N935UP

Part: WEB — CRACKED (L/E SLAT) · airframe 53,246 hrs · 37,511 cycles

CRACK FOUND ON I/B WEB OF REMOVABLE LEADING EDGE AT BS 740 RT. DAMAGED AREA REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: CARRIAGE — WORN (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C WEAR IN NR 7 FLAP CARRIAGE SIDE ROLLER ASSY BRACKETS. FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: SKIN — CORRODED (BS 1000) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C HTD B-NUT HAS FRETTED SKIN IN HYD BAY AT BS 1000 AT STR 23 LEFT. MEASURED AND EVALUATED FRETTED SKIN AND FOUND OUT OF LIMITS IAW SRM 53-30-01. PREVIOUS REPAIR REMOVED IAW SRM 51-30-02. DAMAGE REPAIRED IAW SRM 53-30-3.

Part: LINK — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C NR 5 FLAP CARRIAGE BEARING LINK BEARING A DRIFT AND BUSHING CORRODED. CORROSION FOUND ON INNER SURFACE OF BEARING LINK. BEARING LINK ASSY AND BUSHING REPLACED IAW MM 27-51-03.

Part: CARRIAGE — WORN (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C NR 8 FLAP CARRIAGE AFT SIDE ROLLERS FWD ATTACH HOLES WORN. FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C NR 4 FLAP CARRIAGE FWD LOWER FLANGE CORRODED. FLAP CARRIAGE REPLACED IAW MM 27-51-03.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C NR 5 FLAP CARRIAGE HAS CORROSION ON LWR FWD FLANGE UPPER AND LOWER SURFACES CARRIAGE REPLACED IAW MM 27-51-03.

Part: BEAM — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C SIDE LOAD BEAM AT RIGHT BS 740 CORRODED. ANGLE FABRICATED IAW DRWG 65-15940. INSTALLED SIDE LOAD BEAM ANGLE IAW B727-5310-7477.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C SEAT TRACK AT RBL 40 2 BETWEEN BS 740-760 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 51-30-02. REPLACED SEAT TRACK IAW SRM 51-30-02.

Part: FLOOR SUPPORT — CRACKED (BS 850 LBL 24.75) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI FLOOR SUPPORT CRACKED AT BS 850 RBL 24.75. FLOOR SUPPORT REMOVED IAW SRM 51-30-02. NEW FLOOR SUPPORT FABRICATED I AW SRM 51-40-03. FLOOR SUPPORT PROTECTED IAW SRM 51-10-02. FLOOR SUP PORT PAINTED AND INSTALLED IAW SRM 51-40-03, 51-30-02 AND MM 51-20-90.

Part: CARRIAGE — CORRODED (TE FLAPS) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C, 3 SEQUENCE CARRIAGE HAS CORROSION ON AFT UPPER LUGS SEQUENCE CARRIAGE REPLACED IAW MM 27-51-04.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE: C AND SI CORROSION ON INTERCOSTAL SUPPORT CONTROL CABIN FLOOR, BL 0, FS 277 TO 29 4.5. CORROSION CLEANED AND SUPPORT FOUND TO BE OUTSIDE LIMITS. NEW SUPPORT FABRICATED IAW BOEING DRG 65-17593. NEW SUPPORT INSTALLED IAW SRM 51-30-2 WITH REFERENCE DRG 65-17593.

Part: FLOORBEAM — CORRODED (BS 560 LBL 37) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI CORROSION ON UPPER SURFACE OF FLOORBEAM UPPER FLANGE REPAIR AT BS 560 LBL 37. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS. REPA IR STRAP REMOVED, NEW REPAIR STRAP FABRICATED IAW SRM 51-20-1. REPAIR STRAP REPROTECTED AND PAINTED IAW SRM 51-10-2. STRAP INSTALLED IAW S RM 51-30-2

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION IN NR 6 FLAP TRACK HOLES G AND F. BUSHINGS FABRICATED IAW AAAE-EO-2006-042-08. HEAT TREATED IAW 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION IN \1 FLAP TRACK HOLES E, D AND C. BUSHING FABRICATED IAW AAAE EO 2006-042-005. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.

Part: STRUCTURE — CORRODED (BS 850) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION AT BS 850 RT UNDER STR 18A. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06. FASTENER REINSTALLED IAW SRM 51-30-02.

Part: SEAT TRACK — CRACKED (BS 397 RBL 23) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND IS CRACKED ON SEAT TRACK TOP BS 397 RBL 23 NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90, SRM 5 1-10-2 AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 690-720 RBL 65. CORROSION OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 592 RBL 45) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 5 92 RBL 45. NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-20-90 AND SRM 51-30-2, 53-10-5, AND 51-10-2.

Part: WEB — CRACKED (RT WING) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C SI RT WING STRUCTURE INNER WEB CRACKED AT NR 8 SLAT ACTUATOR CUTOUT, REPAIR OR REPLACE. REPAIRED IAW SRM 51-40-02 FIG 1.

Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION ON NR 7 FLAP TRACK ATTACH PAD HOLE E. BUSHING FABRICATED IAW EO 2006-042-0009. HEAT TREATMENT REFERENCE 06-4 2-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.

Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C NR 8 FLAP TRACK ATTACH PAD HAS CORROSION IN HOLES E, D AND C. BUSHINGS FABRICATED FOR HOLES IAW AAAE EO 2006-042-10. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION ON FLOOR STRUCTURE STIFFENER AT RT SIDE AT BS 230 RBL 36. STIFFENER REPLACED IAW SRM 51-30-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C SMALL NICK ON FUSE SKIN, DAMAGE LOCATED AT BASE OF C, D WINDOW POST. FASTENERS REMOVED FROM REPAIR AREA AND DAMAGE BLENDED OUT IAW SRM 53-30 -03. REPAIR DOUBLER INSTALLED IAW SRM 53-30-03.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 312 - 328 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-6. INTERCOSTAL REMOVED AND REPLACED IAW MM 51-20-90.

Part: INTERCOSTAL — CORRODED (BS 303) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI CORROSION AROUND ANCHOR NUT HOLE UNDER COCKPIT DOOR SILL BS 303. REMOVED INTERCOSTAL UNDER COCKPIT DOOR IAW SRM 51-30-02. FABRICATED I NTERCOSTAL IAW SRM 51-20-1. INTERCOSTAL REPROTECTED IAW SRM 51-10-2. INTERCOSTAL PAINTED IAW MM 54-20-90. INSTALLED INTERCOSTAL IAW SRM 5 1-30-2.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 328 AND 334 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. INTERCOSTAL REMOVED AND NEW INTERCOSTAL INSTALLED IAW SRM 51-30-2 AND DRG 65-21673.

Part: RIB — CRACKED (L/E SLAT) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C SUSPECT CRACK ON NR 5 SLAT 3RD RIB O/B OF IB TRACK AT AFT UPPER CORNER. SLAT REPLACED.

Part: RIB — CRACKED (L/E SLAT) · airframe 53,246 hrs · 37,511 cycles

SUSPECT CRACK ON NR 6 SLAT ON 4TH RIB OB OF ACTUATOR AT UPPER AFT CORNER RIB REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 590-630 LBL45) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI CORROSION ON SEAT TRACK TOP CHORD BS 590-630 LBL 45.5 NEW SEAT TRACK FABRICATED, PAINT AND INSTALLED IAW MM 51-20-90, SRM 51- 30-2, 53-10-5

Part: RIB — CRACKED (L/E SLAT) · airframe 53,246 hrs · 37,511 cycles

SUSPECT CRACK ON NR 6 SLAT ON 1ST RIB O/B OF I/B TRACK ALONG AFT FLANGE. RIB REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-30-02.

Part: STRUCTURE — CORRODED (WINGTIP TE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C SURFACE CORROSION AT BOTH I/B STATIC DISCHARGERS LEFT WING TIP T/E. CORROSION REMOVED IAW SRM 51-10-01 AND FASTENERS REMOVED IAW SRM 51-3 0-02. AREA O/B FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01. DAMAGED AREA REPAIRED IAW SRM 57-20-05. AREA REPROTECTED IAW MM 51-20-91.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 950 RBL 51-56. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06 AND 53-1001. FLOORBEAM TOP CHORD REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 418-427) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C CORROSION ON SEAT TRACK TOP BS 418-427 RBL 45.5. SEAT TRACK REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.

Part: FITTING — CRACKED (BS 740) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C BS 740 TERMINAL FITTING REQUIRES REPLACING. FITTING REPLACED IAW EO B727-5310-7477 AND DRWG 65C13724.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE: C AND SI CRACKS DETECTED ON BS 740 STR 18R - STR 24R. ON INVESTIGATION CRACKS FOUND TO BE OUTSIDE LIMITS IAW SB 727-53-0062. REFERENCE NRC 100347 FOR BS 740 FITTING REPLACEMENT.

Part: FLOORBEAM — CORRODED (BS 328 LBL 27-31) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 328 LBL 27-31 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. NEW FLOOBEAM TOP CHORD FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90 AND SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 420 RBL 52-55. SPLICE ANGLE AND FILLER INSTALLED IAW SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 344 LBL 16-23) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 344 LBL 16-23 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. FLOORBEAM TOMP P CHORD FABRICATED, PAINTED AND INSTALLED IAW SRM 53-10-08 AND MM 51-21- 90.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C CORROSION ON SEAT TRACK TOP CHORD AT BS 950-962 RBL 62.5. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.

Part: WEDGE — DELAMINATED (RT AILERON) · airframe 53,246 hrs · 37,511 cycles

RT O/B AILERON HAS DELAM ON TRAILING EDGE WEDGE. AILERON BEYOND REPAIRABLE LIMITS, AILERON REPLACED IAW MM 27-10-14.

Part: PANEL — DELAMINATED (LT WING) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C LT WING UPPER SURFACE PANEL FWD OF NR 5 AND 6 SPOILERS DELAM AT PREVIOUS REPAIR. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-40-20. PANEL REPLACED IAW SRM 51-30-02.

Part: CHANNEL — CORRODED (APU EXHAUST) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE:C AFT SUPPORT CHANNEL FOR APU EXHAUST ON THE LOWER SIDE UPPER WING PANEL IS CORRODED. CHANNEL REPLACED IAW SRM 51-20-01.

Part: SEAT TRACK — CORRODED (BS 481) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C CORROSION ON SEAT TRACK, TOP CHORD BS 481 RBL 45.5 CORROSION FOUND OUTSIDE LIMITS IAW SRM 53-10-1. SEAT TRACK AND CONNECT OR REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.

Part: FLAP TRACK — CORRODED (NR 5 FLAP) · airframe 53,246 hrs · 37,511 cycles

INSPECTION TYPE-C CORROSION IN NR 5 FLAP TRACK HOLE G. CORROSION REMOVED IAW OHM 57-40-01. MPI CARRIED OUT IAW BSOPM 20-20-0 1. BUSHING FABRICATED IAW EO 20065-042-007. STYLUS CAD PLATING CARRIED OUT IAW SOPM 20-42-10. INSTALLED BUSHING IAW SOPM 20-50-03.

Part: ANGLE — CRACKED (LT WING) · airframe 52,789 hrs · 37,091 cycles

LT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,789 hrs · 37,091 cycles

CORROSION ON FLOORBEAM AT BS 680 LBL 56 FOUND ON REMOVAL OF FLOOR PANELS FOR DOOR SILL INSPECTION. REPAIR CARRIED OUT IAW SRM 51-10-2, 53-10-8, 51-20-4 AND AAAE EO 2005-01 0-004 UPS ENGINEERING FILE NR 727-53-20183.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,789 hrs · 37,091 cycles

AFT AIRSTAIRS ANGLE CRACKED AT FORWARD SIDE OF BS 1203 FRAME LT AT S13L. STOP DRILLED CRACK IAW 51-10-1. HFEC CARRIED OUT IAW NDTM PT6 51-00 -00, CRACK CONTAINED BY STOP DRILLED HOLE. REFER TO UPS FILE NUMBER 727-53-20182.

Part: CASTING — CRACKED (NR 8 SPOILER) · airframe 52,789 hrs · 37,091 cycles

NR 8 SPOILER I/B END HINGE CASTING IS CRACKED AT FASTENER HOLE. HINGE CASTING REPLACED IAW SRM 51-30-2.

Part: SKIN — CRACKED (LT WING DOOR) · airframe 52,789 hrs · 37,091 cycles

SUSPECT CRACK ON LT WING DOOR, ON INNER SKIN AT UPPER FWD END. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SUPPORT BRACKET — CORRODED (NLG DOOR) · airframe 52,789 hrs · 37,091 cycles

NLG DOOR FWD WALL SUPPORT BRACKET CORRODED. SUPPORT REPLACED IAW SRM 51-10-1, SRM 51-30-2 AND 53-10-00.

Part: SPOILER PANEL — DELAMINATED (NR 3 SPOILER) · airframe 52,789 hrs · 37,091 cycles

NR 3 SPOILER HAS 2 AREAS OF DELAMINATION, 1 ON THE UPPER SURFACE AND ONE ON THE LOWER SURFACE. SPOILER PANEL REPLACED IAW MM 27-61-01.

Part: SPOILER PANEL — DELAMINATED (NR 11 SPOILER) · airframe 52,789 hrs · 37,091 cycles

SPOILER PANEL NR 11 HAS AREA OF DELAMINATION ON UPPER SURFACE. NR 11 SPOILER PANEL REMOVED IAW MM 27-61-01. PANEL REPAIRED IAW SRM 51-40-20. SPOILER PANEL REINSTALLED IAW 27-61-01.

Part: SPOILER PANEL — DELAMINATED (NR 13 SPOILER) · airframe 52,789 hrs · 37,091 cycles

NR 13 SPOILER PANEL HAS AREA OF DELAM AT SITE OF PREVIOUS REPAIR UNDER SURFACE. SPOILER PANEL REMOVED IAW MM 27-61-01. SPOILER PANEL REPAIRED IAW SRM 51-40-20. SPOILER PANEL REINSTALLED IAW 27-61-01.

Part: SPOILER PANEL — DELAMINATED (NR 10 SPOILER) · airframe 52,789 hrs · 37,091 cycles

NR 10 SPOILER PANEL HAS AREAS OF DELAMINATION ON UPPER SURFACE. SPOILER REMOVED IAW MM 27-62-01. SPOILER PANEL REPAIRED IAW SRM 51-40-2. SPOILER PANEL REINSTALLED IAW MM 27-62-01.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 52,789 hrs · 37,091 cycles

SLIGHT DELAMINATION ON RT ELEVATOR TAB. DELAMINATED OUT OF LIMITS IAW 51-20-1. ELEVATOR TAB REMOVED AND REPAIRED IAW SRM 51-40-20 REPAIR NR 5. TAB BALANCED AND WEIGHED IAW SRM 51-80 -09. TAB REINSTALLED IAW MM 27-30-11.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 52,298 hrs · 36,656 cycles

INSPECTION TYPE: C, 3 CRACKS AT ADJACENT RIVETS ABOVE DECAL AT LT AFT PRESS PANEL CUTOUT. AREA CUTOUT I.A.W. SRM 51-40-2 FIG.1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,298 hrs · 36,656 cycles

INSPECTION TYPE: C, CORROSION BETWEEN ANGLE SUPPORT AND WWW TORQUE BOX AT RBL 14.5 APPRO X AND BS 294 APPROX ON INVESTIGATION ANGLES FOUND CORRODED. ANGLES REMOVED IAW SRM 51-3 0-2. ANGLES FABRICATED IAW DRAWING 65-18415 AND 65-18417. ANGLES INS TALLED IAW SRM 51-30-2

Part: RIB — CRACKED (NR 6 SLAT) · airframe 52,298 hrs · 36,656 cycles

INSPECTION TYPE:C NR 6 SLAT IB TRACK IB FLAP RIB CRACK AT FWD CORNER NR 6 FLAT IB TRACK REMOVED IAW OHM 57-51-51 REPAIR CARRIED OUT IAW SRM 51-40-3. NR 6 SLAT IB TRACK INSTALLED IAW OHM 57-51-51. FUNCTION TEST CARRIED OUT IAW MM 27-81-00. OPS. OK

Part: RIB — CRACKED (NR 6 SLAT) · airframe 52,298 hrs · 36,656 cycles

INSPECTION TYPE: C, NR 6 SLAT RIB 2ND FROM O/B END CRACKED AT AFT END. REPAIR CARRIED OUT IAW SRM 57-50-03 FIG 9.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,298 hrs · 36,656 cycles

INSPECTION TYPE: C, ON INSPECTION OF CONTROL CABLES BS 740 - 950 CRACK FOUND ON FLOORBEAM WEB BS 520 LBL 50. REPAIR CARRIED OUT IAW SRM 51-40-2

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES WITH NEW BATTERIES.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP-L1 DOOR. REMOVED AND REPLACED BATTERY.

Part: HINGE PIN — CORRODED (HORIZ STAB)

INSPECTION TYPE:IN FOUND SURFACE CORROSION ON BOTH LT AND RT HORIZONTAL STAB HINGE PIN NUTS. PER EO B7275105166 APPX D MUST BE COMPLIED WITH PER EO B727-5510-1566-B, CORROSION SHOULD ONLY BE NOTED ON PIN THREADED END AND REMOVED SURFACE CORROSION WITH MECHANICAL NON ABRASIVE INSTRUMENT. OK FOR SERVICE.

Part: PIN — CORRODED (RT WING)

INSPECTION TYPE:C, EVIDENCE OF CORROSION AT RIGHT WING FRONT SPAR BOTTLE PIN HEAD. REPLACED RIGHT WING FRONT SPAR BOTTLE PIN IN ACCORDANCE WITH MM 57-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C, MAIN CABIN SEAT TRACK, CORRODED FROM BS 344 TO BS 360 AND LBL 22.5. REPLACED SECTION OF SEAT TRACKING ACCORDANCE WITH SRM 53-10-5. MATERIAL USED, P/N BAC1520-1432, 16 INCHES LONG.

Part: SEAT TRACK — GOUGED (FUSELAGE)

INSPECTION TYPE:C, CABIN SEAT TRACK LBL 60, STA 499/501 IS NICKED AND GOUGED. REPLACED CABIN SEAT TRACK FROM STA 499 TO STA 650, LBL 60 IN ACCORDANCE WITH SRM 53-10-5 FIG 3. MATERIAL USED, P/N BACK 1520-1433. ALSO SEE NRC 258775 AND 258778.

Part: SPAR — CRACKED (LT WING)

INSPECTION TYPE:C, CRACK INDICATION AT LEFT WING UPPER CHORD OF THE REAR SPAR UPPER ROW FASTENER WS 568. INSTALLED REPAIR IN ACCORDANCE WITH SRM 57-10-6 FIG 2. MATERIAL USED (1) ANGLE, 7075--T6,0.080 INCH, 20.5 X 2 INCHES AND (1) ANGLE 7075-T6, 0.080 INCH, 15.5 X 2 INCHES.

Part: SEAT TRACK — CRACKED (FUSELAGE)

INSPECTION TYPE:C, MAIN CARGO DECK SEAT TRACK GOUGED AND CRACKED AT RBL 45 BETWEEN BS 480 AND 540. REPLACED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5 FIG 7. MATERIAL USED P/N BAC1520-1434, 60 INCHES.

Part: WEB — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL RIGHT SIDE HAS VERTICAL WEB CRACKED ABOVE RIGHT FORWARD NOSE LANDING GEAR DOOR BS 277. CUT OUT DAMAGED AREA AND INSTALLED WEB REPAIR IN ACCORDANCE WITH SR 51-40-2 FIG 1. MATERIAL USED 024-T3, 0.050 INCH, 5 X 12 INCHES.

Part: SPAR — CORRODED (WS 525)

INSPECTION TYPE:C, CORROSION (C57-562-02.00E-01) AT LT WING STA 525 UPPER SPAR CHORD. REMOVED AND REPLACED SPAR (UPPER CHORD) IAW BFG ER 99-5890 (UPS FILE NR 727-57-2118).

Part: STIFFNER — CRACKED (WING)

INSPECTION TYPE:C RW VERTICAL STIFFENER ON FWD WEB JUST O/B OF 740 BOTTLE PIN IS CRACKED AT BOTTOM FASTENER. REMOVED STIFFENER, FABRICATED A NEW ONE, ALODINED AND PRIMED NEW STIFFENER. INSTALLED STIFFENER, ALL WORK ACCOMPLISHED IAW SRM 51-30-05, BOEING DRAWING NR 69-20117-1, SRM 51-30-2.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE:C, RT VERTICAL MID SPAR FRETTING WHERE PANEL 9602 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WITH SPLICE REPAIR IAW ERN 99-5888.

Part: CHORD — CORRODED (BS 303)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NLG MID CHORD BS 303 BS 303 WL 172 RBL 25. CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPLACED NOSE CHORD IAW SRM 51-30-2, 51-30-5 MM 20-20-01 AND SWPM 20-10-11.

Part: STIFFENER — CORRODED (BS 319)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON STIFFENER BS 319, WL 173 TO 187, RBL 14 HORIZONTAL WALKWAY AREA. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-02.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:C WHILE WORKING CUSTOMER CARD #934321 FOUND CRACKED RIB IN NR 4 SLAT, 3RD RIB I/B OF O/B SLAT TRACK WHERE RIB ATTACHES TO LOWER AFT CHORD. REMOVED CRACKED RIB AND INSTALLED NEW RIB PER SRM 51-30-2.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:C, CRACKED RIB IN NR 4 SLAT, 2ND RIB I/B OF O/B SLAT TRACK WHERE RIB ATTACHES TO LOWER AFT CHORD. REMOVED AND REPLACED RIB PER SRM 51-30-7.

Part: FLOOR — CORRODED (BS 342-351)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON DOG HOUSE FLOOR IN A FEW AREAS BS 342 TO 351, WL 169, RBL 14 TO 16. REMOVED CORRODED FLOOR BS 342 TO 351. FABRICATED NEW FLOOR AND INSTALLED IAW SRM 51-30-05 AND DRG NR 65-18415.

Part: SPAR CHORD — CORRODED (WS 346-642)

INSPECTION TYPE:C, CORROSION C57-562-02-1B, L/W FWD UPPER SPAR CHORD ON HORIZONTAL FLANGE AT NR 4 SLAT ACTUATOR O/B MOUNT ANGLE. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED SECTION FROM FSS 346-FSS 642 FRONT SPAR TO BE REPLACED ON NRC 934257.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD 933983 INT 71, FOUND CORROSION ON BS 328 FLOORBEAM TOP FLANGE WL 208 AT LBL 7 AND LBL 25. REMOVED DAMAGED AREA ON FLOORBEAM. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-8, 51-10-2, 53-10-8.

Part: MOUNTING LUG — CORRODED (NR 6 LE FLAP)

INSPECTION TYPE:C, (CORROSION C57-562-01.00-02) CORROSION ON NR 6 K-FLAP INBOARD MOUNT LUG UPPER BOLT. REMOVED NR 6 K-FLAP PER MM 27-81-01. NR 6 K-FLAP CORROSION OUT OF LIMITS PER SRM ADDENDUM EO B727-5750-5542. REPLACED K-FLAP PER MM 27-81-01.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD NUMBER 933976 INT 64, FOUND CORROSION ON FLOORBEAM BS 312 LBL 3 WL 208. CORROSION OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED ALL WORK DONE IAW SRM 51-10-6, 53-10-1, 51-30-5, 51-30-6 AND SRM 51-10-2.

Part: SPAR CHORD — CORRODED (WS 510)

INSPECTION TYPE:C C57-562-02-1B, EXFOLIATION CORROSION ON LW FWD UPPER SPAR CHORD AT WS 510.0 (MARKED), NR 3 SLAT AT TAI TELESCOPING DUCT. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED DAMAGE CHORD FROM FSS 346 TO FSS 642. REPLACEMENT CHORD WILL BE INSTALLED ON NRC 934257.

Part: STIFFENER — CORRODED (BS 345)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON STIFFENER BS 345 WL 175 RBL 14, HORIZONTAL WALK WAY AREA. CORROSION OUT OF LIMITS SRM 53-10-1. REMOVED AND INSTALLED NEW STIFFENER PER SRM 51-30-2.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE:C, LT VERTICAL MID SPAR FRETTING WHERE PANEL 9601 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WITH SPLICE REPAIR IAW ERN 99-5888.

Part: WEB — CORRODED (BS 309)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON BONDED DOUBLER ON VERTICAL WEB OF HORIZONTAL WALKWAY BS 309. REMOVED DAMAGED BONDED DOUBLER, FABRICATED NEW BONDED DOUBLER AND INSTALLED IAW SRM 51-10-3, 51-10-6, 51-30-2.

Part: BRACKET — CORRODED (RT WING SPAR)

INSPECTION TYPE:C, ANGLE BRACKET CORRODED ON R/W UPPER AFT SPAR CHORD AT NR 14 SPOILER I/B SIDE HINGE. REMOVED SPOILER I/B ANGLE SUPPORT BRACKET. FABRICATED NEW SUPPORT ANGLE PER SRM 51-20-1 AND 51-30-05. INSTALLED NEW BRACKET PER SRM 51-30-02. LEAK CHECKED FUEL TANK AND FUNCTIONAL TESTED NR 14 SPOILER PER MM 27-61-00.

Part: BRACKET — CRACKED (FUSELAGE)

INSPECTION TYPE-N/A, OPENING TO RIGHT OF TAIL SKID FOWARD CROSS MEMBER CRACKED JUST BELOW MANUAL PUMP. REPAIRED BRACKET PER SRM 51-10-02.

Part: HINGE — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE:C, NR 4 K-FLAP OUTBRD HINGE LUG CORRODED AROUND UPPER AND LOWER FASTENER HOLES. REPLACED COMPLETE K-FLAP ASSY PER MM 27-81-01.

Part: FITTING — CORRODED (NR 1 SPOILER)

INSPECTION TYPE:C CORROSION (C57-581-03.00-01) ON NR 1 SPOILER ACTUATOR SUPPORT FITTING. REPLACED SUPPORT FITTING AND REINSTALLED ASSOCIATED PARTS PER MM 27-61-01 AND 27-61-81.

Part: FITTING — CORRODED (NR 4 SPOILER)

INSPECTION TYPE:C CORROSION (C57-581-03.00-01) ON NR 4 SPOILER ACTUATOR SUPPORT FITTING. REPLACED SUPPORT FITTING AND REINSTALLED SPOILER AND ACTUATOR AND ASSOCIATED PARTS PER MM 27-61-01 AND 27-61-81.

Part: SPAR — CORRODED (WS 438/446)

INSPECTION TYPE:C R/W FRONT SPAR LOWER CHORD IS CORRODED AT FSS 438 AND FS 446. REMOVED CORROSION OUT OF LIMITS AND REPAIRED IAW ER NR 98-2449.

Part: SPAR CHORD — CORROSION (RT WING)

INSPECTION TYPE:C R/W UPPER F/SPAR CHORD SHOW SIGNS OF CORROSION AT FSS 398.0, 497.0, 513.5, 521.5, 730.02, 737.0. REMOVE CORROSION FOUND OUT OF LIMITS AND REPLACE SPAR CHORD IAW 98-2421.

Part: CHANNEL — CORRODED (BS 322-334)

INSPECTION TYPE:C CORROSION (C53-224-06.00-01) AROUND NUT PLATES ON U-CHANNEL JUST OUTBOARD OF MOP SILL BETWEEN BS 322-334, WL 209, LBL 63. REMOVED AND REPLACED U-CHANNEL PER SRM 51-30-2.

Part: FRAME — CORRODED (BS 275)

INSPECTION TYPE:C CORROSION ON WEB IN FRONT OF DRAG BRACE SHELF BS 275 WL 149-152 RBL 14 TO LBL 14. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-03.

Part: FRAME — CORRODED (EMER EXIT DOOR)

INSPECTION TYPE:C CORROSION LT AFT OVERWING EXIT BOTTOM OF DOOR UNDER PRESSURE SEAL ON FRAME REMOVED AND REPLACED LOWER FORWARD FRAME SECTION IAW SRM 51-30-02, 51-10-1, 53-10-1.

Part: DOOR SEAL — CORRODED (GALLEY DOOR)

INSPECTION TYPE:C CORROSION ON MID GALLEY DOOR SEAL DEPRESSOR, UPPER FWD AND AFT, VERTICAL SIDE UPPER AND LOWER. REMOVED AND REPLACED 4 (EA) SEAL DEPRESSORS AT MID GALLEY DOOR CUTOUT STRUCTURE.

Part: BATTERY — DISCHARGED (CABIN)

CABIN EMERGENCY LIGHT REMOVED FOR BATTERY CHANGE. CHANGED BATTERIES S106 REINSTALLED EMERG LIGHT, OPS CKS OK.

Part: BATTERY — DISCHARGED (COCKPIT)

DUE TO PREVIOUS HISTORY, REPLACE CONTROL CABIN EMERG EXIT LIGHT BATTERY. REPLACED EMERG EXIT LIGHT BATTERY, OPS CKS OK.

Part: LIGHT — LOOSE (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT EMER EXIT LIGHT CAME ON SLOWLY THEN FADED OUT. BATTERY CK GOOD. RESEATED LIGHT ASSY, LIGHT CK GOOD.

Part: BEARING — DEFECTIVE (RT TE FLAP)

INSPECTION TYPE-N/A, RAISING FLAPS AFTER TAKEOFF, INBOARD FLAPS INDICATED STUCK AT 2 DEGREES. FOLLOWED AOM PROCEDURES, PERFORMED SPLIT/ASYMMETRY FLAP PROCEDURES AND LANDED AT DFW. REPLACED RIGHT INBOARD FLAP JACKSCREW FAIRING FORWARD BEARING AND HOUSING. PERFORMED ADJUSTMENT/TEST OK.

Part: WINDOW GLUE — FUMES (COCKPIT)

INSPECTION TYPE-N/A, NOXIOUS FUMES FROM GLUE USED TO FIX CAPTS WINDOW FORCED CREW TO USE O2 MASKS DURING FLIGHT. REGLUED TRIM.

Part: LIGHTS — INOPERATIVE (COCKPIT)

BOTH EMERGENCY LIGHTS DO NOT ILLUMINATE WITH SWITCH IN ON POSITION. RELAMPED BOTH EMERGENCY LIGHTS. OPS CHKS GOOD.

Part: SEAT TRACK — CORROSION (BS 558-585)

INSPECTION TYPE-C, THE FWD CARGO AT, RT TRACK BS 558 TO 585 HAS INTERGRANULAR CORROSION AND IS SEVERLY WORN. REMOVED SEAT TRACK AT RT SIDE, FWD CARGO PIT FROM STA 550 TO 680 AND INSTALLED TRACK PER SRM 51-30-2.

Part: FRAME — CRACKED (BS 1130)

INSPECTION TYPE-C, BS 1130 FRAME UPPER FLANGE ABOVE STR 29R IS DENTED AND CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3 AND SRM 51-10-6.

Part: SKIN — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE: C. LT WING NR 4 SLAT SKIN TOP SIDE AT OTBD HOOK HAS SEVERAL CRACKS AROUND FASTENERS. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED PLATE PER SRM 57-50-3.

Part: SUPPORT — CORRODED (BS 304-344)

INSPECTION TYPE: C. LAVATORY FLOOR - FLOOR SUPPORT HAT SECTION UNDER LAV DOOR HAS CORROSION FROM STA 304-344. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART I.A.W. DRAWING 65-26173 AND SRM 51-30-2.

Part: FRAME — CRACKED (BS 1203)

INSPECTION TYPE: C. LT WEB CRACKED, FRAME 1203, LBL 40 AT WL 220. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 51-40-2 AND INSTALLED REPAIR PER SRM 51-30-2.

Part: LIGHT — INOPERATIVE (MAIN ENTRY DR)

MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT INOP ABOVE ENTRY DOOR. ALL BATTERIES IN STOCK FAILED TO WORK. ROBBED PART OFF A/C 926 AND INSTALLED ON A/C 935. OPS CHECK GOOD.

Part: ANGLE — CORRODED (BS 1342)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND TORQUE BOX I/B CHORD AT STA 1342, LBL 13, WL 259 CORRODED ANGLE. REPAIRED IAW E.O. B727-5530-1237, SRM 51-10-6, 51-10-2.

Part: CHORD — CORRODED (HORIZ STAB)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.

Part: ANGLE — CRACKED (FS 1362-1380)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND LT UPPER TORQUE BOX BETWEEN F.S. 1362 - 1380, WL 269 ON HORIZONTAL ANGLE CRACKED. REPAIRED IAW SRM 54-10-2, 51-30-2.

Part: CHORD — CORRODED (HORIZ STAB)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.

Part: CHORD — CORRODED (HORIZ STAB)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1342)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND TORQUE BOX I/B CHORD ANGLE AT STA 1342, RBL 13, WL 259 CORRODED. REPAIRED IAW E.O. B727-5530-1237, SRM 51-10-2, 51-10-6.

Part: CHORD — CORRODED (HORIZ STAB)

WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.

Part: EEL — INOPERATIVE (CABIN)

MAINTENANCE FOUND EMERGENCY LIGHTS FAILED TO TEST ON PRE-FLIGHT. REPLACED EMER. LIGHTS.