N996DL

Part: DOOR — OPEN (RT MLG) · airframe 70,084 hrs · 50,612 cycles

RT MAIN GEAR LIGHT ILLUMINATED RED/UNSAFE WITH GEAR HANDLE UP AFTER T.O. ALSO AMBER GEAR DOOR OPEN LIGHT ILLUMINATED. VERBAL FROM FLT CREW , TOWER COMFIRMED GEAR DOOR STATED OPEN. ALSO SUSPECT FLOWN ENTIRE FLIGHT W/GEAR DOOR OPEN. (LP4808728)

Part: TAIL CONE — UNWANTED DEPLOY (FUSELAGE) · airframe 69,696 hrs · 50,286 cycles

WHILE PERFORMING MEET & GREET WALK AROUND AFT TAIL CONE DEPLOYED. TAIL CONE DROPPED DUE TO AFT ENTRY DOOR ACTIVATON PLACARD PUNCTURED, ARM OVER AFT DOOR DEPLOYED. SLIDE DID NOT DEPLOY DUE TO IT BEING PINED. INSTALLED TAIL CONE PER CARD 5350-9645 JOB #000-001: INSTALLED SLIDE PER CARD 2561-4001 JOB 000-002. (LP9788921)

Part: TRAY — STUCK (CABIN) · airframe 69,740 hrs · 50,321 cycles

IN ARM REST TRY TABLE AT 10C STUCK IN DOWN POSITION PASSENGER MANAGED TO OPEN 1 TIME AND WHILE ATTEMPTING TO CLOSE/STORE HE CUT HIS FINGER. OPS CHECK NORMAL. TRAY TABLE STOWS AND COMES OUT NORMALLY AT LOC. 10C. SDR REPORTED DUE TO PASSENGER GETTING INJURED. (LP9788904)

Part: ENGINE — MAKING METAL (NR 2) · airframe 69,503 hrs · 50,116 cycles

THE FLIGHT CREW DIVERTED THE AIRCRAFT TO IAD AFTER THE FAILURE OF THE NR 2 ENGINE DURING CLIMB OUT OF RIC. MAINTENANCE FOUND METAL IN THE TAIL PIPE WITH TURBINE DAMAGE. THE NR 2 ENGINE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,305 hrs · 49,926 cycles

ALL F/C EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-50.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 69,251 hrs · 49,884 cycles

FWR LT AND RT EXIT EMERGENCY LIGHTS OVER WING INOPERATIVE. CYCLED SYSTEM POWER AND EMERGENCY LIGHTS OPS CHECK GOOD ON SEVERAL ATTEMPTS IAW MM 33-51.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 68,369 hrs · 49,180 cycles

SEAT 17D EMERGENCY LIGHT INOPERATIVE. REPLACED THE CONNECTER AT SEAT 17D. EMERGENCY LIGHT CHECKED GOOD IAW AMM 33-53-00.

Part: HEATER BLANKET — DAMAGED (RT WING) · airframe 68,327 hrs · 49,147 cycles

NDT INSPECTION OF THE RIGHT WING HEATER BLANKET, AFTER INSTALLATION SHOWS A VOID ALONG AFT INBOARD EDGE APPROX. 0.5 INCH WIDE X 8 INCHES LONG. THE HEATER BLANKET WAS REMOVED AND REPLACED IAW PRI 567147-14, REV 0 THRU 7.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,327 hrs · 49,147 cycles

EMERGENCY LIGHTS INOPERATIVE 25A AND 25E. REPLACED THE BATTERY PACK IAW AMM 33-57, CHECKED NORMAL.

Part: SKIN PANEL — DEBONDED (LT WING) · airframe 68,163 hrs · 49,035 cycles

LT WING UPPER PANEL FWD OF AILERON HAS AREA OF DISBOND BULGING MARKED. REPLACED PANEL ASSY REF BACDWG 5910515-507 INSTALL.

Part: LANYARD — DISCONNECTED (TAILCONE SLIDE) · airframe 68,163 hrs · 49,035 cycles

TAILCONE SLIDE DEPLOYMENT LANYARD DISCONNECTED. CONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 68,163 hrs · 49,035 cycles

RIGHT MAIN GEAR WHEEL WELL, CRACK IN OUTBOARD AFT ANGLED, CORNER OF WHEEL WELL PREVIOUSLY REPAIRED. REPAIRED JAM PER ERA 520687-14MA REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,163 hrs · 49,035 cycles

CRACK IN FUSELAGE, AFT LEFT SIDE, 20 INCHES FWD OF TAIL JETTISON HANDLE. INSTALLED REPAIR DOUBLER REF SRM 53-01, FIG 4 SHT 4.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 67,918 hrs · 48,853 cycles

RIGHT AFT LAVATORY SMOKE DETECTOR SOUNDED CONTINUOUSLY AFTER SINK FLOODED. SWAPPED WITH LEFT LAVATORY SMOKE DETECTOR. R & R THE LT LAVATORY SMOKE DETECTOR IAW AMM 26-13. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 67,342 hrs · 48,396 cycles

SEAT 18D EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT WIRING HARNESS AND LAMP IAW AIM 33-53. OPS NORMAL.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 67,164 hrs · 48,236 cycles

DURING FINAL APPROACH, FIRST OFFICER`S WINDSHIELD HEAT UNIT ARCED AND SPARKED VISUAL AND AURAL SPARK BOTH WINDSHIELD ANTI- FOG AND ANTI-ICE SWITHES ON, NO CIRCUIT BREAKERS TRIPPED, NO SCORCH MARKS NOTED. PERFORMED AN OPERATIONAL CHECK OF THE WINDSHIELD ANTI-ICING AND ANTI-FOG, NO TROUBLE NOTED. NO DAMAGE AROUND WINDSHIELD IAW AMM 56-10. OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 67,127 hrs · 48,205 cycles

AFT MEGAPHONE INOP. RPLD BATTERIES. NO HELP. INSTALLED NEW MEGAPHONE. OK FOR SVC.

Part: SWITCH — SPARKS (ANTI-FOG SYS) · airframe 67,025 hrs · 48,131 cycles

AFTER LANDING, TURNED ON WINDSHIELD ANTI-FOG. SPARKS BRIEFLY EMITTED FROM ELEMENT ON FIRST OFFICER`S WINDSHIELD SWITCH, PLACED OFF. OPS CHECKED THE FIRST OFFICER'S WINDSHIELD ANTI-FOG IAW AMM 30-41. OPS CHECKED NORMAL.

Part: TRANSMITTER — FAILED (OIL PRESSURE) · airframe 66,992 hrs · 48,109 cycles

CREW DECLARED AN EMERGENCY DUE TO THE RIGHT ENGINE OIL PRESSURE READING HIGH. MAINTENANCE REPLACED THE OIL PRESSURE REGULATING VALVE, THE OIL PRESSURE TRANSMITTER, AND THE OIL PRESSURE TRANSMITTER CONNECTOR PLUG. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLIDE — NO TEST (TAILCONE) · airframe 66,978 hrs · 48,100 cycles

TAILCONE SLIDE FAILED THE DEPLOYMENT TEST. THE TAILCONE DROPPED NORMALLY, LT FWD HOLD DOWN STRAP DID NOT RELEASE ON SLIDE. THE SLIDE WAS REPLACED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,317 hrs · 47,608 cycles

EMERGENCY LIGHT AT 15ED INOPERATIVE. INSTALLED A NEW HARNESS IAW AMM 33-53. OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,469 hrs · 47,021 cycles

SEAT ROW 23 EMERGENCY LIGHT INOP. INSTALLED NEW LIGHT PER MD88 MM 33-52.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,895 hrs · 46,644 cycles

MULTIPLE FIRST CLASS EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED & REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,169 hrs · 45,422 cycles

ONE CRACK WAS FOUND ON STRINGER 17L. STRINGER WAS REPAIRED IAW ER/A 541614-14 AD, REV ORIGINAL AND ER/A 541616-14, REV ORIGINAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,169 hrs · 45,422 cycles

ONE CRACK WAS FOUND ON STR 17R. STRINGER WAS REPAIRED IAW ER/A 541614-14 AD REV ORIGINAL AND ER/A 541616-14, REV ORIGINAL.

Part: SPLICE — CORRODED (BS 1338) · corrosion level 2 · airframe 63,169 hrs · 45,422 cycles

CORROSION ON SPLICE, BS 1338 BETWEEN OF 28RT TO 28LT. SPLICE DOUBLER WAS REPLACED IAW SRM 51-30-5, 51-30-2 AND DWG 9915561, REV CG.

Part: ANGLE — DAMAGED (BS 1338) · airframe 63,169 hrs · 45,422 cycles

ELONGATED HOLES ON ANGLE BS 1338 BETWEEN LONGERON 27-26 LT/RT SIDE AT C3. CLIP WAS REPAIRED IAW ETI-88-16-021, REV 5 AND ER/A 541622-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (BS 1485) · airframe 63,168 hrs · 45,421 cycles

CRACKED FRAME ON BS 1485 CANT BELOW OF PASSENGER AFT ENTRANCE DOOR STAIRWAY ACTUATING CYLINDER. FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43.

Part: BULKHEAD — DENTED (NLG WW) · airframe 63,168 hrs · 45,421 cycles

DENTED FWD BULKHEAD, BS 37, X=0 TO X=-2 AND Z=-18 IN NLG COMPARTMENT. REPAIRED IAW ER/A 543140-14, REV ORIG AND ETI 88-16-047, REV 1.

Part: FRAME — CORRODED (BS 1250) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON FRAME BS 1250 ON LONGERON 30 AT C3. FRAME WAS REPAIRED IAW SRM 53-03"D", FIG 2A SHEET 3.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB FROM 503 TO 598, X=54 TO X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPLACED IAW SRM 51-30-2 AND DWG 9930538, REV CF DUE EXCESSIVE CORROSION.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 63,168 hrs · 45,421 cycles

SUNKEN FASTENERS 9 EA AT REMOVABLE L/E SECOND ROW ABOVE BS ZFS=52.267 VERTICAL STABILIZER. VERTICAL STABILIZER WAS REPAIRED IAW SRM 55-03D, PAR 28, FIG 30, 55-03, PAR 27, FIG 29, 51-10-3, PAR 14/21, 51-10-2, 51-10-4 AND 51-30-5 AND AMDS 55-30-01045-08.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,168 hrs · 45,421 cycles

CRACK OF 0.625" OF LENGTH ON HORIZONTAL STABILIZER CENTER SECTION RT RIB HINGE PIVOT BEARING LUG. RIB WAS REPLACED IAW AMM 20-10-14, 55-10-00-201, PARA 8B, 7B AND CARD 5500-01011-08, JOB 184-0001.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

SCRATCHES AND CORROSION ON LT & RT INBD AND OTBD HINGE PIVOT BORE AT HORIZONTAL STABILIZER. LT & RT INBD AND OTBD HINGE PIVOT BORE WAS REPAIRED IAW SRM 55-02D PAR 7B ETI-88-16-042 REV 1 AND ER/A 543136-14, FINAL 1D.

Part: CARGO TRACK — CORRODED (BS 1212) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT CARGO TRACK SPLICES, BS 1212 AT C3. DUE TO EXCESSIVE CORROSION CARGO TRACK SPLICES WERE REPLACED IAW SRM 51-10-2 AND 51-30-5, DWG 5936660, REV: BZ ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 712-785) · airframe 63,168 hrs · 45,421 cycles

ELONGATED HOLES ON LT TIE TRACK FROM BS X=712 TOY=785 C2. TIE TRACK WAS ATTENDED IAW ERA 543139-14, REV ORIGINAL AND ETI-88-16-046, REV: 1.

Part: WEB — DAMAGED (BS 370) · airframe 63,168 hrs · 45,421 cycles

ELONGATED HOLE ON WEB BS 370 BETWEEN LONGERONS 26-27 RT, AT C1. REPAIR WAS ACCOMPLISHED IAW INSTRUCTIONS OF ER/A 541621-14, REV:ORIGINAL AND ETI 88-16-020, REV 3.

Part: DOUBLER — CORRODED (BS 1231-1250) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON INNER PRODUCTION DOUBLER BS 1231-1250 BETWEEN LONGERONS 28 - 29 RT. REPAIRED IAW ETI-88-16-003, REV 2 AND ER/A 541601-14, REV ORI.

Part: FITTING — CRACKED (BS 886) · airframe 63,168 hrs · 45,421 cycles

CRACKED FITTING INTO CENTER FUEL TANK BS 886, X=0, JUST ABOVE LONGERON 18, REF CARD 124, ZONE 10. FITTING INTO CENTER FUEL TANK BS 886, X=0 WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 1174-1250) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT CUSP WEB FROM BS 1174- 1179 ALSO BS 1242-1250 BETWEEN X=44- X=60 AT CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1060-1211) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT TIE TRACK BETWEEN BS 1060 TO 1211 AT C3. NEW TIE TRACK WAS DRILLED IAW SRM 51-10-4. DRILLED NEW TIE TRACK WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21, 38. NEW TIE TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON PREVIOUS REPAIR FRAME, BS 1309 BETWEEN LONGERONS 29 LT TO 28 RT. REPAIR WAS ACCOMPLISHED IAW SRM 53-03, D, FIG 2A.

Part: FRAME — CRACKED (BS 1451) · airframe 63,168 hrs · 45,421 cycles

CRACKED FRAME CLIP BS 1451 OVER LONG 2 RT. CRACKED FRAME CLIP WAS REPLACE. NEW FRAME CLIP WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 51-10-3 PAR 21 AND 14 AND DWG 9911860, REV L.

Part: CARGO TRACK — DAMAGED (BS 1007-1079) · airframe 63,168 hrs · 45,421 cycles

ELONGATED HOLES ON TIE TRACK RT BETWEEN BS 1007 TO 1079 AT C3. REPLACE TIE TRACK, NEW TIE TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND DGW 5936660, REV BZ.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

AA SCRATCHES AND CORROSION ON LT MLG FITTING BORE. BUSHING BORE WAS REPAIRED WITH FINAL MEASURE: ID 2.3365".

Part: ANGLE — CRACKED (BS 1380) · airframe 63,168 hrs · 45,421 cycles

CRACKED FRAME CLIP, BS 1380 BETWEEN LONGERONS 14RT AND 15RT. FRAME CLIP. BS 1380 WAS REPLACED IAW SRM 51-30-5, DWG 9912246, REV "CY".

Part: SKIN — CORRODED (BS 1231-1250) · airframe 65,118 hrs · 46,810 cycles

FUSELAGE SKIN & DOUBLER CORRODED, BS 1231-1250, LONGERON 29R. REPAIRED IAW ER/A 541601.

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON FRAME BS 1271 BETWEEN LONGERONS 28R TO 28L AT C3. PREVIOUS REPAIR PARTS WERE REPLACED IAW SRM 53-03D, FIG 2A SHEET 3.

Part: FITTING — CRACKED (LONGERON 17L) · airframe 63,168 hrs · 45,421 cycles

CRACKED FITTING OF LONGERON 17 AT LT CENTER FUEL TANK. NEW FITTING WAS DRILLED IAW SRM 51-10-4. FITTING WAS REPLACED AND WILL BE INSTALLED WITH CARD 123, ZONE 10.

Part: FITTING — DAMAGED (RT MLG) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

SCRATCHES AND CORROSION ON RT MLG FITTING BORE. FITTING BORE WAS REWORKED WITH FINAL MEASURE ID 2.256" THEREFORE IT`S WITHIN LIMITS IAW DGW SR09570087, REV B AND AREA WAS TREATED IAW SRM 51-10-3, PAR. 21.

Part: LONGERON — CORRODED (BS 1338) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LONGERON 29L END BS 1338. LONGERON END WAS REPLACED IAW SRM 51-30-5 AND DWG 4917650-1.

Part: SUPPORT — CRACKED (LT SLAT TRACK) · airframe 63,168 hrs · 45,421 cycles

CRACKED AFT INBD FOLLOWER BEARING SUPPORT OF SLAT TRACK NR 5 AT LT WING. BEARING SUPPORT OF SLAT TRACK NR 5 AT LT WING WAS REPLACED IAW AMM 27-80-01.

Part: DOUBLER — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON INNER PRODUCTION DOUBLER AT AFT LAVATORY PANEL BS 1287-1309. REPAIR WAS ACCOMPLISHED IAW ERA 541618-14, REV ORIG SECTION I.

Part: LONGERON — CUT (BS 1287-1309) · airframe 63,168 hrs · 45,421 cycles

LONGERON 22L BS 1287-1309 WAS CUT. LONGERON WAS CUT IAW 53-02, F18. SPLICE WAS FABRICATED IAW SRM 53-02, FIG 18. SPLICE WAS TREATED/PAINTED IAW SRM. 51-10-3 PAR 14 AND 21. SPLICE WAS INSTALLED IAW SRM 51-30-5. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO X=-60 AND BETWEEN BS 1060-1079, UPPER AND LOWER SURFACE AT CABIN FLOOR STRUCTURE. DUE TO AN EXCESSIVE DAMAGE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: FLOOR SUPPORT — CORRODED (BS 1322-1338) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT FLOOR SUPPORT, BS 1322 TO 1338 X 22. FLOOR SUPPORT REPAIRED IAW SRM 53-01, FIG 2.

Part: SKIN — DAMAGED (BS 927) · airframe 63,168 hrs · 45,421 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN, BS 927 BETWEEN LONGERON 1 AND LONGERON 2 RT. LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 927 BETWEEN LONGERON 1 AND 2 RT WAS REPAIRED IAW ETI-88-15-444, REV 2 AND ER/A 541593-14AD, REV ORIGINAL. REPAIR IS APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ER/A REV IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMITS.

Part: FITTING — CRACKED (BS 1350 BULKHEAD) · airframe 63,168 hrs · 45,421 cycles

CRACKED FITTING ON BS 1350 X -15 AND Z 22 AT AFT PRESSURE BULKHEAD VENTRAL DOOR. FITTING ON BS 1350 X=-15 AND Z=22 AT AFT PRESSURE BULKHEAD VENTRAL DOOR WAS REPLACED IAW DWG 5917579, REV DZ AND SRM 51-10-3B, 51-10-3, PAR 21.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON 7R ON BS 1338 AT INTERNAL CABIN STRUCTURE. LONGERON WAS REPLACED SRM 51-30-2, 51-30-5 AND 51-10-3, PAR 14 AND 21.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,168 hrs · 45,421 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AND CUSP WEB BETWEEN BS 446 TO 465 AND X 49 TO X 60. DOUBLER REPAIR WAS REPLACED IAW SRM 51-30-5, PAR 7,8, SRM 53-05, FIG 131A-14, SRM 51-10-3, PAR 14, 21, 38.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 63,168 hrs · 45,421 cycles

DELAMINATED FLOOR PANEL IN PASSENGER CABIN. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON NR 3LT BS 1437. CRACK WAS ATTENDED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 21,14, 53-02, FIG 18 51-10-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON END NR 2L ON BS 1338 AT CABIN PASSENGER LONGERON ENDS, 2EA WERE REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-10-3 PAR 14 AND 21.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,168 hrs · 45,421 cycles

DELAMINATED FLOOR PANEL 617B. A NEW FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: DOOR FRAME — CORRODED (BS 1154-1212) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LOWER DOOR JAMB AREA BS 1154 TO 1212 AT AFT CARGO COMPARTMENT. BEAM FROM BS 1155 TO 1212 WAS REPAIRED IAW SRM 53-05, FIG 123A, 51-10-3, PAR 26, 21 AND 14.

Part: CUSP WEB — CORRODED (BS 1041-1060) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO X=-60 AND BETWEEN BS 1041-1060, UPPER AND LOWER SURFACE, AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, SRM 51-10-3, PAR 14, 21, 26 & 38, SRM 53-01, FIG 1, SRM 53- 05, FIG 131A-13, TOPP 30-10-70.

Part: CUSP WEB — CRACKED (BS 995) · airframe 65,118 hrs · 46,810 cycles

CRACK ON LEFT CUSP WEB BS 995 BETWEEN RBL 54 TO 60. CUSP WEB WAS REPAIRED IAW SRM.

Part: WIRE — BROKEN (TAILCONE SLIDE) · airframe 63,168 hrs · 45,421 cycles

MAINTENANCE FOUND BROKEN WIRES ON THE TAILCONE SLIDE DEPLOYMENT SYSTEM CONTROL CABLE NR 527. CABLE SEGMENT 527 WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 992-997) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB BS 992 TO 997 AND BS Y=1019 BETWEEN X=-54 TO X=-60 AT CABIN FLOOR STRUCTURE REF CARD 253, ZONE 201. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-2, 51-10-3 P.21, 14, 38, 51-30-2.

Part: HOUSING — WORN (L1 DOOR) · airframe 63,168 hrs · 45,421 cycles

WEAR ON LOWER HOOK HOUSING ON L1. HOOK HOUSING ON L1 WAS REPLACED IAW SRM 53-04, FIG 24.

Part: CUSP WEB — CORRODED (BS 693) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION OUT OF LIMITS ON CUSP WEB RT BS 693 AND X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-10.

Part: CHANNEL — CRACKED (MLG DOOR FRAME) · airframe 63,168 hrs · 45,421 cycles

CRACKED PREVIOUS REPAIR ON LT FWD MLG WHEELWELL DOOR JAMB CHANNEL X=60 BS 946. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1460C. FUEL ACCESS DOOR 1460C WAS REPLACED IAW 57-30-00 AND FUEL MEASURING STICK WAS INSTALLED UNDER CARD 343, ZONE 100.

Part: CUSP WEB — DAMAGED (BS 712-740) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

REWORK OUT OF LIMITS ON RT CUSP WEB, BS 712 TO 740 BETWEEN X=44 AND X=60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1335. FUEL ACESS DOOR 1335C WAS REPLACED IAW IPC: 57-30-00.

Part: CUSP WEB — CORRODED (BS 885-908) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO -60 AND BETWEEN BS 885-908, UPPER AND LOWER SURFACER AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIR IAW SRM 53-05, FIG. 131A-13.

Part: PAN — CRACKED (BS 651-661) · airframe 63,168 hrs · 45,421 cycles

CRACK ON LOWER PAN BETWEEN BS 651-661 AT C2 DOOR. CRACK WAS STOPPED IAW SRM 51-01, 21. NEW DOUBLER WAS FABRICATED PAINTED AND INSTALLED IAW SRM 52-03A, 51-10-3, 51-30-2 AND 51-30-4.

Part: RUDDER — DAMAGED · airframe 63,168 hrs · 45,421 cycles

DAMAGE FLAME SPRAY PREVIOUS REPAIR ON LT SIDE OF RUDDER. LT AND RT SIDE OF RUDDER WAS REPAIRED AND PAINTED IAW SRM 51-70-1AD AND 51-10-3B, PROCESS B.

Part: CUSP WEB — CORRODED (BS 617-640) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT CUSP WEB FROM 617 TO 622, 636 TO 640 BETWEEN 54 TO 60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, 30. 51-30-2, 51-30-5, 51-10-8 DWG 9930538, REV CF.

Part: CUSP WEB — CRACKED (BS 805) · airframe 63,168 hrs · 45,421 cycles

CRACK ON RT CUSP IN X=-54 AND BS 805 AT CABIN FLOOR STRUCTURE. CUSP RT IN X=-54 AND BS 805 WAS REPAIRED IAW SRM 53-05, FIG 131A-4, SHEET 1, 51-30-5, 51-30-2, 51-10-3 PAR 21, 14, 38 AND 51-10-4, 51-01 P.25

Part: GUIDE VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT INBD GUIDE VANE OF INBD FLAP INBD HINGE BRACKET. LEFT INBD GUIDE VANE OF INBD FLAP WAS REPLACED FOR NEW 1 IAW AMM 27-51-01 AND WILL BE ADJUSTED UNDER CARD 139.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT CUSP WEB FROM BS 598 TO 617 BETWEEN X=44 TO X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON FWD LAVATORY PANEL INNER SKIN. DUE TO EXCESSIVE DAMAGE, FWD LAVATORY PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-3, AND 51-10-4.

Part: LONGERON — CRACKED (BS 541) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON 3L BS 541 AT CABIN PAX. LONGERON WAS REPAIRED IAW SRM 53-02, PAR 12, FIG 18, SHEET 1.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON 12L BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-10-3 PAR 21/14 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,168 hrs · 45,421 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SEAT TRACK — CORRODED (BS 214-234) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT SEAT TRACK X=-54 BETWEEN BS 214 - 234. A NEW SEAT TRACK WAS DRILLED AND ADJUSTED IAW SRM 51-10-4 AND INSTALLED IAW SRM 53-05, FIG 4F.

Part: WIRE — BROKEN (TAILCONE SLIDE) · airframe 63,168 hrs · 45,421 cycles

MAINTENANCE FOUND BROKEN WIRES ON THE TAILCONE SLIDE DEPLOYMENT CABLES 545 AND 547. CONTROL CABLES 545 AND 547 WERE REPLACED.

Part: SKIN — DAMAGED (BS 261) · airframe 63,168 hrs · 45,421 cycles

LIGHTNING STRIKE ON COUNTERSINK AT FUSELAGE SKIN BS 261 BETWEEN LONGERON 29LT TO 30. FUSELAGE SKIN BS 261 BETWEEN LONGERON 29LT TO 30 IN REF MON, 88 L/L , 0592913; VIS ER/A 498753-II; FSLG SKN ; 996. WAS REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 6 AND 33. PERMANENT REPAIR PERFORMED, PERMANENT REPAIR METHOD VISUAL / INITIAL 8000 CYCLES, REPETITIVE - 8000 CYCLES.

Part: GUIDE VANE — DENTED (LT WING TE FLAP) · airframe 63,168 hrs · 45,421 cycles

DENT LT MID GUIDE VANE OF OTBD FLAP BETWEEN BS XV2=218 AND XV2=245. DENT ON LT MID GUIDE WAS REPAIRED IAW SRM 57-03, PAR 11 AND OPEN 1031, CARD 2000-8149-06.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACE IAW DWG 9957828 AND CORROSION ON FILLER WAS ATTENDED IAW SRM 51-10-3, PAR 26-21-14.

Part: DOUBLER — WORN (BS 1287-1309) · airframe 63,168 hrs · 45,421 cycles

WORN DOUBLER, TITANIUM, ON AFT LAVATORY PANEL BS 1287-1309. DOUBLER WAS FABRICATED IAW SRM 51-30-2, 51-10- 3 AND DWG 5911423, REV CD.

Part: SKIN — CRACKED (BS 100) · airframe 63,168 hrs · 45,421 cycles

RUN CRACK ON EXTERNAL FUSELAGE SKIN BS 100 BETWEEN LONGERONS 27 - 28R. HFEC INSPECTION WAS PERFORMED ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERONS 27RT -28RT, BS 100 AND WAS FOUND A CRACK OF 0.375" LENGTH IAW NDT SPM 06-10-01.001. CRACK WAS STOP DRILLED WITH 0.250" DIAMETER IAW SRM 53-05, PAR.162.D. 2, A AND FIG 158, SHEET 1. AREA WAS REPAIRED WITH REPAIR DOUBLER IAW SRM 53-05, PARA 162 AND FIG 158.

Part: CUSP WEB — CORRODED (BS 582-594) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 582 TO 594, X = 54-60 AT CPAX, IN REF CARD 122, A/C ZONE 201. REMOVE DAMAGE, REPAIR PARTS WAS FABRICATED IAW SRM 53-05, FIG 131A-14. REPAIR PART WAS TREATED AND PAINTED, APPLY CIC IAW SRM 51-10-3, PAR 21,14 AND 38.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1371C. FUEL ACCESS DOOR 1371C WAS REPLACED IAW SRM 51-22-24 AND IPC 57-30-60.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1357C. FUEL ACCESS DOOR 1357C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

SCRATCHES ON COUNTERSINK AT FUEL TANK ACCESS PANEL 1307C. FUEL ACCESS DOOR 1307C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

COOROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1436C. FUEL ACCESS DOOR 1436C WAS REPLACED IAW SRM: 51-22-2A AND IPC:57-30-00.

Part: SEAT TRACK — CORRODED (BS 200-237) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON RT SEAT TRACK X=-44 BETWEEN BS 200 TO 237 AT PAX CABIN IN REF CARD 78, ZONE 200, NRC 20000093922 CARD. SEAT TRACK X=-44 BETWEEN BS 200 TO 237 WAS REPLACED IAW SRM 53-05, FIG 4F, 51-10-4, 51-30-1, AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1454C. FUEL ACCESS DOOR 1454C WAS REPLACED IAW SRM: 51-22-2A AND IPC: 57-30-00.

Part: GUIDE VANE — GOUGED (RT WING TE FLAP) · airframe 63,168 hrs · 45,421 cycles

GOUGE ON RT INBD GUIDE VANE 3 OTBD FLAP LOWER SURFACE BETWEEN BS XV1 =153 AND XV1=181. GOUGE ON RT INBD GUIDE VANE OTBD FLAP LOWER SURFACE BETWEEN XV1=153 AND XV1=181 WAS REPAIRED IAW SRM 57-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1476C. FUEL ACCESS DOOR 1476C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AREA OF FUEL ACCESS PANEL 1355C. FUEL ACCESS DOOR 1355C WAS REPLACED IAW SRM: 51-22-2A AND IPC:57-30-00.

Part: INTERCOSTAL — CRACKED · airframe 63,168 hrs · 45,421 cycles

CRACKED INTERCOSTAL BETWEEN BEAM 3 AND 4 AND MECHANISM AREA AT FWD MAIN ENTRANCE DOOR. THE INTERCOSTAL WAS REPLACED IAW DWG 9955763 REV M AND SRM 51-30-1, 51-30-2, 51-30-5 AND 51-10-4.

Part: DOOR FRAME — WORN (RT MLG WW) · airframe 63,168 hrs · 45,421 cycles

WORN CHANNEL ON RT FWD MLG WHEEL WELL DOOR JAMB BETWEEN X= -30 TO X=-60. CHANNEL WAS REPLACED IAW DWG 5930584, REV BY, SRM 51-30-2, AND SRM 51-30-5.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,168 hrs · 45,421 cycles

CRACKED CHANNEL OF FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, AND SRM 51-70-1D PAR 10. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS FOUND AFTER STOP DRILL.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON 13L BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4 AND 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 63,168 hrs · 45,421 cycles

PUNCTURES ON FLOOR PANEL OF PASSENGER CABIN. FLOOR PANEL WERE FABRICATED IAW AMM 53-20-01-201.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 63,168 hrs · 45,421 cycles

CRACKED FWD EDGE OF BEAM, NR 4 AT FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5.

Part: DOOR — CRACKED (SLAT TRACK) · airframe 63,168 hrs · 45,421 cycles

CRACK ON RT SLAT TRACK DOOR NR 1 AND 13. SLAT TRACK DOOR NR 1 AND 13 WERE FABRICATED IAW ER/A 512356-14MA REV ORIGINAL.

Part: RIB — CRACKED (RT WING) · airframe 63,168 hrs · 45,421 cycles

CRACKED RIB ON RT WING L/E AT BS XRS 339 APPROXIMATELY. RIB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT SETTLEMENT AREA OF FUEL TANK PANEL 1303C. FUEL ACCESS DOOR 1303C WAS REPLACED IAW IPC 57-30-00 ITEM 147.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1409C. ACCESS DOOR 1409C WAS REPLACED IAW IPC 57-30-00, ITEM 147.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1311C. DOOR IS OUT LIMITS AND IT WAS REPLACED IAW IPC 57-30-00 AND SRM 51-22-2A.

Part: MEMBRANE — CRACKED (BS 216) · airframe 63,168 hrs · 45,421 cycles

CRACK ON MEMBRANE BS 216, X=-42 AT CABIN FLOOR STRUCTURE. MEMBRANE WAS REPLACED IAW SRM 51-30-2, SRM 53-14-1, FIG 11, SRM 51-10-4, SRM 51-10-3 PAR 14 & 21, SRM 51-30-5, AND SRM 51-30-8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1464C. FUEL ACCESS DOOR 1464C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON SETTLEMENT OF FUEL TANK ACCESS 1307C. DUE TO ACCESS DOOR WAS FOUND WITH COUNTERSINK OUT OF LIMITS.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1361C. ACCESS DOOR 1361C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION AT SETTLEMENT AREA OF FUEL ACCESS PANEL 1367C. FUEL ACCESS DOOR WAS REPLACED. IAW SRM:51-22-2A AND IPC:57-30-00.

Part: CUSP WEB — DAMAGED (BS 168-200) · airframe 63,168 hrs · 45,421 cycles

PERFORATED CUSP WEB IN BS APPROXIMATELY 168.750 AND 200 X=58 RT. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, SRM 53-01, FIG 4, SH 4, SRM 51-10-3, PAR 14, 21, SRM 51-30-5.

Part: CUSP WEB — CRACKED (BS 199) · airframe 63,168 hrs · 45,421 cycles

CRACK CUSP WEB AT BS 199 X=-22 AT CABIN PASSENGER LIGHT. SUPPORT WAS REMOVED TO ATTEND WEB REPAIR THEN WEB WAS REPAIRED IAW SRM 53-01, FIG 4. FINALLY FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: BEAM — CRACKED (PAX DOORWAY) · airframe 63,168 hrs · 45,421 cycles

CRACKED BEAM NR 2 ON FWD EDGE OF FWD MAIN ENTRANCE DOOR. BEAM NR 2 ON FWD EDGE OF FWD MAIN ENTRANCE DOOR WAS REPAIR IAW SRM 52-05. FIG. 99, SHEET 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,168 hrs · 45,421 cycles

CRACKED LONGERON NR 16, LT BS Y=1437. LONGERON 16 LT WAS REPLACED IAW SRM 53-14-4, FIG 4.

Part: ACCESS DOOR — PUNCTURED (NOT REPORTED) · airframe 63,168 hrs · 45,421 cycles

PUNCTURE ON SECONDARY ACCESS DOOR LOWER SURFACE NR 1410C, TASK CPCP 28-012-02. SECONDARY ACCESS DOOR WAS REPLACED IAW ER/A 530866-14AD, REV ORIGINAL.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACK ON WINDOW RING PAN FWD UPPER CORNER BETWEEN 11R-12R AND BS 946 AT PAX CAB. CORNER UPPER FWD ON WINDOW RING PAN BETWEEN 11RT-12RT AND BS 946 WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ERA 487747-14MA AND ERA 493648-14MA.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,168 hrs · 45,421 cycles

CRACK ON AFT PAN EXTERNAL FACE BETWEEN BEAM NR 1 AND 2 AT C1 DOOR. CRACK ON AFT PAN EXTERNAL FACE BETWEEN BEAM NR 1 AND 2 AT C1 DOOR WAS REPAIRED IAW SRM 52-05.

Part: STOP FITTING — CRACKED (EMERGENCY EXIT) · airframe 63,168 hrs · 45,421 cycles

CRACKED CLIP ON RT FWD OVERWING EMERGENCY EXIT DOOR AT STOP FITTING NR 12. CRACKED CLIP ON RT FWD OVERWING EMERGENCY EXIT DOOR AT STOP FITTING NR 12 WAS REPLACED IAW SRM 51-30-2.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACK ON WINDOW RING PAN FWD UPPER CORNER BETWEEN STR 11R-12R AND BS 845 AT PAX CAB. CORNER UPPER FWD ON WINDOW RING PAN STR 14-12, RT AND BS 845 WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ERA 487747-14MA AND ERA 493648-14MA.

Part: CHANNEL — WORN (BS 937) · airframe 63,168 hrs · 45,421 cycles

WEAR ON CHANNEL AT LT FWD MLG DOOR JAMB BETWEEN X=30 TO X=44 BS 937. CHANNEL AT LT FWD DOOR JAMB BS 937 WAS REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACKED FWD/UPPER CORNER ON LT WINDOW RING PAN BS 294-BS 313 AT CPAX. CORNER UPPER FWD ON LT WINDOW RING PAN BS 294-313 WAS REPAIRED IAW SRM 53-05, FIG 122, ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 63,168 hrs · 45,421 cycles

DELAMINED COCKPIT FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACK ON WINDOW RING PAN FORWARD LOWER CORNER BETWEEN BS 14R-15R AND BS 1155 AT PAX CAB. CORNER LWR FWD ON WINDOW RING PAN BETWEEN STR 14R-15R AND BS 1155 WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ERA 487747-14MA AND ERA 493648-14MA.

Part: SKIN — WORN (NOT REPORTED) · airframe 63,168 hrs · 45,421 cycles

WEAR ON LOWER SKIN XRS=104 SETTLEMENT AREA OF FWD FAIRING HINGE, NR 1. WEAR WAS BLENDED OUT IAW SRM 57-01, FIG 1.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACKED UPPER FWD CORNER ON LT WINDOW RING PAN BS 886-BS 905 AT CPAX. CORNER UPPER FWD ON LT WINDOW RING PAN BS 886-905 WAS REPAIRED IAW SRM 53-05, FIG 122, ER/A 487747-14MA REV ORIGINAL AND ER/A 493648-14MA, REV A.

Part: SKIN — DAMAGED · airframe 63,168 hrs · 45,421 cycles

LIGHTNING STRIKE ON LWR/FWD CORNER WINDOW BELT NR 58. WINDOW BELT WAS REPAIRED IAW ER/A 541594-14, REV ORIGINAL, UT, WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SH 1 AND 2. DIMENTIONS AS FOLLOW WINDOW STA BETWEEN 769 TO 750 RT WINDOW ZONE 1 ORIG THICK=0.090" MIN. REMAINING THICKNESS: 0.084" X1=.300 X2=.300 BLENDED AREA ON CRITICAL ZONE. THEREFORE IT'S WITHIN LIMITS IAW ER/A 541594-14 REV ORIGINAL. THIS REPAIR IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL, DEC-15, IAW ERA 541594-14 REV. ORIGINAL LOG 2288029.

Part: GUIDE VANE — WORN (LT WING TE FLAP) · airframe 63,168 hrs · 45,421 cycles

WEAR ON LT OTBD GUIDE VANE, OTBD FLAP, INBD EDGE. LT OTBD GUIDE VANE, OTBD FLAP INBD EDGE WAS REPAIRED IAW SRM 57-03, PAR 11, ACFT 0996, CARD 2000-8149-08, JOB 000-0012 AND ER/A 521199-14MA, REV ORIGINAL.

Part: PAN — CRACKED (WINDOW) · airframe 63,168 hrs · 45,421 cycles

CRACKED LOWER AFT CORNER ON LT WINDOW RING PAN, BS 886-BS 905 AT CPAX. CORNER LOWER AFT ON WINDOW RING PAN BS 886-BS 905 AT C PAX WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ER/A 487747-14MA, REV ORIGINAL AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1003-1022) · airframe 63,168 hrs · 45,421 cycles

CRACKED UPPER/AFT CORNER ON LT WINDOW RING PAN BS 1003-1022. REPAIRED IAW SRM 53-05, FIG.122, ER/A 487747-14MA, REV, ORIGINAL AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 807-826) · airframe 63,168 hrs · 45,421 cycles

CRACKED FWD/UPPER CORNER ON LT WINDOW RING PAN BS 807-826. REPAIRED IAW SRM 53-05 PAR 139, FIG 122, ER/A 487747-14MA REV ORIGINAL AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 674) · airframe 63,168 hrs · 45,421 cycles

CRACK ON WINDOW RING PAN AFT UPPER CORNER BETWEEN STR 11-12R AND BS 674. REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ER/A 487747-14MA REV ORIGINAL AND 493648-14MA REV A.

Part: PAN — CRACKED (BS 1003-1022) · airframe 63,168 hrs · 45,421 cycles

CRACKED UPPER/AFT CORNER ON LT WINDOW RING PAN BS 1003-1022. REPAIRED IAW SRM 53-05 FIG 122, ER/A 487747-14MA, REV ORIGINAL AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 946-965) · airframe 63,168 hrs · 45,421 cycles

CRACKED UPPER /FWD CORNER ON LT WINDOW RING PAN BS 946-965. REPAIRED IAW SRM 53-05, PAR 139, FIG 122, ER/A 487747-14MA REV ORIGINAL AND ER/A 493648-14MA REV A.

Part: PAN — CRACKED (BS 1212-1231) · airframe 63,168 hrs · 45,421 cycles

CRACKED AFT/UPPER CORNER ON LT WINDOW RING PAN BS Y=1212-1231. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: SKIN — DAMAGED (BS 955) · airframe 63,168 hrs · 45,421 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 955 BETWEEN LONGERONS 1 - 2 RT. SKIN WAS REPAIRED. FASTENER WAS REPLACED IAW SRM 53-04-1 PARR 6C2 CONDITION 2. DAMAGE ON SKIN WAS REPARED IAW SRM 53-04-1 PARR 5C CONDITION 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,168 hrs · 45,421 cycles

CRACK ON AFT CUT OUT SKIN HOUSING AT C2 DOOR. CRACK ON AFT CUT OUT SKIN HOUSING WAS REMOVED IAW ERA 486446-14MA REV ORIGINAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,168 hrs · 45,421 cycles

CRACKED NR 5 STOP FITTING FWD SECTION AT CARGO DOOR. DAMAGE STOP FITTING WAS REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: GUIDE VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON LT INBD GUIDE VANE OF OTBD FLAP, 3 BETWEEN BS XV1 181 AROUND MID ACCESS HINGE. LT INBD GUIDE VANE OF OTBD FLAP, 3 WAS REPLACED IAW AMM 27-51-03-201.

Part: GUIDE VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON OTBD GUIDE VANE OF OTBD FLAP RT LOWER MID SECTION. NEW VANE WAS INSTALLED IAW AMM 27-51-03.

Part: SKIN — WORN · airframe 63,168 hrs · 45,421 cycles

WEAR ON LOWER/ FWD DOUBLER EXTERNAL SKIN AT C1 DOOR. DAMAGE DOUBLER WAS REPLACED IAW ER/A 486624-14MA, REV ORIGINAL.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,168 hrs · 45,421 cycles

CRACKED PAN ON RT FWD OVERWING EMERGENCY EXIT DOOR AT STOP FITTING NR 2. CRACKED PAN ON RT FWD OVERWING EMERGENCY EXIT DOOR AT STOP FITTING NR 2 WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 63,168 hrs · 45,421 cycles

CRACKED ANGLE ON RT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1155-1161) · corrosion level 2 · airframe 63,168 hrs · 45,421 cycles

CORROSION ON PLUG AT RT SEAT TRACK X= -54 BETWEEN BS 1155 - 1161. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A.

Part: SKIN — DENTED (BS 1194-1212) · airframe 63,168 hrs · 45,421 cycles

SEVERAL DENTS ON EXTERNAL SKIN FROM BS 1194 -1212 BETWEEN BEAM NR 5 AT C3 DOOR. AFT CARGO DOOR WAS REPLACED DUE TO EXCESSIVE DAMAGE.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 62,966 hrs · 45,278 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE AFT 6 ROWS OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FRAME — CRACKED (BS 1510) · airframe 62,774 hrs · 45,137 cycles

SPIDERING CRACKS IN AFT CANTED FUSELAGE FRAME BS 1510 AT THE LT 2 LOWER ALIGNMENT PINS. HFEC VERIFIED & MARKED END OF CRACKS (3EA) QC1984. CUT OUT DAMAGED SECTION OF FRAME (2EA). HFEC INSPECTED PER NDT-SPM 06-10-01. 001 BOTH CUTOUTS NO DEFECTS NOTED. DAMAGED CONTAINED QC1984. REMOVED TAILCONE SLIDE, REMOVED AFT SECTION OF WALKWAY (2PIECES), DISCONNECTED LOWER SEGMENT OF TAILCONE RELEASE CABLE & LATCH ASSY, AND REMOVED, TAILCONE SEAL. REMOVED FRAME. CLEANED AREA AND REMOVED. DRILLED UP NEW FRAME P/N 5966769-1. OK TO INSTALL QC1976. INSTALLED FRAME PER BOEING DOCUMENT 9911843. INSTALLED AFT SECTION OF WALKWAY, LOWER SEGMENT OF TAILCONE RELEASE CABLE AND LATCH ASSY, AND TAILCONE SEAL, TAILCONE SLIDE TO BE INSTALLED ON AMDS CARD 2561-4001.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 62,765 hrs · 45,133 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 15D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AND WAS REPLACED. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: FUSE — FAILED (POWER SUPPLY) · airframe 62,465 hrs · 44,901 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROWS 31 - 36 INOPERATIVE. REPLACED THE FUSE ON POWER PACK B5-212.

Part: RELEASE CABLE — CORRODED (TAILCONE) · airframe 61,960 hrs · 44,558 cycles

AFT PASSENGER DOOR EMERGENCY TAILCONE RELEASE CABLE IS FROZEN INTERNALLY, CORRODED. REPLACED EMERGENCY RELEASE CABLE IAW AMM 53-53-00-501.

Part: PIN — MIGRATED (L1 DOOR SLIDE) · airframe 61,066 hrs · 43,946 cycles

MAINTENANCE FOUND THE L1 DOOR SLIDE PARACHUTE PINS MIGRATED OUT OF POSITION. THE L1 DOOR SLIDE RAFT WAS REPLACED. LP6705059.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 60,874 hrs · 43,817 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE FORWARD ENTRY GALLEY MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE UNDER SEAT 1CD. MAINTENANCE INSTALLED A NEW QUICK DISCONNECT AND RECONNECTED THE WIRE AND THE OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (BS 749) · airframe 60,764 hrs · 43,740 cycles

DAMAGED RT FUSELAGE SKIN AT BS 749 BETWEEN STR 20 21R. CUT OUT DAMAGED SKIN IAW SRM 53-04-3, FIG 2, SHEET 3. FABRICATED REPAIR PARTS IAW ARM 53-04-0 FIGURE 2, SHEET 3. INSTALLED REPAIR IAW SRM 53-04-3, FIG 2, SHEET 3, CLASS II REPAIR.

Part: SKIN — DAMAGED (BS 620) · airframe 63,595 hrs · 45,696 cycles

LIGHTNING STRIKE AT A FASTENER BS 620 ABOVE STR 17R. ACFT NR CHANGED FROM: 0966-0996. REMOVED FASTENER, INSTALLED TIME LIMITED FASTENER IAW SRM 53-04-02, PAR 3C, 2,B. REPLACED BLIND FASTENER PRIOR TO 8000 CYCLES FROM 43598. REDEFERRED LOG TO QC, ESTABLISHED MONITOR INSPECTION, 20-0553-8-1248, SN 00966 L/L. BLIND FASTENER WAS REMOVED IAW SRM 51-30-8. HFEC WAS ACCOMPLISHED ON FUSELAGE SKIN AT BS AND BS 17RT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. EQUIPMENT: PHASEC 2D, GD-1041, EXP 27-MAR-16. FASTENER WAS INSTALLED IAW SRM 51-30-2. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-04-2 PAR 3C, 2B, PAGE 11. PLEASE CLOSE THIS LOG 1755090, PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 53-04-2, PAR. 3C, 2, B, PAGE 11. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT 01JAN16 AND LOG COMMENTS.

Part: SKIN — DAMAGED (BS 610) · airframe 63,595 hrs · 45,696 cycles

LIGHTNING STRIKE AT A FASTENER BS 610 ABOVE STR 17R. REMOVED FASTENER INSTALLED TIME LIMITED FASTENER IAW SRM 53-04-02, PAR 3C, 2, B. REPLACE BLIND FASTENER PRIOR TO 8000 CYCLES FROM 43589. REDEFERRED LOG TO QC,ESTABLISHED MONITOR INSPECTION, 20-0553-8-9303, SN 00996 L/L. BLIND FASTENER WAS REMOVED IAW SRM 51-30-8. HFEC WAS ACCOMPLISHED ON FUSELAGE SKIN AT BS 610 AND STR 17RT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01 001. EQUIPMENT: PHASEC 2D, GD-1041, EXP 27-MAR-16. FASTENER WAS INSTALLED IAW SRM 51-30 2. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-04-2, PAR 3C, 2, B, PAGE 11. PLEASE CLOSE THIS LOG 1755083 DUE TO PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 53-04-2 PAR. 3C, 2, B PAGE 11.

Part: PIN — UNSECURE (R1 DOOR SLIDE) · airframe 58,756 hrs · 42,364 cycles

MAINTENANCE FOUND THE R1 DOOR SLIDE PIN NOT SECURE. MAINTENANCE R & R THE DOOR SLIDE PACK IAW AMDS WC 2500-4484.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 58,352 hrs · 42,118 cycles

DURING LINE CHECK, NOTED L1 SLIDE PARACHUTE PINS NOT ENGAGED. REPLACED L1 SLIDE IAW WORK CARD 2500-4484.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,214 hrs · 42,032 cycles

CORROSION FOUND ON OUTER SKIN, BELOW AFT DRAIN MAST. REPAIRED IAW SRM 51-30-5, 51-10-3, 51-30-2, 53-04-3, FIG 11, 51-10-4, AMM 30-72-01 & NDT SPM PART 4, 04-00-07.

Part: FITTING — CORRODED (BS 1338) · airframe 58,215 hrs · 42,033 cycles

LONGERON 24L, STA 1338 AFT PRESSURE BULKHEAD CORRODED. REPLACED FITTING AT LONGERON 24L BS 1338. ALL IAW SRM 53-01, FIG 1, SRM 51-10-3, PARA 26, SRM 51-10-4, PARA 2 AND SRM 51-10-3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,913 hrs · 41,843 cycles

DURING LINE CHECK, NOTED THE OVERHEAD EMERGENCY PATH LIGHTS IN THE TAIL CATWALK AREA WERE INOPERATIVE. BATTERIES IN THE POWER PACK WERE REPLACED PER AMM 33-50 AND OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,257 hrs · 41,386 cycles

DURING SCHEDULED INSPECTION, INTERIOR EMERGENCY LIGHTS FROM ROW 21-26 AND ROW 32-34 WERE NOTED TO BE INOPERATIVE. THE BATTERY PACKS AT ROW 24 AND 33 WERE REPLACED AND OPERATION CHECKED GOOD IAW AMM 33-53.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,655 hrs · 41,010 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 14 IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: ENGINE — FAILED (NR 2) · airframe 55,819 hrs · 40,458 cycles

CREW RETURNED THE ACFT WITH THE NR 2 ENGINE SHUTDOWN. WHILE CLIMBING THRU 12,000 FEET, THE CREW HEARD A SMALL BANG FOLLOWED BY A LOUDER BANG AND THEN SHORTLY THEREAFTER NOTICED N1 AND N2 HAD ROLLED BACK AND THE EGT CLIMBED TO 800 DEG. THE FLIGHT CREW COMPLIED WITH QRH AND SECURED THE FUEL CUTOFF. MX COULD FIND VISIBLE DAMAGE IN EITHER THE INLET OR THE EXHAUST. THE ENGINE WAS CHANGED DUE TO THE HIGH EGT REACHED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,611 hrs · 40,341 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHT AT ROW 34D INOPERATIVE. R & R SEAT HARNESS AT SEAT 34D IAW MM. OPS CHECKS GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 55,373 hrs · 40,190 cycles

COCKPIT O2 BOTTLE HAD GOOD PRESSURE DURING PREFLIGHT. ON TAXI OUT CREW HEARD HISSING NOISE AND FOUND O2 BOTTLE PRESSURE DEPLETING. PRESSURE GAGE READ ZERO BY THE TIME RETURNED TO GATE. INSTALLED NEW O2 BOTTLE IAW AMM. STILL LEAKING. REPLACED OBSERVERS O2 MASK IAW AMM. LEAK AND OPERATION CHECKED GOOD.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 54,813 hrs · 39,792 cycles

AT PSV CHECK, SRM 53-24-0D, PERMANENT REPAIR AFT BAG BIN AFT OF DOOR HAS HOLE IN FLOOR PANEL. C/W SRM 53-24-0D, PERMANENT REPAIR AFT BAG BIN AFT OF DOOR HAS HOLE IN FLOOR PANEL. COMPLETED ON N/R 14. REMOVED PATCH, CLEANED AREA AND FABRICATED NEW DOUBLER OUT OF 2024 T3 .063 ORIGINAL MATERIAL2024 T3 .050 PER SRM 53-01, FIG 4 SHEET.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,398 hrs · 39,504 cycles

DURING CLIMB, FLIGHT ATTENDANT AND PILOTS NOTICED INCREASING ODOR IN CABIN AREA. AT FL250 ODOR WORSENED AND . COMPLIED WITH SMOKE AND PERFORMED AIR TURN BACK. MAINTENANCE TROUBLESHOT. NO FAULTS NOTED. UNABLE TO DUPLICATE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,260 hrs · 39,396 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD EXIT ROW OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,056 hrs · 39,262 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE ROWS1-12. REMOVED AND REPLACED EMERGENCY PATHWAY BATTERY PER AMM. OPS CHECKED NORMAL.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 53,557 hrs · 38,939 cycles

FLIGHT CREW REPORTS INTERMITTENT FUEL ODOR NOTICED IN AIR FLOW FROM PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND CHANGED BOTH COALESCER BAGS. OPERATION AND LEAK CHECKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,992 hrs · 38,587 cycles

LIGHTNING STRIKE SKIN DAMAGE AT BODY STATION 170-180 BETWEEN STA 29R AND 30. CUT OUT DAMAGE, COUNTER SUNK REPAIR DOUBLER, C/W HFEC INSPECTION OF CUTOUT AREA WITH NO ITEMS NOTED, AND REPAIRED PER BOEING MD-88 SRM 53-04.

Part: DOOR — DAMAGED (E/E BAY) · airframe 52,988 hrs · 38,584 cycles

LIGHTNING STRIKE INSPECTION, FOUND AND REPAIRED DAMAGES IAW SRM 53-04 D. NUMEROUS BURNS FROM AFT OF E AND E DOOR TO WING FILLET PANELS. ALL CONTAINED WITHIN AREA OF BLUE PAINT.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 52,868 hrs · 38,494 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-36DE OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 51,470 hrs · 37,543 cycles

FLIGHT RETURNED TO ORLANDO DUE TO ELECTRIC ODOR IN CABIN. REPORTED BY F/A AT 1000 FT. TROUBLESHOT PER AMM 05-50-01-101 PAGE 5 FIG 104. INSPECTED AFT LAVS AND AFT JUMPSEATS, OVERHEAD CEILING AREA. NO ODOR NOTED. INSPECTED AFT CABIN SIDEWALL AND CEILING LIGHTS. REPLACED UPPER LIGHTS AFT BALL CHECKED RECIRC FANS FOR OPS AND SMELL, ALL OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,622 hrs · 37,016 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 22-30 INOPERATIVE. MX REPLACED POWER SUPPLY PACK FOR LIGHTS. OPS OF LIGHTS NOW CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,014 hrs · 36,625 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. MX REPLACED LIGHT ASSY IN ROW 23D. OPS CHECK OF LIGHT, CHECKS OK IAW AMM.

Part: SLIDE — PARTIAL DEPLOY (L4 DOOR) · airframe 42,092 hrs · 22,620 cycles

DOOR 4L OPENED PARTIALLY WHILE ARMED. SLIDE DID NOT FULLY DEPLOY AND DOOR DID NOT FULLY OPEN DUE TO SURVIVAL KIT LANYARD TANGLED IN GIRT BAR. REPLACED 4L DOOR SLIDE AND INFLATOR BOTTLE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 49,523 hrs · 36,283 cycles

MAINTENANCE FOUND THE AFT GALLEY EMERGENCY DOOR LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND A BROKEN CONNECTOR. MAINTENANCE REPLACED A PIN PER WDM 33-51-14.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 49,020 hrs · 35,964 cycles

CRACK ON STIFFENER STA Y=1338 X=0 OF AFT PRESSURE BULKHEAD. REPLACED STIFFENER.

Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 49,020 hrs · 35,964 cycles

INADEQUATE DRILL HOLES ON C-1 DOOR LOWER DOOR JAMB AFT EDGE THRU WEB DOOR JAMB PAN AND BEAM AREA REPAIRED IAW ERA 481732-14, REV ORG.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 49,020 hrs · 35,964 cycles

EXFOLIATING CORROSION ON DOORJAMB LOWER BEAM BTW STA Y=370 TO Y=427 AT FWD CARGO COMPT REPAIRED IAW SRM 53-05.

Part: SKIN — CRACKED (STA 588 L30) · airframe 49,020 hrs · 35,964 cycles

CRACK ON FUSELAGE SKIN STA Y=588, LONGERON 30. REPAIRED IAW SRM 53-04.

Part: SKIN — DAMAGED (STA 769-826) · airframe 49,020 hrs · 35,964 cycles

LIGHTNING STRIKE ON WINDOW BELT PN BTW STA Y=769 TO 788, 807 TO 826. REPAIRED IAW ERA 481287-14 REV ORIG.

Part: SKIN — CRACKED (RT HORZ STAB) · airframe 49,020 hrs · 35,964 cycles

RT HORZ STAB UPPER FWD SKIN PANEL WAS CRACKED BESIDES BARRELNUT HOLE NR 19 TEMP REPAIR INSTALLED IAW ERA 481288-14, REV ORIG.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 49,019 hrs · 35,963 cycles

CORROSION ON BARREL NUT HOLES OF HORTZ STAB RT UPPER SKIN PANEL. BARREL NUT HOLES NR 26, 25, 24 AND 19 WERE REPAIRED IAW ERA 481288-14, REV ORIG.

Part: SKIN — DAMAGED (BS 256-984) · airframe 49,019 hrs · 35,963 cycles

LIGHTNING STRIKE ON WINDOW BELT PNL BTW Y=256 TO 275,Y=965 TO Y=984. DOUBLER INSTALLED STA 965-984, IAW ERA 481287-14, REV ORIG. WINDOW BELT STA 256-275 WAS BLENDED IAW ERA 481287-14, REV ORIG.

Part: SKIN — DAMAGED (RUDDER) · airframe 49,019 hrs · 35,963 cycles

DAMAGED METALIZED OF RUDDER LT AND RT SURFACE. LT AND RT METALIZED SURFACE OF RUDDER WAS REPAIRED IAW OPN 1031, CARDS 1370TO 1378.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 49,019 hrs · 35,963 cycles

EA 09-093855-03AD, REV B, ME02 OPN 0203 RT MLG SUPPORT FTG BUSHING BORE CORR RT MLG SUPPORT BUSHING BORE REPAIR WAS ACCOMPLISHED IAW ERA 481286-14AD REV ORIG.

Part: SKIN — CRACKED (RT HORTZ STAB) · airframe 49,019 hrs · 35,963 cycles

EA 09-460214-12, AD ME08, REV D, HOR STAB REAR SPAR UPPER CAP AFT SKIN INSP C/W EA 09-460214-12AD ME08 REV D, REF N/R T0169330.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 49,019 hrs · 35,963 cycles

EA 09-093855-03, REV B, ME01, CORR LT MLG SUPPORT FTG BUSHING BORE. LT MLG SUPPORT FTG REPAIR WAS ACCOMPLISHED IAW ERA 481286AD, REV ORIG.

Part: BRACKET — BROKEN (RT MLG) · airframe 47,453 hrs · 35,005 cycles

LANDING GEAR HANDLE UP - RT MAIN GEAR RED LIGHT AND GEAR DOOR OPEN LIGHT ON. LANDING GEAR HANDLE DOWN, ALL NORMAL INDICATIONS. FOUND RT MLG RETRACT ACTUATOR LOWER MOUNT BRACKET BROKEN. REPLACED BRACKET AND RESTORED FINISH ON RT MLG STRUT.

Part: CONNECTOR — SHORTED (NR 2 NACELLE) · airframe 46,173 hrs · 34,199 cycles

RT ENG "A" FIRE LOOP INTERMITTENT FAULT IN FLIGHT. FLT CREW MCO AND PLACARD APPLIED PER MEL 26-00-01A. SELECTED "B" LOOP PER MEL. DURING HI SPEED TURN OFF RECEIVED RT ENG FIRE WARNING. PULLED FIRE HANDLE AND SELECTED RT ENG "BOTH" FIRE LOOPS AND MSG EXTINGUISHED WITH LOOP "B" FAULTED. CONFIRMED WITH TOWER NO SMOKE FROM RT ENG. FOUND LOWER ENG LOOP ASSY B LOOP CONNECTOR P1-828 SHORTED AND REPLACED SAME. REPLACED B LOOP CONNECTOR P1-829 AS PRECAUTIONARY MTC. UNABLE TO DUPLICATE A LOOP FAULT. REPLACED LOWER A B LOOP ASSY AND FIRE DETECTION AMP AS PRECAUTION. ALL SYSTEMS CHECK NORMAL.

Part: VALVE — STICKING (NLG STEERING) · airframe 33,124 hrs · 25,548 cycles

AFTER TAKEOFF UNABLE TO RAISE GEAR HANDLE TO UP DETENT. REPLACED NOSE GEAR STEERING VALVE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 33,008 hrs · 25,496 cycles

EMERGENCY FLASHLIGHT LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL.

Part: SEAL — LEAKING (OVERWING EXIT) · airframe 31,266 hrs · 24,316 cycles

LEFT SIDE SQUEAL REPORTED BY FLIGHT ATTENDANT AFTER T/O. REMOVED LEFT FOWARD OVERWING EXIT DOOR CLEARED SEAL INSPECTED SEAL AND DOOR NO FURTHER DEFECTS NOTED PERFORMED OVERWING EMERGENCY EXIT CHECK ON LEFT FORWARD DOOR PER M/M.

Part: FUSE — BLOWN (CABIN) · airframe 29,228 hrs · 22,869 cycles

EMERGENCY EXIT LIGHTS INOP SEAT ROWS 1-4 AND 10-12, ALSO FWD ENTRY DOOR EXIT IDENTIFIER RIGHT SERVICE DOOR EXIT IDENTIFIER AND G2 GALLEY. FOUND BLOWN FUSE ON POWER SUPPLY B5-211. REPLACED FUSE. LIGHTS NOW CHECK NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 28,749 hrs · 22,500 cycles

FOUND F/C AND ROWS 10 AND 11 EMERGENCY LIGHTS INOP. REPLACED FUSE IN FWD EMERGENCY LIGHT BATTERY CRADLE. CHECKS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,573 hrs · 21,587 cycles

FWD FLASHLIGHT LOW BATTERY AND SEAL BROKEN. REPLACED BATTERY.

Part: WIRE — PINCHED (SEAT 24D) · airframe 25,877 hrs · 20,318 cycles

CHECK FOUND SEAT 24D EMERGENCY LIGHTS INOP. FOUND PINCHED WIRE REPAIRED SAME - EMERGENCY LIGHTS NOW OP NML.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 25,852 hrs · 20,302 cycles

ON TAKEOFF CREW NOTICED NOISE AND VIBRATION WHICH SEEMED TO BE COMING FROM BACK OF ACFT. RT HYD SYS PRESSURE AND QTY LOST THEN WHILE TURNING DOWNWIND NOTICED RT ENGINE EPR FLUX FOLLOWED BY REV UNLOCK LIGHT AND BLUE LOCKED LIGHT. EXCESSIVE VIBS APPEARED AND CREW DECIDED TO RUN ENGINE AT IDLE DUE TO CONCERNS THAT REV MIGHT HAVE DEPLOYED. ENG NOT SHUT DOWN AND LANDING NOT HARD. ALTERNATE GEAR EXTENSION ACCOMPLISHED. ENGINE FAILED. NTSB INVESTIGATING.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 24,928 hrs · 19,611 cycles

ON TAKEOFF BOTH AUTO PRESSURIZATION CONTROLLERS FAILED. CONTROLLERS FAULTED A/C MOTORS. REPLACED TRANSMISSION AND MOTOR ASSY ON OUTFLOW VALVE. VERIFICATION BITE OF NR 1 AND 2 CONTROLLERS THEN SHOWED NO FAULT.

Part: BULKHEAD CAP — CRACKED (BS 1463)

THE OUTER CAP ANGLE OF THE FS 1463 CANTED BULKHEAD WAS FOUND WITH A 1 INCH CRACK IN THE HORIZONTAL SKIN ATTACH FLANGE. THE ADJACENT SKIN WAS ALSO CRACKED. THE CRACK WAS AT THE LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE LOCATION. THE ATTACH ANGLE AND VERTICAL STAB SKIN WERE CUT FOR ACCESS. THE SKIN AND ANGLE CRACK WERE ROUTED OUT. THE CRACK CUTOUTS AND ACCESS CUTOUTS WERE REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (BS 1418)

A CRACK WAS FOUND AT L2L AND L2R AT STA 1418, IN THE FRAME. REPAIRED PER ERA 332005-14.

Part: LOCKING CYL — SHEARED (LT MLG)

AFTER GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT ILLUM. GEAR HANDLE DOWN THREE GREEN AND NORMAL INDICATION. CONTROL TOWER CONFIRMED LEFT GEAR WAS EXTENDED. REPLACED LEFT GEAR OVERCENTER LOCKING CYLINDER WAS SHEARED AT ROD END.

Part: TEMP SENSOR — FAILED (TAIL COMPARTMENT)

TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 1OO KIAS 136,000 LBS. REPLACED RIGHT TAIL COMPARTMENT TEMP SENSOR. RAN RIGHT ENGINE AND PACK PER PFHB. ALL SYS CHECK GOOD PER 36-20-02.

Part: BATTERY — DISCHARGED (COCKPIT)

OVERHEAD COCKPIT EMERGENCY LIGHT INOP. C/A REPLACED B5-23 POWER SUPPLY BATTERIES, OP CK OK.

Part: BALLAST — OVERHEATING (CABIN)

ELECTRICAL SMELL ABOVE ROW 17, FOUND BALLAST OVERHEATING AT 16 DEF. REPLACED BALLAST.

Part: SWITCH — FAILED (AUTO FLT CONTL)

ON FINAL APPROACH A/P WOULD NOT DISCONNECT WITH THE YOKE DISCONNECT SWITCHES OR THE ON/OFF SWITCH ON THE AUTO FLIGHT CONTROL PANEL. IT WAS NECESSARY TO PULL C/BS TO DISCONNECT A/P. REPLACED MODE CONTROL PANEL OPERATION NORMAL. ANALYSIS REVEALED THAT THE FGCP FAILURE WAS CAUSED BY A DEFECTIVE AUTOPILOT ENGAGE TOGGLE SWITCH. MICROSWITCH, DIVISION OF HONEYWELL INC HAS IDENTIFIED AN INFERIOR SWITCH MANUFACTURING PROCESS FOR SWITCHES PROCUCED FROM MAR 1991 TO MAY 1993. DELTA ISSUED A SPECIAL INSPECTION TO FIND AND REMOVE FROM SERVICE ALL SUSPECT UNITS.

Part: SKIN — DENTED (FS 522-541)

THE SUBJECT AIRCRAFT WAS DAMAGED BY GROUND EQUIPMENT RESULTING IN TWO PUNCTURES. THE TWO HOLES MEASURED 3.75 X 2 INCHES AND 1.5 X 1.5 INCHES. IN ADDITION, THE FORMER SKIN ATTACH ANGLE LOCATED AT FS 541 ABOVE STR 22R IS DAMAGED ON THE SKIN ATTACH FLANGE AND REQUIRES REPAIR. REPAIRS WERE ACCOMPLISHED PER DL ERA 271193-14.

Part: FRAME — CRACKED (LT MLG W/W)

DURING LETTER CHECK, FOUND A 1 INCH CRACK IN THE 0/B END OF THE LEFT MLG WHEEL WELL OPENING AFT JAMB, LOWER TEE STRIKER ANGLE. REPAIRED PER SRM 53-05 FIG 81A.

Part: SKIN — DENTED (NR 1 SLAT)

DURING LETTER CHECK, FOUND EXISTING FILLER MATERIAL FOR DENT TO NR 1 SLAT COMING LOOSE AND CHIPPED. CHECKED PER SRM 53-07 AND REPAIRED PER SRM 57-03 FIG 18A.

Part: DOOR — DAMAGED (NR 2 CARGO DOOR)

DURING LETTER CHECK, FOUND C-2 CARGO DOOR DOOR PAN/FRAME WITH GOUGE DAMAGE. REPAIRED PER SRM 52-05 FIG 27.

Part: SKIN — CRACK (FWD PAX DOOR)

DURING INSPECTION FOUND .5 INCH CRACK IN THE FWD ENTRY DOOR UPPER AFT CORNER. THE CRACK WAS REPAIRED PER SRM 52-05 FIG 32.