGED SKIN ON RUDDER. REPAIRED IAW SRM 51-70-1, AD PAR 23.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FLOOR PANEL 160G. CORROSION REMOVED, AND FOUND OUT LIMITS, A NEW FLOOR PANEL WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW ER/A 511165-14 MA, REV B, SRM 53-01, FIG 1, 51-10-2, 51-10-3 PAR 14/21 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 561-571) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON LEFT CUSP WEB X 56 TO X 60 BS 561 - 571. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FUEL ACCESS PANEL COUNTERSINKS. ACCESS PANEL WAS REWORKED AND WAS FOUND OUT OF LIMITS. REPLACED IAW REPLACED IAW SRM 51-22-2A.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON LOWER STRUCTURE OF CARGO DOOR FRAME BS 1155-1212 AND LONG 28R. NEW SPACER WAS INSTALLED IAW SRM 53-05, FIG 123 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FUEL ACCESS PANEL 1456C COUNTERSINK. CORROSION REMOVED. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-2A CONDITION II AND 51-10-3, PAR 21.

Part: FLOOR SUPPORT — CORRODED (BS 148.5-200) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FLOOR SUPPORT BS 148.5 - 200 BETWEEN X 7 AND X -7 W1. SUPPORT FLOOR REPLACED IAW SRM 51-10-4 AND DWG 9936534, REV BW.

Part: CUSP WEB — CRACKED (BS 1066) · airframe 63,114 hrs · 46,612 cycles

CRACK ON THE CUSP WEB BS 1066 BETWEEN X -54 TO X -60 . DAMAGE AREA WAS REMOVED, REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED.

Part: SUPPORT — CRACKED (BS 1212) · airframe 63,114 hrs · 46,612 cycles

CRACK ON SLANT SUPPORT BS 1212 BETWEEN LONGERON 28-29L IN AFT CARGO BAY. SUPPORT WAS REMOVED AND INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, P-21-14 AND 28 ER/A 413029-14MA.

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 63,114 hrs · 46,612 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 1287-1309 BL 0. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9936580-45, REV BW.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FUEL ACCESS PANEL COUNTERSINKS. CORROSION WAS REMOVED IAW SRM 51-22-2A, CONDITION 2, FIG 8 AND FOUND OUT LIMITS IAW SRM 51-22-2A, CONDITION 2, FIG 8.

Part: SKIN — CORRODED (BS 1079-1120) · airframe 63,114 hrs · 46,612 cycles

CORROSION ON FUSELAGE SKIN BELOW RUB STRIP BS 1079 - 1120 BETWEEN LONGERONS 27 - 30R. CORROSION REMOVED IAW SRM 57-04, PAR 57, 51-10-3, PAR 21 AND 14.

Part: CUSP WEB — CORRODED (BS 412-452) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BS 412--452, X -54 - X -60. REPAIRED IAW SRM 53-05, FIG 131A-13

Part: CUSP WEB — CORRODED (BS 1103-1110) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION OUT OF LIMITS ON UPPER AND LOWER SURFACE OF RT CUSP WEB BS 1103 - 1110 BETWEEN X -54 AND X -60. REPAIRED IAW SRM 51-10-3, PAR 21, 14, 38 53-05, FIG 131A-7.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

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

Part: BEAM — CORRODED (BS 1220-1231) · airframe 63,114 hrs · 46,612 cycles

CORROSION ON BEAM BETWEEN BS 1220-1231 AND LONGERON 28R AT AFT CARGO BAY. CORROSION REMOVED, AREAS TREATED AND PAINTED, CIC WAS APPLIED IAW SRM 51-10-3, PAR. 26, 21, 14 AND 38.

Part: SKIN — CORRODED (BS 849-855) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 849-855 AND STA X 54 TO 60. REPAIR DOUBLER WAS REMOVED AND A NEW REPAIR WAS FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 53-05 FIG. 131A-1, 51-30-5, 51-10-3 PAR 14,21 AND 28.

Part: STRUCTURE — CORRODED (BS 870-882) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 870-882 AND STA X=54 TO 60. REPAIR DOUBLER WAS REMOVED, FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 53-05, FIG 131A-1, 51-20-0 AND 51-10-3, PAR 14, 21, 38.

Part: SUPPORT — CRACKED (BS 1136) · airframe 63,114 hrs · 46,612 cycles

CRACK ON SLANT SUPPORT OF BS 1136 BETWEEN LONGERONS 24-28. SUPPORT WAS REMOVED, ADJUSTED, DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3, PAR 14 AND 21 AND ERA 413029-14MA. AREA WAS APPLIED CIC IAW SRM 51-10-3, PAR 38.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON BRACKET AT RT OTBD FLAP MID VANE GUIDE TO 31" OF INBD EDGE. SM, CARD 74 ZONE 00. THIS COMPOMPONENT WILL BE REPLACED INTERNAL DAMAGE DUE TO CORROSION BY OUT OF LIMITS FOR REPAIR IAW SRM 57-03D, PAR 11. RT OTBD FLAP MID VANE GUIDE WAS REMOVED. DUE TO EXCESSIVE CORROSION AND SEVERE DAMAGED RT OTBD FLAP MID VANE WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,114 hrs · 46,612 cycles

CRACKED LONGERON 16R BS 1437. LONGERON REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5, 51-10-4, 53-02, FIG 18, 51-10-3 P.

Part: SUPPORT — CORRODED (BS 1155) · airframe 63,114 hrs · 46,612 cycles

CORROSION ON SLAT SUPPORT OF BS 1155 BETWEEN LONGERONS 27- 28L. DUE TO EXCESIVE CORROSION SUPPORT WAS REMOVED AND NEW SUPPORT WAS ADJUSTED DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3, PAR 14 AND 21, AND ERA 413029-14MA AREA WAS APPLIED CIC IAW SRM 51-10-3, PAR 38.

Part: FLOORBEAM — CRACKED (BS 180) · airframe 63,114 hrs · 46,612 cycles

CRACKED FLOORBEAM BS 180 BETWEEN X 10 TO X 44. REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-3, PAR 14/21, 51-10-4.

Part: FLOORBEAM — DAMAGED (BS 160) · airframe 63,114 hrs · 46,612 cycles

FLOORBEAM ANGLE BS 160 BETWEEN X -22 TO X -44. REMOVED AND REPLACED IAW SRM 51-30-2 IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 661-668) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON A PREVIOUS REPAIR X 57 TO X 60, BS 661 - 668 OF CUSP WEB . REPAIR WAS REMOVED AND REPLACED IAW SRM 53-05, FIG 131A-13 AND 51-30-2 AND 51-10-3.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION FOUND ON LT SEAT TRACK PLUG. REMOVED AND REPLACED IAW SRM 53-05, FIG 4.

Part: SEAT TRACK — CORRODED (BS 408) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON SEAT TRACK PLUG X 22, BS 408. SEAT TRACK PLUG WAS REMOVED AND INSTALLED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 546-549) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON BS 546 - 549 SEAT TRACK. REPAIRED IAW SRM 53-05, FIG 4A.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON LT HORIZONTAL STABILIZER SKIN. CORROSION REMOVED. REPAIRED IAW SRM 5503D, PAR 30.

Part: SEAT TRACK — CORRODED (BS 554-560) · corrosion level 2 · airframe 63,114 hrs · 46,612 cycles

CORROSION ON SEAT TRACK X -54 BETWEEN BS 554 - 560. REPAIRED IAW SRM 53-05, FIG 04-A.

Part: LINKAGE — DAMAGED (TAIL CATWALK) · airframe 62,880 hrs · 46,440 cycles

THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY, RT SIDE LINKAGE WAS FOUND DAMAGED. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE LINK AT THE RT SIDE TORSION BAR WAS REPLACED, THE MOVEABLE CEILING, CATWALK, WAS ADJUSTED, AND THE SYSTEM WAS RIGGED TO MEET PUBLISHED SPECIFICATIONS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,325 hrs · 46,040 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS WERE OUT AT ROWS 27, 28, 29 AND 30. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE OPS CHECKED GOOD.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 61,198 hrs · 45,265 cycles

EMERGENCY LIGHT AT SEAT 17DE INOPERATIVE. FOUND HARNESS BROKEN. REPLACED HARNESS IAW IAW AMM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,033 hrs · 45,146 cycles

DURING LINE CHECK, NOTED THE CEILING MOUNTED EMERGENCY LIGHTS AT SEAT 33 WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES AT LOCATION 17 AND 33 IAW AMM 33-53 AND OPS CHECKED GOOD.

Part: LATCH — FAILED (CATWALK) · airframe 59,944 hrs · 44,341 cycles

MX DISCOVERED THAT THE CATWALK IN TAIL SECTION WOULD NOT STAY IN THE UP POSITION WHEN THE VENTRAL STAIRS GO DOWN. THE SPRING LATCH ASSY AND THE CABLES WERE REPLACED, THE SYS ADJUSTED IAW AMM 53-20 AND THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 1437) · airframe 59,944 hrs · 44,341 cycles

DURING SCHEDUED INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT BS 1437 BETWEEN L2L & L3L AT THE TOP 2 FASTENERS. REPAIRS COMPLETED IAW ER/A 516909-14.

Part: BUSHING — WORN (TAILCONE RELEASE) · airframe 59,944 hrs · 44,341 cycles

DURING SCHEDULED INSPECTION, THE TAIL CONE RELEASE HANDLE T-PIN, BUSHINGS & BOLT WERE DETERMINED TO BE WORN. THE T-PIN, BUSHINGS AND BOLT WERE REPLACED IAW AMM 53-53.

Part: HANDLE — GOUGED (TAILCONE RELEASE) · airframe 59,944 hrs · 44,341 cycles

DURING SCHEDULED INSPECTION, UPPER RT TAILCONE RELEASE LATCH HANDLE WAS NOTED TO BE GOUGED. THE UPPER RT RELEASE LATCH HANDLE WAS REPLACED IAW AMM 53-53.

Part: FRAME — CRACKED (BS 1437) · airframe 59,944 hrs · 44,341 cycles

FRAME CRACKED, BS 1437 AT L2R UPPER TAIL INTERIOR OTBD OF RT VERTICAL ATTACH FITTING ON PREV REPAIR. REPAIRED IAW ER/A 516946-14.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 59,944 hrs · 44,341 cycles

DURING SCHEDULED INSPECTION, TAIL CONE RELEASE MECHANISM CAM BASE WAS NOTED TO BE WORN. THE RELEASE MECHANISM WAS REPLACED AMM 53-53-02.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 59,179 hrs · 43,796 cycles

DURING AN OVERNIGHT MX CHECK, THE EMERGENCY EXIT ROW LIGHT AT ROW 24 WAS FOUND TO BE INOPERATIVE. FOUND A WIRE BROKEN AND PIN PUSHED BACK IN CONNECTOR. THE CONNECTOR WAS REPINNED AND AN APPROVED WIRE SPLICE WAS ACCOMPLISHED. OPERATION CHECKED NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 58,889 hrs · 43,601 cycles

OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN INOP. FOUND BATTERIES DISCHARGED IN BATTERY PACK B5-100. REPLACED BATTERIES IAW AMM 33-53. CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,088 hrs · 43,007 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT 32 & 33 WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND CHARGER BASE. THE LIGHTS HAVE RETURNED TO AN OPERATIONAL CONDITION.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 56,225 hrs · 41,764 cycles

MID CAGO DOOR LOWER SECTION DOOR JAMB CORROSION. REMOVED DOOR JAMB MID CARGO DOOR LOWER SECTION. FABRICATED AND INSTALLED NEW DOOR JAMB IAW DC9/MD80 SRM 53-05 DURING MAINTENANCE VISIT.

Part: SILL — CORRODED (FUSELAGE) · airframe 56,225 hrs · 41,764 cycles

AFT CARGO DOOR SILL LOWER SECTION AREA FS 1155 TO FS 1212 AREA OF CORROSION. REMOVED REPAIR SPACER AT AFT CARGO AREA FS 1155 TO FS 1212, FABRICATED SPACER AND INSTALLED IAW DC9/MD80 SRM 53-05 DURING MAINTENANCE VISIT AT ST AEROSPACE SAN ANTONIO.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 56,225 hrs · 41,764 cycles

TWO DENT ON REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN STA 210 AND 229 AND BETWEEN 1, 6 AND 18L. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW DC9/MD80 SRM 53-04 DURING MAINTENANCE VISIT.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,225 hrs · 41,764 cycles

DENT ON FUSELAGE SKIN ON TOP OF FRAME AT STA 237 BETWEEN LONGERON 18L AND 19L. MEASURED DENT ON SKIN, FOUND DENT WITH CREASE, REMOVED DAMAGED AREA AT STA 237 BETWEEN LONG 18-19L, FABRICATED REPAIR PARTS AND INSTALLED IAW DC9/MD80 SRM 53-04 DURING MAINTENANCE VISIT AT ST AEROSPACE SAN ANTONIO.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 54,556 hrs · 40,580 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY ESCAPE LIGHT AT SEAT 19D INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE ON HARNESS. HARNESS WAS REPLACED AND OPERATIONS OF LIGHT NOW CHECKS OK.

Part: OIL SYSTEM — EMPTY (NR 2 ENGINE) · airframe 49,575 hrs · 37,273 cycles

RT ENGINE LOST ALL OIL QTY IN FLT. ON DESCENT AT IDLE POWER, ENGINE SHUTDOWN. REPLACED NR 2 ENG IAW TRANS 9T102.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,111 hrs · 36,966 cycles

FUSELAGE SKIN, LOWER AIRSTAIR DOOR CORNERS BETWEEN STA Y=160 AND Y=200, LONGERON 22LT CRACK REPAIR IAW 09-069085-12 REV DME02. C/W 09-069085-12 REV D ME02

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 49,081 hrs · 36,949 cycles

THE RT HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL HAD CORROSION ON 3 INBD BARREL NUT HOLES AT XH=7.234. THE NR 12, NR 14, AND NR 17 HOLES WERE OVERSIZED, AND THE NR 17 HOLE HAD AN ADDITIONAL BLEND FOR CORROSION. OVERSIZED BUSHINGS WERE INSTALLED PER BOEING APPROVAL.

Part: BEAM — CORRODED (C1 DOOR FRAME) · airframe 49,081 hrs · 36,949 cycles

DURING HMV3 EXFOLIATION CORROSION WAS FOUND ON FWD CARGO COMPARTMENT DOOR JAMB LWD BEAM. BEAM WAS REPAIRED IAW SRM 53-05D FIG 804D.

Part: BEAM — CORRODED (C3 DOOR) · airframe 49,081 hrs · 36,949 cycles

DURING HMV EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR LWR BEAM. BEAM WAS REPAIRED IAW SRM 53-05 FIG 123 AND ERA 472715-14.

Part: BULKHEAD — DAMAGED (AFT ACCESS COMP) · airframe 49,081 hrs · 36,949 cycles

DURING HMV3 TOOLING MARKS WAS FOUND ON "P" DOME "T" BTW LONGERON 29 RT TO 29 LT AFT ACCESSORY COMPARTMENT "P" DOME "T" CAPE WAS REPAIRED IAW SRM 53-03 FIG 37.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 49,081 hrs · 36,949 cycles

DURING HMV3 EXFOLIATION CORROSION WAS FOUND ON MID CARGO COMPARTMENT DOOR JAMB LOWER BEAM. BEAM WAS REPAIRED IAW SRM 53-05 FIG 123

Part: SLEEVE — WORN (TAILCONE) · airframe 49,081 hrs · 36,949 cycles

DURING HMV WEAR WAS FOUND ON TAILCONE RELEASE SYSTEM CONTROL CABLE SLEEVE AT Y=1510 BTW 5:00 TO 7:00 O'CLOCK POSITION TAILCONE RELEASE SYSTEM CONTROL CABLE SLEEVE WAS REPLACED IAW MM 20-30-01.

Part: STRAP — DAMAGED (BULKHEAD) · airframe 42,394 hrs · 32,557 cycles

AFT PRESSURE DOME LOWER CHORD STRAP REPAIR 09-086680-12 IAW 09-086680-12. C/W 09-086680-12 ME13.

Part: OIL CAP — LEAKING (APU) · airframe 36,443 hrs · 28,239 cycles

ON TAKEOFF AFT LAV SMOKE DETECTOR WENT OFF, WITH SLIGHT ODOR IN CABIN AND COCKPIT, AFTER 30 SEC ODOR WENT AWAY AND ALARM CEASED. REPLACED LEAKING APU OIL CAP AND PERFORMED DUCT BURNOUT.

Part: DUCT — LEAKING (A/C BAY) · airframe 35,208 hrs · 27,350 cycles

TAIL COMPARTMENT TEMP HI LIGHT CAME ON DURING CLIMB THRU FL250. FOUND HIGH PRESSURE DUCT LEAKING AT CLAMP. SECURED SAME.

Part: ENGINE — FAILED (NR 2) · airframe 35,167 hrs · 27,322 cycles

CLIMBING THRU 180 RIGHT ENGINE LOST POWER, NO FIRE INDICATION. REDUCED THRUST AND LANDED. UPON LANDING FIRED BOTH BOTTLES. REPLACED NR 2 ENG S/N 725945 PER TRANS 9T102. ALSO REPLACED BOTH FIRE BOTTLES, SEPARATE LOG ITEM.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 35,167 hrs · 27,322 cycles

ON TAKEOFF CLIMBING THRU 180, RIGHT ENG LOST POWER WITH NO FIRE INDICATION. REDUCED THRUST AND LANDED. UPON LANDING FIRED BOTH BOTTLES DUE EGT RISE. FOUND ON INSPECTION RIGHT ENG TURBINE FAILURE. REPLACED ENGINE.

Part: RELAY — FAILED (E/E BAY) · airframe 34,766 hrs · 27,044 cycles

F/A REPORTED HEAVY BURNING SMELL IN CABIN, SHORTLY AFTER SMELL ALSO IN COCKPIT. DIVERTED TO CVG. DISSIPATED AFTER 10-15 MINS. T/S PER OPN 5088 COMPLETED BLOCKS 1 THROUGH 6, NO TROUBLE FOUND. C/W OP 5088 AND 5089 DUCT BURNOUT, NO ODORS NOTED. ALSO DURING T/S FOUND CABIN RECIRC FAN INOP. REPLACED RELAY R2-279, OPS CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 31,605 hrs · 24,780 cycles

EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK POWER SUPPLY AND BATTERIES.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 28,689 hrs · 22,618 cycles

AT CRUISE ALT RT GEN FAILED WITH AN AC CROSSTIE LOCKOUT. RT GEN WAS RESTORED AND FLT CONTINUED WITH GENS ISOL. NO FURTHER EVENTS. APU INOP ON PREV MCO/PLAC. CKD CSD SVC, CKS GOOD. FOUND GEN FAULT ON GCU. REPLACED SAME AND RAN ENGS. GENS AND AC CROSSTIE OPS NML PER PFHB. MCO ON APU GEN CLEARED.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 28,681 hrs · 22,614 cycles

ON 3 OCCASIONS INDICATION OF RT AC FAILURE. AC CROSSTIE REMAINED ON THROUGHOUT. REPLACED RT CSD AND GEN PER M/M, LK CKS, OPS CKS OK. CROSSTIE FUNCTIONS OP NML.

Part: VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 28,547 hrs · 22,511 cycles

LEFT ENGINE, RIGHT C/B OPEN IN FLIGHT. COMPLIED WITH PROCEDURE, CLOSED CB OPENED AGAIN WHEN ANTI ICE SELECTED. REPLACED NR 1 ENGINE RIGHT ANTI ICE VALVE CHECKS OK.

Part: STROBE — FAILED (LT WING TIP) · airframe 26,713 hrs · 21,169 cycles

POSITION LIGHT AND STROBE LIGHT C/B POPS WHEN SWITCH TURNED\ON. REPLACED SW S1-430, NO HELP. DISCONNECTED WING STROBES AND POSITION LIGHTS, NO HELP. C/B''S STILL POPPED. FOUND WHEN LT OUTBOARD LANDING LIGHT CONTROL C/B RESET ALL LIGHTS ILLUM. FOUND SHORTED WIRES AT APPROX STA XFS 70 LT WING L/E. REPLACED WIRE CLAMP AND WIRE. LIGHTS CHECK NORMAL.

Part: BRAKE — FAILED (MLG)

AT 8,000 FT BRAKE OVERHEAT LIGHT ILLUM, TEMP STARTED AT 350 AND ROSE TO 410F. THIS TEMP ON NR 4 BRAKE. COMPLIED WITH POM. LOWERED GEAR AT 14,000 FT, TEMP DECREASED, GEAR RAISED TEMP ROSE TO 275F. FOUND NR 4 TIRE BLOWN. REPLACED NR 4 BRAKE AND NR 3 AND 4 TIRE.

Part: COALESCER — DIRTY (CABIN)

REPORT OF SMOKE IN AFT CABIN BY FLIGHT ATTENDANT SHORTLY AFTER FLIGHT CREW ADJUSTED RT PACK TEMPERTURE CONTROL. REPLACED COALESER BAGS.

Part: COALESCER — CONTAMINATED (CABIN)

AFT LAV SMOKE ALARM SET OFF FOLLOWING TAKEOFF AND DURING CLIMB. F/A SMELLED SMOKE AND VERIFIED NO FIRE. RETURNED TO JFK, SMOKE ALARM RESET ITSELF AND F/A STATED SMOKE ODOR DISAPPEARED. INSPECTED LAVS, AFT GALLEY, TAIL COMP, FOUND NO ODOR. VISUAL CHECK NORMAL. FOUND APU INLET SATURATED WITH OIL. RAN ENGS AND PACKS NO ODOR AND NO SMOKE. REPLACED COALESCER BAGS. CLEANED APU INLET AND PERFORMED DUCT BURNOUT.

Part: COALESCER BAGS — DIRTY (CABIN)

ON INITIAL CLIMBOUT, A STRONG SMOKEY SMELL WAS NOTICED IN THE BACK OF THE A/C AND IN THE COCKPIT. SMELL STABILIZED AS CLIMB CONTINUED BUT DID NOT CLEAR UNTIL DESCENT BACK INTO ATLANTA. PERFORMED DUCT BURNOUT PER M/M AND REPLACED COALESCER BAGS. RAN BOTH ENGS TO T/O POWER WITH BOTH PACKS OPERATING. NO EVIDENCE OF SMOKE OR SMOKE SMELL.

Part: SKIN — PUNCTURED (BS 410)

FUSELAGE SKIN, FS 400-421, STRG 25L-26L, REPAIR FOR SKIN DAMAGE CUTOUT. THE FUSELAGE SKIN BETWEEN FS 400 AND 421 AND BETWEEN STRINGERS 25L AND 26L WAS BADLY DAMAGED BY GROUND EQUIPMENT. THE SKIN DAMAGE WAS REMOVED WITH A 21 BY 6.5 CUTOUT. THE SKIN WAS REPAIRED WITH A CLASS 2 EXTERNAL REPAIR DOUBLER PER THE GUIDLINES OF MD-88 SRM 53-04, FIG. 12B. THE REPAIR WAS DOCUMENTED PER ER/A 365087-14, REV A.

Part: SLIDE — INFLATED (GALLEY DOOR)

LT AFT GALLEY SLIDE FELL OUT AND INFLATED. REPLACED LT AFT GALLEY SLIDE.

Part: FRAME — CORROSION (BS 1271)

THE FS 1271 LOWER FRAME WAS FOUND WITH SEVERE CORROSION BETWEEN STR 28L AND 28R. A REPLACEMENT SECTION WAS SPLICED IN AND APPROVED PER FAA DER FORM 8110-3, DER DESIGNATION SO-889, DTD 06-27-97.

Part: SKIN — CORROSION (BS 788-801)

CORROSION WAS FOUND UNDER THE RT RUB STRIP IN TWO LOCATIONS AT STA 788 AND 807 BETWEEN STR 28R AND 29R. THE RUB STRIP IS LOCATED WHERE THE WING TO BODY FAIRING MEETS THE FUSELAGE. REPAIRED USING DOUBLERS AND WAS APPROVED PER FAA/ DER FORM 8110-3, DER DESGINATION SO-889, DTD 06-27-97.

Part: ELEV HINGE FTG — CORROSION (LT HORIZ STAB)

THE XE = 157-.9 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORZ STABILIZER WAS FOUND TO CONTAIN CORROSION. THE CORROSION WAS DISCOVERED IN THE BORE OF THE INBOARD LUG OF THE BRACKET UPON BUSHING REMOVAL. THE CORROSION WAS REMOVED BY OVERSIZING THE DIAMETER TO .6465. A REPLACEMENT BUSHING WAS INSTALLED. THIS REPAIR WAS APPROVED BY FAA/ DER FORM 8110-3 DER DESIGNATION SO-889, DTD 06-27-97.

Part: SKIN — DENTED (BS 332-370)

THE FUSELAGE SKIN WAS FOUND TO BE DAMAGED BETWEEN FS 332 AND 370 AT STRINGER 19R. THE DENT WAS CUTOUT WITH DIMENSIONS OF 24 FWD/ AFT BY 2.5 UP/DOWN. A REPAIR DOUBLER WAS INSTALLED ON THIS REPAIR AREA AND APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-867, DTD 6-23-97.

Part: SMOKE DETECTOR — FALSE WARNING (LAVATORY)

SHORTLY AFTER T/O, FOWARD LAV SMOKE DET WENT OFF.

Part: SKIN — CRACKED (C3 DOOR CUTOUT)

THE FUSELAGE SKIN AND UNDERLYING DOUBLER HAVE BEEN TORN/CRACKED AT THE AFT EDGE OF THE C-3 DOOR CUTOUT, AT THE NR 3 DOOR STOP. FURTHER DAMAGE WAS FOUND TO THE AFT EDGE OF THE C-3 DOOR CUTOUT BELOW THE NR 3 DOOR STOP. THE TOTAL SIZE OF THE DAMAGE IS APPROX 6 INCHES BY .625 INCH. ACCOMPLISHED REPAIRS PER DL ERA 268651-14 REV D.

Part: BALLAST — OVERHEATED (CABIN)

DURING CRUISE HAD SMOKE IN THE MID CABIN CEILING. IT WAS AN ELECTRICAL SMELL THAT COULD HAVE BEEN FROM THE LT BALLASTS. MTC DEACTIVATED THE CABIN LTS AND FWD TO MCO. SEVERAL OF THE CEILING LTS WERE FOUND INOP. THE SMOKE HAD DISSIPATED WHEN THE A/C WAS IN DESCENT. BURNED OUT LIGHTS WERE REPLACED AND A INSPECTION OF THE LIGHTING SYSTEM WAS DONE, NO DISCREPANCIES WERE FOUND.

Part: SKIN — CRACKED (FUSELAGE)

FOUND DURING E-1 LETTER CHECK, FUSELAGE SKIN CRACKED AT RT NLG STRUT DOOR AFT HINGE. REPAIRED PER SRM 53-05 FIG 62A.

Part: ANGLE — CRACKED (KEEL BEAM)

FOUND DURING E-1 LETTER CHECK, KEEL BEAM AFT ANGLE CROSSOVER CRACKED. REPAIRED PER SRM 53-05 FIG 101.