N563FE

Part: ACCESS DOOR — MISSING (ZONE 100) · airframe 76,479 hrs · 25,027 cycles

DURING WALKAROUND, FOUND AFT ACCESSORY COMPARTMENT DOOR MISSING. NEED IPC 53-52-01-01 ITEM 440 MPN AKC7332-1 LOWER TAILCONE DOOR. REMOVED TAIL CONE IAW MD-10-10 AMM 53-52-00-2. COMPLETED INSTALLATION OF TAIL CONE ASSY. SAFTIED AND LUBED HINGE BOLTS. INSTALLED HINGE FAIRINGS PR MD10-10 M/M 53-52-00-1.

Part: SEAT TRACK — CORRODED (BS 1957) · airframe 76,168 hrs · 24,900 cycles

AFT CARGO COMPT SEAT TRACK F/S 1957 RBL 20 IS EXFOLIATED ON LWR SURFACE. BLENDED SEAT TRACK CORROSION AT STA 1957 RBL 20 AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-00 FIG 5. REMOVED SECTION OF SEAT TRACK IAW SRM 51-31-01 AND SRM 53-70-00 FIG 1. FAB SEAT TRACK IAW SRM 53-70-00 FIG 1 FROM 60-11393/18 BATCH NR 826186, SPLICE CAP FROM 60-71581 BATCH 1336047 AND INSTALLED SEAT TRACK IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,168 hrs · 24,900 cycles

AFT CARGO COMPARTMENT FLOORBEAM AND FLOOR SUPPORT ARE EXFOILIATED AROUND NUMERIOUS NUTPLATES ON UPPER CHORDS ALONG ENTIRE LENGTH AT F/S 1841 BLENDED WORN AREAS IAW SRM 51-21-01 CHECKED LIMITS ORIGINAL MAT. .094 AFTER REWORK .078 WITHIN LIMITS ON FLOORBEAM, ON FLOOR SUPPORT ORIG MAT .063 AFTER REWORK .054 WITHIN LIMITS IAW SRM 53-00-01 FIG 1A. FOUND SECTION OF FLOORBEAM BETWEEN LBL 12 TO RBL 50 OUT OF LIMITS SPLICED NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 FIG 9 VOL 1.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,168 hrs · 24,900 cycles

AFT CARGO COMPARTMENT FLOORBEAM AND FLOOR SUPPORT ARE EXFOILIATED ARROUND NUMEROUS NUTPLATES ON UPPER CHORDS ALONG ENTIRE LENGTH AT F/S 1841 BLENDED WORN AREAS IAW SRM 51-21-01 CHECKED LIMITS ORIGINAL MAT. .094 AFTER REWORK .078 WITHIN LIMITS ON FLOORBEAM, ON FLOOR SUPPORT ORIG MAT. .063 AFTER REWORK .054 WITHIN LIMITS IAW SRM 53-00-01 FIG 1A. FOUND SECTION OF FLOORBEAM BETWEEN LBL 12 TO RBL 50 OUT OF LIMITS SPLICED NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 FIG 9 VOL 1.

Part: SEAT TRACK — CORRODED (BS 1351) · airframe 76,168 hrs · 24,900 cycles

MAIN CARGO DECK STA 1351 RBL 28 SEAT TRACK IS DAMAGED BLENDED AREA OUT OF LIMITS IAW SRM 53-70-00 VOL 1. REMOVED SEAT TRACK IAW SRM 53-70-00. FABBED NEW SEAT TRACK ON TRAVELER NR T7/713046. INSTALLED SEAT TRACK IAW SRM 53- 70-00 FIG 1 VOL.1

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 73,691 hrs · 23,761 cycles

RECEIVED LEVEL 3 CARGO FIRE AFT ALERT. RAN QRH AND FIRED AGENT BOTTLE. PROCEEDED TO NEAREST AIRPORT ABQ. ON DECENT FIRED 2ND AGENT BOTTLE AS PRECAUTION. INST SERVICEABLE FIRE BOTTLE NR 2 POS PER MM 26-22-01-4. INSTALLED SERVICEABLE FIRE BOTTLE NR 1 POS IN REF MD10-10 MM 26-22-01-4. ALL 3 VIA RTS CHECKS GOOD. ACCOMPLISHED LOWER CARGO SMOKE DET TEST. MM 26-14-01-5 CHECK NORMAL. R/R MSC MM 31-42-01-4 RTS CHECKS GOOD. REF.31-42-01-5. PER MOCC REQUEST VERIFIED WIRING IN BULK CARGO AREA DETECTORS A2-44 & A2-45 TO MSC, POWER, & GND. ALL CHK'S NORMAL REF WDM 26-14-01 R/R ALL LOWER CENTER & AFT CARGO COMP FIRE DETECTORS. OP'S CK GOOD. PER MM 26-14-01-4.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,656 hrs · 23,743 cycles

PAINT STRIPED HOLE CLEANED IAW SRM 51-21-01 VOL 2 NDI PERFORMED (SEE JPF) FINDING RECORDED SEE ATTACHED SHEET, STRUCTURAL REPAIR EA NR 8-5710-96067. PERFORMED FABRICATED PART IAW DETAIL PARTS TRAVELER N I012300/N02300 AND DWG ARC0448 SRM 57-31-01 VOL 3 EA NR 8-5710-96067.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

EXT FUSELAGE DEEP DENT ON SKIN FROM STA 1701 TO STA 1710, FROM L 46 LT TO L47LT, DIM 6" BY 3" DEPTH 0.090". STRIPPED PAINT IAW SRM 51-21-01 PARA C AG 26 VOL 2. REMOVED FLOOR PANELS IAW SRM 51-31-01 PAGE 36-41. REMOVED BLANKETS IAW MM 25-80-00-2. TRIMMED OUT DAMAGE AREA AND INSTALLED EXTERNAL REPAIR DOUBLERS AND FINGERS DOUBLER IAW SRM 53-20-00 FIG 6 SHT 3-4 AND SHT 2A PAGE 72 AVOL 1. REINSTALLED BLANKETS IAW AMM25-80-00-2. INSTALLED FLOOR PANELS IAW SRM 53-20-00 FIG 6. RESTORED PAINT IAW SRM 51-21-01 PAR 31-24 VOL2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N02068 IAW SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — CORRODED (BS 1331) · airframe 73,656 hrs · 23,743 cycles

LWR FUSELAGE, BELLY SKIN FOUND ONE EXTERNAL DOUBLER REPAIR ON STA 1331 LONG 52, DIM 8 X 5 INCHES. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND WIDE SPREAD PITTING MODERATE CORROSION ON EXTERNAL DOUBLER & N.12 RIVETS INSTEAD OF HI-LOKS ON LONG 52 IAW 53-40-00 FIG 20 VOL 1. EXISTING DOUBLER WILL BE REMOVED AND DISCARDED DUE TO CORROSION REWORKED AND SKIN REPAIRED COVERED IN NRC N01912.

Part: STRUCTURE — UNKNOWN (T/E FLAP) · airframe 73,656 hrs · 23,743 cycles

REMOVED AND REINSTALLED SECTION INBD FLAP IAW MM 20-50-02-2. FAB PARTS IAW DETAIL PART TRAVELER N02301 AND SRM 57-10-00 FIG 4 VOL1.

Part: FRAME — CORRODED (CENTER WING) · airframe 73,656 hrs · 23,743 cycles

CENTER WING, LWR BARREL SECTION, FOUND CORROSION BETWEEN STA -Y 1319 TO 1339, LONG 50L TO 50R; ON FRAMES, CHORDS, LONGERONS SKIN. FASTENERS REMOVED IAW SRM 53-33-01, CORROSION REMOVED IAW SRM 1-21-01 PARA 34. INSPECTED PERFORMED SKIN REPAIR, COMPLETED IAW SRM 53-20-00 FIG 6 SH 3 VOL 1. FRAME REPAIR COMPLETED IAW SRM 51-33-01 PAR 34/47 VOL 2. FABRICATED PART IAW DETAIL PARTS TRAVELER N01912 AND SRM 53-20-00 FIG 6 SHT 3 VOL 8.

Part: SKIN — DAMAGED (BS 1501-1521) · airframe 73,656 hrs · 23,743 cycles

LWR FUSELAGE, BELLY SKIN, FOUND AN EXTERNAL DOUBLER REPAIR FROM STA 1501 TO STA 1521 BETWEEN LONG 47R AND LONG 47L DIM 11 X 44.5 INCHES. REMOVED EXISTING DOUBLER, INSTALL NEW DOUBLER IAW SRM 53-40-00 FIG 20 AND SRM 51-33-01 PG 34-47. FABRICATED PART IAW DETAIL PART TRAVELER N N01166 AND SRM 53-40-00 FIG 20 VOL 1.

Part: NONE — NONE (NONE) · airframe 73,656 hrs · 23,743 cycles

RIGHT FUSELAGE STA 535 TOP AFT CORNER NR 3 PACK A/C COMPARTMENT FOUND EXISTING DOUBLER REPAIR. INSTALLED NEW ROW FASTENERS IAW SRM 51-33-01 VOL 2 AND 53-50-00 FIG 3 VOL 1.

Part: SKIN — CORRODED (BS 1271) · airframe 73,656 hrs · 23,743 cycles

LWR FUSELAGE, BELLY SKIN FOUND EXTERNAL DOUBLER REPAIR AT STA 1271 LONG 52, 8 X 15 INCHES. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND WIDESPREAD PITTING MODERATE CORROSION ON EXTERNAL DOUBLER N.12 RIVETS INSTEAD OF HI-LOKS ON LONG 52 IAW SRM 53-20-00 FIG 20 VOL 2. EXISTING DOUBLER WILL BE REMOVED ON NRC N01909 - SKIN REPAIRED DUE TO CORROSION REMOVED WILL BE ACCOMPLISHED ON THIS NRC N01909.

Part: NONE — NONE (NONE) · airframe 73,656 hrs · 23,743 cycles

RIGHT FUSELAGE STA 535 TOP AFT CORNER NR 3 PACK A/C COMPARTMENT FOUND EXISTING DOUBLER REPAIR. INSTALLED NEW FASTENERS IAW SRM 51-33-01 VOL 2 & 53-50-00 FIG 3 VOL 1.

Part: NONE — NONE · airframe 73,656 hrs · 23,743 cycles

BUSHING REPAIR ON BRACKET RIGHT WING. PERFORMED INSPECTION ON REPAIR BUSHING FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 1741-1761) · airframe 73,656 hrs · 23,743 cycles

LWR FUSELAGE LT HAND SIDE HAS AN EXTERNAL DOUBLER REPAIR IN SKIN BETWEEN STA 1741 AND 1761 LONG 37 TO 39. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 6 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01197/I011197 IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

CNT CARGO COMPT HAS AN ANGLE REPAIR AT FLOORBEAM STA 1701 RT SIDE X-27 TO X- 40. REMOVED EXISTING 5/32 HI-LOCKS AND REPLACED WITH HLT334-6 IAW SRM 53-00-01 FIG 7. AFTER REWORK REPAIR IS IN COMPLIANCE WITH CRITERIA REQUEST BY EO #8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 1391 S52) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1391 LONG 52. AFTER INSP DOUBLER REMOVED AND REPLACED NEW IAW SRM 53-40-00 FIG 20 SHT 5 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01073/I011073 AND SRM 53-40-00 FIG 20 VOL 1.

Part: NONE — UNKNOWN · airframe 73,656 hrs · 23,743 cycles

LT WING L/E XOS 604 DOUBLER REPAIR FOUND. REMOVED EXISTING REPAIR DOUBLER, DRESSED OUT OF CUTOUT OF SKIN. ACCOMPLISHED STEP 1-2-3-4-5-6-7-8-9-10 OF FEDEX EA 8-5710-95688. FABRICATED PART IAW DETAIL PART TRAVELER N01218/I011218 IAW DWG ARB1137, BOEING ATM P0206335 AND SRM 57-10-00 FIG 68 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FOUND AN EXTERNAL DOUBLER AT FWD JAMB CNT CARGO COMPT ON SKIN FWD STA 1701 BTWN LONG 40-42. REMOVED SCUFF-PLATE IAW SRM 51-31-01 VOL 2. CLEANED AND TREATED AREA IAW SRM 51- 21-01 VOL 2, REPAIRED AREA IAW SRM 53-50-00 FIG 26 SHT 3 VIEW B. REINSTALLED SCUFF PLATE AND RESEAL IAW SRM 51-31-01 VOL 2AND SRM 51-41-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I011177/N01177 AND SRM 53-50-00 FIG 26 VOL 1.

Part: NONE — UNKNOWN · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1475 LONG 52. AFTER INSP DOUBLER REMOVED AND REPLACED NEW IAW SRM 53-40-00 FIG 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01163/I011163 AND SRM 53-40-00 FIG 20 VOL 2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE RT SIDE ON SKIN AFT DOOR JAMB FWD CARGO COMPT FOUND AN EXT DOUBLER REPAIR AT STA 959 BETWEEN LONG 38-42. REMOVED DAMAGE ALONG EDGE OF AFT JAMB IAW SRM 53-50-00 FIG 26 SHT 2 VOL 1. DRESSED OUT EXT SKIN CUTTED OUT INTERNAL DOUBLER, TREATED CUT OUT AREA IAW SRM 51-21-01 VOL 2. REPAIRED JAMB IAW SRM 53-50-00 FIG 26. INSTALLED FILLER, DOUBLERS. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I011171/N01171 AND IAW SRM 53-50-00 FIG 26 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

EXTERNAL FUSELAGE BELLY SKIN STA 995-1029 BETWEEN LONGERONS 51 RT AND 51 LT, FOUND EXTERNAL DOUBLER REPAIR. REMOVED REPAIR IAW SRM 51-35-01 VOL 2. STRIPPED PAINT FROM AREA IAW SRM 51-210-01 PAGE 26 VOL 1. REMOVED FS BETWEEN STA 1000 TO 1045 LONG 48L-48R. CUT SKIN SECTION AT STA 1006 TO 1042. CUT PRODUCTION SKIN SPLICE REPLACEMENT SECTION IAW SRM 53- 20-00 FIG 17 VOL 1 SHT 1-2-5. CUT DAMAGED AREA OF TEAR STRIP AT STA 1019 AND REPAIRED IAW SRM 53-20-00 FIG 18 VOL 1 AT STA 1039. CUT DAMAGED TEARSTRIP AND MADE AN INTERNAL DOUBLER OF THE AFT SPLICE IAW SRM 53-20-00 FIG 17 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE ON EXT SKIN RT SIDE FWD CARGO DOOR FWD JAMB FOUND AN EXTERNAL DOUBLER REPAIR AT STA 879 LONG 38-42. REMOVED EXISTING REPAIR IAW SRM 51-33-01 VOL 2. STRIPPED AREA IAW SRM 51-21-01 PAGE 26 VOL 2. REMOVED DAMAGE ALONG EDGE OF FWD JAMB IAW SRM 53-50-00 FIG 26 SHT 2 VOL 2. REPROTECT REWORKED AREA IAW SRM 51-21-01 VOL 2. INSTALLED DOUBLER REPAIR AT JAMB IAW SRM 53-50-00 FIG 9 VOL 1. REPAIR IS ACCEPTABLE FOR RWSM OPERATION IAW SRM 53-00-02 FIG 1 SHT 2 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

UPPER FUSELAGE FOUND AN EXTERNAL DOUBLER REPAIR ON SKIN AT L-1 DOOR JAMB STA 420 LONG 15-16. REMOVED DOUBLERS IAW SRM 51-33-01 VOL 1. CLEANED AREA IAW SRM 51-41-00 VOL 2 AND BLENDED OUT GOUGED AREA IAW SRM 53-00-01 FIG 1A. PERFORMED INSP IAW NDI, NO CRACK FOUND. REPROTECTED REWORKED AREA IAW SRM 51-21-01 VOL 2 AND INSTALLED REPAIR DOUBLERS IAW SRM 53-50-00 FIG 26 VOL 1.

Part: FRAME — DAMAGED (BS 575 S30R) · airframe 73,656 hrs · 23,743 cycles

AIR COND COMPT STA 575 LONG 30 RT FOUND DEEP WEAR 0.45" LONG .300" ON FRAME P/N ACA3809-401. REMOVED CLIP P/N ACA3809-17 IAW SRM 51-35-01 PAGE 1-13 BLEND OUT DAMAGED SECTION ON FRAME, INSTALLED INTERNAL ANGLE P/N I012284-3. FABRICATED SHIMS P/N I012284-7 AND P/N I012284-11, INSTALLED CLIP P/N I012284-5 IAW SRM 53-30-00 FIG 4 PAGE 13 VOL 1 AND IAW DWG ACA3809 AND SRM 53-00-01 PAGE 20 VOL 1. FAB PART IAW DETAIL PART TRAVELER N02284/I012284 AND SRM 53-30-00 FIG 4 PAGE 13 VOL 1.

Part: REPAIR — UNKNOWN · airframe 73,656 hrs · 23,743 cycles

FOUND AN ANGLE AND SPLICE REPAIR ON FWD CARGO DOOR FWD PAN CLOSE TO THE UPPER CORNER. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 17 VOL 1. FAB PART IAW DETAIL PART TRAVELER N01205 AND SRM 52-10-00 FIG 17 VOL 1.

Part: NONE — NONE · airframe 73,656 hrs · 23,743 cycles

EXT DOUBLER REPAIR DIM 43" BY 46" FROM STA 1089 TO 1129 LONG 42-48 RT. PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. PERFORMED EA NR 8-5330-95691 P1.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 73,656 hrs · 23,743 cycles

FOUND NR 6 REPAIR UPPER SKIN RIGHT OUTBOARD FLAP. REMOVED SKIN TRIMMED OUT DAMAGED RIBS, FABRICATED NR 3 INTERNAL ANGLE REPAIR AND FILLER REPAIR IAW SRM 57-00-01 FIG 10 VOL 1, REPAIRED AND REINSTALLED NEW SKIN IAW SRM 57-10-00 FIG 7 VOL 1. FAB PART IAW DETAIL PART TRAVELER F011229/N01229 IAW SRM 57-10-00 FIG 7 VOL 1 AND SRM 57-00-01 FIG 10 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FOUND EXTERNAL DOUBLER ON RT STA 1039 TO 1059 BETWEEN LONG 40 TO 42. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 6 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01173 AND SRM 53-20-00 FIG 6 VOL 1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

CNT CARGO COMPT LONG 52 HAS A SPLICE REPAIR BETWEEN STA 1741 AND 1761. FITTED NEW SPLICE IAW SRM 53-10-00 FIG 2 SHT 1 VOL 1 AND EA 8-5310-95690, FAB PARTS IAW DETAIL PARTS TRAVELER N01188 AND SRM 53-10-00 FIG 2 VOL 1.

Part: REPAIR — UNKNOWN (BS 1741-1761) · airframe 73,656 hrs · 23,743 cycles

CNT CARGO COMPT BETWEEN STA 1741 AND 1761 HAS A SPLICE REPAIR ON LONG 51 RIGHT. FITTED NEW SPLICE IAW SRM 53-10-00 VOL 1 AND EA 8-5310-95690. FAB PART IAW DETAIL PART TRAVELER N01186 AND SRM 53-10-00 VOL 1.

Part: REPAIR — UNKNOWN (BS 1741-1761) · airframe 73,656 hrs · 23,743 cycles

CNT CARGO COMPT HAS A SPLICE REPAIR ON LONG 51 LT BETWEEN STA 1741 AND 1761. FITTED NEW SPLICE IAW SRM 53-10-00 FIG 2 SHT 1 VOL 1 AND EA 8-5310-95690, FAB PART IAW DETAIL PART TRAVELER N01187 AND SRM 53-10-00 VOL 1.

Part: REPAIR — UNKNOWN (BS 869-889) · airframe 73,656 hrs · 23,743 cycles

FWD CARGO COMPT THERE IS A REPAIR ON LONG BETWEEN STA 869-889. REMOVED SPLICE AT STA 889 IAW SRM 51-33-00 VOL 2. INSTALLED NEW LONG SPLICE IAW SRM 53-10-00 FIG 2 VOL 1 AND ACCOMPLISH EA 8-5310-95690.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

FWD CARGO DOOR AFT PAN HAS AN ANGLE REPAIR DIM 7 X 4 X 1.6 INCHES. PERFORMED GVI ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100- 7-5001 P2.

Part: SPAR CAP — DAMAGED (WING) · airframe 73,656 hrs · 23,743 cycles

DURING NDT INSPECTION FOUND CRACK ON LOWER SPAR CAP HOLE. PERMANENT REPAIR ACCOMPLISHED IAW FEDEX EO 8-5710-7-3318 P2 CONDITION 3 STEP 5 AND DWG SR10570048 CONFIGURATION -7015.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

FOUND AN EXT TRIPLE DOUBLER REPAIR ON SKIN RIGHT SIDE BETWEEN STA 1129 AND 1159 LONG 43 - 48 DIM 25" X 36" , 25" X 35". PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P1.

Part: SKIN — DENTED (BS 979) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY LWR FUSELAGE RT SIDE FOUND MANY DENTS ON SKIN STA 979 LONG 39 TO 42. REMOVED DENT IAW SRM 53-20-00 FIG 13 SHT 14 NOTE (C) VOL 1 PERFORMED INSP IAW SRM 53-20-00 VOL 1 NO CRACK FOUND BLENDED AND POLISH NICKS IAW SRM 53-20-00 FIG 13 SHT 2B VOL 1 ORIGINAL THK IS .068 INCH RESIDUAL THK IS .066 INCH PERCENTAGE MTL REMOVED IS 2.9 PERCENT. VERIFIED LIMITS IAW SRM 53-20-00 TAB (A) FIG 13 SHT 2B VOL 1 MTL REMOVED IS WITHIN LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER REPAIR IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER N00189 AND SRM 53-20-00 FIG 13 SHT 14 VOL 1.

Part: SKIN — CRACKED (BS 383) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY EXISTING DOUBLER FUSELAGE SKIN STA 383 AND 410 Z-30 FOUND EXT DOUBLER REPAIR. REMOVED OLD SKIN INSTALLED NEW SKIN P/N ABA7049-3 IAW DWG ABA7049/ABA7035 AND SRM 53-40-00 FIG 15 VOL 1. ON EXISTING HOLES AT SKIN ABA7048-3 7EA HOLES INSTALLED RIVETS. IAW SRM 51-35-01 VOL 2 AND SRM 53-20-00 FIG 13 VOL 1 INSTALLED SEALANT IAW SRM 51-41-02, FIG 1 VOL 2.

Part: REPAIR — UNKNOWN · airframe 73,656 hrs · 23,743 cycles

FWD CARGO DOOR FWD PAN HAS A SPLICE REPAIR. PERFORMED REPAIR BY REMOVING SPLICE AND INSTALLED NEW ONE IAW SRM 51-33-01 VOL 2, SRM 51-35-01 VOL 2 AND SRM 52-00-01 FIG 7 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01204 AND SRM 52-00-01 FIG 7 SHT 2-3 VOL 1.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

FOUND EXT DOUBLER APPROX 4 X 4 INCH ON RIGHT T/E HORIZ STAB AT STA XE 87.167 UPPER SIDE. PERFORMED GVI ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100- 7-5001 P2.

Part: SKIN — DENTED (BS 1970) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY EXT FUSELAGE LOWER DEEP DENT ON EXT SKIN AT STA 1970 FROM LONG.38 LT TO LONG 39LT. REFORMED DENT AND NDI INSP. NO CRACK FOUND IAW SRM 53-20-00 FIG 13 VOL 1. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-20-00 FIG 13 SHT 14 FABRICATED PART IAW DETAIL PART TRAVELER I010197/N00197 IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

FOUND REPAIR ANGLE IN NLG W/W AT STA 515 LONG 48 LEFT. PERFORMED GVI ON REPAIR ANGLE FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: NONE — NONE (NONE) · airframe 73,656 hrs · 23,743 cycles

FOUND REPAIR STRAP IN LEFT ACC AT STA 561 LONG 48 LEFT. PERFORMED GVI ON REPAIR STRAP FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE · airframe 73,656 hrs · 23,743 cycles

FOUND AN EXT DOUBLER REPAIR ON SPLICED AREA BETWEEN STA 780 AND 809 LT HAND SIDE AND LONG 45-48 DIM 24.5 X 29.5 INCHES. PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P1.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 73,656 hrs · 23,743 cycles

RT OUTBOARD FLAP LOWER SKIN: DURING ACCOMPLISHED NRC N01229 FOUND EXISTING REPAIR INTERNAL LOWER SKIN WITH CUTOUT NOT IN COMPLIANCE WITH SRM. REMOVED PANEL SECTION TO PERFORM REPAIR IAW MM 20-50-02 AND REMOVED SEALANT IAW SRM 51-41-01 VOL 2. REPAIRED SKIN IAW SRM 57-10-00 FIG 7 VOL 1, PANEL SECTION WILL BE INSTALLED WITH NRC N01229, FABRICATED PART IAW DETAIL PART TRAVELER I012287/N02287 AND IAW SRM 57-10-00 FIG 7 VOL 1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 73,656 hrs · 23,743 cycles

DURING U/S INSPECTION OF HORIZONTAL STAB FOUND CRACK ON INTERIOR SKIN PANEL UPPER SURFACE. REMOVED AND REPLACED PANEL.

Part: REPAIR — UNKNOWN (BS 295-313) · airframe 73,656 hrs · 23,743 cycles

EXISTING REPAIR LT SIDE NOSE SECTION STA 295-313 Z-30. REMOVED REPAIR DOUBLER IAW SRM 51-35-01 VOL 2, REMOVED SEALANT AND FR PRIMER IAW SRM 51-41-01 VOL 2. PERFORMED NDI ON INTERNAL FRAME NO CRACK FOUND. FOUND CRACK ON SKIN LONG .5 INCH AT STA 298. REMOVED SECTION OF THE DAMAGE SKIN AND REPAIR IAW SRM 53-20-00 FIG 11 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01155 AND SRM 53-20-00 FIG 11 VOL 1.

Part: REPAIR — UNKNOWN (BS 1250-1256) · airframe 73,656 hrs · 23,743 cycles

MAIN CABIN CTR FUSELAGE L-3 FWD DOOR JAMB HAS AN EXTERNAL DOUBLER REPAIR BOTTOM PART STA 1256 DIM 7 X 10 INCH. REMOVED AND REPLACED BOLTS WITH HLT 436-6 IAW SRM 51-33-01 PAGE 6-10 VOL 2 AND SRM 53-50-00 FIG 19 VOL 1.

Part: SKIN — DENTED (BS 1801-1821) · airframe 73,656 hrs · 23,743 cycles

LWR FUSELAGE RT SIDE FOUND DEEP DENT ON SKIN BTWN STA 1801 AND STA 1821 FROM LONG 34 TO LONG 33. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1 AND SRM 51-33-01 PAG 34-47. FABRICATED PART IAW DETAIL PART TRAVELER I010193/N00193 IAW SRM 53-20-00 FIG 13 SHT 14 VOL 1.

Part: DOOR FRAME — CRACKED (BS 1307) · airframe 73,656 hrs · 23,743 cycles

MAIN CABIN FOUND CRACK 0.25" LONG ON WEB DOOR JAMB AT STA 1307 L15 RT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N00505 AND SRM 53-50-00 FIG 19 VOL 1.

Part: FRAME — CRACKED (BS 695) · airframe 73,656 hrs · 23,743 cycles

FWD CARGO COMPT BILGE FOUND CRACK 0.25" LONG ON CAP ANGLE AT STA 695 FROM L49 RT TO L50 RT. CUT AND REMOVED CAP FRAME BTWN L51-52 RT AND BTWN 47-48 RT INSTALLED NEW SECTION OF FRAME CAP AND NEW SPLICES IAW SRM 53-30-00 FIG 5 VOL 1 REF SRM 53-30-00 FIG 8 SHT 1 NOTE 3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N00292 AND SRM 53-30-00 FIG 5 VOL 1.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 73,656 hrs · 23,743 cycles

MAIN CABIN L3 JAMB DOOR STA 1256 X 100 Z 61 FOUND CRACK 1/2 INCH LONG ON WEB'S JAMB. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01460 AND SRM 53-50-00 FIG 19 VOL 1.

Part: FRAME — CRACKED (BS 715) · airframe 73,656 hrs · 23,743 cycles

FWD CARGO COMPT BILGE FOUND 2 CRACKS ON CAP ANGLE AT STA 715 FROM L49 RT TO L50 RT. CUTTED AND REMOVED CAP FRAME BTWN L51-52 RT AND BTWN L47-48 RT INSTALLED NEW SECTION OF FRAME CAP AND NEW SPLICES IAW SRM 53-30-00 FIG 5 VOL 1 REF SRM 53-30-00 FIG 8 SHT 1 NOTE 3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N00291 AND SRM 53-30-00 FIG 5 VOL 1.

Part: REPAIR — UNKNOWN (SLAT TRACK) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY RIGHT HAND WING L/E SLAT TRACK NR 10 CUT OUT ON LOWER SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XOS 657 DIM. 7.5" X 5" CORRECTIVE ACTION R/R REPAIR IAW SRM 57-10-00 FIG 68 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER N01213 AND SRM 57-10-00 FIG 68 VOL 1.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 73,656 hrs · 23,743 cycles

LT WING OUTBOARD FLAP L/E STA 758 ON RIB FOUND CRACK 0.60 INCH LONG. REMOVED, REPAIRED AND REINSTALLED RIB IAW SRM 57-00-01 FIG 0 SHT 1-3-4 VOL 1, SRM 51-35-01 PAR 1-5 VOL 2 AND SRM 51-33-01 PAGE 34-47 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER N00402 AND SRM 57-00-01 FIG 10 SHT 1-3-4 VOL 1.

Part: DOUBLER — UNKNOWN (RT WING) · airframe 73,656 hrs · 23,743 cycles

RIGHT WING L/E SKIN EXTERNAL DOUBLER AT STA XOS 900 TO STA XOS 916. REWORKED REPAIR IAW SRM 57-10-00 FIG 28 VOL 1, REPAIRED IAW SRM 57-10-00 FIG 28 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER 1214 AND SRM 57-10-00 FIG 28 VOL 1.

Part: BULKHEAD — CRACKED (BS 580) · airframe 73,656 hrs · 23,743 cycles

NLG WHEEL WELL FOUND 2 CRACKS 4" LONG ON LT INTERNAL BULKHEAD AT STA 580 Z-43.5. TRIMMED OUT CRACK FABRICATED FILLER, 2 DOUBLERS AND INSTALLED (INTERNAL NLG) IAW SRM 53-30-00 FIG 6. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I010386/N00386-5, N00386-7, N00386-3 AND SRM 53-30-00 FIG 6 VOL 1.

Part: REPAIR — NONE (CARGO DOOR) · airframe 73,656 hrs · 23,743 cycles

AFT CARGO DOOR AFT PAN HAS AN EXTERNAL DOUBLER AND ANGLE REPAIR DIM 7 X 1.5 INCH. PERFORMED INSPECTION ON DOUBLER AND ANGLE REPAIR IAW SRM 52-10-00 FIG 17 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (A/C DOOR) · airframe 73,656 hrs · 23,743 cycles

FOUND AN EXTERNAL DOUBLER REPAIR ON THE UPPER LIP OF THE NR 2 PACK AIR CONDITIONING DOOR LT SIDE OF FUSELAGE DIM 7 X 3 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-00-01 FIG 4 SHT 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (BS 1159) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY FOUND SPLICE REPAIR INSTALLED AT FRAME STATION 1159 LT SIDE CORRECTIVE ACTION PERFORMED INSPECTION ON SPLICE REPAIR IAW ESO NR 7346-1275302JP FOUND IAW CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

UPPER LIP AIR CONDITIONING DOOR RT SIDE PACK NR 3 HAS AN EXTERNAL DOUBLER REPAIR DIM 31 INCHES BY 2 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 2 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

RT HORIZONTAL STABILIZER UPPER SURFACE ON SKIN FOUND AN EXTERNAL DOUBLER. REPAIR BETWEEN STA XE 67.333 AND XE 87.167 DIM. 15 INCHES X 11 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SB 55-16 FIG 19 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

NR 1 PYLON FOUND TWO BLEND OUTS ON THE OUTBOARD SKIN AREA BELOW THE TRUST REVERSER HINGE STA YN250. PERFORMED INSPECTION ON PREVIOUS REPAIR IAW 1275402-ESO7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

CENTER CARGO DOOR LOWER AFT CORNER HAS AN EXTERNAL DOUBLER REPAIR DIM 7 INCHES BY 4 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 17 VOL 1 . FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSLEAGE) · airframe 73,656 hrs · 23,743 cycles

LT HORIZONTAL STABILIZER LOWER SURFACE TRAILING EDGE PANEL FOUND AN EXTERNAL DOUBLER REPAIR AT STA XE 169.333 DIM. 8.5 INCHES BY 5.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-00-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (CARGO DOOR) · airframe 73,656 hrs · 23,743 cycles

DISCREPANCY CENTER CARGO DOOR FWD LWR CORNER HAS AN EXTERNAL REPAIR DOUBLER INSTALLED CORRECTIVE ACTION PERFORMED INSPECTION ON EXTERNAL REPAIR DOUBLER IAW 1255201JP ESO 7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (VERTICAL STAB) · airframe 73,656 hrs · 23,743 cycles

VERTICAL STABILIZER LT SIDE FOUND A FITTING AND DOUBLER REPAIR ON NR 4 BANJO FITTING. PERFORMED INSPECTION FITTING AND DOUBLER REPAIR IAW ESO7349-ACF1275501. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSLEAGE) · airframe 73,656 hrs · 23,743 cycles

FOUND RT SIDE HORIZONTAL STABILIZER IB ELEVATOR UPPER SURFACE ON SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XE 216.885 DIM. 8 INCHES BY 8.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X-46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

RAM AIR DUCT CUTOUT HAS AN EXTERNAL TRIPLER DOUBLER ON LOWER FWD CORNER BETWEEN STA 557 TO 572 AND LONG 46 TO 48 LT SIDE DIM 15 X 15 INCHES, 12 X 13 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

RAM AIR DUCT CUTOUT ON SKIN HAS AN EXTERNAL TRIPLE DOUBLER REPAIR ON THE UPPER AFT CORNER BETWEEN STA 576-590 LONG 44 TO 46 DIM 14 X 12.5 INCHES, 10 X 11.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FWD CARGO COMPT LOWER FRAME AT STA 879 HAS AN ANGLE REPAIR BETWEEN LONG 49 TO LONG 52 DIM 15 X 2 INCHES. PERFORMED INSPECTION ON ANGLE REPAIR IAW SRM 53-30-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (RT WING) · airframe 73,656 hrs · 23,743 cycles

RT WING OUTBOARD FLAP LOWER SURFACE HAS A DOUBLER REPAIR ON TWO RIBS AT T/E PANEL BETWEEN STA XOF 580 AND XOF 588 DIM 13" BY 8". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (NR 1 SLAT) · airframe 73,656 hrs · 23,743 cycles

FOUND LEFT WING NR 1 SLAT HAS AN EXTERNAL DOUBLER REPAIR AT THE LOWER AFT EDGE OF THE OUTER SKIN DIM. 8.5" BY 5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 84 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (BS 1205) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1205 LONG 52 DIM 4" BY 4". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (BS 1256) · airframe 73,656 hrs · 23,743 cycles

MAIN CABIN R-3 FWD DOOR JAMB HAS AN EXTERNAL DOUBLER REPAIR BOTTOM PART STA 1256 DIM 7" BY 9.75". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X 46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (RT WING SLAT) · airframe 73,656 hrs · 23,743 cycles

RIGHT WING SLAT NR 6 STA XOS 860 HEATED AREA HAS AN EXTERNAL DOUBLER REPAIR DIM 10 X 6 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 12 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE FWD PRESSURE BULKHEAD PANEL HAS A WEB REPAIR ON RIGHT SIDE AT STA 1156 BETWEEN 39 TO 42 DIM 12 X 18 INCHES, 20 X 28 INCHES, 20 X 28 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (R3 DOOR) · airframe 73,656 hrs · 23,743 cycles

FOUND MAIN CABIN CTR FUSELAGE R-3 DOOR AFT JAMB HAS AN EXTERNAL DOUBLER BOTTOM PART DIM 11" BY 12" STA 1311. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

MAIN CABIN CTR FUSELAGE L3 DOOR JAMB AFT HAS AN EXTERNAL DOUBLER REPAIR STA 1311 DIM 11" BY 12" BOTTOM PART. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

PYLON NR 1 HAS AN EXTERNAL DOUBLER REPAIR ON THE UPPER SPAR WEB AFT SECTION BETWEEN STA YN 410 AND YN 417 DIM 7" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 54-20-00 FIG 34 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.

Part: REPAIR — NONE (FUSELAGE) · airframe 73,656 hrs · 23,743 cycles

LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1211 LONG 52 DIM 5 X 4.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.

Part: REPAIR — UNKNOWN (L1 DOOR) · airframe 73,656 hrs · 23,743 cycles

L-1 DOOR UPPER FWD CORNER HAS AN EXTERNAL DOUBLER REPAIR DIM 12" X 6.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 12A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.