N295UP

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 89,540 hrs · 16,469 cycles

INSPECTION TYPE:N/AFUSELAGE SKIN PREVIOUS REPAIR DOUBLER DAMAGED AT PLANE 25, BL 0REPLACED DOUBLER IAW E.O. MD11-553-85332-A

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 89,379 hrs · 16,390 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHT BATTERY TESTS LOWR2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. OPS TEST GOOD

Part: SKIN PANEL — PUNCTURED (RH OTBD FLAP) · airframe 89,252 hrs · 16,327 cycles

INSPECTION TYPE:SVTRANSFERRED FROM LOGPAGE 439463 ITM 1 RH WING OTBD FLAP LOWER SKIN IS PUNCTURED.ACCOMPLISHED PERMANENT MAJOR REPAIR ON RH WING OTBD FLAP LOWER SKIN PANEL PER MD11 EA# 011-5700-01-A9695 I/R AND UPS EO MD11-5750-84718-A AND FAA APPROVED FORM 8100-9 DATED 9/12/22 BY PHILIP LAU

Part: FORMER — CRACKED (L/H WING L/E) · airframe 88,749 hrs · 16,047 cycles

INSPECTION TYPE:C1L/H O/B WING L/E HAS A FORMER THAT IS CRACK JUST I/B OF THE #9 SLAT TRACK.REMOVED, FAB, REPLACED CRACK FORMER IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (R/H WING) · airframe 88,749 hrs · 16,047 cycles

INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 537.2 TO 547.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 537.2 TO 547.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: STIFFENER — CRACKED (RT MLG W/W) · airframe 88,749 hrs · 16,047 cycles

INSPECTION TYPE:1CRT MLG W/W 3RD STIFFENER CRACK AT LOWER END O/B AFT.REMOVED AND REPLACED CRACK STIFFENER IAW SRM 51-35-01 AND 51-35-02 (MINOR).

Part: NONE — DENTED (LOWER SKIN) · airframe 88,616 hrs · 15,976 cycles

INSPECTION TYPE:N/ASMALL DENT ON RIGHT WING INBOARD FLAP LOWER SURFACE T/E AREA BETWEEN STA XIFH 124 AND XW 291MAJOR REPAIR COMPLETED PER E.O. MD11-575080336-A SEE NR 676429 FOR DETAIL PERTAINING TO REPAIR THIS CLEARS D715183

Part: DOOR — INOPERATIVE (L1) · airframe 88,003 hrs · 15,675 cycles

INSPECTION TYPE:N/AUPON ENTERING A/C FOUND L1 DOOR ELECTRIC ACTUATION TO BE INTERMITTENTT/S IAW FIM 34-46-00 & AMM 34-46-00. OPS TEST GOOD AT THIS TIME. THIS CLEARS M754915

Part: PULLEY — INOPERATIVE (L1 DOOR) · airframe 87,994 hrs · 15,668 cycles

INSPECTION TYPE:N/AL1 DOOR FWD TOP DRIVE CABLE IDLER PULLEY DAMAGEDR&R LA DOOR FWD TOP DRIVE CABLE IDLER PULLEY REF AMM 52-11-03, BOEING DRAWING ABA7788, & BOEING AEPL

Part: PULLEY — DAMAGED (L1 DOOR) · airframe 87,994 hrs · 15,668 cycles

INSPECTION TYPE:N/AL1 DOOR AFT TOP CABLE TENSION PULLEY DAMAGED.INSTALLED NEW PULLEY IN TRUNION. AWAITING PART IN ITEM 2 THIS LOG FOR REINSTALLATION. REF MM 52 11 03 CF 3194937 8-22-21/ R&R WITH NEW ROD ASSY ITEM 2. INSTALLED TRUNNION & PULLY WITH TOP AFT L2 DOOR CABLE. REF AMM 52 11 03. ESR: IPC 52 11 05 05 & EO MD11 5230 55810-A

Part: CABLE — BROKEN (L1 DOOR) · airframe 87,957 hrs · 15,645 cycles

FUELING SUPERVISOR REPORTED L1 DOOR WOULD NOT CLOSE INSPECT L1 DOOR AND FOUND AFT LIFT. LOWERING CABLES BROKEN. INSTALLED LOWER L1 DOOR CABLE UP TO AND INCLUDING STEP AMM 52-11-03 E(1) (B) INSTALLED L1 DOOR TOP & BOTTOM AFT CABLES THROUGH SETP E.9 AMM 52-11-03. COMPLETED INSTALL OF L1 DOOR CABLES REF AMM 52-11-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 15,517 cycles

EMERGENCY LIGHTING IN COURIER AREA REMAINS PARTIALLY ILLUMINATED WITH EMERGENCY LIGHT. TEST PASSED ANE WITHOUT INDICATION EAD. DEFERRED EMERGENCY LIGHTS PER MEL 33-50-4 DMP C/W PLACARD INSTALLED.R/R'D EMERGENCY BATTERY PWR SUPPLY PER MM 33-51-01 PG BLK 401. OPS CHECK PER MM 33-51-01-700-802 OPS CHECK NORMAL. M746660 CLOSED. PLACARD REMOVED.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 87,226 hrs · 15,265 cycles

L1 DOOR DOES NOT CLOSE/SEAL COMPLETELY ON FORWARD SIDE. THE DOOR DOES NOT OPERATE SMOOTHLY DURING THE LAST HALF OF THE CLOSING EITHER. ITEM DEFERRED PER MEL 52-10-3-1-2-1 PLACARD INSTALLED. DI# M733638 ASSIGNED. AIRCRAFT OK TO CONT. CRV.CLEANED AND LUBED TRACKS/ROLLERS/BOGIES. OPS CHECK GOOD REF AMM 52-11-02-501. THIS CLOSES M733638. PLACARD REMOVED.

Part: SUPPORT FITTING — CRACKED (NLG TRUNNION) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2C CRACK ON NLG LH TRUNNION SUPPORT FITTING AT FUSELAGE STA Y=582.5 , Z= -114 & X = 24.00.REPAIRED CRACKED LH NLG TRUNNION SUPPORT FITTING AT FUSELAGE STA Y= 582.5 , Z= -114 & X=24.0. IAW SRM 53-10-14 REPAIR 2 FIGURE 202. ( MAJOR )

Part: LONGERON — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCORROSION ON LONGERON 52 AT FWD EXTENDED FUSELAGE SECTION STA Y=6-73.ACCOMPLISHED SPLICE REPAIR ON LONGERON 52 BETWEEN Y= 6-60.00 - Y= 6-80 IAW SRM 53-00-05 REPAIR 1. FIGURE 201 & 202. (MAJOR)

Part: BULKHEAD — CORRODED (NR 3 PYLON) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2C#3 ENG. PYLON AFT BULKHEAD ASSY. HAS CORROSION COMMON TO THE INNER BORE LUG OF BULKHEAD P/N AUB7502-507 & AUB 7502-509.REPAIRED #3 ENG. PYLON AFT BULKHEAD ASSY. IAW VT-SAA EA 011-5410-01-A8166 REV. I/R AND UPS EO MD11-5410-76449-A. (MINOR).

Part: STRINGER — CRACKED (RT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CR/H WING TANK AT STA XORS 330.890, STRINGER # 41 IS CRACKED.ACOMPLISHED REPAIR TO R/H WING TANK AT STA XORS 330.890, STRINGER # 41 IAW VT-SAA EA 011-5710-01-A8138-IR AND UPS EO MD11-5710-76538-A.

Part: MOUNT FITTING — DAMAGED (RT AILERON) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CRT I/B AILERON #2 MOUNT BOTH I/B AND O/B BUSHINGS ARE MIGRATED.REPAIRED DAMAGED RT I/B AILERON #2 MOUNT FITTING I/B AND O/B LUG BUSHING BORES IAW VT-SAA EA 011-5740-01-A8150 REV. IR AND UPS EO MD11-5740-76427-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440 - 488 AT X=19.0.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA. 440 - 488 AT X=19.0 IAW VT-SAA EA 011-5310-01-A8145 REV. IR AND UPS EO MD11-5310-76338-A. (MINOR)

Part: BARRIER — CORRODED (MAIN CABIN) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CRIGID CARGO BARRIER WALL HAS CORROSION ON LOWER FACE.REMOVED AND REPLACED RIGID CARGO BARRIER WALL IAW AMM 25-59-13-00-801 AND 25-59-13-400-801. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -36.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 440-488 AT X= -36 IAW VT-SAA EA 011-5310-01-A8142 REV. I/R AND UPS EO MD11-5310-76312-A. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 IAW VT-SAA EA 011-5320-01-A8152 REV IR AND UPS EO MD11-5320-76347-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 475 AND STA. 488 HAS CORROSION.REPAIRED CORRODED MAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 475 AND STA. 488 IAW VT-SAA EA 011-5310-01-A8146 REV. IR AND UPS EO MD11-5310-76344-A. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN X=47.5 TO X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN X=47.5 TO X=75.25 IAW VT-SAA EA 011-5320-01-A8151 REV IR AND UPS EO MD11-5320-76349-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 421.578-488 AT X=0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 421.578-488 AT X=0 IAW VT-SAA EA 011-5310-01-A8140 REV. I/R AND UPS EO MD11-5310-76290-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -17.REPAIRED CORRODED SEAT TRACK BETWEEN STA 440-488 AT X= -17 IAW VT-SAA EA 011-5310-01-A8141 REV. I/R AND UPS EO MD11-5310-76306-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-475 AT X= 36.0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 459-475 AT X= 36.0 IAW VT-SAA EA 011-5310-01-A8144 REV. I/R AND UPS EO MD11-5310-76302-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 475-515 AT X= 47.5.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 475-515 AT X=47.5 IAW VT-SAA EA 011-5310-01-A8143 REV. I/R AND UPS EO MD11-5310-76303-A. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 TO X=-36 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 TO X=-36 IAW VT-SAA EA 011-5320-01-A8153 REV. IR AND UPS EO MD11-5320-76348-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CSEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 IAW VT-SAA EA 011-5310-01-A8147 REV IR AND UPS EO MD11-5310-76311-A. (MINOR)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CFLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=-78 HAS CORROSION.REMOVED AND REPLACED CORRODED FLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=-78 IAW MD-11 SRM 51-33-01 AND 51-31-01. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-480 AND X=77REMOVED AND REPLACED SEAT TRACK AT SAID LOCATION IAW SRM 51-31-01. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-47.5 TO X=-72.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-47.5 TO X=-72.25 IAW VT-SAA EA 011-5320-01-A8154 REV. IR AND UPS EO MD11-5320-76313-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CMAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA. 459-485 AND X=50 TO X=62.REPAIRED CORRODED SEAT TRACK MBETWEEN STA. 459-485 AND X=50 TO X=62 IAW VT-SAA EA 011-5310-01-A8139 REV. I/R AND UPS EO MD11-5310-76476-A. (MAJOR)

Part: DOOR FRAME — CHAFED (CLG DOOR) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER LANDING GEAR R/H DOOR UPPER AFT CORNER FRAME IS CHAFED.REMOVED FABRICATED AND REPLACED DOOR FRAME IAW DWG. ANB7384 AND SRM 51-31-01. (MINOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON # 52 IS CRACKED BETWEEN STA. 1681-1701.REPAIRED CRACKED CENTER CARGO LONGERON # 52 BETWEEN STA. 1641 TO 1701 IAW VT=SAA EA 011-5310-01-A8157 REV. I/R AND UPS EO MD11-5310-76494-A. (MAJOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CMAIN CABIN INTERUPTED LONGERON 16L IS CRACKED BETWEEN STA. 1139 - 1159.REMOVED AND REPLACED CRACKED MAIN CABIN INTERUPTED LONGERON 16L BETWEEN STA. 1139 - 1159 IAW MD-11 SRM 51-33-01. (MINOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON # 42 R/H IS CRACKED BETWEEN STA. 1641-1661.REPAIRED CRACKED CENTER CARGO LONGERON # 42 R/H BETWEEN STA. 1630 TO 1650.130 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)

Part: LONGERON — CRACKED (TAILCONE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CTAIL CONE R/H UPPER LONGERON BEAM IS CRACKED AT THE FWD. END.REPAIRED TAIL CONE R/H UPPER LONGERON BEAM IAW UPS EO MD11-5350-66790-A. (MINOR)

Part: DOUBLER — WORN (TAILCONE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CTAIL CONE LH UPPER LONGERON @ PRODUTION DOUBLER IS WORN THRU.REPAIRED TAILCONE LONGERON / INTERNAL DOUBLER IAW EO MD11-5350-66790-A. (MINOR)

Part: FRAME — CRACKED (TAILCONE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CTAIL CONE FWD. R/H FRAME IS CRACKED AT THE CENTER GUIDE PIN HOLE.REPAIRED TAIL CONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG. 201. (MINOR)

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CCENTER CARGO LONGERON 29R SPLICE IS CRACKED BETWEEN STA. 1661 AND 1681.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 29R SPLICE BETWEEN STA. 1661 AND 1681 IAW MD-11 SRM 51-33-01. (MINOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON # 38 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 38 R/H BETWEEN STA. 1641 TO 1681 IAW SRM 536-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON # 41 IS CRACKED AT STA. 5-113.REPAIRED CRACKED CENTER CARGO LONGERON # 41 BETWEEN STA. 5-123/1531 AND 1561 IAW SRM 53-00-05- REPAIR 1 FIG. 201. (MAJOR)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON # 37 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 37 R/H BETWEEN STA. 1641 TO 1681 IAW SRM 53-00-05 REPAIR 1 FIG. 201 AND 202. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CLH WING BEADED DOUBLER CRACKED BETWEEN STA XOS 698-703.REPAIRED CRACKED LH WING BEADED DOUBLER BETWEEN STA XOS-698.1 - 703.5 IAW MD-11 SRM 57-40-02 REPAIR 15 FIGURE 205. (MAJOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CCENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 1951 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 1951 IAW MD-11 SRM 51-35-01. (MINOR)

Part: SPLICE — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CCENTER CARGO R/H TUNNEL UPPER AREA SPLICE AT L28R HAS 2 CRACKS.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 28R SPLICE AND CRACKED LONGERON SECTION BETWEEN STA. 1651 AND 1701 IAW MD-11 SRM 53-00-05, REPAIR 1, FIGURE 201 & 202. (MAJOR)

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CL-3 DOOR JAMB INNER SKIN (WEB) IS CRACKED AT STA. 1254 AND Z=-18.REPAIRED CRACKED L-3 DOOR JAMB INNER SKIN (WEB) AT STA. 1254 AND Z=-18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)

Part: WEB — CRACKED (NR 1 PYLON) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2C#1 PYLON AFT FAIRING WEB/RIB IS WORN AND CRACKED.REMOVED AND REPLACED WEB/RIB IAW SRM 54-05-41. (MINOR)

Part: RIB — WORN (NR 3 PYLON) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2C#3 PYLON AFT FAIRING WEB/RIB IS WORN.REMOVED AND REPLACED WEB/RIB IAW SRM 54-05-41. (MINOR)

Part: SKIN — CRACKED (LT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CL/H WING LOWER SKIN AT FUEL ACCESS DOOR COT-OUT STA. XORS. 683.4-713.6 HAS 10 FASTENER HOLES WITH CRACKS.REPAIRED L/H WING LOWER SKIN BETWEEN STA XORS. 683.4 TO 713.6 IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)

Part: SEAL — CORRODED (RT SPOILER) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CR/H WING SPOILER PANEL SILL HAS CORROSION BETWEEN STA. XOFH= 453.931 AND XOSP=521.40.REPAIRED CORRODED R/H WING SPOILER PANEL SILL BETWEEN STA. XOFH=453.931 AND XOSP=453.931 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)

Part: SUPPORT — CRACKED (TE FLAP) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CL/H WING T/E I/B FLAP I/B HINGE FRAME SUPPORT IS CRACKED.REMOVED, FABRICATED AND REPLACED HINGE SUPPORT IAW DWG. ARC0165 AND SRM 51-35-01. (MINOR)

Part: DOUBLER — CHAFED (TAILCONE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CTAIL CONE R/H UPPER PRODUCTION DOUBLER HAS CHAFE DAMAGE.REPAIRED TAIL CONE R/H PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-A. (MINOR)

Part: SKIN PANEL — CRACKED (RT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CR/H WING LOWER SKIN PANEL BETWEEN XORS 683.40 AND XORS 713.65 AT FUEL ACCESS PANEL 636AS DOOR LANDING IS CRACKED.REPAIRED R/H WING LOWER SKIN PANEL BETWEEN XORS 683.40 AND XORS 713.65 IAW VT-SAA EA 011-5730-01-A8159-IR AND UPS EO MD11-5730-76477-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 616.8-621.6.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 616.8-621.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SKIN — CRACKED (LE SLAT) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CL/H WING #1 SLAT UPPER SKIN IS CRACKED AT STA. XIS= 202.246.REPAIRED CRACKED L/H WING #1 SLAT AT STA. XIS= 202.246 IAW VT-SAA EA 011-5754-01-A8165 REV. I/R AND UPS EO MD11-5750-76492-A. (MAJOR)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CAFT FUSELAGE COMP HAS A CRACKED INTERCOSTAL AT RH SIDE SKIN, JUST FWD OF PNL 348AF.REMOVED, FABRICATED AND RELPACE CHANNEL IAW DWG AJC7898 AND SRM 51-31-01. (MINOR)

Part: DOUBLER — GOUGED (LT WING) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CEXISTING EXTERNAL REPAIR DOUBLER ON LH WING FIXED L/E BETWEEN STA XIS 178 AND XIS190.5.REMOVED , FABRICATED AND REPLACED DAMAGED REPAIR DOUBLER BETWEEN STA XIS 178 AND XIS 190.5 IAW SRM 57-40-02 FIGURE 201 REPAIR 5. (MAJOR)

Part: SKIN — GOUGED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CFUSELAGE SKIN AT MCD CUTOUT LOWER AFT CORNER IS GOUGED.REPAIRED GOUGED FUSELAGE SKIN EDGE AT MCD CUTOUT LOWER AFT CORNER BETWEEN LONGERON 26L AND LONGERON 27L AT STA. 767.250 IAW VT-SAA EA 011-5330-01-A8134 REV. IR AND UPS EO MD11-5330-76227-A. (MINOR)

Part: DOOR FRAME — CRACKED (CLG DOOR) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:4CCLG R/H FWD DOOR I/B FWD CORNER PAN (FRAME) IS CRACKED IN RADIUS.REMOVED AND REPLACED CRACKED CLG R/H FWD DOOR I/B FWD CORNER PAN (FRAME) IAW MD-11 SRM 51-33-01, 51-35-01 AND 51-35-02. (MINOR)

Part: SKIN — GOUGED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN REPAIR DOUBLER AND TRIPLER IS GOUGED BETWEEN STA. 1002.3 TO 1009.3 (FWD. LOWER CARGO DOOR CUT-OUT.REPAIRED FUSELAGE SKIN AT STA. 1002.3 TO 1009.3 IAW VT-SAA EA 011-5330-001 A8127 REV. I/R AND UPS EO MD11-5330-76198-A. (MINOR)

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 86,283 hrs · 14,777 cycles

INSPECTION TYPE:2CEXTERIOR FUSELAGE REPAIR DOUBLER / TRIPLER GOUGED AT STA 1781 (CENTER CARGO DOOR CUTOUT).REPAIRED EXT SKIN CARGO DOOR CUTOUT AT STA 1781 IAW VT-SAA EA 011-5330-01-A8131 REV IR AND EO MD11-5330-76279-A. (MINOR)

Part: UNKNOWN — ODOR (CABIN) · airframe 85,890 hrs · 14,594 cycles

INSPECTION TYPE:N/AFAINT ODOR DETECTED WHEN GEAR WAS LOWERED AND LVL 2 AUTOBRAKE FAIL MESSAGE ILLUMINATEDUPON RECEIVING PILOT TURNOVER IMMEDIATELY WENT DOWN TO ELECTRICAL COMPARTMENT. NO ODOR DETECTED. PERFORMED GENERAL VISUAL INSPECTION OF ALL WIRING, CONNECTORS, AND LRU'S PER SWPM 20-10-06. NO FAULTS FOUND. NO LEAKS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,862 hrs · 14,175 cycles

INSPECTION TYPE:N/A LVL 1 :EMER LT BAT 2 LO" ILLUMINATED AFTER AMER LT TEST. REPLACED EMERGENCY LIGHTS BATTERY REF AMM 33-51-01OPS NML ESR 33-51-10-01-005.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,448 hrs · 14,032 cycles

LEVEL 1 "ENG 3 FADEC MAINT" ALERT DISPLAYED AFTER TAKE OFF. FOUND FAULT CODE 351-21 2.5 BLD POSITION IN NR 3 ENG EEC FAULT HISTORY. INSPECTED 2.5 BLEED CLEVIS ROD END AND BELL CRANK AND PIVOT PIN. NO FAULTS FOUND T/S PER FRM/FIM 73-21-00-101 CLEARED FAULT HISTORY AND PERFORMED GROUND RUN AT 1.3 EPR MSG DID NOT RETURN. SYSTEM OK FOR SERVICE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,418 hrs · 14,021 cycles

EMERGENGY LIGHT SYSTEM. REPLACED SWITCH 51-346 PER WDM 33-51-01. NO HELP. ISOLATED TO LIGHTS ON WIRE B312-319-20. WITH THIS WIRE REMOVED FROM 53-692 REMAINING LIGHTS COME ON. REF WDM 33-52-01 PG 2. DMP 33-50-4 COMPLIED WITH. **SUPPLEMENTAL SDR **EMERGENCY LIGHTING PER SUPPLY REF AMM 33-51-01. REPLACED EMERGENCY LIGHT TEST SWITCH PER IAW AMM 33-51-01 & REPAIRED WIRE B312-19-20 AT TB S3-692 PER IAW /SUPPLY 20-10-00 OPS CK'D GOOD PER AMM 33-50-00

Part: FASTENER — LOOSE (L1 DOOR) · airframe 84,386 hrs · 14,014 cycles

INSPECTION TYPE:N/A EXIT SHROUD OVER L1 DOOR NOT CLOSING TO PROPER POSITION. FOUND CABLE CATCH BRACKET HARDWARE LOOSE. RESECURED IAW AMM 20-50-02. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,343 hrs · 13,706 cycles

EMERGENCY POWER LIGHTS DO NOT WORK OR TEST DURING SHUTDOWN. T/S PER AWD 33-51-01, REMOVED AND REPLACED U1 1756 BATERY PACK AND RELAY R2-5700 PER AMM 33-51-01/ 487. SYSTEM CKS OK FOR SVC REF: 33-51-10-01 ITEM 005J.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 83,147 hrs · 13,655 cycles

LT ENTRY DOOR ASSIST BOTTLE PRESSURE IS LOW. R&R L1 ASSIST BOTTLE IAW TC 8324.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT OTBD FLAP, INBD HINGE HAS NUMEROUS AREAS OF CORROSION. REPAIRED THE FLAP HINGE IAW EA 011-5740-01-A7210, REV I/R, AND EO MD11-5740-68166-A.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT OTBD FLAP, OTBD AFT HINGE HAS CORROSION INSIDE LIGHTNING HOLE. REPAIRED THE FLAP HINGE IAW EA 011-5740-01-A7210, REV I/R, AND EO MD11-5740-68166-A.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT OTBD FLAP OTBD HINGE HAS CORROSION INSIDE LIGHTNING HOLE. REPAIRED THE FLAP HINGE IAW EA 011-5740-01-A7210, REV I/R, AND EO MD11-5740-68166-A.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RIGHT OTBD FLAP, INBD AFT HINGE HAS CORROSION AT LIGHTNING HOLE. REPAIRED THE FLAP HINGE IAW EA 011-5740-01-A7210, REV I/R, AND EO MD11-5740-68166-A.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT OTBD FLAP INBD FWD HINGE LOWER LUG FACE HAS CORROSION. REPAIRED THE HINGE IAW CMM 57-44-08, REPAIR 1.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT, OTBD FLAP, INBD HINGE LOWER INBD LUG HAS CORROSION AT THE AFT FACE. REPAIRED THE FLAP HINGE LUG IAW CMM 57-52-04.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING OTBD FLAP OTBD HINGE BRACKET, HINGE BEARING BORE CORRODED. REPAIRED IAW CMM 57-44-09.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT, OTBD FLAP, OTBD AFT HINGE INBD LUG FACE HAS CORROSION. REPAIRED THE FLAP HINGE LUG IAW CMM 57-52-04.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING OTBD FLAP INBD FWD HINGE HAS CORROSION IN THE SPHERICAL BEARING BORE. REPAIRED THE HINGE IAW CMM 57-44-08, REPAIR 1.

Part: LUG — CORRODED (LT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT OTBD FLAP OTBD FWD HINGE LOWER LUG HAS CORROSION IN SPHERICAL BEARING BORE. REPAIRED HINGE LUG IAW CMM 57-44-09, REPAIR 1.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE:3C, RT, OTBD FLAP OTBD AFT HINGE LOWER LUG HAS CORROSION ON BOTH SIDES OF FACE. REPAIRED THE FLAP HINGE LUG IAW CMM 57-52-04.

Part: CAP — CRACKED (BS 1298) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE:3CL/H UNDER WING BARREL CANTED PANEL CAP IS CRACKED AT BS 1298 AND Z=100. REPAIRED IAW EA 011-5310-01-A7209, REV I/R, AND EO MD11-5310-68241-A. MAJOR.

Part: CAP — CRACKED (BS 1278) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT UNDER WING BARREL CANTED PANEL CAP IS CRACKED AT BS 1278, AND Z=-100. REPAIRED IAW EA 011-5310-01-A7209, REV I/R, AND EO MD11-5310-68240-A. MAJOR.

Part: SUPPORT ANGLE — CRACKED (BS 1361) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 2C, LT FUSELAGE EXTERIOR WING-TO-BODY FAIRING SUPPORT ANGLE CRACKED, BS 1361. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG ANB7143 AND SRM 51-31-01.

Part: ANGLE — CRACKED (BS 1278 FRAME) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, FRAME ANGLE CRACKED, RT SIDE, BS 1278. REMOVED, FABRICATED AND INSTALLED A REPLACEMENT ANGLE IAW DWG AYB7035, AND SRM 51-33-01.

Part: ANGLE — CRACKED (BS 1278 FRAME) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE:3C, FRAME ANGLE CRACKED, BS 1278, LT SIDE. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG AYB7035, AND SRM 51-33-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, STRINGER 48 IS CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.

Part: STIFFENER — CRACKED (BS 1841) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, AFT CARGO BAY VERTICAL STIFFNER ANGLE IS CRACKED AT BS 1841 RBL 26. REMOVED, FABRICATED, AND REPLACED THE STIFFNER ANGLE IAW DWG AGA7170, AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY, LONGERON SPLICE 49R IS CRACKED AT BS 5-123. REMOVED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7114, AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY, LONGERON SPLICE 50R, CRACKED AT BS 5-123. REMOVED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7114, AND SRM 51-33-01.

Part: STRINGER — CRACKED · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, STRINGER 49 IS CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, STRINGER 50 IS CRACKED. REPAIRED STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.

Part: CAP — CRACKED (BS 1236) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT UNDER WING BARREL CANTED PANEL CAP IS CRACKED AT BS 1236.8 AND Z=-100. REPAIRED THE PANEL CAP IAW EA 011-5310-01-A7207, REV I/R, AND EO MD11-5310-68235-A. MAJOR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE :3C, STRINGER 47 IS CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.

Part: SUPPORT ANGLE — CRACKED (BS 1781) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY AT BS 1781, LT SLOPE PANEL SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG AFA7295, AND SRM 51-33-01.

Part: SUPPORT ANGLE — CRACKED (BS 969) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO, SLOPE PANEL SUPPORT ANGLE CRACKED, BS 969, LONGERON 41L. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, CENTER ACCESSORY BAY, LONGERON 51R BETWEEN BS 6-70 TO 6-90 IS CORRODED. REMOVED, FABRICATED AND REPLACED THE LONGERON IAW DWG AAA7088 AND NAA6754.

Part: SUPPORT ANGLE — CRACKED (BS 919) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO, SLOPE PANEL SUPPORT ANGLE CRACKED BS 919, LONGERON 41L. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-33-01.

Part: STRINGER — CRACKED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING UPPER STRINGER 15 IS CRACKED AT 2 PLACES. REPAIRED THE STRINGER BETWEEN XORS 433 AND 455 IAW EA 011-5710-01-A7206, REV I/R, AND EO MD11-5710-68173-A. MAJOR.

Part: INTERCOSTAL — CRACKED · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, CRACKED INTERCOSTAL BS 6-50 ALONG LONGERON 42L. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT INTERCOSTAL IAW DWG ACA7049, AND SRM 51-31-01.

Part: STRINGER — CRACKED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING STRINGER 22 IS CRACKED AT XORS 826.5. REPAIRED THE WING STRINGER IAW EA 011-5710-01-A7201, REV I/R, AND EO MD1-5710-68236-A. MAJOR.

Part: STRINGER — CRACKED (LT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT WING UPPER STRINGER 15 IS CRACKED AT 2 PLACES. REPAIRED THE STRINGER BETWEEN XORS. 433 AND 445 IAW EA 011-5710-01-A7205, REV I/R, AND EO MD11-5710-68174-A. MAJOR.

Part: SUPPORT ANGLE — CRACKED (BS 969) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO, SLOPE PANEL SUPPORT ANGLE CRACKED, BS 969, LONGERON 41L. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: SUPPORT ANGLE — CRACKED (BS 939) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO, SLOPE PANEL SUPPORT ANGLE CRACKED, BS 939, LONGERON 41L. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-33-01.

Part: FLOOR SUPPORT — GOUGED (BS 905) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, FLOOR SUPPORT GOUGED AT BS 905. REPAIRED THE FLOOR SUPPORT BETWEEN BS 902 AND 906 AT RBL 82 IAW EA 011-5310-01-A7204, REV IR, AND EO MD11-5310-68103-A.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT ELEVATOR LEADING EDGE PANEL 345CT CRACKED. REMOVED AND REPLACED THE LE PANEL IAW AMM 51-33-01.

Part: SUPPORT ANGLE — CRACKED (BS 775) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO SLOPE PANEL SUPPORT ANGLE AT BS 775, RT SIDE CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: SUPPORT ANGLE — CRACKED (BS 1119) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO SLOPE PANEL SUPPORT ANGLE CRACKED AT BS 1119 RT SIDE. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: TAIL CONE — CHAFED (BS 2163-2165) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, FWD EXTENDED TAILCONE HAS CHAFE DAMAGE AT BS 2163 - 2165, RBL 36.5, BETWEEN Z=40 & Z=60.1. REPAIRED THE TAILCONE IAW EA 011-5350-01-A7198, REV I/R, AND EO MD11-5350-68044-A.

Part: SKIN — CORRODED · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, SKIN HAS CORROSION AT STRINGER 15. REPAIRED THE SKIN IAW EA 011-5730-01-A7196, REV I/R, AND EO MD11-5730-68071-A.

Part: SKIN — CORRODED · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, SKIN CORRODED AT STRINGER 14, FRAME 59. REPAIRED THE SKIN IAW EA 011-5730-01-A7196, REV I/R, AND EO MD11-5730-68071-A.

Part: SKIN — CORRODED · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, SKIN HAS CORROSION AT STRINGER 14. REPAIRED THE SKIN IAW EA 011-5730-01-A7196, REV I/R, AND EO MD11-5730-68071-A.

Part: SKIN — WORN (BS 1159) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN AT BS 1159, LONGERON 44L HAS DEEP WEAR. REPAIRED THE SKIN IAW EA 011-5330-01-A7203, REV I/R, AND EO MD11-5340-67962-A.

Part: TEE FITTING — CRACKED (BS 1321) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN TEE FITTING IS CRACKED AT BS 1321, LONGERON 15R. REMOVED, FABRICATED AND REPLACED THE TEE FITTING IAW DWG AEA7568, AND SRM 51-35-01.

Part: RUB STRIP — CHAFED (WING TO BODY) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, WING TO BODY CHAFE STRIPS ARE WORN BETWEEN BS 1149 - 1199, LONGERONS 44L & RT. REMOVED, FABRICATED, AND REPLACED THE RUB STRIPS IAW EO MD11-5340-67962-A.

Part: TEE FITTING — CRACKED (BS 1321) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CARGO DECK TEE FITTING IS CRACKED AT BS 1321 AND LONGERON 15L. REMOVED, FABRICATED AND REPLACED THE TEE FITTING IAW DWG AEA7568, AND SRM 51-35-01.

Part: WEB — CRACKED (BS 1305-1315) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, L3 DOOR FRAME LOWER AFT WEB IS CRACKED AT UPPER AFT CORNER. REPAIRED L3 DOOR FRAME LOWER AFT WEB BETWEEN BS 1305.25 TO 1315.42. Z=-15.00 TO Z=-19.00 IAW SRM 53-40-15, REPAIR 3, FIGURE 201. MAJOR.

Part: LONGERON — CORRODED (BS 1179-1199) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 16R CORRODED BETWEEN BS 1179 - 1199. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA7065, AND SRM 51-33-01.

Part: DOOR FRAME — CRACKED (BS 1254) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN BS 1254, Z=60, R3 DOOR FRAME FWD UPPER WEB IS CRACKED. REPAIRED THE DOOR FRAME WEB IAW EA 011-5310-01-A7193, REV I/R, AND EO MD11-5310-68077-A. MAJOR.

Part: PAN — CRACKED (CARGO DOOR) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 2C, CENTER CARGO DOOR, LOWER AFT CORNER PAN CRACKED. REMOVED AND REPLACED THE PAN IAW SRM 51-33-01, 51-35-01.

Part: LONGERON — CRACKED (BS 1219) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 27R HAD TWO CRACKS AT BS 1219. REMOVED AND REPLACED THE LONGERON IAW SRM 51-31-01, 51-33-01, AND 51-35-01.

Part: SKIN — CORRODED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING UPPER SKIN HAS CORROSION BETWEEN XORS 97 & 130, STRINGERS 11 - 15. REPAIRED THE SKIN IAW EA 011-5730-01-A7199, REV I/R, AND EO MD11-5730-68143-A.

Part: SKIN — CRACKED (LT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LEFT WING L/E LOWER SKIN IS CRACKED AT THE SLAT TRACK CUT-OUT AT XOS 889. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.

Part: SKIN — CORRODED (LT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT WING, UPPER SKIN HAS CORROSION AROUND SEVERAL FASTENERS HEADS MIDSPAR AT FUSELAGE. REPAIRED THE WING SKIN BETWEEN XORS 97 AND 130.40, BETWEEN STRINGERS 14 AND 16 IAW EA 011-5730-01-A7197, REV IR, AND EO MD11-5730-68095-A.

Part: TEE FITTING — CRACKED (LT WING AILERON) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LT WING T/E COMPARTMENT FWD OF INBD AILERON TEE FITTING IS CRACKED. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-33-01.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 2C, RT WING INBD FIXED L/E COMPARTMENT SUPPORT ANGLE CRACKED AT AFT END INSIDE PANEL 616AB. REMOVED, FABRICATED A REPLACEMENT AND INSTALLED IAW DWG ARB1161, SRM 51-35-02, 51-33-01, AND 51-31-01.

Part: FLOOR PANEL — CORRODED (BS 475) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL IS CORRODED AT BS 475 AND RBL 60. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A7184, AND EO MD11-5320-67995-A.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL IS CORRODED AT BS 475 AND RBL 49. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A7183, REV I/R AND EO MD11-5320-67994-A.

Part: FITTING — CRACKED (RT SLAT TRACK) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E COMPARTMENT INBD SLAT TRACK NR 16 FITTING FOUND CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-31-01, 51-33-01, AND 51-35-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING, FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 633.4 - 636.8. REPAIRED THE DOUBLER IAW EA 011-5730-01-A7191, REV I/R, AND EO MD11-5730-68054-A. MAJOR.

Part: FORMER — CRACKED (LT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 2C, LT WING FIXED L/E FORMER CRACKED XORS480. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FORMER IAW DWG ARB2931 AND SRM 51-33-01.

Part: SPAR CAP — CORRODED (RT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT WING UPPER SURFACE T/E PANEL BULGING AND FASTENERS PULLING THROUGH JUST FWD OF OTBD AILERON. REPAIRED THE WING UPPER SPAR CAP BETWEEN XORS 961.8 TO 1044 IAW EA 011-5710-01-A7202, REV IR, AND EO MD11-5710-68124-A.

Part: SKIN — CHAFED (LT WING) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, LEFT WING L/E SKIN CHAFED ON EITHER SIDE OF THE NR 1 SLAT, NR 1 TRACK CUT OUT. REPAIRED THE WING SKIN IAW SRM 57-40-02, REPAIR 5, FIGURE 201. MAJOR.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, NR 3 RT THRUST REVERSER TRANSLATING SLEEVE AFT BONDED PANEL, FORWARD CLOSURE FRAME CRACKED AT THE 6 O`CLOCK POSITION. REPAIRED IAW SREO MD11-7830-56690-A.

Part: WEB — CRACKED (FUEL TANK) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, UPPER FUEL TANK WEB IS CRACKED AT BS 1372, RBL 80. REPAIRED IAW EO MD11-5710-67889-A. MAJOR.

Part: HINGE FITTING — CHAFED (NR 3 NACELLE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, NR 3 ENGINE LT FAN COWL FWD HINGE FITTING CHAFED AT THE 12 O'CLOCK POSITION. RERPAIRED THE HINGE FITTING IAW EA 011-7110-01-A7181, REV IR, AND EO MD11-7110-67895-A.

Part: HINGE — CHAFED (NR 1 NACELLE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE:3C, NR 1 ENGINE INBD FAN COWL FWD HINGE CHAFED. REPAIRED THE HINGE IAW EA 011-7110-01-A7180, REV A, AND EO MD11-7110-67898-B.

Part: HINGE — CHAFED (NR 1 NACELLE) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, NR 1 ENGINE, INBD FAN COWL FWD HINGE FOUND CHAFED. REPAIRED IAW EA 011-7110-01-A7180, REV IR, AND EO MD11-7110-67898-A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN BS 1501 - 1506, LBL 8.5. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 1, FIG 201. MAJOR.

Part: SKIN — CRACKED (A/C DOOR) · airframe 82,752 hrs · 13,545 cycles

INSPECTION TYPE: 3C, RT A/C DOOR HAS 2 CRACKS ON THE OUTER SKIN. REPAIRED THE DOOR IAW SRM 52-40-01, REPAIR 1, FIG 201.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 81,683 hrs · 13,229 cycles

WITH ALL ANTI-ICE SYSTEMS ON IN ICING CONDITIONS, RECEIVED A LEVEL 1 BLEED AIR 2 OFF AND LEVEL 1 PACK 2 OFF. SHORTLY, A LEVEL 2 BLEED AIR 1 FAULT. OUTFLOW VALVE FULLY CLOSED. LEVEL 2 EXTINGUSHED WITH THROTTLE NR 1 ADVANCED TO MCT. COMPLIED WITH A FUNCTIONAL AND LEAK TEST OF THE NR 1 HSV IAW MM 36-11-03-700-801, NO FAULTS FOUND.

Part: SLIDE — INOPERATIVE (DOOR) · airframe 81,571 hrs · 13,194 cycles

UNABLE TO DISARM EMERGENCY SLIDE. LEVER WOULD NOT MOVE TO FULLY REAR POSITIONAFTER BEING EXPOSED TO TORRENTIAL RAINFALL DURING SDF STOPOVER DOOR WAS FROZEN. AFTER EXPOSURE TO 100 DEGREE AMBIENT TEMPERATURE IN ONT, DOOR OPS CHECKS NORMAL EMERGENCY SLIDE IS PINNED. OK FOR CONTINUED SERVICE

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,590 hrs · 12,980 cycles

DURING PDC EMERGENCY LIGHTS TEST, RECEIVED A BATTERY LOW MESSAGE. DID NOT GO AWAY. R & R THE BATTERY POWER SUPPLY & OPS TEST PASSED IAW AMM 33-51-01.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 80,424 hrs · 12,939 cycles

INSPECTION TYPE: 3C, LT OTBD FLAP INBD AFT HINGE LOWER LUG INBD FACE HAS CORROSION. REPAIRED THE FLAP HINGE LUG IAW CMM 57-52-04.

Part: SOLENOID — INOPERATIVE (L1 DOOR) · airframe 80,211 hrs · 12,900 cycles

L1 DOOR ELECTRIC OPERATION INTERMITTENT FROM BOTH SWITCHES. TROUBLESHOT IAW FIM TASK 52-11-00-101. FOUND LOCK RELEASE SOLENOID FAILED. REMOVED AND REPLACED IAW AMM 52-11-00-101 ALL OPS CHECKED GOOD IAW 52-11-05-05-525 & 52-34-01-05-855

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 80,203 hrs · 12,896 cycles

L-1 ENTRY DOOR INTERM IN ELECT. R & R L1 DOOR CONTROL POWER INTERLOCK SWITCH. OPS CHECKED GOOD IAW AMM 52-11-02.

Part: HOOK AND LOOP — DAMAGED (LIFE VEST) · airframe 78,749 hrs · 12,569 cycles

CAPTAIN`S LIFE VEST WILL NOT STAY STOWED. CLEANED AND SECURED ATTACHMENT HOOK AND LOOP IAW SOPM 20-30-03 AND 20-50-12.

Part: ACTUATOR — INOPERATIVE (L1 DOOR) · airframe 78,375 hrs · 12,477 cycles

L1 ENTRY DOOR WILL NOT LATCH FULL OPEN OR CLOSE. MOTOR IS INTERMITTENT. R & R L1 DOOR ELECTRICAL ACT REF MM 52-11-01. OPS NORMAL, IPC 52-11-05-05.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 78,295 hrs · 12,462 cycles

EMERGENCY LT BAT 1 LOW DURING PREFLIGHT. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01, OPS TEST SATISFACTORY.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, AFT CARGO BAY CEILING FRAME SUPPORT IS CRACKED. R & R FRAME SUPPORT, INTERCOSTAL, IAW DAC DWG. ACA7751 AND SRM 51-35-01.

Part: FITTING — CORRODED (MLG) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, CENTER LANDING GEAR LT PILLOW BLOCK LOWER MATING SURFACE HAS MODERATE CORROSION AROUND FWD. MOUNT HOLE REPAIRED CORRODED CENTER LANDING GEAR LT PILLOW BLOCK LOWER MATING SURFACE IAW EA 011-5310-01-A6228, REV I/R AND EO MD-11 5340-60673-A.

Part: LONGERON SPLICE — CRACKED (MAIN CABIN) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, MAIN CABIN LONGERON SPLICE 4L AT BS 5-0 IS CRACKED. R & R CRACKED LONGERON 4L SPLICE FITTING AT BS 5-0 IAW SRM 51-33-01.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: C2, RT INBD FLAP UPPER SKIN HAS DENTS THROUGHOUT. R & R RT INBD FLAP ASSY IAW AMM 27-50-20-400-801.

Part: SKIN — GOUGED (BS 1781) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, EXTERIOR FUSELAGE SKIN REPAIR DOUBLER IS GOUGED AT BS 1781, L38R TO 40R. REPAIRED GOUGED FUSELAGE SKIN REPAIR DOUBLER AT BS 1781, L38R TO 40R IAW EA 011-5330-01-A6230, REV I/R AND EO MD11-5330-29631-D.

Part: LONGERON SPLICE — CRACKED (MAIN CABIN) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, MAIN CABIN LONGERON SPLICE FITTING 10L AT BS 5-0 IS CRACKED. R & R CRACKED LONGERON 10L SPLICE FITTING AT BS 5-0 IAW SRM 51-33-01.

Part: SKIN — GOUGED (BS 1002 L41R) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, REPAIR DOUBLER GOUGED AT LOWER AFT CORNER OF FWD CARGO DOOR CUTOUT. REPAIRED DOUBLER IAW EA 011-5330-01-A6227, REV IR AND EO MD11-5330-60617A.

Part: LONGERON — CRACKED · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, LONGERON 44R CRACKED AT BS 5-123. REPAIRED L44R BETWEEN BS 5-93 AND 5-123 IAW EA 011-5310-01-A6223, REV IR AND EO MD11-5310-60692-A.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:C2, CENTER CARGO BAY LONGERON SPLICE 37R IS CRACKED AT BS 5-123. R & R CRACKED SPLICE FITTING AT BS 5-123 LONGERON 37 RT IAW DAC DWG. A5A7114 AND SRM 51-33-01.

Part: LONGERON — CORRODED (BS 555-578) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, LONGERON 44 LT IS CORRODED BETWEEN BS 555 TO 578. REPAIRED CORRODED LONGERON 44 LT BETWEEN BS 555 TO BS 578 IAW SRM 53-00-05, REPAIR 2, FIG 201.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, ACCESS PANEL NR 437CL HAS MANY ELONGATED FASTENER HOLES AND CHAFING DAMAGE ALONG EDGE. REPAIRED DAMAGED ACCESS PANEL 437CL IAW EA 011-5420-01-A6222, REV I/R AND EO MD11-5430-60608-A.

Part: RIB — CRACKED (LT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, LT WING NR 1 SLAT L/E FILLET ASSY RIB CRACKED AT BS XIS 150.74. R & R LT WING NR 1 SLAT L/E FILLET ASSY IAW AMM 27-80-21-400-801.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, LEFT INBD FLAP UPPER SKIN HAS CORROSION AND HAIL DAMAGE. R & R LT INBD FLAP ASSY IAW AMM 27-50-20-401-801.

Part: STRUCTURE — CORRODED · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, RCB FWD FACE SKIN CORRODED UNDER LT, NR 1 FLOOR FITTING. REPAIRED NOTED CORROSION IAW EA 011-5310-01-A6217, REV IR AND EO MD11-5320-60601-A.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED LT WING NR 5 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R LT WING NR 5 SPOILER IAW AMM 27-60-30-400-801.

Part: LEVER — CHAFED (MLG) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, CENTER LANDING GEAR ALTERNATE RELEASE MECHANISM LEVER HAS CHAFE DAMAGE ACCOMPLISHED BLEND REPAIR ON CENTER LANDING GEAR ALTERNATE RELEASE MECHANISM LEVER IAW EA 011-3200-01-A6219, REV I/R AND EO MD11-3230-60588-A.

Part: SKIN — DAMAGED (RT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAILSTORM INSPECTION REVEALED RT WING NR 4 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R RT WING NR 4 SPOILER IAW AMM 27-60-30-400-801.

Part: SKIN — DAMAGED (RT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED RT WING NR 2 SPOILER WITH NUMEROUS HAIL STRIKES. R & R RT WING NR 2 SPOILER IAW AMM 27-60-30-400-801.

Part: SKIN — DAMAGED (RT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAILSTORM INSPECTION REVEALED RT WING NR 5 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R RT WING NR 5 SPOILER IAW AMM 27-60-30-400-801.

Part: STRINGER — CRACKED (RT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E UPPER STR IS CRACKED AT BS XOS. 661- 667. REPAIRED CRACKED RT WING FIXED L/E UPPER STR AT BS XOS 661-667 IAW SRM 57-40-03, REPAIR 2, FIG 202.

Part: SKIN — CORRODED (BS 2153-2163) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:C2, CORROSION AROUND 3 FASTENERS INSIDE ACCESS 316AB ON LOWER SKIN ABOVE APU EXHAUST. REPAIRED CORRODED SKIN AT BS 2153-2163 AND LONGERON 33R IAW SRM 57-70-01, FIG 201, REPAIR 3.

Part: FAIRING — CRACKED (RT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, RT INBD WING SLAT PERFORMANCE FAIRING HAS A CRACKED WEB AT UPPER ATTACH POINT. REPAIRED CRACKED RT INBD WING SLAT PERFORMANCE FAIRING WEB IAW VT-SAA EA 011-5754-01-A6216, REV IR AND EO MD11-5720-60560-A.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED LT WING NR 4 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R LT WING NR 4 SPOILER IAW AMM 27-60-30-400-801.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED LT WING NR 1 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R LT WING NR 1 SPOILER IAW AMM 27-60-20-400-801.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED LT WING NR 3 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R LT WING NR 3 SPOILER IAW AMM 27-60-30-400-800.

Part: SKIN — DAMAGED (LT WING SPOILER) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, HAIL STORM INSPECTION REVEALED LT WING NR 2 SPOILER UPPER SKIN WITH NUMEROUS HAIL STRIKES. R & R LT WING NR 2 SPOILER IAW AMM 27-60-30-400-801.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E BEADED DOUBLER AT BS XOS. 661-667 IS CRACKED. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER AT BS XOS. 661-667 IAW SRM 57-40-02 FIG 203, REPAIR 15.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, RIGHT WING FIXED L/E BEADED DOUBLER CRACKED AT BS XOS. 629 - 633. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER AT BS XOS. 629-633 IAW SRM 57-40-02 FIG 203, REPAIR 15.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CRACKED. R & R CRACKED RCB FLOOR FITTING NR 1 IAW DAC DWG SP11250221 AND SRM 51-31-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE: 2C, LT WING L/E INNER SKIN BEADED DOUBLER IS CRACKED AT BS XOS 542-547.5. REPAIRED CRACKED LT WING L/E INNER SKIN BEADED DOUBLER AT BS XOS.542-547.5 IAW SRM 57-40-02, FIG.203, REPAIR 15.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,044 hrs · 12,405 cycles

INSPECTION TYPE:2C, LEFT WING L/E INNER SKIN BEADED DOUBLER IS CRACKED AT BS XOS.551-555. REPAIRED CRACKED LT WING L/E INNER BEADED DOUBLER AT BS XOS 551-555 IAW SRM 57-40-02, FIG 203, REPAIR 15.

Part: ACTUATOR — INOPERATIVE (CROSSFEED) · airframe 78,035 hrs · 12,401 cycles

DIVERSION - NR 1 FUEL TRANSFEED DISAGREE ALERT DURING FLT NR 1 TANK 2000, LBS IMBALANCE AFTER LANDING NR 1 FUEL TRANSFEED DISAGREE LIGHT DISAPPEARED. R & R NR 1 FUEL CROSS FEED VALVE ACTUATOR IN REF TO MM 28-22-31-4. OPS CHECK NORMAL IN REF TO MM 28-22-30. OK FOR SERVICE. EFF SOURCE 28-22-60-01-25.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 77,784 hrs · 12,346 cycles

DURING PDC, FOUND EMERGENCY ESCAPE BOTTLE OF DOOR R1 PRESSURE LOW. R1 DOOR EMERGENCY ESCAPE BOTTLE SERVICED IAW AMM 12-25-04, PB 301, REV 84.04, DATED 02/25/16.

Part: LONGERON — CORRODED (BS 1501-1521) · airframe 77,513 hrs · 12,280 cycles

INSPECTION TYPE:2C, MAIN CABIN LONGERON 16L, HAS CORROSION BS 1501-1521. R & R THE LONGERON IAW DWG AEA0220 AND SRM 51-33-01.

Part: TRANSDUCER — INOPERATIVE (TIRE PRESSURE) · airframe 76,671 hrs · 12,095 cycles

EMERGENCY DECLARED, APPROXIMATELY 1 HR INTO FLIGHT LEVEL A TIRE DIFF PRESSURE LOW NOSE TIRE PRESSURE SLOWLY DECLINE FOLLOWED BY LEVEL 2 TIRE FAILURE. DEFERRED IAW MEL 32-46-1-2 PLACED RTMTP INDICATION SYSTEM TIRE PRESSURE INDICATION FOR LT NOSE TIRE ON DEFERRAL IAW MEL 32 46 1 2. ACOMPLISHED DMP 32 46 1 2. ASSIGNED CONTROL M561059 PLACARD INSTALLED. REPLACED LT NOSE TIRE PRESSURER TRANDUCER , REF AMM 32-46-04 EFF SOURCE, REF IPC 32-46-0-02.

Part: VALVE — STUCK (NR 2 ENGINE) · airframe 75,929 hrs · 11,886 cycles

FLAME OUT LEVEL NR 2 LAT FUEL UNBALANCE CHECK LIST ACCOMPLISH 1 FILL VALVE STUCK OPEN MULTIPLE ATTEMPTS TO CLOSE NR 1 FILL VALVE CYCLED BACK TO AUTO AFTER MANUALLY BALANCING FUEL INADVERTANT ENGINE NR 2 SHUTDOWN DUE TO F/O TURNED OFF NR 2 TRANSFEED PRIOR TO TURNING TANK NR 2 PUMPS ON PERFORMED RTS ON FSC IAW AMM 28-08-01-741-801. ALL TESTS PASS. ACFT OK TO CONTINUE. THIS REPLACES SDR IPXA2015151389060 DUE TO INCORRECT DATE.

Part: ANGLE — CORRODED (BS 1155) · airframe 75,599 hrs · 11,806 cycles

INSPECTION TYPE:3C, CENTER ACCESSORY COMPARTMENT CLIP AT STA 1155 BETWEEN L51R AND L52 HAS CORROSION. R & R CLIP CENTER ACCESSORY COMPARTMENT STA 1155 BETWEEN L51R AND L52 IAW SRM 51-33-01. MINOR

Part: ANGLE — CORRODED (BS 1159) · airframe 75,599 hrs · 11,806 cycles

INSPECTION TYPE:3C, CENTER ACCESSORY COMPARTMENT CLIP AT STA 1159 ON OTBD SIDE ON L50R HAS CORROSION. R & R CLIP IN CENTER ACCESSORY COMPARTMENT AT STA 1159 OTBD OF L50R IAW SRM 51-33-01. MINOR

Part: DOUBLER — CRACKED (LWS 701) · 11,806 cycles

INSPECTION TYPE:3C, LT WING L/E INNER BEADED DOUBLER CRACKED AT XOS701 REPAIRED LT WING BEADED DOUBLER BETWEEN XOS 698-703 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LWS 618) · 11,806 cycles

INSPECTION TYPE:3C, LT WING L/E INNER BEADED DOUBLER CRACKED AT XOS618. REPAIRED LT WING BEADED DOUBLER BETWEEN XOS616-621 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: LIGHT — INOPERATIVE (CABIN)

AFTER ENGINE START, NO APU, ARMED EMERGENCY POWER ON, LIGHT FAIL TO ILLUMINATE. CONFIRMED EMERGENCY POWER SYS TESTED, PASSED IAW AMM 24-24-00-700-802.

Part: VALVE — STUCK (FUEL FILL) · airframe 74,513 hrs · 11,491 cycles

FLAME OUT LEVEL 2 LAT FUEL UNBALANCE CHECK LIST ACCOMPLISHED. NR 1 FILL VALVE STUCK OPEN MULTIPLE ATTEMPTS TO CLOSE NR 1 FILL VALVE CYCLED BACK TO AUTO AFTER MANUALLY BALANCING FUEL INADVERTANT ENGINE 2 SHUTDOWN DUE TO F/O TURNED OFF NR 2 TRANSFEED PRIOR TO TURNING TANK 2 PUMPS ON. PERFORMED RTS ON FSC IAW AMM 28-08-01-741-801. ALL TESTS PASS. ACFT OK TO CONTINUE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS)

EMERGENCY LIGHT TEST FAILED. R & R POWER SUPPLY BATTERY, EMERGENCY LIGHT TEST PASSED IAW AMM 33-51-01/401, 501.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 73,550 hrs · 11,178 cycles

INSPECTION 1C, RT INBD FLAP UPPER SURFACE DENTED AT XIFH249 AND XIFH255. REPAIRED IAW SRM 57-00-01 REPAIR 1, FIG 201.

Part: SUPPORT FITTING — CORRODED (NR 1 SPOILER) · airframe 73,550 hrs · 11,178 cycles

INSPECTION 1C, MULTIPLE CORRODED BUSHING BORES IN RT NR 1 SPOILER ACTUATOR SUPPORT FITTING. REPAIRED SUPPORT FITTING IAW EA 011-5740 01-A5035 REV IR AND EO MD11-5740-53201-A, MINOR.

Part: STRUCTURE — CHAFED (RT ELEVATOR) · airframe 73,550 hrs · 11,178 cycles

INSPECTION 1C, RT DETACHABLE ELEVATOR L/E CHAFE DAMAGE XE 100.12. REPAIRED ELEVATOR IAW EA 011-5520 -01-A5032, REV IR AND EO MD11-5520-53207-A.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 73,550 hrs · 11,178 cycles

INSPECTION TYPE:1C, VERTICAL STAB REAR SPAR LOWER RT INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL IAW EA 011-5530-01-A5031 REV IR, EO MD11-5530-53194-A, AND SRM 55-30- 02 REPAIR 7, FIG 204.

Part: FINGER DOUBLER — CORRODED (BS 1289-1292) · airframe 73,550 hrs · 11,178 cycles

1C INSPECTION, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN FINGER DOUBLER CORRODED BS 1289-1292, LBL 76-96. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG APB7241 AND SRM 51-35-01.

Part: STRINGER — CRACKED (RT WING) · airframe 73,550 hrs · 11,178 cycles

INSPECTION 1C, RT WING STRINGER 7 CRACKED AT XORS 934. REPAIRED IAW STASA EA 011-5710-01-A5017, REV. IR AND EO 5710-53202-A.

Part: STRUCTURE — CHAFED (RT ELEVATOR) · airframe 73,550 hrs · 11,178 cycles

INSPECTION 1C, RT DETACHABLE ELEVATOR L/E CHAFED DAMAGE XE 53.5. REPAIRED ELEVATOR IAW EA 011-5520-01-A5032, REV IR AND EO MD11-5520-53207-A.

Part: SKIN — DAMAGED (FUSELAGE)

SKIN DAMAGE NOTED 3 FEET AFT OF LWR FWD CARGO DOOR. REPAIRED IAW EO MD11-5330-52829A.

Part: SKIN — PUNCTURED (BS 1834)

FUSELAGE SKIN PUNCTURE LOCATED AT BS 1834 BETWEEN LONGERON 37-38R. REPAIRED IAW EO MD11-5330-52829A.

Part: TERMINAL — LOOSE (SWITCH)

L1 DOOR EVACUATION SLIDE REMOTE PUSH TO TEST INDICATION SYS INOPERATIVE. DURING TROUBLESHOOTING, FOUND ROD TERMINAL LOOSE SCREW BACK OUT. REINSTALLED SCREW AND TERMINAL ON SWITCH IAW AMM 25-61-04. OPS CHECKED NORMAL.

Part: BEARING — SEIZED (INBD FLAPS)

EMERGENCY DECLARED, FLAPS FAILED TO EXTEND TO 35 DEGREES ON APPROACH. ACFT LANDED UNEVENTFULLY. FOUND INBD FLAP DOWNSTOP LINK UPPER BEARING FROZEN. REMOVED FLAP DOWNSTOP LINK ASSY ROUTED TO SM FOR RIV. INSTALLED SERVICEABLE FLAP DOWNSTOP LINK ASSY. SET STOP BOLT OT SAME DIMENSIONS AS REMOVED LINK. ACCOMPLISHED FLAP DOWNSTOP CHECK. OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 1918-1988)

DAMAGE TO FUSELAGE SKIN BS 1918 - 1988 BETWEEN L51L AND L50R. REPAIRED IAW EO MD11-5330-48875-A.

Part: RIB — CHAFED (HORIZONTAL STAB) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, CHAFE DAMAGE ON RT HORIZONTAL STAB RIB CUT-OUT AT XE122.594. REPAIRED CHAFE DAMAGE AT RT HORIZONTAL STAB RIB IAW EA 011-5510-01-A4320 REV IR & EO MD11-5510-48819-A. (MINOR)

Part: LONGERON — CRACKED (BS 1239-1250) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, INTERRUPTED LONGERON 17L CRACKED AT BS 1239-1250. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BS 1239-1250 L17L IAW EA 011-5310-01-A4289, REV IR AND EO MD11-5310-48680-A.

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C LOWER AFT RUDDER UPPER HINGE BRACKET AFT FACE CORRODED AT ZAR 387. REPAIRED CORROSION ON RUDDER HINGE BRACKET IAW STASA EA 011-5540-01- A4284 REV IR AND EO MD11-5540-48697-A. (MINOR)

Part: LONGERON SPLICE — CRACKED (BS 1531 L24R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 24R SPLICE FITTING CRACKED AT STA.1531/5-123. REMOVED FABRICATED AND INSTALLED REPLACEMENT L24R SPLICE FITTING AT STA 1531/5-123 IAW DWG A5A7112 AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1631 L12R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 12R SPLICE FITTING CRACKED AT BS 1631. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L12R SPLICE FITTING AT STA 1631 IAW EA 011-5310-01-A4280 REV IR AND EO MD11-5310- 48696-A.

Part: LONGERON — CRACKED (BS 1245 L19L) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, INTERRUPTED LONGERON ALONG L19L CRACKED AT STA 1245. REMOVED, FABRICATED & INSTALLED REPLACEMENT INTERRUPTED L19L AT BS 1245 IAW EA 011-5310-01-A4287, REV IR, EO MD11-5310-48794-A. (MAJOR)

Part: LONGERON — CORRODED (BS 1481 L18R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 18R CORRODED AT BS 1481. REMOVED FABRICATED AND INSTALLED REPLACEMENT LONGERON 18R BETWEEN BS 1481-1501 IAW EA 011-5310-01-A4281 REV IR AND EO 5310-48796-A. MAJOR.

Part: PRESSURE DECK — DENTED (BS 1476 RBL38) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, PRESSURE WEB DENTED IN MAIN CABIN SUBFLOOR ABOVE RT MAIN WHEEL WELL AT BS 1476, RBL 38. REPAIRED PRESSURE WEB IAW SRM 53-00-02, REPAIR 2, FIG 201.

Part: LONGERON SPLICE — CRACKED (BS 1531 L7R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 7L, SPLICE FITTING CRACKED AT STA 1531/5-0. R & R L7R SPLICE FITTING AT STA 1531/5-0 IAW SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1671 L26R) · airframe 70,068 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 26R SPLICE FITTING CRACKED AT STA 1671. R & R LONGERON SPLICE IAW SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1671 L25R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE:4C, LONGERON 25R SPLICE FITTING CRACKED AT STA 1671. R & R L25R SPLCE FITTING AT STA 1671 IAW SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1631 L12L) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LONGERON 12L SPLICE FITTING CRACKED AT BS 1631. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE FITTING AT L12L STA 1631 IAW EA 011-5310-01-A4280, REV IR, EO MD11-5310- 48696-A. (MAJOR)

Part: SKIN — CORRODED (CENTER WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED AT XCW-101 TO -118 BETWEEN S9 AND S10. REPAIRED CENTER WING UPPER SKIN CORROSION IAW EA 011-5730-01- A4282 REV IR AND EO MD11-5730-48695-A.

Part: DOOR FRAME — CRACKED (BS 1253) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, R3 DOOR FRAME LOWER FWD WEB CRACKED AT LOWER FWD LIGHTENING HOLE. REPAIRED R3 DOOR FRAME INTERIOR WEB IAW SRM 53-40-15, REPAIR 3, FIG 201.

Part: SKIN — CORRODED (CENTER WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, CENTER WING UPPER SKIN CORRODED BETWEEN XCW-101 AND -118 OVER S10. REPAIRED CENTER WING UPPER SKIN CORROSION IAW STASA EA 011-5730-01- A4282 REV IR AND EO MD11-5730-48695-A.

Part: INTERCOSTAL — CRACKED (BS 675 L42R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, FWD CARGO BAY INTERCOSTAL CRACKED AT STA 675 ALONG LONGERON 42R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG ACA7049, SRM AND 51-33-01.

Part: INTERCOSTAL — CRACKED (BS 695 L42R) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, FWD CARGO BAY INTERCOSTAL CRACKED AT BS 695 LONGERON 42R. REMOVED FABRICATED AND INSTALLED REPLACED INTERCOSTAL AT BS 695 ALONG L42R IAW DWG ACA7049 AND SRM 51-35-01 AND 51-33-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 664. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 661-667 IAW SRM 57-40-02, REPAIR 15, FIG 202.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS631.5. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 629-633 IAW SRM 57-40-02, REPAIR 15, FIG 202. (MAJOR)

Part: LONGERON — CRACKED (BS 1239-1250) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, INTERRUPTED LONGERON 17R CRACKED AT STA 1239-1250. REMOVED, FABRICATED & INSTALLED REPLACEMENT LONGERON IAW EA 011-5310-01-A4829, REV IR AND EO MD11-5310-48680-A. (MAJOR)

Part: DOUBLER — CRACKED (RWS 654) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 654 REPAIRED INTERNAL BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: SKIN — CORRODED (BS 2033 L31L) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LT SIDE EMPENAGE EXTERIOR SKIN CORRODED UNDER MYLAR TAPE STA 2024-2163, ALONG LANDINGS FOR HORIZONTAL STAB FAIRINGS. ONE AREA AT STA 2033 L31L EXCEEDED ALLOWABLE LIMITS. REPAIRED SAME IAW STASA EA 011-5330-01-A4312 REV IR AND EO MD11-5330-48780-A (MINOR).

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, CHAFE DAMAGE ON UPPER SURFACE OF LT INBD FLAP VANE NEAR INBD END. REPAIRED CHAFE DAMAGE ON LT INBD FLAP VANE UPPER SURFACE T/E NEAR XIFH 138 IAW SRM 57-50-80. REPAIR 2 WET LAYUP BONDED REPAIR. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XORS 443. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN IAW EA 011-5730-01-A4295, REV IR & EO MD11-5730-48781-A. MAJOR.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XORS566 (XOS670). REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 667-673 IAW EO MD11-5730-42916-D AND SRM 57-40-02, REPAIR 9, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XORS 537 (XOS636). REMOVED PREVIOUSLY INSTALLED BEADED DOUBLER REPAIR AT XOS 643-648. INSTALLED NEW REPAIR TO LT WING FIXED L/E INTERNAL BEADED DOUBLER AT XOS 636-648 IAW EO MD11-5730-42916-D & SRM 57-40-02 REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XORS 452. REPAIRED PER EA 011-5730-01-A4277 REV.IR, EO MD11-5730-48759-A. MAJOR REPAIR

Part: SKIN — DENTED (R1 DOOR) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, UPPER AFT CORNER OF R1 DOOR DENTED. REPAIRED EXTERIOR SKIN OF R1 DOOR AT UPPER AFT CORNER STA YPND 5.5 TO 17.3 IAW SRM 52-10-01, REPAIR 3.

Part: SKIN — DENTED (L1 DOOR) · airframe 71,168 hrs · 10,529 cycles

INSPECTION TYPE: 4C, UPPER AFT CORNER OF L1 DOOR IS DENTED. REPAIRED EXTERIOR SKIN AT UPPER AFT CORNER OF L1 DOOR STA YNPD 5.5 TO 17.3 IAW SRM 52-10-01, REPAIR 3. (MAJOR)

Part: LANDING GEAR — UNKNOWN

ON APPROACH WITH A/P ENGAGED, GEAR HANDLE WAS LOWERED. AP2 DISENGAGED AND NO GEAR LOWERED. ALL GEAR INDICATION UNSAFE. LANDING GEAR EXTENSION/RETRACTION ADJUSTED AND TESTED IAW AMM 32-32-00-5. NO FAULTS NOTED.

Part: RETAINER — BROKEN (EXIT SIGN)

EXIT SIGN FOR L1 DOOR HAS A BROKEN RETAINER. R & R RETAINER AND RE-INSTALLED EXIT SIGN IAW AMM 33-22-05-4.

Part: BATTERY PACK — INOPERATIVE (L1 DOOR SLIDE)

L1 DOOR ESCAPE SLIDE DOES NOT PRESS TO TEST, DEFERRED. R & R BATTERIES. OPS CHECKS NORMAL. REF AMM 25-61-01-4. THIS CLEARS M467163. VERIFIED BOTTLE PRESSURE SERVICED TO FULL.

Part: WEDGE — DELAMINATED (LT ELEVATOR)

LT INBD ELEVATOR UPPER SKIN AND WEDGE DAMAGED. REPAIR IAW EO MD11-5520-44561-B AND SRM 55-20-80, REPAIR 2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE: 3C, 3 DENTS ON CENTER CARGO DOOR EXTERIOR AT LOWER FWD CORNER, NEAR STA 1713, L42R. REPAIRED DENTS AT CENTER CARGO DOOR IAW STA EA-011-5230-01-A3454 & EO MD11-5230-44318-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT WING L/E BEADED DOUBLER XOS 667 CRACKED AT 2 PLACES. REPAIRED LT WING FIXED L/E COMP'T INTERNAL BEADED DOUBLER IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-B.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE: 3C, LEFT INBD FLAP LOWER SKIN INBD END HAS A DENT WITH GOUGE BETWEEN XIFH 140.6 & 147.3, 6" UP FROM T/E AND 12.75" FROM INBD END. FABRICATED AND INSTALLED REPLACEMENT SKIN SECTION ON LT INBD FLAP LOWER SURFACE BETWEEN XIFH133.9-147.3, YIFH34.5-78.1 IAW SRM 57-50-01, REPAIR 1, FIG.201

Part: SLAT TRACK — CRACKED (RT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E SLAT TRACK CUT-OUT XOS 891 CRACKED. REPAIRED RT WING FIXED L/E EXTERIOR SKIN AT OTBD CORNER OF SLAT TRACK CUT-OUT AT STA XOS891 IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: STRINGER — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E STRINGER STA XOS 667 CRACKED. REPAIRED LT WING FIXED L/E COMP'T STRINGER IAW SRM 57-40-03, REPAIR 2, FIG.202.

Part: FORMER — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT WING XOS 1025 PANEL LANDING BRACKET (FORMER) CRACKED BETWEEN AFT FASTENERS. REMOVED, FABRICATED, & INSTALLED REPLACEMENT FORMER IN LT WING FIXED L/E INTERIOR AT STA XOS1025 IAW SRM 51-35-01, 51-33-01, AND DWG ARB2920.

Part: SKIN — DAMAGED (RT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, RT UPPER WING RUB PLATE XOS 240 BETWEEN SLAT 1 & 2 GOUGED AND RIVETS DAMAGED. REMOVED EXISTING REPAIR DOUBLER (RUB PLATE) ON RT WING L/E EXTERIOR AT XOS 240. REPAIRED WING L/E SKIN AT SITE IAW SRM 57-40-02, REPAIR 8, FIG 201 BETWEEN XOS243-250.

Part: SKIN — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E SLAT TRACK CUT-OUT XOS660 CRACKED. REPAIRED LT WING FIXED L/E EXTERIOR SKIN AT XOS 657 CORNER OF SLAT TRACK CUT-OUT IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT FIXED L/E SKIN SPLICE STRAP XOS 660 CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE STRAP IN LT WING FIXED L/E INTERIOR IAW SRM 51-33-01 AND DWG ARB3954.

Part: SKIN — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E PANEL LANDING CRACKED AT STA XOS5503 REPAIRED LT WING FIXED L/E PANEL LANDING AT STA XOS550 IAW SRM 57-40-03, REPAIR 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, LT WING L/E BEADED DOUBLER AT XOS 740 IS CRACKED. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS728-734 IAW SRM 57-40-02. REPAIR 9, FIR 203 & EO-5730-42916-B.

Part: SKIN — DENTED (BS 1001 L40-41R) · airframe 68,849 hrs · 9,938 cycles

INSPECTION TYPE:3C, SKIN DENTED ON LOWER AFT SIDE OF FWD CARGO DOOR CUT-OUT BS 1001, L40R-L41R. REPAIRED REPAIR DOUBLER ON FUESLAGE EXTERIOR, BS 1001, L40-41R IAW SRM 53-00-15, REPAIR 8, FIG 201, STA SA EA 011-5330-01-A3451 AND EO MD11-5330-44313-A.

Part: SKIN — DENTED (LT WING TE FLAP)

LT WING INBD FLAP UPPER SKIN DENTED. REPAIRED IAW SRM 57-00-01. REPAIR 1 AND EO MD11-5750-41731-B.

Part: SKIN — DAMAGED (BS 275 BL 0)

FUSELAGE SKIN DAMAGE, PLANE 25 BL 0 FWD OF STA 275. REPAIRED IAW EO MD11-5330-41507-D.

Part: BATTERY — INOPERATIVE (R1 DOOR)

ON PDC FOUND EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYS INOP R1 DOOR. DEFERRED IAW MEL 25-61-2. PLACARD INSTALLED. DMP C/W AND M435556 ASSIGNED. REPLACED BATTERIES AND RELAMPED. OPS CK OK. REF FIM 25-61-00-1, IPC 25-61-05-01-158 AND AMM 25-61-04-4.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 66,427 hrs · 9,366 cycles

INSPECTION TYPE:2C, IN LT WING OTBD L/E COMP AT XOS 610, THE CEILING HAS 2 EA SMALL CRACKS AT FASTERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203, REV 44.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

REF DMI M430723 AND WAN NR 1645465 EMERGENCY LIGHTNING SYS INOP. T/S IAW FIM 33-52-00-1, FIG 103, ITEM 1,2,3,AND 15. CHECKED FOR GROUND A T PIN 6 OF PLUG P1-1756P IAW WDM 33-52-01, PAGE 2. OK. SUSPECT BATTERY PACK INOP. R & R BATTERY PACK IAW AMM 33-51-01-4. NO HELP. REINSTALLED OLD BATTERY PACK. NOTE: WHEN TEST SWITCH SET TO ON-MSG "EMERGENCY LIGHTS DISARM" OWN. DMI REMAINS.

Part: BULB — INOPERATIVE (ESCAPE SLIDE)

L1 EMERGENCY SLIDE PRESS TO TEST WILL NOT ILLUMINATE. R&R BULBS & RESET SUPPLY BATTERY - OPS CHECKED OK PER MM 25-61-04-4. DEFERRAL CLEARED AND C/W DMP PROCEDURES. OK TO RETURN SYSTEM TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW DURING EMERGENCY LIGHT TEST DEF M415689. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY IAW MM 33-51-01. OPS CHECK GOO. THIS CLEARS M415689.

Part: WEB — CRACKED (FUSELAGE)

FLOOR WEB IN FLIGHT DECK CRACKED. REPAIRED IAW EO MD11-5310-35982-A, ON NRC 346053 AND LP 381864/1.

Part: INDICATION SYS — ACTIVATED (FIRE WARNING)

NR 1 FIRE INDICATION WITH ALL ASSOCIATED BELLS AND WARNINGS. COMPLIED WITH ALL QRH CHECKLIST PROCEDURES. DIVERTED TO NAN. PRIOR TO NR 1 ENG SHUTDOWN, ALL NR 1 ENG INDICATIONS WERE NORMAL. EMERGENCY DECLARED.

Part: WIRE — CHAFED (FIRE DETECTION)

INSPECTION TYPE:N/A DIVERSION - NR 1 FIRE INDICATION WITH ALL ASSOC BELLS AND WARNINGS. COMPLIED WITH ALL QRH CHECKLIST PROCEDURES. DIVERTED TO NAN. PRIOR TO NR 1 ENG SHUTDOWN, ALL NR 1 ENG INDICATIONS WERE NORMAL. EMERGENCY DECLARED. FOUNDING WIRING CHAFING ON THE LT "C" DUCT ADJACENT TO THE 8TH STAGE CHECK VALVE WIRING. REPAIRED PER SWMP 20-10-01 PG 298 115 & 116 PARA 11B, OPS CHECKED NORMAL ON ENGINE RUN.

Part: COWLING — CRACKED (THRUST REVERSER) · airframe 63,930 hrs · 8,722 cycles

INSPECTION TYPE:1C NR 2 ENG LT/HD T/R COWL HAS BADLY CRACKED WEB STRUCTURE AT LOWER L/E WELL MARKED JUST AFT OF ELEC/HYD COWL PUMP ASSY. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AND FILLER IAW P&W CMM78-32-35 REPAIR 34.

Part: DOUBLER — CRACKED (RT WING) · airframe 37,941 hrs · 7,347 cycles

INSPECTION TYPE:1C RT WING L/E COMPT AT STA XFS 791 BEADED DOUBLER CRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBER, AND FILLER IAW MD-11 SRM 57-10-00 FIG 27.

Part: DOUBLER — GOUGED (RT WING) · airframe 63,929 hrs · 8,722 cycles

INSPECTION TYPE-1C REPAIR SURVEY SEQ W4-03 RT WING LE DOUBLER/RUB PLATE GAUGED BETWEEN XIS 240-250 SKIN P/N ARB7580-2. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG. 24

Part: SKIN — MISREPAIRED (RT WING) · airframe 63,930 hrs · 8,722 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ W4-02 RT WING L/E AT TELESCOPIC DUCT CUTOUT HAS AN EXISTING REPAIR NOT PER SRM NOT ON MRCSSR. REMOVED EXISTING REPAIR FROM RT WING L/E TELESCOPIC DUCT CUTOUT AT XOS 459-475, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11- 5730-33834-A AND EA 011-5730-01-A1810.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,930 hrs · 8,722 cycles

INSPECTION TYPE:1C DEFERRED ITEM: D-391775: FUSELAGE SKIN DENT AT STA 295 WL 2-2.5. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS, SPLICE PLATE, STRAPS, AND SHIMS IAW MD-11 SRM 53-20-00 FIG 5 SHT 1 & 2.

Part: REPAIR — DAMAGED (NR 2 PYLON)

INSPECTION TYPE:N/A NR 2 ENG PYLON T/E FAIRING HAS PREVIOUS REPAIR ON RT DAMAGED. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER AND INSTALLED IAW EO C-5430-32701-A.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

INSPECTION TYPE:N/A R1 EVACUATION SLIDE REMOTE PRESSURE PPT LIGHT INOP. REMOVED & REPLACED BULBS. OPS CHECK GOOD PER MM 25 61 04 5. THIS CLEARS M393283. PLACARD REMOVED.

Part: WIRE — NOT SEATED (CABIN)

INSPECTION TYPE:N/A INTERIOR EMERGENCY LIGHTS INOP. RESEATED WIRE NUMBER B315-12-20 AT BLOCK 53-692, BLOCK 2. EMERGENCY LIGHTS SYSTEM OPS CHECKED NORMAL REF MM 33-50-00-5.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH IS SUSPECTED TO BE FAULTY. EMERGENCY LIGHTS WILL NOT COME ON. BATT PACK ALREADY REPLACED. REPLACED LIGHT SWITCH PER MM 33-41-01, NO HELP. CYCLED EMERGENCY LIGHTS CONTROL CIRCUIT BREAKER. ALL EMERGENCY LIGHTS OPS NORMAL PER MM 33-50-00-5.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK IN REF TO MD11 MM 33 51, NO HELP. CYCLED C/B B1-382 SYSTEM. OPS OK PER AMM 33 51 01.

Part: HINGE — CORRODED (TE FLAP) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RHW O/B FLAP I/B HINGE (FLAP MOUNTED) UPPER FWD MOUNTING SPOT FACE FOUND CORRODED. CORROSION REMOVED PER BSOPM20-11-02REV60 ORIG THK 0.751" REMAIN THK 0.746" MAT`L REMOVED 0.005". FPI C/OUT PER DAC NDTSPMREV13PT8 NO CORROSION EVIDENT. RHW AFT OB FLAP INBD HINGE UPPER FWD MOUNTING SPOTFACE THK OF 0.746" ACCEPTED PER EN1182-08. RWK AREA ETCH INSP SATIS, C/OUT FLAP PEENING, CAD PLATE AND PAINT PER EN1182-08. REF MD016812 FOR BUSHING REPAIR AND WASHER INSTL.

Part: FITTING — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RHW LOWER WINGLET ASSY AFT FITTING FOUND CRACKED. RHW LOWER WINGLET ASSY ATTACHED BRACKET AND WINGLET FITTING REMOVED. NEW WINGLET FITTING FASTENER HOLES PICKED UP PER SRM 51-31-01VIIR 35. NEW WINGLET INSTALLED PER SRM 51-31-01VIIR35. ATTACH BRACKET INSTALLED PER SRM 51-31-01VIIR35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 1761 - 1781 X=-27.5. CORROSION ON AFFECTED AREA REMOVED. MAT'L THK: 0.145 INCH (CROWN), MAT'L REMOVED 0.030 INCH (STA1767), MAT'L REMAINING: 0.115 INCH, FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA1731 X=-27.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND ON CRACK EVIDENT. NEW SEAT TRACK AND 01 EA SPLICE HAT SECT REWORKED. ONE SPLICE PLATE FAB, NEW SEAT TRACK AND REPAIR PARTS INSTALLED PER SRM 53-70-00F1 VIR 35.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING L/E TOP PANEL 516ET INTERNAL SUPPORT BRACKETS 03 EA FOUND CRACKED. NR 516ET PANEL INTERNAL (3EA) SUPPORT BRACKETS REMOVED. REPAIR BRACKETS 6EA FAB & HEAT-TREATED. FASTENER HOLES PICK-UP ON 6EA REPAIR SUPPORT BRACKETS. SIX EA REPAIR SUPPORT BRACKETS REPROTECTED, PAINTED & INSTALLED AS PER SRM 57-10-00 VOLI FIG 31 REV 35.

Part: BRACKET — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RHW L/E TOP PANEL NR 616ET INTERNAL SUPPORT BRACKET FOUND CRACKED. INTERNAL SUPPORT BRACKET REMOVED. REPAIR BRACKET FAB 2EA SUPPORT BRACKET HEAT-TREATED AND FASTENER HOLES PICKED UP. REPAIR BRACKETS REPROTECTED AND PAINTED AS PER SRM 51-21-01 VIIR35 2EA REPAIR BRACKETS INSTALLED AS PER SRM 57-10-00VI FIG31 R35.

Part: FITTING — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RHW LOWER WINGLET (WING MOUNTED) FOUND ATTACH FITTING CRACKED. RHW LOWER WINGLET ATTACH FITTING REMOVED. NEW FITTING FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. NEW FITTING HOLES PICKED UP, PROTECTED AND PAINTED. NEW FITTING INSTALLED AS PER SRM 51-33-01 VOL II, REV 35.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 550 FOUND CRACKED (2522). AFFECTED SKIN DOUBLER ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA & FOUND NO CRACK. THREE EACH A REPAIR ANGLES, FILLER & DOUBLER FAB (REF TO EARN: N295UP-0030). THREE EA ANGLES HEAT TREATED. REPAIR PARTS HOLES PICKED-UP, PROTECTED & PAINTED. THREE EA REPAIR ANGLES, FILLER, DOUBLER & ATTACH PARTS INSTALLED.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RIGHT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 556 FOUND CRACKED (2522). RIGHT FIXED WING L/E AFT SKIN DBLR ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES, FILLER & DOUBLER FABRICATED. REPAIR PARTS HOLES PICKED UP, PROTECTED/PAINTED. TWO EA REPAIR ANGLES, FILLER, DOUBLER & ATTACH PARTS INSTALLED. REWORKED AREA PAINTED.

Part: WEB — DENTED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CTR CARGO COMPT AT STA 1841, X=-02 & X=-10, WEB FOUND DENTED AS MARKED. DENTED WEB AT STA 1841, RT & ATTACHING FASTENERS REMOVED. NEW WEB FAB USING MAT'L 7075T6 0.050" PER BOEING DWG ACA7170. HOLES PICKED UP & PAINTING DONE ON NEW WEB. NEW WEB INSTALLED PER SRM 51-33-01VIIR35 & FASTENERS RE-INSTALLED PER SRM 51-33-01VIIR35.

Part: SKIN — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RIGHT WING L/E LWR SURFACE ACCESS PANEL CUTOUT FWD APPROX STA XORS 813 FOUND CRACKED. ATTACH DOOR, FASTENERS & BRACKET REMOVED FROM CRACKED ACCESS PANEL CUTOUT. REPAIR DOUBLER FAB & FASTENER HOLES PICK-UP & PAINTED. REPAIR DOUBLER & ATTACHED BRACKET INSTALLED. RIGHT WING L/E PANEL 626FB INSTALLED AS PER AMM20-50-02R53.

Part: SKIN — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 522 FOUND CRACKED (2478). ATTACHED RIBS 2 EA REMOVED. INNER SKIN BEADED SKIN TRIM OFF. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, REPAIR DOUBLERS & FILLER FAB, 3 EA ANGLES HEAT TREATED. REPAIR PARTS HOLES PICKED UP AND PAINTED. REPAIR ANGLES 3 EA, DOUBLER, FILLER & ATTACHED PARTS INSTALLED AS PER SRM 57-10-00VI FIG 27 R40.

Part: SKIN — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C, LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 538 FOUND CRACKED (2477). LEFT WING NR 4 SLAT CABLE PULLEY REMOVED & L/E FIX WING AFT SKIN FASTENERS REMOVED. INNER SKIN BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, DOUBLER & FILLER FAB REPAIR PARTS HOLES PICK-UP, REPROTECTED & PAINTED. THREE EA REPAIR ANGLES, DOUBLERS & FILLER ATTACH PARTS INSTALLED. NR 4 SLAT CABLE PULLEY INSTALLED.

Part: BUSHING — DAMAGED (RT MLG) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CLG RT TRUNNION FITTING AFT HOLE FOUND SCORING MARK ON EXISTING BUSHING. CLG RT TRUNNION FITTING AFT HOLE BUSHING REMOVED. FPI C/O ON REWK AREA AND FOUND NO CORROSION EVIDENT. AFT BOLT HOLE DIA: 1.4380" & FOUND EXCEED LIMIT MAX ALLOWABLE DIA:1.385". TRUNNION FITTING AFT BOLT HOLE DIA 1.4380" EVAL & FOUND ACCEPTED PER EN1153-08. NEW BUSHING FAB & CADMIUM PLATED. NEW BUSHING INSTALLED AT CLG RT TRUNNION FITTING AFT BOLT HOLE.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 5-113 & STA 1541 LEFT LONGERON 44 FOUND SUSPECTED CRACK WITH STICKER NR 5190. HFEC INSP C/O & FOUND CRACK APPROX 1 INCH. CRACKED LONGERON SPLICE BETWEEN STA 5-113 & 1541 LT L-44 REMOVED. SPLICE HOLES PICKED UP & PROTECTED. NEW SPLICE INSTALLED PER SRM 51-33-01VII R35.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 47 FOUND SUSPECTED CRACK WITH STICKER NR 5187 AND 5189. HFEC INSP C/O AND FOUND CRACK APPROX 4 INCHES. CRACKED LONG SPLICE BETWEEN STA 5- 113 AND 1541 REMOVED PER SRM 51-33-01VIIR35. HOLES PICKED UP ON NEW SPLICE AND PROTECTED. NEW LONG SPLICE INSTALLED PER SRM 51-33-01VIIR35.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 40 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 6.5 INCH. LEFT WING NR 40 STRINGER END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACK AREA C/O & HFEC INSP C/O ON REWK AREA & FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING AND NEW CLIP FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. NEW ARROWHEAD FITTING & CLIP INSTALLED. SEALANT APPLIED. FUEL LEAK CHECK SATIS.

Part: DUCT — CHAFED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, LT WING ANTI-ICE TELESCOPIC DUCT LOWER DOOR FWD AREA FOUND CHAFING MARK. LT WING ANTI-ICE TELESCOPIC DUCT LWR DOOR PANEL REMOVED IAW AMM 20-50-02R53. CHAFING MARK REMOVED FOUND EXCEED LIMIT IAW SRM 57-00-01 VIR 35. NEW PANEL FABRICATED IAW DWG ARM 0078. HEAT TREAT TO T62 IAW DPS7.00-1 HRB 75.4 IS ACCEPTABLE LIMITS IAW DPS1.05-3. FASTENER HOLES PICKUP IAW SRM 51-31-01VII R35. PROTECTED & PAINTED IAW SRM51-21-01VII R35. INSTALLED IAW AMM 20-50-03R53.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541 RT LONGERON 45 FOUND SUSPECTED CRACK WITH STICKER NR 5125 AND 5786. HFEC INSP C/O AND FOUND CRACK APPROX 3 INCHES. CRACKED LONGERON SPLICE BETWEEN STA 5-113 AND 1541, L-45R REMOVED PER SRM 51-33-01VIIR35. HOLES PICKED UP ON NEW SPLICE AND SPLICE PROTECTED. NEW SPLICE INSTALLED PER SRM 51-33-01 VIIR35.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CTR CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 44 FOUND SUSPECTED CRACK WITH STICKER NR 5185 AND 5126. HFEC INSP C/O AND FOUND CRACK APPROX 1 INCH CRACKED LONGERON SPLICE BETWEEN STA 5-113 AND 1541, L-44R REMOVED. HOLES PICKED UP ON NEW SPLICE AND SPLICE PROTECTED. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01VIIR35.

Part: STRINGER — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RIGHT WING FUEL TANK LOWER 44 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH. STR 44 END ARROWHEAD FITTING REMOVED. ATTACHED CLIP & FASTENERS REMOVED. CRACKED AREA TRIMMED OFF. HFEC C/O ON TRIM EDGE, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING & ATTACHED CLIP INSTALL. REWORK AREA PAINTED. LEAK CHECK SATIS.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK LOWER 43 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8 INCH. STR 43 END SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWK AREA, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING FAB WITH FRI C/O & FOUND NO CRACK EVIDENNT. REPAIR ARROWHEAD FITTING & CLIP INSTALLED. SEALANT ON REPAIR AREA APPLIED & LEAK CHECK SATISFACTORY.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 12 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 INCH. STR 12 END SPLICE REMOVED. STR 12 ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON RWK AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES FAB & HEAT TREATED. REPAIR ANGLES, ATTACHED CLIP & SPLICE END INSTALLED. SEALANT ON STR 12 REPAIR AREA APPLIED. LEAK CHECK SATIS.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 11 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 INCH. STR 11 SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON SLOT OUT AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLE FAB & HEAT TREATED. TWO EA REPAIR ANGLES, ATTACHED CLIP & SPLICE END INSTALLED. SEALANT ON STR 11 REPAIR AREA APPLIED. REWORK AREA PAINTED. LEAK CHECK SATIS.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK UPPER 14 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH. STR 14 END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWORK AREA & FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES FAB & HEAT- TREATED. CLIP FAB WITH FPI C/O. FOUND NO CRACK EVIDENT. REPAIR ANGLES, STR END SPLICE & CLIP INSTALLED, WITH SEALANT APPLIED. LEAK CHECK SATIS.

Part: STRINGER — CRACKED (RT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RT WING FUEL TANK UPPER NR 13 STRINGER END SUSPECT CRACK. HFEC INSP C/O AND FOUND CRACK APPROX 8 INCH. NR 13 STR END SPLICE REMOVED. STR CRACKED AREA CUT-OFF AND REMOVED. HFEC C/O ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR STR, STRAP AND 02EA ANGLES FAB. FPI C/O ON FAB STRAP AND ANGLES, FOUND NO CRACK EVIDENT. REPAIR STR, STRAP AND 02EA ANGLES AND ATTACH CLIP INSTALLED. REWORKED AREA PAINTED. LEAK CHK SATIS.

Part: STRINGER — CRACKED (LT WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 41 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8.5 INCH. LEFT WING NR 41 STRINGER END SPLICE REMOVED, ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWK AREA, FOUND NO CRACK EVIDENT. REPAIR ARROW HEAD FITTING FAB, FPI C/O & FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING & ATTACH CLIP INSTALLED. SEALANT APPLIED ON STR 41 REPAIR AREA. LEAK CHECK OK.

Part: SPAR — CORRODED (VERTICAL STAB)

INSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT CUTOUT AT STA ZFS 516-443 APPROX FOUND MINOR CORROSION AS MARKED. VERTICAL STABILIZER FRONT SPAR RT CUTOUT STA ZFS 516.443 APPROX MINOR CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 35, MATL REMOVED 0.005", ORG THICKNESS 0.125". FOUND WITHIN LIMIT AS PER SRM 55-00-01 VOL I FIG 1A REV 35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA1199 X=-8. CORROSION AT AFFECTED AREA REMOVED MAT'L REMOVED 0.040" (STA1199), MAT'L REMN: 0.105", FOUND OUT OF LIMIT. NEW SEAT TRACK FROM STA 1129 TO 1209 X=-8 REWORKED. HOLES PICKED UP ON NEW SEAT TRACK AND PAINTED. NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIG VIR35.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CTR CARGO - BILGE AREA AT BS 1701 TO BS 1710 LONGERON 52 FOUND CRACKED AS MARKED. EXISTING SPLICE AT STA 1701 - 1710 LONGERON 52 REMOVED, CRACKED LONGERON TRIMMED. HFEC INSP C/O ON REWORKED AREA, FOUND NO CRACK EVIDENT. REPAIR LONGERON FABRICATED. FPI C/O ON FAB LONGERON, FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB & FPI C/O, FOUND NO CRACK EVIDENT. HOLES PICK-UP ON LONGERON & SPLICE. NEW LONGERON & SPLICE PAINTED & INSTALLED PER SRM 51-33-01VII R35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE AT STA 808-839 X=107. CORROSION ON AFFECTED AREAS REMOVED. MAT'L THK:0.080" (FLANGE), MAT'L REMOVED: 0.040" (STA 808-824), MAT'L REMN:0.040" FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXIST SPLICE HAT SECT FROM STA 765-889 X=107 REMOVED. HFEC INSP C/O ON TRIM OFF AREA, NO CRACK EVIDENT. NEW SEAT TRACK FROM STA 765-889 X=10 7 REWORKED, HOLES PICK-UP, REPROTECTED, PAINTED AND FINALLY, INSTALLED.

Part: FRAME — CHAFED (TAILCONE) · airframe 62,294 hrs · 8,296 cycles

INSP TYPE-C, FWD TAILCONE ACCESS CUT OUT LT FRAME, FOUND CHAFED MARK ON PREVIOUS REPAIR. FWD TAILCONE UPPER FWD DOOR OPENING MECH ASSY REMOVED FOR ACCESS. CHAFE MARK FOUND OUT OF LIMIT & REMOVED IAW SRM 51-31-01 VII R35. FAB NEW FWD TAILCONE FRAME WITH HEAT TREATMENT C/O. NEW FRAME REWORKED, HOLES KED-UP, PROTECTED & PAINTED. NEW FRAME INSTALLED. OPENING MECH ASSY INSTALLED. FWD TAILCONE UPR DOOR ADJUSTED & OPS CHECKED C/O 'SATISFACTORY'.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 893 X=107. CORROSION ON AFFECTED AREA REMOVED. MAT'L THK:0.145" (CROWN), MAT'L REMOVED:0. 045", MAT'L REMN:0.100" FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXIST SPLICE HAT SECT FROM STA 889 TO STA 969, X=107 REMOVED. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK FROM STA 889-969 X=107 REWORKED. NEW SEAT TRACK HOLES PICK-UP, RE-PROTECTED, PAINTED & INSTALLED.

Part: SKIN — CORRODED (WING) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, CORROSION AROUND FASTENER HEADS ON O/WING CTR FUEL TANK UPPER SURFACE AT STA 1229 X=-87 TO -107. LOCK FASTENER ON AFFECTED AREA REMVD FOR ACCESS. CORROSION REMOVED, MEASURED THK: 0.170", MAT'L REMOVED:0.067", MAT'L REMN:0.103". FOUND OUT OF LMT FPI & 10X VISUAL INSP C/O ON REWK AREA, FOUND NO CORROSION OR CRACK. REWORK AREA REPROTECTED & PAINTED. LOCK FASTENERS INSTALLED FUEL VAPOR BARRIER SEAL APPLIED. FUEL LEAK CHECK C/O, SATIS.

Part: SEAT TRACK — CORRODED (BS 1841) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C AFT CABIN - CORROSION IN SEAT TRACK CHANNEL AT STA 1841 X=107. CORROSION AT AFFECTED AREA REMOVED MATL THK:0.100" (CHANNEL) MATL REMOVED:0.05 0" (STA1841-1853), MATL REMN:0.050". FOUND OUT OF LIMIT. DISCREPANT SEA TRACK AT STA1831 X=107, TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. 01EA SPLICE HAT SECT & 01EA SPLICE PLATE FAB. NEW SEAT TRACK FROM STA 1831-2007 X=107 & REPAIR PARTS INSTALLED SRM 53-70-00 FIG 1 VI R35.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C RHW O/B FLAP O/B HINGE CENTER CAVITY HOLE FOUND CORRODED AS MARKED. RHW AFT O/B FLAP O/B HINGE FWD MOUNTING CENTER CAVITY HOLE CORROSION. REMOVED ORG DIA EVIDENT FLAP HINGE CENTER CAVITY HOLE OF DIA 1.788 INCH EVAL AND FOUND ACCEPTED PER EN1181-08. REWORK AREA ETCH INSP AND FOUND SATIS. FLAP PEENING, CADMIUM PLATING AND PAINTING C/O AS PER EN1181-08.

Part: BUSHING — CORRODED (LT WING TE FLAP) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT IB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03 PG 442-444 R60 ORIG DIA 1.188, FINAL 1.257 MAX ALLOWABLE 1.220. FPI C/O DACNDTSPMR13PT8 NO CORR EVIDENT. RW K AREA PORTECTED, PAINTED & STEP BUSHING FABRICATED IAW EN1179-08. HEAT TREAT D PS5.00-2 HRC41.7 IAW DPS1.05-5. MPI C/O NDT SPM R13PT07 NO CRACK EVIDENT. BUSHING CAD PLATED & INSTALLED IAW EN1179-08.

Part: BUSHING — CORRODED (LT WING TE FLAP) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT OB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03PG442-444R60 ORIG DIA 1.187" FINAL 1.258" MAX ALLOWABLE 1.220". FPI C/O NDT SPM R13PT8 NO CORROSION EVIDENT. AREA PROTECTED & PAINTED, BUSHING FABRICATED IAW EN1179-08. HEAT TREAT DPS 5.00- 2 HRC 43.7 IAW DPS1.05-5. MPI C/O NDT SPM R13PT7 ON BUSHING NO CRACK. BUSHING CAD PLATED & INSTALLED ON EN1179-08.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, RT WING OB FLAP IB HINGE (FLAP MOUNTED) UPPER MOUNTING POINT FWD OB NR 2 BORE HOLE FOUND CORRODED AS MARKED. CORRODED IN AFFECTED AREA REMOVED. ORG DIA 0.599", FINAL DIA 0.6725". FPI C/O ON REWORK AREA & FOUND NO CORROSION EVDNT. BORE FINAL DIA OF 0.6725" EVAL. & FOUND ACCEPTED IAW EN1182-08. FLAP PEENING, CADMIUM PLAT & PAINTING C/O ON REWORK AREA. BUSHING & WASHER FAB AND HEAT-TREATED. BUSHING INSTL WITH BUSHING LINE REAM TO DIA: 0.583". NEW WASHER INSTL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 791 - 909 X=+75.25 FOUND CORROSION. CORR ON AFFECTED AREA REMOVED MAT'L THK:0.145"(CROWN), MAT'L REMOVED: 0.045"(STA.869-896), MAT'L REMN:0.100". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXISTING SPLICE HAT SECT FROM STA 765 TO STA 909 X=+75.25" REMOVED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK FROM STA 765-909 X=+75.25" REWORKED & INSTALLED.

Part: SEAT TRACK — CORRODED (BS 919-969) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN, SEAT TRACK AT STA 919 - 969 X=-75.25 FOUND CORROSION. CORROSION AT AFFECTED AREA REMOVED. MAT'L THK:0.145", MAT'L REMOVED 0.040 INCH (STA 939), MAT'L REMOVED: 0.105 INCH. FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK TRIM OUT. C HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK REWORKED, 1 SPLICE HAT SECT AND 1 SPLICE PLATE FAB. NEW SEAT TRACK AND REPAIR PARTS REPROTECTED, PAINTED AND INSTALLED PER SRM 53-70-00 FIG 1 VIR35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 909 X=+27.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L THK: 0.145", MAT'L REMOVED: 0.040" (STA899), MAT'L REMN: 0.105". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 849 TO 929 X=+27.5 TRIMMED OUT. HFEC INSP C/O ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 2 SPLICE HAT-SECT REWORKED. TWO SPLICE PLATES FAB. NEW SEAT TRACK AND REPAIR PARTS INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 919 X=+8.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L THK: 0.080" (FLANGE), MAT'L REMOVED: 0.050", MAT'L REMN: 0.030 INCH (STA 880) FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 849 AND STA929 X=+8.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 01 SPLICE HAT SECT REWORKED. NEW SEAT TRACK AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIG 1 VIR35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN SEAT TRACK AT STA 929 - 979 X=+8.5, FOUND CORROSION. CORROSION ON SEAT TRACK AT AFFECTED AREA REMOVED MAT'L THK: 0.100"(BASE) MAT'L REMOVED: 0.040", MAT'L REMN: 0.060"(STA959), FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 929-989 X=+8.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 2 SPLICE HAT SECTION REWORKED. TWO SPLICE PLATES FAB NEW SEAT TRACK FROM STA 929-979, X=+8.5 INSTALLED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE-C, CENTER CARGO DOOR CUTOUT, FOUND PREVIOUS REPAIR DOUBLER AT LOWER AFT EDGE CRACKED AND WITH NON STANDARD FASTENERS AS MARKED. CENTER CARGO DOOR CUTOUT-LOWER AFT SIDE HEATING TUBE REMOVED. PREVIOUS REPAIR DOUBLER REMOVED. SKIN TRIMMED & PROTECTED. HFEC INSP C/O ON TRIMMED OFF AREA & FOUND NO CRACK EVIDENT. 3EA REPAIR DOUBLERS & 3EA FILLERS FAB, WITH HOLES PICKED-UP, PROTECTED & PAINTED. 3EA REPAIR DOUBLERS & 3 EA FILLERS INSTALLED. HEATING TUBE RE-INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN CORROSION ON SEAT TRACK CROWN AND FLANGE AT STA 824-865 X=-27. CORROSION ON AFFECTED AREA REMOVED. MATL THK:0.145 INCH (CROWN), MATL REMVD:0.060" (STA 859-861), MATL REMAINED:0.085 INCH FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK REMOVED SEAT TRACK FROM STA 781-869 X=-27 REWORKED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT, NEW SEAT TRACK ON EXISTING SPLICE HAT-SECTION LOCATION FROM STA 781 TO 869 X=-27 INSTALLED PER SRM 51-31-01VIIR35.

Part: SEAT TRACK — CORRODED (BS 830-899) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 830-899 X=-75. CORR AT AFFECTED AREA REMVD. MAT'L THK:0.145"(CROWN), MAT'L REMVD:0.05 0" (STA840), MAT'L REMN:0.095". FOUND OUT OF LMT. DISCREPANT SEAT TRAC K (STA830-929) TRIMMED OUT. HFEC C/O IAW DAC NDT SPM REV13 PART 06-10- 01.001 ON TRIM EDGE & FOUND NO CRACK. NEW SEAT TRACK REWORKED. NEW S.T RACK & REPAIR PARTS REPRTECTED & INSTL PER SRM53-70-00FIG1VOLIREV35.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,294 hrs · 8,286 cycles

INSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT LOWER SKIN EDGE FROM RT L37-L42 FOUND SEVERAL BLENDOUT REPAIRS AS MARKED. FWD CARGO DOOR CUTOUT AFT LOWER HEATING TUBE & SKIN FASTENERS REMOVED. SKIN BLENDED REPAIR AREA TRIM OUT & REPROTECTED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLERS & FILLERS FABRICATED, WITH HOLES PICKED UP, PROTECTED & PAINTED. FAB REPAIR DOUBLERS & FILLERS INSTALLED. HEATING TUBE INSTALLED.

Part: SKIN — CHAFED (TAILCONE) · airframe 62,294 hrs · 8,296 cycles

INSPECTION TYPE:C, RIGHT TAIL CONE DOOR ASSY INTERIOR BELOW BARRIER KEEPER SKIN CHAFED. KEEPER SKIN CHAFE MARK REMOVED & REPROTECTED. MAT'L REMOVED 0.008" ORG THK 0.032", REMN THK 0.024" FOUND OUT OF LIMIT. EXCEEDED LIMIT SKIN TRIMMED OFF. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB, HOLES PICKED UP, REPROTECTED & PAINTED. NEW REPAIR DOUBLER INSTALLED & REWORKED AREA PAINTED.