N321FE

Part: FRAME — CORRODED (BS 374 L47-50L) · airframe 104,762 hrs · 32,732 cycles

INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & # 2 ACM AT STATION 541.667 BOTTOM OF ACA3348-3 FRAME HAS CORROSION AT LOWER FLANGE. REPAIRED INBOARD LOWER FLANGE OF ACA 3348-3 WEB. REF SRM 53-00-01 FIG. 8 VOL. 1 AND DAC DWG ACA 3348.

Part: ANGLE — CORRODED (BS 540) · airframe 104,762 hrs · 32,732 cycles

INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & #2 ACM APPROX. STA 540 AT BOTTOM OF BULKHEAD VERTICAL FLANGE OF CHORD ANGLE HAS EXFOLIATION CORROSION APPROX. FOUR SQUARE INCHES. (MKD) 0003748737 : KOTSOGLOU, CHRISTOPHER - 28-AUG-2021 03:26 REMOVED , FABRICATED , AND INSTALLED REINFORCEMENT ANGLE NCA6050-33 PER SRM 51- 31-01 V2 AND DOUGLAS DRAWING NCA6050. 0003748737 : KOTSOGLOU, CHRISTOPHER - 28-AUG-2021 03:32 REMOVED , FABRICATED , AND INSTALLED REINFORCEMENT ANGLE NCA6050-33 PER SRM 51- 31-01 V2 AND DOUGLAS DRAWING NCA6050. "MAJOR REPAIR"

Part: RIB — CRACKED (VERTICAL STAB) · airframe 104,762 hrs · 32,732 cycles

VERTICAL STAB L/E - PNL #371CLE HAS CRACKED RIB - 7TH FROM BOTTOM L/H SIDE TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER REFERENCE SRM 55-00-01 FIG. 7 SHEET 1 VOL. 1. "MAJOR REPAIR"

Part: SKIN — CRACKED (RUDDER) · airframe 104,762 hrs · 32,732 cycles

LOWER AFT RUDDER, BOTTOM RHS AFT SECTION HAS AN APPROX 1" CRACK, MARKED. REMOVED AND REPLACED LOWER AFT RUDDER. REF AMM 27-20-01-4 INSTALLED P/N: NMC6015- 505 S/N: 48450.

Part: SKIN — DELAMINATED (RT ELEVATOR TE) · airframe 104,762 hrs · 32,732 cycles

R/H O/B ELEVATOR TRAILING EDGE DELAM. (MARKED) REPAIRED O/B TRAILING EDGE ELEVATOR ENVELOPE PER SRM 55-30-00 VOL.1 PGS 1-9. "MAJOR REPAIR"

Part: SKIN — DENTED (BS 1850 S38-39R) · airframe 104,762 hrs · 32,732 cycles

FUSELAGE EXTERIOR SKIN DENT/CREASE - AFT OF CENTER CARGO AT APPROX STA.1850 BETWEEN LONGS 38-39. CUT OUT DAMAGED SKIN AT STA. 1850 BETWEEN LONGERONS 38R AND 39R AND INSTALLED REPAIR PER SRM 53-20-00 FIG. 6 SH.12-15 VOL.1. "MAJOR REPAIR"

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 104,762 hrs · 32,732 cycles

LEFT WING O/B FLAP UPPER I/B T/E SPLIT AT CONNECTION AND DAMAGED AT CORNER. (DOT 6) REMOVED, FABRICATED AND INSTALLED L/H WING O/B FLAP UPPER I/B T/E DAMAGED SECTION REF SRM 57-20-00 VOL 1 PARAGRAPH 13 STEPS A-E.

Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 104,762 hrs · 32,732 cycles

FWD CARGO FLOOR PANEL ADA0241-51(127WF) FABRICATED NEW FLOOR REF FEDEX DWG SRZ-25-005

Part: LOCK — SHEARED (LT WING) · airframe 104,762 hrs · 32,732 cycles

L/H WING TOP SURFACE - TAPER LOCK STICKING UP FROM TOP SURFACE OF WING - APPROXIMATE STA XORS 275 ON GROSS WEIGHT MOD DOUBLER AFT OF REAR SPARE 0003748737 : KOTSOGLOU, CHRISTOPHER - 14-AUG-2021 04:01 REMOVED AND REPLACED L/H WING TOP SURFACE FASTENER PER E.A. 8-5730- T0363119 "WINGS - PLATES AND SKIN -LH WING UPPER SKIN MAIN LANDING GEAR DOUBLER FASTENER SHEARED OFF AT XW228"

Part: LONGERON — WORN (BS 1775 L47R) · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMPT L47R HAS EXFOLITATION CORROSION ON INBOARD SIDE STA 1775. INSTALLED NEW SECTION OF LONGERON 47R FROM EXISTING SPLICE LOCATION AT STA. 1775 TO REPAIR SPLICE AT STA. 1811. REF. SRM 53-10-00 FIG. 2 VOL.1 AND DOUGLAS DRAWING AGA7027.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK FLOOR BOARD AT STATION 1039 L/H SIDE WITH 5/L MARKING FOUND TO BE SPONGE/SOFT FABRICATED NEW FLOOR PANEL MAIN DECK AT STATION 1039 L/H SIDE WITH 5/L MARKING REF FEDEX DRAWING SRZ-25-005

Part: FRAME — WORN (BS 1787 L47-49R) · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMPT FUSE FRAM SECTION REMOVED TO FOM STA 1787 L47R-L49R. INSTALLED STA. 1787 FRAME SECTION FROM LONGERON 47R TO 49R REF DOUGLAS DRAWING AFA 7112. INSTALLED FRAME REPAIR CHANNELS AND REPAIR STRAP BETWEEN L45R-L46R REF EA 8-5310-T0363372 " FUSELAGE- MAINFRAME- CTR LWR CARGO JAMB FRAME REPAIR AT STA 187 BETWEEN L-45 AND L-46 RH SIDE. 'MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1801 L45R-47L) · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMPT FUSE FRAME SECTION REMOVED TO FOM STA 1801 L47L-L45R. INSTALLED STA. 1801 FRAME SECTION FROM LONGERON 47L AT B/P SPLICE TO 45R REF.DOUGLAS DRAWING AFA7166 . INSTALLED FRAME SPLICE AT LONGERON 45R REF. EA 8- 5310-T0363251 "FUSELAGE-MAIN FRAME-FRAME REPAIR AT STA. 1801 BETWEEN L-45 AND L46 RH SIDE". "MAJOR REPAIR"

Part: SUPPORT — CORRODED (BS1891-2007 S24R) · airframe 104,762 hrs · 32,732 cycles

MAIN CABIN AFT LAV SUPPORT AGA7087-504 STATION 1891-2007 RBL-24 EXFOLIATION CORROSION EXISTS UNDER DOME NUTS. INSTALLED NEW/FABRICATED AFT LAV SUPPORT ON MAIN CABIN AT STATION 1891-2007 RBL 24 REF, DOUGLAS DWG NO. AGA7087 AND MD10-30 SRM 51-31-01 VOL 2.

Part: RIB — CRACKED (RT WING) · airframe 104,762 hrs · 32,732 cycles

R/H WING UPPER FILLET PANEL SUPPORT RIB ANB7142-10 AT STATION 1341 CRACKED LOWER END. REMOVED AND REPLACED RIGHT HAND WING UPPER FILLET PANEL SUPPORT RIB ANB7142- 10 AT STATION 1341 I.A.W DAC DWG ANB7102 AND SRM 51-31-01 VOL. 2.

Part: BULKHEAD WEB — WORN (BS 2007) · airframe 104,762 hrs · 32,732 cycles

MAIN CARGO STATION 2007 LBL 30 HOLE DAMAGED ON PRESSURE BULKHEAD AT FLOOR BOARD SUPPORT TEE REPAIRED HOLE PER SRM 51-39-01 VOL II. REF. E.A # 8-5310-T0363077 TITTLE: FUSELAGE-MAIN FRAME- AFT PRESSURE BULKHEAD WEB AND DOUBLER DAMAGED AT FASTENER HOLE. "MAJOR REPAIR".

Part: SUPPORT — CORRODED (BS1891-2007 S24L) · airframe 104,762 hrs · 32,732 cycles

MAIN CABIN AFT LAV SUPPORT AGA7544-1 STATION 1891-2007 LBL 24 EXFOLIATION CORROSION EXISTS ON FOWARD END BEYOND LIMITS INSTALLED NEW/FABRICATED AFT LAV SUPPORT ON MAIN CABIN AT STATION 1891-2007 LBL 24 REF, DOUGLAS DWG NO. AGA7087 AND MD10-30 SRM 51-31-01 VOL 2.

Part: VANE — WORN (RT WING TE FLAP) · airframe 104,762 hrs · 32,732 cycles

R/H INB'D T/E FLAP VANE INB'D L/E AREA SHOWING RUBBING DAMAGE. REPAIRED R/H INB FLAP VANE I/B L/E PER SRM 51-71-00 VOL II PAR 16 PG 64. I.A.W. SRM 57-00-01 FIG 4 SHEET 1. RSC TRACKING E.A. 8-5750-T-0362626 FLT. SURFACES - R/H I/B FLAP VANE STRUCTURE REPAIR. (MAJOR REPAIR)

Part: ANGLE — CRACKED (NR 2 SLAT) · airframe 104,762 hrs · 32,732 cycles

L/H WING #2 SLAT OUTBOARD CAP CRACKED AT THE ANGLE #2 SLAT OUTBOARD CAP ANGLE REPAIR PER SRM 57-00-01 FIG 10 VOL 1 . "MAJOR REPAIR"

Part: FRAME — CRACKED (LT WING LE) · airframe 104,762 hrs · 32,732 cycles

LEFTHAND WING; XORS=570 LEADING EDGE INTERNAL FRAME STRAP HAS 6" CRACKS @ UPPER OUTBOARD SECTION. REMOVED AND REPLACED LEFT WING XORS 570 LEADING EDGE INTERNAL FRAME STRAP UPPER OUTBOARD SECTION REF DWG ARB3954.

Part: LONGERON — CORRODED (BS 1750-1781 L46) · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMP. APPROX. STA 1750 TO 1781 LONG 46R FOUND SEVERAL AREAS OF CORROSION INSIDE HAT SECTION OF LONGERON. (MKD) REMOVED CORRODED SECTIONS AND INSTALLED NEW SECTIONS OF LONGERON 46R FROM STA. 1671 AT EXISTING SPLICE LOCATION TO STA. 1831. REPAIR SPLICES INSTALLED AT STA. 1791 AND 1831. REFERENCE SRM 53-10-00 FIG. 2 VOL.1 AND DOUGLAS DRAWINGS AFA7098 AND AGA7039. "MAJOR REPAIR"

Part: LONGERON SPLICE — CORRODED (BS 1808 L46R) · airframe 104,762 hrs · 32,732 cycles

CENTER GARGO COMPARTMENT BILGE - APPROX STA.1808 46R - EXFOLIATION CORROSION ON LONG AND SPLICE. REMOVED CORRODED LONGERON SECTIONS AND INSTALLED NEW SECTIONS OF LONGERON 46R FROM STA. 1671 AT EXISTING SPLICE LOCATION TO STA. 1831. REPAIR SPLICES INSTALLED AT STA. 1791 AND 1831. REFERENCE SRM 53-10-0 FIG. 2 SH. 1-6 VOL.1 AND DOUGLAS DRAWINGS AFA7098 AND AGA7039. (REF. NR 615)

Part: WEB — DENTED (BS 1841) · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMPT STA 1841 AT FLOOR LEVEL WEB IS DENTED FROM CONTAINER CONTACT. MRKD LBL 15 TO RBL 5. REMOVED AND REPLACED DAMAGED WEB AGA7170-3 IAW DAC DWG AGA7170 AND SRM 51-31- 01 VOL. 2.

Part: FLOOR SUPPORT — CORRODED (BS 2007 L/RBL 32) · airframe 104,762 hrs · 32,732 cycles

AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. LBL24, (MARKED #13) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SRM 51-33-01 VOL. 2. AND DAC DWG NJC6040.

Part: FLOOR SUPPORT — CORRODED (BS 1741 S55R) · corrosion level 2 · airframe 104,762 hrs · 32,732 cycles

CENTER CARGO COMPT MAIN DECK FLOORBOARD SUPPORT CORRODED STA 1741 RBL 55. MRKD REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA. 1741 RBL 55 CTR CARGO COMPT. PER SRM 51-31-01 VOL 2 AND DWG NO. S2929169

Part: FLOOR SUPPORT — CORRODED (BS 2007 R/LBL 32) · airframe 104,762 hrs · 32,732 cycles

AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. RBL24, (MARKED #12) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SRM 51-33-01 VOL. 2. AND DAC DWG NJC6040.

Part: SKIN — CORRODED (BS 2002 L45R) · airframe 104,762 hrs · 32,732 cycles

AFT FUSE WASTE TANK COMPT, CORROSION ON INTERIOR OF FUSELAGE SKIN, AT EXISTING EXTERIOR DOUBLER AREA, AT STA 2000 BETWEEEN L-45 AND L-45 R/H. (MARKED #11) REMOVED CORROSION FOUND TO BE WITHIN LIMETS REF SRM 53-20-00 FIG 4 SHT 2 NOTE 16 VOL 1 .

Part: DOOR FRAME — WORN (BS 535 L23L) · airframe 104,762 hrs · 32,732 cycles

MAIN CARGO DECK, LH SIDE, STA. 535, LONG 23, FRAME GOUGED BY LOWER HINGE HARDWARE OF CARGO NET BRACKET. DOT #10. REMOVED DAMAGED PREVIOUS "L" ANGLE REPAIR AND INSTALLED NEW REPAIR AT STA. 535 LONGERONS 22 TO 25 REF. MD10-30 SRM 53-30-00 FIG. 13 SHEET 1 VOL.1

Part: DOOR FRAME — DAMAGED (BS 535 L20L) · airframe 104,762 hrs · 32,732 cycles

MAIN CARGO DECK, LH SIDE, STA. 535, LONG 20, FRAME GOUGED BY UPPER HINGE HARWARE OF CARGO NET BRACKET. DOT #9. REMOVED PREVIOUS "L" ANGLE REPAIR AND INSTALLED NEW REPAIR AT STA.535 LONGERON 18 TO 21 REF. MD10-30 SRM 53-30-00 FIG. 14 SHEET 1 VOL.1

Part: SKIN — DENTED (BS 1894 L46-44L) · airframe 104,762 hrs · 32,732 cycles

LH FUSELAGE APPROX STA.1894 BETWEEN L43-L44 - DENT ON SKIN. REPAIRED DAMAGED SKIN REF SRM 53-20-00 FIG.6 SHEETS 12-13 VOL. 1 AND SRM 51-31-01 VOL. 2.

Part: SEAT TRACK — WORN (BS 1501-1551) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK: SEAT TRACK WORN, NEAR STA 1501 LBL 8.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 8.5 FROM STA 1501-1551 REF SRM 53-70-00 FIG 1 VOL 1, AND SRM 51-31-01 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002

Part: SEAT TRACK — WORN (BS 1129-1149) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 LBL 47.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 47.5 FROM STA 1129-1149 REF SRM 53-70-00 FIG 1 VOL 1, AND SRM 51-31-01 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002

Part: SEAT TRACK — WORN (ZONE 200) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK: SEAT TRACK WORN, NEAR STA 1370 RBL 47.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 47.5 FROM STA 1313-1411 REF SRM 53-70-00 FIG 1 PAGE 3 VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002.

Part: SEAT TRACK — WORN (BS 1039 LBL 78) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK, GOUGES ON SEAT TRACK LOBES AT STA 1039 LBL 78 (MARKED #18) INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 78 FROM STA 1009-1089 REF SRM 53-70-00 FIG 1 PAGE 6A VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002 REF SRM 53-70-00 FIG 1 PAGE 3 VOL 1

Part: SEAT TRACK — WORN (ZONE 200) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 RBL 8.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 8.5 FROM STA 1129-1069 REF SRM 53-70-00 FIG 1 PAGE 3 VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 104,762 hrs · 32,732 cycles

MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005

Part: ENGINE — FAILED (LEFT) · airframe 104,431 hrs · 32,588 cycles

APPROXIMENTELY 30 MINUTES IN TO FLIGHT (FL350) CREW HEARD A VERY LOUD BANG WITH SIGNIFICANT AIRCRAFT YAW. OBSERVED ENGINE NO 1 N1 ROLL BACK WITH CONFIRM ENG OUT ON FMS. DETERMINED N1 ON ENG 1 HAD SEIZED AND EXECUDED PHASE 1. COMPLIED AND COMPLETED ENGING 1 FIRE/OR SEVERE DAMAGE CHECK LIST. RECOVERED AT KDEN RWY 35L. REPLACED LH ENGINE.

Part: BOOT — DEFECTIVE (AC BAY) · airframe 103,000 hrs · 31,878 cycles

JUST AS BEGAIN DESCENT ONTO MEM RECEIVED LEVEL ONE AIR SYST 3 OFF ALERT AT APPROX IMATELY FL370 ASSOCIATED RED MANF LT NEXT TO #3 BLEED ALSO ILLUMINATED CORRESPONDING PNEUMATIC LINE FROM #3 BLEED TO #3 PACK REMAINED ILLUMINATED FOR APPOXIMATELY 5=10 MINUTES. REMOVED AND REPLACED AFT RUBBER BOOT AND CLAMPS BETWEEN HEAT EXCHANGER AND ACM. REF M/M 21-53-02-2.LEAK CHECKS GOOD.

Part: ADIRU — FAILED (ZONE 100) · airframe 102,976 hrs · 31,863 cycles

AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN QRH. IT APPEARED CAPTAINS AIRSPEED WAS IN ERROR. TRIED TO SELECT AUX CADC. THIS DID NO FIX IT. ENDED UP WITH CAPT ON CADC 2. REMOVED AND REPLACED 1 ADIRU. OPS CHECK NORMAL. PURGED CAPT AND AUX PITOT STATIC LINES. PREFORMED AUTO LAND LLM RTS ON BOTH FCC 1&2 TEST PASSED. REMOVED AND REPLACED AUX ADIRU & TEST NORMAL.

Part: ADC — FAILED (NR 1) · airframe 102,976 hrs · 31,863 cycles

AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN QRH. IT APPEARED CAPTAINS AIRSPEED WAS IN ERROR. TRIED TO SELECT AUX CADC. THIS DID NO FIX IT. ENDED UP WITH CAPT ON CADC 2. REMOVED AND REPLACED 1. OPS CHECK NORMAL. PURGE CAPT AND AUX PITOT STATIC LINES. PREFORMED AUTO LAND LLM RTS ON BOTH FCC 1&2 TEST PASSED

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 102,534 hrs · 31,596 cycles

MDIS 321 33-50 6660 04JAN20 MEM OPEN U LOGPAGES:3133468 EMERGENCY LT BATT 1 LOW VOLTS FACT 05JAN20 22:09 MEM REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPLY OPS CHECK NORMAL REF AMM: 33-51-01-4-0

Part: DIMMER — FAILED (CONTROL PANEL) · airframe 102,295 hrs · 31,475 cycles

DURING CLIMB ABOVE 18,000 FT, OVERHEAD PANEL WENT COMPLETELY DARK. NO INDICATION LIGHTS OF ANY KIND EXCEPT ENGINE IGNITION WERE ILLUMINATED. ON PREFLIGHT THE NR 4 & 5 DISPLAY UNITS BLANKED OUT FOR ABOUT 30 SECONDS & THE HYD PANEL SAID SELECT MANUAL. THOSE ISSUES WENT AWAY AND THE PREFLIGHT PROCEEDED NORMALLY. NOTED O/H PANEL LIGHTING NORMAL ON ARRIVAL TO THE ACFT. MM 33-11-03-2. REMOVED AND REPLACED THE DIMMER, CYCLED POWER BACK AND FORTH BETWEEN GROUND POWER AND APU POWER WITH ALL INDIATIONS NORMAL, RHEOSTAT DIMMED AND BRIGHTENED ALL BACK LIGHTING ON OVERHEAD PANEL, OPS TEST NORMAL IAW 33-11-03-2. ACFT OK TO CONTINUE.

Part: SEAT — FAULTY (COCKPIT) · airframe 102,144 hrs · 31,402 cycles

CREW REPORTS CAPTAINS SEAT WILL NOT MOVE AFT MANUALLY WHEN POSITIONED FWD ALL THE WAY. REMOVED AND REPLACED CAPTAINS SEAT PER AMM 25-11-01-4, FUNCTION CHECK GOOD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

UPPER MAIN DECK SEAT TRACK STA 645, LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 645 TO STATION 664, LBL 107 REF. SRM 53-70-00 FIG. 1 VOL. 1. AND DWG SR10-53-002.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

UPPER MAIN DECK SEAT TRACK STA 735 LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 705 TO 725 REF. SRM 53-70-00 FIG. 1 VOL. 1, SRM 51-31-01 VOL. 2 AND SR10-53-002.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

#1 ACM CORROSION ON INTERCOSTAL AND ATTAHING STRUCTURE STA 554 -595 AT APPROX LONGERON 45R. REMOVED AND REPLACED INTERCOSTAL ACA3816-503 AND SPLICED IN NEW SECTION OF LONGERON ACA3353-3 FROM STA. 560-595 REF. DRAWING ACA3353 AND SRM 53-00-01 FIG. 7 SH.2 VOL.1 REMOVED AND REPLACE CLIPS ACA3816-527,529,525 REFERENCE DRAWING ACA3353.

Part: SKIN — CRACKED (RT WING) · airframe 101,928 hrs · 31,284 cycles

RT WING TOP SURFACE T/E REAR SPAR, ISLAND SECTION BETWEEN I/B AILERON AND O/B FLAP, HAS SEVERAL FASTENERS PULLED THROUGH SKIN AND ONE FASTENER HOLE IS CRACKED. VERIFIED WITH HFEC REPAIRED IAW EA 8-5710-T0347737.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 101,928 hrs · 31,284 cycles

R/H IN/BD FLAP VANE: DELAMINATION FOUND ON UPPER SKIN, O/B SIDE, 8" FROM T/E. APPROX AREA OF DELAM 8" X 7" REPAIRED TO DELAMINATION AREA ON R/H INBD FLAP VANE PER SRM 57-00-01 VOL.I.

Part: CHANNEL — CRACKED (BS 1710) · airframe 101,928 hrs · 31,284 cycles

CENTER CARGO COMPARTMENT: FLOOR ROLLER TRAY HAS A CRACK AT FASTENER HOLE, APPROX. 1" LONG, STA. 1710, RBL 36. REPAIRED CRACK ON ROLLER TRAY PER E.A. 8-2550-T0347453 "CARGO LOADING SYSTEM- ROLLER TRAY CRACK REPAIR".

Part: FLOOR SUPPORT — CORRODED (BS 1821-2007) · airframe 101,928 hrs · 31,284 cycles

MAIN CARGO - FLOOR SUPPORT EXFOLIATED CORROSION FON FLOOR BOARD LAND REMOVED AND REPLACE DAMGED FLOOR SUPPORT REF DAC DWG AGA7544

Part: SKIN — WORN (NR 2 NACELLE) · airframe 101,928 hrs · 31,284 cycles

#2 ENG LH FAN COWL JAMB ON INLET, SKIN FX AJC7415-3 WORN BEYOND LIMITS. REMOVED AND REPLACED WORN SKIN #2 ENG L/H FAN COWL LAND, REF DGLS DRWG AJC7415, SRM-35-01, VOL II, & SRM-33-01, VOL-II.

Part: SKIN — CORRODED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

UPPER AFT FUSE. COMPT: ZONE 312 (DOGHOUSE) RT SKIN FROM STA. 2033-2123 (FWD TO AFT BULKHEAD) SHOWS CORROSION/EXFOLIATION ADJACENT TO SEVERAL NUTPLATES. (AREAS MRKD) REPAIRED PER EA 8-5330-T0347818. RT SKIN PANEL CORROSION, STA. 2116 LONG L11 & L12.

Part: SKIN — CRACKED (LT WING) · airframe 101,928 hrs · 31,284 cycles

LT WING ACCESS DOOR CUT OUT AT XORS 696 HAS 1 EA. ATTACH HOLE WITH A CRACK INDICATION AT THE 5 O'CLOCK POSITION. REPAIRED CRACK INDICATION ON LT WING ACCSS DOOR CUTOUT ATTACH HOLE PER SRM 57-10-00 VOL I, PG 218A JPF ITEM 1: OPEN WORK ITEM: REAM TO REMOVE CRACK INDICATION FOUND ON ATTACH HOLE CORRECTIVE ACTION: REAMED TO REMOVE CRACK INDICATION ON LT WING ACCESS DOOR CUT OUT ATTACH POINT HOLE DIA .321 AT 5 O'CLOCK POSITION PER SRM 57-10-00 PG 218A VOL I., ITEM 2: RII: N/A, OPEN WORK ITEM: NDT TO CHECK REAMED HOLE FOR INDICATIONS CORRECTIVE ACTION: C/W HFEC INSIDE HOLE DIA. NO DEFECTS NOTED PER NDTSPM 93K0393. INSP: ITEM 3: OPEN WORK ITEM: FABRICATE REPAIR BUSHINGS CORRECTIVE ACTION: FABRICATED REPAIR BUSHINGS FOR LT WING ACCESS DOOR CUT OUT ATTACH HOLE PER SRM 57-10-00 VOL I. PG 218A, NOTES: 2 (C)., ITEM 4: OPEN WORK ITEM: INSTALL REPAIR BUSHING CORRECTIVE ACTION: INSTALL REPAIR BUSHING ON LT WING ACCESS DOOR CUT OUT ATTACH HOLE PER SRM 57-10-00, VOL I PG 218A, NOTES: 2 (C)(D).

Part: FRAME — GOUGED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

MAIN DECK: FRAME HAS DEEP GOUGE UNDER "T" BRACKET AT STA 695 BETWEEN LONGERON 16R AND 17R (MARKED AND DOT 71) REPAIRED DAMAGED FRAME REF. SRM 53-30-00 FIG. 5 SHT.1 PAGE 15 VOLUME 1.

Part: SKIN — CRACKED (RT WING) · airframe 101,928 hrs · 31,284 cycles

R/H WING ACCESS DOOR CUT OUT AT XORS 696 HAS 1 EA. ATTACH HOLE WITH A CRACK INDICATION AT THE 7 O'CLOCK POSITION. (MARKED) REPAIRED CRACK INDICATION ON R/H WING ACCESS DOOR CUT OUT ATTACH HOLE PER SRM 57-10-00 VOL.1 PG. 218A JPF ITEM 1: OPEN WORK ITEM: REAM TO REMOVE CRACK INDICATION FOUND ON ATTACH HOLE CORRECTIVE ACTION: REAMED TO REMOVE INDICATION ON R/H WING ACCESS DOOR CUT OUT ATTACH POINT HOLE TO .317 DIA. AT 7 O'CLOCK POSITION PER SRM 57-10-00 PG. 218A VOL.1 ITEM 2: RII:N/A, OPEN ITEM: NDT TO CHECK REAMED HOLE FOR INDICATIONS CORRECTIVE ACTION: C/W HFEC INSIDE HOLE DIA. NO DEFECTS NOTED PER NDTSRM 93K0393 INSP. ITEM 3: OPEN WORK ITEM : FABRIACTE REPAIR BUSHING, CORRECTIVE ITEM: FABRICATED REPAIR BUSHING FOR R/H WING ACCESS DOOR CUT OUT ATTACH HOLE PER SRM 57-10-00 VOL.1 PG. 218A, NOTES: 2 (C)., MECH: JJ 5093341 ITEM 4: OPEN WORK ITEM: INSTALL REPAIR BUSHING, CORRECTIVE ACTION: INSTALL REPAIR BUSHING ON R/H WING ACCESS DOOR CUT OUT ATTACH HOLE PER SRM 57-10-00 VOL.1 PG. 218A, NOTES 2 (C)(D).

Part: BRACKET — CORRODED (BS 1021) · airframe 101,928 hrs · 31,284 cycles

FWD CARGO COMPT STA1021 BY LONG52, STRAP/DOUBLER CRACK/CORROSION BY FASTENER (MARKED) REMOVED CORRODED NDA6014-5 ANGLE BRACKET. FABRICATED AND INSTALLED NEW -5 ANGLE BRACKET AND LONGERON REPAIR CHANNEL REF. E.A 8-5310-T0347392 "FUSELAGE- MAINFRAME-FWD CARGO COMPT. LONGERON 52".

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 101,928 hrs · 31,284 cycles

CTR CARGO COMPT BILGE, CORROSION ON CARGO TRACK, STA 1781 L42 RT. (MARKED) REPAIRED PER EA T8-5321-T0347816 P1,P2.

Part: CHANNEL — CORRODED (BS 1770) · airframe 101,928 hrs · 31,284 cycles

CTR CARGO COMPT BILGE, CORROSION ON BOTTOM SIDE OF CARGO TRACK, STA 1770 L42 L/H. REMOVED AND REPLACED CHANNEL REF DWG NFJ 6010

Part: FRAME — CORRODED (BS 1907) · airframe 101,928 hrs · 31,284 cycles

AFT CARGO COMPT BS 1907 11LBL FRAME HAS CORROSION. REPAIRED FRAME REF SRM CH 53-30-00,FIG 4, VOL1.

Part: SUPPORT ANGLE — CORRODED (BS 1841) · airframe 101,928 hrs · 31,284 cycles

AFT CARGO COMPT STA1841 30RBL HAS CORROSION UNDERSIDE. REMOVED AND REPLACED AGA7170-19 SUPPORT ANGLE PER DWG. AGA7170

Part: FRAME SPLICE — CORRODED (BS 1701) · airframe 101,928 hrs · 31,284 cycles

CTR CARGO COMPT BILGE, CORROSION ON FRAME REPAIR ANGLE AT STA 1701 L51. (MARKED) REMOVED AND REPLACED PREVIOUSLY INSTALLED FRAME SPLICE REPAIR ANGLE AT STA. 1701 LONG 52C TO 50R. REF SRM 53-30-00 FIG 5 & FIG 8 VOL I, DRAWING AFA0012

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

AFT CARGO COMPT STA1851 LONG48L TO 46L SHEAR TIE LEGS HAS CORROSION (MARKED) REPLACED SHEAR CLIP, REF SRM CH 53-30-00,FIG 10, VOL 1.

Part: SKIN — DENTED (RT AILERON) · airframe 101,928 hrs · 31,284 cycles

RH INBD AILERON LOWER SURFACE HAS A GOUGE APPROX 6 BY 2 INCHES. REF WRI (27105212). REPAIRED R/H INBD. AILERON LOWER SKIN PER SRM57-10-00 FIG. 85 SHT. 1, VOL.1 REFERENCE E.A. 8-5750-T0347271"WINGS-RH INBD. AILERON LOWER SURFACE PLATING REPAIR-RSC TRACKING"

Part: STRIP — DAMAGED (FUSELAGE) · airframe 101,928 hrs · 31,284 cycles

LT MLG W/W: GEAR STRUT DOOR OPENING REAR ON AUX STRUCTURE. (T/E BEAM AUXILIARY STRUCTURE), APPROX 15" FROM W/W OPENING THERE IS A SMALL HOLE IN AUX STRUCTURE WITH LITTLE EDGE DISTANCE. HOLE IS COUNTERSUNK ON UPPER AND LOWER SIDES. ADJACENT STAINLESS CHAFE STRIP IS ALSO DAMAGED. MARKED. REPAIRED PER EA 8-5710-T0347847.

Part: SEAT TRACK — WORN (BS 485-536) · airframe 101,928 hrs · 31,284 cycles

MAIN DECK SEAT TRACK SHOWING DAMAGE AT STA 520, RBL 48.(MARKED) REPLACED DAMAGED SEAT TRACK FROM RBL -48 ,STA 485 TO STA 536. REF SRM 53-70-00 FIG1. VOL1. FDX DWG SR10-53-002 AND SRM 51-31-01 VOL2.

Part: BATTERY — LOW (CABIN) · airframe 101,580 hrs · 31,103 cycles

EMER LT BAT 1 LO. RELEASED FOR SERVICE PER MEL 33-50-02 CATEGORY C EXPIRATION : 28FEB19. MEL 33-50-02: EMER LIGHTS - INOP.

Part: CLAMP — LOOSE (HEAT EXCHANGER) · airframe 101,563 hrs · 31,090 cycles

PDIS 321 36-22 5781 10FEB19 ABQ OPEN U LOGPAGES:3072516 AT FL350 MANF 1 ON AIR STATUS PAGE WENT RED.FOLLOWED BY A LEVEL 3 AIR MANF 1 FAIL ALERT. AIRCRAFT SYSTEMS TURNED #1 BLEED TO OFF AND CREW ACCOMPLISHED QRH INFO 10FEB19 17:38 MEM R WITH PACKS OPERATING FOUND 2 EACH SLEEVE COUPLER SEALS GOING INTO BOTH HEAT EXCHANGERS LEAKING AND CLAMPS LOOSE. RESECURED CLAMPS ON BOTH PACKS. REF JRH, RAN ALL 3 ENGINES APPROXIMATELY 10 MINTUES BOOSTING POWER ON #1 UP TO 85%N2 FOR VALVE SHIFT INDICATION. ALL INDICATIONS NORMAL. NO FAULTS NOTED DURING RUN. ACFT OK FOR SERVICE

Part: SWITCH — LOOSE (L1 DOOR) · airframe 101,396 hrs · 31,003 cycles

MDIS 321 25-60 5644 01JAN19 MTY OPEN U LOGPAGES:2862948 RT MAIN DOOR EVAC SLIDE TEST SWITCH WILL NO ILUMINATED. MEL 01JAN19 00:00 MTY U RELEASED FOR SERVICE PER MEL : 25-61-01 CATEGORY : C EXPIRATION : 11JAN19 "MEL 25-61-01: EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY." VERIFIED SYSTEM WORKS WITH PUSHBUTTOM FROM L1 DOOR OK C/7169023 FACT 02JAN19 16:25 GDL FOUND SW METAL TAB AND RE-SECURED ALL SW ASSY OPS CK GOOD PER AMM 25-61-03-5.

Part: SWITCH — NO TEST (DOOR SLIDE) · airframe 101,384 hrs · 30,997 cycles

RT HAND TROOP DOOR EVAC SLIDE TEST SWITCH WILL NOT ILLUMINATE WHEN DEPRESSED. REMOVED AND REPLACED R/H DOOR EVAC PUSH BUTTON SWITCH I.A.W 25-61-03-02 AND OPERATIONAL CHECK C/O OK IAW 25-61-03-5. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 101,278 hrs · 30,945 cycles

FWD A/C PACK EXHAUST DOOR LOWER AFT CORNER FUSELAGE SKIN CRACK. REPAIRED CRACKED SKIN PER SRM 53-50-00 FIG 3A AND EA 8-5330-T0343870 P2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 101,278 hrs · 30,945 cycles

FWD A/C PACK EXHAUST DOOR LOWER FWD CORNER FUSELAGE SKIN CRACK. REPAIRED CRACKED SKIN PER SRM 53-50-00 FIG 3A AN EA 8-5330-T0343870 P1.

Part: PITOT TUBE — CLOGGED (FIRST OFFICER'S) · airframe 100,940 hrs · 30,755 cycles

MODERATE RAIN, ALL ANTI-ICE SYSTEMS ON. DURING DESCENT, RECEIVED IAS COMPARTER ALERT FOLLOWED SHORTLY BY SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVRD LEVEL 2 ALERTS. ALSO RECEIVED A/P AND ATS DISCONNECTED. SUSPECT F/O PITOT STATIC FROZEN. FOLLOWED QRH FOR AIRSPEED UNRELIABLE ONCE IN WARMER TEMPERATURES. RECONNECTED THE A/P AND ATS AND ALL INDICATIONS WERE NORMAL. INSPECTED AND LEAK TESTED THE CAPTAIN`S, AUX & FIRST OFFICER`S PITOT STATIC SYSTEM IAW AMM: 34-11-00-2. FOUND DRAIN HOLES IN F/O'S PITOT TUBE PLUGGED. PURGED THE FIRST OFFICER'S PITOT SYSTEM AND CAPTURED, CONFIRMED PRESENCE OF BIOLOGICAL DEBRIS. REMOVED AND REPLACED THE FIRST OFFICER'S PITOT TUBE IAW AMM 34-11-02-2, AND OPS CHECKED GOOD, ALL PITOT STATIC CHECKS WERE GOOD. HEAT TESTED GOOD IAW AMM 34-16-00-5. ACCOMPLISHED A NR 1 & 2 FCC AFS TESTS AND ALL TESTS PASSED IAW AMM 22-00-00-2.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 99,611 hrs · 30,077 cycles

IN FLT AT ALL ALTITUDES AND AIRSPEEDS, WHEN DEPLOYING SPOILERS, AIRCRAFT ROLLED LEFT 5* AOB W ITH 1/3 SPOILER, 7* AOB WITH 2/3 SPOILERS, AND 10* AOB WITH FULL SPOILER. WHEN SPOILERS RETRACTED, PULLED BACK RIGHT. LEAD TO UP TO 0.5NM OFF TRACK W/SPOILERS DEPLOYED. NO ROLL NOTED WITH SLATS EXTENDED. PERFORMED SPOILER SYSTEM FAULT ISOLATION REF AMM 27-60-00-2. NO FAULTS NOTED AT THIS TIME. CLEANED AND LUBRICATED SPOILER ACTUATORS REF AMM 12-21-04-3. PERFORMED SPOILERS SYSTEM OPERATIONAL CHECK REF AMM 27-60-00-2. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 99,103 hrs · 29,824 cycles

LEFT MLG OUTBD LOWER SUPPORT BEAM HAS A CRACKED RAIL. REPAIR SUPPORT REF DWG ANB7203.

Part: WEB — CRACKED (BS 488-494) · airframe 99,103 hrs · 29,824 cycles

LEFT NOSE GEAR WHEEL WELL SUPPORT BEAM WEB AT Z=64 BETWEEN BS 488 AND 494 HAS THREE CRACKS AT FASTENER HOLES. REPAIRED THE WEB IAW SRM 53-00-01, FIG 10, SHEET 4, AND FIG 10, SHEET 5, VOL 1.

Part: WEB — CRACKED (BS 473) · airframe 99,103 hrs · 29,824 cycles

RIGHT NOSE GEAR WHEEL WELL SUPPORT BEAM WEB AT BS 473 AND Z=55.5 HAS THREE CRACKS AT FASTENER HOLES. REPAIRED THE WEB IAW SRM 53-00-01, FIG 10, SHT 4, VOL 1.

Part: WEB — CRACKED (NLG WW) · airframe 99,103 hrs · 29,824 cycles

NOSE LANDING GEAR, LEFT INNER WEB UPPER CORNER HAS CRACK. REPAIRED IAW SRM 53-00-01 FIG 10, SHEET 4, PG 50, VOL I. MAJOR REPAIR.

Part: ANGLE — CRACKED (RT WING) · airframe 99,103 hrs · 29,824 cycles

RIGHT WING SLAT DRIVE PANEL OTBD ANGLE IS CRACKED IN 2 PLACES. REMOVED AND REPLACED IAW SRM 51-31-01,VOL 2, AND DWG ARB2918.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 99,103 hrs · 29,824 cycles

FLOOR SUPPORT CORRODED IN TWO SPOTS. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-31-01, V2, AND DWG SR84864.

Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 99,103 hrs · 29,824 cycles

SPOILER SKIN HAS DELAMINATION UNDER THE SIDE OTBD AREA. PERFORM A TAP TEST IAW SRM 51-61-01, VOL II, AND REPAIRED IAW SRM 51-71-00, VOL II. FOUND BEYOND ECONOMICAL REPAIR. R & R THE RT NR 3 SPOILER AND OPS CHECKED GOOD IAW AMM 27-60-01-4.

Part: SKIN — DELAMINATED (LEFT ELEVATOR) · airframe 99,103 hrs · 29,824 cycles

LEFT OTBD ELEVATOR EXTERIOR STRUCTURE TRAILING EDGE, NEAR MID SECTION SHOWS SEPARATION AND LOOSE FROM FASTNERS. REMOVED AND REPLACED THE LT OTBD ELEVATOR TRAILING EDGE IAW SRM 55-30-00, VOL I, PAGE 5.

Part: FLOOR SUPPORT — CORRODED (BS 879) · airframe 99,103 hrs · 29,824 cycles

FWD CARGO BS 879 RIGHT OF CENTER FLOORBOARD TEE SUPPORT IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG ADA 3626.

Part: FLOOR SUPPORT — CORRODED (BS 879) · airframe 99,103 hrs · 29,824 cycles

FWD CARGO BS 879 LEFT OF CENTER FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG ADA 3626.

Part: BULKHEAD WEB — CRACKED (BS 1841) · airframe 99,103 hrs · 29,824 cycles

CENTER CARGO BAY, BS 1841 AFT BULKHEAD WEB AT CENTER FLOORLINE LONGERON 52 FOUND CRACKED. REPAIRED DAMAGED AFT BULKHEAD WEB IAW SRM 53-00-01, FIG 10, VOL 1.

Part: ANGLE — CRACKED (RT WING) · airframe 99,103 hrs · 29,824 cycles

RIGHT WING OTBD OF FUELING PANEL ANGLE CRACKED. REPAIRED THE ANGLE IAW SRM 57-20-00, FIG 1. SHEET 6.

Part: CARGO TRACK — WORN (BS 1341) · airframe 99,103 hrs · 29,824 cycles

MAIN CARGO BAY BS 1341, LBL 47.50, CARGO TRACK GOUGED. REPLACED THE SEAT TRACK BS 1285 - 1411 IAW SRM 53-70-00, FIG 1, VOL 1.

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 99,103 hrs · 29,824 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT BS 520, RBL 48. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 2A, SHEET 2, PAGES 10 AND 11, VOL. 1.

Part: CARGO TRACK — GOUGED (BS 1441) · airframe 99,103 hrs · 29,824 cycles

MAIN CARGO BAY BS 1441 RBL 27.50 , CARGO TRACK GOUGED. REPLACED DAMAGED CARGO TRACK, BS 1431 TO 1451, RBL 27.50 IAW SRM 53-70-00, FIG 1, VOL 1.

Part: SWITCH — INOPERATIVE (EVAC SLIDE) · airframe 98,919 hrs · 29,752 cycles

R1 SLIDE PRESS TO TEST SWITCH INOPERATIVE. WHEN SLIDE PTT SWITCH IS FULLY SECURED, INDICATION LIGHT REMAINS ON. UNABLE TO VERIFY SLIDE PRESSURE. REMOVED AND REPLACED R1 EVACUATION SLIDE IAW AMM 25-61-01-2. PRESSURE INDICATOR LIGHT OPS CHECKED GOOD.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 98,028 hrs · 29,348 cycles

R1 DOOR SLIDE PRESSURE LIGHT WILL NOT PRESS TO TEST. REPLACED REMOTE SLIDE PACK PRESSURE INDICATOR IAW AMM 25-61-03-2.

Part: WIRE — DISCONNECTED (SWITCH) · airframe 98,005 hrs · 29,335 cycles

R1 DOOR SLIDE REMOTE PRESS-TO-TEST FOUND INOPERATIVE. FOUND TERMINAL DISCONNECTED FROM BACK OF PUSH BUTTON SWITCH. ASSEMBLED PUSH BUTTON SWITCH AND PRESS-TO-TEST LIGHT OPS CHECKED GOOD. IAW AMM 25-61-03-2. OK FOR SERVICE.

Part: BRAKE — FAILED (NR 7) · airframe 96,931 hrs · 28,884 cycles

FOUND NR 7 BRAKE HAS EVIDENCE OF A ROTOR OR STATOR COMING APART, CARBON FLAKES, NEAR THE BRAKES PISTONS. R & R NR 7 MAIN BRAKE ASSEMBLY IAW MM 32-43-01-4. INSPECTED NR 7 AXLE, NR 7 WHEEL & TIRE ASSEMBLY & ADJACENT AREAS, NO FURTHER DEFECTS OR DAMAGE NOTED. ALL DAMAGE CONTAINED WITHIN NR 7 MAIN BRAKE ASSEMBLY. OPERATIONS CHECKED SATISFACTORY, NO LEAKS NOTED.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 961 hrs · 28,557 cycles

ON CLIMB OUT, PASSING FL 180, OIL QTY RAPIDLY DECREASED TO 0. OIL PRESSURE DROPPED TO BELOW 12 PSI. OIL TEMP INCREASED TO 147 DEGREES & CLIMBING, IAW QRH ENGINE SHUTDOWN. INSTALLED NR 2 ENGINE IAW WC 71T1710. OPS & LEAK CHECKED NORMAL. OK FOR SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 960 hrs · 28,495 cycles

CORROSION CLEANED & TREAT CORROSION.

Part: SKIN — DAMAGED (ACCESS DOOR) · airframe 960 hrs · 28,495 cycles

RIGHT ACCESS DOOR 618FB FOR SLAT DRIVE MECHANISM, 3IN X 2IN SECTION OF OUTER SKIN TORN. REPAIRED IAW SRM 51-71-00 VOL 2 & PAINTED IAW SRM 51-21-02 VOL 2.

Part: SKIN — DENTED (BS 449) · airframe 960 hrs · 28,495 cycles

FUSELAGE SKIN ON RIGHT SIDE APPROXIMATE BS 449, Z LOCATION APPROXIMATELY 40 HAS VERTICAL BUCKLING. N/R 432 WRITTEN FOR PREVIOUS REPAIR IN SAME AREA. FOUND SKIN WITHIN LIMITS IAW SRM 53-20-00 FIG 13 PAGE 116 PARA 1.

Part: SKIN — CORRODED (ZONE 600) · airframe 960 hrs · 28,495 cycles

RIGHT WING LOWER TE INTERIOR SKIN CORRODED. PILLOWED AROUND FASTENERS & 1 SHEARED. MARKED STATION XW920. REPAIR IAW SRM 57-00-01 FIG 4 SHT 2.

Part: DOUBLER — CORRODED (FUSEALAGE) · airframe 960 hrs · 28,495 cycles

BULGING DOUBLER. REMOVE DOUBLER INSPECTION.

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 960 hrs · 28,495 cycles

CRACK FOUND ON CORE COWL NEXT TO PREVIOUS WELD REPAIR. WELD IAW 70-41-00.

Part: SEAT TRACK — WORN (NOT REPORTED) · airframe 960 hrs · 28,495 cycles

SEAT TRACK WORN. R & R DAMAGE SECTION OF TRACK.

Part: FLOOR SUPPORT — CORRODED (BS 1521) · corrosion level 2 · airframe 960 hrs · 28,495 cycles

MAIN DECK FLOOR SUPPORT BEAM LOWER SURFACE IS EXFOLIATED WITH HEAVY CORROSION AT BS 1521, RBL 30. REPAIRED IAW SM 53-00-01 FIG 7 AND SRM 51-21-01 VOL I.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 960 hrs · 28,495 cycles

MAIN DECK ABOVE CTR WW AREA, THE FINGER DOUBLER IS BULGED WITH SIGNS OF CORROSION BETWEEN STATION 1501 & 1521, RBL 30. REPAIRED CORRODED AREA IAW EA 8-5330-T0319219. CLASSIFIED AS A MAJOR REPAIR.

Part: PANEL — GOUGED (RT WING) · airframe 960 hrs · 28,495 cycles

RIGHT WING PANEL 618BT HAS A DEEP GOUGE. REPAIRED RT SIDE PANEL 618BT IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02.

Part: BATTERY — FAILED (CABIN) · airframe 955 hrs · 28,260 cycles

ON PREFLIGHT GOT, EMER LIGHT BATTERY 1 LOW, MSG. R & R EMER EXIT LIGHTS BATTERY IAW AMM 33-51-01-4. TESTED GOOD. OK TO CONTINUE SERVICE.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 94,165 hrs · 27,645 cycles

STANDBY ALTITUDE UNUSABLE. DURING CLIMB THE ALTIMETER STUCK AT 11, 5, 12, 4, 14, 7, 15, 5, 17, 4, 18, 6, 19, 3, 19, 5, 20 & 4 & OTHER ALTITUDES AFTER REACHING 350 THE ALTIMETER FINALLY CAUGHT UP TO THE OTHER ALTIMETERS. ON DESCENT STBY ALT STUCK MULTIPLE TIMES. R & R STBY ALTIMETER. OPERATIONS CHECKED NORMAL.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 94,165 hrs · 27,645 cycles

STANDBY ALTIMETER LAGS BY 1000' DURING CLIMB OUT. COMPLIED WITH STANDBY ALT & AIRSPEED INDICATOR TEST. TEST IS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 94,011 hrs · 27,583 cycles

ALL 4 BULBS ON EMER POWER INDICATOR BURNED OUT. R & R BULBS IAW SMP. OPERATIONS CHECKED GOOD, FINAL CLOSED.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 93,801 hrs · 27,488 cycles

DTW OPEN RIGHT AFTER LOAD CREW EXITED ACFT. MX FOUND L1 DOOR OUTSIDE DOOR ARMING HANDLE PUSHED IN FLUSH TO ACFT. ATTEMPTED TO OPEN DOOR & DOOR BLEW WITH SLIDE FALLING OUT ONTO THE CREW STAIRS. INSPECTED DISARM HANDLE & ALL OPERATION IS NORMAL & NO DAMAGE TO L1 DOOR OR TRACK. R & R L1 SLIDE ASSEMBLY IAW AMM 25-61-01-2-0.

Part: CHECK VALVE — FAILED (NR 1 ENG BLEED) · airframe 93,427 hrs · 27,314 cycles

DURING INITIAL DECENT FROM 350 NR 1 ENGINE BEGAN A THUMPING NOISE ALONG WITH DECAY IN N1 & RISING. EGT N2 WAS MATCHING NR 2 & 3 ENGINES. ENGINE SHUTDOWN, CHECKLIST ACCOMPLISHED, MANUAL SHUT DOWN NR 1 ENGINE FIRE BOTTLE DISCHARGED. REMOVED NR 1 ENGINE LOW PRESSURE BLEED CHECK VALVE IAW AMM 36-11-03-2. FOUND STOP TUBE INSIDE THE CHECK VALVE SHEARED & MISSING. NR 1 ENGINE STALL INSPECTION & CHECK CARRIED OUT IAW AMM 72-00-00-6-1. LOW PRESSURE CHECK VALVE R & R IAW AMM 36-11-03-2. NR 1 ENGINE IDLE RUN CARRIED OUT IAW JRH. ALL PARAMETERS & INDICATION NORMAL. ACFT OK FOR SERVICE.

Part: INDICATOR — FAILED (SLIDE PRESSURE) · airframe 93,268 hrs · 27,253 cycles

DOOR EVACUATION SLIDE REMOTE PRESS-TO-TEST SWITCH DOESN'T LIGHT WHEN PRESSED. REPLACED LAMP AND CHANGED BATTERIES IAW AMM 25-61-03-2, SWITCH STILL DOES NOT LIGHT WHEN PRESSED. REMOVED AND REPLACED THE R1 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR IAW AMM 25-61-03-2. OPS CHECKED GOOD.

Part: FAIRING — DELAMINATED (CARGO DOOR) · airframe 93,252 hrs · 27,244 cycles

FOUND CENTER CARGO DOOR FAIRING DELAMINATED IN CENTER OF FAIRING FROM FORWARD EDGE TO AFT EDGE. INSTALLED NEW CENTER CARGO DOOR FAIRING IAW SRM 51-31-01.

Part: BATTERY — FAILED (SLIDE PRESSURE) · airframe 93,003 hrs · 27,135 cycles

ESCAPE SLIDE TEST LIGHT INOPERATIVE. REMOVED SLIDE COVER IAW AMM 25-61-01-2 AND REPLACED BATTERIES FOR SLIDE BOTTLE PRESSURE LIGHT. OPS CHECKED NORMAL IAW AMM 25-61-03-5. OK FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (LT ELEVATOR) · airframe 90,206 hrs · 25,980 cycles

DURING DESCENT, FL300 BELOW LT OTBD ELEVATOR FLUCTATED UP & DOWN ON CONFIGURATION PAGE. AT 3000 FT ON APPROACH- FELT CYCLING IN YOKE TO A BUFFETING- AUTOPILOT OFF- WENT AROUND-AUTOPILOT SEEMS TO HELP. IAW CREW DEBRIEF, THEY NOTICED ISSUE DURING PREFLIGHT CHECK PRIOR TO DEPARTURE SEEMED TO GO AWAY CONTINUED ON. AFTER BLOCK IN RAN HYD AND CYCLED ELEVATORS SEVERAL TIMES NOTICED A RATCHETING IN CONTROL COLUMN AND AN AUDIBLE HISSING SOUND FROM GROUND, APPEARS TO BE FROM LT INBD ELEVATOR ACTUATOR AREA, WHEN HYD ON AND NO MOVEMENT. RT SIDE NORMAL. TRIED TO LOCATE HISSING SOUND TRACED IT TO AFT ACCESSORY COMPT. RAN HYD, CYCLED ELEVATOR THROUGH MULTIPLE TIMES WITH STAB SETTING AROUND 1.3. THE HISS IS MORE PRONOUNCED AND THE RACHETING THROUGH THE CONTROLS FROM ALL THE FWD BACK THROUGH NEUTRAL. THE VIBRATION SHAKES THE WHOLE ACFT AND IS VISABLE THROUGH THE ELEV LINKAGE. WHEN STAB SETTING IS GREATER THAN 2 SMOOTH MOVEMENT AND SOUND SUBSIDES. NO FLUID LEAKAGE NOTED IN THIS COMPT OR FROM ANY ELEVATOR ACTUATORS. THE VIBRATION IS MOST NOTICABLE AT CURRENT STAB SETTING 1.3. REMOVED AND REPLACED RT OB ELEVATOR ACTUATOR THROUGH STEP 29 AND COMPLETED RIGGING.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 90,070 hrs · 25,921 cycles

CRACK FOUND ON RT LOWER AFT VERTICAL STABILIZER BULKHEAD FITTING. NR 4 BANJO FITTING RT LEG FOUND CRACKED EMANATING FROM CENTER HOLE ALONG RADIUS PASS LOWER FASTENER. REMOVED PAINT & BURNISHED AREAS FOR NDT IAW 51-00-01. REPAIRED IAW EA 8-5530-156730. VERIFY END OF CRACK, CHECK EXISTING HOLES FOR CRACK. ITEM 1 VERIFIED END OF CRACK & EXISTING FASTENER HOLES. ITEM 2 STOP DRILL CRACK TO .025 IAW SRM 51-00-01. ITEM 3 VERIFIED STOP DRILL HOLE HFEC NDT SPMT PMDC-93K.

Part: LONGERON — CRACKED (BS 1997 L47L) · airframe 90,070 hrs · 25,921 cycles

LONGERON 47L CRACKED ON THE INBD SIDE AT BS 1997. R & R LONGERON IAW DWG NGA6313.

Part: LONGERON — CRACKED (BS 1997 L45L) · airframe 90,070 hrs · 25,921 cycles

AFT FUSELAGE, WASTE COMPARTMENT LONGERON 45L CRACKED ALONG THE OTBD SIDE AT BS 1997. REMOVED AND REPLACED LONGERON PER SRM 51-33-01 VOL. II

Part: WARNING LIGHT — MULTIPLE FAIL · airframe 88,871 hrs · 25,456 cycles

AT FL 340, 2 10 HR IN FLT, BLEED NR 1 OFF ALERT FOLLOWED 1 MIN LATER WITH LEVEL 3 AIR MANF 1 FAIL ALERT. NR 1 AIR SYSTEM SHOWED 25 PSI STILL IN SYSTEM WHEN ALERT DISPLAYED. 5 MIN LATER, LEVEL 3 ALERT EXTINGUISHED AS PRESSURE DROPPED TO LESS THAN 5. FOUND LT WING DIFFERENTIAL PRESSURE SWITCH FAULT BALL TRIPPED. R & R LT WING DIFFERENTIAL PRESSURE SWITCH IAW MM 36-23-03-4. PERFORMED LEAK CHECK. NO LEAKS NOTED. COMPLIED WITH NR 1 PNEUMATIC SYS DECAY CHECK IAW MM 36-00-01-5. DECAY CHECKED OK. ACCOMPLISHED NR 1 MANIFOLD FAILURE DETECTION PRESSURE SWITCH ADJUSTMENT AND TEST WITH NORMAL RESULTS REF MM 36-23-03-5. OK TO CONTINUE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 87,399 hrs · 24,895 cycles

CREW AND JUMPSEATER SMELLED ACRID ELEC ODOR FOLLOWED BY CONSIDERABLE AMOUNT OF SMOKE IN COCKPIT. DECLARED EMERGENCY AND LANDED.

Part: COALESCER BAG — ODOR · airframe 87,399 hrs · 24,895 cycles

CREW AND JUMPSEATER SMELLED ACRID ELEC ODOR FOLLOWED BY CONSIDERABLE AMOUNT OF SMOKE IN COCKPIT. DECLARED EMERGENCY AND LANDED. PERFORMED GENERAL VISUAL INSP OF E&E BAY NO ODOR OR APPEARANCE OF SMOKE FOUND ALL DUCTING APPEARED NORMAL. PERFORMED GVI OF UPPER DECK CARGO AREA, FOUND NO EVIDENCE OF ELECTRICAL FIRE OR MALFUNCTION. NO MALODOROUS SMELLS DETECTED. ALL CIRCUIT BREAKERS WERE SET, ALL EQUIPMENT WAS IN WORKING ORDER IAW CREW DEBRIEF. IAW MOCC CHANGING COALESCER BAGS AFTER ENGINE RUN. INSTALLED NR1, NR2, AND NR3 PACK COALESCERS IAW AMM 21-54-03-2. RAN ALL 3 ENGINES IAW JRH FOR 30 MIN. DURING ENGINE RUN, TURNED ON ALL 3 PACS INDIVIDUALLY. NO SMOKE SMELL OR SMOKE IN THE COCKPIT NOTED FROM THE PACS UTILIZING ENG BLEED AIR. WITH PACS ON ALSO CHANGED ENG THROTTLE POWER SETTINGS AND STILL NO SMOKE IN THE COCKPIT OR SMELL OF SMOKE. ACFT OK FOR FLIGHT AT THIS TIME.

Part: RELAY — MALFUNCTIONED · airframe 87,031 hrs · 24,762 cycles

AFTER TAKEOFF, ENG ANTI-ICE ON, RECEIVED AIR SYS 2 LEVEL 1 ALERT. 45 SECS LATER RECEIVED MANF 2 FAIL LEVEL 3 ALERT. COMPLIED WITH QRH & DIVERTED. AFTER 4 MINS WITH NR 2 ENG AT IDLE, LEVEL 3 ALERT OUT. RELEASED FOR SERVICE IAW MEL: 36-23-01-02. ON MANF FAIL DET BOX IN CAC, NO FAULTS, AIU NR 1 SHOWED NO CURRENT OR FAULT LAST LEG FAULTS. DECAY CHK ON NR 2 PNEU SYS FOR 32 SECS IAW MM 36-00-01-5, 20 SECS MIN REQUIRED. COMPLIED WITH MEL. MFDC & SENSE ELEMENTS CHK OK IAW MM 36-23-00-0. R & R R2-8990 AS PRECAUTION IAW SMP. MFDC & SENSE ELEMENTS CHK OK IAW MM 36-23-00-0. RAN NR 2 ENG IAW JRH, THROUGH POWER SETTINGS WITH PNEUMATICS ON, NO DEFECTS. DECAY CHK PREV COMPLIED WITH NO HISTORY FOR 99 DAYS. OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 86,548 hrs · 24,590 cycles

MAIN CABIN FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — CRACKED (ZONE 200) · airframe 86,548 hrs · 24,590 cycles

MAIN CABIN FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.

Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 86,548 hrs · 24,590 cycles

MAIN CABIN FOUND CRACK ON WEB JAMB DOOR. REPAIRED AREA IAW SRM 53-50-00 FIG 19 VOL I.

Part: CHANNEL — CORRODED (BS 886) · corrosion level 2 · airframe 86,548 hrs · 24,590 cycles

FWD CARGO COMPT, STA 866 X= 58, FOUND EXFOLIATION CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 86,548 hrs · 24,590 cycles

CTR CARGO COMP STA 1701, X=-34, Z=-100, LWR FLOORBEAM FLANGE WITH 1EA CRACK 7,5 " LONG REPAIRED AREA IAW SRM 53-60-01 FIG 3, VOL I.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 86,548 hrs · 24,590 cycles

CTR CARGO COMPT, STA 1701 X= 34, Z=-100, FLOORBEAM LWR FLANGE WITH 1EA CRACK 3" LONG AND 1EA CRACK 1" LONG. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I.

Part: SEAT TRACK — CORRODED (BS 464) · corrosion level 2 · airframe 86,548 hrs · 24,590 cycles

MAIN CABIN ENTRY WAY SEVERE INTERGRANULAR CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.

Part: FRAME — CRACKED (ZONE 700) · airframe 86,548 hrs · 24,590 cycles

LT MLG WW FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-00-01 FIG 8 SHT 2 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,548 hrs · 24,590 cycles

LT AIR CONDITIONING COMPT FOUND SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & SRM 53-40-00 FIG 15 VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 86,548 hrs · 24,590 cycles

RT WING, OTBD AILERON UPPER SURFACE FOUND 1EA CRACK 1 INCH LONG ON UPPER SKIN AND DEFORMED ON RIB AT STA XOA 1024 REPAIR IAW SRM 57-10-00 VOL I, FIG.85.

Part: SKIN — WORN (RT WING LE SLAT) · airframe 86,548 hrs · 24,590 cycles

RT L/E SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN L/E DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG.4 VOL 3 AND SRM 57-00-01 FIG 4 SHEET 2 VOL 1.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 86,548 hrs · 24,590 cycles

COCKPIT, CRACK 2 INCHES LONG ON HORIZ WEB AT STA 276, X=-47, Z=-4 REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2 AND FIG 10, SHEET 1, VOL 1.

Part: RIB — CRACKED (ZONE 600) · airframe 86,548 hrs · 24,590 cycles

RT WING INTERNAL L/E FOUND CRACK 1 INCH LONG ON INTERNAL RIB AT STA XOS 691 REPAIR FORMER IAW SRM 57-00-01 VOL 1, FIG 10, SHT 1.

Part: SKIN — WORN (LT WING LE SLAT) · airframe 86,548 hrs · 24,590 cycles

LT WING SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN SLAT DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG 4, VOL 3 AND SRM 57-00-01 FIG4, SHEET 2, VOL.1

Part: BULKHEAD — CRACKED (BS 305) · airframe 86,548 hrs · 24,590 cycles

COCKPIT, FOUND 1EA CRACK 2 INCHES LONG ON HORIZ WEB AT STA 305, X=-14 REPAIR MEMBRANE IAW SRM 53-00-01 FIG 4, SHT 2, VOL 1.

Part: SKIN — CRACKED (ZONE 600) · airframe 86,548 hrs · 24,590 cycles

RT WING INTERNAL L/E FOUND 1EA CRACK 3 INCHES LONG ON INTERNAL SKIN DOUBLER UPPER AT STA XOS 667. REPAIR BEADED DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.

Part: BULKHEAD — CRACKED (BS 305) · airframe 86,548 hrs · 24,590 cycles

COCKPIT, 1EA CRACK 2 INCHES LONG ON HORIZ WEB AT STA 305, X= 14 REPAIR MEMBRANE IAW SRM 53-00-01 FIG 4, SHEET 2 VOL 1.

Part: STRAP — CRACKED (ZONE 100) · airframe 86,548 hrs · 24,590 cycles

FWD AVIONICS COMPARTMENT, AFTER NOSE SKIN REMOVAL WITH OAN J/C SP10530242-7002- 4JR, FOUND CRACK ON INTERNAL SPLICE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: ANGLE — CRACKED (ZONE 100) · airframe 86,548 hrs · 24,590 cycles

LEFT AIR CONDITIONING COMPT CRACK ON ANGLE. REPAIRED AREA IAW SRM 53-00-01 FIG 2 SHT 2 VOL I.

Part: SKIN — CRACKED (ZONE 300) · airframe 86,548 hrs · 24,590 cycles

DURING U/S INSP OF HORIZONTAL STB, CONSTANT SECTION, FOUND PANEL P/N 7226-1 & 7224-1 LOWER INTERIOR SKIN PANELS WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-130928.

Part: SKIN — DENTED (ZONE 100) · airframe 84,198 hrs · 23,464 cycles

DIRECTLY INLINE WITH AFT CARGO COMPARTMENT DOOR FORWARD FRAME ON LOWER BELLY SKIN ARE 2 SCRATCHES/CREASED ACROSS BELLY STRINGERS APR 4 1/2 FEET LONG LT TO RT. TERMINATING ACTION ACCOMPLISHED FOR SRM 53-20-00 AT 84,197:34 H 23,464 C, REMOVED CLASS 2 DOUBLER IAW SRM 51-31-01. INSTALLED NEW DOUBLER AND TRIPLER IAW SRM 53-20-00 FIG 6 SH 5 VOL 1. FAB DOUBLER AND TRIPLER FROM 2024-T3 .050C BATCH NR 1323872. FAB FINGER DOUBLER FROM 2024- T3 .040 BATCH NR 0001198113 IAW SRM 53-20-00 FIG 6 SH 5. TREATED, PRIMED AND PAINTED IAW SRM 51-21-01 AND 51-21-02 VOL 2. REPAIR IS CLASSIFIED AS PERMANENT MAJOR REPAIR.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,198 hrs · 23,464 cycles

AFT CARGO COMPARTMENT BILGE FOUND CORRODED ON LONG 51L BETWEEN STA 1967 TO 1947. REMOVED LONGERON CAP, FRAME, SHEAR TIE AND INTERCOSTAL IAW SRM 51-31-01. FAB REPAIR PARTS ON MAE TRAVELERS NR T7/697762 AND T7/697769. INSTALLED PARTS IAW SRM 53-30-00 FIG 5 SHEET 1. PAINTED AREA IAW SRM 51-21-02. THIS REPAIR IS CLASSIFIED AS A CAT B MAJOR REPAIR. FOLLOW UP ACTION IS REQUIRED. INITIAL INSPECTION IS AT 12,000 CYCLES AND REPETITIVE INSPECTIONS AT EVERY 8,000 THERE AFTER. CURRENT CYCLES ARE 23464.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,198 hrs · 23,464 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 1641-1781 LBL48 REMOVE, FABRICATED AND INSTALLED DAMAGED SEAT TRACK PER SRM.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,198 hrs · 23,464 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1039-1059 LBL 107. REMOVED DAMAGED SEAT TRACK AND FABRICATED AND INSTALL NEW SEAT TRACK AND HAT SPLICES.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 84,198 hrs · 23,464 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1380-1530 LBL8. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK AND HAT SPLICES.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 82,682 hrs · 22,781 cycles

ON APPROACH CONFIGURING NORMALY TO 22DEGS / EXT GEAR DOWN. WHEN SELECTING 35 / EXT GOT RED DIS-AGREE LIGHT. RAN RED TABS AND PUT FLAPS / SLATS IN 22 DEGS FOR LANDING. NO OTHER PROBLEMS NOTED. MEL 26OCT06 16:17 SJC R ACN RELEASED FOR SERVICE PER MEL/CDL: 27-06-01 CATEGORY: C EXPIRATION: 04NOV06 "MEL 27-06-01: INBD FLAP DISAGREE FLAG INOP. VERIFY FLAP OPERATION AND SYMMETRY PRIOR TO EACH DEPARTURE. FOUND RIGHT INBD TRANSMITTER FAILED. REMOVED AND REPLACED RIGHT INBD IAW DC10 AMM 27-54-03-2. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 81,706 hrs · 22,357 cycles

CABIN FLOOR PANEL SUPPORT HAS CORROSION LOCATED UNDER R-1 DOOR SILL PLATE BS 421 TO 460 RBL 107.0. REPAIRED CABIN PANEL SUPPORT IAW E8-5310-96466, FUSELAGE - SEAT TRACK CORROSION AT STA 443 TO 456 INTERIM REPAIR. MAJOR REPAIR.

Part: REPAIR — MISINSTALLED (BS 755-787) · airframe 81,706 hrs · 22,357 cycles

DOUBLER REPAIR AT FS 755-787, L47L-49L EVALUATED AND FOUND NOT TO BE PER SRM. REMOVED AND REPLACED DOUBLER WITH NEW DOUBLER IAW DC10 SRM 53-20-00 FIG 6 VOL I. THIS WAS CONSIDERED TO BE A MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1636-1644) · airframe 81,706 hrs · 22,357 cycles

FOUND MAIN CABIN SEAT TRACK LBL 8 TWO LUGS WORN STA 1636 AND 1644. REPLACED DAMAGE SEAT TRACK BY SPLICING IAW DC10 SRM 53-70-00 FIG 1 VOL I FROM LBL 8 STA 1530 TO STA 1651. ALODINED AND PRIMED IAW DC10SRM 51-21-01 VOL II. INSTALLED IAW DC10 SRM 51-31-01 VOL II.

Part: FITTING — SHEARED (RN 1 PYLON) · airframe 81,706 hrs · 22,357 cycles

NR 1 AND NR 3 PYLONS HAVE SHEARED BOLTS AT FWD PYLON TO WING MOUNT FITTING, FASTENERS ARE COMMON TO OUTER SKIN AND TOMB-STONE FITTING AND UPPER CHORD ANGLE. REMOVED AND REPLACED FASTENERS IAW DC10-SRM 51-31-01-VOL 2 AND DC10-30 AMM 20-50-02.

Part: SEAL — UNSECURE (CARGO DOOR) · airframe 80,477 hrs · 21,873 cycles

IN CRUISE AT FL330 FOR FL340 HAD A RAPID DECOMPRESSION. THE CABIN RAPIDLY CLIMBED TO THE A/C ATTITUDE & A EMERGENCY DESCENT WAS IN PROGRESS. PERFORMED QRH PHASE ONE'S AND LOSS OF PRESSURIZATION CHECKLIST. FOUND MAIN A SECTION OF MAIN CARGO DOOR SEAL PROTRUDING FROM THE DOOR. FOUND TWO FWD LATCH SPOOL BRACKETS AND SURROUNDING AREAS DAMAGED. REPLACED UPPER & LOWER DOOR SUPPORT BEAMS (STA 622-767). REPLACED ATTACH FITTINGS (632-634) REPLACED DOOR SPOOLS. REPLACED DOOR STRIKER & LATCH TRIGGER. PERFORMED EDDY CURRENT INSPECTIONS. INSTALLED DOOR SEAL. CHECKED DOOR JAM FIT/FAIR AND RIG. PERFORMED PRESSURIZATION LEAK CHECK

Part: MANIFOLD — LEAKING (PNUMATIC SYS) · airframe 80,172 hrs · 21,741 cycles

CLIMBING OUT OF SLC THRU 10,000 FT NR 3 MANIFOLD FAIL LIGHT ILLUMINATED, RAN RED TABS AND RETURNED TO SLC DUE TO ICING CONDITIONS. ALSO WING ANTI-ICE WAS NOT ON AND NR 3 TEMP GAUGE WAS RED-LINING. PERFORMED NR 3 SYS DECAY CHECK RAN ENGINES AND DETERMINED NR 3 ENG BLEED SYSTEM RUNNING HIGHER TEMP THAN NR 1 SYSTEM, ACCOMPLISHED DECAY CHECK USING ENG, DETERMINED NO LEAKS IN MANIFOLD. FOUND LEAK IN AC BAY 3 AT THE TRIM AIR PRESSURE REGULATOR VALVE ROTATED CLAMP AND REPLACED FILTER SEAL LEAK CHECKS GOOD NOW, REPLACED SENSE LOOP IN THE AC BAY AS A PRECAUTION ALL WORK DONE IAW SMP. RAN NR 3 ENG AND PERFORMED NR 3 PNEUMATIC SYS TEST IAW JRH 7-3. ALL CHECKS NORMAL. OK FOR SERVICE.

Part: SKIN — DAMAGED (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

NR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABRICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-00-01 VOL I, 51-21-01 VOL II, 51-35-01 VOL II AND EA 8-7110-81479. APPLIED ANTI-CHAFFE IAW SRM 51-23-01 VOL II. INSTALLED CORE COWL IAW MM 71-13-01. READJUSTED AFT LATCH AND REISTALLED IAW MM 71-13-01-2. REFERENCE N/R N01383

Part: SKIN — DAMAGED (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

REPAIR DOUBLER ON RIGHT HAND FUSELAGE STA 1781 TO 1815 BETWEEN L-29R AND L-30R, NOT IAW DC10-30 SRM. REMOVED REPAIR DOUBLERS IAW DC10-30 SRM 51-33-01 VOL II AND 51-35-01 VOL II. FABRICATED FINGER DOUBLERS AND EXTERNAL DOUBLERS AND INSTALLED IAW DC10-30 SRM 53-20-00 VOL I, 51-33-01 VOL II AND 51-35-01 VOL II. REFERENCE N/R N01311.

Part: VENTILATOR PANEL — CRACKED (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

NR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FEDEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKIN IAW DC10-30 SRM 51-35-01 VOL II. REFERENCE N/R N00689.

Part: FITTING — NICKED (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

LEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND TO BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPROXIMATELY 0.060 INCH. REFERENCE N/R N01272.

Part: PIPE — BROKEN (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

AFT CARGO COMPARTMENT HEATING PIPE BROKEN AT STA 1910. REMOVED PIPING LINE FOR REPAIR IAW DC10 MM 20-10-01. CUT OUT AND FABRICATED AND WELDED IN NEW SECTION IAW FEDEX EA 8-2140-81471. INSTALLED PIPING AT AFT CARGO COMPARTMENT IAW DC10-30 MM 20-10-01, LEAK CHECK PIPING IAW DC10-30MM36-00-00 AND INSTALLED FLOORING IAW DC10-30 SRM 51-31-01 VOL II. REFERENCE N/R N01349.

Part: BEARING — MIGRATED (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

NR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARING IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01-0 20-50-02-2, REMOVED AFT BULKHEAD FITTING P/N AUB7025-33 IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, LOCATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB7025 FEDEX DC10-0 SRM 51-31-01 VOL 2 P/N AUB 7025-33, INSTALLED FITTING IAW DAC DWG AUB7025 FEDEX SRM DC10-30 51-31-01, 51-38-01VOL 2. R/R FUEL DRAIN LINE IAW FEDEX DC10-30 M 20-50-01-2, 20-50-02-2 TORQUED USING T-8347G REAMED 2 UPPER HOLE IAW FEDEX DC10-30 MM 51-31-01 VOL 2, ALL FASTENERS INSTALLED.

Part: BEARING — MIGRATED (ENGINE MOUNT) · airframe 78,715 hrs · 21,204 cycles

NR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03.

Part: BUSHING — WORN (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

NR 3 PYLON THRUST LINK PYLON LUGS HAS 2 WORN BUSHINGS. REMOVED AND REPLACED IAW FEDEX DC10 CMM 20-20-07.

Part: BEARING — CORRODED (ZONE 400) · airframe 78,715 hrs · 21,204 cycles

NR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 78,715 hrs · 21,204 cycles

MAIN CABIN, CARGO SEAT TRACK HAS 2 CRACKS AT LBL 24 & STA 1009 TO 1059 (MRK). REMOVED 2 FLOORBOARDS. REMOVED AND REPLACED SEAT TRACK IAW 51-31-01 VOL 2 OF FEDEX DC10-30 SRM MAT ID FOR SEAT TRACK 7929147-1350 IAW FEDEX DC10-30 SRM 53-42-01 FIG 4 SH1 VOL 3 MAT ID FOR SPLICES IAW DC10-30 FEDEX SRM 53-70-00 VOL 2 IS 4932154 P/O 458386.12 .050 7075T6 PO 446672.5. FABED SPLICES IAW DC 10-30 SRM FEDEX 53-70-00 FIG 1 VOL 1 SH 1 FABED SEAT TRACK IAW DC10 SRM FEDEX 51-31-01 VOL 2 & DAC DWG ACA7105 AND PRIMED IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 19-44. REMOVED AND REPLACED SEAT TRACK AND SPLICES IAW DC 10-30 FEDEX SRM 51-31-01 VOL 2 AND 70-00 VOL I, IR/R FLOORBOARDS IAW FED DC10-30 SRM.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

AFT PIT STA 1902, 20 LBL TO 20 RBL FLOOR SUPPORT FRAME CORRODED TOP SIDE OF T-CAP. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 3, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I. REMOVED DAMAGE IAW DC10 SRM 53-00-01 VOL I. FAB FILLER DOUBLER IAW DC10 SRM 51-00-01 VOL I AND DWG ABA3850, MAT ID FOR FILLER DOUBLER 7075-T6 .063 PO 456445.7 IAW DWG ABA3850, FRAME, FILLER AND DOUBLER ALODINED, PRIMED IAW DC10 SRM 51-21-01 VOL I. DOUBLERS HEAT TREATED IAW FORM QA-0084A, LOCATED, DRILLED DOUBLER IAW DWG AGA3850. INSTALLED DOULBER, FILLER AND FRAME IAW DC 10 SRM 51-35-01 AND 51-33-01 VOL 2.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

AFT PIT STA 1902 FLOOR SUPPORT FRAME T-CAP CORRODED UPPER SURFACE. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 2. CORROSION OUT OF LIMITS IAW FEDEX DC10 SRM 53-00-01 VOL I, PG 8. MATERIAL FOR T-CAP ANGLE IS 7075-T6 .063 P/O 353160.4 IAW DC 10 SRM 53-16-01 VOL 3 AND DAC DWG AGA3850. FAB'D T-CAP ANGLE IAW DAC DWG AGA3850. ALODINED AND PRIMED T-CAP ANGLE IAW DC10 SRM 51-21-01 VOL 2, INSTALLED ANGLE ON FRAME IAW DC10 SRM 51-33-01 VOL 2.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

R/S AFT PIT STA 1841 TO 1902 OUTBOARD FLANG OF SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 21. FOUND TO BE OUT LIMITS, IAW FEDEX DC10 SRM 53-70-00 PG 21 VOL I, MAKE NEW SEAT TRACK IAW DAC DWG AGA3855, TREATMENT ALODINE PRIMER IAW FED EX DC10 SRM 51-21-01 VOL 2 PGS 24, 21 AND INSTALLED NEW SEAT TRACK IAW FEDX DC10-30 SRM 51-33-01 VOL 2 PG 1.

Part: FITTING — MIGRATED (ZONE 600) · airframe 78,715 hrs · 21,204 cycles

NR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, REMOVED AFT BULKHEAD FITTING IAW FEDEX DC10-30 SRM 51-31-01 VOL 2 P/N AUB7025-33. LOCATED, DRILLED FITTING IAW DAC DWG AUB7075, INSTALLED NEW FITTING P/N AUB7025-33 IAW DAC DWG AUB 7025 FEDEX DC10-30 SRM 51-38-01 VOL 2, REAMED 2 EA HOLES IAW FEDEX DC10-30 SRM 51-31-01 VOL 2, INSTALLED FUEL DRAIN LINE IAW DC 10-30 MM 54-10-00.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 78,715 hrs · 21,204 cycles

NR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BE NAS64044. INSTALLED NEW BEARING ASSY WITH BOLT WET WITH SEALENT AND TORQUED IAW DC-10-30 AMM 54-40-02-2.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 78,715 hrs · 21,204 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF .9997 INCHES, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81452, LISTED ON N/R N00371 FOR CORRECTIVE ACTION. REFERENCE N/R N00371.

Part: LINER — CRACKED (ZONE 100) · airframe 78,715 hrs · 21,204 cycles

AFT LOWER CARGO COMPARTMENT FORWARD THRESHOLD ATTACH EAR IS CRACKED. WELD REPAIRED AFT CARGO DOOR LINER IAW FEDEX EA 8-5320-81459. REFERENCE N/R N00682.

Part: PANEL — DELAMINATED (ZONE 500) · airframe 78,715 hrs · 21,204 cycles

LEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 REV E, REFERENCE N/R N00794.

Part: ROLLER — CORRODED (ZONE 500) · airframe 78,715 hrs · 21,204 cycles

LEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED TO FEDEX N/R N00910, REFERENCE N/R N00925.

Part: FITTING — MIGRATED (NR 3 PYLON) · airframe 78,715 hrs · 21,204 cycles

NUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTING, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38-01 VOL II, REAMED 2 EACH HOLES IAW FEDEX DC10 SRM 51-31-01 VOL II. INSTALLED DRAIN LINE PREVIOUSLY REMOVED IAW DC10-30 SRM 54-10-00.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 78,715 hrs · 21,204 cycles

LEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL DIAMETER OF 1.0001, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81451. REFERENCE N/R N00367.

Part: PANEL — DELAMINATED (ZONE 600) · airframe 78,715 hrs · 21,204 cycles

RIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239.

Part: FITTING — MIGRATED (NR 1 PYLON) · airframe 78,715 hrs · 21,204 cycles

NUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31-01 VOL II, LOCATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB 7025 AND DC 10-30 SRM 51-31-01 VOL II, PIN AUB 7025-33 INSTALLED IAW DAC DWG AUB 7025 AND DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00494.

Part: DOUBLER — TORN (ZONE 500) · airframe 78,715 hrs · 21,204 cycles

LEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N00730.

Part: LINE — FAULTY (HYD SYSTEM) · airframe 75,249 hrs · 20,133 cycles

AFTER APPROX 3 HRS OF FLT WHILE CRUISING AT FL 330 NO 1 HYD SYSTEM QTY SLOWLY DECREASED FROM 6.0 GALS TO 2.8 GALS AND STILL SLOWLY DECREASING. TURNED OFF #1 HYD PUMPS C/W RED TABS. TURNED PUMPS ON FOR LANDING, CONFIGURATION TO FLAP 35 EXTENSION NOTED 2.3 GALS ON FINAL APPROACH. REPLACED HYD LINE ASSY PER M.M.20-10-01-2, TYPE 2 REPAIR. SERVICED #1 HYD SYSTEM AND OP'S AND LEAK CHECKED NO LEAKS NOTED A/C OK FOR SERVICE.

Part: FITTING — CRACKED (T/E FLAP)

FOUND DURING B-CHECK R/OUTBD FLAP CARRIAGE SUPPORT FITTING CRACKED APPROX 80 PERCENT OF FITTING. THIS IS SECOND CRACK FOUND IN THIS AREA.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS)

HYD NR 1 QUANTITY DECREASED TO ZERO & PRESS LESS THAN 1000. REMOVED AND REPLACED HYD LINES. LEAK CHECK OK.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 69,311 hrs · 18,279 cycles

LEFT NR 3 DOOR FWD FROM THE TOP NR 5 MOUNTING TOP-STUD BRACKET FOUND CRACKED. *S/D* REMOVED AND REPLACED PER DC10 SRM 51-35-02 VOL II.

Part: SEAT TRACK — CRACKED (BS 635)

MAIN DECK UPPER FUSELAGE, CRACK FOUND ON SEAT TRACK AT BS 635 X=27.5 LH-687. MAIN DECK UPPER FUSELAGE CRACK ON SEAT TRACK AT BS 635 X=75.25 RH-688. MAIN DECK CRACK ON SEAT TRACK AT BS 775X=8.5 RH-700. *S/D* REPAIRED SEAT TRACKS 687, 688, 700 AS PER SRM 53-70-00 FIG 1, VOL 1.

Part: INS — INOP (E & E COMPT)

98-312 - COULD NOT GET INS UNIT TO R-NAV UPDATE. GOT R-NAV YELLOW LIGHTS BUT WOULD NEVER GO TO GRN. UPDATED ALL 3 INS WITH SOFTWARE FX9813 PER MM 34-43-00-3. CKD SYS PER MM 34-43-00-1 ON GRD ALL CKD OK. OK TO CONT.

Part: CONTROL — INOP (LT MLG)

NR 5 BRAKE TEMP 150 DEG, LEFT GEAR DOWN. REMOVED AND REPLACED NR 5 BRAKE ASSY TEMP SENSOR AND ANTISKID CONTROL UNIT, PERF BITE TEST.

Part: SPAR — CORRODED (RT WING)

RT WING UPPER SURFACE JUST INBOARD AND FORWARD OF NR 2 SPOILER HAS CORROSION THAT RUNS FROM (XORS 480) TO (XORS 492). REPAIR WAS C/W BY DOUGLAS PROVIDED E.A. NOTE: MAXIUM DEPTH OF CORROSION WAS .050 INCH.

Part: STRAP — CRACKED (LT TE FLAP)

SNRM 5074. LEFT WING - OTBD FLAP INBD HINGE SUPPORT FITTING OTBD TENSION STRAP IS CRACKED LOWER BOLT HOLE EXTERNAL SURFACE. REMOVED AND REPLACED SUPPORT FITTING TENSION STRAP PER EA 8-5710-29040 AND EO 8-5750-7-4320B3 PT 1.

Part: FITTING — CRACKED (BS 2033)

SNRM 3063. HORIZONTAL STABILIZER CENTER SECTION FITTING IS CRACKED AT RT FORWARD UPPER TORQUE BOX PLANE, STA 2033, STR 13R. ****S/D***** VERIFIED CRACK WITH HFEC. FABRICATE REPAIR ANGLE AND DOUBLER. INSTALLED PER EA 8-5310-29041.

Part: BRACKET — CRACKED (R/WING)

SNRM 6004 R/H WING - O/B SLAT DRIVE MECHANISM, OUTER BRKT HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. R/R SLAT DRIVE MECHANISM BRACKET PER MM 27-83-02.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

LANDING GEAR DIDN'T EXTEND WHEN LANDING GEAR HANDLE WAS PLACED IN DOWN POSITION. DOORS OPENED, BUT GEAR DIDN'T EXTEND. HYD PRESS WAS OK AND GEAR NOT DOWN CONFIRMED BY GEAR HORN ON STDY AT FLAPS 35 DEGREES. RECYCLED GEAR AND GEAR EXTNEDED ON SECOND ATTEMPT, SLOWLY. CHECKED L/GEAR RETRACTION AND EXTENSION COMPONENTS FOR FAULTS, NONE FOUND. PINNED GEAR AND OPERATED GEAR SELECTOR VALVE SEVERAL TIMES. OPS OK, AND A/C OK FOR SVC. PINS REMOVED.