N938UP

Part: METERING VALVE — MALFUNCTIONED (LEFT MLG BRAKE)

BRAKES DO NOT SEEM TO RELEASE AFTER BRAKE APPLICATION A/C COMES TO COMPLETE STOP AND HAVE TO ADD POWER TO TAXI A/C. ALSO, SEE L/P 694861 ITEM 2 ADJUSTED LT MLG BRAKE METERING VALVE WRT 32-41-11 SYSTEM OPS CK GOOD.

Part: OXYGEN MASK — INOPERATIVE (2ND OBSERVER)

INSPECTION TYPE:N/A, 2ND OBSERVER O2 MASK INOP. REMOVED AND REPLACED 2ND OBSERVER O2 MASK IAW 35-11-41. OPS & LEAK CHECK GOOD. PLACARD REMOVED. DEFERRAL CLOSED (M289816).

Part: RIB — CORRODED (LT WING L/E) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, EXFOLIATION CORROSION FOUND ON FIXED WING L/E RIB LOWER CHORDS AT LES 236.217 AND LES 243.977. REMOVED CHORDS ON ABOVE AREA IAW SRM 51-30-02. FABRICATED AND INSTALLED CHORDS ON ABOVE AREA IAW BOEING DRAWING NR 65-16269.

Part: PANEL — DELAMINATED (RT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, RIGHT WING UPPER SURFACE T/E PANEL DELAM ON UPPER SURFACE AT I/B AFT CORNER. PANEL REPLACED IAW MM 20-80-01.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, RIGHT WING ACCESS PANEL NR 8640 DELAM ALONG EDGE AND SUSPECT CRACK ON LWR SURFACE. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 51-40-20.

Part: SKIN — CORRODED (NR4 KRUEGER FLAP) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, NR 4 KRUEGER FLAP HAS CORROSION ON INNER SURFACE BELOW ACTUATOR ATTACH AREA. CORROSION REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 57-50-01. L/ED GE KRUEGER FLAP REMOVED IAW AMM 27-81-01 STEP 2. ACTUATOR ROD END BEARING FOUND TO BE WORN AND CORRODED. ACTUATOR REMOVED IAW AMM 27-81-22 FLAP ACTUATOR REPLACED IAW AMM 27-81-22. KRUEGER FLAP INSTALLED IAW AMM 27-81-01. ADJUSTMENT TEST CARRIED OUT IAW AMM 27-81-01.

Part: SKIN — CORRODED (RT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, AREA OF LITE SURFACE CORROSION AROUND FASTENER HEADS ON HORIZ FLANGE OF RT WING UPPER SPLICE PLATE AT BS 850. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IN ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. ALL CORROSION REMOVED. STRESS RELIEVED AREA, INSTALLED FASTENERS AND REPROTECTED AREA IAW SRM 51-10-02.

Part: SKIN — CRACKED (NR3 KRUEGER FLAP) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON ANTI ICE SKIN AT I/B LOWER CORNER OF NR 3 KRUEGER FLAP. SKIN REPLACED IAW DRAWING 65-16225.

Part: PLATE — CORRODED (LT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND FASTENER HEAD ON HORIZ FLANGE OF LT WING UPPER SPLICE PLATE AT BS 848. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-021. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. FASTENER INSTALLED IAW SRM 51-30-02. AREA SEALED IAW MM 28-11-00.

Part: SKIN — CRACKED (NR 7 SLAT) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON NR 7 SLAT OUTER SKIN AT O/B HOOK. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4, 3 CRACKS NOTED AND MARKED ON SLAT. CRACKS FOUND TO BE CONTAINED WITHIN RIVET HOLES.

Part: STRUCTURE — CORRODED (NR3 KRUEGER FLAP) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, PITTING CORROSION ON NR 3 KRUEGER FLAP BULLNOSE AT O/B LOWER MOUNT LUG. BULLNOSE REPLACED IAW OHM 57-51-21.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, DELAMINATION FOUND ON RIGHT ELEVATOR TAB. REPLACED RIGHT ELEVATOR TAB.

Part: BOLT — CORRODED (NR 2 ENGINE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, NR 2 ENG MOUNT FITTING RIGHT SIDE HAS ONE CORRODED ATTACH BOLT ON UPPER SURFACE OF HORIZONTAL FIRE WALL. BOLT REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 RT VAPOR SEAL REMOVED FOR ACCESS IAW MM 51-30-00. CORROSION REMOVED ON LOWER FLANGE OF STR 18A IAW SRM 51-10-02. HFEC OF ABOVE AREA CARRIED OUT IAW B727-NDTM 51-00-00 PT6 FIG 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIR STRAPS FABRICATED IAW DRWG 6 5C27166 AND EO 2004-083-008 (727-53-20165) CAD PLATING CARRIED OUT.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 LT SIDE CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IAW B727NDTM 51- 00-00 PT 6 FIG 4, ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03.

Part: STRINGER — CORRODED (WING CNTR SECT) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN AT STR 10C RBL 65 BS 810. CLEANED CORROSION IAW SRM 51-10-01. HFEC CARRIED OUT IAW B727-NDTM -5 1-00-00 PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOP M 20-10-03. AREAS REPROTECTED.

Part: FRAME — CRACKED (CENTER WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON WING CENTER SECTION AT BS 775 RBL 45 ON LOWER FLANGE. HFEC CARRIED OUT IAW NDT M 51-00-00. RESULT - CRACKS CONFIRMED. FWD SECTION OF CHORD REMOVED AT BS 740 - BS 780 RBL 45 IAW 51-30-2. CENTER SECTION CHORD FWD SECTION AT RBL 45 BS 740 - 780 INSTALLED.

Part: SKIN — CORRODED (WING CNTR SECT) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN BETWEEN STR 12-13C RBL 65 BS 795 IN THE AREA INTERFACING WITH Y FLANGE FITTING. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT ON BLENDED AREA IAW B727 NDTM 51-00-00PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIRED IAW AAAE EO 2004-083-021 (B727-57-20125).

Part: SPAR — CORRODED (LT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD LEFT WING AT WBL 245. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. CORROSION MARKED ON AIRCRAFT. REPAIR OF AREA CARRIED OUT IAW EO B727-5710-17848 APPENDIX C AND AAAE EO 2004-083-004 (B727-57-20125).

Part: PANEL — DELAMINATED (WING T/E PANEL) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C DELAM ON RT WING T/E PANEL LOWER SURFACE OF WING BELOW NR 13 SPOILER. REPAIRED DELAM ON PANEL IAW SRM 51-40-20.

Part: SKIN — DELAMINATED (RT MID FLAP) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, DELAM ON RIGHT O/B MIDFLAP T/E WEDGE FWD FACE I/B OF NR 2 AFT FLAP TRACK. DELAM OUT OF LIMITS. MIDFLAP REPLACED IAW MM 27-51-12.

Part: SPAR — CORRODED (RT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD, RIGHT WING BETWEEN WS 290-320 APPROX. REPAIR CARRIED OUT IAW UPS EO B727-5710-17848-B APPROX C AND AAAE EO 200 4-083-004 (727-5710-21057).

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, PANEL NR 3512 LT REQUIRES COMPOSITE REPAIR. PANEL REPAIRED IAW SRM 51-40-9.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, SKIN DEFORMATION AT STR 11R BS 1342 (RT SIDE OF NR 2 ENGINE FIREWALL). CUT OUT DAMAGED SECTION OF SKIN & PREVIOUS REPAIR DOUBLER REMOVED IAW SRM 53-30-3G FIG 3A. HFEC CARRIED OUT AROUND CUTOUT AND HOLES COMMON TO REPAIR IAW BOE 727 NDT MANUAL 51-00-00 PT 6 FIG 4 AND FIG 16, NO DEFECTS. INSTALLED REPAIR PARTS IAW SRM 53-30-03.

Part: STRUCTURE — CRACKED (LOWER LEFT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, LOWER LEFT WING, FIXED WING STRUCTURE WHICH SECURES NR 3 FLAP TRACK FAIRING IS CRACKED ON BOTH I/B AND O/B SIDES. HFEC CARRIED OUT ON SUSPECT CRACKS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONFIRMED ENDS MARKED. DAMAGED AREA REMOVES IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-40-03.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, INTERCOSTAL CRACKED ON TOILET COMPARTMENT FLOOR BS 294.5-312. INTERCOSTAL REMOVED IAW SRM 51-30-02 AND DAMAGE REMOVED IAW SRM 51-40-03. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, NO DEFECTS FOUND. INSTALLED REPAIR AND INTERCOSTAL IAW SRM 51-30-02.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING, REPAIR BUSHINGS IN BOTH O/B HOLES HAVE MIGRATED. REPAIRED IAW UPS EO B727-5440-11592-A.

Part: YOKE — CORRODED (LT MLG) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, ON REMOVAL OF LT MLG SWING LINK, YOKE OVER SWING LINK FOUND TO HAVE PITTING CORROSION. REPLACED YOKE ASSY IAW MM 32-32-00.

Part: LAP JOINT — CORRODED (FUSELAGE SKIN) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, RIVETS PULLED BETWEEN BS 810-830 STR 4L, CORROSION AT LAP JOINT OUT OF LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-30-1.

Part: ANGLE — CRACKED (NR 2 SPOILER) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, NR 2 SPOILER ACTUATOR SUPPORT CASTING ANGLE CRACKED AT LOWER INBOARD ATTACH POINT. REPLACED ANGLE IAW SRM 51-30-02. REINSTALLED NR 2 SPOILER ACTUATOR IAW 27-61-81.

Part: PANEL — DELAMINATED (LT WING) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, LEFT WING UPPER SURFACE T/E PANEL FWD OD MLG BEAM HAS DELAMINATION ON AFT END, ALSO HAS UPPER SURFACE DENTS. REPAIRED AND INSTALLED PANEL AS PER DRAWING 65-21655 IAW SRM 51-30-02.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON INTERNAL STRUCTURE OF AFT LOWER CARGO DOOR. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED ENDS MARKED. REPLACED ANGLE IAW EO B727-5230-0032.

Part: TAB — DELAMINATED (RT AILERON) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED AT OUTBOARD UPPER TRAILING EDGE. AILERON TAB REPLACED IAW MM 27-10-19.

Part: SPOILER — CRACKED (NR 14) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE: C, NR 14 SPOILER PANEL HAS EVIDENCE OF DELAM AT LOWER I/B CORNER. NR 14 SPOILER PANEL REPLACED IAW MM 27-61-01.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, RIGHT WING DOOR LOWER SKIN HAS TWO SUSPECT CRACKS IN SKIN AT FWD END MID WAY ON DOOR. WING DOOR REPLACED ON NRC 733172.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, BULGING CORROSION AND CRACKED SKIN FOUND ON BS 870 BULKHEAD RBL 43 APPROX HALF WAY DOWN ON BULKHEAD. DERIVETED REPAIR STRAP ON BULKHEAD IAW SRM 51-30-02. REPAIR FOUND OUT OF LIMITS. DAMAGED SECTION CUT OUT IAW SRM 53-10-09. HFEC CARRIED OUT ON AFFECTED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND. REPAIR FABRICATED AND INSTALLED IAW SRM 51-30-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON LEFT 950 O/B LUG AFT SIDE. FITTING REPLACED IAW SRM 51-30-02 AND AAAE EO 2004-083-001R1 (727-53- 20161).

Part: DOOR — CRACKED (TAIL SKID) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, SUSPECT CRACK AT ATTACH LUG OF TAIL SKID DOOR AND STRUT. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00. RESULT - CRACK CONFIRMED. INSTALLED NEW TAIL SKID DOOR IAW MM 32-71-61. TAIL SKID TESTED SATISFACTORY IAW MM 32-71-01.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 53,145 hrs · 34,107 cycles

INSPECTION TYPE:C, ANGLE BRACKET ON LOWER FWD BS 880 CORRODED RT MLG WW. INSTALLED NEW BRACKET IAW SRM 51-30-02.

Part: CARRIAGE — WORN (LT OB TE FLAP)

ATB FL 330 IN CLIMB EXPERIENCED MODERATE VIBRATION. FOUND LEFT OUTBOARD TRAILING FLAP, INBOARD TRACK AFT ROLLER CLEARANCE OUT OF TOLERANCE. REPLACED ROLLER.

Part: CARRIAGE — WORN (TE FLAPS)

AIRFRAME HAS A VIBRATION - ATB. TE FLAP CARRIER HAS EXCESS PLAY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT OVERHEAD FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERIES FORWARD ENTRY EMERGENCY EXIT LIGHT ASSY. CHECKS NORMAL.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,743 hrs · 33,744 cycles

INSPECTION TYPE: C, INTERCOSTAL MOUNT BRACKET BS 1060 CRACKED. FABRICATED NEW BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-10-2, MOUNT BRACKET INSTALLED IAW SRM 51-30-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,743 hrs · 33,744 cycles

INSPECTION TYPE: C, INTERCOSTAL IN AFT FREIGHT HOLD CRACKED BS 1040 BS 1060 (SUPPORTS DOOR HOLD-PEN BRACKET). FABRICATED INTERCOSTAL BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-20-2. INTERCOSTAL INSTALLED IAW SRM 51-30-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,743 hrs · 33,744 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT 480 BETWEEN STRINGER 10R AND 14R. REPAIRED IAW UPS REPAIR FILE 727-53-20106.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,743 hrs · 33,744 cycles

INSPECTION TYPE: C, EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT BS 480 RT BETWEEN ST R10 AND 14 RT. LFEC C/W MATERIAL LOSS INDICATIONS MARKED. PAINT STRIPPED AND FASTENERS REMOVED IAW SRM 51-30-2. DAMAGED AREA CUT OUT, CUTOUT HFEC AND NDF, HOLES HFEC AND NDF. REPAIR ACCOMPLISHED UPS EO B727-53-20106.

Part: LIGHT — NOT SEATED (COCKPIT)

INSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHT ILLUMINATED IN ARMED POSITION. RESEAT COCKPIT EMERGENCY EXIT LIGHT, OPS CHECK GOOD.

Part: GUSSET — CRACKED (TORQUE BOX) · airframe 52,743 hrs · 33,744 cycles

INSPECTION TYPE: C, SUSPECT CRACK AT 1263 UPPER BEAM AT INNER RADIUS OF FLANGE ADJACENT TO THIRD FASTENER VERT, FROM I/B END, RT TORQUE BOX (GUSSET). HFEC C/W CRACK CONFIRMED AND ENDS MARKED. GUSSET AND ANCILLARY STRUT URE DISPLACED IAW SRM 5130-02. NEW GUSSET INSTALLED IAW DWG 65C1387 4 AND UPS EO B727-5310-1239.

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

INSPECTION TYPE:C NWW PRESSURE CEILING IS CRACKED BETWEEN BS 270 - 273 RBL 14, CONFIRMED BY NDT. CUT OUT CRACK APPROX 4 X 1 INCH AT NWW PRESS CEILING BS 270 - 273 RBL 14 IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON NWW PRESS CEILING IAW B727 SRM 51-40-2.

Part: SKIN — CRACKED (NWW BS290-288)

INSPECTION TYPE:C NOSE W/W PRESSURE CEILING IS CRACKED AT BL-0. BETWEEN BS 290-288, CONFIRMED BY NDT. CUT OUT CRACK AT NWW PRESSURE CEILING AT BL-0 STA 303 APPROX 3"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR ON NWW PRESSURE CEILING IAW B727 SRM 51-40-2.

Part: SKIN — CRACKED (NWW BS285)

INSPECTION TYPE:C NWW PRESS CEILING IS CRACKED AT BS 285, BETWEEN RBL 3 AND RBL 6, CON FIRMED BY NDT. CUT OUT CRACK AT NWW PRESS CEILING RBL 3 APPROX 4"X1" AND AT LBL 6 APPROX 5"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT NWW PRESS CEILING BS 285 IAW B727 SRM 51-40-2.

Part: SKIN — CRACKED (NWW BS277)

INSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED EXTENDING FROM REPAIR DOUBLER AT BS 277, APPROX 8" FROM BOTOM OF WW, CONFIRMED BY NDT. REMOVED OLD DOUBLER REPAIR IAW B727 SRM 51-40-2. CUT OUT CRACK AT N WW RH PRESSURE WEB BS 277 IAW B727 SRM 51-40-2. INSTALLED EXTENDED DOUBLER REPAIR AND FILLER IAW B727 SRM 51-40-2.

Part: SKIN — CRACKED (NWW BS260-265)

INSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED BETWEEN BS 260-265, JUST BELOW PANEL #3125, CONFIRMED BY NDT. CUT OUT CRACK AREA AT NWW R/H PERSURE WEB BS 260-365 AS PER B727 SRM 51-40-2 APPROX 2"X1". INSTALLED DOUBLER REPIAR AS PER B727 SRM 51-4 0-2.

Part: SKIN — CORRODED (BS300 STR25L)

INSPECTION TYPE:C LEFT NOSE SECTION EXTERIOR FUSELAGE SKIN SHOWS BULGE STR 25L AND BS 300. CUT OUT DAMAGED AREA AT EXTERIOR FUSELAGE SKIN L/H STR 25L BS 300, APROX 10"X3" IAW B727 53-30-3 FIG 3. REMOVED CORROSION ON SKIN STA 310 STR 25L, MATERIAL LOST .003"; WITHIN LIMITS IAW B727 SRM 53-10-1 INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3.

Part: SPLICE PLATE — CRACKED (BS 935 STR 18A)

INSPECTION TYPE:C RIGHT MAIN W/W CENTER SPLICE PLATE CRACKED AT STR 18A RT. STA 935 STOP DRILLED END OF CRACK IAW B727 SRM 51-10-1. INSTALLED REPAIR IAW EO B727-5330-3815A ON FUSELAGE SKIN BS 935 STR 18A R/H SIDE.

Part: SPLICE PLATE — CRACKED (STR18 ALT SIDE)

INSPECTION TYPE:C LEFT MAIN WHEEL WELL CENTER SPLICE PLATE, CRACK AT STR 18 ALT BS935 STOP DRILED END OF CRACK IAW B727 SRM 51-10-10, INSTALLED REPAIR STR 18 ALT SIDE FUSELAGE SKIN IAW B727 EO B727-5330-3815A.

Part: BEAM — CRACKED (RT WING)

INSPECTION TYPE:C NUMBER 3 FUEL TANK CRACK ON L/G SUPPORT BEAM AT WS 304. REPLACED BUSHING RT LANDING GEAR O/B END OF BEAM IAW SB 727-57-167. REMOVED AND REPLACED FWD AND AFT FITTINGS AT WS 304 LEFT GEAR SUPPORT BEAM AS PER B727 SRM 51-10-2. PERFORMED HFEC INSP PER BOEING NDT MANUAL PART 6-51-01-00 FIG 11, NO CRACK FOUND.

Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE)

INSPECTION TYPE:N/A DIVERSION-UNABLE TO PRESSURIZE AIRCRAFT. CLEARED DEBRIS FROM OUTFLOW VALVE.

Part: CONNECTOR — LOOSE (TE FLAPS)

INSPECTION TYPE:N/A ATB-OUTBD FLAPS WOULD NOT MOVE ON INITIAL EXTENSION AT MCI. SECURED CONNECTORPLUG IN RT W/W, OPS CHECK GOOD

Part: GYRO — FAILED (COCKPIT)

INSPECTION TYPE:N/A (BTB) DURING TAKEOFF INITIAL ACCELERATION F/O''S EADI BLANKED. REPLACED NR 2 VERT GYRO PER BMM 34-22-21. NOTE: THIS SAME NR 2 VG WAS REPLACED ON INB FLT FOR A 5 DEGREE ROLL. THE S/N REMOVED FROM BTB IS 81144914, THE PIREP DEBRIEF, INDICATED THE EADI BLANKED WHEN A/C WAS TURNED OR BRAKED DURING OUTBOARD TAXI. A/C DEPARTED WITHOUT FURTHER PROBLEMS.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY.

Part: RELAY — FAILED (EMERGENCY EXIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS IN ARMED POSITION AND CIRCUIT BREAKER POWER FAIL RELAY POPPED, WILL NOT RESET. REMOVED AND REPLACED R70 CHARGER CONTROL RELAY.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, LWR FWD CARGO HOLD DOOR CRACK ON SUPPORT ANGLE UNDER BALANCE SPRING SUPPORT BRACKET. ANGLE FABRICATED AND INSTALLED IAW DRAWING NR 65-18620.

Part: SUPPORT FITTING — CORRODED (NR 5 FLAP TRACK) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 5 FLAP TRACK FWD SUPPORT FITTING CORRODED. NR 5 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING NR 65-21651.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CRACK ON ANGLE BETWEEN FRAME AND FLOOR AT LWR FWD CARGO DOOR FWD HINGE CUTOUT AT BS 535 STR 17. REPLACEMENT ANGLE FABRICATED AND INSTALLED IAW DRAWING NR 65-16352.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CRACK ON STRINGER AT ATTACHMENT POINT TO FRAME AT BS 720 STR 21L IN LWR FWD CARGO HOLD. HFEC INSPECTION CARRIED IAW B727 NDTM PT6 51-00-00 FIG 4. CRACK CONFIRMED. CRACK CONTAINED IAW SRM 51-10-2. HFEC INSPECTION CARRIED OUT IAW B727 NDTM PT6.51-00-00 FIG 4. NO DEFECT FOUND.

Part: BEAM — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CORROSION FOUND ON LWR RT BEAM OF DELTA BEAM AT BODY FAIRING SUPPORT LUG. CORROSION REMOVED FROM SUPPORT LUG AND FOUND TO BE OUT OF LIMITS. LUG REMOVED FROM BEAM. ALL CORROSION REMOVED FROM AFFECTED AREA IAW SRM 51-10-6. HFEC INSPECTION CARRIED OUT IAW B727 NDTM PT6.51-00-00 FIG 4. NO DEFECTS FOUND. FPI CARRIED OUT IAW B7277OHM 20-20-02. NO DEFECT FOUND. REPAIR C/O IAW SMRO EO 2000-15-13.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CRACK ON STRINGER AT BS 440 AT STR 22L FWD OF CARGO HOLD FWD WALL. REPAIR CARRIED OUT IAW SRM 53-10-3 FIG 2. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4. NO DEFECT FOUND POST DAMAGE REMOVAL.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SEAT TRACK DAMAGED BETWEEN BS 498 & 502 LBL 62.5. SECTION OF TRACK REPLACED IAW SRM 53-10-2 FIG 7 AND SRM 53-10-5 FIG 3.

Part: SUPPORT FITTING — CORRODED (NR 4 FLAP TRACK) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD SUPPPORT FITTING CORRODED. NR 4 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING 65-21651.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CRACK ON FRAME SUPPORTING FWD CARGO DOOR HINGE AT BS 535 BETWEEN STR 17 & 18. REPLACEMENT FRAME FABRICATED AND INSTALLED IAW BOEING DRAWING 65-16352.

Part: ANGLE — CRACKED (BS 1183) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CRACK ON SPLICE ANGLE UNDER CABIN FLOOR AT BS 1183 BLK AT STR 17R IN LWR AFT CARGO HOLD. REPLACED CRACKED ANGLE IAW SRM 51-20-1, 51-30-2 & 51-10-1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, LWR AFT CARGO COMPARTMENT CORROSION ON FLOOR SUPPORT CHANNEL AT STA BS 1040 AT STR 28L. REPAIRED CORRODED SECTION IAW SRM 53-10-5 FIG 4.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CORROSION FOUND ON OUTER SURFACE OF REAR SPAR LWR CHORD CENTER SECTION LBL 55. REPAIR CARRIED IAW SMRO EO 2000-015-011 UPS ENGINEERING FILE NR 727-57-2155.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, ENGINE NR 3 FWD MOUNT FITTING, PITTING CORROSION IN AFT O/B HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.

Part: FLAP TRACK — CORRODED (WING) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 5 FLAP TRACK ON RT ML G BEAM. REPAIRED IAW SMRO EO 2000-015-007 UPS ENGINEERING FILE NR 727-57-2154.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, EVIDENCE OF CORROSION ON SUPPORT TANG, LT SIDE DELTA BEAM, LWR CHORD BS 760. CORROSION REMOVED FROM SUPPORT LUG AND AREA FOUND TO BE OUT OF LIMITS. LUG REMOVED FROM BEAM, ALL CORROSION REMOVED IAW SRM 51-10-6. HFEC I NSPECTION CARRIED OUT IAW NDTM PT6 FIG16. NO DEFECT FOUND. FPI CARRIED OUT IAW OHM.20-20-02, NO DEFECT FOUND. REPAIR CARRIED OUT IAW SMRP EO 2000-015-012.

Part: FLAP TRACK — CORRODED (WING) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 4 FLAP TRACK ON LT ML B BEAM. REPAIR CARRIED OUT IAW SMRO EO 2000-015-006 UPS ENGINEERING FILE NR 727-57-2153.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, ENGINE NR 1 FWD MOUNT FITTING, PITTING CORROSION IN BOTH O/B HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CRACK ON SPLICE ANGLE UNDER FLOOR AT BS 1180 I/B OF STR 17 RT IN LWR AFT CARGO HOLD. REPLACED CRACKED SPLICE ANGLE IAW SRM 51-20-1, SRM 51-30-2 & SRM 51-10-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CRACK AT LIGHTENING HOLE IN WEB AT STA 1223 RT. CRACK AT WEB REPAIRED IAW SRM 51-40-2 FIG 1.

Part: FLAP TRACK — CORRODED (WING) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 6 FLAP TRACK AFT MOUNT OUTER SURFACE CORRODED (UPPER.) FOR REPAIR REF SMRO EO 2000-015-009 UPS ENGINEERING FILE NR 727-57-2152.

Part: FLAP TRACK — CORRODED (WING) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 3 FLAP TRACK CORROSION AT AFT MOUNT OUT SURFACE FOR REPAIR REF SMRO EO 2000-015-08 UPS ENGINEERING FILE NR 727-57-2151.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 5 FLAP CARRIAGE SPINDLE INNER BORE CORRODED. PART REPLACED IAW TC C57-581-04-4D.

Part: FLAP TRACK — CRACKED (WING) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP TRACK SPACER BLOCK CRACKED AT AFT STOP FWD ATTACH HOLE. FLAP TRACK REPLACED REF TC C57-581-04-4D.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 4 FLAP CARRIAGE SPINDLE INNER BORE CORRODED. PART REPLACED IAW TC C57-581-04-3D.

Part: CARRIAGE — CORRODED (NR 3 FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 3 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE. PART REPLACED FOR INSTALLATION OF ASSY REF TC C57-581-04-3D.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE AND SMALL BEARING OUTER SURFACE END. PART REPLACED IAW TC C57-581-04-4D.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 2 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE AND SMALL BEARING OUTER SURFACE END. CARRIAGE ASSY REPLACED IAW OHM 57-52-11.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 1 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE. PART REPLACED IAW TC C57-581-04-3D.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 8 FLAP CARRIAGE SPINDLE INNER BORE CORRODED. PART REPLACED IAW TC C57-581-04-4D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, FRAME CRACKED AT BS 486 STR 18 LT. FRAME REPAIRED IAW SRM 51-40-02.

Part: WEB — CRACKED (FIREWALL) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, ENG NR 2 SUSPECT CRACK ON RT WEB AT BS 1387 OVER HORIZ FIREWALL. CRACKED WEB REPLACED IAW DRAWING REF 65-17555.

Part: WEB — CRACKED (FIREWALL) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, NR 2 ENG SUSPECT CRACK ON LT WEB AT BS 1387 OVER HORIZONTAL FIREWALL. WEB REPAIRED IAW DRAWING NR 65-17555.

Part: SUPPORT BRACKET — CRACKED (NR 3 ENGINE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, ENG NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. O/B FAIRING MID SUPPORT BRACKET CHANGED AND FITTED IAW MM 78-30-48.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CORROSION AT LAP S 10 RT BS 1120. REPAIR CARRIED OUT IAW SRM 51-10-6 & 53-30-3 FIG 14 SRM 51-30-2 & MM 53-11-00 & UPS EO B727-5330-0509 APP B.

Part: PIN — CORRODED (WING TO BODY) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, RT FRONT SPAR WING TO BODY BOTTLE PIN HAS PITTING CORROSION. BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: SKIN — CORRODED (BS 870) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CORROSION ON SKIN AT BS 870 S15R. REPAIR CARRIED OUT IAW SMRO EO 2000-015-003 UPS ENGINEERING FILE NR 727-53-2253.

Part: PIN — CORRODED (WING TO BODY) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, RT REAR SPAR TO BODY BOTTLE PIN CORRODED. REPLACED BOTTLE PIN IAW MM 57-41-01.

Part: SKIN — CORRODED (HORIZONTAL) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, LT HORIZ STAB REAR SPAR UPPER CHORD SKIN UNEVEN AT 2 AREAS. FWD OF NR 4 ELEV HINGE AND FWD OF NR 6 ELEV HINGE. DAMAGE REPAIRED IAW SRM 55-10-5 FIG 1.

Part: FITTING — CRACKED (DRAG BRACE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, CRACK INDICATION ON NLG DRAG BRACE FITTING. CRACK INDICATION ON DRAG BRACE FITTING VERIFIED SEE EO B727-5340-016 6 FOR SIGN OFF. REPLACE DRAG BRACE FITTING IAW EO B727-5340-0167-D.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CORROSION AT LAP S6L BS 720. REPAIR TO LAP CARRIED OUT IAW SRM 53-30-3 FIG 14.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 51,734 hrs · 32,797 cycles

INSPECTION TYPE:C+SI, SUSPECT CORROSION ON LAP S 4 RT BETWEEN BS 520 & 540. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 5 & UPS EO B727-5330-0509 & SRM 51-30-2.

Part: FLOOR — CRACKED (CARGO COMPT)

INSPECTION TYPE:N/A, CRACK APPROX 6 INCHES LONG IN AFT LOWER PIT FLOOR JUST FORWARD OF DOOR. FABRICATED AND INSTALLED FLOOR PANEL I/B OF DOOR PER SRM 51-10-1.

Part: REGULATOR — INOP (LT COCKPIT)

INSPECTION TYPE:N/A, CAPT'S O2 MASK AND SYSTEM FAILED NORMAL O2 TEST. FLOW METER INDICATES FLOW IN OFF. REMOVED AND REPLACED CAPT'S O2 REGULATOR, OPS AND LEAK CHECKS GOOD.

Part: FIRE WARNING — ACTIVATED (RT MLG WW)

INSPECTION TYPE:N/A ATB-WHEEL WELL FIRE LIGHT AND BELL CAME ON IN FLIGHT. CREW DECLARED EMERGENCY AND PERFORMED A NORMAL LANDING. UPON INSPECTION FOUND NO EVIDENCE OF SMOKE OR FIRE. LIGHT STAYED ON AFTER ENGINE SHUTDOWN. FOUND RIGHT WHEEL WELL SENSE ELEMENT AT FAULT CAUSING WARNING INDICATIONS. REMOVED AND REPLACED ELEMENT IAW MM 26-12-00.

Part: FORGING — CORRODED (BS 940)

INSPECTION TYPE-C, CORROSION (B727-5310-5596A) ON BS 940 FORGING ON PRESSURE WEB ATTACH FLANGE RBL 65 TO 70 WL 200. STANDARD REPAIR ACCOMPLISHED PER UPS EO B727-5310-4501A APP C.

Part: WEB — CORRODED (BS 944)

INSPECTION TYPE-C, CORROSION (B727-5310-5596A) ON PRESSURE WEB BS 944 WL 200 LBL 61. REPLACED PRESSURE WEB AT 944 WL 200 LBL 61 IAW SRM 53-10-1 SRM 51-20-1, 51-30-02. CORROSION WAS OUT OF LIMITS IAW SRM 51-10-6.

Part: RIB — CRACKED (RT TE FOREFLAP)

INSPECTION TYPE-C RT WING I/B FOREFLAP TRACK SUPPORT I/B RIB ASSY IS CRACKED. REMOVED AND REPLACED RIB ASSY PER SRM 51-30-02.

Part: RIB — CRACKED (WING)

INSPECTION TYPE-C, 7TH RIB FROM I/B END CRACKED AT FASTENER HOLE. REPAIRED PER SRM 51-30-5.

Part: SPAR — CRACKED (VERT STAB)

INSPECTION TYPE-C, LT VERTICAL FIN REAR SPAR CHORD IS CRACKED AT INTERSECTION WITH BS 1342 BULKHEAD. STOP DRILLED CRACK, ALODINED AND PRIMED STOP DRILL HOLE, FABRICATED REPAIR ANGLE AND FILLER DRILLED UP AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-20-01, 53-30-05, 51-30-02, SB 727-55-0076.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE-C, CORROSION RT WING O/B AILERON CENTER O/B HINGE FITTING. REMOVED AND REPLACED PER SRM 51-30-2.

Part: FRAME — CRACKED (BS 930)

INSPECTION TYPE-C, CRACK IN FRAME AT STA 930, STR 14R, RBL 65, WL 232. TRIMMED CRACKED MATERIAL AWAY AND INSTALLED FRAME REPAIR PER BAC DWG 65C10084.

Part: STRINGER — CORRODED (BS 930-940)

INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD NR 890693 (INT61) FOUND CORROSION AROUND FASTENERS HEADS ON STRINGER 18 RT STA 930 TO 940, WL 201. REMOVED FASTENERS, BLENDED CORROSION, REPAIRED AND REINSTALLED FASTENERS IAW UPS ER NR 99-5139.

Part: DOOR — CORRODED (SERVICE DOOR)

INSPECTION TYPE-C, MGD OUTER SKIN CORRODED BETWEEN LOWER LT FRAME AND PRE-EXISTING REPAIR DOUBLER. FOUND SKIN CRACKED AND BLENDED ALL CORROSION, CUT OUT ALL DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 52-00-3.

Part: ANGLE — CORRODED (GALLEY DOOR)

INSPECTION TYPE-C, ATTACH ANGLE FOR LOWER HINGE LOWER WEB CORRODED ON MID GALLEY DOOR. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED OLD ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 52-00-2, SRM 52-40-1, SRM 51-20-1, SRM 51-30-1.

Part: SKIN — CRACKED (NR 2 LE FLAP)

INSPECTION TYPE-C, CRACKS IN FASTENER HOLES ON NR 2 K-FLAP TAI SKIN FROM 17 I/B OF O/B EDGE AND 31 I/B OF O/B EDGE AND AT 39 I/B OF O/B EDGE. REMOVED TAI SKINS AT 17, 31 AND 39 OF O/B EDGE AND INSTALLED 3 NEW TAI SKINS IAW SRM 51-30-2, OHM 20-50-01.

Part: WEB — CORROSION (GALLEY DOOR)

INSPECTION TYPE-C WHILE WORKING NRC 890638, FOUND CORROSION ON MID GALLEY DOOR LWR HINGE CAVITY LWR WEB. REMOVED OLD WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 52-40-1, SRM 51-20-1, SRM 51-30-2, SRM 52-00-2.

Part: SKIN — CRACKED (BS 214.5)

INSPECTION TYPE-C, DURING NDI INSPECTION FOUND SKIN TO BE CRACKED AT TWO ADJACENT FASTENERS ON SECTION 41 SKIN, LEFT HAND SIDE, BS 243.7 WL 214.5, FWD AND AFT FASTENER ROW FASTENERS CRACKED. REMOVED 1 X 3 AREA OF DAMAGED SKIN AND INSTALLED STANDARD DOUBLER AND FILLER REPAIR PER SRM 53-30-3 AND MM 51-20-31, SRM 51-30-8 AND OHM 20-50-01.

Part: WEB — CRACKED (NR 6 LE FLAP ACT)

INSPECTION TYPE-C, NR 6 K-FLAP ACT MOUNTING STRUCTURE LWR WEB BETWEEN I/B AND O/B MOUNT IS CRACKED. REMOVED OLD WEB AND INSTALLED NEW WEB IAW SRM 51-30-2, SRM 51-20-1, OHM 20-50-01, SRM 51-10-2.

Part: BRACKET — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, NR 4 K-FLAP CORROSION AROUND I/B NUT OF I/B BULLNOSE HINGE MOUNTING BRACKET ON K FLAP (C57-562-01.00-02). REMOVED BOLT, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED BRACKET IAW UPS ER NR 99-5145 AND REINSTALLED BOLT IAW MM 27-81-01.

Part: RIB — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, NR 4 K FLAP I/B BULLNOSE BONDING JUMPER CORROSION ON NUT SIDE OF RIB OF K-FLAP (C57-562-01.00-02). REMOVED DAMAGE ON RIB, FABRICATED AND INSTALLED REPAIR ANGLES AND DOUBLER IAW SRM 57-50-3. RELOCATED BONDING JUMPER TO INBOARD RIB IAW UPS ADENDUM EO B727-5740-3980.

Part: FIRE DETECTOR — MALFUNCTIONED (WHEEL WELL)

INSPECTION TYPE-N/A, WHEEL WELL FIRE LIGHT INTER ON CLIMBOUT. CHECKLIST COMPLETED, LIGHT REMAINED OUT. WHEEL WELL FIRE DETECTION SYSTEM DEFERRED IAW MEL REF 26-8. CONTROL NR M-163903 ASSIGNED DMP COMPLIED WITH PLACARD INSTALLED. CLEARED DEFFERAL SEE ITEM 1 P-321667, PLACARD REMOVED, OK FOR CONTINUED SERVICE.

Part: STRINGER — GOUGED (BS 344)

INSPECTION TYPE-C, GOUGE IN STR 20 RT BS 344. REPAIR CARRIED OUT IAW SRM 53-10-3 FIG 1.

Part: BLKHD STIFFENER — DAMAGED (AFT PRESS BLKHD)

INSPECTION TYPE-C, HYD LINE RUBBING STIFFENER. STIFFNER FOUND TO BE DAMAGED NECESSITATING A REPAIR. REPAIR CARRIED OUT IAW SRS EO 97-24-008 UPS ENG FILE NUMBER 727-53-1 967.

Part: SKIN — CORRODED (BS 1030)

INSPECTION TYPE-C, SUSPECT CORROSION AT BS 1030 RT STR 4 RT. REPAIRED IAW SRM 53-30-3 FIG 5 AND IAW EO-727-5330-0509 APP 8.3.

Part: SKIN — CORRODED (BS1090)

INSPECTION TYPE-C, SUSPECT CORROSION FOUND BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 TO 1110, STR 11 AND 12 RT. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 97-29-04, UPS ENGINEERING FILE NUMBER 727-53-1964.

Part: PRESSURE PANEL — CORRODED (NLG WW)

INSPECTION TYPE-C, BULGING OF NOSE WHEEL WELL PRESSURE FLOOR AT NOSE WHEEL SNUBBER PAD MOUNT RT SNUBBER SUPPORT. REPAIRED IAW SRM 53-10-9 FIG 4.

Part: BRACKET — CRACKED (NR 7 SPOILER)

INSPECTION TYPE-C, NR 7 SPOILER PANEL GROUND SPOILER HINGE BRACKET I/B IS CRACKED. REPLACED BRACKET IAW SRM 51-30-2 AND IAW DRG NR 65-16216.

Part: WEB — CRACKED (BS 1263-1273)

INSPECTION TYPE-C, CRACKS IN VERTICAL WEB OF VENTRAL STAIRWELL TORQUE BOX BETWEEN BS 1263 TO 1273. VERTICAL WEB REPAIRED IAW ENGINEERING ORDER B727-5310-1239E.

Part: STRINGER TABS — CRACKED (WS 629.00)

INSPECTION TYPE-C, LT WS 629.00 UPPER VENT STRINGER TABS ARE CRACKED AT STRINGER 13 AND 14 AT UPPER RIB ATTACHMENTS. CRACKS STOP DRILLED AND REPAIR CARRIED OUT IAW EO B727-5710-1325.

Part: INTERCOSTAL — CRACKED (BS 1233)

INSPECTION TYPE-C, SUSPECT CRACK ON INTERCOSTAL SUPPORT ON HORIZONTAL WEB OF LT AIRSTAIR TORQUE BOX AT BS 1233. CRACKS STOP DRILLED AND INTERCOSTAL REPAIRED IAW SRM 5-10-2 FIG 6 AND SRM 51-40-3 FIG 1.

Part: SKIN — GOUGED (LT TE FOREFLAP)

INSPECTION TYPE-C, LT INBOARD FOREFLAP SEVERAL DEEP GOUGES ON UPPER SKIN. FOREFLAP REPLACED IAW MM27-51-01.

Part: SKIN — CORRODED (BS 1170-1183)

INSPECTION TYPE-C, AREAS OF LIGHT SURFACE CORROSION ON FUSELAGE SKIN BETWEEN BS 1170 AND 1183, BETWEEN STRINGER 5 AND 8 LEFT HAND. CORROSION REMOVED AND DAMAGE REPAIRED IAW SRM 53-30-3 FIG 14.

Part: SKIN — CRACKED (LT EMER EXIT)

INSPECTION TYPE-C, FWD LEFT HAND OVERWING EXIT HAS CRACK IN SKIN AT TOP END OF EXIT. AREA REPAIRED IAW SRM 52-20-2.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, SUSPECT CORROSION FOUND ON BODY STATION 740 FITTING RT. NEW FITTING INSTALLED IAW UPS EO B727-5310-7477 AND SKIN REPAIR CARRIED OUT IAW SRS EO 97-29-007.

Part: FITTING — CORRODED (BS 740)

INSPECTION TYPE-C, SUSPECT CORROSION FOUND ON BS 740 FITTING LT. LT BS 740 FITTING REPLACED IAW UPS EO B727-5310-7472 AND SKIN REPAIR CARRIED OUT IAW SRS EO 97-29-005 UPS ENG FILE NUMBER 727-53-1966.

Part: SKIN — DELAMINATED (LT TE FLAP)

INSPECTION TYPE-C, DELAMINATION 18 LONG ON LT OUTBD T/E FLAP 38 FROM INBD FLAP EDGE, 9 FROM TOP. DEFERRED DEFECT D128974. LEFT AND OUTBOARD TRAILING EDGE FLAP REPAIRED IAW SRM 51-40-6.

Part: SKIN — GOUGED (BS 348)

INSPECTION TYPE-C, INSTALL PERMANENT REPAIR TO GOUGE IN FUSELAGE, RIGHT HAND SIDE APPROX BS 348 AT STRINGER 19 (DAMAGE 0.020 DEEP, 1 0.75 DIAMETER). REPAIR CARRIED OUT IAW SRM 53-30-3 FIGURE 13.

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

INSPECTION TYPE:N/A, UPON REMOVAL OF MAIN CARGO DOOR FOUND UPPER DOORWAY FRAME WEB FROM STA 480 TO 620 TO HAVE CORROSION ON IT. REMOVED CORRODED WEB AND DOUBLERS FABRICATED NEW PARTS AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.

Part: BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE:N/A, UPON REMOVAL OF MAIN CARGO DOOR RAIN DAM FOUND MAIN CARGO DOOR UPPER BEAM CORRODED. REMOVED CORRODED PARTS AND INSTALLED NEW PARTS IAW SRM 51-30-2, 53-10-1.

Part: SEAT TRACK — CRACKED (BS 870)

SEAT TRACK AT BS 870 LBL 1 WL 208 HAS CORNER CRACKED OFF. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5.

Part: SKIN — DELAMINATED (LT TE FLAP)

WHILE ON GROUND, MAINTENANCE FOUND LEFT WING INBOARD FLAP TE 3 INCHES FROM OUTBOARD EDGE DELAMINATED 17 INCHES BY 4 INCHES, T/E IS SPLIT 3 INCHES. MAINTENANCE REMOVED AND REPLACED AFT FLAP ASSY IAW MM 27-51, OPS CK NORMAL.

Part: WEB — CRACKED (BS 1110-1130)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON WEB AROUND FASTENER HOLES, STA 1110-1130, RBL 26, WL 208. INSTALLED REPAIR PER SRM 51-10-1, 51-10-2, 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON LWR FLANGE OF FLOOR BEAM BS 740, WL 199, RBL 4-LBL 4. INSTALLED REPAIR PER UPS EO B727-5310-6752A.

Part: SKIN — CORRODED (BS 850-863)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON INTERNAL SKIN AT STA 850-863, WL 192, RBL 70. INSTALLED REPAIR PER UPS EO B727-5310-6754A.

Part: SKIN — CORRODED (BS 870-855)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON INTERNAL SKIN BS 870-855, WL 192, LBL 70. INSTALLED REPAIR PER UPS EO B727-5310-6754.

Part: NR 1 KFLAP — CORRODED (LT WING)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED PER MM 27-81-01.

Part: CHORD — CRACKED (LT WING)

WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER CHORD LEFT WING STA 656.5, S-8 VENT BOX, FWD. INSTALLED REPAIR PER SB 727-57-0127.

Part: SPAR CHORD — CRACKED (WS 71-73)

WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER SPAR CHORD RT WING BS 870, WS 71-73. INSTALLED REPAIR PER UPS EO B727-5710-6737A, B727-5710-6722A.

Part: FUEL CELL CUTOUT — CORRODED (RT WING)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON LWR SURFACE OF RT WING FUEL CELL CUT OUT 7606. INSTALLED REPAIR PER UPS EO FILE NR B727-57-1088.

Part: FORGING — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 870 BODY FORGING, FWD SIDE, WL 190, LBL 65-70. INSTALLED REPAIR PER UPS EO B727-5310-6769.

Part: CENTER TANK SKIN — CRACKED (BS 763)

WHILE IN "D" CHECK MAINTENANCE FOUND CRACKS EMANATING FROM FASTENER HOLES AFT ON SKIN LWR SURFACE CENTER TANK AT BS 763, RBL 70 WL 201. REPAIRED PER UPS EO B727-5710-6738A.

Part: FORGING — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 740 BODY FORGING WL 206-208, LBL 65. INSTALLED REPAIR PER UPS EO B727-5310-6770A.

Part: RIB CHORD — CORRODED (WING/BODY)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON UPPER VERTICAL FLANGE OF THE WING TO BODY RIB UPPER CHORDS AT BS 760, RBL 70.5, AND LBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-1271F.

Part: FWD TRUNNION — CORRODED (RT MLG)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON RT MLG RT FWD TRUNNION FITTING INNER FACES AROUND BUSHING BORES. REPLACED PER SRM 51-30-2.

Part: FRAME — CRACKED (BS 500)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 500 AT OR NEAR STRINGER 21-26R. STRINGER 19R HAS CRACK AT SAME LOCATION. INSTALLED REPAIR PER SRM 51-10-2, 51-40-5, 51-40-3, 51-30-2.

Part: CHORD — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FLANGE OF THE 740 CHORD RBL 10-45. INSTALLED REPAIR PER UPS EO B727-5710-6628A AND B727-5710-6763.

Part: FORGING — CORRODED (BS 740)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 740 BODY FORGING WL 206-209, RBL 65. INSTALLED REPAIR PER UPS EO B727-5310-6770A.

Part: FORGING — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 870 BODY FORGING WL 208.1, RBL 59-64, UNDER FLOOR BEAM. INSTALLED REPAIR PER UPS EO B727-5310-6771A.

Part: WEB — CORRODED (BS 1110-1130)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STA 1110-1130, RBL 60-65, WL 208. INSTALLED REPAIR PER SRM 51-10-6, 51-40-0.

Part: FORGING — CORR/CRACKED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACKS AND CORROSION ON 870 BODY FORGING FLANGES WL 207-205, LBL 58-LBL 64. INSTALLED REPAIR PER UPS EO B727-5310-6771A.

Part: NR 5 SPOILER — DELAMINATED (LT WING)

WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 5 SPOILER. INSATLLED REPAIR PER SRM 51-40-6, 57-50-6.

Part: STRINGER — CORRODED (BS 464)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON STRINGER 24R AT BS 464. INSTALLED REPAIR PER SRM 51-20-1, 51-30-23.

Part: FRAME — CRACKED (BS 480)

WHILE IN 'D' CHECK, MAINTENANCE FOUND TWO CRACKS ON FRAME AT BS 480, BETWEEN STRINGERS 22L AND 23L. INSTALLED REPAIR PER UPS EO B727-5310-6760A.

Part: NR 3 LE FLAP — CORRODED (RT WING)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED PER MM 27-81-01.

Part: NR 4 SPOILER — DAMAGED (LT WING)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE ON NR 4 SPOILER. REPLACED PER MM 27-61-01.

Part: NR 6 KFLAP — CORRODED (RT WING)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP. REPLACED PER MM 27-81-01.

Part: SPAR CHORD — CORRODED (WS 102-114)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON RT WING LWR AFT SPAR CHORD BS 870, RT WING STA 102-114. INSTALLED REPAIR PER SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1050)

WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 1050, RBL 60, WL 180. INSTALLED REPAIR PER SRM 53-10-1, 51-30-00, 51-10-2, 51-30-2, AND MM 51-20-151.

Part: FWD FLANGE — CORRODED (BS 950)

WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON THE FWD FLANGE BS 950, RBL 58, WL 208. REPAIRED PER UPS EO FILE NR B272-53-1528.

Part: SEAT TRACK — CORRODED (BS 960-1176)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON FLANGES OF SEAT TRACK STA 960-1176, BL 0, WL 208. INSTALLED REPAIR PER SRM 53-10-1, 51-10-1, 51-30-2.

Part: FRAME — CORRODED (BS 500)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 500, NEAR STR 20-24L. INSTALLED REPAIR PER SRM 53-10-2, 51-40-3, 51-30-2.

Part: STIFFENER — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, LBL 8.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1.

Part: FRAME — CORRODED (BS 1090)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT BS 1090, RBL 70.5, WL 202. REPLACED PER SRM 51-30-2, 51-10-1, 51-10-2, MM 51-20-151.

Part: STRINGER — CORRODED (BS 510)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 21L AT BS 510. INSTALLED REPAIR PER SRM 53-10-3.

Part: SEAT TRACK — CORRODED (BS 570-640)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION IN FWD CARGO BAY IN 'WELL' OF FLOOR TRACK AT STA 570-640, LBL 18, WL 155. INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, 51-10-02.

Part: FRAME — CRACKED (BS 660)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 660 BETWEEN STR 22-23L, AND FRAME CRACKED AT STR 25L. INSTALLED REPAIR PER SRM 51-40-3.

Part: STIFFENER — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, RBL 8.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1.

Part: STIFFENER — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, RBL 16.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1.

Part: ANGLE — CORRODED (BS 760)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON ANGLE AT BS 760 LBL 62 WL 205 ATTACHED TO FUSELAGE FRAME. INSTALLED REPAIR PER SRM 51-30-2, 51-20-4, 51-10-2, 51-20-1.

Part: SEAT TRACK LINK — CORRODED (BS 740-760)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK EXPANSION LINK FROM BS 740-760, LBL 45, WL 208. INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, OHM 20-50-03.

Part: SPLICE PLATE — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON UPPER SPLICE PLATE BS 870, RBL 65-70. REPLACED PER SRM 51-10-1, 51-30-2, 51-20-4.

Part: EXPANSION LINK — CORRODED (BS 740-760)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK BOLT ATTACH POINTS BS740-760, LBL 25, WL 207. INSTALLED REPAIR PER SRM 51-10-6, 51-10-1, 51-10-2, 51-20-4, 51-30-2, OHM 20-50-3, MM51-20-151.

Part: STRINGER — CORRODED (BS 1050)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON AFT UPPER AND LWR SIDES OF STR 20R, BS 1050, RBL 60, WL 180. INSTALLED REPAIR PER SRM 53-10-3, 51-30-2,51-20-21.

Part: SKIN — CORRODED (NR 2 LE FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED PER MM 27-81-00, 27-81-01.

Part: NR 3 SPOILER — DAMAGED (LT WING)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE AND CONTAMINATION ON NR 3 SPOILER. REPLACED PER MM 27-61-01.

Part: BODY FORGING — CORRODED (BS 870)

WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STA 870 BODY FORGING, WL 90, RBL 65-70. INSTALLED REPAIR PER SRM 51-10-6, 51-10-2, 51-30-10, OHM 20-10-3, MM 51-20-00.

Part: STIFFENER — CORRODED (BS 740)

DURING 'D' CHECK MAINTENANCE REPORTED CORROSION ON VERTICAL STIFFENER CONNECTING UPPER AND LOWER KEEL BEAM AT BS 740, RBL 13, WL 163. REPLACED STIFFENER PER SRM 51-30-2.

Part: FLOOR BEAM — CRACKED (BS 870)

DURING 'D' CHECK MAINTENANCE REPORTED CRACK IN FLOOR BEAM AT STA 870. REPLACED FLOOR BEAM PER SRM 51-10-1.

Part: BLKHD ANGLE — CORRODED (BS 740)

DURING 'D' CHECK MAINTENANCE REPORTED CORROSION ON ANGLE ON PRESSURE BULKHEAD AT BS 740, WL 170. REPLACED ANGLE AND SIDE LOAD BEAM PER SRM 51-10-1, 51-10-2, 51-20-1.

Part: EXPANSION LINK — CORRODED (BS 740-760)

DURING 'D' CHECK MAINTENANCE REPORTED EXPANSION LINK CORRODED AT BS 740-760, RBL 45, WL 207. REPLACED LINK PER SRM 51-30-2, 53-10-1.

Part: STIFFENER — CORRODED (BS 294-300)

DURING 'D' CHECK MAINTENANCE REPORTED HORIZONTAL STIFFENER CORRODED AT BS 294-300, RBL 15, WL 178. REPLACED STIFFENER PER SRM 51-30-5, 51-10-1, 51-30-1.

Part: STRINGER — CRACKED (FS 294.5)

DURING 'D' CHECK MAINTENANCE FOUND CRACKS IN STRINGERS 14L, 15L, 16L AT STA 294.5. REPAIRED PER UPS EO B727-5310-1259F.

Part: STRINGER — CRACKED (BS 352.5)

DURING 'D' CHECK MAINTENANCE FOUND CRACK AT STA 352.5, STR 20, WL 120. REPAIRED PER SRM 53-10-3.

Part: FRAME — CORRODED (BS 600)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 600 FRAME, STR 22-23L. REPAIRED FRAME PER SRM 51-40-3, 51-30-2.

Part: STIFFENER — CORRODED (BS 870-880)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON PRESSURE WEB STIFFENER AT RBL 45, WL 202, BS 879. REPLACED STIFFENER PER SRM 51-10-1, 51-30-2.

Part: FRAME — CORRODED (BS 640)

DURING 'D' CHECK MAINTENANCE FOUND FRAME CORRODED AT BS 640, STR 20L, 22L, 23L, 25L. REPAIRED FRAME PER SRM 51-40-3.

Part: SEAT TRACK — CORRODED (BS 858)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK AT BS 858, RBL 1, WL 208. REPLACED SEAT TRACK PER SRM 51-30-2.

Part: WEB — CORRODED (BS 870)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL WEB AT STA 870, LBL 10-25, WL 200. REPLACED WEB PER SRM 51-20-4, 51-30-2.

Part: SEAT TRACK — CORRODED (FS 848-870)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION IN WELL OF SEAT TRACK ON EXPANSION LINK AT STA 848-870. REPLACED SEAT TRACK PER SRM 51-30-2, 51-10-1.

Part: STRINGER — CORRODED (BS 1110)

DURING 'D' CHECK MAINTENANCE FOUND STRINGER 4L CORRODED AT BS 1110. REPAIRED STRINGER PER SRM 53-10-3.

Part: EXPANSION LINK — CORRODED (BS 850-870)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 850-870, RBL 45, WL 207. REPLACED LINK PER SRM 51-30-2, 51-10-1.

Part: BLKHD STIFFENER — CORRODED (BS 740)

DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 740 BULKHEAD STIFFENER AT RBL 14. REPAIRED PER SRM 51-10-2, 51-30-2.

Part: STRINGER — CORRODED (BS 721-736)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 25L, STA 721-736. REPAIRED PER SRM 53-10-03.

Part: FRAME — CRACKED (BS 572)

DURING "C" CHECK MAINTENANCE FOUND CORR AND CRACK ON FWD CARGO DOOR AFT A/C FRAME, BS 572, STR 25 AND 26R. REPAIRED PER SRM 51-30-02.

Part: FRAME — CORRODED (BS 600)

DURING "C" CHECK MAINTENANCE FOUND CORR ON FRAME BS 600, STR 17-28R. REPAIRED PER SRM 51-30-02.

Part: STIFFENERS — CORRODED (BS 312-344)

DURING "C" CHECK MAINTENANCE FOUND CORR ON FWD ENTRY DOOR SILL LWR STIFFENERS AT NUT PLATE HOLES BS 312-344, WL 208, LBL 58 AND 61. REPAIRED PER SRM 51-30-02.

Part: STRINGER — CORRODED (BS 304-440)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 3R, BS 304-328, 360-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04.

Part: RIB — CORRODED (LT HORIZ STAB)

DURING "C" CHECK MAINTENANCE FOUND CORR ON LT HORIZ STAB UPPER CLOSURE RIB CHORD, I/B END. REPAIRED PER SRM 51-30-2.

Part: WEB — CORRODED (BS 785-805)

DURING "C" CHECK MAINTENANCE FOUND CORR ON WEB STA 785-805, RBL 62-70, WL 208. REPAIRED PER SRM 51-30-02.

Part: STRINGER — CORRODED (BS 360)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 22R, BS 360, WL 140, RBL 45. REPAIRED PER SRM 53-10-03, MM 53-11-00.

Part: STRINGER — CORRODED (BS 304-440)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 5R, BS 304-328, 344-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04.

Part: SILL — CORRODED (FWD ENTRY DOOR)

DURING "C" CHECK MAINTENANCE FOUND CORR ON FWD ENTRY DOOR SILL BS 297-360, WL 208, LBL 57. REPAIRED PER SRM 51-30-02.

Part: STRINGER — CORRODED (BS 304-440)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 2R, BS 304-440, ON FLANGES AND SIDES. REPAIRED PER SRM 53-10-03, 51-30-02.

Part: FRAME — CRACKED (BS 480)

DURING "C" CHECK MAINTENANCE FOUND CORR AND A CRACK ON FRAME BS 480, STR 23-25R. REPAIRED PER SRM 51-40-03.

Part: CHORD — CORRODED (NR 6 SLAT)

DURING "C" CHECK MAINTENANCE FOUND CORR ON NR 6 SLAT LWR CHORD AT ROD END CUT OUT. REPAIRED PER SRM 57-50-02.

Part: STRINGER — CORRODED (BS 304-440)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 4R, BS 304-328, 344-360, 360-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04.

Part: STRINGER — CORRODED (BS 308)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 20R, BS 308, WL 189. REPAIRED PER SRM 53-10-03, 51-30-02, MM 51-31-0, 51-20-21, 51-20-31.

Part: TIE — CRACKED (BS 740)

DURING "C" CHECK MAINTENANCE FOUND CRACK ON STRINGER 7R TIE, FWD SIDE OF BS 740. REPAIRED PER SRM 51-30-02.

Part: FRAME — CORRODED (BS 520)

DURING "C" CHECK MAINTENANCE FOUND CORR ON FRAME BS 520, STR 20-24L. REPAIRED PER SRM 51-40-3.

Part: FLOOR BEAM — CORRODED (BS 1030)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 1030, RBL 41, WL 208. REPAIRED FLOOR BEAM PER SRM 53-10-8.

Part: STIFFENER — CORRODED (BS 770)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON DELTA BEAM WEB AT BS 770, LBL 5, WL 148. REPLACED STIFFENER PER SRM 51-10-1, 51-30-2, 51-20-4.

Part: FRAME — CORRODED (BS 560)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT BS 560, STR 22L-24L. REPAIRED FRAME PER SRM 51-40-03.

Part: STIFFENER — CORRODED (BS 300)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER AT BS 300, RBL 15, WL 208. REPAIRED STIFFENER PER SRM 53-10-1, 51-30-2, 51-20-4, 51-10-1.

Part: FRAME — CORRODED (BS 620)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT BS 620, STR 19R-23R. REPLACED FRAME AT BS 620, STR 19R-23R PER SRM 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 580)

DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 580, RBL 47-59, WL 201. REPAIRED FLOOR BEAM PER UPS EO FILE NUMBER 727-53-1482.

Part: STRINGER — CORROSION (BS 360-400)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AT NR 2 STR LT STA 360-400; ON FLANGES/SIDES. INSTALLED REPAIR IAW SRM 53-10-3, 51-30-2 AND 53-10-4.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION BS 870 WEB STIFFENER AT LBL 57.5. INSTALLED REPAIR IAW SRM 51-30-2.

Part: FLOOR — CORROSION (FS 950)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FASTENERS THROUGH PRESSURE FLOOR STA 950 LBL 28 WL 201. INSTALLED REPAIR IAW SRM 51-30-02 AND 51-20-04.

Part: RIB — CRACK (RT TE MID-FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND R/W O/B MID-FLAP I/B FOREFLAP SUPPORT RIB IS CRACKED ON FLANGE BETWEEN FASTENERS ON I/B SIDE. INSTALLED REPAIR IAW SRM 51-30-2 AND 57-50-4.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB STIFFENER AT RBL 57 OUT OF LIMITS. INSTALLED REPAIR IAW SRM 51-30-2.

Part: SKIN — CORROSION (FS 740-758)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION UPPER FUEL CELL SKIN STA 740-758 RBL 25-62. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-6, 57-30-2 AND OHM 20-10-03.

Part: FLOOR BEAM — CORROSION (BS 680)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM BS 680 RBL 15-45 WL 208. INSTALLED REPAIR IAW SRM 53-10-8.

Part: STIFFENER — CORROSION (FIN STA 233.746)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL FIN INTERSPAR SKIN STIFFENER RT SIDE AT VERTICAL FIN STA 233.746 INSIDE VERTICAL FIN. INSTALLED REPAIR IAW 51-30-5 AND 51-30-2.

Part: FLOOR BEAM — CORROSION (FS 1110)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM STA 1110 LBL 60 AND LBL 43-3 WL 208. INSTALLED REPAIR IAW SRM 53-10-8.

Part: FLOOR BEAM — CORROSION (BS 600)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 600 TOP CHORD RBL 48-61 WL 208. INSTALLED REPAIR IAW 53-10-8.

Part: BUTT JOINT — CORROSION (FS 479)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD SIDE OF BUTT JOINT STA 479 BETWEEN STR 9 AND 10. INSTALLED REPAIR IAW EO 727-5310-1371 APPEN. 8.5, BOEING DWG 69-62161 AND SRM'S 51-10-02 AND 51-30-02.

Part: CARRIAGE — CORROSION (NR 5 TE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 5 FLAP CARRIAGE SPINDLE. INSTALLED REPAIR IAW MM 27-51-03.

Part: SEAT PEDESTAL — CRACKS (BS 228-245)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKS ON BOTH UPPER AND LOWER AFT FLANGES OF INBOARD AFT CAPT'S SEAT PEDESTAL AT LBL 12 WL 208 BS 228-245. INSTALLED REPAIR IAW SRM 51-20-1 AND 51-30-2.

Part: ANGLE — CORROSION (FS 545-556)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CARGO DOOR THRESHOLD ANGLE BS 545-556 RBL 28 WL 154. INSTALLED REPAIR IAW SRM 51-30-2.

Part: SHEAR TIE — CRACKED (BS 1030)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SHEAR TIE AT BS 1030 WL 185 RBL 55 (BETWEEN STR 19R-20R). INSTALLED REPAIR IAW SRM 51-40-3 AND 53-10-2.

Part: SPAR CHORD — CORROSION (LT HORIZ STAB)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LT HORIZONTAL STAB LOWER REAR SPAR CHORD AT STAB. STA 223 STA 194-200 AND STA 186. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND BS 870 WEB STIFFENER AT LBL 45 CORRODED OUT OF LIMITS. INSTALLED REPAIR IAW SRM 51-10-2.

Part: STRINGER — CORROSION (FS 710-714)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AT STA 710-714 STRINGER 21L. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 480)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED STRINGER BS 480 STR 25 RT RBL 31 WL 154. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2 AND 51-10-3.

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

WHILE IN 'D' CHECK MAINTENANCE FOUND SEAT TRACK STA 344-360 LBL 60 WL 208 TO HAVE CORROSION IN FASTENERS HOLES. INSTALLED REPAIR IAW SRM 51-30-2.

Part: SKIN — CORROSION (BS 754-773)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION BS 754-773 UPPER FUEL CELL SKIN RBL 25-44 WL 205. INSTALLED REPAIR IAW UPS EO 727-57-1075.

Part: STRINGER — CORROSION (FS 360-380)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 3 STRINGER LT; FLANGES STA 360-380. INSTALLED REPAIR IAW SRM 53-10-1, 53-10-3, 51-10-2, 51-30-2 AND MM 51-20-151.

Part: SPAR CHORD — CORROSION (RT HORIZ STAB)

WHILE IN 'D' CHECK MAINTENANCE FOUND RT HORIZONTAL STAB. CLOSURE RIB UPPER CHORD IS CORRODED ON BOTTOM SIDE OF FLANGE AND CRACKS RUNNING FROM FASTENER TO FASTENER. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRINGER — CORROSION (FS 259-277)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STR 2R FROM STA 259-277 AROUND NUTPLATES. INSTALLED REPAIR IAW SRM 51-30-2, 53-10-1 AND MM 20-43-01.

Part: WEB — CORROSION (BS 311)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL WEB DOUBLER RBL 15 WL 175 BS 311. INSTALLED REPAIR IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SKIN — CORROSION (TE MID FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND WINGS 321 I/B MIDFLAP LOWER AFT SKIN CRACKED AT AFT EDGE BEHIND NR 4 CARRIAGE. INSTALLED REPAIR IAW SRM 57-50-4.

Part: FLOOR BEAM — CORROSION (BS 720)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES BS 720 RBL 45-62 WL 208. INSTALLED REPAIR IAW SRM 53-10-8.

Part: FLOOR BEAM — CORROSION (FS 294)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STA 294 FLOOR BEAM AROUND NUTPLATES WL 208 LBL 30 TO RBL 10. INSTALLED REPAIR IAW UPS EO 727-53-1461.

Part: FLOOR BEAM — CORROSION (BS 326)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 326 WL 208 RBL 14-LBL 55. INSTALLED REPAIR IAW UPS EO B727-5310-6625.

Part: STRINGER — CORROSION (BS 1080-1088)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BACKSIDE OF STRINGER AT BS 1080-1088 STRINGER 20L. INSTALLED REPAIR IAW SRM 53-10-3, 51-70-2.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB STIFFENER AT LBL 28. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRINGER — CORROSION (FS 520-540)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER STA 520-540 STR 3 RT SIDE. INSTALLED REPAIR IAW SRM 53-10-3.

Part: INTERCOSTAL — CORROSION (FS 326-344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INTERCOSTAL FROM BS 326-344 WL 208 RBL 42. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRAP — CORRODED (FS 970-1050)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATES BS 970-1050 LBL 2-RBL 2 ON CEILING STABILIZER STRAP. INSTALLED REPAIR IAW SRM 51-10-1, 51-30-2, 51-10-2 AND MM 51-20-31.

Part: FLOOR BEAM — CORROSION (FS 1030)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND AND UNDER BOLTS AT BS 1030 RBL 56-63 WL 201 ON LOWER FLANGE OF FLOOR BEAM. INSTALLED REPAIR IAW B727-5310-6627A.

Part: CHANNEL — CORROSION (FS 230)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S AFT SEAT PEDESTAL FORWARD INTERCOSTAL AT STA 230 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 53-10-1, 51-20-1 AND 51-10-2.

Part: SEAT PEDESTAL — CORROSION (FS 246)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S AFT SEAT PEDESTAL AFT INTERCOSTAL AROUND BOLT HOLES THROUGH FLOOR AT STA 246 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2 AND 53-10-1.

Part: HAT CHANNEL — CORROSION (FS 344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION THROUGHOUT HAT CHANNEL BOTH TOP AND BOTTOM SIDES AT BS 344 WL 208 RBL 17-61. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-1 AND 51-30-2.

Part: FLOOR BEAM — CORROSION (FS 540)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 540 UNDER NUTPLATE LBL 41-55 WL 208. INSTALLED REPAIR IAW UPS EO B 727-5310-6647.

Part: CHANNEL — CORROSION (FS 227)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S FORWARD SEAT PEDESTAL, AFT INTERCOSTAL STA 227 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-1, 53-10-1 AND 51-10-2.

Part: FLOOR BEAM — CORROSION (FS 312)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 312 WL 208 FROM RBL 14 TO LBL 55. INSTALLED REPAIR IAW UPS EO NR B727-5310-6624.

Part: FLOOR BEAM — CORROSION (FS 344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 344 WL 208 FROM RBL 65 TO LBL 65. INSTALLED REPAIR IAW UPS EO NR B727-5310-6623A AND SRM 51-30-2.

Part: INTERCOSTAL — CORROSION (BS 326-344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INTERCOSTAL IN SEVERAL AREAS BS 326-344, LBL 30, WL 208. INSTALLED REPAIR IAW SRM 51-10-1AND 51-30-2.

Part: SPAR — CRACKED (HORIZ STAB)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT FRONT STAB STA 124 HAS CRACK IN UPPER SPAR IN STAB, UPPER FLANGE WHERE SPAR HAS BEEN PREVIOSLY BLENDED. (CORROSION ALSO FOUND). INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2, 55-10-2, AND 65-20661.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON WEB STIFFENER BS 870 RBL 51. INSTALLED REPAIR IAW SRM 51-30-2.

Part: BULKHEAD — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD SIDE OF 870 BULKHEAD WEB AT TEARSTRAP ON MAIN LANDING GEAR BULKHEAD FROM, LBL 20 RBL 30 WL 160. INSTALLED REPAIR IAW SRM 53-10-9, 51-30-2 AND UPS EO 727-53-1462.

Part: EXPANSION LINK — CORROSION (FS 740-760)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON EXPANSION LINK AROUND NUTPLATES STA 740-760, RBL 25, WL 208. SEAT TRACK ALSO FOUND OUT OF LIMITS. INSTALLED REPAIR IAW OHM 20-50-03 AND 20-50-01, 51-10-1, 51-10-2, 51-10-6, 51-20-4, 51-30-2 AND MM 51-20-151. (P/N 69-24621-3 AND 65-34144-23).

Part: RIB — CRACKED (NR 3 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT 9TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON WEB STIFFENER BS 870 RBL 24.5. INSTALLED REPAIR IAW SRM 51-30-2.

Part: TRACK — CRACKED (NR 8 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT I/B AND O/B TRACK COMMON TO SKIN ANGLES ARE CRACKED. INSTALLED REPAIR IAW UPS OHM 57-51-31, SRM 51-30-2 AND IPC 57-50-1-1.

Part: BEAM — CORROSION (LT HORIZ STAB)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LT HORIZ. STAB. LOWER T/E BEAM AT ELEVATOR STA 169-157, STA 142 AND STA 125-121. INSTALLED REPAIR IAW SRM 51-30-2.

Part: SKIN — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LOWER SIDE OF UPPER FUEL SKIN BS 870, LBL 65 AND RBL 65. INSTALLED REPAIR IAW SRM 51-30-2 AND UPS EO 727-57-1081.

Part: RIB — CRACKED (NR 6 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RT (O/B) ACTUATOR ATTACH POINT RIB FLANGE IS CRACKED COMMON TO COVE PANEL LOWER ATTACHMENT STRINGER. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.

Part: RIB — CRACKED (NR 5 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT THIRD RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.

Part: HINGE FITTING — CORROSION (MID GALLEY DOOR)

WHILE IN 'D' CHECK MAINTENANCE FOUND MID GALLEY DOORWAY UPPER HINGE CUTOUT CASTING TO BE CORRODED. INSTALLED REPAIRS IAW SRM 51-30-2, 51-10-2, 51-30-5, 51-20-4, 51-30-8 AND OHM 20-41-02. (PART NUMBERS - 65-18252-3 AND 65-16722-58).

Part: FRAME — CORROSION (BS 580)

WHILE IN 'D' CHECK MAINTENANCE FOUND FASTENER HOLES ON THE BS 580 FRAME AT OR NEAR STR 19R TO 22R EXHIBITS CORROSION INDICATION. INSTALLED REPAIR IAW SRM 51-40-3.

Part: SKIN — DISBONDED (NR 14 SPOILER)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 14 SPOILER HAS AN AREA OF DISBOND ON I/B FORWARD CORNER UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-20-151.

Part: FLAP — CORROSION (NR 2 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND DAMAGE DUE TO EXCESSIVE CORROSION, REMOVED AND REPLACED NR 2 K-FLAP. INSTALLED REPAIR IAW MM 27-81-1.

Part: RIB — CRACK (NR 5 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT 2ND RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.

Part: SKIN — CORROSION (BS 860-870)

WHILE IN 'D' CHECK MAINTENANCE FOUND UPPER FUEL CELL SKIN CORRODED AT BS 860-870, LBL 60-70. INSTALLED REPAIR IAW UPS EO 727-57-1081.

Part: ANGLE — CORROSION (FS 350)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON ANGLE BS 350 WL 170-174 LBL 15. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-10-1 AND 51-30-2.

Part: RIB — CRACKED (NR 6 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT 3RD RIB OUT FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.

Part: RIB — CRACK (NR 5 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT 4TH RIB IN FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.

Part: STIFFENER — CORROSION (FS 344)

WHILE IN 'D' CHECK MAINTENANCE FOUND STIFFENER CORRODED BEYOND LIMITS AT BS 344 LBL 15 WL 169. INSTALLED REPAIR IAW SRM 51-20-4, 51-10-1, 51-10-2 AND 51-30-2.

Part: CHORD — CRACKED (FS 344-351)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN HORIZONTAL FLANGE OF UPPER LEFT HAND NOSE CHORD FROM BS 344-351, LBL 15, WL 169; CRACK RUNS TO A PREVIOUS REPAIR AT BS 340. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-1, 51-20-4 AND 51-30-2.

Part: FLAP — CORROSION (NR 6 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP O/B UPPER ATTACH LUG I/B SIDE AROUND FASTENERS. INSTALLED REPAIR IAW SRM 57-50-1.

Part: FLAP — CORROSION (NR 7 TE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 7 FLAP CARRIAGE SPINDLE AND YOKE. INSTALLED REPAIR IAW MM 27-51-13.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB WL 171 STIFFENER AT LBL 50.5. INSTALLED REPAIR IAW SRM 51-30-2.

Part: DOORWAY STOP — CORROSION (FS 740-760)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON AFT CARGO DOORWAY STOP PAD FITTING ON AFT DOORWAY AT STR 24. INSTALLED REPAIR IAW SRM 51-30-2 AND 51-10-2.

Part: BEAM — CORROSION (BS 745)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LOWER LONGITUDINAL BEAM CHORD, RBL 13 WL 157 BS 745. INSTALLED REPAIR AIW SRM 51-10-2, 51-30-2 AND 51-40-4.

Part: FLAP — CORROSION (NR 3 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP I/B LOWER BONDING JUMPER UPPER AND LOWER ATTACH POINTS. INSTALLED REPAIR IAW SRM 57-50-1.

Part: DOOR THRESHOLD — CORROSION (FS 304)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLIGHT DECK DOOR THRESHOLD SILL AROUND NUTPLATES AT STA 304, WL 208, RBL 12, LBL 8. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2 AND 51-10-6.

Part: FITTING — CORROSION (CARGO DOORWAY)

WHILE IN 'D' CHECK MAINTENANCE FOUND AFT CARGO DOORWAY STOP PAD FITTING ON AFT DOORWAY AT STR 25 TO BE CORRODED. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-30-2.

Part: RIB — CRACKED (NR 8 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 2ND RIB IN FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND DWG 65-16224.

Part: RIB — CRACK (NR 6 LE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT 3RD RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.

Part: STIFFENER — CRACKED (ELEV STA 167)

WHILE IN 'D' CHECK MAINTENANCE FOUND BEAD STIFFENER CRACKED AT APROX. R.E.S. 167 APPROX. 3075 INCH FROM TRAILING EDGE. INSTALLED REPAIR IAW SRM 55-20-3.

Part: ATTACH LUG — CORROSION (NR 2 TE FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP O/B BULLNOSE ATTACH POINT LUG UPPER SURFACE AROUND FASTENERS. INSTALLED REPAIR IAW MM 27-81-1.

Part: RIB — CRACKED (NR 7 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT FIRST RIB ON O/B END CRACKED. INSTALLED REPAIR IAW 51-10-1 AND DWG 65-16223.

Part: CLIP — CORROSION (BS 1166)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER CLIP AT BS 1166 STRINGER 18R. INSTALLED REPAIR IAW SRM 53-10-3, 51-10-02, 51-30-2 AND MM 51-20-151.

Part: RIB — CRACKED (NR 4 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT NR 4 SLAT I/B END RIB CRACKED IN FWD RADIUS. INSTALLED REPAIR IAW SRM 51-30-02 AND OHM 57-51-61.

Part: RIB — CRACKED (NR 4 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT, 7TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B END RIB IS CRACKED. INSTALLED REPAIR IAW SRM 51-10-1.

Part: RIB — CRACKED (NR 8 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 1ST RIB FROM I/B IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2 AND DWG 65-16224.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B RIB AT I/B TRACK IS CRACKED AT FLANGE COMMON TO COVE PANELS AND IS NOT CONTAINED BY PREVIOUS REPAIR. INSTALLED REPAIR IAW BSRM 57-50-3.

Part: WEB — CRACKED (BS 1290)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1290 LBL 21 WL 180. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151.

Part: WEB — CRACKED (BS 1226)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1226 WL 188 RBL 21. INSTALLED REPAIR IAW SRM 51-20-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151.

Part: WEB — CORROSION (FS 251.6)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD AND AFT SIDE OF WEB STA 251.6 LBL 42 WL 218. INSTALLED REPAIR IAW SRM 53-10-2, 51-40-2, 51-30-2 AND MM 51-20-151.

Part: ANGLE — CRACKED (CARGO DOOR)

WHILE IN 'D' CHECK MAINTENANCE FOUND MAIN CARGO DOOR HAS CRACKED L ANGLE AT BS 540 STR 4. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-151.

Part: STRINGER — CORROSION (FS 835)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER 16 RT AT STA 835. INSTALLED REPAIR IAW SRM 51-10-2, 51-30-2, 51-20-4 AND MM 51-20-151.

Part: FLOOR BEAM — CORROSION (FS 480)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AND SEVERAL AREAS OF BARE METAL ON UPPER CHORD OF FLOOR BEAM AT BS 480 WL 208 FROM RBL 0-60. INSTALLED REPAIR IAW SRM 53-10-8.

Part: SPAR CHORD — CORROSION (RT HORIZ STAB)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON RIGHT HAND STAB. LOWER REAR SPAR CHORD AT STAB. STA 212-223 AND STA 172-169.

Part: RIB — CRACKED (RT TE MIDFLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED RIB ON THE RT WING O/B MID FLAP 9 INCHES IN FROM THE O/B END IN THE TRAILING EDGE COVE. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-30-5, 51-20-4 AND MM 51-20-151.

Part: RIB CHORD — CRACK (WS 686.5)

WHILE IN 'D' CHECK MAINTENANCE FOUND RIGHT WING RIB CHORD CRACKED AT WS 686.5 LOWER CHORD STRINGER 6. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-1, 51-10-2 AND 51-30-2.

Part: ANGLE — CRACKED (NR 7 ELEV HINGE)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SUPPORT ANGLE FOR NR 7 ELEVATOR HINGE RIB ON REAR SPAR CHORD WEB STAB STA 223.05 LT. INSTALLED REPAIR IAW SRM 51-30-2 AND DRAWING 65-16876.

Part: STIFFENER — CORROSION (BS 870)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 STIFFENER LBL 33. INSTALLED REPAIR IAW SRM 51-30-2, 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1130)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SHEAR TIE AT BS 1130, WL 186, STRINGERS 19R AND 20R. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 53-10-2.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 13TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 14TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.

Part: PANEL — CRACKED (NR 4 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT COVE PANEL CRACKED AT O/B UP STOP. INSTALLED REPAIR IAW SRM 51-20-1 AND 51-30-02.

Part: STRINGER — CORROSION (FS 1020)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER NR 2L ON UPPER FLANGE AT BS 1020. INSTALLED REPAIR IAW SRM 53-10-3.

Part: SKIN LAP — CORROSION (BS 683-685)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INNER SKIN LAP BS 683-685 STRINGER 4 RT. INSTALLED REPAIR IAW SRM 53-30-3.

Part: RIB — CRACKED (NR 4 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 4 SLAT, 6TH RIB FROM O/B END (JUST I/B OF O/B TRACK) IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01.

Part: SKIN — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND TAI SKIN CRACKED 1 INCH O/B OF O/B TRACK TO SLAT ATTACH POINT. INSTALLED REPAIR IAW EO 727-57-1080.

Part: RIB — CRACKED (NR 7 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND I/B TRACK O/B RIB FLANGE CRACKED. INSTALLED REPAIR IAW EO727-57-1078.

Part: RIB — CRACKED (NR 4 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT RT (I/B) ACTUATOR RIB CRACKED BETWEEN FLANGES COMMON TO SPAR AND UPPER SKIN. INSTALLED REPAIR IAW EO 727-57-1077.

Part: RIB — CRACKED (NR 6 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 13TH FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.

Part: RIB — CRACKED (NR 6 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 12TH FROM I/B END IS CORRODED. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-10-6 AND DWG 65-17296.

Part: FLOOR BEAM — CORROSION (BS 344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM WEB, DOUBLER AND BONDED DOUBLER BS 344, WL 208, RBL 11 TO 27. INSTALLED REPAIR IAW SRM 51-40-2 AND EO 727-53-1463.

Part: FLAP — CORROSION (NR 6 K FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 K FLAP CORRODED ON VERY INBD SIDE AT FASTENERS FOR END BULB SEAL. INSTALLED REPAIR IAW UPS EO B727-5740-3980.

Part: TRANSVERSE BEAM — CRACKED (AFT CARGO DOOR)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 2 TRANSVERSE BEAM. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRINGER — CORROSION (FS 540-560)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER NR 8R BS 540-560. INSTALLED REPAIR IAW SRM 53-10-1.

Part: RIB — CRACKED (LT TE MIDFLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP HAS CRACKED RIB IN T/E COVE 52 INCHES IN FROM INBOARD SIDE. INSTALLED REPAIR IAW SRM 51-30-2.

Part: WEDGE — CORROSION (LT TE MID FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP T/E WEDGE HAS NUMEROUS AREAS OF CORROSION. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-1.

Part: STIFFENER — CORROSION (BS 740)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL STIFFENER BS 740 WL 163 LBL 13. INSTALLED REPAIR IAW SRM 51-10-1 AND 51-30-2.

Part: ANGLE — CORROSION (FS 825)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRUCTURE SUPPORT ANGLE ON FORWARD SIDE OF UPPER CORD STUB BEAM STA 825 RBL 55-62 WL 208. INSTALLED REPAIR IAW SRM 51-10-01, 51-20-04 AND 51-30-2.

Part: WEDGE — CRACKED (LT TE MID FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SKIN SUPPORT CHORD ANGLE CRACKED AT NR 2 AFT FLAP TRACK CUTOUT. INSTALLED REPAIR IAW SRM 51-40-4, 51-20-2 AND OHM 20-50-02.

Part: WEB — CRACKED (BS 1256)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1256 WL 192 RBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 51-10-2 AND MM 51-20-151.

Part: WEB — CRACKED (BS 1226)

WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1226 WL 188 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 53-10-2 AND MM 51-20-151.

Part: RIB — CRACKED (NR 3 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 4TH FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.

Part: STIFFENER — CORROSION (BS 344)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STIFFENER WL 182 LBL 14 TO LBL 10 BS 344. INSTALLED REPAIR IAW SRM 51-10-6 AND 51-30-2.

Part: ANGLES — CRACKED (NR 1 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 1 SLAT I/B AND O/B TRACK TO SKIN ANGLES ARE CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND IPC 57-50-1.

Part: SKIN — CORROSION (FS 110)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON SKIN AT STR 4L STA 110. INSTALLED REPAIR IAW SRM 53-30-2, 53-30-1, 53-30-3.

Part: RIB — CRACKED (NR 7 SLAT)

WHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT 12TH RIB FROM I/B IS CRACKED COMMON TO LWR CHORD. INSTALLED REPAIR IAW SRM 57-50-3, PAGE 26, FIGURE 9.

Part: SUPPORT — CORROSION (TE MID FLAP)

WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON RT WING MID FLAP O/B FLAP CARRIAGE BEARING SUPPORT. INSTALLED REPAIR IAW MM 27-51-13.

Part: SKIN LAP — CORROSION (BS 927/940)

WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON SKIN LAP STR 4 LT AT STA 927, 940. INCLUDED STA 954-958 AT STR 4 LT.

Part: SUPPORT BLOCK — CORROSION (LT WING)

WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON LT WING O/B FLAP, I/B AFT SUPPORT BLOCK. INSTALLED REPAIR IAW MM 27-51-13.

Part: SUPPORT BLOCK — CORROSION (LT WING)

WHILE IN 'D' CHECK, MAINT FOUND CORROSION O/B FLAP O/B AFT SUPPORT BLOCK CORRODED AND WORN ON LEFT WING. INSTALLED REPAIR IAW MM 27-51-13.

Part: RIB MOUNT TAB — CRACKED (WS 656.5)

WHILE IN 'D' CHECK, MAINT FOUND VENT BOX STR 12 RIB MOUNT TAB CRACKED AT WS 656.5 (KIT P/N 65C26139-16), LT WING. INSTALLED REPAIR IAW SRM 57-10-4 AND SB 57A159.

Part: TRANSVERSE BEAM — CORROSION (AFT CARGO DOOR)

WHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR NR 1 TRANSVERSE BEAM CORRODED. INSTALLED REPAIR IAW SRM 51-30-2.

Part: STRINGER — CORROSION (BS 410)

WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON STR NR 23R BS 410 WL 164 RBL 42. INSTALLED REPAIR IAW SRM 53-10-3.

Part: UPPER GATE — CORROSION (FWD ENTRY DOOR)

WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON FORWARD ENTRY DOOR UPPER GATE. INSTALLED REPAIR IAW SRM 51-10-2, 51-30-2, 51-30-8 AND MM 51-20-151.

Part: TRANSVERSE BEAM — CRACKED (AFT CARGO DOOR)

WHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR HAS 2 CRACKS ON THE NR 3 TRANSVERSE BEAM AND WEB. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-30-2.

Part: BUTT JOINT — CORROSION (FS 441)

WHILE IN 'D' CHECK, MAINTENANCE FOUND STA 441, STR 6L TO 10L CORROSION EMANATING FROM FWD SIDE OF BUTT JOINT. INSTALLED REPAIR IAW EO B727-5310-1371E, APP. 8.5.

Part: FLAP — DELAMINATION (RT TE FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 72 INCHES FROM O/B END ON T/E. INSTALLED REPAIR IAW ARM 51-40-06.

Part: RIB — CRACKED (WS 656.5)

WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING RIB CHORD WAS CRACKED AT WING STA 656.5, LOWER CHORD S-8. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-2, 51-20-1, 51-30-2.

Part: FLAP — DELAMINATION (RT TE FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 31 INCHES FROM I/B END LOWER SURFACE. INSTALLED REPAIR IAW ARM 51-40-06.

Part: FLAP — DELAMINATION (RT TE FLAP)

WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 57 INCHES FROM I/B END. INSTALLED REPAIR IAW ARM 51-40-06.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 60 INCHES FROM I/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6.

Part: WEB — CORROSION (RT HORIZ STAB)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION IN WEB AT STA 68.92 INSIDE RT HORIZONTAL STAB. INSTALLED REPAIR IAW SRM 55-10-2, 55-10-1, AND 51-30-2.

Part: SUPPORT ROLLER — PITTED (NR 5 TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND R/W O/B FLAP I/B CARRIAGE (NR 5) AFT SUPPORT ROLLER IS PITTED. INSTALLED REPAIR IAW 51-10-6.

Part: HINGE — CORROSION (LT AILERON)

DURING 'D' CHECK, MAINTENANCE FOUND L/W, O/B AILERON, AFT I/B HINGE HALF IS CORRODED. INSTALLED REPAIR IAW MM 27-10-41.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS DENT WITH DELAMINATION 12 INCHES FROM O/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND 51-20-151.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS AREA OF DELAMINATION ON I/B T/E CORNER LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND MM 51-20-151.

Part: RIB — CRACKED (WS 629)

DURING 'D' CHECK, MAINTENANCE FOUND L/W RIB CHORD IS CRACKED WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP T/E HAS EDGE DELAMINATION AT O/B CORNER. INSTALLED REPAIR IAW SRM 51-40-6.

Part: RIB — CRACKED (WS 629)

DURING 'D' CHECK, MAINTENANCE FOUND R/W RIB CHORD IS CRACKED AT WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.

Part: SKIN — CORROSION (FS 1020)

DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AT SKIN LAP AT BS 1020, WL 188, RBL 55. INSTALLED REPAIR IAW SRM 53-30-3.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 86 INCHES FROM O/B END LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6.

Part: FRAME — CRACKED (FS 660)

DURING 'D' CHECK, MAINTENANCE FOUND FLOURESCENT LIQUID PENETRANT INSPECTION OF FASTENER HOLES ON BS 660 FRAME AT OR NEAR STRINGER 19R EXHIBIT A CRACK INDICATION FROM SCREW HOLE TO FASTENER HOLE. INSTALLED REPAIR IAW SRM 51-40-3, 51-30-2, AND 51-10-2.

Part: WEB — CRACK (BS 1226)

WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 RBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND 51-20-151.

Part: WEB — CRACK (BS 1226)

WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 53-10-2 AND MM 51-20-151.

Part: WEB — CRACK (BS 1290)

WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1290 WL 180 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151.