N926UP

Part: HYDRAULIC SYSTEM — LEAKING (HYD)

INSPECTION TYPE:N/A ATB - HYD QTY AFTER TAKEOFF WENT TO 2.0 GALS AFTER FLAP RETRACTION QTY HELD STEADY AT 2.3 GALS. FOUND ASYS QTY LOW, SERVICED TO PROPER LEVEL PER M/M 12-12-00-2. CHECKED L/E SLAT ACTUATOR AND FLAP POW'S FOR LEAKS, NONE FOUND. NO OTHER LEAKS NOTED ON A/C. RAN ENGS & CYCLED FLAPS AND FLT CONTROLS HYD REMAINED THE SAME.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

ONE LAMP INOP IN EMERGENCY EXIT LIGHT AT L1 DOOR. RELAMPED OK FOR SERVICE.

Part: SLIDE — INOPERATIVE (L1 DOOR)

INSPECTION TYPE:N/A L-1 DOOR SLIDE INOP. REMOVED AND REPLACED SLIDE ASSY PER 25-60-14, THIS CLEARS M310071.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,493 hrs · 39,150 cycles

C NDI HAS MATERIAL LOSS INDICATION AT S19 RT BS 441, SKIN CUT OUT AND REPAIR IN CONJUNCTION WITH NRC 792106 LAP REPAIR.

Part: STRUCTURE — CORRODED (NR 1 NACELLE) · airframe 52,493 hrs · 39,150 cycles

ENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A.

Part: BUSHING — DAMAGED (NR 3 NACELLE) · airframe 52,493 hrs · 39,150 cycles

ENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,493 hrs · 39,150 cycles

CRACK IN FUSELAGE SKIN BS 355 BETWEEN S26L AND 27L. REPAIR CARRIED OUT IAW SRM 53-30-3 AND 51-10-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,493 hrs · 39,150 cycles

CLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CLEAT IAW SRM 51-30-2.

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 52,493 hrs · 39,150 cycles

ENG NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 52,493 hrs · 39,150 cycles

ENG NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,493 hrs · 39,150 cycles

CRACK ON SKIN AT FWD ENTRY DOOR UPPER FWD AREA (BETWEEN S6 AND S 7L) OF CUT OUT. REPAIR CARRIED OUT IAW EO B727-5330-1460 OPTION 1.

Part: SUPPORT BRACKET — CRACKED (FLAP ACTUATOR) · airframe 52,493 hrs · 39,150 cycles

NR 2 LE FLAP ACTUATOR O/B SUPPORT BRACKET CRACKED AT UPPER FWD CORNER. BRACKET FABRICATED AND REPLACED IAW SRM 51-20-1, 51-30-02 AND DRAWING 65 -16269.

Part: SKIN — DEBONDED (ELEVATOR TAB) · airframe 52,493 hrs · 39,150 cycles

INSPECTION TYPE:C RT ELEVATOR TAB DISBONDED AT LOWER SURFACE 24 INCHES O/B OF INNER EDGE, AT LOWER SURFACE 3 INCHES FROM O/B EDGE 2 SUSPECT AREA RT UPPER OUTER CORNER AND RT UPPER INNER CORNER. REMOVED ELEVATOR TAB IAW MM 27-30-11. REPAIRED TAB IAW SRM 51-40-20. TAB REPAINTED IAW MM 51-21-00. DURING REBALANCING TAB MOVEMENT FOUND TO BE EXCESSIVELY OUT OF LIMITS. REPLACED TAB IAW MM 27-30-11. ADJUSTMENT/TESTED IAW MM 27-30-11 AND FOUND OK.

Part: HINGE — CRACKED (AILERON) · airframe 52,493 hrs · 39,150 cycles

INSPECTION TYPE:C SUSPECT CRACK ON LEFT O/B AILERON I/B TAB HINGE ASSY LWR HALF. HFEC CARRIED OUT ON SUSPECT AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED. FWD HINGE HALF REPLACED IAW SRM 51-30-02. APPLIED CIC TO EXPOSED AREA IAW SRM 51-10-02.

Part: LAP JOINT — CORRODED (FUSLEAGE) · airframe 52,493 hrs · 39,150 cycles

INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT S19R BETWEEN BS 390 AND 441 AREA BETWEEN BS 390 AND 441 PAINT STRIPPED IAW MM 51-20-01. AREA REINSPECTED, COROSION FOUND EVIDENT CONTINUE OPEN UP AND REPAIR IAW APPX C OF EO B727-5330-0509. REMOVED CORROSION IAW SRM 51-10-06 AND FOUND OUT OF LIMITS IAW SRM 53-30-01. UPPER LAP SKIN CUT AT BS 390-441 IAW SRM 53-30-03. LOWER SKIN CORROSION REMOVED IAW SRM 51-10-06, REINSPECTED.

Part: SKIN — CORRODED (LT ELEVATOR TAB) · airframe 52,493 hrs · 39,150 cycles

INSPECTION TYPE:C LT ELEVATOR TAB UPPER SKIN CORRODED 5 INCHES FROM O/B END. REMOVED CORROSION IAW SRM 51-10-01, BLENDOUT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01. REMOVED TAB IAW MM 27-30-11. TAB UPPER SKIN REPAIRED IAW SRM 51-40-20. TAB REPAINTED IAW MM 51-20-00. TAB REBALANCED IAW SRM 51-20-09. TAB REINSTALLED IAW MM 27-30-11. ADJUSTMENT/TEST CARRIED OUT IAW MM 27-30-11 AND FOUND OK.

Part: ACTUATOR — BROKEN (RT MLG)

INSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACED RIGHT MLG LOCK ACTUATOR, PERFORMED MAIN GEAR EXTENSION AND RETRACTION ADJ/TEST W/R/T MM 32-32-00.

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL.

Part: CASTING — CRACKED (RT FLAP) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. REPAIR SECTION FABRICATED IAW SRM 51-40-3 & INSTALLED IAW SRM 51-40-3.

Part: FLAP TRACK — CRACKED (NR 6 FLAP) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02.

Part: FRAME — CORRODED (FAIRING) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE NR B727-5310-20302-A

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 REPAIR CARRIED OUT IAW SRM 51-20-1 AND SMRO EO 2004-027-002. UPS ENGINEERING FILE NR B727-5310-20302-A

Part: BEAM — CORRODED (RT HORIZ STAB) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8.

Part: DRUM — CORRODED (LT MIDFLAP) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01.

Part: SKIN — CRACKED (KRUGER FLAP) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3.

Part: RIB — CRACKED (L/E SLAT) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.

Part: RIB — CRACKED (L/E SLAT) · airframe 52,009 hrs · 38,746 cycles

INSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.

Part: STIFFENER — CORRODED (LOWER END) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED DOUBLER & FILLER IAW SRM 51-40-2, INSTALLED FILLER & DOUBLER IAW SRM 51-40-2 FIG 2.

Part: WEB — CRACKED (BS 235) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSPECTION CONFIRMED CRACK REMOV AL. REPAIR PARTS FABRICATED AND REPAIR INSTALLED IAW SRM 51-40-2, FI G. 1.

Part: SKIN — CRACKED (NO.4 KRUGER FLAP) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02.

Part: SKIN — CRACKED (#3 LE FLAP) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082

Part: SPAR — CORRODED (RT WING) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LOCATION BETWEEN WS 173 AND WS 175. REPAIR CARRIED OUT IAW SMRO 2002-044-004.

Part: SKIN — CRACKED (#4 KRUEGAR FLAP) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082

Part: WEB — CRACKED (BS 1243) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SRM 51-10-4

Part: DOUBLER — CRACKED (BS 269.5) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DOUBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OUT CRACK CONFIRM ED & END OF CRACK MARKED. DOUBLER AND FILLERS FABRICATED AND INSTALL ED IAW SRM 51-40-2 FIG 2

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW EO B727-5311-0631 STEP 3. HEFC INSPECTION CONFIRMED CRACK CONTAINED. AREA REPAIRED IAW B727-5311-0631.

Part: WEB — CRACKED (BS 269.5) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB AREA. NEW WEB AND DOUBLERS FABRICATED AND INSTALLED IAW DRAWING 65-18414

Part: SKIN — CORRODED (BS418-441,S2L-4L) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS INDICATION FROM BS 440 TO BS 411 APPR OX. 20% - 30%. CORRODED INTERNAL DOUBLER ALSO FOUND TO BE DISBONDED. DOUBLER REMOVED IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SMRO EO 2002-044-003, REF. UPS EO B727-5330-1 7405-A.

Part: STIFFENER — CRACKED (FAIRING) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CRACK ON SEAT TRACK IN LWR AFT CARGO COMP AT BS 960 BBL 18L. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5.

Part: INTERCOSTAL — CRACKED (BS 1130 BBL6R) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CRACK ON INTERCOSTAL AT BS 1130 BBL 6 R INTERCOSTAL REMOVED IAW SRM 51-30-02 INTERCOSTAL FABRICATED IAW SRM 51-20-1 FIG 7 AND INSTALLED IAW SRM 51-30-2

Part: SKIN — CORRODED (CROWN, BS 1183) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C CORROSION FOUND ON FUSELAGE SKIN AT BS 1181, BETWEEN S-5L AND S-6L. TO REMOVE CORROSION COMPLETELY, SKIN CUT-OUT WAS MADE FROM BS 1145 T O BS 1180, BETWEEN S-5L AND S-10L. REPAIR WAS CARRIWED OUT IAW SMRO EO 2002-044-002 R2. REF. UPS EO B727-5330-17442-A

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C ON REMOVAL OF FAIRING 3610, CRACK FOUND ON FAIRING 3608 SUPPORT FRAME AT BS 1010 STR 25 RBL 64. HFEC CARRIED OUT POST CUT OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. SUPPORT FRAME REPAIRED IAW SRM 51-40-3 FIG 1 & SRM 53-50-1 FIG 9.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C R/H I/B MIDFLAP DISBOND UPPER SURFACE T-EDGE WEDGE 10 INCHES FROM EN D APPROX. REPAIRED IAW SRM 51-40-20

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 51,472 hrs · 38,218 cycles

INSPECTION TYPE:C, RT WHEEL WELL BS 870 BULKHEAD VERT STIFFENER CORRODED AT UPPER END AT RBL 50 APPROX JUST FWD OF L/E CONTROL VALVE. NEW VERT STIFFENER FABRICATED IAW DRAWING 65-16330, VERT STIFFENER INSTALLED IAW DRAWING 65-16330 & SMRO EO 2002-044-005 UPS ENGINEERING FILE B727-53-20071.

Part: CARRIAGE — CORRODED (NR 7 FLAP TRACK) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, CORROSION ON LOWER SKIN & ON INTERNAL DOUBLER BS 1183 -1110 BETWEEN S20R & 21R REPAIR CARRIED OUT IAW SRM 51-10-6 & 53-30-3

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, LT MLG AFT BULKHEAD STIFFENER CRACKED AT LBL 45 APPROX. REPAIRED IAW SRM 51-40-3

Part: PANEL — CORRODED (WS 270) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C & SI, RT WING & NR 1 FUEL PANEL HAS LIGHT SURFACE CORROSION ON LWR SURFACE, PANEL REPLACED IAW MM 28-11-21

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK HORIZONTAL STIFFENER AT FLANGE RADIUS IN CONTACT WITH INTERIOR SKIN 20 INCHS FWD OF AFT EDGE STIFFENER RUNS BETWEEN FWD AND AFT DOOR STOP ON FWD CARGO DOOR. REPLACED DOOR IAW NRC 320552

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK ON DOOR FRAME INTERIOR FWD CARGO DOOR. DOOR REPLACED ON NRC320552

Part: SKIN — CORRODED (CENTER WING BOX) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, WING CENTER SECTION UPPER SKIN CORROSION FOUND ON LWR SURFACE BETWEE N LBBL 49 & RBBL 45 AT BS 870 AND CORROSION FOUND IN 3 FASTENER HOLE S AT R BBL 61 - 64 AT BS 870. REPAIR CARRIED OUT IAW SMRO EO 2001-010-014 UPS ENGINEERING FILE NO. B727-5710-14405-A

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK FWD CARGO DOOR INTERIOR AT HORIZONTAL STIFFENER LWR FLANGE IN CONTACT WITH INTERIOR SKIN FROM FWD END. REPLACED DOOR IAW NRC 320552

Part: BRACKET — CRACKED (NR 6 SLAT) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, RT WING NR 6 SLAT - I/B SLAT TRACK - O/B TRACK TO SLAT SKIN SUPPORTIN G ANGLE CRACKED REPLACED BRACKET IAW MM 27-81-11

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK IN RTH OB VERTICAL STIFFENER AFT PRESSURE BULKHEAD. REPAIR CARRIED OUT IAW UPS EO B727-5310-1109-E & UPS DRG. 66C33724

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK FWD CARGO DOOR VERTICAL STIFFENER AT FWD UPPER CORNER ADJACENT TO INTERIOR SKIN AND HINGE ATTACH POINT FWD, REPLACED DOOR ON NRC320552

Part: HINGE — CRACKED (RUDDER) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, UPPER RUDDER HINGE SUPPORT FITTING IN VERT STAB HAS SUSPECT CRACK AL ONG LH FLANGE AT FWD END. REPLACED RUDDER HINGE SUPPORT FITTING IAW SMRO EO 2001-010-003 UPS ENGINEERING FILE 727-27-20001

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, CRACK IN FWD CARGO DOOR AT VERTICAL STIFFENER FWD UPPER CORNER SUPPORT ANGLE ADJACENT TO AFT HINGE AFT SIDE. REPLACED DOOR IAW NRC320552

Part: FITTING — CORRODED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, TOP FWD CORNER FITTING CORRODED & CRACKED IN MAIN CARGO DOOR. TOP FWD CORNER FITTING REPLACED ON MCD IAW SRM 51-30-2

Part: SPAR — CRACKED (LT WING) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, CRACK ON REAR SPAR WEB AT APPROX LBBL 16 AT TOP CORNER OF CUTOUT FOR ACCESS PANEL WEB REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1

Part: FITTING — CORRODED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, TOP AFT CORNER FITTING CORRODED & CRACKED ON MAIN CARGO DOOR. TOP AFT CORNER FITTING REPLACED ON MCD IAW SRM 51-30-2.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SPLICE PLATE AT RBBL 70.5 UPPER & BS 870 CRACKED REPAIR CARRIED OUT IAW SRM 51-30-2

Part: PRESSURE PANEL — CORRODED (NLG WW) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, EVIDENCE OF CORROSION ON TOP PANEL NWW BS 312 RT, 2ND STIFFENER. REPAIR CARRIED OUT IAW SRM 51-30-2 & BOEING DRG. 65-18417

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, SUSPECT CRACK IN STIFFENER ON NOSE WW CEILING BL 0 BS 340. NEW STIFFENER INSTALLED IAW PRODUCTION DRWQING 65-18417

Part: FRAME — CORRODED (FAIRING) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, LT WING TO BODY FAIRING NR 3335 HAS CORRODED FRAME. RIVETS REMOVED FROM CORRODED FRAME IAW SRM 51-30-2 CORRODED FRAME CUT OUT IAW SRM 51-10-6 REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1

Part: FLAP TRACK — CORRODED (NR 5) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 5 FLAP TRACK FWD ATTACH LUG CORRODED. REPLACED #5 FLAP TRACK FWD ATTACH LUG IAW DRG 65-21651

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C+SI, BULGING AT LAP JOINT 1342 STR8L DETECTED, UPON INVESTIGATION CRACK A ND CORROSION WAS FOUND. REPAIRED IAW SRM .

Part: SPAR — DAMAGED (CENTER WING) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C&SI SEVERAL RIVET HEADS POPPED ON THE CENTER SECTION REAR SPAR UPR CHORD & VERT. WEB AT LBL 37 LBL 17. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 51-30-01

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C+SI, DURING INSPECTION A CRACK WAS FOUND ON BS 930 RT FRAME RUNNING BETWEEN TWO FASTENERS HOLES BELOW STR 17. FRAME REPLACED.

Part: FRAME — CRACKED (GALLEY DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C&SI CRACK FOUND ON MID GALLEY DOOR AT AFT UPPER FRAME GALLEY DOOR AT AFT UPPER FRAME REPAIRED IAW SRM ADDENDUM UPS EO B727 -5240-4626 APPENDIX D

Part: ATTACH FITTING — CORRODED (LT WING TE FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 1 FLAP TRACK FWD ATTACH LUG HAS SURFACE CORROSION ON THE LUG I/B FACE, REPAIR CARRIED OUT IAW SMRO EO 2001-010-005 UPS ENGINEERING FILE 727-32-20001

Part: CARRIAGE — CORRODED (NR 4 FLAP) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 4 FLAP CARRIAGE HAS HEAVY SURFACE CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED IAW MM 27-51-01 & OHM 57-58-02

Part: CARRIAGE — CORRODED (TE FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 2 FLAP TRACK CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 1 FLAP TRACK CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. REPLACED CARRIAGE

Part: CARRIAGE — CORRODED (NR 5 TE FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 5 FLAP CARRIAGE HAS CORROSION INSIDE BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-58-02

Part: CARRIAGE — CORRODED (NR 8 FLAP) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 8 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED IAW MM 27-51-13

Part: CARRIAGE — CORRODED (TE FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 6 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. NR 6 FLAP CARRIAGE REPLACED IAW MM 27-51-03

Part: PAD — CORRODED (NR 5 FLAP) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 5 FLAP TRACK, AFT MOUNT PAD HAS SURFACE CORROSION ON PAD SURFACE. REPAIR CARRIED OUT IAW UPS EO B727-5742-0651

Part: CARRIAGE — CORRODED (TE FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, FLAP CARRIAGE NR 3 HAS CORROSION IN SPINDLE BORE. FLAP CARRIAGE REPLACED IAW MM 27-51-01 & OHM 57-58-02

Part: PAD — CORRODED (NR 4 FLAPS) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, NR 4 FLAP TRACK AFT MOUNT PAD, HEAVY SURFACE CORROSION ON PAD. CORROSION REMOVED FROM AFT MOUNT PAD WITHIN LIMITS IAW OHM 57-40-01

Part: SUPPORT BRACKET — CORRODED (FLAP TRACK) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C+SI, NR 4 FLAP TRACK ATTACH LUG ON LWR SURFACE OF LT WING HAS LIGHT SURFACE CORROSION ON FACES OF LUG AND DUR TO PREVIOUS REWORK HAS FREEZE PLUG INSERTED AND BUSHING FIT IS VERY LOOSE. NR 4 TRACK ATTACH LUG REPLACED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C & SI, LT BS 910 CRACKED MRR FILED AS OPEN AWAITING LOG PAGE. CRACK REPAIRED IAW EO B727-5310-1896-B

Part: CYLINDER — CORRODED (TAIL SKID) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE: C & SI, TAIL SKID CYLINDER HAS CORROSION ON OUTER SURFACE BELOW MID CLAMP. TAIL SKID CYLINDER REPLACED IAW MM 32-71-22

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C+SI, DURING INSPECTION A CRACK WAS FOUND ON BS 1183 VERTICAL BEAM AT 26,8 3 RT AT WATER LINE 262. REPAIRED IAW EO 727531106311 USING BOEING DWG 65C34406 AND KIT 6 5C34406-5

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 50,160 hrs · 37,219 cycles

INSPECTION TYPE:C&SI ON REMOVAL OF MCD UPPER BEAM ON DOOR FOUND CORRODED. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6 MCD UPPER BEAM REPLACED IAW SRM 51-80-2 WITH REF TO BOEING DRG 65- 25337 & 65-36524 & SMRO EO 2001-010-015 UPS ENGINEERING FILE NO. 727-21-0018

Part: MOUNT — CORRODED (NR 3 ENGINE)

INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT, PITTING CORROSION 4 MOUNT HOLES. NR 3 ENGINE MOUNT FWD MOUNT FITTING HOLES REPAIRED IAW EO NR B727-544 0-11592-A.

Part: MOUNT — CORRODED (NR 1 ENGINE)

INSPECTION TYPE:C ENGINE NR 1 FWD MOUNT PITTING CORROSION ON OUTBOARD ENGINE MOUNT HOLES NR 1 ENGINE FWD MOUNT FITTING OUTBOARD HOLES. REPAIRED IAW EO NR B727- 5440-11592-A.

Part: TE WEDGE — CORRODED (WS 251-383)

INSPECTION TYPE:C, DURING REPAIR ON RT INBOARD MID FLAP DELAMINATION, CORROSION FOUND O N T/E WEDGE UPPER SURFACE. REPLACED MID FLAP IAW MM 27-51-23.

Part: BRACKET — CRACKED (NR 1 NACELLE)

INSPECTION TYPE:C ENGINE NR 1 NACELLE ANTI-ICE DUCT CRACKED AT ATTACH BRACKET. REPAIR CARRIED OUT IAW SMRO EO 99-26-002 UPS ENGINEERING FILE NR 727-53-2165.

Part: INTERCOSTAL — CRACKED (BS 380 - 400)

INSPECTION TYPE:C, INTERCOSTAL CRACKED LT SIDE OF E & E BAY BETWEEN BS 380 - 400 LEVEL WITH FLOOR. REPLACED INTERCOSTAL IAW SRM 51-20-01 FIG 7.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE:C NR 3 LE SLAT RIB CRACKED O/B SIDE OF I/B SLAT TRACK. RIB REPAIR CARRIED OUT IAW 57-30-3.

Part: BRACKET — CRACKED (BS 950)

INSPECTION TYPE:C ON REMOVAL OF LT MLG PRESSURE WEB DOUBLER AND BRACKETS ONE BRACKET AT BS 950 BL 60 FOUND TO BE CRACKED. REPLACED ANGLE IAW DRAWING NR 65-89360.

Part: SKIN — CORRODED (RT TE MID FLAP)

INSPECTION TYPE:C RT OUTBOARD MID FLAP, EVIDENCE OF CORROSION ON TE SKIN LWR SURFACE AREA AFT OF NR 8 TEARDROP FAIRING. DAMAGED SKIN REPAIRED IAW SRM 51-40-6 FIG 41.

Part: FRAME — CRACKED (BS 930)

INSPECTION TYPE:C ON REMOVAL OF LT PRESSURE WEB REPAIRS IN LT MLG CEILING A SUSPECT CRACK DETECTED ON FRAME AT BS 930 BELOW S-17. NEW FRAME INSTALLED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 1330)

INSPECTION TYPE:C, SUSPECT CORROSION ON SKIN BS 1330 S9 LT. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3.

Part: SKIN — CORRODED (BS 1072)

INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLERS BS 1072 BETWEEN S 17 AND 16 RT. REPAIR CARRIED IAW SRM 53-30-3 FIG 3 A AND EO 99-26-003 UPS ENGINEERING FILE NR 727-30-0011.

Part: BRACKET — CRACKED (NR 1 ENGINE)

INSPECTION TYPE:C, ENGINE NR 1 THRUST REV OUTBOARD FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. NR 1 ENGINE THRUST REVERSER OUTBOARD FAIRING MID AND AFT SUPPORT BRACKETS REPLACED IAW MM 78-30-00.

Part: BRACKET — CRACKED (RT WING)

INSPECTION TYPE:C RT WING, LWR FIXED TE PANEL SUPPORT BRACKET CRACKED AREA AT NR 8 SPOILER CENTER HINGE SUPPORT FITTING. BRACKET REMOVED AND REPLACED IAW SRM 51-10-3 SRM 51-20-1 SRM 51-30-2.

Part: STRAP — CRACKED (RT COCKPIT)

INSPECTION TYPE:C, ON X-RAY INSP OF E & F WINDOW POST RT SIDE OF COCKPIT CRACK FOUND IN PT F OF STEEL STRAP. REPAIR CARRIED OUT IAW UPS EO B727-5310-0012 USING KIT (P/N 65C 35282-8).

Part: HOUSING — CRACKED (RT MLG TRUNION)

INSPECTION TYPE:C SUSPECT CRACK ON RT MLG TRUNNION BEARING HOUSING. REPAIR CARRIED OUT IAW SRM 20-20-01, MM 32-11-51, OHM 32-10-13 AND MM 32-32-00.

Part: WEB — CRACKED (BS 940)

INSPECTION TYPE:C, CRACK FOUND LT MLG WHEEL WELL PRESSURE WEB LBL 36 BS 940. REPAIRED PRESSURE WEB ON LT MLG WHEEL WELL IAW DRAWING NR 65 -89360 AND EO B727-5310-0460 APPENDIX C.

Part: CASTING — CRACKED (RT AILERON)

INSPECTION TYPE-C, CRACK ON RIGHT HAND AILERON LOCKOUT CASTING. CASTING REPLACED IAW DRAWING 65-21779 AND SRS ENGINEERING ORDER 98-0 6-005.

Part: SPLICE — CORRODED (BS 520)

INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 522 BETWEEN S1R AND 2R. CORROSION ON SKIN FOUND TO BE WITHIN LIMITS. CORROSION ON BUTT SPLICE STRAP REMOVED AND REPAIRED IAW SRS ENGINEEIRNG ORDER 98-06-002R1, UPS ENGINEERING FILE NUMBER 727-53-2007.

Part: EEL ASSY — INOPERATIVE (CABIN)

M/X DISCOVERED FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD. ON (P/N 10-0067-9) (S/N 9493), OFF (P/N 10-0067-9) (S/N 17745).

Part: BATTERY — LOOSE (CABN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. FOUND BATTERIES LOOSE. TIGHTENED BATTERIES AND REINSTALLED EMERGENCY EXIT LIGHTS, OPS CK GOOD.

Part: CARRIAGE — CORRODED (NR 6 TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 6 FLAP CARRIAGE UNDER THE THRUST NUT. MAINTENANCE REMOVED AND REPLACED THE FLAP CARRIAGE PER MM 57-52-01.

Part: CORE — DAMAGED (NR 5 SPOILER)

DURING 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE AND CONTAMINATION ON PREVIOUS REPAIR AREA, NR 5 SPOILER. INSTALLED REPAIR PER SRM 57-50-6, MM 51-20-151.

Part: BLKHD SUPPORT — CORRODED (FWD CARGO BAY)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FORWARD CARGO BAY AFT BULKHEAD UPPER SUPPORT. MAINTENANCE FABRICATED NEW UPPER SUPPORT, PREPARED AND INSTALLED PER SRM 51-10-2, 51-20-151, AND SRM 51-30-2.

Part: LINK MOUNT — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON TORSION LINK MOUNT AT STATION 740, RBL 36, WL 164 MARKED. MAINTENANCE REMOVED AND REPLACED THE CORRODED TORSION LINK MOUNT IAW SRM 51-30-2.

Part: SKIN — DELAMINATED (NR 14 SPOILER)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SURFACE OF THE NR 14 SPOILER. MAINTENANCE REMOVED THE DAMAGED AREA, FINAL REPAIR PER SRM 51-40-6.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 188.5 AND SS 195.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.

Part: RIB — CRACKED (NR 3 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SLAT RIB AT SS 225 LOWER AFT CORNER. MAINTENANCE REPAIRED THE RIB USING DOUBLER PER 727 SRM 57-50-3.

Part: RIB — CRACKED (NR 4 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 4 SLAT END RIB AT SLAT STATION ZERO. MAINTENANCE REMOVED AND INSTALLED A NEW RIB ASSEMBLY PER SRM 51-10-1.

Part: FRAME — CRACKED (BS 660)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE FRAME AT STATION 660 AND STRINGER 26R. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-10-1, 51-30-2, 53-10-1, 53-10-4, 51-40-3, AND 51-40-4.

Part: BRACKET — CORRODED (BS 364)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON BRACKET BETWEEN STRINGERS S5L AND S6L AT STATION 364. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW SRM 51-30-2.

Part: TIE — CORRODED (BS 950)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TIE FORWARD SIDE AT STATION 950 AND STRINGER S2R. MAINTENANCE REMOVED THE CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED THE LOWER STRINGER S2R TIE IAW SRM 53-30-1 AND 51-30-02.

Part: STRINGER — CORRODED (BS 740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2L AT STATION 740 TO 870. MAINTENANCE REMOVED THE CORROSION, CUT OUT DAMAGED AREA OF STRINGER, FABRICATED PANTS, AND INSTALLED REPAIR PARTS AND DOUBLERS IAW SRM 53-10-1, 51-10-6, 53-10-3, 51-20-1, 51-10-2, 51-30-2, 51-30-4 AND MM 51-20-15, 53-11-00.

Part: RIB — CRACKED (NR 5 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 105 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-02 AND 57-50-3.

Part: RIB — CRACKED (NR 5 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT STATION 97.5 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER AND FINAL INSTALLATION IAW SRM 51-30-02 AND 51-50-3.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE SKIN OF THE NR 6 SLAT BETWEEN STATION 166.5 AND STATION 161.5 AT FORWARD FASTENERS. MAINTENANCE REMOVED THE FASTENERS, STOP DRILLED, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-20-04, 51-10-2 AND MM 51-20-151.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT MOST INBOARD RIB (SEAL RETAINER RIB AT SLAT STATION 120). MAINTENANCE REMOVED THE CRACKED RIB, INSTALLED NEW RIB AND FINAL INSTALLATION IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER — CORRODED (BS 360-480)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R AT STATION 360 TO 480. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-10-3 AND FINAL INSTALLATION IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 660/680)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY STRINGER 23L AT STATION 660 AND 680. MAINTENANCE FABRICATED NEW STRINGER REPAIR SECTIONS PER SRM 51-30-5, 51-10-6 AND SRM 51-10-3.

Part: FITTING — CORRODED (BS 704)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER FITTING NR 2R AT STATION 740 AFT SIDE. MAINTENANCE REMOVED THE CORROSION ON NR 2R STRINGER AT STATION 704 AFT SIDE, FOUND TO BE OUT OF LIMITS, WORK ACCOMPLISHED PER SRM 51-10-6, ORDERED NEW PART AND INSTALLED IAW SRM 51-30-2.

Part: LINK MOUNT — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON TORSION LINK MOUNT AT STATION 740, RBL 13 AND WL 164. MAINTENANCE REMOVED THE CORRODED LINK AND LINK MOUNT AND INSTALLED NEW LINK AND LINK MOUNT IAW SRM 51-30-2.

Part: BLKHD STRAP — CORRODED (BS 351)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRAP ON TOP OF 351 BULKHEAD AT WL 160, LBL 25 TO RBL 25. MAINTENANCE FABRICATED A NEW STRAP AND INSTALLED STRAP PER SRM 51-30-2.

Part: RUB STRIP — DELAMINATED (TE FORE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATED STAINLESS STEEL RUB STRIP AND AREAS UNDER THE RUB STRIP. MAINTENANCE REPAIRED THE AREA PER 727 SRM 51-40-06.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R AT STATION 950 TO 1183. MAINTENANCE FABRICATED 'J' ANGLE REPAIR PARTS AND INSTALLED PER EO 727-53-1570.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT ATTACHING FASTENER BETWEEN SS 147 AND SS 154.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.

Part: K-FLAP — CORRODED (NR 2 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 2 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE AT BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW OHM 57-51-11 AND MM 27-81-01.

Part: FRAME — CRACKED (BS 660)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE FRAME AT STATION 660 AND STRINGER 26L AROUND HOLE. MAINTENANCE FABRICATED REPAIR DOUBLER, VERIFIED, CRACK REMOVED, BY NDI. INSTALLED FABRICATED PARTS PER SRM 51-40-3, 51-30-2, 51-10-2, 51-20-4 AND 51-20-1.

Part: K-FLAP — CORRODED (NR 3 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 3 K-FLAP OUTBOARD HINGE LUG UPPER AND LOWER BOLTS ON OUTBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.

Part: K-FLAP — CORRODED (NR 4 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 4 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE BOTH MOUNT BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.

Part: CHORD — CRACKED (LT TE MID FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND TWO 20 PLUS INCH CRACKS IN THE LEFT WING INBOARD MID FLAP AFT LOWER CHORD. MAINTENANCE REMOVED THE LOWER CHORD IAW SRM 51-30-2, FABRICATED, NEW EXTRUSION A LOWER CHORD. FINAL INSTALLATION IAW SRM 51-10-2.

Part: STRINGER — CORRODED (BS 480-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3R AT STATION 480 TO 740. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-1, 51-10-0, 51-10-02, 51-20-151, 51-30-2 AND 53-10-3.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT RADIUS OF THE RIB AT SS 140 FORWARD END AT RIB, UPPER FLANGE RADIUS AREA. MAINTENANCE REMOVED THE RIB, FABRICATED NEW RIB AND FINAL INSTALLATION IAW SRM 51-10-2 AND 51-20-151.

Part: ANGLE — CRACKED (BS 1084)

DURING 'D' CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK IN THE AFT CARGO DOOR NR 3 HORIZONTAL BEAM UPPER OUTBOARD L-ANGLE AT STATION 1084. MAINTENANCE REMOVED AND REPLACED THE L-ANGLE, UPPER OUTBOARD HORIZONTAL BEAM IAW SRM 51-30-5, 51-30-2 AND 51-10-1.

Part: STRINGER — CORRODED (BS 620-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9L AT STATION 620 TO 740. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-3, 51-30-2 AND 51-10-3.

Part: STRINGER — CORRODED (BS 870-950)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6R AT STATION 870 TO 950. MAINTENANCE BLENDED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-2, 51-20-04, MM 51-20-151, AND UPS EO 727-53-1570.

Part: SEAT TRACK — CORRODED (BS 948)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP CENTER OF SEAT TRACK AT STATION 948, BL 0. MAINTENANCE REPLACED THE SEAT TRACK FROM BS 870 TO 960, BL 0. ALL WORK DONE PER SRM 53-10-1, 51-10-2, 53-10-5 AND 51-30-2.

Part: CELL CUTOUT — CORRODED (WINGS)

DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7206 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 1 AT STATION 950 TO 1183. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-1, 51-10-0, 51-10-02, 51-20-151, 51-30-2 AND 53-10-3.

Part: RIB — CRACKED (BS 760.5)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS IN FORWARD TWO AND AFT UPPER HOLES AND RIB CHORD AT STATION 760.5 AND RBL 70.5. MAINTENANCE REMOVED AND REPLACED FAIL SAFE STRAP AND T-CLIP AND REPAIRED RIB CHORD PER UPS EO B727-5710-6847A AND UPS EO B727-57-1338.

Part: K-FLAP — CORRODED (NR 5 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 5 K-FLAP OUTBOARD HINGE LUG OUTBOARD FACE UNDER BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.

Part: WEB — CRACKED (BS 1243)

DURING 'D' CHECK, MAINTENANCE FOUND CRACK AT STA 1243, LBL 15, WL 180, ON VERTICAL WEB FOR LWR TORQUE BOX, AT 7 O'CLOCK POSITION OF LWR LIGHTENING HOLE. REPAIRED PER SRM 51-40-2, 51-10-1.

Part: STRINGER — CORRODED (BS 360-480)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER S5R FROM STATION 360 TO 480. MAINTENANCE FABRICATED REPAIR SECTION AND INSTALLED IAW SRM 53-10-3, 53-10-1, 51-10-2 AND 51-10-6.

Part: SEAT TRACK — CRACKED (BS 600)

DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON SEAT TRACK FLANGE STA 600, RBL 55. REPLACED PER SRM 51-10-1, 51-10-2, 51-30-2, MM 51-20-151.

Part: BEAM — CRACKED (BS 1096)

DURING 'D' CHECK, MAINTENANCE FOUND A 1 INCH CRACK IN THE AFT CARGO DOOR NR 2 HORIZONTAL BEAM AT STATION 1096. MAINTENANCE REMOVED AND REPLACED THE BEAM PER SRM 51-30-5 AND 51-30-2.

Part: KEEL BEAM — CRACKED (BS 872)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE KEEL BEAM VERTICAL WEB JUST FORWARD OF APU CUTOUT AT STATION 872, RBL 5.5, WL 162 IN RIGHT HAND MAIN LANDING GEAR WHEEL WELL. MAINTENANCE REMOVED THE DAMAGED STRUCTURE PER UPS EO B727-5330-7995.

Part: CELL CUTOUT — CORRODED (WINGS)

DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7202 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT AT RIB SS 182, AFT CORNER WHERE LWR CHORD ATTACHES TO RIB. REPAIRED PER SRM 57-50-3.

Part: STRINGER — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9R AT STATION 740 TO 870. MAINTENANCE REPLACED WITH NEW SECTION OF STRINGER IAW SRM 53-10-1, 53-10-2, 51-10-6, 51-10-02 AND MM 51-20-151.

Part: SKIN — DELAMINATED (NR 14 SPOILER)

DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON PREVIOUS REPAIRED NR 14 SPOILER HAD EXPOSED FIBERS ON THE LEADING EDGE AND OUTBOARD EDGE UPPER SURFACE. MAINTENANCE REMOVED THE PREVIOUS REPAIR AND DELAMINATION PER SRM 51-50-6, FINAL REPAIR PER SRM 51-40-6.

Part: CLIP — CRACKED (BS 970)

WHILE IN 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE STRINGER CLIP AT STATION 970, STRINGER 9R. MAINTENANCE REMOVED AND REPLACED THE STRINGER CLIP PER 727 SRM.

Part: TRIM TAB — DELAMINATED (RT INBD AILERON)

DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT HAND INBOARD AILERON TRIM TAB AT THE TRAILING EDGE. MAINTENANCE REMOVED THE DELAMINATION AND FINAL REPAIRS PER SRM 51-40-6 AND SRM 51-80-3.

Part: JOINT — CORRODED (BS 855)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION JOINT AT STATION 855 TO 870, RBL 45, WL 203 AT AFT ATTACH POINT. MAINTENANCE REMOVED THE CORROSION FROM EXPANSION JOINT AND FOUND DAMAGE OUT OF LIMITS. REPLACED PART IAW SRM 53-10-1 AND 51-30-02.

Part: SKIN — DELAMINATED (RT TE FORE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD FORE FLAP ON THE INBOARD END UPPER SURFACE. MAINTENANCE REPAIRED BY REMOVING DELAMINATION AND PRIOR REPAIR PER SRM 51-40-06 AND FINAL REPAIR PER SRM 51-40-00.

Part: WEB — CORRODED (BS 203)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE WEB AT STATION 203 TO 204, LBL 34 TO 40 AND WL 208. MAINTENANCE REMOVED, FABRICATED REPAIR PART, INSTALLED PER SRM 51-10-6, 51-30-2 AND MM 51-20-15.

Part: RUDDER TAB — DELAMINATED (RUDDER)

DURING 'D' CHECK, MAINTENANCE FOUND THE UPPER RUDDER TAB LOWER SURFACE TO BE DELAMINATED. MAINTENANCE REPAIRED PER SRM 51-40-6.

Part: JOINT — CORRODED (BS 855)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION JOINT (LINK) AT STATION 855 TO 820, RBL 45. MAINTENANCE REMOVED AND REPLACED EXPANSION LINK PER SRM 51-10-1.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TPI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 176 AND SS 182. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.

Part: SKIN — CRACKED (RUDDER TAB)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE BULLNOSE SKIN AT THE UPPER RUDDER TAB, UPPER BULLNOSE ABOVE UPPER HINGE. SKIN WAS PULLED BACK. MAINTENANCE REMOVED THE NOSE SKIN, RECEIVED NEW END CAP AND FINAL INSTALLATION PER SRM 51-30-2 AND 51-20-151.

Part: SEAT TRACK — CORRODED (BS 380)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP OF AND IN SEAT TRACK WELL AT STATION 380 TO 430 AND RBL 23. MAINTENANCE REMOVED SEAT TRACK AND REPLACED IT WITH NEW PER SRM 5-10-6.

Part: RIB — CRACKED (NR 5 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 112 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-2 AND 57-50-3.

Part: CHANNEL — CRACKED (PIE SECTION)

DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE END ENCLOSURE RIB CHANNEL, OUT BOARD END OF RIGHT PIE SECTION. MAINTENANCE REMOVED THE CRACKED CHORD, FABRICATED PER SRM 51-30-2 AND FINAL INSTALLATION IAW SRM 51-30-5.

Part: STRINGER — CORRODED (BS 480-620)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6R AT STATION 480 TO 620. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-01 AND 53-10-3.

Part: FRAME — CORRODED (BS 312)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME ON TOP AND BOTTOM FLANGES BETWEEN STRINGERS 2L TO 5L AT STATION 312. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR CHANNEL PER SRM 53-10-4 AND FINAL INSTALLATION PER SRM 53-10-4.

Part: STRINGER — CORRODED (BS 480-620)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8R AT STATION 480 TO 620. MAINTENANCE REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 51-30-2, 53-10-3 AND 51-20-4.

Part: CLIP — CORRODED (BS 420)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER CLIP AT STATION 420, STRINGER 6L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP PER SRM 51-30-2, 51-10-2.

Part: FLOORBEAM — CORRODED (BS 660)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON NUTPLATES AT BOTTOM OF FLANGE OF FLOORBEAM AT STATION 660, RBL 64 TO LBL 64, WL 208.1. MAINTENANCE REMOVED TOP OF FLOORBEAM FROM WEB RBL 17 OUTBOARD TO END OF BEAM, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8.

Part: SKIN — CORRODED (BS 760-785)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE INNER SKIN AT STATION 760 TO 785 BETWEEN STRINGERS S8R AND S10R. MAINTENANCE REMOVED THE CORROSION, HFEC INSPECTED AREA, FLAP PINNED AREA AND REINSTALLED SURFACE FINISH IAW EO 95-2345.

Part: FLOORBEAM — CORRODED (BS 680)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON NUTPLATES AT BOTTOM OF FLANGE OF FLOORBEAM AT STATION 680 FROM LBL 64 TO RBL 64 AND WL 208.1. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-10-8.

Part: STRINGER — CORRODED (BS 680-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9R AT STATION 680 TO 740. MAINTENANCE CUT FRAME AT BS 720, STR 9R FOR ACCESS. FABRICATED FRAME REPAIR PARTS, INSTALLED STRINGER 9R AND FRAME REPAIR PARTS PER SRM 53-10-4, 51-30-2 MM 51-20-151.

Part: SPOILER — DELAMINATED (NR 10 SPOILER)

DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION AND CONTAMINATION ON THE NR 10 SPOILER. MAINTENANCE REPLACED THE SPOILER IAW MM 27-61-01.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2R AT STATION 950 TO 1183. MAINTENANCE SPLICED A NEW SECTION OF STRINGER FROM BS 950 TO 1036 IAW SRM 53-10-3.

Part: K-FLAP — CORRODED (NR 6 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 6 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE UNDER THE UPPER LUG. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.

Part: K-FLAP — CORRODED (NR 1 LE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND PITTING CORROSION ON THE NR 1 K-FLAP AT CENTER ATTACH LUG ON UPPER INBOARD, UPPER OUTBOARD AND LOWER INBOARD MOUNT BOLT AREAS. MAINTENANCE REPLACE THE NR 1 K-FLAP IAW MM 27-81-01.

Part: STRINGER — CORRODED (BS 480-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 4R SIDE AT STATION 480 TO 740. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLATION PER EO 95-2388, SRM 51-10-2 AND 51-30-2.

Part: SKIN — CORRODED (BS 1148-1163)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER SKIN AT SKIN LAP AT STATION 1148 TO 1163, STRINGER 25L TO 26L, STRINGER FITTING ALSO, CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FITTING, THE CORRODED SKIN AND DOUBLER IAW SRM 51-30-2, SRM 53-30-3, SRM 51-30-4, SRM 51-20-4 AND UPS EO 727-53-1563.

Part: STRINGER — CORRODED (BS 480-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 5R SIDE AT STATION 480 TO 740. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLATION PER EO 95-2388, SRM 51-10-2 AND 51-30-2.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3R AT STATION 950 TO 1183. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED PER SRM 53-10-2.

Part: STRINGER SPLICE — CORRODED (FS 740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICE FORWARD ON TERMINATION ENDS OF STRINGER CENTER THROUGH 9L SIDE ON FORWARD SIDE FRAME STATION 740. MAINTENANCE REMOVED AND REINSTALLED NEW STRINGER SPLICES AT STRINGERS 1 AND 8 AT STATION 740 FRONT SIDE IAW SRM 51-10-2 AND 51-10-1.

Part: FLOORBEAM — CORRODED (BS 344)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES UPPER AND LOWER FLANGES OF FLOORBEAM AT STATION 344, RBL 11 TO RBL 20, WL 208.1. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW UPS EO B727-5310-6844A.

Part: CHANNEL — CORRODED (BS 344)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER FLANGE OF THE CHANNEL AT STATION 344 FROM RBL 10 INCHES TO 60 INCHES AND WL 208. MAINTENANCE FABRICATED A NEW CHANNEL IAW SRM 51-10-1, 51-10-2, 51-30-2 AND MM 57-20-151.

Part: FRAME — CORRODED (BS 351.2)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER CHORD AND STRAP AT STATION 351.2 BETWEEN STRINGERS 26L AND 25L. MAINTENANCE TRIMMED OUT FAIL SAFE CHORD FOR ACCESS, BLENDED OUT CORROSION, FREEZE PLUG DISCREPANT HOLES. FABRICATED NESTING REPAIR ANGLES, FILLER, AND TAPERED SHIMS AND INSTALL REPAIR PARTS. WORK IAW UPS EO B727-5310-6860A.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 5R AT STATION 950 TO 1183. MAINTENANCE REMOVED CORROSION, FABRICATED NEW STRINGER, SENT OUT FOR HEAT TREATMENT AND INSTALLED IAW SRM 51-30-2, 51-10-6, 53-10-1, 53-10-3 AND MM 51-20-151.

Part: RIB — CRACKED (NR 4 LE SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT RIB AT SS 63, FWD UPPER CORNER. REPAIRED PER SRM 57-50-3.

Part: CELL CUTOUT — CORRODED (WINGS)

DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7207 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER EO 727-57-1123.

Part: TE SKIN — CRACKED (NR 7 SLAT)

DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT T/E. INSTALLED REPAIR PER SRM 51-40-2, 51-30-2, MM 51-20-21, 51-20-71.

Part: CELL CUTOUT — CORRODED (WINGS)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7606 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123.

Part: CELL CUTOUT — CORRODED (WINGS)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7607 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123.

Part: FLOORBEAM — CORRODED (BS 720)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FLOORBEAM AT STATION 720, RBL 51 AND RBL 61, WL 208. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED ALL WORK DONE PER SRM 51-10-1, 51-10-6, 51-10-2, 51-30-2 AND UPS EO B727-5310-6839A.

Part: STRINGER — CORRODED (BS 480-740)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 1 AT STATION 480 TO 740. MAINTENANCE REMOVED THE DAMAGED SECTIONS OF STRINGER 1 FROM BS 480 TO 511, BS 620 TO 740, FABRICATED AND INSTALLED REPAIR SPLICES AND NEW SECTIONS OF STRINGER. ALL WORK DONE PER SRM 53-10-3 AND UPS EO B727-53-1570.

Part: SEAT TRACK — CORRODED (BS 954-958)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP CENTER AND BOTTOM OUTBOARD FLANGE OF SEAT TRACK AT STATION 954 TO 958, RBL 24.75. MAINTENANCE REMOVED THE DAMAGED SECTION OF SEAT TRACK, REPLACED PER SRM 51-10-2, 51-30-2 AND MM 51-20-151.

Part: SEAT TRACK — CORRODED (BS 942)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM INBOARD FLANGE OF SEAT TRACK AROUND FASTENER HOLES AT STATION 942, LBL 45.5. MAINTENANCE FABRICATED NEW SECTION OF SEAT TRACK AND REPAIR SPLICES, INSTALLED, PER SRM 51-10-6, 53-10-1, 51-30-2, 51-10-1, 51-10-2 AND MM 51-20-151.

Part: STRAP — CRACKED (BS 760.5)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS IN FORWARD TWO AND AFT UPPER HOLES AND RIB CHORD AT STATION 760.5 AND LBL 70.5. MAINTENANCE REMOVED AND REPLACED FAIL SAFE STRAP AND T-CLIP AND REPAIRED RIB CHORD PER UPS EO B727-5710-6847A AND UPS EO B727-57-1338.

Part: STRINGER — CORRODED (BS 620-680)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R STA 620 TO 680. REPLACED PER SRM 53-10-1.

Part: CLIP — CORRODED (BS 760)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON T-CLIP AT STA 760, WHILE ACCESSING FOR 70.5 INSP. REPLACED PER SRM 51-30-02, 51-30-05.

Part: SKIN — DAMAGED (NR 7 SLAT)

DURING 'C' CHECK, MAINTENANCE FOUND NR 7 SLAT TRAILING EDGE SKIN AT I/B SLAT HOOK IS DAMAGED FROM LOOSE FASTENERS. INSTALLED REPAIR PER UPS ENGINEERING FILE NR B272-57-1339.

Part: STRINGER — CORRODED (BS 480-620)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 7R STA 480-620. REPLACED PER SRM 53-30-2.

Part: SKIN — DELAMINATED (RT TE MID FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND DELAMINATION ON LWR SKIN OF RT I/B MID FLAP. INSTALLED REPAIR PER SRM 51-40-6.

Part: INTERCOSTAL — CORRODED (BS 600-680)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL IN FWD CARGO BAY STA 600-680, RBL 65. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-20-1, 51-30-2.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 4L STA 950-1183. REPLACED STRINGER PER SRM 51-30-2, 53-10-3.

Part: SEAT TRACK — CORRODED (BS 344-360)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 344-360, LBL 61. REPLACED PER SRM 51-30-2, 51-10-1, 57-30-8.

Part: BEAM — CRACKED (AFT CARGO DOOR)

DURING 'C' CHECK, MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 4 HORIZONTAL BEAM AT BS 1084. REPLACED BEAM PER SRM 51-30-05, 51-30-02, 51-10-1.

Part: FRAME — CORRODED (BS 950)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BS 950 FRAME FORGING AROUND NUT HEAD ON BOTTOM OF FWD FORGING EAR WL 207, RBL 64. INSTALLED REPAIR PER SRM 51-10-6.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8L STA 950-1183. REPLACED STRINGER AND SPLICES PER SRM 51-30-2, 53-10-3, 51-10-2, MM 51-20-151.

Part: STRINGER — CORRODED (BS 950-1183)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8R STA 950-1183. REPLACED STRINGER PER SRM 51-30-2, 51-40-5, 53-10-4, 53-40-4.

Part: STRINGER — CORRODED (BS 740)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICE ENDS AND ON TERMINATION ENDS ON STRINGERS NR 2 THROUGH NR 9R ON FWD SIDE OF BS 740 FRAME (PRODUCTION JOINT). FITTINGS AT STRINGERS 3, 5, 8, 9, WERE REPLACED. STRINGER FITTINGS AT STRINGERS 2, 4, 6, 7, FOUND TO BE WITHIN LIMITS. ALL WORK DONE IN ACCORDANCE WITH SRM 51-10-6, 51-10-2, 51-20-4, 51-30-21, MM 51-20-151, AND 53-11-40-00.

Part: SEAT TRACK — CORRODED (BS 950-970)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK I/B FLANGE STA 950-970, LBL 62.0. REPLACED SEAT TRACK PER SRM 53-10-1, 53-10-05.

Part: FLOOR BEAM — CORRODED (BS 312)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLE UPPER FLANGE OF FLOORBEAM AT STA 312, LBL 45, WL 208. REPLACED PER UPS EO B727-5310-6838A.

Part: HAT CHANNEL — CORRODED (BS 315)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES IN UPPER FLANGE OF HAT CHANNEL AT STA 315, RBL 12. WL 208. REPLACED PER SRM 51-10-02, 51-30-2, 51-10-6, AND MM 51-20-151.

Part: FORGING — CORRODED (LT WING)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION IN LT FWD BOTTLE PIN FORGING AND FITTING 740. REPLACED BUSHINGS PER UPS EO FILE NR B727-53-1548.

Part: STRINGER — CORRODED (BS 480-740)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 2R, BS 480-740. INSTALLED REPAIR AND REPLACED SECTIONS OF STRINGER PER SRM 53-10-3.

Part: INTERCOSTAL — CRACKED (BS 854)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATES AND CRACKS AROUND ATTACH POINTS OF INTERCOSTAL STA 854, LBL 25-45, WL 206. REPLACED PER SRM 51-30-2.

Part: STRINGER SPLICE — CORRODED (BS 950)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICES FWD SIDE STA 950, STRINGERS 2, 4, 6, 7, 8, 9 L. REPLACED STRINGERS SPLICES 2L AND 7L, BLENDED REMAINING STRINGER SPLICES. ALL WORK ACCOMPLISHED PER SRM 51-10-6, 51-30-2, 51-20-4, MM 51-20-151.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 3 SLAT RIB, LWR AFT CORNER WHERE RIB AND LWR CHORD ATTACH. INSTALLED REPAIR PER SRM 51-30-2, 57-50-3.

Part: SKIN — CRACKED (LOWER RUDDER)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON LWR RUDDER BOTTOM SKIN. REPLACED SKIN PER SRM 51-30-2, 51-10-2, 51-10-1, MM 51-20-71.

Part: RIB — CRACKED (RT O/B MID FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK ON RT WING O/B MID FLAP, O/B AFT END RIB, AT LWR CORNER. REPLACED RIB PER SRM 51-30-2, 51-10-1, 51-10-2.

Part: SPAR CHORD — CRACKED (LT O/B AILERON)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON LT WING O/B AILERON, UPPER FWD SPAR CHORD. INSTALLED REPAIR PER SRM 51-40-4, 51-10-2, 51-30-2, MM 51-20-00.

Part: FLAP — DELAMINATED (RT I/B AFT FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON RT I/B AFT FLAP, UPPER SIDE, FWD I/B CORNER. INSTALLED REPAIR PER SRM 51-40-06.

Part: SKIN — OIL CANNED (STA 690-700)

WHILE IN 'D' CHECK MAINTENANCE FOUND OIL CANNED FUSELAGE SKIN AT BS 690-700, STRINGER 20-21R. INSTALLED REPAIR PER SRM 51-20-4, 51-30-2.

Part: STRINGER CLIP — CORRODED (STA 328)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER CLIP STA 328, STRINGER 21R. REPLACED PER SRM 51-20-1, 51-30-2, MM 51-20-21.

Part: TAB — DELAMINATION (UPPER RUDDER)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB, UPPER LT SIDE. INSTALLED REPAIR PER SRM 51-40-6.

Part: TAB — DELAMINATION (LOWER RUDDER)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON LWR RUDDER TAB T/E. INSTALLED REPAIR PER SRM 51-40-9.

Part: SLAT CUT OUT — SHEARED FASTENER (NR 7 SLAT)

WHILE IN 'D' CHECK, MAINTENANCE FOUND SHEARED FASTENERS ON NR 7 SLAT HOOK I/B CUT OUT ON UPPER AFT SIDE. INSTALLED REPAIR PER SRM 57-30-4.

Part: FLAP — DELAMINATION (RT WING FORE)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON RT O/B FOREFLAP, T/E UPPER AND LWR SURFACE, ON PREVIOUS REPAIR. INSTALLED REPAIR PER SRM 51-40-06.

Part: STRINGER — CORRODED (STA 360-480)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L, STA 360-480. INSTALLED REPAIR PER SRM 53-10-3.

Part: SPOILER — DELAMINATION (LT WING NR 1)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 1 SPOILER UPPER SURFACE I/B FWD CORNER. INSTALLED REPAIR PER SRM 51-40-6.

Part: FLAP — CORRODED (NR 3 LE FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP, O/B BULLNOSE, UPPER HINGE LUG ATTACH FRAME, UPPER SURFACE ON BOTH NUTS. REPLACED K-FLAP PER SRM 57-50-01, OHM 57-51-21, MM 27-81-01.

Part: SHEAR TIE — CRACKED (STA 1148)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT STA 1148, BETWEEN STRINGER 25 AND 16L. REPLACED PER DRM 53-10-4, 51-20-4, 51-30-1, 51-20-1.

Part: SPOILER — DELAMINATED (NR 12 SPOILER)

WHILE IN 'D' CHECK, MAINTENANCE FOUND NR 12 SPOILER CORE TO BE DELAMINATED. INSTALLED REPAIR PER SRM 57-50-6.

Part: RIB — CRACKED (RT I/B MID FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON RT WING I/B MID FLAP, RIB, IN LEADING EDGE, JUST I/B OF FOREFLAP CENTER TRACK CUT OUT. REPLACED RIB PER SRM 51-30-2.

Part: SPOILER — DELAMINATION (LT WING NR 4)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 4 SPOILER LWR SURFACE O/B FWD CORNER. INSTALLED REPAIR PER SRM 51-40-6 AND 57-50-6.

Part: STRINGER — CORRODED (STA 950-1183)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L, STA 950-1183. INSTALLED REPLACEMENT AND REPAIR PER SRM 53-10-1, 53-10-3.

Part: SKIN — DELAMINATED (NR 9 SPOILER)

WHILE IN "D" CHECK, MAINTENANCE FOUND NR 9 SPOILER DELAMINATED ON LOWER SURFACE OUTBOARD FWD CORNER. MAINTENANCE REPAIRED IAW SRM 57-50-6 AND 51-40-6.

Part: RIB — CRACKED (NR 6 LE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT HAS CRACKED RIB AT SS 225 AT AFT CORNER WHERE LOWER CHORD ATTACHES TO RIB. MAINTENANCE REPAIRED IAW SRM 57-50-3 AND 51-30-2.

Part: RIB — CRACKED (NR 4 LE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND NR 4 SLAT HAS CRACKED RIB AT SS 112 LOWER AFT CORNER. MAINTENANCE REPAIRED IAW SRM 57-50-3.

Part: TE SKIN — DELAMINATED (RT TE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE LOWER SURFACE DELAMINATED 63 INCHES FROM OUTBOARD END AND 18 INCHES FROM INBOARD END AROUND AFT FLAP TRACK CUTOUTS. MAINTENANCE REPAIRED IAW SRM 51-40-6.

Part: TRIM TAB — DELAMINATED (LT AILERON)

WHILE IN "D" CHECK, MAINTENANCE FOUND OUTBOARD AILERON TRIM TRAILING EDGE DELAMINATED IN 2 AREAS ON LEFT WING. MAINTENANCE REPAIRED IAW SRM 51-40-6.

Part: TE SKIN — DELAMINATED (RT TE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE DELAMINATED 12 INCHES OUTBOARD OF INBOARD END. MAINTENANCE REPAIRED IAW SRM 51-40-6.

Part: SLAT — CRACKED (NR 6 LE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT INBOARD END CRACKED. MAINTENANCE REPAIRED IAW SRM 51-30-2 AND 57-50-3.

Part: SKIN — DELAMINATED (RT TE FLAP)

WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD AFT FLAP HAS A PREVIOUS REPAIR THAT IS DELAMINATING ON UPPER SURFACE. MAINTENANCE REPAIRED IAW SRM 51-40-6.