N766NC

Part: SUPPORT FITTING — DAMAGED (LEFT) · airframe 81,598 hrs · 80,891 cycles

LT MAIN GEAR SUPPORT FITTING BORE AND FACE DAMAGED. REPAIRED IAW ER/A 509731-14AD, REV ORIG.

Part: ATTACH FITTING — DAMAGED (LT MLG) · airframe 81,622 hrs · 80,918 cycles

LEFT MLG RETRACT ACTUATOR ATTACH FITTING, BORE AND FACE DAMAGED. MACHINED BORE AND FACE TO REMOVE DAMAGE. BORE WITHIN LIMITS BUT FACE IS NOT IAW AA CARD 5740-01114-01A. BORE IS WITHIN LIMITS FOR A .025 O/S BUSHING. REMOVED .017 FROM INBD FACE TO REMOVE CORROSION.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 81,154 hrs · 80,400 cycles

LT ELEVATOR UPPER OTBD SKIN HAS A LIGHTNING STRIKE. REMOVED DAMAGE (CUT-OUT) ON LT ELEVATOR UPPER OTBD SKIN, FABRICATED REPAIR DOUBLER FROM CLAD 2024-T3 AND REWORKED TO 0.036. PERFORMED HFEC INSPECTION AND NOTED NO CRACKS AT CUT OUT. LOCATED AND DRILLED REPAIR, TREATED AND PRIMED DOUBLER AND FILLER. MAINTENANCE THEN INSTALLED DOUBLER AND FILLER ON OUTBOARD SKIN OF UPPER ELEVATOR. AIRCRAFT NOW OKAY FOR SERVICE AFTER ELEVATOR BALANCE.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 81,154 hrs · 80,400 cycles

FWD CARGO DOOR HAS OUTER EDGE DAMAGE, WEAR, GOUGES, AND BENDS. DAMAGE ON FWD LWR CARGO DOOR OUTER SKIN FOUND TO BE OUT OF LIMITS IAW MD-88 SRM 52-01 PG 6. PERFORMED PRI 505976-14 REV O, ACCOMPLISHED ER/A 505976-14 REV ORIGINAL AT FWD CARGO DOOR OUTER SKIN ON THE FWD END LOWER SIDE OF P/N 5910141-129 SKIN.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 81,154 hrs · 80,400 cycles

FWD CARGO COMPARTMENT DOOR CUT OUT LOWER FRAME HAS SURFACE CORROSION. REPAIRED FWD CARGO COMPARTMENT DOOR CUT OUT LOWER FRAME.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 81,154 hrs · 80,400 cycles

DURING EDDY CURRENT INSPECTION FWD SERVICE DOOR JAMB FORWARD UPPER CORNER SECT 01B, CRACK INDICATIONS (1 ON SKIN, 2 SUB-SURFACE) WERE DETECTED EMANATING FROM FASTENERS AS MARKED, ALL CRACKS APPROX 1/8 INCH IN LENGTH. REPAIRED FWD SERVICE DOOR JAMB FWD UPPER CORNER.

Part: SPAR — CRACKED (RT WING) · airframe 81,154 hrs · 80,400 cycles

RIGHT WING REAR SPAR XRS 137, WEB HAS CRACK AT TOP OF LIGHTENING HOLE. REMOVED RT FLAP FORWARD MOVABLE VANE FOR ACCESS, REMOVED DAMAGED WEB ASSEMBLY AT RT WING REAR SPAR. REMOVED ALL SUPPORT ATTACH ANGLES TO RT WING REAR SPAR WEB. FABRICATED RIB LT WING REAR SPAR, LOCATED AND DRILLED WEB ASSY. INSTALLED WEB ASSEMBLY AND ALL SUPPORT ATTACH ANGLES AT RT WING REAR SPAR AND INSTALLED RT FLAP FORWARD MOVABLE VANE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,842 hrs · 80,018 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE LIGHTS IN THE TAIL COMPARTMENT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT FIXTURES AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 3,737 hrs · 3,441 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 AND 23-26 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: COALESCER BAG — DIRTY (FWD GALLEY) · airframe 78,799 hrs · 77,915 cycles

ENROUTE, FLIGHT DIVERTED, DUE TO A PERSISTENT HOT PLASTIC BURNING ODOR IN THE FORWARD GALLEY BETWEEN MAIN DOOR AND FORWARD LAVATORY. THERE WAS NO VISUAL CONFIRMATION OF SMOKE. MAINTENANCE FOUND THE COALESCER BAGS SATURATED AND DIRTY, REMOVED AND REPLACED THEM. LEAK AND OPS CHECK WAS GOOD. NO FURTHER BURNING ODOR WAS NOTED. AIRCRAFT OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 78,525 hrs · 77,674 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING BY THE GALLEY CLOSET AREA WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR BEHIND THE POWER SUPPLY UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: OUTFLOW VALVE — UNRESPONSIVE (CABIN PRESSURE) · airframe 78,522 hrs · 77,672 cycles

FLIGHT DIVERTED TO BUF WITH A LOSS OF CABIN PRESSURIZE. AT FL330, CABIN WAS CLIMBING 2KFT/MIN AND THE OUTFLOW VALVE SEEMED UN-RESPONSIVE. CREW COMPLIED WITH QRH PROCEDURES, DONNED MASK AND COMMENCED AN EMERGENCY DESCENT. CABIN ALTITUDE REACHED 14K BUT MASKS DID NOT DEPLOY. THE OUTFLOW VALVE WAS MANUALLY RECOVERED AT FL100. BUF MAINTENANCE MELD THE CABIN AIR OUTFLOW VALVE PER 21-00-25 AND FERRIED AIRCRAFT TO DTW. THE OUTFLOW VALVE WAS REPLACED AND 2 RELAYS WERE RESEATED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

1D/111 FORWARD CARGO COMPT STA 503-522 RBL 48 INTERCOSTAL IN TUNNEL AREA IS CRACKED AND INBD WATER TANK SUPPORT BRACKET HAS 3 SHEARED FASTENERS. REMOVED INTERCOSTAL PART 5919741-6 IAW DC9 SRM 51-30-2 STOP DRILLED CRACKS IAW DC9 SRM 53-01 FIG 2 SHT.3 ACCOMPLISHED HFEC INSP OF 5 STOP DRILLS IAW NDT SPM 06-10-01.001 CRACKS CONTAINED AT STOP DRILLS FAB AND INSTALLED REPAIR DOUBLER, REPAIR TAG INTERCOSTAL IAW DC9 SRM 51-30-2, 51-30-5, AND 53-01 FIG 2 SHT.3. INSTALLED REPAIR TAG IAW PROCESS STANDARD 900-5-1, NR 4. REQUIRED INSPECTION COMPLETED.

Part: PAN — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

1D/29 FWD CARGO COMPT CARGO DOOR LOWER JAMB PAN HAS EXFOLIATED CORROSION ON SEVERAL AREAS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 AND NDT SPM 04-00-06. FABRICATED REPAIR AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-4, 53-05 FIG 44 SH 4 P245. REQUIRED INSPECTION COMPLETED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

1F/46 AFT ACCESSORY COMPARTMENT CANTED FRAME 1303 AT RT LOWER END IS CRACKED. REMOVED DAMAGED AREA 1"X1" NDTHFEC USING A2469 ZETEC PER NDT SPM FOUND CRACK FREE AREA. FABRICATED .050 REPAIR DOUBLER & .040 FILLER & INSTALLED IAWDC-9 SRM 51-10-3, 51-70-5 & ER/A 489354-14 P245 REQUIRD INSPECTION COMPLETED, ASSOCIATED ER/A 14-489354 ADDEDFOR AC 0857

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 78,354 hrs · 77,526 cycles

LT MLG W/W DOOR INTERIOR SIDE FWD ZEE CHANNEL IS CRACKED AT INBD END. REMOVED CHANNEL IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-6. LOCATED DRILLED AND INSTALLED NEW CHANNEL IAW DC9 SRM 51-10-4, 51-30-2, 51-30-5 AND 51-30-6, P-205 Q-948 490448. REQUIRED INSPECTION COMPLETED BY Q-968 280012.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO COMPT RT SIDE TIEDOWN TRACK BETWEEN FUS STA 218 AND STA 370 HAS CORROSION. REMOVED CORROSION IAW DC9 SRM53-01 FIG 1 ORIG MAT'L .100 REMOVED .027 .073 REMAINING FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. REMOVED DAMAGED TRACK IAW DC9 SRM 51-30-1. LOCATED DRILLED AND INSTALLED NEW TRACK IAW DC9 SRM 51-10-, 51-30-1. P245.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPARTMENT STA 1167 RBL 50 UPPER FLOORBEAM HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED CORRODED FLOORBEAM ANGLE FABRICATED REPAIR PARTS AND GUSSETUSING TRAVELER NR 2446 N01735 AND 2446N01744. INSTALLED REPAIR PARTS IAW DC9 SRM 53-01 FIG 2, 51-30-5, 51-30-2, P245.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE EXTERIOR STA 489 L27L FASTENER HOLE IN SKIN TORN OUT. REMOVED DAMAGE IAW BOEING DOCUMENT NR 5609530001 M1 NDT NO DAMAGE INDICATION NOTED. MAT ID FILLER .050 IAW DC9 SRM 53-30-0 FIG 2 SHT 1 AND 2 AND 51-60-0 FIG 1 SHT 1 FINGER DOUBLER .032 IAW BOEING DOC. FABRICATED LOCATED DRILLED DEBURED IAW DC9 SRM 51-10-2 AND 51-10-4 TREATED AND PRIMED DOUBLER AND FILLER IAW DC9 51-10-3. INSTALLED IAW DC9 SRM 51-30-2 AND BOEING DOC 5609530001 M1 P106 18FEB11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE EXTERIOR STA 475 L27L FASTENER HOLE IN SKIN TORN OUT. REMOVED DAMAGED IAW BOEING DOC NR 5609530001 M1 MAT ID FILLER IAW DC9 SRM 53-30-0 FIG 2 SHT 1 AND 2 AND 51-60-0 FIG1 SHT 1. FINGER DOUBLER .032 IAW BOEING DOC 560950001 M1 PO NR 1120167 FABRICATED LOCATED DRILLED DEBURED IAW DC9 SRM 51-10-2 AND 51-10-4. TREATED PRIMED IAW DC9 SRM 51-10-6. INSTALLED IAW DC9SRM 51-30-2 AND BOEING DOC 5609530001 M1 P106 18FEB11.

Part: FLOOR SUPPORT — CORRODED (BS 237 RBL 14) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 237, RBL 14 FLOOR SUPPORT CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ORIGINAL MAT .050, REMOVED .049, REMAIN .001 RECEIVED MATERIAL FABRICATED NEW PART LOCATED DRILLED DEBURRED TREATED AND PRIMED AND INSTALLED NEW PARTS IAW DC9, ARM 51-30-2 & 51-30-5 & 53-13-2 FIG 4, SHT1&2, P106.

Part: FITTING — CORRODED (CARGO BAY) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO COMPARTMENT STA 360 BETWEEN L27R AND L28R TIE DOWN TRACK FITTING HAS CORROSION. REMOVED AND REPLACED TIE DOWN CLIP HAD 100% MATERIAL LOSS IAW DC 9 SRM 53-01 FIG 1. INSTALLED IAW DC9 SRM 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

DURING CURRENT M-CHECK DENTS WERE FOUND ON FUSELAGE SKIN LOCATED BETWEEN STA 1380 TO STA 1401, AND BETWEEN S-27R AND S-29L. ER/A 489003-14 SECTION I ACCOMPLISHED DURING M-CK. SECTION II APPROVAL IS LIMITED TO 12 MONTHS (365DAYS) SERVICE ONLY. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE LONGER THAN 12 MONTHS FROM SECTION I.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL 41 HAS APPROX 10EA CRACKS. FOUND FLOOR PANEL 41 UNREPAIRABLE. FABRICATED NEW PANEL. IDENTIFIED PANEL AS PERMANENT STENCILED PANEL "NOT FOR RESALE" PER ERA 488345-14 AND DC9 SRM 51-10-3.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE EXTERIOR FORWARD AIR STAIR DOOR FRAME INTERIOR HAS CORROSION. REMOVED AND REPLACED DOOR FRAME IAW DC-9 SRM 51-30-1 AND 51-30-2. REMOVED AND INSTALLED DOOR ASSEMBLY FOR ACCESS IAW MM 52-62-00. PRESSURE LEAK CHECK TO BE ACCOMPLISHED ON OM12 S/N31386 ITEM 6 P214.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL 84 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION FOUND PANEL TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. ORG THICKNESS IS .025 IAW DWG PL9957919. REMOVED, .016.009 REMAINS. FABRICATED NEW PANEL AND HAT CHANNEL DRILLED UP PANEL AND HAT CHANNELS DEBURRED TREATED AND PRIMED IAW DC9 SRM 51-10-3 ASSEMBLED IAW ER/A 488721-14.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN FLOOR PANEL 81 HAS SEVERAL ELONGATED FASTENERS HOLES AT FWD FLANGE BS 851. REMOVED PANEL FOUND UNREPAIRABLE. FABRICATED ALODINED AND PRIMED NEW FLOOR PANEL APPLIED STENCIL & ID TAG 'P' PER ERA 488732-14 INSTALLED PANEL.

Part: FLOOR PANEL — TORN (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN FLOOR PANEL 60B HAS 1EA TEAR AND SEVERAL PULL THROUGH RIVETS BS 617. REMOVED FLOOR PANEL IAW DC9 SRM 51-30-5. PANEL FOUND TO BE BEYOND REPAIR. OBTAINED MATERIAL TO FABRICATE NEW PANEL PER ER/A 488738-14 DRILLED PANEL AND HAT CHANNELS UP IAW DC9 SRM 51-10-4. DEBURRED COUNTERSUNK TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED CHANNELS IAW DC9 SRM 51-30-2 & ER/A 488738-14.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL 101 AFT END 3EA ELONGATED HOLES. FABRICATED NEW FLOOR PANEL 101 FROM ER/A 488734-14. LOCATED DRILLED COUNTERSINK HOLES IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2 & ER/A 488734-14.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN FLOOR PANEL 60D HAS 3EA CRACKS AT RIVET HOLES AND PULLED THROUGH RIVETS BS 674. REMOVED FOUND TO BE UNREPAIRABLE FABRICATED ALODINED AND PRIMED NEW FLOOR PANEL. APPLIED STENCIL & ID TAG 'P' PER ERA 488739-14 INSTALLED PANEL 60D.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL 5 HAS CORROSION ON SKIN. REMOVED CORROSION IAW DC9 SRM 53-01 FIG 1 SHT 3 OUT OF LIMITS. FABRICATED IAW DWG 9957808 FABRICATED DRILLED DEBURRED & INSTALLED IAW DWG 9957808 & ER/A 488726-14.

Part: FRAME — CRACKED (BS 1245) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY COMPARTMENT CANTED FRAME 1245 CRACKED AT FASTENER HOLE L4L. REMOVED DAMAGED CANTED FRAME 1245 IAW SRM 51-30-2 & 51-30-5. LOCATED, DRILLED, & INSTALLED NEWFRAME IAW SRM 51-30-2, 51-30-5. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CRACKED (BS 775) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL NR 75 HAS 1EA CRACKED AT INBD FLANGE AND 1EA ELONGATED HOLE BS775, CORRECTED. FABRICATED FLOOR PANEL 75..

Part: SKIN — CRACKED (DOOR CUT OUT) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE EXTERIOR FWD PASSENGER DOOR JAMB AFT UPPER DOOR STOP SKIN HAS APPROX .250 INCH CRACK RUNNING AFT OF DOOR STOP REF SR09530252-7001 DWG FOR REPAIR. REMOVED DAMAGE 2EA CUTOUTS 3.75" X 1.75" AND 2.1" X 3.75 AND INSTALLED DOUBLER & TRIPLER REPAIR IAW SRM53-05. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 60A HAS 4 EA HAT CHANNELS CRACKED. FABRICATED FLOOR PANEL 60A IAW ER/A 488737-14 REV ORG P214, CORRECTED.

Part: DOUBLER — CORRODED (BS 674-697) · airframe 78,354 hrs · 77,526 cycles

FWD CARGO COMPARTMENT, STA 674-697, L28L-L28R INTERNAL DOUBLER CORRODED. GAINED ACCESS, R & R INTERNAL DOUBLER AND RESTORED ACCESS IAW SRM 51-30-1, 51-30-5, AND AMDS CARD 5331-01180-02. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CORRODED (CAABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 63 HAS CORROSION ON OTBD EDGE. RECEIVED FLOOR PANEL NR 63 IAW SRM 53-23-0, FIG 4 INSTALLED 1EA NEW FLOOR PANEL NR 63.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 27 HAS CORROSION ON SKIN. FOUND DAMAGED BEYOND REPAIR IAW SRM 53-01, FIG 1. FABRICATED 1EA FLOOR PANEL IAW DWG 9957919 & ER/A 488729-14. INSTALLED 1EA FLOOR PANEL NR 27 IAW DCARD 0590-0020-8M. REQUIRED INSP COMPLETED.

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN, STA 804, RBL 8, INTERCOSTAL HAS CHAFE MARK FROM FASTENER HEAD. BLEND CHAFE SMOOTH ORIGINAL MATERIAL .050 REMAINING .025 FOUND OUT OF LIMITS 1" X 1". REMOVED DAMAGE 97 & 7075T6 .063, DOUBLER FABRICATED LOCATED, DRILLED, DEBURRED, TREATED, PRIMED & INSTALLED IAW SRM 51-10-3, 51-30-5, 53-13-3, 51-70-5, 51-10-4 & ER/A 489356-14. REQUIRED INSP COMPLETED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY COMPARTMENT AFTER REMOVAL OF CANTED 1245 FRAME, CHANNEL CRACKED. STOP DRILLED CRACK, HFEC INSPECTED IAW NDT SPM 06-10-01. FOUND CRACK CONTAINED, FABRICATED REPAIR PARTS USING AND INSTALLED IAW IAW SRM 53-01, FIG 2. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN METAL SKIN FLOOR PANEL, NR 67 HAS CORROSION AROUND EDGES. RECEIVED 1EA NEW FLOOR PANEL NR 67 & IAW SRM 53-23-0. DRILLED UP IAW SRM 51-10-4. INSTALLED, 1EA FLOOR PANEL NR 67. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — BENT (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL NR 85 IS BENT AT FWD FLANGE, BS 851. REMOVED PANEL NR 85 IAW SRM 51-30-1, CUTOUT DAMAGE IAW SRM 53-05, FIG 2. FABRICATED DOUBLER & FILLER IAW SRM 53-05, FIG 2, INSTALLED DOUBLER & FILLER IAW 53-05, FIG 2. COMPLETED.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 30 HAS CORROSION ON SKIN PREVIOUS REPAIR. REMOVED PANEL NR 30 FROM CABIN FLOOR IAW SRM 51-30-1. FABRICATED FLOOR PANEL NR 30 IAW ER/A 488731-14. INSTALLED FLOOR PANEL NR 30 IAW SRM 51-30-1. REQUIRED INSP COMPLETED.

Part: CAP — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPARTMENT L19R AFT END CAP HAS CORROSION. REMOVED END CAP, LONGERON, INTERCOSTAL, & WEB FOR CORROSION OUT OF LIMITS REMOVED FASTENERS STA 1151-1167, L18R-L21. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, ALL PARTS & AREAS & INSTALLED ALL FASTENERS IAW SRM 53-01, 51-10-3, 51-30-5.

Part: SKIN — CORRODED (FLOOR PANEL) · airframe 78,354 hrs · 77,526 cycles

MAIN METAL SKIN FLOOR PANEL NR 79 HAS CORROSION AROUND EDGES TOP & BOTTOM SURFACE. REMOVED FLOOR PANEL NR 79 IAW SRM 53-13-0, FIG 4, INSTALLED 1EA NEW FLOOR PANEL NR 79 IAW CARD 0590-4020-8M.

Part: SKIN — CORRODED (FLOOR PANEL) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 83 HAS CORROSION AROUND EDGES. RECEIVED 1EA FLOOR PANEL NR 83 IAW SRM 53-23-0, FIG 4. DRILLED UP IAW SRM 51-10-4. INSTALLED ON CARD 0590-4020-8M. REQUIRED INSP COMPLETED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FWD CARGO COMPARTMENT STA 658 BETWEEN L29L-L30 INNER SKIN HAS CORROSION, CORRECTED. SKIN REPLACED.

Part: SKIN — CORRODED (FLOOR PANEL) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 91 HAS CORROSION ON OTBD EDGE. REMOVED & RECEIVED 1EA NEW FLOOR PANEL NR 91. FURNISHED IAW SRM 53-13-0, FIG 4 INSTALLED 1EA NEW FLOOR PANEL NR 91 IAW CARD 0590-4020-8M, CORRECTED.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT ACC COMPARTMENT STA 1252 LT SIDE ASSEMBLY SKIN PANEL BETWEEN 2EA REPAIRS IS CRACKED. REMOVED 2 EA DOUBLERS IAW DC9 SRM 51-30-2. CUT OUT DAMAGED AREA IAW BOEING DRAWING SG0950002. FABRICATED FINGER DOUBLER, EXTERNAL DOUBLER AND 3 EA FILLERS IAW DC9 SRM 53-04 FIG 38, 37 AND 51-10-2 AND 51-10-4. INSTALLED DOUBLERS IAW DC-9 SRM 51-30-2. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL 59 HAS CORROSION ON END. FABRICATED NEW FLOOR PANEL PER ER/A 488730-14.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO COMPARTMENT STA 435 RT SIDE BETWEEN LONG 27 AND 28 TIE DOWN TRACK FITTING HAS CORROSION. REMOVED CORROSION FROM TRACK FITTING PART OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 SHT 3 ORDERED REPLACEMENT FITTING RECEIVED NEW FITTING AND INSTALLED IAW DC9 SRM 51-30-5.

Part: CAP — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPARTMENT L21L AFT END CAP HAS CORROSION. REMOVED L21R END CAP STA 1167 IAW DC9 SRM 51-30-2. CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. DRILLED NEW END CAP IAW DC9 SRM 51-10-4 AND INSTALLED IAW DC9 SRM 51-30-2.

Part: SUPPORT FITTING — CORRODED (CARGO BAY) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO COMPARTMENT STA 598 LT BETWEEN LONG 27 AND 28 TIE DOWN TRACK SUPPORT FITTING HAS CORROSION. UPON FURTHER INSPECTION TIE DOWN MOUNT FOUND TO BE OUT OF LIMITS IAW DC9 SRM 51-10-3 & 53-01 FIG 1 DUE TO EXFOLIATED CORROSION. INSTALLED NEW MOUNT IAW DC9 SRM 51-30-1/-05 P202.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

VERTICAL STA LT STA 1230 ATTACH ANGLE FUSELAGE TO VERTICAL IS CRACKED. REMOVED CRACKED ATTACH ANGLE IAW DC9 SRM 51-30-2 & 51-30-5 FABRICATED PER DWG 5912188 IAW DC9 SRM 51-10-2. HEAT TREAT OF NEW ANGLE ACCOMPLISHED ON 2446N01636. LOCATED, DRILLED, TREATED AND PRIMED ATTACH ANGLE IAW DC9 SRM 51-10-4, 51-10-3. INSTALLED ATTACH ANGLE IAW DC9 SRM 51-30-2 & 51-30-5 PER DWG 5912188.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER JAMB WEB FWD O/B STRAP HAS CORROSION. REMOVED STRAP IAW DC9 SRM 51-30-5 LOCATED AND DRILLED IAW DC9 SRM 51-10-4. INSTALLED NEW STRAP IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — CANNING (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL 64 HAS OIL CAN DAMAGE AT FORWARD END BS 674. CUTOUT DAMAGE 7/8"X5 1/2" HFEC INSPECTED PER NDT SPM FABRICATED DOUBLER AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 1.

Part: CAP — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO L20 AFT END CAP HAS CORROSION. REMOVED L20R END CAP STA 1167 IAW DC9 SRM 51-30-2. CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01. DRILLED NEW END CAP IAW DC9 SRM51-10-4 AND INSTALLED IAW DC9 SRM 51-30-2.

Part: SUPPORT FITTING — CRACKED (SPOILER) · airframe 78,354 hrs · 77,526 cycles

LEFT WING I/B SPOILER TORSION BAR CENTER SUPPORT FITTING IS CRACKED. REMOVED SUPPORT FITTING IAW DC9 SRM 51-30-2, 51-30-1, 51-30-5 LOCATED DRILLED DEBURRED IAW DC9 SRM 51-10-4. INSTALLED NEW SUPPORT FITTING IAW DC9 SRM 51-30-5.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

RIGHT MAIN WHEEL WELL STA 813 XCW 58 PRESSURE DECK WEB DOUBLER CRACKED. REMOVED WEB INSIDE CABIN ST FS 813 AND REMOVED -5 AND -7 DOUBLERS IAW DC9 SRM 51-30-2 AND 51-30-5. FABRICATED DOUBLER IAW DC9 DWG 9930873 LOCATED, DRILLED, AND DEBURRED DOUBLERS IAW DC9 SRM 51-10-4 & INSTALLED DOUBLERS IAW DC9 SRM 51-30-5 INSTALLED WEB IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STATION 160 LONGERON L4L CRACKED. REMOVED AND REPLACED L4L IN MAIN CABIN AREA AT STA 148 TO STA 22 9 IAW DC9 SRM 51-30-5, 51-30-1, 51-30-2, & 51-20-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

DURING AGING AIRCRAFT INSPECTION, AN EXISTING REPAIR PER EA 98-092037 WAS FOUND A THE FORWARD CARGO DOOR CUTOUT AFT LOWER CORNER, EA 98-092037 REPAIR MUST BE REMOVED TO EVALUATE DAMAGE. GAINED ACCESS REMOVED SECTION OF SKIN STA 360-503 L26L TO L26R. DRILLED DEBURRED AND C'SUNK NEW SKIN FABRICATED 16 REPAIR DOUBLERS AND 16 STRAPS, 2 FINGER DOUBLERS AND 2 ANTENNA DOUBLERS TREATED PRIMED AND INSTALLED REPAIR PARTS AND NEW SECTION OF SKIN RESTORED ACCESS IAW DC9 SRM 53-04 FIG 12C AND 53-04 FIG 12E P174. REQUIRED INSPECTION COMPLETED BY Q919.

Part: FRAME — CRACKED (NLG WW) · airframe 78,354 hrs · 77,526 cycles

NOSE WHEEL WELL THROUGH ACCESS HOLE STA 51 BL0 OVER HEAD FRAME IS CRACKED APPROXIMATELY 3 INCHES. REMOVED DAMAGED SECTION OF FRAME NDT VERIFIED CRACK FREE CONDITION IAW SPM 06-10-01.001 FABRICATED REPAIR PARTS IAW SRM DC9 SRM 51-18-1FIG 1 SHT 2 INSTALLED IAW DC9 SRM 51-30-2, 51-30-5, & 53-04 FIG 20 P245.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 750 LBL 44 WEB TO CENTER TANK SUPPORT CRACKED APPROX 3 INCHES. REMOVED AND REPLACED SUPPORT FROM STA 712 TO 794 LBL44 IAW DWG 5910464.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STATION 160 LONGERON L3L CRACKED. REMOVED AND REPLACED L3L IN MAIN CABIN AREA AT STA 148 TO STA 22 9 IAW DC9 SRM 51-30-5, 51-30-1, 51-30-2, & 51-20-1.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY STATION 1190 BETWEEN L17L AND L18L FRAME ATTACH CLIP CRACKED. REMOVED CRACKED ATTACH CLIP FROM AFT ACCESSORY COMPARTMENT AT STA 1190 IAW DC 9 SRM 51-30-2. FABRICATED, LOCATED DRILLED DEBURRED TREATED, PRIMED AND INSTALLED IAW DWG 5913 596, 51-10-4, 51-10-2, 51-10-3, 51-20-0, 51-30-5, P106.

Part: FITTING — CORRODED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN BETWEEN STA 693-712 RBL-55 BATH TUB FITTING HAS CORROSION. REMOVED CORROSION ON BATH TUB FITTING OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 SHT 3. REMOVED AND INSTALLED BATH TUB FITTING IAW DC9 SRM 51-30-5 AND DWG 5910464.

Part: ATTACH ANGLE — CRACKED (NR 2 PYLON) · airframe 78,354 hrs · 77,526 cycles

NR 2 PYLON REAR SPAR WEB ATTACH ANGLE CRACKED. REMOVED ATTACH ANGLE IAW SRM 51-30-5 AND ORIG MATERIAL .040 TITANIUM IAW SRM DWG 9915500, REV K, FABRICATED ATTACH ANGLE IAW DWG 9915500. INSTALLED ATTACH ANGLE IAW DWG 9915500.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 26 HAS CORROSION ON SKIN. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED NEW FLOOR PANEL FABRICATED DOUBLER IAW DWG 9957918 TREATED AND PRIMED DOUBLER IAW SRM 51-10-3. INSTALLED DOUBLER TO THE PANEL NR 26 IAW SRM 51-30-2 P224.

Part: SHEAR TIE — CRACKED (BS 1243 L4L) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY COMPARTMENT CANTED FRAME 1243, SHEAR TIE CRACKED AT L4L. NDT VERIFIED CRACK IN SHEAR TIE REMOVED. SHEAR TIE FABRICATED, ALODINED, PRIMED AND INSTALLED NEW TIE IAW SRM 51-30-2, 51-10-3 & 9911858, REV BA P174.

Part: SUPPORT ANGLE — CRACKED (RT NACELLE) · airframe 78,354 hrs · 77,526 cycles

RT ENGINE PYLON AFT SIDE OF REAR SPAR OTBD SUPPORT ANGLE CRACKED APPROX 1 INCH. REMOVED SUPPORT ANGLE IAW SRM 51-30-5 & 51-30-1 AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-1 & 51-30-5 & DWG 9915500, REV K.

Part: FRAME — CORRODED (BS 1003) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPARTMENT, STA 1003, FRAME HAS CORROSION ON AFT LOWER SIDE. REMOVED CORROSION IAW SRM 51-10-3, ORIGINAL MATERIAL WAS .071 IAW SRM 53-13-3, REMAINING .044. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1 CUTOUT DAMAGED AREA AND REPAIRED IAW SRM 53 -03, PG 401, FIG 2A, SHEET 4. REQUIRED INSP COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1151 L14R-15R) · airframe 78,354 hrs · 47,739 cycles

MAIN PASSENER CABIN STA 1151 BETWEEN L14R-L15R SHEAR TIE CRACKED. REMOVED CRACKED SHEAR TIE & SPLICE RECEIVED NEW PART FOR L17R-L13R. INSTALLED ALL PARTS IAW DWG 5060119, SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4. P202 REQUIRED INSP COMPLETED.

Part: CUSP WEB — CRACKED (STA 674, RBL 57) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN CUSP WEB AT STA 674, RBL 57 CRACKED AND 2 EA FASTENER HOLES HAS SHORTED. CUTOUT DAMAGE IAW SRP 53-10-16, APPROX 1" X .5" NDT VERIFY DAMAGE. REMOVED FABRICATED REPAIR DOUBLER AND INSTALL IAW SRP 53-10-16 MATERIAL .025 FABRICATED FILLER .020. P224 REQUIRED INSPECTION COMPLETED.

Part: CUSP WEB — CRACKED (BS 1136 LBL 55) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FWD OF STA 1136, LBL 55, CUSP WEB CRACKED. REMOVED FLOOR SUUPORT FOR STA 1136 TO 1100 LBL-55 CUTOUT DAMAGED AREA 1.5" X 3" NDT VERIFIED CRACK REMOVED. HFEC FOUND CRACK REMOVED DOUBLER .050. DOUBLER REMOVED & REINSTALLED FABRICATED PARTS IAW DWG SG 09530019. P202 REQUIRED INSP COMPELTED.

Part: SHEAR TIE — CRACKED (BS 1151 L16-17R) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN, STA 1151, RT BETWEEN LONG 16 AND 17, FRAME HAS SEVERAL ELONGATED HOLES FOUND HOLES AFTER REMOVING CRACKED SHEAR TIE. REMOVED FRAME SPLICE. FABRICATED. 3 EA FRAME SPLICES INSTALLED ALL PARTS IAW DWG J060119, SRM 51-30-2, 51-30-5, 51-30-1, 53-03, FIG 3. P202 REQUIRED INSP COMPLETED.

Part: CUSP WEB — CRACKED (STA 693, RBL 52) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN, STA 693, RBL 52, CUSP WEB IS CRACKED. REMOVED CRACKED WEB IAW SRM 51-30-2. FABRICATED NEW IAW DWG SG09530019 AND INSTALL MATERIAL .020. FABRICATED 5 EA RING DOUBLER .050, 3EA, .071 AND INSTALLED IAW DWG SG09530019 & 51-30-2. P224 REQUIRED INSPECTION COMPLETED.

Part: SKIN — CRACKED (NLG DOOR) · airframe 78,354 hrs · 77,526 cycles

EXTERIOR DOUBLER CRACKED AT LT AFT NLG DOOR AFT HINGE. R & R DOUBLER IAW SRM 53-05. IDENTIFIED REPAIR IAW DPS 900-5-1, NR4, PG1 NDT VERIFIED CRACK CONTAINED. REQUIRED INSPECTION COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1187 L18R) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 1187 AT L18R SHEAR TIE CRACKED. REMOVED OLD PART AND INSTALLED NEW AFT PRESSURE BULKHEAD SHEAR TIE IAW SRM 51-10-5 AND 51-30-2.

Part: LONGERON — CRACKED (BS 130-230 L2L) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 200 L2L CRACKED. R & R LONGERON L2L, STA 130 TO 230 IAW SRM 51-10-4, 51-30-5.P-202. CORRECTED.

Part: INTERCOSTAL — CRACKED (BS 1292 L18L) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESORY COMPARTMENT, STA 1292, L18L INTERCOSTAL CRACKED AFT END CRACK RUN PASS STOP DRILL. REMOVED ATTACH CLIPS AND INTERCOSTAL OBTAIN NEW INTERCOSTAL DRILLED AND DEBURRED AND INSTALLED INTERCOSTAL AND ATTACH CLIPS IAW SRM 51-30-02 & 51-30-5.

Part: SKIN — CRACKED (NLG DOOR) · airframe 78,354 hrs · 77,526 cycles

EXTERIOR DOUBLER CRACKED AT RT AFT NLG DOOR AFT HINGE. REMOVED & INSTALLED DOUBLER IAW SRM 53-05. IDENTIFIED REPAIR IAW DPS 900-5-1 NR 4, PG 1 NDT VERIFIED CRACK CONTAINED. REQUIRED INSPECTION COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1275 L16-17L) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY CANTED FRAME 1275 SHEAR TIE CRACKED BETWEEN L16L AND L17L. REMOVED CRACKED SHEAR TIE IAW SRM 01-30-21-51-305. DWG 9911859 & 51-10-2 & 51-10-4. INSTALLED SHEAR TIE IAW 51-30-2 & 51-30-5. REQUIRED INSP COMPLETED.

Part: WEB — CRACKED (BS 69 LBL 15) · airframe 78,354 hrs · 77,526 cycles

NOSE WHEEL WELL, STA 69, LBL 15 THROUGH ACCESS HOLE WEB IS CRACKED APPROX 1". STOP DRILLED CRACK. NDT VERIFIED. FABRICATED REPAIR DOUBLER AND NEW ANGLE IAW SRM 53-01 AND 51-10-1, 51-10-2. INSTALLED DOUBLER IAW SRM 53-01. INSTALLED ANGLE IAW SRM 51-30-2, 51-30-5. IDENTIFIED REPAIR IAW DPS 900-5-1, NR 4, PG 2. REQUIRED INSP COMPLETED.

Part: SEAT TRACK — GOUGED (BS 906-911) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 906-911 LT INBD SEAT TRACK GOUGED. USING A DEPTH GAUGE MEASURE, DEPTH OF GOUGE. MATERIAL THICKNESS.115 IAW SRM 51-10-1, FIG 26, SHEET PAGE 86. DEPTH OF GOUGE IS .060 MATERIAL IS OUT OF LIMIT IAW SRM 53-01. INSTALLED SEAT TRACK PLUG IAW SRM 51-30-1. REQUIRED INSPECTION COMPLETED.

Part: SEAT TRACK — GOUGED (BS 580) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 580, RT INBD SEAT TRACK GOUGED. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-05, FIG 4B. ROUTED OUT DAMAGED AREA FOR SEAT TRACK PLUG IAW SRM 53-05 FIG 4A NDT VERIFIED NO CRACKS OF INDICATORS NOTED. INSTALLED SEAT TRACK PLUG IAW SRM 51-30-1. REQUIRED INSPECTION COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1136 L14-15R) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 1136, BETWEEN L14R-L15R SHEAR TIE CRACKED AT PYLON SUPPORT MOUNT FASTENER. R & R SHEAR TIE AT MAIN PASSENGER, STA 1136, PYLON SUPPORT BETWEEN L14R & L15R IAW SRM 51-10-4, 51-30-4, 51-30-05 AND DWG SRO9540004. REQUIRED INSP COMPLETED.

Part: BULKHEAD — CRACKED (BS 69 LBL 15) · airframe 78,354 hrs · 77,526 cycles

NOSE WHEEL WELL, STA 69, LBL 15, BULKHEAD THROUGH ACCESS HOLE. WEB IS CRACKED APPROX 1 INCH. STOP DRILLED CRACK. NDT VERIFIED. FABRICATED REPAIR DOUBLER IAW SRM 53-01. INSTALLED DOUBLER IAW SRM 53-01, FIG 2 SHT 3. IDENTIFIED REPAIR IAW DPS 900-5-1, NR4, PG.6. REQUIRED INSP COMPLETED.

Part: LONGERON — DAMAGED (BS 180 L2R) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN LONGERON 2R HAS 1 EA BENT APPROX 1" LONG AFT OF FRAME, STA 180. REMOVED LONGERON 2 RT, END CAP AND SPLICE IAW SRM 51-30-2. LOCATED AND DRILLED IAW SRM 51-10-4. INSTALLED LONGERON 2 RT FROM STA 160-237, END CAP AND SPLICE IAW SRM 51-30-2.P-180.

Part: CUSP WEB — CRACKED (BS 706) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 706, RBL 58 CUSP WEB IS CRACKED. REMOVED DAMAGED CUSP WEB LOCATED AND DRILLED NEW CUSP WEB AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-30-5. P245. REQUIRED INSP COMPLETED.

Part: WEB — DAMAGED (BS 1245 L4R) · airframe 78,354 hrs · 77,526 cycles

AFTER REMOVAL OF FRAME FOUND ELONGATED HOLE IN WEB AT CANTED FRAME 1245, L4R. REMOVED DAMAGED WEB IAW SRM 51-30-2 & 51-30-5. FABRICATED LOCATED DRILLED & INSTALLED NEW WEB IAW SRM 51-10-2, 51-10-4, 51-10-3, 51-30-2, 51-30-5, & DWG 9911838. P245 REQUIRED INSPECTION COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1258 L1R) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESORY COMPARTMENT, STA 1258 AFT SIDE OF CANTED FRAME RT SIDE OF LONG 1 SHEAR TIE IS CRACKED APPROX 1 INCH. REMOVED CRACKED SHEAR TIE IAW SRM 51-30-2 & 51-30-5. FABRICATED NEW SHEAR TIE IAW DWG 9911840, SRM 51-10-4. HEAT TREAT OF NEW SHEAR TIE ACCOMPLISH ON TRAVELER 2446N01586. LOCATED, DRILLED AND INSTALLED NEW SHEAR TIE IAW SRM 51-10-4, 51-30-2, 51-30-5 IAW DWG 9911840.

Part: WEB — CRACKED (BS 1292-1303) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY COMPARTMENT WEB BETWEEN 1292 AND 1303 AT TIP IS CRACKED IN 2EA PLACES. STOP DRILLED CRACKS IAW SRM 53-01, FIG 2, SHT 3 FABRICATED, DRILLED 2EA DOUBLERS IAW SRM 51-10-2 AND 51-10-4 DOUBLERS ARE .050 7075T6 IAW SRM 53-35-0, FIG 4 SHT 2 AND 4. INSTALLED REPAIR DOUBLERS IAW SRM 53-01, FIG2. REQUIRED INSPECTION COMPLETED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

A CRACK AT OTBD HOLE FOUND AFTER REMOVING INTERCOSTAL CLIP. BLENDED OUT CRACK IAW SRM 53-01, FIG 4 SHT.4 FINAL HOLE DIA .375 NDT VERIFIED CRACK CONTAINED IAW NDT SPM 06-10-01. FABRICATED DOUBLER AND FILLER IAW 53-01, FIG 4, SHT 4 IAW 53-13-4, FIG 3. INSTALLED IAW 53-01, FIG 4, SHT 4. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL, NR32, CRACKED APPROX 1 INCH. FOUND CRACK TO BE OUT OF LIMITS IAW SRM 53-01, FIG.1. R & R FLOOR PANEL NR32 IAW SRM 51-30-3. CORRECTED.

Part: LONGERON — CRACKED (BS 1245 L5R) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY COMPARTMENT AFTER REMOVAL OF FRAME AT STA 1245 FOUND 1" CRACK ON L5R AT FASTENER ATTACHMENT. CUTOUT DAMAGED SECTION OF LONGERON 18" IAW SRM 53-02, FIG18. TRIMMED TO FIT LOCATED, DRILLED, & INSTALLED NEW LONGERON SECTION & 2 EA SPLICES IAW SRM 53-02, FIG 18. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR46 HAS CORROSION ON OTBD EDGE. REMOVED CORROSION .020 ORIG MAT, .007 REMOVED, .013 REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R FLOOR PANEL NR46 IAW SRM 51-30-3. CORRECTED.

Part: SKIN — CHAFED (LT WING) · airframe 78,354 hrs · 77,526 cycles

LT WING L/E SKIN AFT OF NR 2 SLAT INBD AND OTBD OF CTR TRACK CUTOUT EXISTING REPAIR IS CHAFED. REMOVED OLD REPAIR NR 2 SLAT BROKE CABLE TENSION, REMOVED NR2 SLAT PULLEY AND BRACKET FAB NEW REPAIR DOUBLER INSTALLED NR2 SLAT EXTENSION CABLE PULLEY AND BRACKET CABLE TENSION TO BE RIGGED ON CARD 2446R881 IAW EA 98-204144 & SRM 51-10-3, 51-30-5 AND AMM 27-80-01 & 20-16-00. INSPECTION COMPLETED.

Part: SKIN — CRACKED (BS 1258 L2R) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE SKIN CRACKED APPROX 1 INCH AT FASTENER STA 1258 AT L2R NDT VERIFIED AND MARKED STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER ALL WORK ACCOMPLISHED IAW SRM 53-01, FIG 2, 51-60-0 FIG 1 AND TOPPS 30-10-70. P214. REQUIRED INSPECTION COMPLETED.

Part: SUPPORT ANGLE — CRACKED (STA 681-718) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 681 TO 718, RBL 55 Z-ANGLE SUPPORT CRACKED 2EA PLACES. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-10-4 PRIMED SUPPORT IAW SRM 51-10-3.

Part: FLOOR PANEL — CORRODED (BS 313-389) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FLOOR PANEL NR32 FWD END OTB FLANGE HAS CORROSION FROM BS 313-389. REMOVED CORROSION .020 ORIG MAT.006, REMOVED .014, REMAINING FOUND TO BE OUT OF LIMITS. REPLACED FLOOR PANEL IAW SRM 51-30-5. CORRECTED.

Part: GUSSET — CRACKED (STA 832 LBL16) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 832, LBL 16 GUSSET IS CRACKED. REMOVED GUSSET IAW SRM 51-30-2. FABRICATED NEW GUSSET IAW SRM 51-10-2 & DWG 4915719 LOCATED & DRILLED GUSSET IAW SRM 51-10-4. INSTALLED GUSSET IAW SRM 51-30-5.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR38 HAS CORROSION ON OTBD EDGE. R & R FLOOR PANEL NR 38 IAW SRM 51-30-3. REMOVED CORROSION .020 ORIGINAL .008 REMOVED .012. REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-01. CORRECTED.

Part: SUPPORT ANGLE — CRACKED (LT WING TE FLAP) · airframe 78,354 hrs · 77,526 cycles

LT WING FLAP OTBD SIDE OF NR 4 FLAP HINGE INSIDE ACCESS PANEL 1545A SUPPORT ANGLE IS CRACKED. REMOVED CRACKED HINGE BRACKET, OBTAIN NEW BRACKET, DRILLED AND DEBURRED AND INSTALLED IAW SRM 51-30-5 & 51-30-2.

Part: SKIN — CRACKED (BS 1258 L3-4L) · airframe 78,354 hrs · 77,526 cycles

FUSELAGE SKIN CRACKED 2EA PLACES JUST AFT OF STA 1258 BETWEEN L3L AND L4L NDT VERIFIED AND MARKED STOP DRILLED 2EA CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLER FROM .063 7075T6. ALL WORK ACCOMPLISHED IAW SRM 53-01, FIG 2, 51-60-0, FIG 1. CORRECTED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR 37 HAS CORROSION ON OTBD EDGE. R & R FLOOR PANEL NR37 IAW SRM 51-30-1. ORIGINAL PANEL THICKNESS .020. REMOVED .005 MATERIAL, REMAINING .015 WHICH IS OUT OF LIMITS IAW SRM 53-01, FIG 1, P245. CORRECTED.

Part: CUSP WEB — DAMAGED (STA 541) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 541 RT CUSP WEB HAS HOLE. REMOVED .5" DAMAGE, FABRICATED REPAIR PART. HFEC AREA FOUND CRACK FREE CONDITION IAW NDT SPM 06-10-01 INSTALLED AND PRIMED, WORK ACCOMPLISHED IAW SRM 51-13-2, FIG 4, 51-10-4, 51-10-3, DWG SG09530019. REQUIRED INSPECTION COMPLETED.

Part: ANGLE — CRACKED (BS 1326) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY BETWEEN CANTED FRAME 1326 RBL-24 UPPER INTERCOSTAL SUPPORT ANGLE CRACKED APPROX 2 INCHES. REMOVED CRACKED STIFFENER IAW SRM 51-30-2 & 51-30-5. RECEIVED NEW STIFFENER LOCATED & DRILLED & DEBURRED IAW SRM 51-10-4. INSTALLED STIFFENER IAW SRM 51-30-2 & 51-30-5.

Part: FLOORBEAM — CRACKED (BS 598) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 598 BL-0 TO LBL-22 FLOOR SUPPORT PANEL. SUPPORT IS CRACKED. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-30-2. RECEIVED METAL FOR FABRICATION OF NEW FLOORSUPPORT INSTALLED NEW FABRICATED FLOOR SUPPORT IAW SRM 51-30-2.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 78,354 hrs · 77,526 cycles

AFT ACCY COMPARTMENT ABOVE Y-DUCT WHERE VERT STABILIZER LT ATTACH BOLT FITTING IS LOCATED, FRAME HAS 2 EACH CRACKS. REMOVED CRACKED FRAME IAW SRM 51-30-5. LOCATED, DRILLED AND INSTALLED NEW FRAME, CUSTOMER FURNISHED PART IAW SRM 51-10-4 & 51-30-5.

Part: FRAME — CRACKED (BS 1209) · airframe 78,354 hrs · 77,526 cycles

AFT ACCY FRAME 1209 CRACKED AT LIGHTNING HOLE, APPROX 4 INCHES AT L12R. STOP DRILLED VERIFIED CRACK NO LONGER EXIST IAW NDT SPM 06-10-01. FABRICATED REPAIR DOUBLER, HEAT TREATED TO T6, DRILLED AND DEBURRED DOUBLER, ALODINE, PRIMED AND INSTALLED IAW SRM 53-01, FIG 2 & 51-10-3 & 51-10-4. REQUIRED INSP COMPLETED.

Part: FLOORBEAM — CRACKED (BS 636) · airframe 78,354 hrs · 47,739 cycles

MAIN PASSENGER CABIN, STA 636 BETWEEN BL-0 AND LBL-22 FLOOR PANEL SUPPORT IS CRACKED. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED NEW FROM IAW SRM 53-13-12 DRILLED, LOCATED, DEBURRED IAW SRM 51-10-4. TREATED & PRIMED IAW SRM 51-10-3, TABLE 1. INSTALLED NEW FLOOR SUPPORT IAW SRM EC9 51-30-2, P174. CORRECTED.

Part: STRUCTURE — CHAFED (BS 190 RBL 4) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 190, RBL 4 PREVIOUS REPAIR CHAFED. R & R REPAIR DOUBLER AT STA 190, RBL-4. ORIGINAL MATERIAL .020, 7075T6 IAW SRM 53-01, FIG 4 SHY.4 & DC9-A-53-20-03-801-66 3A-A, P106.

Part: WINDOW FRAME — CRACKED (RT BS 693) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN, RT SIDE, STA 693 LOWER FWD WINDOW FRAME IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS IAW DC9-A-56-20-02-801-663A-A. HFEC AREA FOUND CRACK FREE CONDITION IAW NDT SPM 06-10-01. TREATED, PRIMED, INSTALLED & TOPCOATED IAW SRM 51-10-3 AND SRM 51-30-2, 51-30-5, SRM 51-10-488251. REQUIRED INSPECTION COMPLETED.

Part: SUPPORT FITTING — CRACKED (BS 1060) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPT STA 1060 RT TIE DOWN TRACK SUPPORT FITTING IS CRACKED. REMOVED ORIGINAL FITTING AND FOUND WITH 100 PERCENT MATERIAL LOSS. FABRICATED NEW FITTING LOCATED, DRILLED, DEBURRED THEN TREATED AND PRIMED INSTALLED NUTPLATE THEN FITTING WET IAW DWG 5956034, SRM 51-30-5, 51-30-2, 51-10-2, 51-10-4, 51-10-3.

Part: SUPPORT FITTING — DAMAGED (BS 1136) · airframe 1,665 hrs · 1,439 cycles

AFT CARGO COMPT RT SIDE CARGO TIEDOWN TRACK FITTING IS BROKEN AT AFT SIDE OF FRAME STA 1136. REMOVED TIEDOWN TRACK FITTING AT STA 1136 IAW SRM 51-30-5 RECEIVED PN 5956034-503N DRILLED, DEBURRED, TREATED, & PRIMED ATTACH HOLES IAW SRM 51-10-3 & 51-10-4. INSTALLED FITTING IAW SRM 51-30-5 & DWG 5956034.

Part: DOUBLER — CRACKED (BS 694) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 694 LT LOWER FWD WINDOW FRAME DOUBLER IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS IAW DC9-A-56-20-02-801-663A-A. HFEC AREA FOUND CRACK FREE CONDITION IAW NDT SPM 06-10-01. TREATED, PRIMED, INSTALLED & TOPCOATED IAW SRM 51-10-3 AND SRM 51-30-2, 51-30-5, SRM 51-10-3. REQUIRED INSP COMPLETED.

Part: FLOORBEAM — CRACKED (BS 1108) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN, STA 1108, BETWEEN RBL 23-38 FLOOR SUPPORT CRACKED. REMOVED CRACKED FLOOR SUPPORT, STA 1108, RBL 23-38 IAW SRM 51-30-2. FABRICATED, DRILLED, DEBURRED IAW SRM 51-10-4 AND DWG 5914617. INSTALLED IAW 51-30-2 .040 7075T6 PO 1023415.

Part: FLOORBEAM — CRACKED (BS 237) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 237, BL0-LBL 22 FLOOR PANEL SUPPORT IS CRACKED. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED NEW SUPPORT IAW SRM 51-10-2. LOCATED AND DRILLED IAW SRM 51-10-4. TREAT & PRIME IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2 & 51-30-5.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR21 HAS CORROSION ON SKIN AND ON COVER PLATE. FLOOR PANEL EXFOILIATED LOSS OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED NEW PANEL AND DRILLUP IAW SRM 51-10-4 AND 51-10-2.

Part: FLOOR SUPPORT — DAMAGED (BS 1100 LBL 55) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN FWD OF STA 1100, LBL 55 FIBERGLASS FLOOR SUPPORT BROKEN OUT AT FASTENER HOLE. REMOVED FLOOR SUPPORT STA 1100, LBL 55 IAW SRM 51-30-2. RECEIVED & FABRICATED NEW FLOOR SUPPORT IAW SRM 51-10-2. RECIEVED & FABRICATED NEW BRACKET. FABRICATED, DRILLED, & LOCATED IAW SRM 51-10-2 & 51-10-4. INSTALLED IAW SRM 51-30-5.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 78,354 hrs · 77,526 cycles

RT ENGINE PYLON ELECTRICAL COMPARTMENT UPPER FWD STIFFENER CRACKED ON INBD END APPROX .5 INCH. REMOVED CRACKED STIFFENER IAW SRM 51-30-2. RECEIVED MATERIAL TO FABRICATE NEW STIFFENER IAW SRM 54-10-0, SHT 1, 51-10-2. LOCATED, DRILLED, D-BURRED IAW SRM 51-10-4. TREATED & PRIMED IAW SRM 51-10-3. INSTALL NEW STIFFENER IAW SRM 51-30-2. REQUIRED INSPECTION COMPLETED.

Part: FLOOR SUPPORT — CORRODED (STA 1167-1176) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN BETWEEN STA 1167-1176, RBL 18 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-30-1. REMOVED CORROSION. FROM FLOOR SUPPORT FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT IAW SRM 51-10-2. HEAT TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED SUPPORT IAW SRM 51-30-1, P174.

Part: FLOORBEAM — DAMAGED (BS 813 RBL 52) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 813, RBL 52, FLOORBEAM ATTACH CLIP AFT SIDE HAS DRILL MARK DAMAGE. REMOVED ATTACH CLIP AFT SIDE OF STA 813, RBL 52 IAW SRM 51-30-2, 51-30-1. FABRICATED, LOCATED, DRILLED AND DEBURRED ATTACH CLIP IAW SRM 51-10-4. INSTALLED ATTACH CLIP IAW SRM 51-30-5.

Part: FLOORBEAM — DAMAGED (BS 813 RBL 52) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 813, RBL 52, FLOORBEAM ATTACH CLIP FWD SIDE HAS DRILL MARK DAMAGE. REMOVED ATTACH CLIP FORWARD SIDE OF STA 813, RBL 52 IAW SRM 51-30-2, 51-30-1. FABRICATED, DRILLED, LOCATED AND DEBURRED ATTACH CLIP IAW SRM 51-10-4. INSTALLED ATTACH CLIP IAW SRM 51-30-5.

Part: FLOORBEAM — CRACKED (BS 617) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 617, BL-0 TO LBL-22 FLOOR PANEL SUPPORT IS CRACKED. REMOVED FLOOR SUPPORT & ANGLE ATTACHED. FOUND ANGLE OUT OF LIMITS IAW SRM 51-30-2 & 53-01, FIG 1. RECEIVED NEW ANGLE AND MAT FOR NEW FLOOR SUPPORT. FABRICATED, DRILLED, DEBURRED AND TRIMMED TO FIT NEW ANGLE & FLOOR SUPPORT IAW 53-13-12 51-10-2, 51-10-4 INSTALLED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 1167) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 1167, RT SIDE APB NR5 VERTICAL FRAMETOP ANGLE CRACKED. REMOVED TOP CLIP ANGLE FROM STA 1167 RT APB NR 5 IAW SRM 51-30-5 & 51-30-2. ORG MAT 050 IAW DWG 9915558. FABRICATED CLIP ANGLE IAW SRM 51-10-2 AND DWG NR 9915558. LOCATED & DRILLED IAW SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR20 HAS CORROSION. REMOVED CORRSION FROM MAIN CABIN METAL SKIN FLOOR PANEL NR20 IAW SRM 51-10-3. ORIGINAL MATERIAL THICKNESS .025 MATERIAL LOSS.013, REMAINING MAT .012 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, SHEET 3. LOCATED DRILLED AND DEBURRED IAW SRM 51-10-4.

Part: CUSP WEB — CRACKED (BS 761 RBL 58) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 761, RBL 58, CUSP WEB IS CRACKED. REPAIRED MAIN PASSENGER CABIN CUSP WEB AT STA 761, RBL 58 IAW SRP DC9-A-53-10-16-801-663A-A. HFEC INSP FOUND CRACK CONTAINED IAW NDT SPM 06-10-01. REQUIRED INSPECTION COMPLETED.

Part: CUSP WEB — CHAFED (BS 775 RBL44-55) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 775, RBL 44-55, CUSP WEB CHAFED 2EA PLACES. BLENDED IN 2EA PLACES IAW SRM 53-01, FIG 1, SHT 3 (1"X 1.5") ORIG MAT .020. REMOVED .017 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, SHT 3. CUTOUT DAMAGED AREA (2" X 2.5") IAW NW SRP DC9-A-53-10-16-801-663A-A. FAB 2EA FILLERS, 1EA DOUBLER IAW NW SRP DC9-A-53-10-16-801-663A-A. INSTALLED 2EA FILLER & 1EA DOUBLER IAW SRM 51-30-2 & NW SRP DC9-A-53-10-16-801-663A-A. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR45 HAS CORROSION AROUND EDGES. CORRECTED, RECIEVED NEW FLOOR PANEL FROM SUPPLY PN 09-5300-3-1731, PO 1011W022.

Part: STRUT — CRACKED (BS 655) · airframe 78,354 hrs · 77,526 cycles

FWD CARGO COMPARTMENT STA 655 RT SIDEWALL STRUT CRACKED AT LOWER END. HFEC INSPECTED FOUND CRACK TO BE CONTAINED IAW NDT SPM 06-10-01. REPAIRED CRACKED STRUT IAW SRM 53-01, FIG 2, SHT 4. REQUIRED INSPECTION COMPLETED.

Part: SUPPORT — CRACKED (BS 655) · airframe 78,354 hrs · 77,526 cycles

FWD CARGO COMPARTMENT STA 655 LT SIDEWALL STRUT CRACKED AT LOWER END. HFEC INSPECTED FOUND CRACK TO BE CONTAINED IAW NDT SPM 06-10-01. REPAIRED CRACKED STRUT IAW SRM 53-01, FIG 2, SHT 4. REQUIRED INSPECTION COMPLETED.

Part: CARGO TRACK — CORRODED (BS 1022) · airframe 78,354 hrs · 77,526 cycles

AFT CARGO COMPT STA 1022 RT TIEDOWN TRACK BETWEEN LONGERON 27 AND 28 SUPPORT FITTING UNDER TRACK HAS CORROSION. REMOVED, IDENTIFIED, SUPPORT FITTING AND NUTPLATE. REMOVED CORROSION, ORIGINAL MATERIAL .125 REMAINING, .091 REMOVED, .034 FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND DEBURRED NEW FITTING PN 2922368-1. TREATED, PRIMED, THEN INSTALLED WET IAW SRM 51-10-3, 51-30-5, & 53-01 FIG 1.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR31 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION FROM MAIN CABIN FLOOR PANEL NR31 ORIGINAL THICKNESS .020, REMOVED .007 WITH .013. REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED CUST FURNISHED FLOOR PANEL PN 09-5300-3-1731.

Part: CUSP WEB — CRACKED (BS 768 RBL 58) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 768, RBL 58, CUSP WEB IS CRACKED. REPAIRED MAIN PASSENGER CABIN CUSP WEB AT STA 768, RBL 58 IAW SRP DC9-A-53-10-16-801-663A-A. HFEC INSP FOUND CRACK CONTAINED IAW NDT SPM 06-10-01. REQUIRED INSPECTION COMPLETED.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO AT STA 674 LONGERON 26 RT HAS 3 ELONGATED HOLES. REPAIRED 3 ELONGATED HOLES IN FWD CARGO COMP AT STA 674 L26R PER EA 488342-14. THREE EA FREEZE PLUGS FABRICATED AND INSTALLED ON TRAVELER 42446N01553 IAW DC9A-51-20-03-801-663A.

Part: FLOOR SUPPORT — DAMAGED (BS 237 RBL 55) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 237, RBL 55 FIBERGLASS FLOOR SUPPORT ELONGATED HOLE. REMOVED FLOOR SUPPORT STA 190, RBL 55, LOCATED & DRILLED DEBURRED REPLACEMENT IAW SRM 53-20-01-801-663A-A, 51-10-2, 51-10-4 TREATED & PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN APB OTBD SIDE NR5 VERTICAL FRAME BOTTOM OLD REPAIR CRACKED. REMOVED EXISTING REPAIR FABRICATED, TRIMMED, LOCATED, DRILLED, DEBURRED, TREATED & PRIMED. NEW REPAIR ANGLES INSTALLED NEW REPAIR ANGLES INBD SIDE NR 5. VENTRAL FRAME APB IAW SRM 53-01 FIG 2, SHT 4, 53-13-3, FIG 8, SHT 1&2, 51-10-3, & 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

FORWARD CARGO COMPARTMENT AT STA 674 LONG 26 LT HAS 2 ELONGATED HOLES. REPAIRED 2 ELONGATED HOLES IN FORWARD CARGO COMPARTMENT AT STA 674 L26L PER EA 486153-14 ON TRAVELER NR 2446N01553 FREEZE PLUGS FABRICATED AND INSTALLED ON TRAVELER 2446N01553 IAW DC-9-51-20-03-801-663A.

Part: SUPPORT — CRACKED (BS 753 RBL 44) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 753, RBL 44, VERTICAL T-ANGLE SUPPORT IS CRACKED AT BOTTOM OF ANGLE. REMOVED ANGLE FITTING IAW SRM 51-30-5. FABRICATED ANGLE IAW DWG 9923417 AND FABRICATED FITTING ON TRAVELER 2446N01382 IAW DWG 3925811. INSTALLED ANGLE AND FITTING IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: FLOORBEAM — CRACKED (BS 775 RBL 44) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 775, RBL 44, FLOORBEAM SUPPORT IS CRACKED AT BOTTOM OF ANGLE. REMOVED CRACKED FITTING, STA 775, RBL 44, LOCATED, DRILLED NEW FITTING, INSTALLED IAW SRM 51-10-4, 51-30-5, DWG 3925812.

Part: FRAME — CRACKED (BS 1292) · airframe 78,354 hrs · 77,526 cycles

AFT ACCESSORY CANTED FRAME 1292 AT APPROX L14R WEB HAS 1 EA HOLE. FOUND HOLE TO HAVE A CRACK TRIMMED OUT .5" DIA, HFEC INSP IAW NDT SPM 06-10-01.001. REPAIRED & INSTALLED DOUBLER IAW SRM 53-01, REQUIRED INSPECTION COMPLETED.

Part: FLOORBEAM — CHAFED (BS 237, RBL4-8) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 237, RBL 4 -RBL 8, FLOORBEAM CHAFED. BLENDED CHAFE IAW SRM 51-10-3, ORIG MAT .125 IAW SRM 51-10-1, FIG 22, PN 2777897 AND 51-13-2, ITEM 6. REMOVED .040 REMAINING .085 FOUND TO BE OUT OF LIMITS IAW SRM 53-05, FIG 20A. REPAIRED DAMAGED FLOORBEAM STA 237, RBL4 TO RBL8 IAW SRM 53-05, FIG 20A. REQUIRED INSP COMPLETED.

Part: FLOORBEAM — CRACKED (BS 775 LBL 44) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 775, LBL 44, FLOORBEAM SUPPORT IS CRACKED AT BOTTOM OF ANGLE. REMOVED CRACKED FITTING LOCATED DRILLED DEBURRED NEW FITTING & INSTALLED IAW DWG 392581241, SRM 51-10-4, 51-30-5, 51-30-2, & 51-30-1. REQUIRED INSPECTION COMPLETED.

Part: FRAME — DAMAGED (BS 389 L16R) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN STA 389, RT SIDE AT L16R FRAME HAS 1 EA HOLE. REMOVED DAMAGED PORTION OF FRAME IAW SRM 53-05, FIG 4. FABRICATED FILLER, REPAIR PLATE, REPAIR ANGLE TREATED AND PRIMED PARTS IAW SRM 51-10-3. INSTALLED FRAME REPAIR IAW SRM 51-30-2, 53-03, FIG 4. APPLIED CPC IAW SRM51-10-3. REQUIRED INSPECTION COMPLETED.

Part: FLOORBEAM — CORRODED (BS 200 RBL 2-20) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 200, RBL 2-20 FLOOR SUPPORT CORRODED. REMOVED CORROSION 100 PERCENT MAT LOSS. R & R WITH NEW FLOOR SUPPORT IAW SRM 51-30-5. CORRECTED.

Part: FLOORBEAM — CORRODED (STA 200 LBL1-21) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 200, BETWEEN LBL 1-21 FLOOR SUPPORT CORRODED. REMOVED CORROSION ON FLOOR SUPPORT STA 200, LBL1-21, ORG MAT .070 REMOVED .022" REMAINING. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT WITH NEW SUPPORT CORRECTED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN CABIN METAL SKIN FLOOR PANEL NR97 HAS CORROSION OTBD EDGE. REMOVED CORROSION IAW SRM 51-10-3. ORIGINAL MAT .020 REMOVED.004 REMAINING MAT .016 WITHIN LIMITS. TOOL NR A1-118057, DUE DATE 30 JULY 11. FOUND GAUGE TO BE OUT OF LIMITS. RECEIVED AND FABRICATED FILLER AND DOUBLER IAW SRM 53-05. DRILLED, LOCATED, DEBURRED IAW SRM 51-10-4. INSTALLED FLOOR PANEL IAW SRM 51-31-1. REQUIRED INSP COMPLETED.

Part: CUSP WEB — DAMAGED (BS 256-275) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN LT SIDE CUSP WEB CTR LIGHTNING HOLE HAS 1EA GOUGE BETWEEN BS 256 AND BS 275, L18L. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND DWG SG09530019. REQUIRED INSP COMPLETED.

Part: LONGERON — CRACKED (BS 1136 L16R) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN AFT SIDE OF STA 1136, L16R CRACKED TOP LEG. REMOVED, FABRICATED, & INSTALLED NEW SPLICE W/FASTENERS IAW SRM 53-02, FIG 18 AND 51-30-5. REQUIRED INSP COMPLETED.

Part: INTERCOSTAL — CRACKED (BS 120) · airframe 78,354 hrs · 77,526 cycles

E & E COMPT STA 120 LT LONG 29, INTERCOSTAL CRACKED CPCP TASK NR REMOVED, FAB, & INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2 AND 51-10-5.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 78,354 hrs · 47,739 cycles

MAIN PASSENGER CABIN STA 160-STA 200, RBL 44, FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM SUPPORT. FOUND TO BE OUT OF LIMITS. REMOVED ORIGINAL FLOOR SUPPORT. FABRICATED & INSTALLED NEW SUPPORT WET IAW SRM 51-10-03, 53-13-01 FIG 11, 53-01, FIG 1, 51-10-02, 51-10-03 AND 51-30-05.

Part: SUPPORT — CRACKED (BS 773) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 773, RBL 44-55 TANK TO WEB SUPPORT IS CRACKED APPROX 3 INCHES. FABRICATED AND INSTALLED WEB SUPPORT AND FITTING IAW SRM 51-30-5 AND DWG 5910464. REQUIRED INSP COMPLETED.

Part: FRAME — CRACKED (BS 617 L24R) · airframe 78,354 hrs · 77,526 cycles

FWD CARGO COMPARTMENT, STA 617 FRAME JUST ABOVE L24R ATTACH CLIP TO ANGLE CRACKED. REMOVED, FAB, & INSTALLED A NEW CLIP IAW SRM 51-10-3, 51-30-1, 51-30-2. DWG 5956092. ITEM 72 W. SMART 114251, 469380, 14 JAN 11 P-180. REQUIRED INSP COMPLETED.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 78,354 hrs · 77,526 cycles

NLG WHEEL WELL, STA 37, BRACE ASSY ON FWD BULKHEAD HAS A CRACKED U-CHANNEL AT RBL 5. R & R U-CHANNEL RT PN 9911500-188 IAW DWG PN 9911500. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CRACKED (BS 775 RBL 22) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 775, RBL 22-45 FLOOR PANEL SUPPORT IS CRACKED. REMOVED CRACKED BRACKET AND ATTACH ANGLE IAW SRM 51-30-2. FABRICATED & INSTALLED IAW SRM 51-30-45 AND 51-30-2. REQUIRED INSP COMPLETED.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 78,354 hrs · 77,526 cycles

NLG WHEEL WELL STA 37, BRACE ASSY ON FWD BULKHEAD HAS A CRACKED U-CHANNEL AT LBL 5. R & R U-CHANNEL LT PN 9911500-187 IAW DWG PN 9911500. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CRACKED (BS 753 BL 0) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 753, BL 0, FLOOR PANEL SUPPORT IS CRACKED AT UNDER SIDE. REMOVED FLOOR PANEL SUPPORT, STA 671-794 IAW SRM 51-30-5 & 51-30-1. INSTALLED FLOOR SUPPORT IAW SRM 51-30-1. REQUIRED INSP COMPLETED.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 78,354 hrs · 77,526 cycles

NOSE WHEEL WELL STA 37 RT SIDE SUPPORT AT FWD BULKHEAD IS CRACKED APPROX .2500 INCH. R & R WEB PN 9911500-183 IAW DWG PN 9911500. REQUIRED INSP COMPLETED.

Part: CUSP WEB — CORRODED (BS 832-851) · airframe 78,354 hrs · 77,526 cycles

MAIN PAX CABIN RT SIDE CUSP WEB HAS CORROSION ON UPPER SURFACE BETWEEN BS 832 AND BS 851, RBL 57 INCHES. TASK 58-53309. REMOVED CORROSION AND REPAIRED CUSP WEB AT STA 851, RBL 57 IAW DWG NR SG09530019, CPCP 5100-01570-01A. REQUIRED INSP COMPLETED BY Q-983 451017.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,354 hrs · 77,526 cycles

NOSE WHEEL WELL STA 37 LT SIDE SUPPORT AT FWD BULKHEAD IS CRACKED APPROX .2500 INCH. R & R WEB PN 9911500-183 IAW DWG 9911500. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CRACKED (BS 775 LBL 16) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 775, LBL 16 FLOOR PANEL SUPPORT IS CRACKED. REMOVED, FABRICATED, AND INSTALLED MAIN PASSENGER CABIN STA 775, LBL16, SUPPORT. SEALED AND INSTALLED IAW SRM 51-20,51-30-2.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 78,354 hrs · 77,526 cycles

MAIN METAL SKIN FLOOR PANEL NR79 AFT OTBD CORNER BROKEN OFF. NO CPCP TASK NR. CUT OUT DAMAGE IAW SRM 53-01, FIG 4. FABRICATED & INSTALLED DOUBLER AND FILLER IAW SRM 51-30-02. REQUIRED INSP COMPLETED.

Part: FLOOR SUPPORT — CORRODED (STA 232-294) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 232-STA 294, BL 0 FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, SHEET. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. DRILLED/DEBURRED NEW FLOOR SUPPORT IAW SRM 51-10-4. INSTALLED WET IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 200 RBL 43) · airframe 78,354 hrs · 77,526 cycles

MAIN PASSENGER CABIN STA 200, RBL 43, FLOOR SUPPORT CORRODED. FLOOR SUPPORT AT STA 200, RBL 43 CORRODED BEYOND LIMITS IAW SRM 53-01, FIG 1. R & R FLOOR SUPPORT ANGLE IAW SRM 51-30-5.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 77,118 hrs · 76,449 cycles

DURING LINE CHECK FOUND DAMAGE TO FRAME AT BS1190 RT SIDE BELOW AUG VALVE. REPAIRED IAW ERA 482388-14, SRM 51-20-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,634 hrs · 76,030 cycles

DURING LINE CHECK, MX FOUND THAT THE CEILING EMERGENCY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,436 hrs · 75,864 cycles

FLIGHT CREW DISCOVERED THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,169 hrs · 74,788 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.

Part: WIRE — BROKEN (CABIN) · airframe 73,820 hrs · 73,583 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE RED EMERGENCY LIGHT AT SEAT 13D IS INOPERATIVE DUE TO BROKEN WIRES IN THE OUTER SEAT TRACK. MAINTENANCE REPAIRED BROKEN WIRES AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (S)

Part: UNKNOWN — ODOR (CABIN) · airframe 72,825 hrs · 72,706 cycles

A STRONG SMELL OF JET FUEL CIRCULATED ABOUT THE CABIN AND COCKPIT. CREW SWITCHED FROM APU SUPPLIED AIR TO ENGINE AIR AND FUMES REMAINED/REOCCURRED. COCKPIT CREW DONNED OXYGEN MASKS FOR DURATION OF FLIGHT. CREW NOTED THAT THE FUMES WERE STRONG ENOUGH TO CAUSE THEM HEADACHES. LANDING IN DTW WAS NORMAL AND PASSENGERS DEPLANED NORMALLY. NO EVIDENCE OF ANY FUEL LEAKING FROM EITHER POWERPLANT, APU, FUEL TANKS, OR FUEL LINES. THE AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 60,930 hrs · 61,898 cycles

DURING MCK IN ATL, CORROSION WAS FOUND ON THE LT SIDE MLG FIXED SIDE BRACE LUG. REPAIRED PER EA 98-185385.

Part: TIRE — FAILED (MLG)

DURING TAKEOFF AT MDW, THE LEFT OUTBOARD NR 1 MAIN WHEEL AND TIRE ASSEMBLY DEPARTED THE AIRCRAFT. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FLIGHT CREW DECLARED AN EMERGENCY. MAITNENANCE REPLACED THE LEFT BOTTOM MAIN LANDING GEAR STRUT AND NR 1 MAIN WHEEL ANTI-SKID TRANSDUCER. INSPECTED HYDRAULIC LINES AND LEFT LANDING GEAR ANTI-SKID WIRING AND REPLACED NR 1 AND NR 2 MAIN TIRE AND BRAKE ASSEMBLIES. OPERATIONAL CHECK OK.

Part: TIRE — FAILED (NR 4 MAIN)

DURING TAKEOFF AT ORD, NR 4 MAIN TIRE BLEW AT APPROXIMATELY 140 KNOTS CAUSING EXCESSIVE VIBRATION. FLIGHT WAS CONTINUED TO DESTINATION. CREW DECLARED A YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 4 MAIN TIRE. ALSO, REPAIRED DAMAGE TO AXLE, FLYING DOOR, FLAP AND FUSELAGE. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FAILED (RIGHT)

DURING CRUISE AT 33,000 FEET, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DUE TO CONTAINED FAILURE.

Part: CLAMP — LOOSE (LT ACM)

DURING CLIMBOUT, THE TAIL COMPARTMENT HIGH TEMPERATURE INDICATION LIGHT ILLUMINATED 30 SECONDS AFTER TAIL DEICE WAS SELECTED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. RETURNED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AND REPLACED A LOOSE CLAMP AT THE AFT SECTION, LEFT SIDE, AIR CYCLE MACHINE, AND INSPECTED TAIL COMPARTMENT DUCTING. OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — FAILED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND AFT INTERIOR EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.

Part: BULKHEAD SKIN — CRACKED (AFT PRESS BLKHD)

DURING ROUTINE MAINTENANCE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE LOWER LEFT CORNER AT THE DOOR JAMB. REPAIRED PER EA 98-152271.

Part: SEAL — FAILED (GALLEY DOOR)

DURING TAKEOFF, HEARD BANGING NOISE OUTSIDE OF GALLEY DOOR. FLIGHT RETURNED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. FOUND GALLEY DOOR TRIM AESTHETIC SEAL HANGING OUTSIDE OF GALLEY DOOR. REMOVED TORN SECTION OF SEAL.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN FIRST CLASS AND GALLEY EXIT DOOR SIGNS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK GOOD.

Part: PRESS PANEL — CRACKED (BS 105)

DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL, RIGHT SIDE AT INBOARD BULKHEAD STIFFENER FS 105. REPAIRED PER EA 98-151600.

Part: PRESSURE PANEL — CRACKED (BS 83)

DURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83, RIGHT SIDE. REPAIRED PER EA 98-151594.

Part: PRESSURE PANEL — CRACKED (BS 105)

DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 105, LEFT INBAORD AND OUTBOARD STIFFENERS. REPAIRED PER EA 98-151600.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND ROWS 1-4 EMERGENCY PATHWAY LIGHTS INOPERATIVE. REPAIRED OPEN WIRE. OPERATIONAL CHECK OK.

Part: MICROPHONE JACK — FAILED (LT COCKPIT)

AFTER TAKEOFF, CATPAIN'S VHF TRANSMITTER BECAME INOPERATIVE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND CAPTAIN'S MICROPHONE JACK INTERMITTENT. REPLACED MICROPHONE JACK, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING PERIODIC CHECK, LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS AND THIRD SECTION OF FLOOR PROXIMITY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY AND OPERATIONAL CHECK OK.

Part: EEL WIRES — BROKEN (CABIN)

DURING PERIODIC CHECK, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SECTION ONE VERY DIM. REPAIRED BROKEN WIRES AND OPERATIONAL CHECK OK.

Part: FLOOR SUPPORT — CRACKED (FS 636-737)

DURING H-CHECK, FOUND A CRACK ON THE FUSELAGE FLOOR SUPPORT VERTICAL WEB, FS 636-737. REPAIRED SUPPORT (P/N 5910740-13) PER EA 98-102007.

Part: FITTING — CORRODED (FS 1167)

DURING H-CHECK, FOUND CORROSION IN THE LONGERON 22R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30.

Part: DOOR PAN — CRACKED (EMER EXIT DOOR)

DURING H-CHECK, FOUND CRACKS IN (2) EMERGENCY EXIT DOOR PANS (RIGHT AFT, LEFT FORWARD), ONE EACH AT THE UPPER FORWARD AND AFT DOOR STOPS. REPAIRED THE PANS (P/N 5913195-1) PER EAS 98-103345 AND -103347.

Part: RELEASE MECH — OUT OF ADJUST (TAILCONE)

DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LEFT LATCH DURING THE DROP CHECK. ADJUSTED THE CLIPS AND MODIFIED THE TAILCONE RELEASE CABLE LOCKING FITTING PER CITEXT 09-5353-1-0003. CHECKED OK.

Part: RELEASE MECH — OUT OF ADJUST (TAILCONE)

DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE TAILCONE, CHECKED OK.

Part: DOOR CABLE — FAILED (LT MLG)

EN ROUTE BIS-MSP, MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT CONTINUED TO DESTINATION AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR SEQUENCING PUSH/PULL CABLE. ALSO, REPLACED TORQUE TUBE LOWER BEARINGS, DOOR SKIDS, AND INSTALLED DOUBLERS ON BOTH DOORS. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE.

Part: WINDOW SEAL — LOOSE (LT EYEBROW)

DURING CLIMB JAX-MEM THE FLIGHT CREW HEARD A LOUD FLAPPING NOISE NEAR THE CAPTAIN'S EYEBROW WINDOW. MAINTENANCE CONTROL WAS NOTIFIED AND THE AIRCRAFT RETURNED TO JAX WITHOUT FURTHER INCIDENT. FOUND LOOSE SEALANT AT THE AFT SIDE OF THE CAPTAIN'S EYEBROW WINDOW. TRIMMED SEALANT AND DEFERRED REPAIR. INSPECTED THE NR 1 ENGINE INLET. CHECKED OK.