N991DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,768 hrs · 52,248 cycles

LT AND RT AFT OVERWING EXIT UPPER EXIT LIGHTS INOP. REF MD88 WDM 33-51-12 B4105 BATTERY PACK (982729 SSFD) REPLACED B5-105 BATTERY PACK PER MD88 AMM 33-53. (LP6406268)

Part: SKIN — CRACKED (RT WING) · airframe 71,768 hrs · 52,248 cycles

CRACK IN UPPER RIGHT WING. INSTALLED TAPE AT DAMAGE 613056 REMOVED TAPE AND INSTALLED PERMANENT REPAIR PER MD88 SRM 51-90-00. (LP6406264)

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 71,432 hrs · 51,911 cycles

STALL INDICATION FAILURE MESSAGE ON EOAP ON GROUND. WOULD NOT CLEAR. MULTIPLE LOTS STALL WARN 2 CORD ON RESET BUT COMP HAS ELECT SMELL & TEST SW STICKS INTO IN NORMAL. R&R SAME. OPS NORMAL. REF AIM 34_19. COMPUTER, STALL OFF 88-3415-9-0001 S/N01946. (LP4623602)

Part: TIRE — FAILED (LT MLG) · airframe 71,112 hrs · 51,640 cycles

SHIP 0991 - THE CREW RETURNED THE AIRCRAFT TO ATL DUE TO A #2 TIRE FAILURE DURING TAKE OFF. GEAR WAS NOT RETRACTED BUT SHOWED A "LEFT GAR UNSAFE" MESSAGE. THE AIRCRAFT LANDED BELOW MAXIMUM WEIGHT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 AND #2 MAIN TIRE ASSEMBLIES, THE #1 ENGINE LOWER COWL, AND ALSO REPAIRED LEFT GEAR DOOR LOCK SENSOR AND WIRING. (LP #5163244)

Part: APU — MALFUNCTIONED (APU BAY) · airframe 70,814 hrs · 51,377 cycles

APU FAILED DURING RIGHT ENG START. SMOKE APPEARED IN THE AFT CABIN AND SOON DISIPATED. INSTALLED APU REF CARDS 4900-2121, 4900-4573, 4900-7165, 4900-4169,. C/W NO GO ODI PREVENTION ATA 4999, ATA 2172 PER CARDS 4900-1185, 2121,2368, 7100-2619. APU OPN NORMAL. (LP5721132)

Part: DEFLECTOR — MISSING (NLG) · airframe 70,234 hrs · 50,853 cycles

NOSE LANDING GEAR DEBRIS DEFLECTOR LEFT AND RIGHT AFT NOSE DEBRIS DEFLECTOR MISSING. REPLACED SPRAY DEFLECTOR LT AND RT AFT DEFLECTORS PER AMM 32-20. (LP0956812)

Part: WIRE — BURNED (COFFEEMAKER) · airframe 70,188 hrs · 50,816 cycles

DUE TO REPORTS FROM F/A OF SMOKE AND ODOR, PERFORM ODI ATA 2172 SMOKE FUME OF UNKNOWN SOURCE. C/W NO GO ODI W/C 2120-2367. FOUND WIRES ON BACK OF NO.2 COFFEEMAKER BY L-1 DOOR BURNT AND C/B POPPED. REPLACED COFFEMAKER PER MD88 AMM 25-36. LK AND OPS CK GOOD. SEE LOG NO. 4885180. (LP0952604)

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 70,188 hrs · 50,816 cycles

COFFEMAKER NO.2 C/B POPPED. F/A'S BRIEFLY SMELLED SMOKE WHICH DISAPPATED QUICKLY WITH NO SMOKE. SEE LOG NO. 0952604. REPLACED COFFEMAKER NO.2 BY L-1 DOOR PER MD88 AMM 25-36. LK AND OPS CK GOOD. (LP4885180)

Part: RUDDER — DAMAGED (TAIL) · airframe 70,011 hrs · 50,670 cycles

DURING PAINT VISIT FOUND RUDDER TO HAVE DAMAGED MISSING FLAMESPRAY . RUDDER P/N SN5955501-1 S/N 49321, STOCK NUMBER 88-5554-9-0005, FTN 34R21A. REMOVED RUDDER P/N SN5955501-1, S/N 49321, STK NUMBER 88-5554-9-0005, FTN 34R21A, FROM A/C 991. INSTALLED RUDDER P/N 5955501-1, S/N 558, STK NUMBER 88-5554-9-0001, FTN 47RRM3 ON A/C 991 PER WORKCARD 2720-4421 FORECAST NUMBER 88-0511-8-9010, ERA 574680-14 REV ORIG AND AMM 27-20-01 PAGEBLOCK 401.. C/W REQUIRED RII INSPECTIONS ALL SAFETIES AND OPS CHECK GOOD. (LP5215055)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 69,967 hrs · 50,630 cycles

AFT LAV FO SIDE SMOKE DETECTOR STARTED BEEPING AT CRUISE NO SMOKE DETECTED TRASH CAN INSPECTED NO EVEDANCE OF SMOKE OR FIRE. REPLACED AFT RT LAV SMOKE DETECTOR PER AMM 26-13-00 PG BLK 401. (LP5215018)

Part: TIRE — LOOSE (NR 1 MLG) · airframe 69,070 hrs · 49,861 cycles

NR 1 MLG TIRE ASSY LOOSE. R & R THE NR 1 MLG WHEEL & TIRE ASSY IAW AMM 32-41.

Part: SLIDE — LOOSE (TAILCONE) · airframe 68,197 hrs · 49,161 cycles

TAILCONE SLIDE LOOSE IN CONTAINER. REPLACED THE TAILCONE SLIDE IAW AMDS 2561-4001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,521 hrs · 48,676 cycles

EMERGENCY LIGHT CEILING TAIL SECTION INOP. REPLACED D CELL BATTERIES IN AFT RT LAV BATTERY PACK. OPERATIONAL CHECKS GOOD P/N AD4002P.

Part: CAP — MISSING (APU OIL) · airframe 66,360 hrs · 47,767 cycles

THE FLIGHT CREW REPORTED HAZE AND SMOKE IN CABIN DURING CLIMB WITH BOTH AFT LAVATORY SMOKE DETECTORS SOUNDING. AN AIR TURN BACK TO DEPARTURE WAS ACCOMPLISHED. MAINTENANCE FOUND AN APU OIL LEAK WHICH RESULTED FROM THE CAP BEING LEFT OFF. THE APU WAS REPLACED DUE TO OIL CONTAMINATION. THE LEFT AND RIGHT ACM, LEFT AND RIGHT PRIMARY AND SECONDARY HEAT EXCHANGERS, AND THE APU LOAD CONTROL VALVE WERE REPLACED. THE CROSSOVER DUCT AND CROSSFEED VALVES WERE INSPECTED FOR CONTAMINATION AND CLEANED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 66,102 hrs · 47,575 cycles

RIGHT WING, INBOARD AFT FLAP, REMOVABLE PANEL DENTED AND CRACKED. COMPLIED WITH A PERMANAT REPAIR IAW ERA557696-14, REV ORIG. REMOVED AND REPLACED THE PANEL IAW DWG 5930479.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,204 hrs · 46,211 cycles

CEILING EMERGENCY LIGHTS OUT AT ROWS 23, 24, AND 25. REPLACED BATTERIES IN POWER SUPPLY UNIT AT ROW 24E, SN-29942. REF AMM 33-53-00-401. OPS CHECK OK.

Part: SKIN — DENTED (LE SLAT) · airframe 63,911 hrs · 45,999 cycles

RT SLAT DENTED ON L/E ON NR 1 SLAT AT XFS 100. REPLACED RT NR 1 SLAT IAW CARD 2700-4224 RH-01.

Part: STRUCTURE — CORRODED (BS 1155) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERCOSTAL FUSELAGE SKIN BS 1155 BETWEEN LONG 29LT- 29RT AT C3. AREA WAS REPAIRED IAW 543161-14, REV ORIGINAL AND ETI- 88-16-073, REV 3.

Part: LANYARD — TORN (TAILCONE) · airframe 62,966 hrs · 45,352 cycles

MAINTENANCE FOUND YELLOW KEVLAR CORD TORN DURING THE TAILCONE KEVLAR CABLE INSPECTION. THE CABLE WAS REPLACED.

Part: SKIN — CORRODED (BS 689) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERNAL SKIN BS 689 BETWEEN, LONG 30 TO 29 RT AT MID CARGO COMPARTMENT. INTERNAL SKIN WAS REPAIRED IAW ETI-8816-084, REV 2 AND ERA 543173-14, REV ORIGINAL.

Part: STATIC PORT — DAMAGED (LEFT) · airframe 62,966 hrs · 45,352 cycles

OUT OF LIMITS MISMATCH OF LT ALTERNATE STATIC PORT. DUE TO EXCESSIVE DAMAGE AREA WAS REPAIRED IAW ETI-88-16-083 AND ERA 543168-14, REV ORIGINAL.

Part: SKIN — CORRODED (BS 689) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERNAL SKIN BS 689 BETWEEN LONGERON 30 TO 29 RT AT MID CARGO COMPARTMENT. INTERNAL SKIN WAS REPAIRED IAW ETI-88-16-084, REV 2 AND ERA 543173-14, REV. ORIG WITHIN EVERY 8,000 CYCLES AFTER ACCOMPLISHMENT OF ERA 543173-14, REV ORIG SECTION I REPAIR, PERFORM GENERAL VISUAL INSPECTION OF SECTION I REPAIR IAW ERA 543173-14, REV ORIGINAL SECTION II.

Part: RIB — CRACKED (RT WING) · airframe 62,966 hrs · 45,352 cycles

CRACKED RIB BS XOS.553 AT RT WING FIXED L/E IN REF CARD 89, ZONE 10. RIB WAS REPAIRED IAW ER/A 543160-14 AND SRM 51-10-2, 51-10-3 PAR 14 AND 21, SRM 57-06A.

Part: SKIN — DENTED (BS 579) · airframe 62,966 hrs · 45,352 cycles

DENT ON PREVIOUS REPAIR EXTERNAL SKIN AT BS 579 BETWEEN LONG 28 AND 30 RT. DUE TO EXCESSIVE DENTS AREA WILL BE REPAIR IAW SRM 53-04-1, PAR 7. C, 5, A, 1 AND ER/A 543172-14. REPAIR WAS ACCOMPLISHED IAW SRM 51-30-2, 51-30-5, 51-10-3 AND ER/A 543172-14, REV ORIGINAL.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON FWD SERVICE DOOR FRAME LOWER CUSP ANGLE. THE CUSP ANGLE WAS REPAIRED IAW SRM 53-05, FIG 18 AND ETI 88-16-056, REV 1 AND ER/A 543155-14, REV ORIGINAL.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 62,966 hrs · 45,352 cycles

DENTS ON UPPER SURFACE LT OTBD FLAP INBD GUIDE VANE AT BS XV1=190, XV1=187, XV1=160 AND XV1=161. DENTS XVI=160 AND XVI=161 WERE REPAIRED UNDER ERA 543162-14, REV. A.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 62,966 hrs · 45,352 cycles

CRACK ON PREVIOUS REPAIR FWD UPPER CORNER ON ACCESS NR 6301A AT VERTICAL STABILIZER. REPAIR WAS ACCOMPLISHED IAW ETI-88-16-089 R1 & ER/A 543178-14 REV ORIGINAL.

Part: RIB — CRACKED (RT WING) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RIB AND CLIP AT BS XFS=309 AT RT WING FIXED L/E. CRACK RIB AND CLIP WERE REPLACED IAW SRM 51-30-5, 51-30-2 AND DGW 9937588.

Part: HINGE FITTING — DAMAGED (LT NACELLE) · airframe 62,966 hrs · 45,352 cycles

ELONGATED HOLES ON HINGE FITTING YN=83, 2 EA, YN=111, 2EA, YN=154, 1EA, YN=184, 1EA AND YN=214, 1EA AT LT NACELLE APRON. FITTING BS YN=83 LWR/UPPER, YN=111 UPPER, YN=154 UPPER, YN=214 UPPER WERE REPAIRED IAW CMM 71-10-10 AND ERA 228793-14 AND FITTING BS YN=184 LWR WAS REPAIRED IAW EA 09-372728-14, REV B AND FITTING BS YN=111 LWR OF APRON LT WAS REPLACED DUE TO EXCESSIVE DAMAGE FOR A NEW FITTING IAW CMM 71-10-10.

Part: RIB — CRACKED (LT WING) · airframe 62,966 hrs · 45,352 cycles

CRACKED RIB BS XOS=455 AT LT WING FIXED L/E IN REF CARD 55, ZONE 10, CARD 172, ZONE 10. RIB WAS REPAIRED IAW SRM 51-30-2, 51-30-5, ETI 88-16-085 R2 AND ER/A 543174-14, REV ORIGINAL.

Part: SKIN — CRACKED (RT WING) · airframe 62,966 hrs · 45,352 cycles

SIX CRACKS WERE FOUND ON HOLES BETWEEN STR 12 AND STR 15: XRS=200; XRS=201; XRS=202; XRS=203; XRS=205, FWD ROW AND XRS=198, AFT ROW; AT THE RT LOWER WING SKIN ACCESS CUTOUT. REPAIR ON HOLES WAS PERFORMED IAW ER/A 543185-14 AD, REV ORIGINAL. THIS REPAIR IS LIMITED TO 67.00 TOTAL CYCLES ONLY IAW ER/A 543185-14AD, REV ORIGINAL SEC II AND WILL BE MONITORED UNDER LOG 2375110.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 62,966 hrs · 45,352 cycles

THREE CRACKS WERE FOUND ON HOLES BETWEEN STR 12 AND STR 15: XRS=199, XRS=203, FWD ROW AND XRS=198 AFT ROW; AT THE LT LOWER WING SKIN ACCESS CUTOUT. REPAIR ON HOLES WAS PERFORMED IAW ER/A 543185-14AD, REV ORIGINAL. THIS REPAIR IS LIMITED TO 67,000 CYCLES ONLY IAW ER/A 543185-14AD, REV ORIGINAL SEC II AND WILL BE MONITORED UNDER LOG 2375110.

Part: SKIN — CRACKED (BS 194-203) · airframe 62,966 hrs · 45,352 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN BETWEEN BS 194-203 AND LONGERON 16-18, RT WITH IDTAG: N991DL, SRM 53-05, P 02-08-10. REPAIR WAS FOUND AND MADE IAW ERA NR 543128-14AD, REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL CYCLES ER/A REV IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. THIS RESTRICTIONS WILL BE FOLLOWED.

Part: CUSP WEB — CRACKED (BS 218) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RT CUPS WEB IN BS Y=218 X= -45, LOWERSIDE AT CABIN PAX. CUPS WEB WAS REPLACED IAW SRM 51-30-2, DWG 9930538-39, REV BW.

Part: CHANNEL — CRACKED · airframe 62,966 hrs · 45,352 cycles

CRACKED W CHANNEL ON FLOOR PANEL 886C AT CABIN PAX. W CHANNEL ON FLOOR PANEL 886C AT CABIN PAX WAS REPLACED IAW DWG 9936639, REV P, SRM 51-30-1.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,966 hrs · 45,352 cycles

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

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACKED FWD SERVICE DOOR JAMB PAN AFT LOWER CORNER IN REF CARD 277 ZONE 201. CRACKED FWD SERVICE DOOR JAM PAN WAS REPAIRED IAW SRM 53-05, FIG 55 AND ER/A N. 543171-14, REV ORIG.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON FORWARD SERVICE DOOR JAMB CUSP ANGLE AFT LOWER EDGE. DUE TO EXCESSIVE CORROSION DOOR JAMB CUSP ANGLE WAS REPAIRED IAW SRM 53-05, FIG 55.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,966 hrs · 45,352 cycles

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

Part: CARGO TRACK — CORRODED (BS 1003-1220) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT CARGO TRACK FROM BS 1003 - 1220 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4 .

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON CARGO TRACK RT SIDE FROM BS 1003 - 1155 IN AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, SRM 51-30-1 AND DWG 5956705 REV AY.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 62,966 hrs · 45,352 cycles

PUNCTURED FLOOR PANEL IN PAX CABIN. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,966 hrs · 45,352 cycles

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

Part: VANE — WORN (RT WING TE FLAP) · airframe 62,966 hrs · 45,352 cycles

WEAR ON L/E AT RT OTBD FLAP INBD GUIDE VANE BS XV1=162.5. DAMAGE AT OTBD FLAP INBD GUIDE VANE RT WAS REPAIRED IAW SRM 57-03D, PARR 11 AND CARD 2000-8149-14, 1966324.

Part: HINGE — WORN (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

FREE PLAY ON FWD AND AFT HINGE AT FWD CARGO DOOR. AFT HINGE OF FWD CARGO DOOR WAS REPAIRED IAW ER/A 497387-14 AND INSTALLED IAW AMM 52-31-02. FWD HINGE WAS REPLACED AND NEW ONE WAS INSTALLED IAW AMM 52-31-02. FWD CARGO DOOR WILL BE INSTALLED INTO CARD 5231-4386.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CARGO TRACK FROM BS 1212 - 1322 AT AFT CARGO COMPARTMENT. THE CARGOTRACK WAS REPLACED IAW SRM 51-30-1, SRM 51-30-2, AND DWG 5956705, REV.

Part: LONGERON — CORRODED (BS 256-275) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LONGERON 22RT FROM BS 256-BS 275 IN FWD CARGO COMPARTMENT. LONGERON SECTION DAMAGE WAS R & R IAW 53-02, FIG 18.

Part: DOOR FRAME — CORRODED (BS 665-690) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON MID CARGO COMPARTMENT LOWER FWD DOOR JAMB BEAM BETWEEN BS 665-690. JAMB BEAM WAS REPAIR IAW ERA 543157-14.

Part: LONGERON SPLICE — CORRODED (BS 256-275) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON SPLICE OF LONG 22 RT BETWEEN BS 256-275 AT RT TUNNEL OF FWD CARGO COMPARTMENT. SPLICE WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5.

Part: CUSP WEB — PUNCTURED (BS 1041-1061) · airframe 62,966 hrs · 45,352 cycles

PUNCTURE ON CUSP WEB BETWEEN BS 1041 - 1060 AND -X=60 TO -X=54 AT CABIN PASSENGER DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A-8, SHEET 1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION COUNTERSINK HOLES ON SECONDARY ACCESS DOOR . CORROSION REMOVED. FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES. REPLACED.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,966 hrs · 45,352 cycles

CRACK ON SKIN NEXT TO HOLD AT LT FLOOR PANEL NR 389A. FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4 AND 51-10-3 PAR 14 AND 21.

Part: SCOOP — CRACKED (VERTICAL STAB) · airframe 62,966 hrs · 45,352 cycles

CRACK ON VERTICAL STABILIZER RAM AIR SCOOP LT EDGE. CRACK ON VERTICAL STABILIZER RAM AIR SCOPE LT EDGE WAS REPAIRED, WELDED IAW ER/A 420329-14MA, REV C. THE RIVETS ON NEW FILLER WILL BE INSTALL WHIT NR 20000099368, CARD 3, ZONE 63.

Part: VANE — WORN (RT WING TE FLAP) · airframe 62,966 hrs · 45,352 cycles

WEAR ON L/E RT MID GUIDE VANE OTBD FLAP BS XV2=264. WEAR ON L/E RT MID GUIDE VANE OTBD FLAP STA XV2=264 WAS REPAIRED IAW SRM 57-03D, PARR II AND CARD 2000-8149-02, 1882436.

Part: PAN — DAMAGED (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

ELONGATED HOLES ON INTERNAL PAN APPOXIMATELY 381, HOLES OF FWD HINGE, AT FWD CARGO COMPARTMENT DOOR. ELONGATED AREA WAS REPAIRED AND INSTALLED A BUSHING IAW ERA 461029-14, REV A, THE INTERNAL FITTING WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — DENTED (LT WING) · airframe 62,966 hrs · 45,352 cycles

DENT ON OTBD EDGE AT LT WING TIP. DENT AND CRACKS ON OTBD EDGE AT LT WING TIP, WAS REPAIRED IAW EA 09-478904-14 MA, REV ORIGINAL AND AREA WAS TREATED IAW PS 900-2-4-1, N02.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 62,966 hrs · 45,352 cycles

DENTS ON UPPER SURFACE BETWEEN BS XOVI=65, TOXOVI=72 AT LT INBD FLAP OTBD GUIDE VANE. DOUBLER WAS REPLACED IAW DWG 5930495, REV N.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON AFT LOWER SIDE INNER PAN PROJECTION OF BEAM NR 1 AT MID CARGO COMPARTMENT DOOR. PAN DOOR L2 WAS REPAIRED IAW ER/A 533156-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 598 AND 617 BETWEEN X=-54 AND X=-60 AT CABIN PASSENGER CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-7, SHEET 1.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 62,966 hrs · 45,352 cycles

CRACK ON CHANNEL AT FLOOR PANELS 927E AND 826G MAIN CABIN. CRACKS WERE STOPPED DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-05, 51-30-02.

Part: CUSP WEB — PUNCTURED (BS 1018) · airframe 62,966 hrs · 45,352 cycles

PUNCTURE ON LT CUSP WEB BS 1018 X=53 AT CABIN PAX. TRACK WAS REMOVED; DAMAGE WAS REMOVED. HFEC INSPECTION WAS PERFORMED AND NO CRACK FOUND; DOUBLER REPAIR WAS FABRICATED, TREATED, PAINTED AND INSTALLED. CIC WAS APPLIED AND SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIG 131A-2, SRM 51-10-3, PAR 14, 21, 38 SRM 51-30-2 AND 51-30-1.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 62,966 hrs · 45,352 cycles

CRACKED CHANNEL OF FLOOR PANEL 256E, 389G, 313E, 465E. DOUBLERS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-02, 51-10-03.

Part: FLOOR SUPPORT — CRACKED (PAX CABIN) · airframe 62,966 hrs · 45,352 cycles

CRACK ON CHANNEL AT FLOOR PANELS 256A, 769G, 465E CABIN PASSENGER CRACK WERE STOPPED, DOUBLERS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, 51-10-03, 51-30-02.

Part: MOUNT — CORRODED (ENGINE) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORRODED AFT BORES ON LT YOKE AT LT ENGINE. DAMAGE ON UPPER HOLE WAS REMOVED IAW DWG 5935710 AND HOLE WAS MEASURED WITH ID 01.2505. THEREFORE WITHIN LIMITS IAW DWG 5935710, LOWER HOLE WAS REWORKED IAW AMM 71-20-03-201, TABLE 201 WITH FINAL ID 0 1.271. THEREFORE OUT OF LIMITS IAW DWG 5935710, YOKE WAS REPLACED AND UNDER NRC2.

Part: FLOOR SUPPORT — BROKEN (NOT REPORTED) · airframe 62,966 hrs · 45,352 cycles

BROKEN CHANNEL AT LT FLOOR PANEL NR 617A. DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-03, 51-30-02.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 62,966 hrs · 45,352 cycles

CRACK ON CHANNEL AT LT FLOOR PANEL NR 389A. CRACK STOPPED DRILL, DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131, 51-30-02.

Part: DUCT — CRACKED · airframe 62,966 hrs · 45,352 cycles

CRACKS ON Y DUCT, UPPER SETTLEMENT AREA, 1 EA LUGS, 2 EA AND NEAR OF FLANGE 1EA. CRACKS ON Y DUCT WERE REPAIRED, WELDED) IAW SOPM 20-10-19 AND ERA 503276-11 MA REV C AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. FPI WAS ACCOMPLISHED ON "Y" DUCT, NO CRACKS FOUND IAW ER/A 503276-14MA, REV C.

Part: PAN — DAMAGED (BS 1212) · airframe 62,966 hrs · 45,352 cycles

ELONGATED HOLE ON INBD PAN AT BS 1212 BETWEEN BEAMS 2 AND 3 AT C3 DOOR. PAN AT BS 1212 BETWEEN BEAM 2 AND 3 WAS REPAIRED IAW ER/A 543152-14, REV ORIGINAL.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,966 hrs · 45,352 cycles

CRACKED RIB BS ZFS= 36.5 LT SIDE AT VERTICAL STABILIZER FRONT SPAR. RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3, PAR 14 AND 21 AND DWG 9911883, REV J.

Part: CUSP WEB — CORRODED (BS 1103-1169) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BS 1162 TO 1169, 1149 AND 1150, BS 1120 AND 1131, 1108 TO 1117, 1099, 1103 BETWEEN X=-60 AND X=-54 AT PAX CAB. RT CUSP WEB ON STA 1098-1174, X=-54 WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, SRM 10-10-3 PAR 14, 21 SRM 53-05, AND DWG 9930612, REV OG.

Part: PAN — CRACKED (BS 712-731) · airframe 62,966 hrs · 45,352 cycles

CRACKS ON RING PAN AFT LOWER CORNER IN BS 712 AND 731 LT SIDE AT CABIN PASSENGER RING PANS WERE REPAIRED IAW ER/A 543142-14, REV ORIGINAL.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

ELONGATED HOLE ON FWD HINGE OF MID CARGO COMPARTMENT. FWD HINGE OF MID CARGO DOOR WAS REPAIRED IAW ER/A 10-521061-14 AND INSTALLED IAW AMM 02-31-02, HINGE ADJUSTMENT AND DOOR INSTALLATION WILL BE PERFORMED INTO CARD 5200-4291, JOB 001-0317.

Part: CUSP WEB — CORRODED (BS 728) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON DOUBLER REPAIR LT CUSP WEB BS 728 BETWEEN BS X= 59 TO X= 57 AT PAX CABIN. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, 51-30-2 AND 51-10-3, PAR 14, 21 AND 38.

Part: CUSP WEB — CORRODED (BS 541-552) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 541 AND 552, X -60 AND -54. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-30-2 AND 51-10-3 PAR 14, 21 AND 38.

Part: PAN — CRACKED (BS 946-1250) · airframe 62,966 hrs · 45,352 cycles

CRACKS ON RING PAN FWD LOWER CORNER IN BS 946, 1079, 1098 AND 1250 LT SIDE AT CABIN PAX. RING PANS ON BS 946, 1098 AND 1250 WERE REPAIRED IAW SRM 53-05, FIG 122 AND BS 1079 WAS REPAIRED IAW ER/A 543142-14, REV ORIGINAL.

Part: BEAM — CRACKED (BS 627) · airframe 62,966 hrs · 45,352 cycles

CRACK ON BEAM ON BS 927 BETWEEN -X=60 TO -X=54 AT THE BEAM WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 51-10-3, 51-10-4, PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 638-653) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT CUSP WEB BS 653 TO BS 638.5 X=54, X=60. FABRICATED DOUBLER AND RING DOUBLER REPAIR IAW SRM 53-05, FIG 131A-14, SHEET 1. OK TO TREAT AND PAINT IAW SRM 51-10-3 PAR 14 AND 21 AND OK TO INSTALL IAW SRM 51-30-2 AND OK TO APPLY CIC IAW SRM 51-10-3, PAR 38.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT CUSP WEB FROM BS 579 TO BS 598 AT CABIN FLOOR STRUCTURE. DAMAGE AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND REPAIR PARTS WERE TREATED, PAINTED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131A-14 AND 51-10-3 PAR 14 AND 21 AND 38.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 62,966 hrs · 45,352 cycles

DAMAGE FLAME SPRAY ON RUDDER. DAMAGE AREA WAS REPAIRED IAW ER/A 092613-14MA AND SRM 51-70-1A PAR 23.

Part: CUSP WEB — CORRODED (BS 856-845) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 826 AND 845 BETWEEN X=-54 AND X=-60 AT CABIN PAX. PREVIUS REPAIR DOUBLER WAS REMOVED AND WERE FABRICATED NEW REPAIR PART TREATED AND PAINTED AND WERE INSTALLED IAW SRM 51-30-5, 53-05 FIG 131 A-13, 51-10-3, PAR 21 AND 14.

Part: CUSP WEB — CORRODED (BS 1003) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON PREVIOUS REPAIR AT LT CUSP WEB, BS 1003 BETWEEN X=54 AND X=60. REMOVE PREVIOUS REPAIR AND NEW REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131A-1.

Part: CUSP WEB — CORRODED (BS 645) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON CUSP WEB BS 645 BETWEEN X=-54 AND X=-60 FOR EXCESIVE CORROSION WAS REPAIRED CUSP WEB IAW SRM 53-05, FIGURE 131A-13, SHEET 1.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON INTERCOSTAL BETWEEN BEAM NR 4 AND BEAM 5 AT MAIN PASSENGER DOOR ENTRY. INTERCOSTAL BETWEEN BEAM NB 4 AND BEAM 5 WAS REPLACED IAW SRM 51-30-2 AND DWG 9955763 REV K.

Part: STRUCTURE — CRACKED (BS 180) · airframe 62,966 hrs · 45,352 cycles

CRACK ON CLIP BETWEEN BEAM NR 4 AND 5 AND BS 180 APPROXIMATELY AT FWD ENTRY DOOR. CLIP BETWEEN BEAM NR 4 AND 5 WAS REPLACED IAW SRM 51-30-2 AND DWG 5956563, REV DC.

Part: SKIN — BENT (PAX DOOR) · airframe 62,966 hrs · 45,352 cycles

LOWER SKIN FWD AND AFT CORNER AT FWD ENTRY DOOR FOUND BENT. REPAIR FABRICATED IAW SRM 52-05D, FIG 64, TREATED IAW SRM 51-10-03, PAR 14 - 21, AND INSTALLED IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 1418) · airframe 62,966 hrs · 45,352 cycles

CRACKED PREVIOUS REPAIR FRAME BS 1418 BETWEEN LONG 1-2R AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-10-4, 51-30-5 AND DWG SR09530003, REV "S".

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON AFT UPPER SIDE INNER PAN OF BEAM NR 5 AT MID CARGO DOOR. CRACK ON AFT UPPER SIDE INNER PAN OF BEAM NR 5 AT MID CARGO COMPARTMENT DOOR C2 WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: BEAM — CRACKED (PAX DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON BEAM NR 1 AFT EDGE AT AFT ENTRY DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-05D, FIG 97.

Part: DOOR FRAME — CRACKED (BS 1326) · airframe 62,966 hrs · 45,352 cycles

CRACK ON AFT CABIN BULKHEAD DOOR JAMB INTERCOSTAL AT BS 1326 LONGERON 15LT. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, SRM 51-10-4, SRM 51-10-3 PAR 14 AND 21, SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 1338) · airframe 62,966 hrs · 45,352 cycles

CRACKED INTERCOSTAL BETWEEN LONGERON 3R-4R BS 1338 IN AFT ACCESSORY COMPARTMENT. RT INTERCOSTAL IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 522-541) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT CUSP WEB FROM BS 522-541 AT CABIN FLOOR STRUCTURE. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-10-3, PARA 19-21 AND SRM 51-30-2, SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON FUEL ACCESS PANEL 1456 COUNTERSINK AREA. ACCESS PANEL WAS REPLACED.

Part: BEAM — CRACKED (PAX DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON BEAM NR 2 FWD EDGE AT FWD ENTRY DOOR. CRACK ON BEAM NR 2 FWD EDGE OF .270" WAS STOP DRILL IAW SRM 52-05D. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-05D, FIG 100 AND TREATED IAW SRM 51-10-3, PAR 14 AND 21. DOUBLER WAS INSTALLED IAW SRM 51-30-05.

Part: CUSP WEB — MISREPAIRED (BS 788-807) · airframe 62,966 hrs · 45,352 cycles

MISINSTALLED PREVIOUS REPAIR OR RT CUSP WEB AT BS 788-807 BETWEEN TRACK X=54/ X=60. PREVIOUS REPAIR WAS REPLACE IAW SRM 53-05, FIG 131A-7.

Part: CUSP WEB — WORN (BS 1152-1158) · airframe 62,966 hrs · 45,352 cycles

WEAR ON LT CUSP WEB BS 1152.5-1158.5 BETWEEN BS X=48 TO X=50 AT PAX CABIN. WEAR WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 3 AND REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PG 14 AND 21 AND APPLIED CIC IAW SRM 51-10-3.

Part: CUSP WEB — CORRODED (BS 886) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB AT BS 886 BETWEEN TRACK X=60 TO X=54 IN REF CARD 154, ZONE 201. DUE TO EXCESSIVE CORROSION CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: MEMBRANE — CRACKED (BS 198-200) · airframe 62,966 hrs · 45,352 cycles

CRACK ON MEMBRANE FROM BS 198-200 BETWEEN X=6 AND X=8 AT PAX CABIN STRUCTURE. DAMAGE AREA WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 62,966 hrs · 45,352 cycles

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

Part: CUSP WEB — CRACKED (BS 218) · airframe 62,966 hrs · 45,352 cycles

CRACK ON LT CUSP WEB IN BS 218 X 45, LOWERSIDE. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-20.

Part: DOOR FRAME — WORN (CARGO BAY) · airframe 62,966 hrs · 45,352 cycles

WEAR ON PREVIOUS REPAIR ON AFT CARGO COMPARTMENT LOWER FWD BEAM OF JAMB BETWEEN 1197-1203. DAMAGED REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-5; NEW SPACER WAS FABRICATED IAW SRM 53-05; FIG 123 WAS TREATED AND PAINTED IAW SRM 51-10-3 AND CIC WAS APPLIED IAW SRM 51-10-3.

Part: YOKE — CORRODED (LT PYLON) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT PYLON FWD SUPPORT YOKE LOWER BORE. CORROSION ON LOWER BORE WAS REMOVED WITH FINAL ID 01.314" AND BUSHING REPAIR IAW SRM 54-04D, PAR15, B, PAGE 96.

Part: CUSP WEB — CRACKED (BS 845) · airframe 62,966 hrs · 45,352 cycles

CRACK ON CUSP WEB LOWER SURFACE STA 845 AND X= 54 AT CABIN PASSENGER CUSP WEB BS 807 TO 845 AND X=54 WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 53-05, FIG 131A- 24 AND SRM 51-10-3 PAR 14, 21.

Part: PAN — CRACKED (BS 750-984) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RING PAN FWD UPPER CORNER IN BS 750-984 SIDE AT CABIN PAX. DAMAGED AREAS WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON LT BARREL NUT HOLE NR 12 BS XH 6.6 AT HORIZONTAL STABILIZER CENTER BOX. CORROSION ON LT BARREL NUT HOLE NR 12, STA XH 6.6 AT HORIZONTAL STABILIZER CENTER BOX IN THE REF CARD 23, ZONE 60 WAS REPAIRED IAW ER/A 543144-14 REV ORIGINAL.

Part: VANE — WORN (LT WING TE FLAP) · airframe 62,966 hrs · 45,352 cycles

WEAR ON REPAIR DOUBLER UPPER SURFACE STATION XV2=297 AT LT OTBD FLAP, OTBD GUIDE VANE. AREA WAS REPAIRED IAW SRM 57-003D AND CARD 2000-8149-04.

Part: LONGERON — CRACKED (BS 465) · airframe 62,966 hrs · 45,352 cycles

CRACKED LONGERON 4L BS 465 AT PAX CABIN CROWN AREA. DAMAGE SECTION LONGERON WAS REPAIRED IAW SRM 51-30-5, 53-02, FIG 18.

Part: DOUBLER — CORRODED (BS 204-211) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERNAL PRODUCTION DOUBLER FROM BS 204-211 BETWEEN LONGERONS 29RT AND 28RT IN E/E COMPARTMENT. INTERNAL PRODUCTION DOUBLER WAS REPLACED IAW DWG 9923686, REV D WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 21, 14.

Part: FAIRING — DAMAGED (RUDDER) · airframe 62,966 hrs · 45,352 cycles

EXPOSE METALIZER MATERIAL ON RUDDER FAIRING NR 6508A. THE METALIZER WAS INSTALLED IAW SRM 51-70-1AD, PAR 23.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,966 hrs · 45,352 cycles

CRACKED FLOOR PANEL 1307B. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: FRAME — CRACKED (BS 1380) · airframe 62,966 hrs · 45,352 cycles

CRACKED FRAME BS 1380 AND LONGERON 15L AT AFT ACCESSORY COMPARTMENT FRAME WAS REPLACED IAW SRM 53-14-4, FIG 1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1429) · airframe 62,966 hrs · 45,352 cycles

CRACKED LONGERON 16L, BS 1429. THE LONGERON WAS REPLACED IAW SRM 53-14-41, 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 769-788) · airframe 62,966 hrs · 45,352 cycles

CRACKED INTERCOSTAL BETWEEN BS 769 -788 AND X 0. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-4 AND 51-10-3, PAR 21 AND 14.

Part: INTERCOSTAL — CORRODED (BS 1347) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERCOSTAL IN BS 1347 BETWEEN X -18 TO X -25. DAMAGE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW INTERCOSTAL WAS DRILLED IAW SRM 51-10-4. NEW HOLES ON INTERCOSTAL WERE TREATED AND PAINTED IAW SRM 51-10-3 OAR 14 AND 2. NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1077) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB BS 1077 AT X -60 AND X -54. EXECESS DAMAGE WAS REMOVED IAW SRM 51-30-2. FABRICATE DOUBLER, RING DOUBLER AND FILLER IAW SRM 53-05, FIG 131-A-7 SHEET 1 AND WERE TREATED AND PAINTED IAW SRM 51-10-3 PARR 14 AND 21. REPAIR PART WERE INSTALLED IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 1429) · airframe 62,966 hrs · 45,352 cycles

CRACKED LONGERON 16R BS 1429 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-14-4, 51-30-2 AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 858) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON SEAT TRACK PLUG AT BS 858. THE PLUG WAS REPLACED IAW SRM 53-05, FIG 4.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON SETLEMENT AREA AND COUNTERSINK AT FUEL ACCESS PANEL 1436C. THE ACCESS PANEL WAS REPLACED.

Part: FERRULE — DAMAGED (FLOOR PANEL) · airframe 62,966 hrs · 45,352 cycles

DAMAGE FERRULES ON FLOOR PANEL. DAMAGE FERRULE REPLACED IAW AMM 53-20-01-201.

Part: FLOOR SUPPORT — CRACKED · airframe 62,966 hrs · 45,352 cycles

CRACKED CHANNEL AT LT FLOOR PANEL 1155 A. CHANNEL AT LT FLOOR PANEL NR 1155A WAS REPAIRED IAW SRM 51-70-1D, PAR 10.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON FUEL ACCESS PLATE NR 1367C COUNTERSINK AREA. FUEL ACCESS WAS REPLACED.

Part: CUSP WEB — CRACKED (BS 807-826) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RT CUSP WEB BETWEEN BS 807 - 826 BETWEEN SEAT TRACK X=54, X=60. CRACKED RT CUSP WEB BETWEEN BS Y=807, Y=826 BTW SEAT TRACK X=54, X=60 WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CRACKED (BS 242) · airframe 62,966 hrs · 45,352 cycles

CRACKED ON LT CUSP WEB AND MISSING BRACKET BS 242 BETWEEN X=60 AND X=54 AT CAB PASSENGER REMOVED DAMAGE AND DOUBLER WAS FABRICATED. TREATED AND PAINTED AND DOUBLER WAS INSTALLED IAW SRM 53-05; 51-10-3 PAR 14 AND 21; 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 1355) · airframe 62,966 hrs · 45,352 cycles

CRACK ON PREVIOUS REPAIR OF INTERCOSTAL IN BS 1355, FRONT OF AFT PRESSURE BULKHEAD X= -25 AT CABIN FLOOR STRUCTURE. INTERCOSTAL WAS REPAIRED IAW SRM 51-10-3, PAR 21 AND 14, SRM 51-30-2 AND SRM 51-30-5.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON INTERNAL STRUCTURE TO ATTACH CLEVIS BS XV2=245 AT LT OTBD FLAP MID GUIDE VANE. LT OTBD FLAP MID GUIDE VANE WILL BE REPLACE DUE TO SEVERAL DAMAGE THEREFORE WAS REMOVED WITH CARD 2710-4629, JOB 001-0166 AND WAS REPLACED WITH REPAIRED LT OTBD FLAP MID GUIDE VANE AND WILL BE INSTALLED WITH CARD 2710-4628, JOB 001-0165.

Part: PAN — CRACKED (EMERGENCY DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON PAN AT LOWER FWD CORNER OF LT AFT EMERGENCY EXIT DOOR. PAN WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CORRODED (BS 897) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION UPPER AND UNDER AT TRIPLER AND DOUBLER FROM LT CUSP WEB BS 897. REPAIR DOUBLER AND TRIPLER WERE REPLACED IAW SRM 53-05, FIG 131A-11, SHEET 1.

Part: STOP FITTING — WORN (CARGO DOOR) · airframe 62,966 hrs · 45,352 cycles

WEAR ON FWD AND AFT STOPS BETWEEN BEAM 1 AND 2 AT FWD CARGO DOOR. STOPS WERE REPLACED IAW SRM 51-30-1.

Part: PAN — CRACKED (EMERGENCY DOOR) · airframe 62,966 hrs · 45,352 cycles

CRACK ON PAN AT UPPER FWD CORNER OF LT FWD EMERGENCY EXIT DOOR. PAN FWD CORNER OF LT FWD EMERGENCY EXIT DOOR WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CORRODED (BS 4784-527) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN BS 484, BS 527 BETWEEN TRACK X=54/ X=60. DOUBLER WAS REPLACED IAW SRM 51-30-2 53-01, FIG 2 AND 51-10-3, PAR 14, 21.

Part: SEAT TRACK — CORRODED (BS 1264) · corrosion level 2 · airframe 62,966 hrs · 45,352 cycles

CORROSION ON PLUG, BS 1264, X=54 AT LT FLOOR CABIN PAX PLUG ON BS 1264, X=54 WAS REPLACED AND NEW PLUG INSTALLED IAW SRM 51-30-1, SRM 53-05, FIG 4A, SHEET 1.

Part: DOUBLER — WORN (CAROG DOOR) · airframe 62,966 hrs · 45,352 cycles

WEAR ON FWD AND AFT LOWER PRODUCTION DOUBLERS AT FWD CARGO COMPARTMENT DOOR EXTERNAL SKIN. DOUBLERS WERE REMOVED, NEW DOUBLERS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW 51-30-2, 51-10-3, PAR 21 AND 14, 51-10-4 ER/A 486624-14MA REV ORIG.

Part: ANGLE — CRACKED (BS 1003) · airframe 62,966 hrs · 45,352 cycles

CRACK ON ANGLE CLIP OF RING PAN AFT UPPER CORNER BS 1003 RT SIDE AT CABIN PASSENGER ANGLE WAS REPLACED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 845-1231) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RING PAN FWD LOWER CORNER IN BS 845, 946, 984 AND 1231 RT SIDE AT CABIN PASSENGER RING PANS ON BS 845, 946 AND 984 WERE REPAIRED IAW SRM 53-05, FIG 122 AND ON RING PAN BS Y=1231.

Part: PAN — CRACKED (BS 750-1079) · airframe 62,966 hrs · 45,352 cycles

CRACK ON RING PAN FWD UPPER CORNER IN BS 750, 788 AND 1079 RT SIDE AT CABIN PASSENGER RING PANS BS 750 AND 788 WERE REPAIRED IAW SRM 53-05, FIG 122 AND ON RING PAN BS 1079.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,248 hrs · 44,173 cycles

MAINTENANCE FOUND A VISIBLE CRACK ON THE LOWER SKIN OF THE CENTERWING BOX. THE CRACK IS LOCATED ON THE FORWARD EDGE OF THE AFT WING SKIN, AND AFT EDGE OF THE FORWARD WING SKIN. THE CRACK ALSO PROPAGATED THROUGH THE UNDERLYING STRINGER IN THE CENTER WING BOX. MAINTENANCE COMPLIED WITH ER/A 535437-14AD, REV ORIGINAL.

Part: RELEASE CABLE — MISROUTED (TAILCONE) · airframe 60,201 hrs · 43,495 cycles

DURING CHECK, MAINTENANCE FOUND THE FORCE REQUIRED TO RELEASE THE TAILCONE EXCEEDED THE LIMITS. MAINTENANCE FOUND THE RELEASE CABLE ROUTED IMPROPERLY AND ROUTED THE CABLE TO THE PROPER POSITION AND PERFORMED A TAILCONE FUNCTIONAL TEST.

Part: UNKNOWN — CRACKED (BS 1380) · airframe 60,180 hrs · 43,479 cycles

LT AFT FUSELAGE BS 1380 IS CRACKED AT FASTENER APPROXIMATELY 12" ABOVE PYLON. ACCOMPLISHED WORK STEPS OF PRI 531053-14, REV 0 AND COMPLIED WITH ER/A 531053-14, REV ENTERED AND DEFERED FOR SDR REPORTING.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 60,180 hrs · 43,479 cycles

OVERWING EMERGENCY DOOR RT AFT PAN STRUCTURE CRACKED AT UPPER FWD BRACKET. ACCOMPLISHED REPAIR IAW INSTRUCTION OF PRI 531058-14, REV 0. COMPLIED WITH ER/A 531058-14, REV ORIGINAL SCEPTRE LOG PAGE ENTERED AND DEFERED FOR SDR REPORTING.

Part: PIN — WORN (TAILCONE LATCH) · airframe 60,201 hrs · 43,495 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE LOWER LEFT RELEASE LATCH PIN WORN. MAINTENANCE REPLACED THE LATCH PIN.

Part: ATTACH BRACKET — WORN (TAILCONE RELEASE) · airframe 60,180 hrs · 43,479 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE SPRING ATTACH BRACKET WORN. MAINTENANCE REPLACED THE WORN BRACKET.

Part: CABLE — FRAYED (TAILCON) · airframe 60,180 hrs · 43,479 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE KEVLAR CABLE TO BE FRAYED. MAINTENANCE REPLACED THE KEVLAR CABLE.

Part: RECEPTACLE — WORN (TAILCON) · airframe 60,180 hrs · 43,479 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE UPPER LT LATCH PIN RECEPTACLE HAS A WORN EAR. MAINTENANCE REPLACED THE RECEPTACLE.

Part: BUSHING — WORN (TAILCONE) · airframe 60,201 hrs · 43,495 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE TEE PIN BUSHING WORN. MAINTENANCE REPLACED THE BUSHING.

Part: QUICK DISCONNECT — UNSECURE (EMERGENCY LIGHTS) · airframe 58,862 hrs · 42,557 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE AFT STAIRWAY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND A QUICK DISCONNECT TERMINAL NOT SECURE AND THEY SECURED THE TERMINAL. OPERATIONAL CHECK WAS NORMAL. (LP 6007433).

Part: FRAME — CORRODED (BS 1271) · airframe 56,475 hrs · 41,011 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND IN THE AFT CARGO BAY ON FRAME AT BS 1271 FROM LONGERON 28L TO 28R. REPAIRED IAW SRM 53-03 FIG 2A.

Part: SKIN — DAMAGED (BS 946) · airframe 56,475 hrs · 41,011 cycles

DURING SCHEDULED CHECK, IT WAS NOTED THE UPPER FUSELAGE HAS EVIDENCE OF A LIGHTNING STRIKE BETWEEN LONGERON 8 AND 9R, BS 946. DAMAGE FOUND TO BE OUT OF LIMITS AND WAS REPAIRED IAW SRM 53-04-1, & 53-04-2.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 56,475 hrs · 41,011 cycles

DURING SCHEDULED MX INSPECTION, CORROSION WAS NOTED AT THE AFT LOWER CARGO COMPARTMENT DOOR JAMB. REPAIRS WERE INCORPORATED IAW SRM 53-05, FIGURE 123 AND 51-30-5.

Part: LIGHT — INOPERATIVE (ROW 21) · airframe 54,463 hrs · 39,702 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND ROW 21 EMERGENCY PATHWAY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM. OPS CHECKED GOOD.

Part: SKIN — DENTED (LT WING) · airframe 53,404 hrs · 39,042 cycles

DUE AT PSV SRM 57-03D PERMANENT REPAIR AT DENT AND 5 GOUGES ON THE LEFT WING LEADING EDGE AT STATION 273. MAINTENANCE REMOVED SEALANT AND SPEED TAPE FROM TEMPORARY REPAIR. NDT PER NDTSPM 04-00-06. 5 DENTS THICKNESS REMAINING .028 - .036QC 1972 MAX ORIGINAL THICKNESS .040 +/- .005 PER BOEING DRAWING 9937512.

Part: SKIN — CRACKED (FUSELAGE) · airframe 534,041 hrs · 39,042 cycles

DURING PSV IN MSP A CRACK WAS NOTED COMMON TO THE FUSELAGE SKIN LOCATED AT STA 1418 JUST ABOVE S-3R. THE CRACK WAS REPAIRED IN ACCORDANCE WITH ERA#500702-14 REV 0 ON NR#104.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,549 hrs · 38,528 cycles

ESCAPE PATH LIGHT INOPERATIVE AT ROW 17D. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,495 hrs · 38,483 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT EXIT DOORS 1L & 1R IN THE CABIN, WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE CONTROLLER AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 49,369 hrs · 36,469 cycles

MAINTENANCE FOUND THE ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 22DE. MAINTENANCE SECURED THE QUICK DISCONNECT. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,549 hrs · 35,921 cycles

DURING HMV A CRACK WAS FOUND OF .300" ON FUSELAGE SKIN AT STA Y=194 AT LOWER AFT CORNER OF THE FWD SERVICE DOOR JAMB CRACK WAS REPAIRED IAW SRM 53-05 FIG 112.

Part: WINDOW FRAME — DAMAGED (BS 370-389) · airframe 48,549 hrs · 35,921 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON AFT SECTION WINDOW FRAME NR 17 BTW STA Y=370-389 AT FUSELAGE OUTER SKIN AREA WAS REPAIRED IAW ERA 479731-14 REV ORIG.

Part: HEATER BLANKET — DAMAGED (LT WING) · airframe 48,549 hrs · 35,921 cycles

COMPLY WITH IN HMV ERA 420436-14AD REV B REPAIR THE EDGE VOIDS AT VARIOUS LOCATIONS AROUND THE PERIMETER OF THE LT HEATER BLANKET AREA WAS REPAIRED IAW AMM 30-80-02-801 AND ERA 420436-14AD REV C.

Part: WINDOW FRAME — DAMAGED (BS 769) · airframe 48,549 hrs · 35,921 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON FWD EDGE OF WINDOW BELT NR 58 BTW STA Y=750-769 AT RT SIDE FUSELAGE OUTER SKIN AS WELL LIGHTNING STRIKE ON FUSELAGE SKIN AT STA Y=769 BTW LONGERON 16 AND 17 RT AREA WAS REPAIRED IAW ERA 479602-14 REV ORIG.

Part: HEATER BLANKET — CORRODED (RT WING) · airframe 48,549 hrs · 35,921 cycles

DURING HMV PITTING CORROSION WAS FOUND ON RT WING HEATER BLANKET AROUND FUEL TANK ACCESS PLATE NBR 1410C AREA WAS REPAIRED IAW ERA 478632-14AD REV ORIG.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 48,549 hrs · 35,921 cycles

DURING HMV PITTING CORROSION WAS FOUND ON LT MLG SUPPORT FITTING BEARING BORE AREA WAS REPAIRED IAW EA 09-093855-03AD0104 REV B.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 48,549 hrs · 35,921 cycles

DURING HMV SCRATCHES AND PITTING CORROSION WAS FOUND ON LT MLG SUPPORT FITTING BUSHING BORE AREA WAS REPAIRED IAW EA 09-093855-03AD 0104.

Part: HEATER BLANKET — CORRODED (RT WING) · airframe 48,549 hrs · 35,921 cycles

DURING HMV PITTING CORROSION WAS FOUND ON RT HEATER BLANKET AROUND ACCESS PLATE NBR 1409C AREA WAS REPAIRED IAW ERA 478632-14AD REV ORIG.

Part: SKIN — DAMAGED (RUDDER) · airframe 48,549 hrs · 35,921 cycles

DURING HMV DAMAGED METALLIZED COAT WAS FOUND ON RT SKIN OF RUDDER DAMAGE WAS REPAIRED IAW SRM51-70-1AD PARA 23.

Part: PAN — CRACKED (CARGO DOOR) · airframe 48,549 hrs · 35,921 cycles

DURING HMV A CRACK WAS FOUND ON MID CARGO COMPARTMENT DOOR AT INTERSECTION OF UPPER BEAM FWD EDGE CRACK WAS REPAIRED IAW SRM 52-05D FIG 50.

Part: HEATER BLANKET — CORRODED (LT WING) · airframe 48,549 hrs · 35,921 cycles

DURING HMV PITTING CORROSION WAS FOUND ON LT WING HEATER BLANKET AROUND FUEL ACCESS PLATE NR 1307C AREA WAS REPAIRED IAW ERA 478632-14AD REV ORIG

Part: SKIN — CRACKED (BS 1437 L3-4L) · airframe 48,549 hrs · 35,921 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1437 BTW LONGERON 3 AND 4LH AREA WAS REPAIRED IAW ERA 479729-14 REV ORIG.

Part: HEATER BLANKET — DAMAGED (LT WING) · airframe 48,549 hrs · 35,921 cycles

DURING HMV TOOLING MARKS WAS FOUND ON LT WING HEATER BLANKET AROUND FUEL ACCESS PLATE NR 1307C AREA WAS REPAIRED IAW ERA 478632-14AD REV ORIG.

Part: HEATER BLANKET — CORRODED (LT WING) · airframe 48,549 hrs · 35,921 cycles

DURING HMV PITTING CORROSION WAS FOUND ON LT HEATER BLANKET AROUND ACCESS TANK PLATE NBR 1303C AREA WAS REPAIRED IAW ERA 478632-14AD REV ORIG.

Part: SKIN — CRACKED (BS 191-193 L22L) · airframe 48,549 hrs · 35,921 cycles

DURING HMV EA 09-069085-12AD REV E ME01 OPN 0101 WAS PERFORMED AND 2 CRACKS WERE FOUND ON FUSELAGE SKIN AT STA Y=191 AND Y=193 AND LONGERON 22LH OF .186" AND .125" RESPECTIVELY AREA WAS REPAIRED MOD IAW EA 09-069085-12AD REV E ME02 OPN 0203.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 48,549 hrs · 35,921 cycles

DURING HMV A SCRIBE LINE WAS FOUND ON AFT SECTION OF WINDOW FRAME NR 63 BTW STA Y=807-826 AT FUSELAGE OUTER SKIN WINDOW BELT WAS REPAIRED IAW ERA 479731-14 REV ORIG.

Part: WINDOW FRAME — DAMAGED (BS 693-712) · airframe 48,549 hrs · 35,921 cycles

DURING HMV TOOLING MARKS WERE FOUND ON UPPER FWD EDGE OF WINDOW BELT NBR 52 BTW STA Y=693-712 AT RT SIDE FUSELAGE OUTER SKIN AREA WAS REPAIRED IAW ERA 479602-14 REV ORIG.

Part: TIRE — DAMAGED (NR 2) · airframe 37,167 hrs · 28,514 cycles

NR 2 TIRE TREAD THROWN ON TAKEOFF. NR 1 ENGINE DAMAGED AND SHUTDOWN. REPLACED TIRE AND ENGINE.

Part: INLET — CONTAMINATED (APU) · airframe 36,026 hrs · 27,696 cycles

BURNING OIL SMELL IMMEDIATELY AFTER TAKEOFF LASTED ONLY A FEW MINUTES. FOUND SMALL AMOUNT OF HYD FLUID IN APU INLET. CLEANED APU INLET, PERFORMED ALTERNATE DUCT BURN OPN 5090. REPLACED WATER SEPARATOR BAGS, NO FURTHER ODOR NOTED.

Part: BATTERY — OVERHEATED (E/E COMPT.) · airframe 34,666 hrs · 26,718 cycles

DURING MAINTENANCE TAXI, SHIP'S BATTERIES OVERCHARGED, CAUSING SMOKE EMISSION FROM E/E COMPARTMENT. REPLACED BATTERIES AND CHARGER.

Part: LIGHT — BROKEN (TAIL CONE) · airframe 28,283 hrs · 22,202 cycles

WORKING L/O FOUND EMERGENCY LIGHTS IN TAIL CONE INOP. REPAIRED CONNECTOR - OPS NML.

Part: MEGAPHONE — DAMAGED (MID CABIN) · airframe 27,681 hrs · 21,731 cycles

MID CABIN MEGAPHONE HANDLE DAMAGED._REPLACED MEGAPHONE WITH SERVICABLE UNIT.

Part: ENGINE — DAMAGED (NR 1) · airframe 26,830 hrs · 21,067 cycles

ABORTED TAKEOFF 100 KIAS LEFT ENG EGT PEAK 610 DEGREES. MTC FOUND NR 1 ENG HAS LINER DAMAGED IN COLD STREAM AT APPROX 11:00 POS. REPLACED ENGINE.

Part: SWITCH — INOP (RT MLG)

CVG AIRBORN RETURN, RED LIGHT ON RT MAIN GEAR DOWN LOCK INDICATOR STAYED ON AFTER GEAR RETRACTION. GEAR EXTENDED NORMALLY. REPEAT WRITE-UP. REPLACED PROX SW ELECTRONICS UNIT AND RT MLG UP PROXIMITY SW PER M/M. OPN CKS NML GEAR CYCLED SEVERAL TIMES ALL INDICATION GOOD.

Part: LINE — LEAKING (LT HYD SYST)

LEFT HYD SYS QTY WENT TO ZERO. PRESS WENT TO ZERO. FOUND LT SYSTEM SUPPLY LINE LEAKING. PERMASWAGED LINE.

Part: ENGINE — FAILED (NR 2)

ON T/O, NR 2 ENG AT V1 ROLLED BACK TO JUST ABOVE IDLE POWER. FLT ATTENDENT IN REAR HEARD LOUD NOISE. ENG WOULD NOT RECOVER THRUST. WE LEFT ENG AT IDLE. ON LANDING EGT STARTED TO INCREASE. SHUT DOWN ENG, NO OVER TEMPS. FOUND 13TH STAGE DUCT BLOWN INTERNALLY AND SEPARATED FROM CASE. REPLACING ENGINE.

Part: SKIN — DENTED (BS 240)

SEVERAL DENTS WERE FOUND IN THE FUSE SKIN FROM FS 232 TO 251, NEAR L18L. REPAIRED PER ERA 331712-14.

Part: SKIN — DENTED (BS 226)

SEVERAL DENTS FOUND IN FUSE SKIN AT APPROX FS 224 TO 227 NEAR L18L. REPAIRED PER ERA 331715-14.

Part: SKIN — DENTED (BS 235)

FUSELAGE SKIN AFT OF THE L1 DOOR WAS FOUND WITH SEVERAL DENTS FROM STA 230 TO 240 AND BETWEEN L18-20 L. REPAIRED PER ERA 331699-14.

Part: APU — FAILED (APU COMPT)

APU SHUTDOWN AUTOMATICLLY, ATTEMPT AT RESTART UNSUCCESSFUL. LEFT GENERATOR ON MCO. DIVERTED TO CVG. REPLACED APU.

Part: COALESCER — CONTAMINATED (CABIN)

ODOR THROUGH AIR CONDITIONING AT TAKEOFF POWER. SUSPECT H2O SEPARATORS. ODOR SET OFF SMOKE DETECTOR IN AFT LEFT LAV. REPLACED WATER SEPARATORS, NO ODOR NOTED.

Part: BULB — FAILED (CABIN)

EMERGENCY TRACK LIGHTING BY FWD GALLEY REQUIRES RELAMPING.

Part: SENSOR SPRING — BROKEN (RT MLG UP SENSOR)

AFTER TAKEOFF WITH GEAR UP, THE RT GEAR UNSAFE LIGHT STAYED ON. GEAR DOOR CLOSED INDICATION OK AND NO ADVERSE FLT CHARACTERISTICS. FOUND RT MLG UPLOCK SENSOR SPRING BROKEN. REPLACED SAME, PERFORMED GEAR SWING, AND CHECK-OUT PER MM 32-60-00. ALL INDS AND OPERATION CHECK NORMAL.

Part: AIR DISTR — SMOKE (CABIN)

AT FL 280 ON CLIMBOUT, CABIN SMOKE WAS OCCURING IN AFT CABIN AREA. LAV SMOKE DETECTOR WENT OFF AND VISIBLE SMOKE AND SMELL WAS SENSED. DESCENT WAS INITATED AND SMOKE DISAPPEARED REMAINDER OF FLIGHT. A/C PACKS APPEARED NORMAL. PACK TEMPS 60F AT TIME OF INCIDENT. RT PACK TEMP WAS TURNED TO WARM UP CABIN AT TIME. CKD ENGINE AND APU FOR OIL LEAKS, NONE FOUND. ACM OIL LEVEL NORMAL. REPLACED WATER SEPARATOR BAGS, RAN PACKS WITH ENGINE AIR FOR 30 MINS, DUCT TEMP TO 140 DEGREES NO SMOKE OR SMELL.

Part: SOCKET — BURNT (CABIN)

ELECTRICAL ODOR IN CABIN AND COCKPIT. FOUND UPPER SIDEWALL LT SOCKET BURNED THROUGH AT SEAT 13ABC. REPLACED SOCKET AND BULB.

Part: IRU — FAILED (E/E COMP)

AFTER TAKEOFF, NR 1 INERTIAL REFERENCE UNIT FAILED, WITH ASSOCIATED SYSTEM FAILURES. DIVERTED CVG. REPLACED IRU, OPERATION NORMAL.