N786NC

Part: WIRE — CUT (EMERGENCY LIGHTS) · airframe 71,431 hrs · 65,200 cycles

SEAT EMERGENCY PATH LIGHTS INOPERATIVE AT SEATS 6, 7 AND 8. FOUND CUT WIRE UNDER SEAT 8. SPLICED IN NEW HARNESS IAW BSWPM 20-00. CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,366 hrs · 65,129 cycles

DURING L CHECK, CARGO DOOR CUTOUT WAS FOUND DENTED/BENT. CORROSION WAS ALSO FOUND. REMOVED THE CORROSION AND PERFORMED REPAIRS IAW ER/A 507883-14, SECTION 1.

Part: DOOR FRAME — CRACKED (SERVICE DOORWAY) · airframe 71,366 hrs · 65,129 cycles

CRACK NOTED AT FWD SERVICE DOOR JAMB FWD UPPER CORNER. CRACK UNDER EXTERIOR SKIN APPROX 25" IN LENGTH ACCOMPLISHED REPAIR AT FWD SERVICE DOOR JAMB FWD UPPER CORNER AREA IAW DWG SRO9530172, CONFIG -7003 AND INSTALLED ID TAG ON DOUBLER REPAIR IAW PS 900-5-1 NR 4 PERFORM NDT INSPECTION IAW SRM 51-10-5C. INITIAL INSPECTION AT 28000 LANDINGS AND AFTER INITIAL INSP PERFORM REPETITIVE INSP AT INTERVALS OF 20000 LANDINGS.

Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 70,742 hrs · 64,418 cycles

DURING LINE CHECK, MAINTENANCE REPORTED A GOUGE ON THE FORWARD CARGO DOOR. MAINTENANCE DETERMINED THE GOUGE TO BE OUT OF LIMITS, REPLACED THE CARGO DOOR, AND RETURNED THE AIRCRAFT TO SERVICE AFTER INSPECTION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 3,415 hrs · 3,094 cycles

EMERGENCY EGRESS AISLE LIGHTS, ROWS 19-22, AND RIGHT AFT OVERWING EXIT SIGN, INOP. REPLACED POWER SUPPLY UNIT AT AFT RIGHT OVERWING EXIT, CHECKS OK.

Part: WIRE — BROKEN (CABIN) · airframe 69,185 hrs · 62,822 cycles

MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AND CRACKED AT ROWS 5 - 8. MAINTENANCE FOUND WIRE UNDER SEAT 8DEF BROKEN AND RE-ATTACHED IT. MAINTENANCE ALSO REPLACED ALL THE CRACKED LENSES. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FRAME & WEB HAS CORROSION AT STA 157 LT SIDE, FWD OF AIRSTAIR CUTOUT REMOVED CORR FROM FRAME AT STA IAW SRM 51-10-3 FOUND TO BE WITHIN LIMITS FRAME IAW SRM 53-01 WEB AT STA 157 LT SIDE FWD OF AIRSTAIR CUTOUT. FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1 CUTOUT DAMAGED AREA AT WEB IAW SRM 51-70-4 FIG 1, FABBED WEB AND REPAIR DOUBLER IAW SRM 51-70-4. INSTALLED REPAIR PARTS IAW SRM 51-70-4 FIG 1AND SRM 51-30 FIG 12.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOORBOARD PANEL 29 HAS BOTTOM GUIDE SUPPORTS WITH SEVERAL CRACKS. FABRICATED PANEL IN REF TO TRAVELERS 87145850001 ASSY, 87145860001 TOP SKIN 87145840001 HAT CHANNELS IAW ERA 489927-14 REV 0.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

CORROSION ON PAN & STRUCTURE FOR POTABLE WATER STA 149 TO STA 160. LIMITS OF CORR AREA ON POTABLE WATER PAN WITHIN LIMITS PER DC9 SRM 51-10-3 WEB & STRUCTURE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1, CUT OUT DAMAGED AREAS ON WEB IAW DC9 SRM 51-70-4 FABBED AND INST REPAIR PARTS FOR WEB IAW SRM 51-70-4, & FABBED & INST FLOOR SUPPORTS IAW 53-13-1, FIG 11, 51-30-5, & 51-30-2 INST REPAIR PARTS IAW SRM 51-30-2 AND SRM 51-30-5.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FWD CARGO COMPARTMENT FUEL AUX TANK STRINGERS ARE CRACKED 2EA AS MARKED ON FWD FACE. FOUND DURING TANK RE-INSTALLATION. INSPECTION DETECTED 2EA CRACKS AT STRINGERS ABOVE 28L DETAIL I AND DETAIL II 26R, ASSET 09-182 CAL DOC 04/19/10, FABRICATED REPAIRS CHANNELS FWD CARGO COMPARTMENT. FUEL AUX TANK LOWER STR FROM 7075-0 TO 7075-T6. BATCH #0001753973.

Part: WEB — CRACKED (PAX DOOR) · airframe 68,643 hrs · 62,328 cycles

FWD PASSENGER INTERNAL DOOR WEB HAS 1 INCH LONG CRACK. FABRICATED DOUBLER REPAIR, TREATED AND PRIMED, INSTALLED DOUBLER REPAIR IAW SRM 52-01 FIG 2 SHEET 3 PAGE 10 AND SRM 51-30-2 FIG 2 PAGE 3 AND RE-INSTALLED INNER SKIN IAW SRM 51-30-2 FIG 2 PAGE 3 INSTALLED REPAIR DOUBLER AT FWD PASSENGER DOOR WEB IAW SRM 52-01 FIG 2 SHEET 3 PAGE 10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FWD CARGO COMP FUEL AUX TANK LWR STRINGERS ARE CRACKED 2EA.FWD FACE FABBED REPAIR CHANNEL STR PER SRM 53-05 FIG46. FABBED FILLERS PER SRM 53-05 PG 244, CUT OUT CRACKED AREAS PER SRM DC9 53-05 PG 244 INSPD AREAS HFEC. NO CRACK NOTED. INSTALLED REPAIR PARTS DETAIL I & DETAIL II 26R. LOCATED & DRILLED HOLES AT 4EA REPAIR CHANNELS & 2 FILLERS SRM DC9 53-05 TREATED, PRIMED & INSTALLED. REPAIR AREAS SRM 53-05 PG 244.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR SUPPORT FOR MAIN CABIN WORN AT FLOOR PANEL CONTACT POINT RT SIDE AT 408 & 427. REMOVED FLOOR PANEL FROM MAIN CABIN RT STA 389 TO 465 IAW DC-9 SRM 53-05 FIG 20A, FOUND OUT OF LIMITS IAW DC-9 SRM 53-01 PAGE 8 AT STA 408 AND 427 RBL 4. FABBED AND INST 2EA REPAIR ANGLES 2EA WEAR STRIPS AND1EA SHIM IAW DC-9 SRM 53-05 PG 100 FIG 20A. INST FLOOR PANEL IAW DC-9 A 53-20-01-201-925A-A.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR SUPPORT FOR MAIN CABIN WORN AT FLOOR PANEL CONTACT POINT LT SIDE AT STA 484, 503, 522 FWD CARGO AREA. REMOVED FLOORBOARD IAW DC9-A-53-20-01-201-925 BLEND OUT DAMAGE AREA IAW DC9 SRM 53-01 IN LIMITS IAW DC9 SRM 53-01 FIG 1. CRACK ON REPAIR PLATE, REMOVED PLATE AT STA 522 BETWEEN LBL 6 & LBL 7 IAW 51-30-02 FABBED PLATE IAW DC9 SRM 53-05 FIG 20. INST WEAR STRIP PLATE IAW DC9 SRM 53-05 FIG 20 AND 51-30-2 PG 11.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

LONGERON 17L CRACKED AT FRAME STA 389 ATTACH POINT REMOVED DAMAGE AT MAIN CABIN STA 380 TO 445 LONGERON 17 LT IAW SRM 53-02 FIG 18 PAGE 49-52. FABBED 1 EA LONGERON SECTION AND 1 EA REPAIR SPLICE IAW 53-02 FIG 18. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-3 PAGE 1 AND INSTALLED LONGERON SECTION AND 2EA SPLICES AT MAIN CABIN STA 380 TO 445 LONGERON 17 LT IAW SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

LONGERON 2 LT CRACKED AT FRAME INTERSECTION STATION Y=160. REPAIR LONGERON SECTION FROM L-2 STA 148.5 TO STA 169 IAW SRM 53-02 PG 50 FIG 18.

Part: PAN — CRACKED (DOOR FRAME) · airframe 68,643 hrs · 62,328 cycles

CRACK IN DOOR PAN STRUCTURE JUST OTBD OF SAFETY HOOK. STOP DRILLED CRACKS IN DOOR PAN IAW SRM 51-01, PG2, HFEC SURFACE INSP GS 24, 26B & 2001 NO CRACKS PASS STOP DRILL, FABRICATED REPAIR DOUBLER, IAW SRM 52-05 AND SRM 51-10-2. LOCATED & DRILLED REPAIR DOUBLER IAW SRM 51-10-4 INST REPAIR DOUBLER, STOP SUPPORT, CHANNEL, ANGLE AND "TEE" FITTING IAW SRM 51-30-2, SRM 51-30-1, SRM 51-30-4, SRM 52-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR SUPPORT ANGLE CRACKED AND BENT AT STA 712 RBL-22 TO 33. REMOVED SUPPORT ANGLE AT STA 712 RBL 22 TO 33 PER SRM 53-30-5. FABRICATED SUPPORT ANGLE PER SRM 53-13-3 PG 26. TREATED AND PRIMED AND INSTALLED FLOOR SUPPORT ANGLE PER SRM 51-30-2 PG 1 & SRM 51-10-3 PG 28 TO 32.

Part: SKIN — GOUGED (PAX DOOR) · airframe 68,643 hrs · 62,328 cycles

LT FWD PASSENGER DOOR EXTERNAL SKIN IS GOUGED AND DENTED AT HOLD OPEN LATCH AFT SIDE. BLENDED OUT DAMAGE, IAW SRM-52-12-0, FIG1, ITEM 12, MATERIAL LOSS MEASURED FOUND TO BE OUT OF LIMITS IAW DC9-52-01, FIG 1 FABBED REPAIR DOUBLER, IAW DC9-SRM-52-05, FIG20. ALODINED REPAIR DOUBLER & BLENDED AREA IAW DC9-SRM-51-30-2, DC9-SRM-51-30-5.

Part: LONGERON — CRACKED (BS 133 L25L) · airframe 68,643 hrs · 62,328 cycles

LONGERON 25L, CRACK AT FRAME STA 133 ATTACH POINT. CUT OUT DAMAGE SECTION OF LONGERON BETWEEN STA 110-133 25 LT LONGERON IAW SRM 53-02. FABRICATE LONGERON SECTION AND LONGERON SPLICE IAW SRM 53-02, PAGE 49-52, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-3. INSTALLED LONGERON AND LONGERON SPLICE IAW SRM 53-02, PAGE 50.

Part: FLOORBEAM — CRACKED (BS 712) · airframe 68,643 hrs · 62,328 cycles

RT FLOOR STUB BEAM UPPER CHORD AND WEB CRACKED FWD AND AFT SIDES STA 712 UNDER CUSP WEB AREA. REMOVED, FABRICATED, RT FLOOR STUB BEAM WEB, IAW SRM 51-30-3, PG 19 AND DWG 9923410, TREATED AND PRIMED WEB IAW SRM 51-10 -4, PG1 AND INSTALLED WEB IAW SRM 51-30-5, PG 1-3. R & R RT FLOOR STUB BEAM UPPER CHORD IAW SRM 51-30-5 PG1-3 AND SRM 51-30-2 PG1. COMPLETED INSPECTION.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 64 UNDERSIDE OF PANEL, STRIP IS CRACKED AND DISBONDED. FABRICATED NEW FILLER STRIP AND REPAIR DOUBLER, .025 IAW DWG PL9957921 AND DC9-SRM-53-01, FIG 2, SHEET 3, PG12. TREATED AND PRIMED REPAIR DOUBLER, IAW DC9-SRM-51-10-313, PAR 2, PG 1-7. INST REPAIR DOUBLER, IAW DC9-SRM-51-30-2, PAR 7. APPLIED ADHESIVE AND FILLER STRIPS TO UNDERSIDE OF PNL IAW DWG PL9957921.

Part: SKIN — CORRODED (BS 1063 L30L) · airframe 68,643 hrs · 62,328 cycles

STA 1063 AND LONGERON 30 CORROSION UNDER DOUBLER FOUND DURING MAUS INSP. REMOVED EXISTING REPAIR DOUBLER AT STA 1063 TO 1078, L29R TO L29L IAW SRM 51-30-5, PAGE 29. BLENDED OUT CORRODED AREA IAW SRM 53-04, PAGE 209, FIG 38: HFEC SURFACE INSP IAW NDTSPM 06-10-01.001. NO CRACKS NOTED AT INSP AREA, AREA OUT OF LIMITS IAW SRM 53-01, FIG 1, SHT 3. FABBED, TREATED, PRIMED AND INST INTERNAL REPAIR DOUBLER IAW SRM 53-04, FIG 38, VIEW G .

Part: FRAME — CRACKED (BS 275) · airframe 68,643 hrs · 62,328 cycles

FOUND FRAME CRACKED AT STA 275, STR 17R ATTACH POINT. REMOVED DAMAGE ON AREA AT FRAME STA 275, STR 17R IAW SRM-53-03-FIG 4, PG 5, FABRICATED REPAIR PARTS, REPAIR ANGLE, REPAIR FILLER, REPAIR PLATE IAW SRM 53-03, PG 5, FIG 4, TREATED AND PRIMED REPAIR PARTS, IAW SRM 53-03, PG 5 FIG REPAIR ANGLE AND REPAIR FILLER HEAT TREATED 7075-0 TO 7075-T6 COMPLETED. REQUIRED INSP COMPLETED.

Part: FRAME — CRACKED (BS 275 S17R) · airframe 68,643 hrs · 48,148 cycles

FOUND FRAME CRACK AT STA 275 S17R ATTACH POINT, CORRECTED. REMOVED DAMAGE ON AREA AT FRAME STA 275, STR 17R IAW SRM-53-03, FIG 4, PG 5. FABRICATED REPAIR PARTS, REPAIR ANGLE, REPAIR FILLER, REPAIR PLATE, AND PLATE REPAIR, IAW SRM 53-03, PG 5, FIG 4, TREATED AND PRIMED REPAIR PARTS SRM 51-10-3, PG 40, PAR 24.

Part: FLOOR PANEL — CORRODED (BS 200-237) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 21 HAS CORROSION AND BARE METAL. REMOVED SURFACE CORROSION FROM FLOOR PANEL, STA 200 TO 237, FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABRICATED FLOOR PANEL IAW EXISTING FLOOR PANEL LAYOUT IAW SRM 51-30-2, PG'S 15, 24, 26B TREATED & PRIMED IAW SRM 53-23-0 PG4-6. FASTENER INSTALLATION IAW SRM 51-30-2 PG 15, 24, 26B.

Part: FLOOR SUPPORT — CORRODED (BS 237-275) · airframe 68,643 hrs · 62,328 cycles

CENTER LINE FLOOR PANEL BEAM, FROM STA 237 TO 275, HAS CORROSION REMOVED FLOOR SUPPORT UPPER FLANGE STA 218 TO 303, BL0 FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1, PAG 3. FABBED NEW FLOOR SUPPORT LOCATED AND DRILLED IAW SRM 53-13-1, FIG 11, 51-10-4 AND SRM 51-30-2, PAR 2 AND SRM 51-30-05, PAGE 1 AND INST INTERCOSTAL FROM STA 275 TO 294 BL0. REMOVED AND INST NEW FLOOR SUPPORT STA 218 TO 303 BL 0 IAW SRM 51-30-5, PAR 7, PAGE 12.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

E&E COMPARTMENT STA Y207, LONGERON 24 L CRACKED. REMOVED DAMAGED SECTION OF LONGERON 24 LT STA Y207. FABBED LONGERON, LONGERON SPLICE IAW DC9 SRM 53-02 FIG 18 PG 50. REMOVED FASTENERS AT STA 207 AND 237 LT LONG 25 AND 26 AND OPENED SKIN IAW DC9 SRM 51-30-8 PG 7 PAR 13. INST REPAIR LONGERON, LONGERON SPLICE IAW SRM 51-30-2 FIG 18 PG 50. INST FASTENERS AT STA 207 -237 LT LONGERON 25 AND 26 AND CLOSED SKIN IAW DC9 SRM 51-30-2 ITEM 8 PG 26B.

Part: FRAME — CRACKED (BS 332 S17R) · airframe 68,643 hrs · 62,328 cycles

FOUND FRAME CRACK AT STA 332, STR 17R ATTACH POINT. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, REPAIR PLATE, REPAIR FILLER, AND PLATE FILLER IAW SRM 53-05, FIG 4, PG 5, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-3, PG 40, PAR 24 AND PG 15, INSTALLED REPAIR SRM 53-03, PG 5, FIG REPAIR ANGLE AND REPAIR FILLER HEAT TREATED 7075-O TO 7075-T6. COMPLETED.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 65 HAS A CORNER BROKEN. FABRICATED REPAIR DOUBLER FOR FLOOR PANEL 65 IAW SRM 53-01, PG 25, TREAT AND PRIME IAW SRM 51-10-3, PG 31. FASTENER INSTALLATION IAW SRM 51-30-2 COMPLETED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

OVERSIZED RIVNUT HOLE ON AFT SIDE OF FWD CARGO DOOR IS MISSING RIVNUT AND HOLE IS CRACKED. FABRICATED REPAIR DOUBLER IAW SRM 52-03, FIG 1. ALODINED REPAIR DOUBLER IAW SRM 51-10-3, PARA 21. PRIMED REPAIR DOUBLER IAW SRM 51-10-3B, PARA 2 F . INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, PARA 2 AND 51-30-4, PARA 2.3 AND 11. INSTALLED REPAIR DOUBLER ON AFT SIDE OF FWD CARGO DOOR CL OF DOOR COMPLETED & INSPECTED.

Part: SKIN — CORRODED (BS 1116 28L) · airframe 68,643 hrs · 62,328 cycles

FUSELAGE SKIN CORROSION AT STA 1116, STR 28L, FOUND DURING MAUS SCAN INSP. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-04, PG 218, FIG 38. CUT OUT DAMAGE AREA IAW SRM 53-04 PG. FABRICATED REPAIR PARTS IAW SRM 53-04 TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-3, PG 5. INSTALLED CONICAL WASHER ON EXISTING COUNTERSINKS ON THE AREA IAW SRM 53-04. INSTALLED REPAIR PARTS ON THE AREA IAW SRM 53-04.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 68,643 hrs · 62,328 cycles

CORROSION ON BEAM FROM STA 160 TO 200 AT PANELS 18 AND 19, ENTIRE LENGTH. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW FIG 1, REMOVED CORRODED BEAM, FABRICATED, TREATED AND PRIMED IAW SRM 51-10-4 AND 53-13-1, FIG 11 INSTALLED BEAM FLOOR SUPPORT ON STA 160 TO STA 200 IAW SRM 51-30-5, PAGE 12, PARA 7. COMPLETED INSP BY SAA INSP 108 RII BY SAA 10 8, RII SAA.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL 73, HAS NUMEROUS SCREW HOLES CORRODED, BLENDED. FLOOR PANEL FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1 AND SRM 53-25-0, FIG 4. RECEIVED MATL FOR FLOOR PANEL IAW SRM 53-23-0, FIG 5, FABRICATED FLOOR PANEL IAW SRM 53-23-0, FIG 5. TREATED AND PRIMED IAW SRM 51-10-3, PG 31, 32. INSTALLED NEW SKIN TO PANEL STRUCTURE IAW SRM 51-30-02, COMPLETED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

LONGERON 3L CRACKED AT FRAME INTERSECTION STATION BS 160. REPAIRED LONGERON SECTION 3L, STA BS 160 IAW DC9 SRM 53-02, FIG 18, PAGES 50-52.

Part: DOOR FRAME — CRACKED (BS 1068 S28R) · airframe 1,820 hrs · 1,567 cycles

AFT CARGO COMPT LOWER JAMB AT STA 1068 AND STR 28R STRINGER CLIP CRACKED. REMOVED 2 EA SPLICE REPAIR AND 1 EA TEE BRACKET AT STA 1068 AND 28R AFT5 CARGO IAW SRM 51-30-15, PG 29. REMOVED 1 EA CRACKED CLIP IAW SRM 51-30-15, PG 29, LOCATED AND DRILLED NEW STR CLIP AT STA 1068 AND 28R IAW SRM 51-30-5, PG 12 INSTALLED 2 EA SPLICE REPAIRS AND 1 EA STRINGER CLIP IAW SRM 51-30-5, PG 12.

Part: LONGERON — DAMAGED (BS 522-541 L24R) · airframe 68,643 hrs · 62,328 cycles

RT STATIC PORT PLATE UPPER LONGERON HAS HOLES DRILLED IN UPPER CAP TRIMMED OUT DAMAGE AT LONGERON 24R, BETWEEN STA 522 TO 541 IAW AMM DC9-A-53-10-04-801-663-A-A, PERFORMED HFEC SURFACE INSP AT TRIMMED OUT AREA. NO CRACKS NOTED IAW NDT SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR ANGLE AT LONGERON 24R, BETWEEN STA 522 TO 541, IAW AMM DC9-A-53-10-04-801-663A-A INSTALLED ID TAG IAW PSM 900-5-1, COMPLETED AND INSPECTED.

Part: DOUBLER — CRACKED (NR 2 PYLON) · airframe 68,643 hrs · 62,328 cycles

CRACK ON REPAIR DOUBLER AT PYLON 2 AFT APRON SECTION WEB IN FRONT OF AFT MOUNT FITTING INSIDE ACCESS 8206A. REMOVED REPAIR DOUBLER IAW DC-9 SRM 51-30-5 PARA 8. HFEC INSPECTION PREV STOP DRILL NO PROGRESSION NOTED. FABBED REPAIR IAW SRM 54-01 FIG 2 SHEET 2 DC-9 SRM 54-10-0FIG 1 AND DC-9 SRM 51-10-2 PG: 1-3. HFEC SURFACE INSP AND NO CRACKS NOTED PRIMED NEW REPAIR DOUBLER IAW DC-9 SRM 51-10-3 AND INST IAW SRM 54-01 FIG 2 SHEET 2 AND DC-9 SRM 51-30-05.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 68,643 hrs · 62,328 cycles

CRACK ON SUPPORT ANGLE AT PYLON 2 WEB BEHIND PNEUMATIC DUCTS /FIRE SHIELD ACCESS THRU DOOR 8206A. DRILLED .025 STOP HOLE AT END OF THE CRACK IAW DC-9 SRM 54-01 FIG 2 SHT 3 HFEC INSPECTION STOP DRILL AND NO PROG NOTED FABBED NEW REPAIR ANGLES 2 EA. HFEC SURFACE OF 2 ANGLES PER NDT SPM 06-10-01.001 NO CRACKS DETECTED. TREATED AND PRIMED 2 REPAIR DOUBLER ANGLES IAW DC-9 SRM 51-10-3 PARA 14, 21 INST IAW DC-9 SRM 54-01 FIG 2 SHT 3.

Part: LONGERON — CRACKED (BS 351 L17R) · airframe 68,643 hrs · 62,328 cycles

CRACKED AT FRAME STA 351 ATTACH POINT. REMOVED LONGERON NR 17R STA 323-437 IAW SRM 51-30-2 P 24 PAR A 7 FIG 19-20 LOCATED AND DRILLED NEW LONGERON PART NR S2777922-3-25000, BATCH 0002001515 PER SRM 51-10-4 PG 1 FIG 4. INSTALLED NEW LONGERON 17R FROM STA 323 TO 437 PER SRM 51-10-4 PAGE 1-4 AND SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 160-217) · airframe 68,643 hrs · 62,328 cycles

CORROSION ON FLOOR SUPPORT FOR PANELS 17 AND 18 ON TOP AND BOTTOM. BLENDED OUT DAMAGE AREA ON UPPER FLANGE ON FLOOR SUPPORT AT STA 160 TO 217 FOUND TO BE OUT OF LIMITS IAW SRM 53-01 PAGE 3 FIG 1 SHEET 3. REMOVED FLOOR SUPPORT STA 160 TO 217 BL 0 IAW SRM 51-30-5 PAGE 29, IAW SRM 53-13-1 PAGE 25, 26 AND 72. TREATED AND PRIMED SUPPORT IAW SRM 51-10-3 PAGE 1, 2 PARA 21, 14. INSTALLED FLOOR SUPPORT IAW SRM 51-30-5 PAGE 1, 3.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 68,643 hrs · 62,328 cycles

FLOORBEAM JUST LEFT OF AC CENTER BEAM AT STA 200 HAS CORROSION. REMOVED CORROSION ON UPPER FLANGE ON FLOOR PANEL BEAM AT STA 200 FROM X1 TO X 20, DAMAGE FOUND OUT OF LIMITS IAW DC-9 SRM 53-01 PARA 3 SHEET 3 FIG 1. REMOVED AND REPLACED FLOOR PANEL BEAM SUPPORT AT STA 200, FROM X1 TO X20IAW SRM 51-30-5 PAGE 1-3 FIG 2.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 68,643 hrs · 62,328 cycles

PAX CABIN FLOOR PANEL NR 68, LOWER STRUCTURE CHANNEL WITH CRACKS. REMOVED DAMAGE PAX CABIN FLOOR PANEL NR 68 LOWER STRUCTURE AND INSTALLED FLOOR SUPPORT LOWER STRUCTURE, BATCH NR 0001870883 IAW SRM 51-30-2 PARA 8 PG 26B.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOORBOARD PANEL NR 68 HAS BOTTOM GUIDE SUPPORTS WITH SEVERAL CRACKS. REMOVED 7 EA DAMAGED AREA, AND PREPARED DAMAGE AREA ON FLOORBOARD IAW MM 53-22-01-801-663A-A AND IAW SRM 51-90 -0, PARA 5E. APPLIED REPAIR PLIES AND HOT BONDED ON FLOOR BOARD DATE DUE 08/27/11, ID NR 10-574, IAW MM 53-22-01-801-663A-A, AND IAW SRM 51-90-0, PARA 6.0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,643 hrs · 48,148 cycles

LT SIDE VERTICAL STABILIZER STA ZFS43 HAS A CRACK FROM FASTENER HOLE. AT FIFTH OPEN HOLE 3 INCHES LONG FROM THE BOTTOM OF THE RIB (LT) THAT EXTENDS ON OTBD FLANGE FWD AND TERMINATES AT OPEN HOLE OF RIB SUPPORT, STA ZFS43 IAW SPM 06-10-01.001. FABBED REPAIR PARTS IAW SRM 55-02, FIG 27, VIEW B, SECTION F-F, PG 104, 111 AND 106. TREATED AND PRIMED IAW SRM 51-10-3, PARA 13E AND 14, PG 31. INSTALLED AT LT SIDE VERTICAL STAB IAW SRM 51-30-2, PG 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 15 HAS CORROSION ON TOP AND BOTTOM OF PANEL. OUT OF LIMITS IAW NWA DC9 SRM 53-01, FIG 1 CRACK ON FWD END OF NR 2, BLENDED OUT SURFACE CORR ON HAT CHANNELS 1, 3, 4, 5, AND BLENDED OUT 1/8 INCH CRACK ON NR 2 HAT CHANNEL IAW NWA DC9 SRM 53-01. FABBED FLOOR PNL SKIN IAW NWA DC9 SRM 53-23- INST IAW SRM 51-30-2, PG 1-5. ORIG MAT FLOOR PANEL SKIN IS .040, MAT REMOVED IS .020, ORIG MAT HAT CHANNELS IS .025, MAT REM IS .001.

Part: SKIN — DENTED (BS 268) · airframe 1,820 hrs · 1,567 cycles

LT EXTERIOR FUSELAGE IS DENTED AT BS 268 AND ABOVE LONGERON 23L. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-04, CUT OUT DAMAGE IAW SRM 53-04, FIG 38. FOUND CRACK AROUND CUTOUT AND EXISTING FASTENER HOLES IAW NDT SPM O6-10-01. 001 AND NDT SPM 06-10-01.003, FABRICATED, TREATED, PRIMED AND INSTALLED DOUBLER IAW SRM 53-04, FIG 38, VIEW 14, AT STA 268, ABOVE LONGERON 23L.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 63 HAS CRACKS ON THE EDGE OF FLOOR PANEL. REMOVED 2 EA CRACKS IN FLOOR IAW SRM 53-01. FABRICATED 2 EA REPAIR DOUBLERS IAW SRM 53-23-0. TREATED & PRIMED IAW SRM 51-10-3, PG 3. INSTALLED REPAIR DOUBLER IAW SRM 5 3-01. DETECTED NO CRACKS AT 2 EA CUTOUT REPAIR AREAS.

Part: SKIN — DENTED (RT WING TE FLAPS) · airframe 68,643 hrs · 62,328 cycles

RT WING FWD MOVEABLE FLAP VANE UPPER SURFACE HAS A DENT AT XF STA 85.5 REPAIRED IAW SRM 51-70-02. PREPARED CORE, PLUGS AND DOUBLERS IAW SRM 51-70-02, PARA 10D, PG 43, CURED IAW SRM 51-70-02. SEALED IAW SRM 51-70-02. INSTALLED FASTENERS IAW SRM 51-70-02.

Part: DOUBLER — CRACKED (NR 1 PYLON) · airframe 68,643 hrs · 62,328 cycles

NR 1 PYLON APRON LOWER AFT AREA FWD OF AFT ENGINE MOUNT, INTERNAL DOUBLER CRACKED AT LWR RADIUS 60-11. REMOVED DOUBLER IAW SRM 51-30-2, PG 24, PARA 1. FABRICATED DOUBLER IAW SRM 54-01, PG 10, FIG 2. TREATED AND PRIMED DOUBLER IAW DC9 SRM 51-10-3, PG 40, PARA 21 AND SRM 51-10-3, PG 31, PAR 14. INSTALLED DOUBLER IAW SRM 51-30-2, PG 24, PARA 7.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

LONGERON 16L CRACKED AT FRAME STA 389 ATTACH POINT RL072. REMOVED, FABRICATED, AND REPLACED LONGERON 16 LT FROM STA 379 TO 435 PER SRM 53-02, FIG 18. FABRICATED REPAIR SPLICE NDT INSPECTED, NO DAMAGE NOTED AND INSTALLED REPAIR PARTS PER SRM 53-02, PAR 12, FIG 18, PG 49 TO 52.

Part: INTERCOSTAL — CRACKED (BS 674) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOOR INTERCOSTAL WEB CRACKED AND UPPER TEE CHORD CRACKED AT STA 674, BL-0 RBL 082. REMOVED CRACKED TEE CHORD FROM STA 570 TO 674, BL-0 AT MAIN CABIN FLOOR IAW SRM 51-30-02, PG 29. INTERCOSTAL EVALUATED BY NDT-NO CRACKS FOUND. FABRICATED TEE CHORD AND REPAIR ANGLES IAW SRM 51-70-5, PG 16-26. INSTALLED CHORD AND REPAIR ANGLES IAW SRM 51-30-02 PGS 1-5, AMD FIG 3, PG 16, SRM 51-70-5.

Part: LONGERON — CRACKED (BS 237 L17R) · airframe 68,643 hrs · 62,328 cycles

LONGERON 17R CRACKED AT FRAME STA 237 ATTACH POINT. REMOVED FASTENERS AT STA 229 BETWEEN LONGERONS 15R TO 18R IAW SRM 51-30-. REMOVED LONGERON 17R FROM STA 230 TO 320 IAW SRM 51-30-2, PAGE 24, PAR 7, DRILLED NEW LONGERON IAW SRM 51-10-4, PARA 2, PAGES 1 AND 2; INST LONGERON 17R FROM STA 230 TO 320 IAW SRM 51-30-2, PAGES 1, 2, AND 3, FIG 1, 2 AND SRM 51-30-5, PARA 7, PAGE 12. INSTALLED FASTENERS AT STA 229 BETWEEN LONGERONS 15R TO 18R IAW SRM 51-30-2, PAGES 1 ,2 AND 3, FIG 1 AND 2.

Part: FLOOR PANEL — DAMAGED · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 62 HAS 5 HOLES THAT ARE OVERSIZED. 5 EA SCREW HOLES WORN BEYOND LIMITS IAW NWA SRM 53-01. FABRICATED REPAIR DOUBLER TREATED AND PRIMED IAW NWA ARM 51-10-3. INSTALLED REPAIR DOUBLER IAW NWA SRM 53-01, ON FLOOR PANEL 62.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR BOARD SUPPORT HAS CORROSION, AT STA 200 FROM CENTERLINE TO 20 INCHES RIGHT. REMOVED CORROSION IAW DC9 SRM 51-10-3, PARA 26, FOUND OUT OF LIMITS IAW DC9 SRM 53-01, FIG 1, SHT 3. FABRICATED, LOCATED, DRILLED AND INSTALLED FLOOR BOARD SUPPORT AT STA 200, BL0 TO RBL 20 IAW DC9 SRM 53-13-1, FIG 11, ITEM 11, SRM 51-40-04, PARA C, AND SRM 51-30-5, PARA7.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL 79 HAS CORROSION ON NUMEROUS SCREW HOLES. BLENDED OUT NUMEROUS SCREW HOLES OF CORROSION, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01. FABBED FLOOR PNL SKIN, IAW DC9 SRM 51-10-4. INST HAT CHANNELS TO FLOOR PNL 79 SKIN IAW DC9 SRM 51-30-02, REMOVED HAT CHANNELS FROM FLOOR PNL IAW DC9 SRM 51-30-2, PG 24.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 79 HAS CORROSION ON NUMEROUS SCREW HOLES. BLENDED OUT NUMEROUS SCREW HOLES OF CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABRICATED FLOOR PANEL 79 SKIN IAW SRM.

Part: SKIN — PUNCTURED (FLAP VANE) · airframe 68,643 hrs · 62,328 cycles

RIGHT WING AFT MOVABLE FLAP VANE UPPER SURFACE HAS A PUNCTURE AT WING STA XF104. REMOVED DAMAGED SKIN AND CORE, FABRICATED NEW FILLER AND CORE, TREATED AND PRIMED FILLER, BONDED NEW CORE, FABRICATED REPAIR DOUBLER, TREATED AND PRIMED ALL SURFACES FOR BONDING, BONDED REPAIR DOUBLER AND ATTACHED MECHANICAL FASTENERS PER B DC-9 SRM 51-70-02. TREATED REPAIR AREA PER BDC-9 SRM 51-20-01. APPLIED FILLET SEAL AROUND REPAIR AREA PER B DC-9 SRM 51-10-3B.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL NR 78 HAS 2 SCREW HOLES WITH CRACKS EXTENDING TO EDGE OF PANEL. TRIMMED OUT DAMAGED AREA IAW DC-9 SRM 53-00-01, PG 25, FIG 4, STEP 1 FABRICATED REPAIR PARTS, TREATED AND PRIMED IAW DC-9 SRM 53-23-0, PG 8, FIG 5, ANS SRM 51-10-03, PG 5. INSTALLED REPAIR PARTS IAW DC-9 SRM 53-01-00, PG 25, FIG 4.

Part: FLOORBOARD — CORRODED (MAIN CABIN) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOORBOARD NR 26 HAS CORROSION ON TOP SURFACE. UPON FURTHER INSP, FOUND MATERIAL LOSS AROUND CUPHOLDER FROM CORROSION, WEB IS OUT OF LIMITS REF SRM 53-01. REMOVED INSERT IN CUP HOLDER HOLE, AS WELL AS HAT CHANNELS FILLER, REF SRM 31-30-2, PG 1-13. FABBED NEW WEB REF SRM 53-23-0, PG 7, FIG 4. INST ON NEW WEB, HAT CHANNELS, FILLERS & CUP HOLDER HOLE INSERT REF DC9 51-30-2, PG 1.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 68,643 hrs · 62,328 cycles

FLOOR BOARD NR 66 HAS A CORNER BROKEN. REMOVED DAMAGE IAW SRM 53-01, PG 2, FIG 4, NDT FOR CRACKS, FABRICATED DOUBLER REPAIR IAW SRM 41-30-2, PG 1 AND 2, SRM 53-01, PG 25, FIG 4, SHEET 4. FAB FILLER REPAIR 7075-T6 IAW SRM 53-01, PAGE 25, .025, TREATED AND PRIMED IAW SRM 51-10-3, PG 31, AND INSTALLED REPAIR IAW SRM 51-30-2, PAGE 1 AND 2, AND SRM 53-01, PAGE 25, FIG 4, SHEET 4.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 68,643 hrs · 62,328 cycles

REPAIR LOCATED AT THE EDGE OF THE FLOORBOARD NR 75 IS DISBONDED AND HAS A CRACK IN THE BACKSIDE. REMOVED DAMAGED AREA AND TRIM OUT, HFEC SURFACE INSP PER NDT SPM 06-10-01.001, NO CRACK ON CUT OUT AREA. FAB DOUBLER, .032, AND REPAIR FILLER .025, APPLIED ALODINE AND PRIMER IAW SRM 51-30-3, PG 31. INSTALLED DOUBLER, FILLER REPAIR IAW SRM 51-30-2, PAGE 2, AND SRM 51-30-8, PAGE 1, AND SRM 53-01.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL 65 HAS A CORNER BROKEN. FABRICATED REPAIR DOUBLER FOR FLOOR PANEL 65 IAW SRM 53-01, PG 25. TREATED & PRIMED IAW SRM 51-10-3, PG 31, FASTENER INSTALLATION IAW SRM 51-30-2.

Part: FLOOR PANEL — CRACKED · airframe 68,643 hrs · 62,328 cycles

FLOOR BOARD PANEL NR 74 HAS A HOLE CRACKED AND ANOTHER CRACK BESIDE. REMOVED DAMAGE ON FLOOR PANEL IAW SRM 53-01, PG 25, FIG 4. FABRICATED DOUBLER 7075-T6 .032, FABRICATED FILLER REPAIR, 7075-T6 .025, IAW SRM 53-01, PG 25, FIG 4, STEP 2, AND SRM 53-23-0, PG 7, FIG 4. PRIMED AND TREATED IAW SRM 51-10-3, PG 3. INSTALLED REPAIR IAW 51-30-2, PGS 1 AND 2, AND SRM 53-01, FIG 4, SHEET 4.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR PANEL 60A UNDERSIDE SUPPORTS ARE CRACKED AT EDGES. REMOVED UNDERSIDE SUPPORTS CRACKED ON FLOOR PANEL 60A IAW DC9 SRM 51-30-2, PG 28. HAT CHANNELS FOUND TO BE OUT OF LIMITS. OK TO FABRICATE IAW NWA DC9 SRM 53-05, PG 9. HAT CHANNELS IAW NWA DC9 SRM 51-10-1. FABRICATED TREATED, PRIMED, IAW NWA DC9 SRM 51-10-3. INSTALLED HAT CHANNELS ON FLOOR PANEL WITH RIVETS IAW DC9 SRM 51-30-2, PG 28.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOOR PANEL NR 25 HAS CORROSION ON TOP SURFACE. REMOVED CORROSION IAW AMM 51-21-03-701-929A -A, PG 2-11, FOUND TO BE OUT OF LIMITS IAW SRM 53-01-00, PG 8, FIG 1 SHEET 3. REMOVED FLOOR PANEL IAW SRM 51-30-02, PG27, FIG 19. FABRICATED FLOOR PANEL, TREATED AND PRIMED IAW DWG NR 9957882, AND SRM 51-10-03, PG 5, PAR 3, TABLE 1. INSTALLED FLOOR PANEL REF SRM 51-30-02, PG 1-10.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FWD CARGO DOOR SILL, CORRODED FRAME STA 408, BETWEEN WEB AND FRAME. REMOVED FASTENERS FROM FRAME IAW DC-9 SRM 51-30-05. BLENDED CORROSION IAW SRM 51-10-3, PG 46, PARA 26. FRAME FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01, FIG 1, SHT 3. REMOVED DAMAGED SECTION IAW DC9 SRM 53-03, FIG 5, PG 6. FABRICATED REPAIR PARTS, TRAVELER 87145470001, & INSTALLED REPAIR IAW DC9 SRM 53-03, FIG 5, PG 6.

Part: SKIN — DEBONDED (ELEVATOR TAB) · airframe 68,643 hrs · 62,328 cycles

RT ELEVATOR T/E WEDGE O/B OF ELEVATOR GEAR TAB SKIN IS DISBONDED FROM FILLER. FABBED SPACE FILLER IAW DW PL5918046 55-20-1, PG 1-7. CUT OUT DAMAGED AREA IAW DC9 SRM 55-03, PG 19, TREATED AND PRIMED IAW DC9 SRM 51-10-3, PG 31. INST NEW WEDGE AND FABBED "Z" IAW DC9 SRM 55-03, PG 19.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

FLOOR SUPPORT FOR MAIN CABIN WORN AT FLOOR PANEL CONTACT POINT RT SIDE AT STA 408 & 427. REMOVED FLOOR SUPPORT MAIN CABIN RT STA 389 TO 465 IAW DC9-A-53 -20-01-201-925A-A. REMOVED DAMAGE STA 408 & 427 IAW DC9 SRM 53-05, FIG 20A OUT LIMITS - FABRICATED (2EA) ANGLE REPAIR, (2EA) WEAR STRIP & (1EA) SHIM, IAW DC9 SRM 53-05, PG 100, FIG 20A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AND CORRODED BL 0. REMOVED INTERCOSTAL AT MAIN CABIN STA 235 TO 294 BL 0 IAW SRM 51-30, PG 1. TRIMMED OUT CRACKED AND CORRODED AREA AT FWD END INTERCOSTAL WEB IAW SRM 53-01, FIG 4. FABBED DOUBLER AND FILLER IAW SRM 53-01, FIG 4. LOCATED & DRILLED DOUBLER, FILLER REPAIR IAW SRM 51-10-4, PAGE 1. INSTALLED DOUBLER & FILLER TO INTERCOSTAL IAW SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 275-294 BL 0) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AND CORRODED, STA 275-294, BL0. REMOVED INTERCOSTAL AT MAIN CABIN STA 235 TO 294, BL 0 IAW SRM 51-30, PG1, TRIMMED OUT CRACKED AND CORRODED AREA AT FWD END OF MAIN CABIN INTERCOSTAL WEB, IAW SRM 53-01, FIG 4, SHT 4, PG 25, FABRICATED DOUBLER AND FILLER, REPAIRED IAW SRM 53-01, FIG 4.

Part: INTERCOSTAL — CORRODED (BS 275-294 BL0) · airframe 68,643 hrs · 62,328 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AND CORRODED STA 275-294, BL 0. REMOVED INTERCOSTAL AT MAIN CABIN STA 235 TO 294, BL0, TO FOM IAW SRM 51-30, PG 1. TRIMMED OUT CRACKED AND CORRODED AREA AT FWD END MAIN CABIN INTERCOSTAL WEB IAW SRM 53-01, FIG 4, SHT4, PAGE 25. FABRICATED DOUBLER AND FILLER REPAIR IAW SRM 53-01, FIG 4.

Part: SKIN — GOUGED (FUSELAGE) · airframe 68,643 hrs · 62,328 cycles

RIGHT FWD GALLEY DOOR HOLD OPEN LATCH HOOK REPAIR CUTOUT IS GOUGED ON FUSELAGE EXTERNAL SKIN. REMOVED AND REPLACED RIGHT FWD GALLEY DOOR HOLD OPEN LATCH HOOK DOUBLER IAW DC9 SRM 51-30-2, PG 1 TO 10, AND SRM 53-04, FIG 24.

Part: LIGHT — MISSING (SEAT 6D) · airframe 67,804 hrs · 61,605 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 6D MISSING. MX INSTALLED NEW LIGHT ASSY AT 6D IAW CMM 25-28-62. OPS CHECK OF LIGHT IS NOW GOOD.

Part: SKIN — CRACKED (BS 1303 L14-15R) · airframe 67,748 hrs · 61,554 cycles

DURING LINE INSP, FOUND CRACK IN FUSELAGE SKIN AT BS 1303.604 BETWEEN LONGERON 14R AND LONGERON 15R. REPAIRED IAW SRM 53-01-12 & TRM DC9-A-53-30-01-801-663A.

Part: SKIN — CRACKED (BS 1303 L15R) · airframe 67,748 hrs · 61,554 cycles

DURING LINE INSP, FOUND CRACK IN FUSELAGE SKIN AT BS 1303.604 BELOW LONGERON 15R. REPAIRED IAW SRM 53-01-12 & TRM DC9-A-53-30-01-801-663A.

Part: LINE — FAILED (HYD SYSTEM) · airframe 60,648 hrs · 55,306 cycles

WHILE ON FINAL APPROACH AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED THE AIRCRAFT LOSS ALL OF THE FLUID AND PRESSURE IN THE RT HYDRAULIC SYSTEM. THE CREW CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. TAXI OR TOWED TO GATE WAS NOT SPECIFIED. MAINTENANCE FOUND A FAILED RIGID HYDRAULIC LINE IN THE RT WHEEL WELL AND REPLACED IT WITH A TEMPORARY FLEX LINE. THE SYSTEM WAS RE-SERVICED AND LEAK CHECKED BEFORE THE AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 58,435 hrs · 53,309 cycles

AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMELL IN AFT AIRCRAFT CABIN. FLIGHT CREW RETURNED AC TO DEPARTURE AIRPORT. MAINTENANCE PLACED APU ON MEL AND REPLACED THE WATER SEPARATORS.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 57,439 hrs · 52,392 cycles

DURING H-CHECK FOUND CRACK IN BULKHEAD HAT CHANNEL AT BS 855. REPAIRED PER EA 98-202509.

Part: SWITCH — FAILED (ELEVATOR) · airframe 57,043 hrs · 52,032 cycles

THE CREW REPORTED, THE AIRCRAFT FEELING VERY HEAVY ON THE CONTROLS THAT IT TOOK EXCESSIVE BACK PRESSURE TO CONTINUE TO CLIMB AFTER TAKEOFF. THE 'ELEVATOR POWER ON' LIGHT ILLUMINATED AT THE SAME TIME AND REMAINED ILLUMINATED UNTIL 10,000 FT. COMPLIED WITH COM PROCEDURES AND THE CREW RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT ATL. MAINTENANCE FOUND THE ELEVATOR POWER SWITCH BAD AND REPLACED IT. ALSO, CHECKED THE ELEVATOR, TAB, BOOST ACTUATOR SYSTEM, FOLLOW-UP MECHANISM, AND THE LOAD FEEL SPRING. ALL COMPONENTS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (TAIL CONE)

DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — FAILED (TAIL CONE)

DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ALONG CATWALK IN TAILCONE SECTION INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.

Part: BATTERIES — DISCHARGED (TAIL COMPARTMENT)

DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 9 THRU 13. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY, OPERATIONAL CHECK NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECITON, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS IN VENTRAL STAIR AREA INOPERATIVE. MAINTENANCE REPLACED 3 BATTERY PACKS, OPERATIONAL CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND CATWALK AND EXIT HANDLE EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: FUSE — BLOWN (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS AND AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BLOWN FUSE, OPERATIONAL CHECK NORMAL.

Part: WIRE — PINCHED (CABIN)

DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHTS LOCATED IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED PINCHED WIRE IN ROW 3 FOOT REST, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS LOCATED IN THE FIRST CLASS SECTION WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK OK.

Part: STRUT — LOW PRESSURE (NLG)

NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION ACCOMPANIED BY TAKEOFF WARNING HORN AND LOSS OF PRESSURIZATION. CREW RECYCLED GEAR AND GEAR INDICATION AND SYSTEM FUNCTIONS RETURNED TO NORMAL. FLIGHT WAS CONTINUED TO DESTINATION AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NOSE GEAR STRUT SCHRADER VALVE AND SERVICED STRUT TO PROPER LEVEL. OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EXIT EMERGENCY LIGHT AND FLOOR PROXIMITY LIGHTS BETWEEN ROWS 19 THRU 22 INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS AT SEAT ROWS 9 THRU 13 FLICKERED ON AND OFF IN FLIGHT. MAINTENANCE CHECKED ASSOCIATED WIRING AND REPLACED THE POWER SUPPLY, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING FLIGHT AND WHILE ON THE GROUND, EMERGENCY EXIT LIGHTS AT SEAT ROWS 9 THRU 13 FLICKERED ON AND OFF AND REMAINED ILLUMINATED CONTINUOUSLY WHEN FLIGHT IS SMOOTH. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND FORWARD LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND THAT THE CATWALK EMERGENCY LIGHTS WOULD NOT EXTINGUISH WITH THE COCKPIT EMERGENCY LIGHT SWITCH. REPLACED TAILCONE COMPARTMENT EMERGENCY PATHWAY LIGHTING POWER SUPPLY. OPERATIONAL CHECK OK.

Part: BATTERIES — DISCHARGED (TAIL CONE)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS ON TAIL CONE CATWALK AND OVER TAIL CONE RELEASE HANDLE INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.

Part: ENGINE — FAILED (RIGHT)

DURING CRUISE, THE RIGHT ENGINE OIL QUANTITY AND OIL PRESSURE INDICATIONS DROPPED TO NEAR ZERO READING. CREW SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO BUF. MAINTENANCE REPLACED THE RIGHT ENGINE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND AFT ENTRANCE STAIR EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY AND POWER PACK, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAIL INTERIOR INOPERATIVE. REPLACED BATTERIES AND LIGHT ASSEMBLY, OPERATIONAL CHECK OK.

Part: TEMP CONTL BOX — FAILED (LEFT)

LEFT ICE PROTECTION TEMPERATURE LOW LIGHT ILLUMINATED WITH MAX CLIMB THRUST SET. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. WITH LEFT SYSTEM OFF AND RIGHT SYSTEM ON AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED. WHEN TAIL WAS SELECTED, ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. MAINTENANCE REPLACED TEMPERATURE CONTROL BOX ON LEFT SIDE AND ANTICIPATOR AND THERMOSTAT ON RIGHT SIDE. PERFORMED OPERATIONAL CHECK, CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND AFT SECTION AISLE EMERGENCY LIGHTS INOPERATIVE AT ROWS 19-25. REPLACED BATTERY POWER SUPPLY IN ACCORDANCE WITH MM 33-53-0. OPERATIONAL CHECK OK.

Part: BUSHING — WORN (NLG)

ON TAKEOFF, GROUND SHAFT FAILED TO GO TO FLIGHT MODE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR TORQUE ARM BLOCK CLAMP-UP BUSHING WORN. REPLACED BUSHING, OPERATIONAL OF GEAR CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (NACELLE)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT NACELLE SCAN POSITIONS REMAINED ON. REPLACED NACELLE LIGHT POWER SUPPLY, CHECKED AFT ENTRY POWER SUPPLY AND ALL LIGHTS OPERATIONALLY CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND FOUR CEILING LIGHTS AND BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY B5-33, B5-25 AND B5-26, OPERATIONAL CHECK OK.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS AT ROWS 20 - 25 AND 7 - 11 FAILED TO TEST. REPLACED BATTERIES IN POWER SUPPLIES AT ROWS 8 AND B2 - 58. OPERATIONAL CHECK OK.

Part: FITTING — CRACKED (LT SPOILER)

DURING B-CHECK, FOUND A .5 INCH CRACK IN THE LEFT OUTBOARD SPOILER INBOARD HINGE FITTING. REPLACED FITTING.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND FORWARD CABIN EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND THE CABIN EMERGENCY LIGHTS FROM STA 750 TO 1020 INOPERATIVE. REPLACED THE POWER SUPPLY B5-26. REPLACED THE BATTERIES IN THE POWER SUPPLY B5-58, ALL LIGHTS OPERATIONALLY CHECKED GOOD.

Part: RELEASE MECH — OUT OF ADJUST (TAILCONE)

DURING EO 5350-01032 TAILCONE FUNCTION RECHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND THAT INADEQUATE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE EXTERIOR HANDLE. ADJUSTED CLIPS AND LATCHES. CHECKED OK.

Part: RELEASE MECH — MALFUNCTIONED (TAIL CONE)

DURING EO 5350-01032 TAIL CONE FUNCTION CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HANDLE FROM THE CLIPS. ALSO, FOUND THAT THE TAIL CONE DID NOT DROP FROM THE AIRCRAFT, BUT HUNG UP ON THE UPPER LOCKPINS. RERIGGED THE TAIL CONE PER MM 53-50-3, PAR 4 AND CITEXT 09-5350-1-0024, CHECKED OK.

Part: FLOORBEAM — CORRODED (FS 1136)

DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOORBEAM CAP 3 INCHES INBOARD OF THE RIGHT INBOARD SEAT TRACK. REPAIRED TRACK (P/N 9912243-55), PER EA 98-102610.

Part: FITTING — CRACKED (FS 1167)

DURING H-CHECK, FOUND A CRACK IN THE FS 1167 FLOORBEAM END FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-30-5.

Part: DOOR PAN — CRACKED (EMERGENCY EXIT)

DURING H-CHECK, FOUND A CRACK IN BOTH THE RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR PANS, BENEATH NR 14 SUPPORT. REPAIRED PANS (P/N 5913195-1), PER EA 98-101997 AND 98-101998.