N944UP

Part: SLIDE — OUT OF POSITION (PAX DOOR)

INSPECTION TYPE: N/A MAIN ENTRY DOOR ESCAPE SLIDE FALLS OUT OF ITS CONTAINER WHEN DOOR IS MOVED. FOUND COMPARTMENTAL COVER LATCH CABLE DISCONNECTED. REPAIRED IAW 25-60-14-2. OPS CK GOOD.

Part: SLIDE — DISLODGED (COCKPIT)

ESCAPE SLIDE FELL OUT OF STORAGE HOUSING IN FLIGHT. ATTEMPTED TO RESTORE SLIDE. REPACKED SLIDE ASSY AS REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C DURING REMOVAL OF FASTENERS TO FACILITATE THE FLOOR SUPPORT REPAIR FOR NRC 100734 CRACK FOUND ON FRAME FOR INNER RADIUS BS1050 RBL 12. CRACKED FRAME AT ABOVE LOCATION REPAIRED IAW SRM 53-10-02 AND SRM 51-4 0-3

Part: SPAR — CRACKED (LT ELEVATOR) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C ON INSP CRACK DETECTED ON THE LEFT ELEVATOR REAR SPAR STA 138 APPROX. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. ELEVATOR REMOVED IAW MM 27-30-01. NEW ELEVATOR INSTALLED IAW MM 27-30-01. ELEVATOR FRICTION CHECK CARRIED OUT IAW MM 27-30-01 PAGE 409 STEP H. ADJ/TEST CARRIED OUT IAW MM 27-30-01. SYSTEM RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C FLOOR SUPPORT FOUND TO BE CRACKED AT BS 1060 LBL 6. DAMAGE CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30-02. REPAIR PARTS FABRICATED IAW SRM 53-10-05 AND REPROTECTED IAW SRM 51-10- 02. REPAIR PARTS INSTALLED IAW SRM 51-30-02.

Part: SKIN — CRACKED (AFT AIRSTAIRS) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C SUSPECT SKIN CRACK IN AFT AIRSTAIRS SKIN AT THE NR 8 STEP FROM THE BOTTOM POSITION. CARRY OUT NDI AND RECTIFY AS NECESSARY. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONFIRMED, ENDS MARKED. REPAIR CARRIED OUT IAW SRM 51-30-2 & 52-10-2.

Part: WEB — CRACKED (AFT AIRSTAIRS) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C CRACK ON THE LEFT WEB IN THE AFT AIRSTAIRS AREA MARKED. REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C AFT CARGO DOOR SUSPECT CRACK ON FRAME AT UPPER AFT DOOR STOP. AREA CLEANED AND REINSPECTED, CRACK CONFIRMED VISUALLY AT AFT UPPER DOOR STOP CUTOUT. DUE TO EXCESSIVE WORK REQUIRED TO REPAIR, DOOR TO BE REPLACED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C AFT CARGO BAY CRACK ON FLOOR SUPPORT AT BS 1060 RBL 0. DAMAGED AREA CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30 -02. REPAIR PARTS FABRICATED IAW SRM 53-10-05. REPAIR PARTS REPROTECTED IAW SRM 51-10-02. REPAIR PARTS INSTALLED IAW SRM 53-10-05 AND 51-30- 02

Part: WEB — CRACKED (AFT AIRSTAIRS) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C AFT AIRSTAIRS RT LIGHTENING HOLE CRACKED. AREA MARKED, PLS REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C AFT CARGO BAY BS 1110 RBL20 FLOOR SUPPORT CORRODED AT ANCHOR NUTS LOCATION. TO GAIN ACCESS FLOOR PANEL AND SCUFF PLATE AT CARGO DOOR CUT OUT REMOVED IAW SRM 51-30-02. DAMAGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10* 0-01. DAMAGED SECTION REMOVED IAW SRM 51-40-4. SCUFF PLATE RE-INSTALLED IAW SRM 51-30-02. FLOOR PANEL RE-INSTALLED IAW SRM 51-30-02

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C DURING RECTIFICATION OF NRC 100332 ADJACENT ANGLE OF FWD CARGO BLKD UP PER SECTION BS 680 RBL 30 TO 40 FOUND TO BE CORRODED AT ANCHOR NUT LOCATIONS. ON CLEAN UP CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AFT BLKD ANGLE IAW SRM 51-30-2. REPLACED BLKD ANGLE IAW SRM 51-20-2 & 51-30-2.

Part: SUPPORT ANGLE — CRACKED (RAM AIR INLET) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C BS660 LT CRACK ON OB SUPPORT ANGLE FOR RAM AIR INTAKE DUCTING AT FASTENER LOCATION. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-02. FABRICATED SUPPORT ANGLE AND HEAT TREATED IAW SRM 51-20-1. INSTALLED SUPPORT ANGLE IAW SRM 5 1-30-02.

Part: SPAR — CRACKED (ELEVATOR) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C X-RAY INSPECTION HAS DETECTED 2 SUSPECT CRACKS ON INSPAR RIBS LOCATED BETWEEN ELEVATOR STATION 99.50-136.50 DISPLACED UPPER ELEVATOR SKIN FROM BS 99.5 TO BS 136.5 IAW SRM 51-30- 02 AND REMOVED REPAIR DOUBLER FROM LOWER SKIN. HFEC CARRIED OUT ON THE ABOVE AREA IAW B727-NDTM 51-00-00 PT 6 FIG 4. 1 CRACK CONTAINED WITHI N PREVIOUSLY STOP DRILLS. NO OTHER DEFECTS FOUND. ELEVATOR BEYOND ECO NOMIC REPAIR. REF NRC 100783 FOR REPLACEMENT AND MOR

Part: RIB — CRACKED (LT ELEVATOR) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C X-RAY INSP DETECTED ONE SUSPECT CRACK ON THE LT ELEVATOR INTERNAL RIB LOCATED BETWEEN ELEV STA 179.50 - 205.50. ELEV BEYOND ECONOMIC REPAIR REF NRC 100783 FOR REPLACEMENT OF LT ELEVATOR.

Part: SUPPORT — CHAFED (FUSELAGE) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C ON REMOVAL OF FLOW VENTURI SENSE LINE CROSS SUPPORT STRUCTURAL MEMBER AT LBL 40 BETWEEN BS 1203 AND 1223 FOUND CHAFFED. CROSS STRUCTURAL MEMBER REMOVED IAW SRM 51-30-02. REPLACEMENT REQUIRED. INSTALLED NEW CROSS STRUCTURAL MEMBER IAW SRM 51-30-02.

Part: CASTING — CRACKED (FOREFLAP) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C LEFT O/B FOREFLAP I/B SECTION HAS CRACKS FROM FASTENER HOLES. PAINT STRIPPED AREA IAW MM 51-20-01. HFEC INSP CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. RESULT - CRACK CONFIRMED. FOR FLAP REPLACEMENT REF NRC 100295 DUE TO I/B CASTING NOT AVAILABLE.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 53,598 hrs · 41,182 cycles

INSPECTION TYPE:C NR 9 SPOILER DELAM ON LOWER SURFACE AT O/B FWD CORNER. DELAMINATED SKIN REMOVED AT O/B FWD CORNER IAW SRM 51-40-20. DELAM LIMITS FOUND TO BEYOND ECONOMIC REPAIR. SPOILER REPLACED.

Part: LIGHT — FAILED (ENTRY EMER LIGHT)

MAIN ENTRY EMERGENCY LIGHT DIM. REPLACED LIGHT ASSEMBLY. REF 33-50-67.

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING WEEKEND CK FOUND MAIN ENTRY EMERGENCY LIGHTS VERY DIM UPON TEST ING. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-50-01. F/C OK.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, E/E FLOOR PANEL RIGHT SIDE BS 440 TO 400 HAS ONE CRACK. CRACK STOP DRILLED IAW 51-10-1. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACK CONTAINED. AREA REPAIRED IAW SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NOSE WHEEL WELL) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, LT NOSE WHEEL WELL HAS CRACKS ON FASTENER ROW, BS 243, 4 INCHES BELOW FWD PRESSURE PANEL OPENING. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACKS CONFIRMED. FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE:C, SUSPECT CRACK FROM RIGHT TERMINAL FITTING FOR STABILIZING LINK LWR IN TA TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02.

Part: FITTING — CRACKED (TAIL SKID) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE:C, SUSPECT CRACK FROM LT TERMINAL FITTING FOR STABILIZING LINK LWR IN TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02.

Part: BOLT — DAMAGED (NR 3 ENGINE) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, NR 3 ENGINE FWD AND AFT CRANE BEAMS SHOULDER BOLTS HAVE CAD PLATING DAMAGE. BOLTS REPLACED IAW MM 71-10-32.

Part: SKIN PANEL — CORRODED (LT ELEVATOR) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, SURFACE CORROSION ON LT ELEVATOR LOWER SKIN AT BUTT JOINT BETWEEN 5TH AND 6TH ACCESS PANELS FROM OUTBOARD. CORROSION REMOVED IAW SRM 51-10-1. BLEND OUT AREA FOUND TO BE WITHIN LIMITS IAW SRM 55-20-1. AREA REPROTECTED IAW SRM 51-10-2.

Part: PANEL — CRACKED (NLG WW) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE:C, HULL PRESSURE LEAK IN NLG WHEEL WELL CEILING PANEL (DUE TO CRACKING) AT BS 260 LBL 20. DAMAGED AREA REMOVED AS REQUIRED IAW SRM 51-40-2. HFEC CARRIED OUT - NO DEFECTS FOUND. REPAIR PARTS FABRICATED IAW SRM 51-40-2. REPAIR PARTS INSTALLED IAW SRM 51-40-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON RIGHT 950 FITTING HORIZONTAL WEB WL 202 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-06, 51-10-02 & AAAE EO 2004-085-001. UPS ENGINEERING FILE 727-53-20166.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,763 hrs · 40,573 cycles

INSPECTION TYPE: C, EVIDENCE OF CRACK ANGLE FITTING RIGHT SIDE ON SHELF MID WAY UP 950 AFT RIGHT WALL. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-10-01, 51-10-02, 51-30-2 & SOH M 20-10-03 FIG 9.

Part: HINGE FITTING — CRACKED (NR 5 SPOILER) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SUSPECT CRACK FOUND ON NR 5 SPOILER CENTRE HINGE FITTING HFEC INSP. CARRIED OUT ON NR 5 SPOILER CENTER HINGE FITTING IAW B727 N DTM PT 6 51-00-00 FIG 4 RESULT: CRACK CONFIRMED. CENTER HINGE FITTI NG REPLACED IAW SRM 51-30-02

Part: FRAME — CORRODED (RT WING) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, FRAME ASSY ON LWR SURFACE OF APU EXHAUST PANEL ON RT WING IS CORRODED. FRAME ASSY REPLACED IAW DRAWING 6562837 & SRM 51-30-32

Part: SUPPORT — CRACKED (RAM AIR DOOR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, RT RAM AIR INTAKE DOOR SUPPORT BRACKET FOUND CRACKED AT BS 600 S25R. DOOR SUPPORT BRACKET FABRICATED IAW SRM 51-20-1 FIG 7, NEW BRACKET RE-PROTECTED IAW SRM 51-10-02 NEW DOOR SUPPORT AND FASTENERS RE-INSTALLED IAW SRM 51-30-02

Part: RIB — CORRODED (W/B FAIRING) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3430, FWD FORMED SECTION SUPPORT RIB HAS EVIDENCE OF HEAVY CORROSION UNDER ANCHOR NUT PLATES, JUST FWD OF GRND MOVER DOOR CUT OUT DOOR REMOVED IAW SRM 51-30-02. FRAME REMOVED IAW SRM 51-30-02. CORR OSION REMOVED FROM SKIN IAW SRM 51-10-01 FOUND WITHIN LIMITS. FRAME FOUND OUT OF LIMITS IAW SRM 51-10-01 FABRICATED NEW FORMED SECTION IAW SRM 51-20-1. INSTALLED NEW SECTION IAW SRM 51-30-2

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, RT MLG DOOR, DOOR SKIN ON O/B SECTION OF DOOR ASSY CRACKED BS 910 AREA OF CRACKED SKIN TRIMMED OUT IAW SRM 52-80-02. HFEC INSP. CARRI ED OUT AROUND CUTOUT AT R/H MLG DOOR SKIN ON O/B SECTION OF DOOR ASS Y IAW B727 NDTM PT 6 510000 FIG 4. REPAIR CARRIED OUT IAW SRM 52- 80-02

Part: PANEL — ERODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, AIRSTAIRS COMPARTMENT, CLOSE OUT PANEL AT STA 1223 LOBE THAT JOINS TO EXTERNAL SKIN IS SHOWING SIGNS OF ERROSION ALONG ITS EDGE ON LT SIDE. AREA REPAIRED IAW SRM 51-40-3 FIG 1

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SUSPECT CRACK AT NR 1 STOP FITTING CUT OUT ON FWD FRAME OF AFT CARGO DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-02 & SMRO EO 2003-025-021 UPS ENGINEERING FILE NO. B727-5330-18744-A

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CRACK ON AFT CARGO DOOR INNER SKIN AT HOLE CUT OUT FOR BALANCE MECHANISM CABLE PULLEY. STOP DRILLED HOLE IAW SRM 51-10-1 REPAIR WAS THEN CARRIED OUT IAW SR M 51-40-2 REPROTECTED IAW SRM 51-10-2

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CRACK ON ANGLE, AFT CARGO DOOR INTERIOR, ABOVE AFT DOOR STOP. REMOVED ANGLE FROM DOOR INTERIOR IAW SRM 51-30-2 FABRICATED NEW ANGL E IAW SRM 51-20-1 FIG 7 INSTALLED NEW ANGLE IAW SRM 51-30-2

Part: CARRIAGE — CORRODED (NR 6 TE FLAP) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, NR 6 FLAP CARRIAGE SPINDLE INTERNALLY CORRODED. NR 6 FLAP CARRIAGE REPLACED IAW OHM 57-58-02 & OHM 57-52-01 REF. TC C5 7-581-04-4D FOR INST. & DUAL

Part: BUTT JOINT — DAMAGED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE:C&SI NDT INSP. HAS INDICATION OF MATERIAL LOSS AT BS 1080 BUTT JOINT BETW EEN S2L & 2R. VISUAL INSP. CARRIED OUT CORROSION FOUND TO EXTEND UP TO S3L NEW CUT OUT LINE MADE IAW 69-62161 S3L REPAIR CARRIED OUT IAW DRAWINGS 69-6 2161 & UPS EO B727-5330-1177-M

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SUSPECT CRACK ON FRAME ADJACENT TO HINGE STRUCTURE AT FWD END OF FWD CARGO BAY DOOR. ON REMOVAL OF STIFFENER IN PREPARATION FOR REPAIR A NEW CRACK WAS FO UND WHICH WAS OUTSIDE THE PERMITED REPAIR AREA. FRAME WAS REMOVED IAW SRM 51-30-02. FRAME FABRICATED IAW SRM 51-30-02 FRAME INSTALLED IA W SRM 51-30-02. REPAIR CARRIED OUT IAW SRM 51-10-1

Part: PANEL — CONTAMINATED (NR 9 SPOILER) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, AFTER X-RAY INSP. NR 9 SPOILER FOUND TO HAVE WATER INGRESS AND CELL DISTORTATION SPOILER PANEL REPLACED IAW MM 27-61-01 & MM 27-62-01

Part: RADOME — DAMAGED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, RADOME FAILED MOISTURE CHECK. RADOME REPLACED IAW MM 53-15-00. RESISTANCE CHECK CARRIED OUT ON RADOME IAW MM 53-15-00. CHECK FOUND TO BE SATISFACTORY

Part: ATTACH FITTING — CRACKED (RT MLG) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, RT MLG WING DOOR ACTUATING ROD ATTACH FITTING CRACKED FITTING REPLACED IAW EO B727-3210-2583-G APP. D, E, F & G

Part: WEB — CRACKED (BS WL) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, NOSE WHEEL WELL LT SIDE AT STA 992 WL 140 TWO SMALL CRACKS ON HORIZONTAL WEB. HORIZONTAL WEB REMOVED & REPLACED IAW SRM 51-20-01 & 51-30-02

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CORROSION ON FRAME TIE ANGLE BS 351.2 S24L - S25L. DAMAGE REMOVED IAW SRM 51-10-01 FOUND OUTSIDE LIMITS. REPAIR SECTIO N FABRICATED IAW FLAP PATTERN LAYOUT AS PER SRM 51-20-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CORROSION UNDER ANCHOR CLIP ON LWR SIDE OF FLOORBEAM TOP STRUCTURE BS 344 LBL 12 APPROX. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7

Part: STRUCTURE — CRACKED (AIRSTAIR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CRACK AT BELLED HOLE ON VERTICAL WEB ON LT SIDE OF AIRSTAIRS AT STA . 1306 (LOWER HOLE). CRACKS STOP DRILLED IAW SRM 51-10-1. HFEC INSP. CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4 RESULTS - NDF CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM 51-40-2

Part: HINGE — CORRODED (LT WING OB TAB) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, O/B AILERON, LT WING, O/B TAB HINGE HAS EXCESSIVE CORROSION 2ND I/ B IS CRACKED AND THE OTHER TWO ARE PITTED EXTENSIVELY. TAB HINGES REPLACED IAW SRM 51-30-02 FOR O/B AILERON TAB INSTALLATION REF. NRC 664356

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SURFACE CORROSION ON ANGLE AT LWR END OF BS 950 FITTING LT AT STR. 22 LT IN LT MLG WHEEL WELL. REPAIR CARRIED OUT IAW SMRO EO 2003025009.

Part: TAB — DELAMINATED (LT WING AILERON) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, LT WING, I/B AILERON TAB HAS 2 ARMS OF DELAMINATION ON UPPER SURFACE. I/B AILERON TAB REMOVED IAW MM 27-10-05. FITTED NEW AILERON TAB IAW MM 27-10-05. I/B AILERON TAB BALANCE CHECKED IAW SRM 51-80-03. ADJ /TEST CARRIED OUT IAW MM 27-10-05

Part: ATTACH FITTING — CRACKED (LT MLG SWIVEL) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C/SI, LT MLG SWIVEL VALVE LINK ARM ATTACH BRACKET CRACKED AT UPPER ATTACH POINT. BRACKET REPLACED IAW SRM 51-20-1

Part: FRAME — CORRODED (W/B FAIRING) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, BODY FAIRING NR 3430, HAS CORRODED FRAME AFT OF GND. COOLING FAN DOOR CUT OUT. FRAME REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 OUT OF LIMITS IAW SRM 51-10-01. NEW FRAME FABRICATED IAW SRM 51-20- 1 FIG 7. NEW FRAME INSTALLED IAW SRM 51-30-2

Part: ACCESS PANEL — CORRODED (#2 TANK) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C CORROSION ON LH #1 ACCESS PANEL FOR #2 TANK LH INTEGRAL REPLACED IAW MM 28-11-21

Part: HINGE — CRACKED (BS 1376 #2 ENG.) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C ENG. #2 PYLON, CRACK ON R/H COWLING HINGE CUTOUT AT BS 1376 CRACK ON HINGE CUTOUT STOP DRILLED IAW SRM 51-10-1 REPAIR CARRIED OUT IAW SMRO EO 2001-050-002 UPS ENGINEERING FILE NO 727-54-20016

Part: PANEL — DELAMINATED (#2 ENG. INTAKE) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C DELAM ON CORNER OF PANEL ON DOG BOX HOUSIG (#2 ENG. INTAKE) AT BS 11 50 AT 9 O CLOCK POS. REPAIRED IAW SRM 51-40-9

Part: HINGE — CRACKED (ELEVATOR) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C NR 5 BALANCE PANEL RT ELEV ATTACH HINGE CRACKED AT O/B MOST HINGE SEGMENT. HINGE HALF REPLACED IAW MM 20-80-02

Part: ANGLE — CRACKED (STN. 35.0 APPROX) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C R/H ELEVATOR (REF X-RAY) CRACK NOTED IN LWR ANGLE INTERNAL APPROX LO CATION 6" AFT OF FRONT SPAR AT STN 35.0 REPLACED LWR ANGLE AT STN. 35.0 IAW DRAWING 65-25634

Part: TAB HINGE — CORRODED (L/H I/B TAB AIL) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C L/H INBD AILERON TAB O/B HINGE CORRODED. HINGE REPLACED IAW OHM 57-50-11

Part: HINGE BRACKET — CRACKED (NR 7 SPOILER) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C NR 7 SPOILER I/B HINGE BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 & DRAWING 65-98296

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FWD ENTRY DOOR EMERG EXIT LIGHT AS PER MM 33-50-01

Part: ROD — CRACKED (NR 7 SPOILER) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C O/B TENSION TIE ROD FOR NR 7 SPOILER O/B HINGE BRACKET CRACKED. TIE ROD FOR NR 7 SPOILER REPLACED IAW MM 20-80-01

Part: LAP JOINT — CORRODED (BS 1141 STR. 4) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT AT BS 1141 STR 4 R LFEC CARRIED OUT, 30%CORROSION INDICATED. AREA OF DAMAGE , CUTOUT HF EC NDF. REPAIR PARTS FABRICATED AND INSTALLED IAW UPS EO B727-5330-0 509 APPENDIX 8.3. AREA REPROTECTED IAW SRM.

Part: LEVER — CORRODED (LT MLG WW) · airframe 51,422 hrs · 39,426 cycles

INSPECTION TYPE:C LT W/W AILERON PCU, LINKAGE/CRANK TO TAB DRUM IS BADLY PITTED. LEVER ASSY REMOVED IAW OHM 27-17-01, NEW LEVER ASSY INSTALLED IAW OH M 27-17-01 FASTENERS INSTALLED IAW SRM 51-30-02

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, FLOORBEAM LOWER CHORD CORRODED BS 600 LBL 12 TO 14. CORROSION REMOVED PER SRM 51-10-06, FLOORBEAM REPAIRED IAW SMRO EO 2000-018-006, UPS ENGINEERING FILE NUMBER 727-53-2257.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C&SI, CORROSION UNDER ANCHOR NUT ON CARGO FLOOR, FLOORBEAM AFT CARGO BAY, AT STA 1045 APP AND RBL 8. REPAIR CARRIED OUT IAW SRM 51-30-2 SRM 51-10-6 53-10-5 FIG 4.

Part: BEAM — CRACKED (TAIL) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, TAIL SKID COMPARTMENT, TERMINAL-TRANSVERSE BEAM STABILIZING LINK AFT UPPER LT CRACKED. TERMINAL FITTING REPLACED IAW SRM 51-30-2.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, CRACK FOUND AT I/B RIB NR 5 SLAT. CRACK STOP DRILLED IAW 51-10-01, REPAIR CARRIED OUT IAW SRM 57-50-0 3 FIG 9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, EVIDENCE OF CORROSION ON STR 18A UPPER AND LOWER FLANGE AT BS 855 RT. CORROSION REMOVED AND REPAIRED IAW SMRO EO 2000-018-004, UPS ENGINE RING FILE NUMBER 727-53-2259.

Part: DRAG LINK — CRACKED (TAILSKID) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, EVIDENCE OF CRACK TO TAIL SKID AT TAIL SKID CARTRIDGE ATTACH LUG RT SIDE. TAIL SKID DRAG LINK REPLACED IAW MM 32-71-61.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, A NUMBER OF SCRATCHES ON FWD CARGO DOOR EXTERNAL SKIN AND DENTS. FWD CARGO DOOR REPLACED IAW MM 52-31-01.

Part: SUPPORT FITTING — CORRODED (NR 4 FLAP TRACK) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C&SI, NR 4 FLAP TRACK FWD SUPPORT FITTING UPPER HOLE HAS PITTING CORROSION. REPAIR CARRIED OUT IAW SMRO EO 2000-018-001 UPS ENGINEERING FILE NOL 727-57-2159.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:SI, A NUMBER OF SCRATCHES ON FWD CARGO DOOR EXTERNAL SKIN AND DENTS. DUE TO THE FACT A NUMBER OF THE SHARP CREASES WERE BEYOND SRM LIMITS FWD CARGO WAS REPLACED IAW MM 52-31-01.

Part: FITTING — CORRODED (NR 5 FLAP TRACK) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C&SI, NR 5 FLAP TRACK FWD SUPPORT FITTING UPPER HOLE HAS PITTING CORROSION. REPAIR CARRIED OUT IAW SMRO EO 2000-018-002 UPS ENGINEERING FILE NR 727-57-2160.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, CRACKS FOUND AT BOTH RIBS I/B TRACK TO NR 7 SLAT CONN. REPAIR CARRIED OUT IAW SRM 57-50-03, FIGURE 9.

Part: RIB — CRACKED (LE SLAT) · airframe 50,185 hrs · 38,398 cycles

INSPECTION TYPE:C, CRACK FOUND AT NR 3 RIB AT INNER SKIN CONNECTING NR 7 SLAT. REPAIR CARRIED OUT IAW SRM 57-50-3, FIGURE 9.

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE:AD V AFT CARGO DOOR NR 2 AFT DOOR STOP FITTING CRACKED. FITTING REPLACED IAW B727-5230-0032 APPENDIX C & D.

Part: FRAME — CRACKED (BS 930)

INSPECTION TYPE-C, CRACK AT BS 930 LT FRAME CRACK. REPAIRED IAW DRAWING 65-80107 AND EO B727-5310-2611.

Part: CROSS STRUT — CORRODED (NR 2 ENGINE)

INSPECTION TYPE-C, ENGINE NR 2 PITTING CORROSION ON TUBE OF CROSS STRUT. REPLACED CROSS STRUT ASSEMBLY IAW MM 71-12-11.

Part: WEB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-C, LT WING NR 4 LE SLAT AND ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW SRM 57-50-3.

Part: SKIN — CRACKED (NR 1 ENG TR UNIT)

INSPECTION TYPE-C, ENGINE NR 1 THRUST REVERSER LOWER DOOR INNER SKIN CRACKED (2 LOCATIONS). CRACKS STOP DRILLED IAW SRM 78-30-01.

Part: SKIN — DAMAGED (NR 5 LE SLAT)

INSPECTION TYPE:C BLEND OUT ON TE OF NR 5 LE SLAT RT WING. DAMAGE REPAIRED IAW SRM 57-50-3.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 RT FITTING AT AFT OUTBOARD FLANGE ABOVE STRINGER 9. REPAIR CARRRIED OUT IAW B727-5310-3057 AND DRAWING 65C35277.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE:C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING A FWD OUTBOARD FLANGE ABOVE STRINGER 9. REPAIR CARRIED OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C35277.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING AT FWD OUTBOARD FLANGE ABOVE STRINGER 9. REPAIR CARREID OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C35277.

Part: SHEAR TIE — CRACKED (BS 520)

INSPECTION TYPE-C, FWD CARGO HOLD ON INSPECTION OF CARGO DOOR LATCH SUPPORT FITTINGS SHEAR TIE ON FRAME AT BS 520 FOUND CRACKED. REPAIRED IAW SRM 51-40-02, 51-40-03, FIG 1.

Part: WEB — CRACKED (BS 1376)

INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE, SUSPECT CRACK ON WEB AT BS 1376 RT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: BRACKET — CRACKED (NR 1 ENGINE TR)

INSPECTION TYPE:C ENGINE NR 1 THRUST REV FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01 AND MM 78-30-00.

Part: SKIN — LIGHTNING STRIKE (BS 400)

INSPECTION TYPE:C LIGHTNING STRIKE ON FUSELAGE SKIN BS 400 BETWEEN S2R AND S3R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1.

Part: BRACKET — CRACKED (NR 3 ENGINE TR)

INSPECTION TYPE:C ENGINE NR 3 THRUST REV FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01 AND MM 78-30-00.

Part: SHEAR TIE — CRACKED (BS 540)

INSPECTION TYPE:C DURING INSPECTION OF MAIN CARGO DOOR LATCH, SUPPORT FITTINGS SHEAR TIE FOUND CRACKED ON FRAME AT BS 540 AT LATCH SUPPORT FITTING. REPAIR CARRIED OUT IAW SRM 51-40-02, 51-40-03 FIG 1.

Part: RIB — CRACKED (NR 2 NACELLE)

INSPECTION TYPE-C, SUSPECT CRACK ON CENTER ENGINE AFT MOUNT SUPPORT RIB RIGHT CHORD APP ROX 17 INCHES FROM TOP OF CHORD. RIB CHORD REPLACED IAW DRAWING 65-22913, 65-17553, 65-17551.

Part: WEB — CRACKED (BS 1376)

INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 LT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: ANGLE — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C LT STAB TE INBD SUSPECT CRACKS ON WEB SUPPORT ANGLE UPPER AFT END, INBD AND OUTBD OF NR 5 BALANCE BAY. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SKIN — DELAMINATED (NR 9 SPOILER)

INSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5.

Part: SKIN — CRACKED (PAX DOORWAY)

INSPECTION TYPE:C SUSPECT CRACK ON FUSELAGE SKIN AT UPPER FWD CORNER OF FWD ENTRY DOOR. REPAIRED PER EO NR B727-5330-1460-C.