N945UP

Part: SLIDE — DISLODGED (COCKPIT)

ESCAPE SLIDE FELL OUT OF HOUSING. REINSTALLED ESCAPE SLIDE.

Part: ACTUATOR — ILLUMINATED (TAIL SKID)

ALL 3 RED GEAR UNSAFE LIGHTS ILLUMINATED ACCOMPANIED BY TAIL SKID DOWN INDICATION. FERRY PERMIT 9007. REMOVED & REPLACED TAIL SKID ACTUATOR. OPS CHECK GOOD AT THIS DATE PER MM 32-71-12-4. PERFORMED MAIN GEAR & NOSE GEAR RETRACTION EXTENSION PER MM 32-32-005, 32-33-005. THIS CLEARS DEFERRAL D333932.

Part: SKIN — CRACKED (CARGO DOOR)

CRACK ON MAIN CARGO DOOR. A/C WILL FERRY TO SDF NR 9184 D 323101 ISSUED. MCD OUTER SKIN APPROX BS 500 UPPER FWD CORNER CRACKED. REMOVED PREVIOUS DOUBLER AND REMOVAL DAMAGED SKIN. OK TO INSTALL QC 0557511/COMPLETED REPAIR SRM 52-00-03 THIS CLEARS D323101.

Part: UPLOCK SWITCH — MISINSTALLED (MLG)

ON GEAR RETRACTION OUT OF BGR, NOSE GEAR AMBER DOOR LIGHT AND TAIL SKID LIGHT DID NOT ILLUMINATE. LIGHTS TESTED OK. UNAIRWORTHY CONDITION OCCURRENCE REPORT RECEIVED FROM SNN. UPLOCK SWITCH LINKAGE HAD BEEN REPLACED IN C CK AT SNN. THE UPLOCK SWITCH LINKAGE HAD TO BE DISCONNECTED AND CORRECTLY INSTALLED. MLG EXTENSION/RETRACTION CARRIED OUT TO VERIFY SYSTEM INTEGRITY. INDICATION SYSTEM TESTED NORMAL PER MM 32-61-01/501 PARA C.

Part: SKIN — DENTED (BS 1183) · airframe 56,277 hrs · 43,775 cycles

INSPECTION TYPE:C GOUGE ON FUSELAGE SKIN AT BS 1183 BETWEEN STR 7R AND 8R. PLEASE GAIN ACCESS TO MAIN CABIN INTERIOR AND REPAIR AREA IAW SRM. DAMAGE EVALUATED AND FOUND TO BE OUTSIDE LIMITS. FASTENERS REMOVED AND DAMAGED AREA CUT OUT. FILLER AND REPAIR DOUBLER FABRICATED. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 56,277 hrs · 43,775 cycles

INSPECTION TYPE:C RIGHT NR 7 SLAT ACTUATOR RAM FWD ATTACHMENT FITTING INBOARD SUPPORT RIB CRACKED. PLS INVESTIGATE AND RECTIFY. SLAT ACTUATOR RIBS I/B AND O/B DISPLACED IAW SRM 51-30-3. HFEC CARRIED OUT AND FWD ATTACH FITTING INBOARD SUPPORT RIB CRACKS CONFIRMED. CRACKS STOP DRILLED. HFEC CARRIED OUT AND 2 ADDITIONAL CRACKS FOUND. O/B WEB REMOVED AND I/B WEB REMOVED. WEBS FABRICATED IAW BOEING DRAWING 65-17306-3. NR 7 SLAT ACTUATOR I/B AND O/B WEBS INSTALLED IAW BOEING DRAWING 65-17306.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 56,277 hrs · 43,755 cycles

INSPECTION TYPE: C AFT CARGO FLOOR SUPPORT BEAM CRACK ON S28 BETWEEN FR 1060 AND 1090 AT SP LICE PLATE FROM RIVET HEAD. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT IAW SRM REF 53-10-5. FABRICATED REPAIR PARTS IAW SRM REF 53-10-5 FIG 4. REPAIR CARRIED OUT IAW SRM REF 53-10-5 FIG4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,775 hrs · 43,351 cycles

C FRAME LEG CRACKED AT BS 294, STR 9/10L. DAMAGED PORTION OF FRAME REMOVED IAW SRM 53-10-4. HFEC CARRIED OUT AROUND CUTOUT: NO DEFECTS FOUND. REPAIR CARRIED OUT IAW 53-10-4.

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, ENGINE NR 2 NACELLE UPPER FRAME CRACKED BETWEEN MID AND AFT HINGE POINTS. FABRICATED FRAME IAW SRM 54-10-06, FRAME REPLACED IAW SRM 51-30-02.

Part: PANEL — ERODED (LT WING) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, LT WING LOWER FIXED L/E PANEL FSS 262 TO FSS 312 ERRODED ALONG L/E AT O/B END. PANEL REMOVED IAW 51-30-2. PANEL DERIVETED FROM BRACKET IAW 51-30-2. FUEL DRAIN PIPES DISCONNECTED IAW MM 29-00-00. PANEL FABRICATED IAW DRG 65-21653. PANEL AND ATTACH BRACKET INSTALLED IAW 51-30-2. PANEL SEALED IAW SRM 20-60-01. FUEL DRAIN PIPES RECONNECTED.

Part: PANEL — DELAMINATED (NR 1 PYLON) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, ENGINE NR 1 PYLON PANEL 5401 IS DELAMINATED INNER SURFACE FWD END ENG NR 1 PYLON PANEL 5401 REPAIRED IAW SRM 51-40-20.

Part: CASTING — CORRODED (AILERON) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, CORROSION ON LEFT O/B AILERON I/B CASTING. CASTING REPLACED IAW SRM 51-30-2.

Part: SKIN — DELAMINATED (RT FORE FLAP) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01.

Part: DUCT — CRACKED (THRUST REVERSER) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, NR 3 ENGINE THRUST REVERSER, SUSPECT CRACK ON INNER SURFACE OF JET PIPE DUCT ON AFT SIDE OF LT LATCH BOX FRAME FASTENERS. REPAIR CARRIED OUT IAW AAAE EO 2004-073-001 R1 UPS ENG FILE 727-78-20015.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE:C LT IB AFT FLAP LWR SKIN DELAMINATION AT IB END AND BELOW NR 7 CARRIAGE. AFT FLAP REMOVED IAW MM 27-51-02. NEW AFT FLAP INSTALLED IAW MM 27-51-02.

Part: WEB — CRACKED (LT MLG WING DOOR) · airframe 55,775 hrs · 43,351 cycles

LT MLG WING DOOR LWR END WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC INSPECTION CARRIED OUT. CRACK CONTAINED IN STOP DRILLED HOLE. REPAIRED IAW 51-40-02.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, CRACK ON LT MLG WING DOOR INNER SKIN AT TE. HFEC CARRIED OUT AND CRACK CONFIRMED. CRACK STOP DRILLED IAW SRM 51-10-1.HFEC CARRIED OUT AND CRACK CONTAINED WITHIN DRILLED AREA. REPAIR CARRIED OUT IAW SRM 52-80-2 FIG 5.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, LT MLG WING DOOR AFT Z-SECTION CRACKED. Z-SECTION REMOVED IAW SRM 51-30-02 Z-SECTION FABRICATED IAW SRM 51-20-1 Z-SECTION INSTALLED IAW SRM 51-30-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BS 304 BETWEEN S8L AND S10L. AFTER BLENDING CORROSION FOUND TO BE EXTENSIVE. ACCESS PROVIDED AND A 1 INCH CRACK FOUND IN UPPER FWD ENTRY DOOR. AREA REPAIRED IAW QUERY RESPONCE AAAE-2004-073-31.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON ANGLE IN RIGHT W/W OUTBOARD OF BS 870 FITTING AT LOWER END. NEW ANGLE FABRICATED & INSTALLED IAW SRM 51-20-1 & SRM 51-30-2.

Part: PANEL — CRACKED (LT MLG WW) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, CRACK FOUND ON SKIN IN LT W/W I/B SKIN JUST BEHIND BRACKET FOR PLUMB BOB. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER IAW SRM 51-40-2. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2.

Part: CROSSOVER TUBE — CRACKED (NR 2 ENGINE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, DURING NDT OF NR 2 ENGINE MOUNTING COMPONENTS THE CROSSOVER STRUT WAS FOUND TO BE CRACKED. REPLACED CROSSOVER STRUT IAW SRM 51-30-02.

Part: BRACKET — CRACKED (WATER SEPARATOR) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, RIGHT WATER SEPARATOR SUPPORT BRACKET CRACKED. REPAIR CARRIED OUT IAW SRM 51-10-6 & 51-40-3.

Part: WEB — CRACKED (RT MLG WING DOOR) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, RT MLG WING DOOR UPPER FWD WEB CRACKED AT AFT END REPAIR CARRIED OUT IAW SRM 51-30-02 & 51-40-3.

Part: HINGE — CRACKED (LT OB AILERON) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, LT OB AILERON OB HINGE FITTING ON AIRCRAFT HAS A SUSPECT CRACK. NDT CARRIED OUT AND CRACK CONFIRMED. LT OB AILERON REMOVED IAW 27-10 -14. OB HINGE REMOVED IAW SRM 51-30-2. NEW HINGE INSTALLED IAW SRM 51-30-2.OB AILERON INSTALLED MM 27-10-14.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, RT I/B AILERON TAB HAS SEPARATION AT TRAILING EDGE AND DELAMINATION AT I/B & O/B ENDS. REPAIR CARRIED OUT IAW SRM 51-40-20 & MM 27-10-05 & 51-80-3.

Part: RIB — CRACKED (NR 6 SLAT) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, NR 6 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. ROD END DISCONNECTED IAW MM 27-81-32. ROD END RIBS DERIVETED IAW SRM 51-30-02. RIBS REMOVED IAW SRM 51-30-02. ON REMOVAL O/B RIB AND CENTER CHANNEL FOUND CRACKED. NEW CENTER CHANNEL, I/B AND O/B RIBS INSTALLED IAW SRM 51-30-02.

Part: ACCESS PANEL — CRACKED (NR 7 SLAT) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, NR 7 SLAT INNER SKIN ACCESS PANEL, EXISTING REPAIR DOUBLER IS CRACKED. NR 7 SLAT INNER SKIN ACCESS PANEL REMOVED FOR ACCESS IAW SRM 51-30-02 & CRACKED DOUBLER REPLACED IAW SRM 51-30-02.

Part: PANEL — DELAMINATED (RT WING) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, PANEL ON LOWER SURFACE OF RT WING L/E FALSEWORK PANEL FSS 195 TO FSS 314 HAS DELAMINATION AT FWD EDGE. PANEL REMOVED IAW SRM 51-10-06. PANEL FABRICATED IAW DRG 65-21653 AND SRM 51-40-9. ON INSTALLATION OF PANEL, FUEL PIPE FOUND TO BE DAMAGED. FUEL PIPE FABRICATED REF CPT 3132. REPLACE FUEL PIPE.

Part: SKIN — DELAMINATED (RUDDER TAB) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, UPPER RUDDER TAB HAS DELAMINATION AT LWR LT SIDE UPPER RUDDER REPLACED IAW MM 27-20-11.

Part: FAIRING — DELAMINATED (TAILCONE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE:C, VERTICAL STAB TIP FAIRING (TAIL CONE) DELAMINATED AT BOTTOM NEAR WEDGE. REPAIR CARRIED OUT IAW SRM 51-40-9 & 51-30-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, ON REMOVAL OF RIGHT CONTROL COLUMN, CRACK FOUND ON SUPPORT ANGLE AT I/B SIDE OF COLUMN CUTOUT IN FLOOR, COMING FROM ANCHOR NUT HOLE. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-30-2.

Part: SKIN — CRACKED (LT WING TIP) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, 0.5 INCH CRACK IN LOWER WING SKIN AT LEFT WING TIP, APPROX 8 INCHES FROM TIP AND JUST FWD OF STRINGER FAIRING. CRACK STOP DRILLED IAW SRM 51-10-1. CRACK CONTAINED WITHIN DRILLED AREA. HOLE DRILLED IN RIB COMMON TO REPAIR SCHEME FOR NDT. HFEC CARRIED OUT ON 8 FASTNER HOLES, NO DEFECTS FOUND. CUT OUT CARRIED OUT IAW EO 2004-073-005. DOUBLER FABRICATED. DOUBLER INSTALLED. ALL AREA REPROTECTED.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,775 hrs · 43,351 cycles

INSPECTION TYPE: C, REPLACE LT WINDOW FRAME AT BS 1100 P/N:65-19850-149. FRAME REPLACED WITH NEW FRAME IAW SRM 51-30-2.

Part: REGULATOR — INOPERATIVE (OXYGEN SYSTEM)

INSPECTION TYPE: PFLT, OXYGEN REGULATOR AT S/O POSITION HAS FLOW IN ALL POSITIONS. REMOVED AND REPLACED S/O OXYGEN REGULATOR, OPS CHECK NORMAL.

Part: DOUBLER — CORRODED (KRUEGER FLAP)

FOUND CORROSION ON NR 3 KRUEGER FLAP EXTENDING UNDER DOUBLER REPAIR R&R REQUIRED. REMOVED AND REPLACED NR 3 KRUEGER FLAP IAW MM 27-81-01.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FWD ENTRY DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-67, OPS CK GOOD. P/N ON 38931-002.

Part: SKIN — CRACKED (BS360 I/B STR.4) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C+SI 5 MM CRACK FOUND PROPAGATING FROM THE SIXTH FASTENER I/B OF STR.4 R AT BS360 AFT SKIN AFT FASTENER ROW. FASTENERS REMOVED IAW SRM 51-30-02. CRACK TRIMED OUT IAW SRM 51-10-06 REPAIR CARRIED IAW EO.B727-5310-1371+DRG.NO.69-62161.

Part: BEAM — CORRODED (HORIZONTAL STAB) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, RT HORIZ STAB UPPER T/E BEAM BETWEEN RIB AT STR 66.50 & STR 99.76 IS CORRODED UNDER RUBSTRIP. BEAM REPLACED IAW DRAWINGS 65-20657, 65-20658, 65-20659, 65-20660-65 22402 & 65-22987

Part: SEAL — CRACKED (NR 6 & SLAT) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, NR 6 & 8 LEADING EDGE SLAT CRACK FOUND AT I/B END UNDER PORK CHOP SEAL. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 5.

Part: FRAME — CORRODED (FAIRING) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, FAIRING 3429 HAS CORRODED FRAME SECTION ABOVE ACCESS PANEL 3420. CUTOUT CORRODED FRAME SECTION, REMOVED IAW SRM 51-30-2. NEW FRAME SECTION FABRICATED IAW SRM 51-20-1 FIG 7 AND SRM 53-50-1 FIG 2. NEW FRAME SECTION INSTALLED IAW SRM 51-30-2.

Part: WEB — CHAFED (LT STAIRWELL) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, LT STAIRWELL HORIZONTAL WEB IS CHAFED UNDERNEATH LT & RT AIRCON. FLOW CONTROL & SOV'S. REPAIR CARRIED OUT IAW SRM 51-40-02.

Part: CARRIAGE — CORRODED (LT WING) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C+SI, NR 3 FLAP CARRIAGE HAS CORROSION AT BASE OF SPINDLE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03 DUE TO CORROSION.

Part: STRINGER — CRACKED (AIRSTAIR) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI CRACK IN AIRSTAIR CENTRE STRINGER AT LWR END OF 2ND BAY FROM TOP OF STAIR REPAIR CARRIED OUT AS REQUIRED IAW SRM 53-10-3

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, SURFACE CORROSION ON FLOORBEAM TOP CAP BS 312 LBL 10 & LBL 24.75. CARRIED OUT REPAIR AT ABOVE LOCATION IAW SRM 53-10-8.

Part: HINGE — CRACKED (NR 11 SPOILER) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, SMALL CRACK ON RT WING UPPER T/E AT SPOILER NR 11 OUTER HINGE CUTOUT. REPAIR CARRIED OUT IAW SRM 57-30-4.

Part: FLANGE — CORRODED (BS 930) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI R/H W/W BS 930 HORIZ. INTERCOSTAL COMMON TO BS 930 FRAME EVIDENCE OF CORROSION ON HORIZ. AND VERTICAL FLANGE REPAIR CARRIED OUT IAW SMRO EO 2003-003-013 UPS ENGINEERING FILE NO. 727-53-20093

Part: SUPPORT — CORRODED (TOILET) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C+SI, CORROSION ON TOILET SUPPORT BEAM BETWEEN BS 328 AND 344. INSTALLED NEW SUPPORT BEAM AT ABOVE LOCATION IAW SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 233 RL 16) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI CORROSION AT FLOOR LEVEL I/B STIFFENER BS 233 APPROX RBL 16 APPROX U NDERNEATH 1ST OFFICERS SEAT SUPPORTS CORROSION REMOVED AND FOUND OUTSIDE LIMITS OF SRM 51-10-6 & 51-10-1 STIFFENER CHANNEL REPLACED IAW SRM 51-30-2

Part: CHANNEL — CRACKED (BS 1263 R/H) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI BS1263 R/H, VENTRAL STAIR TORQUE BOX HORIZ. BEAM IS CRACKED AT I/B U PPER RADIUS CHANNEL REPLACED IAW DRAWING 65C13874& SRM 51-30-02

Part: FITTING — CORRODED (#3 SPOILER) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI ON #3 SPOILER ACTUATING QUADRANT DISCONNECTION #3 SPOILLER SUPPORT F ITTING FOUND TO BE CORRODED BEYOND THE LIMITS REPLACED FITTING IAW DRAWING 65-21622-22 & MM 20-10-05

Part: SUPPORT — CORRODED (BS 850-870 RBL62) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK SUPPORT BS 850 - 870 RBL 62.5 SUPPORT REPLACED IAW SRM 51-30-02

Part: BRACKET — CRACKED (BS 580 S2L) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI BRACKET CRACKED AT MAIN CARGO DOOR SUPPORT BEAM BS 580 STR. 2 L/H REPAIR CARRIED OUT IAW SMRO EO 2003-003-008 UPS ENGINEERING FILE NO. 727-55-20034

Part: FLAP TRACK — CORRODED (NO.3 FLAP TRACK) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C+SI NO.3 FLAP TRACK HAS CORROSION ON PAD B, BETWEEN HOLES G AND F AND AL SO ON THE LWR FLANGE AROUND HOLE G. REPAIRED IAW SMRO EO 2003-003-010 AND EO 2003-003-003.

Part: SKIN — CRACKED (RUDDER TAB) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, LOWER RUDDER TAB HAS AN AREA OF DELAM AT LWR AFT CORNER RT SIDE. SKIN CRACK AND LARGE DENT ON LT SIDE 12TH FROM BOTTOM ON T/E AREA LOWER RUDDER TAB REPLACED IAW MM 27-20-11.

Part: FLAP TRACK — CORRODED (NO.2 FLAP TRACK) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C+SI NO.2 FLAP TRACK HAS CORROSION IN BORE OF HOLE.D. NO.2 FLAP TRACK REPAIRED IAW SMRO EO 2003-003-002

Part: HOUSING — CRACKED (SPOILER ACTUATOR) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, .75 INCH CRACK FOUND IN NR 11 SPOILER ACTUATOR SUPPORT FITTING LWR O/B LUG IN UPPER RADIUS. REPLACED NR 11 SPOILER ACTUATOR SUPPORT CASTING IAW DRAWING 65-17315.

Part: ANGLE — CRACKED (#3 SPOILER.) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C+SI NO.3 SPOILER SUPPORT FITTING I/B FITTING ATTACH ANGLE FOUND TO BE DA MAGED.CRACK FOUND IN LWR. MOUNT BOLT HOLE PROPRAGATING TO EDGE.EXIST ING REPAIR ALSO CRACKED FROM LWR BOLT HOLE TO FREE EDGE. CRACKED ANGLE REMOVED IAW SRM 51-30-2. INSTALLED NEW ANGLE IAW SRM 51-30-2 + DRG.65-16201.

Part: SHEAR TIE — CRACKED (BS 320 BL20R/H) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI FLOOR BEAM SHEAR TIE CRACKED AT BS 320 APPROX AND BL 20 R/H FLOOR BEAM SHEAR TIE REPAIRED AT BS 320 AND BL 20 R/H IAW SRM 53-10- 3 FIGURE 6

Part: STRUCTURE — DAMAGED (NR 1 SPOILER) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, NDT CARRIED OUT ON SPOILERS, SPOILER NR 1 FOUND TO HAVE CORE DAMAGE AND WATER INGRESSION. SPOILER REPAIRED IAW MM 27-61-01 & SRM 51-40-5.

Part: STRUCTURE — DAMAGED (NR 9 SPOILER) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, NDT CARRIED OUT ON SPOILERS, SPOILER NR 9 FOUND TO HAVE CORE DAMAGE. REPAIR CARRIED OUT IAW SRM 51-40-5.

Part: WINDOW FRAME — CRACKED (BS 1100 L/H S12) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI CRACK ON WINDOW FRAME BS 1100 L/H STR. 12 CRACK STOP DRILLED IAW SRM 51-10-1 SEE SMRO EO 2003-003-009 FOR REPAIR INSTRUCTION. UPS ENG. FILE NO. 727-53-20092

Part: SHEAR TIE — CRACKED (BS 322 BL 0) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI FLOOR BEAM SHEAR TIE CRACKED AT BS 322 APPROX AND BL0 FLOOR BEAM SHEAR TIE AT BS 322 AND BL 0 REPAIRED IAW SRM 53-10-8 FIG 6

Part: BRACKET — CRACKED (HOR STAB R/H) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C+SI R/H HOR-STAB,REAR SPAR,T-BRACKET ON REAR SPAR AT ELEV.RIB ST.66.50 I S CRACKED. BRACKET REMOVED IAW SRM 51-30-2 AND DRG.NO.65-16876. NEW BRACKET FITTED IAW SRM 51-30-2 AND DRG. NO.65-16876.

Part: BRACKET — CORRODED (BS 610 S28L/H) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI BODY FAIRING SUPPORT ANGLE BRAKCET CORRODED UNDER ANCHOR NUT AT BS 6 10 S28 L/H BRAKCET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-1 FIG. 7 & SRM 53-50-1 FIG 1. INSTALLED IAW SRM 51-30-02

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE: C&SI, CORROSION ON FRAME AT INTERSECTION WITH NLG WW & BS 300 RT SIDE. REPAIR CARRIED OUT IAW SRM 51-10-6, MM 20-40-00, SRM 51-30-02, & DRAWING 6518915.

Part: SKIN — CRACKED (BS 360 S4R) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI 5MM CRACK FOUND PROPAGATING FROM THE FASTENER I/B OF STR.4R AT BS 36 0 AFT SKIN AFT SIXTH FASTENER ROW REPAIR CARRIED OUT IAW EO B727-5310-1371 7 DRAWING 69-62161

Part: FRAME — CRACKED (BS 930 R/H W/W) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI CRACK FOUND ON BS 930 FRAME R/H W/W REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-04 FIG 1, 53-10-3 FIG 1, DRAWING 65C15732, 65-16336 AND SRM 51-30-05

Part: HINGE — CRACKED (#13 SPOILER PANE) · airframe 55,290 hrs · 42,912 cycles

INSPECTION TYPE:C&SI #13 SPOILER PANEL I/B HINGE CRACKED REMOVED #13 SPOILER PANEL IAW MM 27-61-01 . REPLACED I/B HINGE IAW O HM 57-53-01 REPLACED I/B CENTER SPOILER HINGE BEARING DUE TO WEAR IA W OHM 57-53-01 PG 402. INSTALLED #13 PANEL IAW MM 27-61-01

Part: SLIDE — LOOSE (ENTRY DOOR)

INSPECTION TYPE:N/A FE KNOCKED THE SLIDE OFF THE DOOR WHILE CLOSING REINSTALLED SLIDE

Part: SUPPORT BRACKET — CRACKED (#6 KREUGER FLAP) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C #6 KREUGER FLAP ACTUATOR, BASE MOUNT SUPPORT BRACKET IS CRACKED ON O UTBOARD SIDE. #6 KREUGER FLAP ACTUATOR REMOVED IAW MM BASE MOUNT SUPORT BRACKET FABRICATED AND INSTALLED.

Part: FRAME — CRACKED (BS 910LH) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C CRACK IN BS 910 FRAME L/H BELOW FLOOR LEVEL REPAIRED IAW DWG 65C27194

Part: TRUNNION — CORRODED (RT MLG) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C, RT MLG TRUNNION FITTING HAS CORROSION AND SUSPECT CRACKING AROUND INBD SPECIAL STUD HOLE ON INBD FLANGE. TRUNNION FITTING REPLACED.

Part: BRACKET — CRACKED (#8GRND SPOILER) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C #8 GRND SPOILER INBD END HINGE , CASTING ATTACHED TO MLG BEAM WHICH SUPPORTS THE END HINGE THROUGH A SUPPORT ROD IS CRACKED. REPLACED BRACKET IAW SRM 51-30-02. BRACKET REPLACED WITH ORIGINAL BO LTS.

Part: FITTING — CRACKED (TAILSKID) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C TIAL SKID BAY L/H UPPER TIE LINK AFT FITTING, EVIDENCE OF CRACK ON V ERTICAL FLANGE BETWEEN FASTENERS. FITTING REPLACED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C, AFT PRESSURE BULKHEAD BS 1183 CRACK OF FWD FLANGE OF BL 17.8 LEFT VERTICAL BEAM AT WL 273 APPROX. REPAIRED/ MODIFIED PER EO B727-5310-11743-B APP C AND E.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C, NR 5 FLAP TRACK FWD ATTACH LUG HAS CORROSION ON BORE LANDING GEAR FWD TRUNNION SUPPORT BEARING PIN. ATTACH LUG REPLACED.

Part: WEB — CRACKED (BS612.9) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C ON INSPECTION OF MCD LATCH FITTINGS BY NDT, CRACK FOUND IN FRAME WEB CLEAT AT BS 612.9 DAMAGED AREA TRIMMED OUT AND REPAIRED IAW SRM 51-40-2

Part: WINDOW POST — CRACKED (F+N WINDOW POST) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C CRACK FOUND IN F+N WINDOW POST ON SKIN DOUBLER ATL/H WINDOW POST AT WINDOW CUTOUT RADIUS POINT E REPAIRED IAW UPS EO B727-5310-0012

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C, CRACK FOUND IN SKIN DOUBLER AT F+N WINDOW POST RT AT WINDOW CUTOUT, RADIUS AT POINT E THROUGH XRAY INSPECTION. REPAIR CARRIED OUT PER UPS EO B727-5310-0012 APPENDIX D.

Part: SKIN PANEL — CRACKED (BS1343 WL246.5R) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C CRACK IN SKIN BS 1342.4 AT WL246.5R CRACKED REMOVED BY BLENDING MATERIAL. DAMAGED AREA REPAIRED IAW SRM5 3-30-3FIG3A USING 2024T3.050 AND .040.

Part: RIB — CRACKED (L/E SLAT) · airframe 54,338 hrs · 42,065 cycles

INSPECTION TYPE:C, NUMBER ONE SLAT HAS CRACK IN RIB O/B OF I/B TRACK. REPAIRED IAW SRM 57-50-3.

Part: SKIN — SPLIT (FLAP TRACK)

INSPECTION TYPE:C, NR 2 FLAP TRACK MID FAIRING, SKIN SPLIT AT I/B FWD SIDE. NR 2 FLAP TRACK MID FAIRING REPAIRED IAW SRM 51-40-20.

Part: CASTING — CRACKED (FLAP TRACK)

INSPECTION TYPE:C, NR 8 FLAP TRACK, MID FAIRING FWD TRACK SUPPORT CASTING SUSPECT CRACKS AREA PAINT STRIPPED, CASTING FOUND CRACKED CASTING REPLACED IAW DRAWING NR 65-21796 AND SRM 51-30-2.

Part: SPLICE — MISMANUFACTURED (BS 735 - 740)

INSPECTION TYPE:C DUE TO LACK OF EDGE DISTANCE ON FASTENER HOLES ON NEW BS 740 FITTING. CARRY OUT SKIN SPLICE REPAIR FROM BS 735 TO BS 740 S17R TO S24R. SKIN SPLICE REPAIR AT BS 735 TO BS 740 T/H STR 17R TO STR 24R CARRIED OUT IAW SMRO EO 2000-001-02 UPS ENGINEERING FILE NR 727-53-2215.

Part: CASTING — CRACKED (FLAP TRACK)

INSPECTION TYPE:C, NR 2 FLAP TRACK MID FAIRING, TRACK FWD SUPPORT CASTING, SUSPECT CRACKS CASTING FOUND CRACKED IN AREA PAINT STRIPPED. CASTING REPLACED IAW DRAWING NR 65-21796 AND SRM 510.

Part: BRACKET — DAMAGED (BS 1110)

INSPECTION TYPE:C SUPPORT BRACKET DAMAGED AT BS 1110 STRINGER 28 RT. SUPPORT BRACKET REPLACED IAW SRM 51-10-02 AND 51-30-02.

Part: SKIN — DELAMINATED (AILERON)

INSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT O/B AILERON TE AREA JUST O/B OF AILERON TAB. REPAIRED IAW SRM 510 FIG 40.

Part: BRACKET — CORRODED (BS 312)

INSPECTION TYPE:C DURING ACCOMPLISHMENT OF EVACUATION SLIDE FLOOR MOUNTED BRACKET INSTALLATION CORROSION WAS DISCOVERED OUTSIDE LIMITS AT BS 312 LBL 46. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE:C, BS 740 FITTING RT, CRACK ON LWR FLANGE OF FITTING. FITTING REPLACED IAW EO B727-5310-7477-E AND SMRO EO 2000-001-02 UPS ENGINEERING FILE NR 727-53-2215.

Part: BALANCE PANEL — CORRODED (LT HORIZ STAB)

INSPECTION TYPE:C SURFACE CORROSION ON NR 5 BALANCE PANLE LT STAB. BALANCE PANEL REMOVED AND REPLACED IAW MM 27-30-21.

Part: FRAME — CRACKED (BS 940)

INSPECTION TYPE-N/A, CRACK FOUND AT BS 940 FRAME FITTING LT. REPLACED PER UPS EO B727-5310-4501.

Part: FITTING — CRACKED (BS 520)

INSPECTION TYPE-C, DURING INSPECTION OF OF BS 520, A CRACK WAS DISCOVERED IN LATCH SUPPORT FITTING. LATCH SUPPORT FITTING REPLACED IAW EO B727-5310-4501, APPENDIX C.

Part: BEAM — CORRODED (HORIZ STAB)

INSPECTION TYPE-C, CORROSION ON HORIZONTAL STAB TRAILING EDGE UPPER SURFACE AT STAB STATION 188.65 LT. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-19-008, UPS ENGINEERING FILE NUMBER 727-55-0372.

Part: WEB — CRACKED (BS 1381)

INSPECTION TYPE: C, CRACK ON WEB ABOVE NR 2 ENG HORIZONTAL FIREWALL RT SIDE AT STA 1381. WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: MOUNT — CORRODED (NR 1 ENGINE)

INSPECTION TYPE-C, PITTING CORROSION ON BORE OF HOLES ON NR 1 ENGINE INBD FWD MOUNT FITTING (FOUR HOLES). REPAIR CARRIED PER SRS ENGINEERING ORDER 98-19-001, REF UPS ENGINEERING FILE NR 727-71-0069 AND SRS ENGINEERING ORDER 98-19-003, REF UPS ENGINEERING FILE NR 727-71-0067.

Part: SKIN — CORRODED (BS 1080-1183)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER, BS 1120 BETWEEN S20R AND S19R. ON FURTHER INVESTIGATION, EXTESNIVE CORROSION DISCOVERED, SKIN PANEL. REMOVED BETWEEN BS 1183 AND BS 1080, STR 14 TO 209 RT. NEW PANEL AND DOUBLERS FABRICATED AND INSTALLED IAW SRS EINGEERING ORDER 98-19-00 5, REF UPS ENGINEERING FILE NR 5330-2041.

Part: BRACKET — CRACKED (RT ELEVATOR)

INSPECTION TYPE:C ANGLE BRACKET CRACKED ON RT ELEVATOR AFT OF REAR SPAR INBD OF NR 5 TAB HINGE. ANGLE BRACKET REPLACED IAW DRAWING NO 69-19144.

Part: MOUNT — CORRODED (NR 3 ENGINE)

INSPECTION TYPE-C, PITTING CORROSION ON BORE OF HOLES ON NR 3 ENGINE INBD FWD MOUNT FITTING (FOUR HOLES). REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-19-002, REF UPS ENGINEERING FILE NUMBER 727-71-0070, AND SRS ENGINEERING ORDER 98-19-00 4, REF UPS ENGINEERING FILE NR 727-71-0068.

Part: SKIN — CORRODED (BS 1048)

INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER AT BS 1048, STR 18 RT. REPAIR TO SKIN CARRIED OUT IAW SRS ENGINEERING ORDRE 98-19-006, REF UPS ENGINEERING FILE NR 727-53-2042.

Part: SLAT — DAMAGED (ACTUATOR)

INSPECTION TYPE:C, NR 5 SLAT O/B ACTUATOR RIB DAMAGED. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SLAT — DAMAGED (NR 5 LE SLAT)

INSPECTION TYPE:C, NR 5 SLAT I/B ACTUATOR RIB DAMAGED. REPAIR CARRIED IAW SRM 51-40-2.

Part: STRINGER — CRACKED (WS 686.5)

INSPECTION TYPE-D, NR 12 VENT STRINGER TO WING RIB TAB LT WING WS 686.5 IS CRACKED. REPAIRED PER SB B727-57A159.

Part: SUPPORT — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE: D. FLAP TRANSMISSION SUPPORT FITTING TRANSMISSION ATTACH MOUNTINGS CORRODED. TRANSMISSION SUPPORT REPLACED IAW SRM 51-30-2. FITTING KIT 65-95600- 1791.

Part: GEAR BEAM — CORRODED (LT MLG)

INPECTION TYPE-D, SUSPECT CORROSION IN FLAP ATTACH HOLES OF LT LANDING GEAR BEAM. REPAIRED IAW SRS EO 97-02-021, UPS FILE NR 727-57-1782.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-D, CORROSION AND CRACKING FOUND ON BS 740 LT TERMINAL FITTING. BS 740 LT FITTING REPLACED IN ACCORDANCE WITH UPS EO B727-5310-7477-C. FUSELAGE SKIN BETWEEN S17L AND S24L REPAIRED IAW SRM 53-30-3 FIG 3A AND FIG 5 TO PREVENT INSTALLATION OF O/S FASTENERS IN SKIN.

Part: JACKSCREW — WORN BALLNUT (NR 6 TE FLAP)

INSPECTION TYPE-D, NR 6 FLAP JACKSCREW BALLNUT HAS EXCESSIVE PLAY. JACKSCREW REPLACED IAW OHM 27-54-03.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, RT WING I/B FLAP O/B CARRIAGE CORROSION IN BORE OF SPINDLE. NR 6 FLAP CARRIAGE ASSY REPLACED PER MM 27-51-03.

Part: INTERCOSTAL — CORRODED (BS 227)

INSPECTION TYPE-D, CORROSION FOUND ON FUSELAGE FRAME INTERCOSTAL ANGLE BS 227 BETWEEN S30L AND S30R. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS PER SRM 51-10-6. INTERCOSTAL ANGLE REPLACED IAW SRM 51-30-2 AND 51-10-1.

Part: INTERCOSTAL — CORRODED (BS 211-219)

INSPECTION TYPE-D, CORROSION FOUND ON FRAME INTERCOSTAL S26R BETWEEN BS 211 AND 219. INTERCOSTAL FOUND TO BE BEYOND REPAIR PER SRM 51-10-6. INTERCOSTAL REPLACED PER SRM 51-30-2 AND 51-10-1.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-D, CORROSION ON FLAP TRACK AT AFT MATING SURFACE WITH AUX SPAR. ALSO, CORROSION IN BOLT HOLES, NR 6 FLAP TRACK. REPAIR CARRIED OUT PER SRS EO 97-02-023, REF UPS ENGINEERING FILE NR 727-57-1783.

Part: CASTING — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 7 FLAP TRACK FWD ATTACH CASTING ON WING HAS CORROSION. REPAIR CARRIED OUT IAW SRS EO 97-02-016, REF UPS ENGINEERING FILE NR 727-57-1775.

Part: FLAP TRACK — CORRODED (NR 3/4)

INSPECTION TYPE-D, NR 3 AND NR 4 FLAP TRACK AFT SUPPORT HOLES CORRODED. NR 3 FLAP TRACK REPAIRED PER OHM, NR 4 FLAP TRACK CORROSION REMOVED IAW SRM 51-10-6. HFEC PER NDT PT6 51-00-00 F13 AND MAG PARTICLE PE RBD6072 CARRIED OUT, NO CORROSION FOUND. REPAIR CARRIED OUT TO NR 4 FLAP TRACK PER BOEING INSTRUCTIONS SRV-SNN-97-0020RR, SRS EO 97-02- 022 AND UPS EO B727-5750-8994-A.

Part: GEAR BEAM — CORRODED (RT MLG)

INSPECTION TYPE-D, FLAP TRACK ATTACH HOLES ON LANDING GEAR BEAM HAVE EVIDENCE OF CORROSION NR 5 TRACK. REPAIR CARRIED OUT IAW SRS EO 97-02-020, UPS FILE NR 727-57-1767.

Part: BOLT — CORRODED (TE FLAP)

INSPECTION TYPE-D, NR 7 FLAP TRACK OUTER BOLT AT REAR SPAR CORRODED. BOLT REPLACED IAW MM 27-51-31.

Part: CARRIAGE — CORRODED (NR 8 FLAP TRACK)

INSPECTION TYPE-D, RT WING OUTBOARD FLAP OUTBOARD CARRIAGE, CORROSION IN BORE OF SPINDLE. NR 8 FLAP TRACK CARRIAGE ASSEMBLY REPLACED IAW MM 27-51-13.

Part: FITTING — CORRODED (BS 740)

INSPECTION TYPE-D, CORROSION UNDERSIDE OF LT BS 740 FITTING. FITTING REPLACED PER EO B727-5310-7477-C, REF NRC 502825 / MRR UPS97 221859.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LT INBOARD FLAP OUTBOARD CARRIAGE CORROSION IN AREA OF LARGE BEARING AREA THRUST WASHER OF CARRIAGE SPINDLE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LT OUTBOARD FLAP OUTBOARD CARRIAGE, CORROSION IN AREA OF LARGE BEARING AREA THRUST WASHER OF CARRIAGE. NR 1 FLAP CARRIAGE REPLACED PER MM 27-51-13, REF NRC 502511 MRR UPS97 221950.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LT OUTBOARD FLAP INBOARD CARRIAGE, SUSPECT INTERNAL CORROSION IN SPINDLE BORE. NR 2 FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: CARRIAGE — CORRODED (NR 5 FLAP TRACK)

INSPECTION TYPE-D, CORROSION ON RT INBD FLAP TRACK CARRIAGE SPINDLE AT END OF TAPER, RT WING NR 5. NR 5 FLAP TRACK CARRIAGE ASSY REPLACED IAW MM 27-51-03, REF NRC 502622 MRR UPS97221896.

Part: CARRIAGE — CORRODED (NR 5 FLAP TRACK)

INSPECTION TYPE-D, CORROSION ON THRUST BEARING COLLAR ON RT INBD FLAP TRACK INBOARD CARRIAGE RT WING. NR 5 FLAP TRACK CARRIAGE ASSY REPLACED IAW MM 27-51-03.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LEFT HAND INBOARD FLAP INBOARD CARRIAGE CORROSION IN AREA OF LARGE BEARING AREA THRUST WASHER AND SMALL BEARING AREA OF CARRIAGE SPINDLE. NR 4 FLAP CARRIAGE ASSY REPLACED IAW MM 27-51-03.

Part: DOOR BEAM — CORRODED (BS 480-620)

INSPECTION TYPE-D, CORROSION FOUND ON UPPER BEAM OF MAIN CARGO DOOR AT HINGE LINE UNDER WEATHER SEAL. BEAM REPLACED, NO REPLACEMENT BEAMS AVAILABLE. BEAM FABRICATED LOCALLY IN TWO SECTIONS TO FACILITATE HEAT TREAT AND SPLICED PER BOEING INSTRUCTIONS, REF UPS ENGINEERING FILE NR 727-52-0176 AND BOEING DRAWING 65-25337.

Part: INTERCOSTAL — CRACKED (BS 840- 870)

INSPECTION TYPE-D, FLOOR SUPPORT HAS CRACKED SUPPORT BRACKETS BETWEEN BS 840 TO 870 AND LBL 24.5 AND 45.5. INTERCOSTAL REPLACED PER BOEING DRG 65-46611 AND SRM 51-30-2.

Part: FLOOR SUPPORT — BROKEN (BS 760)

INSPECTION TYPE-D, FLOOR SUPPORT JUST FORWARD OF BS 760 BETWEEN LBL 45.5 AND 62.5 HAS BROKEN ATTACH ANGLE. FLOOR SUPPORT REPLACED IAW SRM 51-30-2.

Part: INTERCOSTAL — DAMAGED (BS 303.9)

INSPECTION TYPE-D, UPPER CHORD OF INTERCOSTAL AT LOCATION BS 303.9 LBL 40 DAMAGED. NEW INTERCOSTAL FABRICATED AND INSTALLED PER BOEING DRG 65-17593 AND INSTALLED PER SRM 51-30-2.

Part: CASTING — CORRODED (NR 5 FLAP TRACK)

INSPECTION TYPE-D, EVIDENCE OF CORROSION ON NR 5 FLAP TRACK FWD ATTACH CASTING ON WING. CORROSION REMOVED IAW SRM 51-10-6. HFEC PER NDT PT6 51-00-00 F13 AND MPI PER BS6072 CARRIED OUT, NO FURTHER CORROSION. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS, REF UPS ENGINEERING FILE NR 727-57-1773.

Part: BOTTLE PIN — CORRODED (BS 740)

INSPECTION TYPE-D, EVIDENCE OF CORROSION ON LEFT HAND FRONT SPAR TO BODY BOTTLE PIN AND ASSOCIATED BUSHING. BOTTLE PIN REPLACED PER UPS EO B727-5310-7477 ITEM 30F. NEW BUSHING INSTALLED, BS 740 FITTING PER EO B727-5310-7477 ITEM 30D, REF NRC 502825 / MRR UPS97221859 FOR BS 740 TERMINAL FITTING CHANGE.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LT OUTBOARD FLAP INBOARD CARRIAGE CORROSION IN AREA OF LARGE BEARING AREA THRUST WASHER OF CARRIAGE SPINDLE. NR 2 FLAP CARRIAGE REPLACED PER MM 27-51-13, REF NRC 502507 MRR UPS97 221949.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE-D, LT OUTBOARD FLAP OUTBOARD CARRIAGE, SUSPECT CORROSION IN BORE OF CARRIAGE SPINDLE. NR 1 FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: FITTING — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LOWER SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED IAW SRM 51-10-6, HFEC C/O PER NDTPT6 51-00-00 F13, MPI C/O PER C/O PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 1 WING MOUNTED FLAP TRACK ATTACH FITTING IAW UPS ENGINEERING FILE NR 727-57 -1771.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 2 FLAP TRACK FWD ATTACH POINT LUGS CORRODED, BOLT CORRODED AND BUSHINGS WORN. CORROSION REMOVED IAW SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI C/O PER BS6072, NO CORROSION FOUND. REPAIR TO NR 2 FLAP TRACK FORWARD ATTACH LUGS CARRIED OUT PER BOEING INSTRUCTIONS UPS ENGINEERING FILE NR 727-57-1769.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE-D, NR 1 FLAP TRACK FORWARD ATTACH POINT LUG CORRODED, BOLT CORRODED AND BUSHINGS WORN. CORROSION REMOVED IAW SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI C/O PER BS6072, NO CORROSION FOUND. NR 1 FLAP TRACK FORWARD LUGS REPAIRED PER BOEING INSTRUCTIONS UPS ENGINEERING FILE NR 727-57-17 70.

Part: FITTING — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LWR SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED PER SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI CO PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 2 WING MOUNTED FLAP C/O PER UPS ENGINEERING FILE NR 727-57-1772.

Part: SKIN — CORRODED (BS 441-521)

INSPECTION TYPE-D, CORROSION FOUND IN CROWN SKIN BS 441 TO 521 S4R TO S10L. CROWN SKIN REPLACED, NO OEM SKINS AVAILABLE. SKIN REPLACED IN SECTIONS PER BOEING INSTRUCTIONS, REF UPS ENGINEERING FILE NR 727-53-1855.

Part: SHIM — CORRODED (NR 3 FLAP TRACK)

INSPECTION TYPE-D, SHIM CORRODED ON NR 3 FLAP TRACK MID ATTACH POINT. NEW SHIM (P/N 69-11179-10) FITTED PER SRM 51-20-1.

Part: FLOOR BEAM — CORRODED (BS 344)

INSPECTION TYPE: D. FLOOR BEAM CORRODED AT BS 344. UPPER T-SECTION REPLACED BETWEEN RBL 70 AND LBL 70.

Part: SUPPORT — CORRODED (NR 9 SPOILER)

INSPECTION TYPE-D, NR 9 SPOILER SUPPORT CASTING HAS CORROSION ON PERIPHERY OF BOLT HOLE SPOILER CASTING. REPLACED PER BOEING DRAWING 65-16216.

Part: SUPPORT — CORRODED (BS 310-350)

INSPECTION TYPE: D. CORROSION FOUND ON FWD LAVATORY PARTITION SUPPORT RUNNING FROM BS 310 -BS 350 AT RBL 16 APPROX FLOOR LEVEL. NEW TOP-HAT SECTION INSTALLED PER SRM 51-30-2. FABRICATED FROM BAC 15 10-335 EXTRUSION.

Part: SUPPORT — CORRODED (NR 7 SPOILER)

INSPECTION TYPE-D, NR 7 SPOILER SUPPORT CASTING HAS CORROSION ON PERIPHERY OF BOLT HOLE. SPOILER CASTING REMOVED AND REPLACED IAW BOEING DRAWING 65-16216.