N286FE

Part: SLAT — FALSE INDICATION (N/A) · airframe 143 hrs · 69 cycles

ON FINAL APPROACH CONFIGURING TO FLAPS 25, RECEIVED A LE SLAT DISAGREE EICAS MESSAGE. ***EMERGENCY DECLARED*** AMM: 27-88-00-5 UPON ENTERING FLIGHT DECK FOUND FLAP HANDLE NOT IN 25 DEG DETENT, WHEN PLACED IN DETENT LE SLATS DISAGREE MESSAGE EXTINGUISHED. OPERATED FLAP LEVER FROM RETRACT TO 25 DEG AND ALL OPS AND INDICATIONS NORMAL M/M REF 27-51-00-5, SUBTASK 27-51-00-5-215-115. PERFORMED OP TEST OF LEADING EDGE SLAT POSITION SYSTEM M/M REF 27-88-00-5, INDICATIONS NORMAL. FSEU LEG 0 SHOWED LVR 1 NOT IN DETENT FIM REF 27-51-00 FT 809, WHICH AGREES TO WHAT WAS NOTICED UPON ENTERING FLIGHT DECK. A/C OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,719 hrs · 26,716 cycles

FUSELAGE SKIN DAMAGED, INSTALLED REPAIR IAW EA 7-5330-153076 PART 1 AND ATTACHED REPAIR SKETCH.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 41,638 hrs · 26,638 cycles

SETTING T/O POWER HAD LOUD BANG AND ALL ENG NR 1 INSTRUMENTS DROPPED. REPEATED T/O PRIOR TO T/O. REJECTED T/O PRIOR TO T/O POWER BEING SET. ENG NR1 WAS RUNNING ROUGH AND SMOOTHED OUT AS ENG WOUND DOWN. OPEN COWLING FOUND MASSIVE AMOUNT OF OIL IN COWL. INSPECTED INTAKE, NO DAMAGE, INSPECTED EXHAUST SECTION FOUND ALL THE BLADES WITH SEVERE DAMAGE AND EXHAUST WITH SEVERAL HOLES. NOTIFIED MOCC ENGINE CHANGE REQUIRED. THE ENGINE IS APPROVED FOR REMOVAL. ENGINE IS APPROVED FOR R & R DUE TO TURBINE BLADES DAMAGED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,125 hrs · 26,249 cycles

DURING PRE-DISPATCH CHECKS FOUND FWD ENTRY DOOR ESCAPE LIGHT INOP. DEN R RELEASED FOR SERVICE IAW MEL: 33-16-02-A CATEGORY: B EXPIRATION: 24SEP10 "MEL 33-16-02-A: FWD ESCAPE SLIDE LIGHT - INOP." L/E-LAMPED IAW SMP NO HELP.ITEM IS DEFFERED. R & R EMERGENCY SLIDE LIGHT BATTERY PACK IAW MM 33-50-051-2, OPS CKS NORMAL AT THIS TIME. NO TRACKING LEVEL ASSIGNED.

Part: VALVE — UNKNOWN (PRBC VALVE) · airframe 40,847 hrs · 26,017 cycles

SHORTLY AFTER T/O HEARD LOUD POP. OBSERVED FLUCTUATING EPR ON ENG NR 2 WITH OIL TEMP APPROX 115 DEGREES C. RESTARTED NR 2 ENG AT REDUCED POWER SETTING REMAINDER OF FLIGHT WITH NORMAL INDICATIONS INCLUDING NORMAL OIL TEMP. INSPECTED INLET AND EXHAUST OF NR 2 ENG FOR ANY EVIDENCE OF DAMAGE. NONE FOUND. PERFORMED COMPRESSOR BLEED VALVE OPS TEST IN REF TO CHP 7-5 OF 727 JRH. OPS CK GOOD. PERFORMED TAKEOFF EPR TEST IN REF TO JRH CHP 7-15. TEST GOOD. NO FLUCTUATIONS IN EPR AND NO COMPRESSOR STALLS. ALL ENG PARAMETERS WERE WELL WITHIN LIMITS. GOOD, STRONG, STABLE ENG R & R THE NR 2 ENG PRESSURE RATIO BLEED CONTROL IN REF TO AMM 75-31-011-4 AS PRECAUTIONARY IAW MOCC. RAN ENG AND PERFORMED THE COMPRESSOR BLEED VALVE TEST IN REF TO JRH. NO PROBLEMS NOTED. AWAITING TDR RESULTS.

Part: ENGINE — POWER LOSS (NR 2) · airframe 40,821 hrs · 25,989 cycles

DURING STANDARD PWR TAKEOFF AT 2000 FT, EXPERIENCED SUDDEN VIBRATION IN CTR PEDESTAL ACCOMPANIED BY ABNORMAL NOISE. DISCOVERED RETARDING NR 2 THROTTLE RESOLVED VIBRATION. ALL ENGINE INDICATIONS NORMAL. ENG HAS BEEN APPROVED FOR REMOVAL BY POWERPLANT ENGINEER. REMOVED AND REPLACED NR 2 ENGINE

Part: STRINGER — CORRODED (BS 490-500) · airframe 40,584 hrs · 25,788 cycles

CORROSION ON OTBD SIDE OF STR 28L BETWEEN STA 490 AND 500. CUT OUT DAMAGED AREA, FABRICATED 2 REPAIR SPLICES, FABRICATED STRINGER FILLERS AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.

Part: SKIN — CORRODED (BS 496 S28L) · airframe 40,584 hrs · 25,788 cycles

CORROSION ON SKIN AT STA 496 OTBD OF STR 28L. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3, 53-30-2 AND 51-30-2.

Part: STIFFENER — CRACKED (BS 301) · airframe 40,584 hrs · 25,788 cycles

NLG LT TRUNNION FITTING AFT VERTICAL STIFFNER CRACKED. REMOVED VERTICAL STIFFNER IAW SRM 51-30-2. LOCATED AND DRILLED NEW VERTICAL STIFFNER PN 65-19863-5 PO NR 29105141 IAW SRM 51-30-5. INSTALLED NEW VERTICAL STIFFNER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 40,584 hrs · 25,788 cycles

MAIN CABIN SEAT TRACK BS 480 - 380 BL0 IS CORRODED AT I/B FLANGE. FABRICATED NEW SEAT TRACK SECTION FROM BS 380 TO BS 480 BL 0 USING PN BAC 1520-792 PO NR 9006020 APPROX 109.6250 INCH FABRICATED REPAIR SPLICE ANGLES AND REPAIR STRAP IAW SRM 53-10-5 FIG 1, TREATED AND PRIMED PARTS IAW SRM 51-10-2, REMOVED AND REPLACED MAIN CABIN SEAT TRACK BS 380-480 BL 0, IAW SRM 51-30-2.

Part: SUPPORT FITTING — MISSING (SEAT TRACK) · airframe 40,584 hrs · 25,788 cycles

MAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, LBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.

Part: SKIN — DAMAGED (BS 1101) · airframe 40,584 hrs · 25,788 cycles

NR 2 ENGINE "S" DUCT INLET NOSE COWL CAP HAS DENT AT 8 O'CLOCK POSITION, BS 1101. EVALUATED DENT AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA , FABRICATED 2 DOUBLERS AND LIP SKIN FILLER, HEAT TREATED PARTS TO T4 CONDITION AND INSTALLED IAW SRM 54-30-1, 54-30-3 AND 51-30-2.

Part: STRUCTURE — CORRODED (BS 350) · airframe 40,584 hrs · 25,788 cycles

NLG WHEEL WELL UPPER STRUCTURE - CORROSION ON MID CHORD UPPER SURFACE AT APPROX STA 350, LT SIDE, ( INSIDE FWD WALKWAY ACCESS). REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 5312412 PO NR 29105100 AND INSTALLED IAW SRM 51-30-5 AND 51-30-2.

Part: SKIN — GOUGED (BS 480) · airframe 40,584 hrs · 25,788 cycles

FWD PIT - SKIN GOUGED AT BS 480, AFT SIDE, BETWEEN STRINGERS 27L AND 26L. CUT OUT DAMAGED TEAR STRAP, CUT OUT SKIN, FABRICATED SKIN DOUBLER, TRIPLER, STRUCTURAL FILLER, FILLER, TEAR STRAP REPAIRS AND SHEAR TIE REPAIR, HEAT TREATED PART TO T6 CONDITION IAW ER 2-37153-801 REV A, AND INSTALLED REPAIR PARTS IAW SRM 53-30-4, 53-10-4, 53-30-3 AND 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,584 hrs · 25,788 cycles

CORR AT SEAT TRACK LBL 45, STA 852-STA 870 REMOVED OLD SEAT TRACK ON LBL 45 STA 852 TO STA 870 IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-1466 PO 8205123 DIM: 16 INCHES X 4 INCHES IAW SRM 53-10-2 TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — GOUGED (ZONE 800) · airframe 40,584 hrs · 25,788 cycles

MCD DOOR AFT LWR SIDE GOUGED AT OLD REPAIR REMOVED OLD DOUBLER OUT OF LIMITS IAW SRM 51-30-2, FAB NEW DOUBLER USING MAT 301.1/2HD .063 PO NR 29067392, DIM: "8.5 X 4.8750" IAW PF SDMCER 01-049 REV H AND 52-30-2 FIG 2A. PAINTED IAW SRM 51-10-2, INSTALLED NEW DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 440-460) · corrosion level 2 · airframe 40,584 hrs · 25,788 cycles

MAIN CABIN SEAT TRACK BS 440-460, LBL 24 IS CORRODED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED ANGLES, ONE STRAP, AND NEW SEAT TRACK SECTION AND INSTALLED PARTS IAW SRM 53-10-5 AND 51-30-2.

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 40,584 hrs · 25,788 cycles

LT INBD MID FLAP LWR T/E ON ACT ROD CUTOUT WBL 106 ANGLE IS CRACKED. REMOVED ANGLE CRACKED FROM LT I/B MID FLAP IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 51-40-4 FIG 1 SRM 57-50-2 FIG 5. INSTALLED NEW ANGLE IAW SRM 51-30-2 SRM 57-20-2 INSTALLED LOWER SKIN PANEL IAW IAW SRM 51-30-2.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 40,584 hrs · 25,788 cycles

RT WING INBD MID-FLAP, AFT LWR CHORD ANGLE IS CRACKED IN 2 PLACES AT WBL 100. REMOVED LWR SKIN PANEL IAW SRM 51-30-2. REMOVED LWR CHORD ANGLE ON IB MID FLAP IAW SRM 51-30-2 REV 101. FABRICATED NEW CHORD ANGLE 5 FT X 1.5 INCHES FROM BAC1503-100046 7075 T6, PO NR 9008875 IAW SRM 51-40-3 FIG 1, REV 101. LOCATED AND DRILLED IAW SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED LOWER CHORD IAW SRM 51-30-2. INSTALLED LWR SKIN PANEL IAW SRM 51-30-2, REV 101.

Part: SKIN — MISINSTALLED (ZONE 200) · airframe 40,584 hrs · 25,788 cycles

MAIN CARGO AREA, STA 660, STR 4L, ABOVE STRINGER, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PARTS IAW SRM 51-30-2, 53-30-3, 51-30-5 AND 53-30-4.

Part: DOUBLER — GOUGED (LT WING TE FLAP) · airframe 40,584 hrs · 25,788 cycles

RT WING INBD FORE FLAP OTBD L/E HAS DEEP GOUGE FROM LONG SCREW IN WING LWR T/E. STOP DRILLED DEEP GOUGE AT RT WING INBD FORE FLAP OTBD L/E IAW SRM 51-10-1 REV 101. HFEC INSPECTED AREA IAW NDTM 51-00-00, FIG 23 PART 6, NO DEFECTS NOTED. FABRICATED REPAIR PLATE FROM 2024 T3 .050 INCH PO NR 9008655 DIM 3.7500 INCH X 4.5 INCH IAW SRM 57-50-4 FIG 1, REV 101 TREATED AND PRIMED. REPAIR PLATE IAW SRM 51-10-2, REV 101 INSTALLED REPAIR PLATE IAW SRM 51-30-2 REV 101.

Part: SKIN — CRACKED (MLG DOOR) · airframe 40,584 hrs · 25,788 cycles

RT MLG WING DOOR SKIN CRACKED UNDER UPPER SEAL RETAINER AFT HINGE AREA. REPAIRED MLG WING DOOR IAW EO 7-5280-7-4301 PART 4.

Part: SKIN — CHAFED (BS 303 S15-16L) · airframe 40,584 hrs · 25,788 cycles

FWD ENTRY DOOR FRAME AT BS 303.9, STR 15 AND16 WEB CUT OUTS HAS JAGGED EDGES AND RUBBING AGAINST DOOR STRAP. TRIMMED OUT EDGE UPPER SECTION ON FRAME STR 15L DIM: .063 AND STR 16L DIM: .090 IAW SRM 51-10-1 AND EA 7-5310-126849. HFEC AREA IAW NDTM 51-00-00, FIG 23, PART 6. NO DEFECTS NOTED. ACCOMPLISHED .040 INSURANCE CUT TRIM IAW EA 7-5310-126849. TREATED AND PRIMIED IAW SRM 51-10-2.

Part: SKIN — MISINSTALLED (BS 660 S4L) · airframe 40,584 hrs · 25,788 cycles

MAIN CARGO AREA, STA 660, STR 4L, BELOW STR, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP DIMS 3 INCHES X 5.5 INCHES, CUT OUT DAMAGED AREA OF SKIN, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PARTS IAW SRM 51-30-2, 53-30-3, 51-30-5 AND 53-30-4.

Part: FRAME — DAMAGED (BS 1090) · airframe 40,584 hrs · 25,788 cycles

AFT PIT BS 1090 FRAME IS PUNCTURED IN THE UPPER FLANGE ABOVE STR 27L. CUT-OUT DAMAGED AREA IAW SRM 51-10-1 REV 101. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. HEAT TREATED 7075-0 TO T6 CONDITION IAW ER 2-37153-801 REV A. CW CONDUCTIVITY TEST IAW NDTM PT 6, 51-00-00, FIG 20, CONDUCTIVITY TEST EQUAL TO 7075T6. LOCATED AND DOUBLER IAW SRM REV 101, 51-30-5. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM REV 101 51-30-2.

Part: SUPPORT FITTING — MISSING (SEAT TRACK) · airframe 40,584 hrs · 25,788 cycles

MAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, RBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING PART IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.

Part: FRAME — PUNCTURED (BS 1050 S27R) · airframe 40,584 hrs · 25,788 cycles

AFT PIT BS 1050 FRAME PREVIOUS REPAIR DOUBLER IS PUNCTURED ABOVE STR 27R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW DOUBLER, HEAT TREATED DOUBLER TO T-6 CONDITION IAW FASI FORM 2-37153- 801 REV A, AND INSTALLED IAW SRM 51-40-3, 53-10-2 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 740-870) · airframe 40,584 hrs · 25,788 cycles

CORROSION AT SEAT TRACK STA 740 TO STA 870, LBL 24. REMOVED OLD SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 620-640 S4L) · airframe 40,584 hrs · 25,788 cycles

MAIN CARGO AREA, STA 620-640, STR 4L, INNER SKIN HAS DEEP GOUGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED PARTS IAW SRM 51-10-1 AND EA 7-5310-126850.

Part: SKIN — DAMAGED (BS 1086-1097) · airframe 40,584 hrs · 25,788 cycles

LT SIDE OF FUSELAGE, OUTER SKIN, SCRATCHES BETWEEN STA 1070 TO STA 1130, AND STR 23L TO STR 27L. REPAIRED LT SIDE OF FUSELAGE OUTER SKIN STA. 1086 TO 1097 BETWEEN STR 24L TO 25L IAW SRM 53-30-3 FIG 1 REV 101, 53-30-3, FIG 1, AND 51-30-2..

Part: SPAR — CRACKED (LT WING TE FLAP) · airframe 40,584 hrs · 25,788 cycles

LT WING LOWER T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED DOUBLER, CUT-OUT LOWER CHORD, FABRICATED NEW WEB, 2 EACH ANGLES, NEW LWR CHORD, NEW DOUBLER, STRAPS, 2 FILLERS AND INSTALLED PARTS IAW DWG SR27-57-038 REV C.

Part: WEB — CRACKED (BS 1275) · airframe 40,584 hrs · 25,788 cycles

AFT AIRSTAIR STA 1275 LIGHTNING HOLE LT SIDE OF AIRSTAIR CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER FROM 7075-T6 .032 PO NR 9008186 APPROX DIM: 4 INCHES X 2.3750 INCHES AND INSTALLED NEW REPAIR DOUBLER AT BS 1275 LH AFT AIRSTAIR WEB IAW SRM 51-40-2, FIG 1 ALL IAW SRM 53-10-2 FIG 6 AND SRM 51-10-2.

Part: SPAR — CRACKED (RT WING TE FLAP) · airframe 40,584 hrs · 25,788 cycles

RT WING LWR T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED LWR CHORD SECTION IAW DWG 27-57-038 REV C & DOUBLER IAW DWG SR27-57-038 REV C. TRIMMED OUT INBD AREA IAW DWG SR27-57-038, REV C & FABRICATED 2 ANGLES & HEAT TREATED ANGLES TO T6 IAW ER NR 2-37153-801 REV A. FABRICATED NEW WEB SECTION IAW DWG NR SR27-57-038 REV C & FABRICATED NEW CHORD IAW DWG NR SR727-52-038 REV C. FABRICATED STRAP IAW DWG NR SR27-57-038 REV C & FABRICATED 2 RADIUS FILLER IAW DWG NR SR27-57-038 REV C. FABRICATED NEW DOUBLER IAW DWG SR27-57-038 REV C. TREATED & PRIMED REPAIR PARTS & INSTALLED ALL IAW SRM 51-30-2, SRM 51-30-2, AND DWG NR SR27-57-038, REV C.

Part: VALVE — FAILED (HYD SYSTEM) · airframe 40,192 hrs · 25,469 cycles

TOTAL LOSS OF A HYDRAULICS UPON GEAR RETRACTION, (LEVEL AND PRESSURE 0). A PUMPS RAN AMAX OP 3 MINS BEFORE SHUTOFF. REMOVED AND REPLACED LT GEAR LOCK SEQUENCE VALVE IAW MM 32-32-031-4. PERFORMED GEAR SWING IAW AMM 32-32-00-005. REMOVED BOTH NR1 AND NR 2 HYD PUMPS DUE TO HYD FLUID LOSS IAW AMM 29-11-033-4 AND INSTALLED BOTH PUMPS. REMOVED AND REPLACED BOTH A SYS PRESSURE FILTERS IAW MM 29-11-041. REMOVED AND REPLACED BOTH NR 1 AND NR 2 ENG CASE DRAIN FILTERS IAW AMM 29-11-041. PERFORMED LEAK CKS, NO LEAK NOTED AT THIS TIME.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 39,187 hrs · 24,651 cycles

RT HORIZONTAL STAB ELEVATOR, OB MOST UPPER SURFACE STATIC WICK. CORROSION ON SKIN SURFACE, AROUND AND UNDER STATIC WICK BASE, AND ON WICK BASE ALSO REMOVED CORROSION ON UPPER RT OUTBOARD ELEVATOR STATIC WICK, FOUND TO BE OUT OF LIMITS BY NDT. MATERIAL LOSS OF .008". REPAIRED AREA IN REF TO SRM 55-20-3 PG 2-3, SRM 55-20-1 DETAIL 1, MM 23-61-00-6 PG 1, MM 51-20-151-7 PG 1-3. THIS IS CLASSIFIED MINOR REPAIR, LEVEL 1 CORROSION.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN DECK FLOOR STRUCTURE, UPPER BEAM CAP HAS MULTIPLE DRILL HOLES UNDER REMOVED SEAT TRACK STA 1166, RBL 25. INSTALLED TWO FREEZE PLUGS IN 1166 FLOORBEAM. PLUG TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO TO BLUE PRINT SIZE IN FREEZE PLUG. IN REF TO EA 7-5310-113070. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION ON UPPER SURFACE OF UPPER T- CAP ON FLOOR BEAM, STA 950, LBL 10.5 AND LBL 21". REMOVED CORROSION FROM SURFACE ON UPPER T-CAP REF SRM 51-10-01. REMOVED SEAT TRACK SRM 51-30-2. REMOVED WEB SUPPORT AND BRACKET AT 950. REMOVED TWO STRAPS BS 950 UNDER T- CAP, LBL 22-63. FAB REPAIR ANGLE, FAB UPPER T-CHORD, HEAT TREATED AND PRIMED, INSTALLED UPPER T-CHORD, BS 950, RBL 13 TO LBL 62. WORK ACCOMPLISHED ON EA NR 7-5310-113054. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

BS 740, VERTICAL ANGLE AND BULKHEAD SKIN, ABOVE STR S-28 HAS 2 EA PLUG RIVETS THROUGH ALL PARTS (PREVIOUS DAMAGE) ACCOMPLISHED WORK INSTRUCTION ON EA NR 7-5310-11068 FOR REPAIR OF 2 (EA) PLUG RIVETS THROUGH VERTICAL ANGLE, AND BULKHEAD.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LWR FUSELAGE RT SIDE STA 743, RBL 7", SUPPORT FRAME AT IB SIDE OF ACCESS DOOR 3449R IS CORRODED OB SIDE REMOVED BEACON, REMOVED PANELS 3449R AND 3346. CORROSION THROUGH SUPPORT FRAME. REMOVED SUPPORT FRAME. FABRICATED NEW PARTS, ASSEMBLED NEW FRAME. INSTALLED NEW PARTS, REF SRM 51-40-02. TREATED AND PRIMED PARTS REF SRM 51-10-2. REINSTALLED PANELS 3449R AND 3346 REF SRM 51-30-2. INSTALLED BEACON AND OPS CHECKED (GOOD) REF SWPM 20-30-12 PG 88-89. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE, BODY FRAME CHORD IS CORRODED, BS 740, STR 27L- 28L, WL149 REMOVED AND REPLACED CHORD ANGLE REF B727 SRM 51-30-02 PG 2 DUE TO CORROSION BEING OUT OF LIMITS REF SRM 727 SRM 51-10-1, CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

FWD ENTRY DOOR CUTOUT, LOWER HINGE REPAIR, 3 HOLES ARE CRACKED. NEED ENGINEERING EVALUATION PER WIC 53308429 ITEM 5. HOLES CIRCLE IN BLACK, ALSO ON NR00077 LT FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT LWR HINGE CUTOUT. REPAIR OF LOWER HINGE CUTOUT ACCOMPLISHED ON EO NR 7-5330-7-2345 P2. BOTH DISCREPANCIES NR00077 AND NN00500 ARE REPAIRED ON THIS EO.

Part: STRINGER — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LWR FWD CARGO PIT FUSELAGE STRINGER UPPER O/B FLANGE HAS CRACK, STA 720 PLUS 14.5" STR 25R. REMOVED DAMAGE REF SRM 53-10-3. FABRICATED REPAIR REF SRM 53-10-3 FIG 2, SHEET 2. INSTALLED REPAIR REF 51-30-2 PG 1, PG 1-3, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT REPAIR, 5 HOLES ARE CRACKED NEED EVALUATION PER WIC 53308429 ITEM 5, HOLES ARE CIRCLED IN BLACK. ALSO FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT UPPER HINGE ON WO NR 36352/N00076 COMPLIED WITH EA NR 7-5330-113939. WORKED IN CONJUCTION WITH WO NR 36352/ N00076 AND N00499. UPPER HINGE CUTOUT DOUBLER AND TRIPLER.

Part: SKIN — DAMAGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FOUND DOUBLE DRILLED HOLE AT STA 720F PLUS 5", STR 27R IN NEW SKIN. REMOVED DAMAGE, FABRICATED REPAIR FILLER, STRUCTURAL FILLER AND REPAIR DOUBLER. TREATED AND PRIMED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS. REF SRM 53-30-3/FIG NR 3/PAGES 12-14, CLASSIFIED AS A MAJOR REPAIR.

Part: SKATE ANGLE — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

LT WING IB TE NR 3 FLAP TRACK FWD FRG IB SKATE ANGLE IS CRACKED AT 2 WING SKIN FASTENERS WBL 199, 3" FWD AND AFT OF SPAR. REPAIRED NR 3 FLAP TRACK SKATE ANGLE IAW B 272-200 SRM 51-40-3 AND 51-30-2. ALL LEAK CK'S GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY SKIN STIFFENER IS BUCKLED/CRACKED, BS 720B PLUS 13" 5", IB OF STR 28R, WL 148. REMOVED DAMAGE SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE, REF BOEING DWG NR 65-54577 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 718, STR 29L, ABOUT LBL 2, FLOOR SUPPORT IS CORRODED ON REPAIR ANGLE REMOVED DAMAGE. FABRICATION REPAIR PART, TREATED AND PRIMED REPAIR PARTS AND INSTALLED. THIS REPAIR IS CLASSIFIED AS MINOR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 700 TO 705, STR 28R, AT RBL 4 TO RBL 7, STRINGER IS CORRODED REMOVED CORRODED SECTION OF STRINGER FROM STA 680 TO STA 720 AND INSTALLED NEW SECTION REF SRM 51-30-2, AND BOEING DOCUMENT NUMBER 65-54577, ID NR 0004/FRAME NR 1.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION ON UPPER SHEAR DECK, UNDER FLOORBOARDS, STA 1166 PLUS 8", RBL 17" TO RBL 36" (BETTER VIEW FROM LWR AFT PIT) REMOVED SEAT TRACK AT STA 1128 - 1178, RBL 25 AND 45. REMOVED ATTACHING STRUCTURE FOR SHEAR WEB REMOVAL. REMOVED SHEAR WEB. DRILLED UP SHEAR WEB. INSTALLED REMOVED STRUCTURE, SEAT TRACK, RBL 25-45 AND SHEAR WEB REF. 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

MAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090, RBL 24 BLENDED CORROSION. ORIGINAL "T" .090", REMOVED .025" OUT OF LIMITS REF SRM 51-10-1 PG 15. FABRICATED REPLACEMENT SEAT TRACK, FABRICATED SPLICE REPAIR PARTS, TREATED AND PRIMED SEAT TRACK AND REPAIR PARTS. INSTALLED SEAT TRACK AND REPAIR PARTS REF SRM 53-10-5 FIG 1. INSTALLED 3 U- CHANNELS REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LOWER FUSELAGE SKIN ATTACH ANGLE TO FAIRING WEB SUPPORT HAS CORROSION AT BS 720F AND RBL 11-22. REMOVED CORRODED ANGLE AND 65-25577-14 REPLACED. REFERENCE SRM 51-30-02 AND BOEING DOCUMENT NR 65-25577/ID NR 0003/FRAME NR 1, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LOWER CARGO BAY REINFORCING ANGLE DOUBLER AT AT BS 740 BULKHEAD STR S-27R IS CORRODED REMOVED CORRODED REINFORCING ANGLE. REMOVED CORROSION AND ANGLE WAS OUT OF LIMITS. FABRICATED NEW REINFORCING ANGLE ON SNRM NR N01045, 8130 FORM TRACKING 2007-06-143. INSTALLED REINFORCING ANGLE REF BOEING DOCUMENT NR 69-64841, ID NR 0001/FRAME NR 1, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN CARGO DECK FLOOR STRUCTURE, SEAT TRACK BETWEEN STA 1130 TO 1166 PLUS 8", RBL 25", HAS CORROSION ON LOWER FAYING SURFACE AT AFT END. FABRICATED NEW SEAT TRACK, REF DWG 53FX 976, SEAT TRACK INSTALLED ON N/R N00816. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FUSELAGE, BS 740, S-27L, 2 STR CLIPS CORRODED REMOVED CLIPS, REMOVED CORROSION AND CLIPS ARE OUT OF LIMITS. FABRICATED NEW CLIPS, TREATED AND PRIMED AND INSTALLED. REF BOEING DOCUMENT DRAWING NR 69-45628/ID NR 0001/FRAME NR 1 CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT BILGE BODY FRAME STR SPLICE IS CORRODED, BS 1008-1012, STR 29L, WL 140. REMOVED STRINGER SPLICE, CLEANED DAMAGE HOLE, HFEC STRINGER, FABRICATED STRINGER SPLICE. FABRICATED STRINGER CLIPS, TREATED AND PRIMED PARTS, PERFORMED HIDDEN DAMAGE INSPECTION. INSTALLED STRINGER SPLICE AND STRINGER CLIP REF EA NR 7-5310-113077. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LWR CARGO PIT BILGE STRINGER TIE, ON PRESSURE BULKHEAD HAS CORROSION, STA 740, STR 27R. REMOVED CORRODED STRINGER TIES, FABRICATED NEW STRINGER TIES, AND INSTALLED. REF BOEING DRAWING NR 69-45628 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — FAILED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING, A/C INSP FOUND EXISTING REPAIR ON FRAME AT BS 700 BETWEEN STR 24L AND 26L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, FABRICATED REPAIR, HFEC FRAME TRIM OUT, NO CRACKS EXIST. INSTALLED FORMED REPAIR. REF FED EX EA 7-53-113940. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP FOUND EXISTING REPAIR ON FRAME 720A BETWEEN STR 24L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, FABRICATED FORMED SECTION REPAIR REF SRM 51-40-3 AND INSTALLED REF FED EX EA NR 7-5310-113941 THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXISTING REPAIR ON FRAME 680 BETWEEN STR 22L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTNG REPAIR, REMOVED EXISTING SLICE PLATE AT STR 25L. FABICATED REPAIR AND INSTALLED REF SRM 51-40-3 AND FED EX EO NR 7-5310-113081 THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LWR CARGO PIT, VERTICAL WEB HAS CORROSION AT LWR, BETWEEN STA 700 AND 720 STR 28L. REMOVED AND REPLACED VERTICAL WEB P/N 69-46346-1 REF SRM 51-30-2 DUE TO CORROSION. FASTENER COMMON TO SKIN WILL BE INSTALLED ON N/R N01157. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LWR FWD CARGO PIT U-CHANNEL HAS 3 EXTRA HOLES ON UPPER LEG INBD END AT FWD SIDE OF STA 640 BELOW FRAME SPLICE AGAINST SKIN SHEAR TIE, BETWEEN STR 22L AND 23L. REMOVED U CHANNEL, REF SRM 51-30-2. FABRICATED NEW CHANNEL REF DWG 53FX1465 AND SENT FOR HEAT TREAT. LOCATED FASTENER HOLES ON U-CHANNEL REF SRM 51-30-5. ALODINE NAD PRIMED U-CHANNEL REF MM 51-20-21 AND 51-30-2. INSTALLED U-CHANNEL REF 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK SURFACE OF FLOORBEAM HAS CORROSION AT NUT PLATE HOLE STA 1030, LBL 9". REMOVED CORROSION FROM AFT UPPER MAIN DECK UPPER SURFACE FLOORBEAM STA 1030, LBL 9". FOUND AREAS OF CORROSION REMOVAL TO BE OUT OF LIMITS. REMOVED DAMAGE SECTION OF FLOORBEAM AND INSTALLED REPAIR REF SRM 53-10-8 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP FOUND, EXISTING INTERNAL SKIN REPAIR. REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 1. [08-28-07] REMOVED AND REPLACED PREVIOUS REPAIR REF. FED EX EA 7-5330-113262, REPLACED CORRODED STRINGER SECTION REF SRM 53-10-3, 51-30-2 TREATED AND PRIMED REF SRM 51-10-2.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

CUSTOMER REQUEST FOR PREVIOUS WORKMANSHIP, BS 680, STR S-23L STRINGER UPPER FLANGE WAS BLENDED, ON AND HAS TOOLING MARK IN AREA UNDER PREVIOUS REPAIR. BLEND OUT TOOLING MARK IAW B727 SRM 51-10-1 FIG 2. INSTALLED STRINGER TYPICAL REPAIR IAW B727 51-10-3-FIG 2, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — FAILED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSPECTION, FOUND EXISTING REPAIR AT STA 1070-1090, STR 25R-27R, DID NOT CONFORM TO SRM 53-30-03. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW SKIN REPAIR FROM 2024-T3, .063 FILLER 2024-T3 .071" DOUBLER PER EA NR I070489 IR,THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 702 TO 705 AT STR 28R ABOUT RBL 8 INTERCOSTAL IS CORRODED IN LOWER FWD CORNER. REMOVED STIFFENER AT STA 700 RBL 8, AND STA 720 RBL 8. REMOVED INTERCOSTAL AT RBL 8 BTW STA 700-720. FABRICATED NEW INTERCOSTAL AND INSTALLED. INSTALLED STIFFENER AT RBL 8 STA 720. INSTALLED STIFFENER AT STA 700, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

MAIN CABIN TRACK HAS CORROSION AROUND NUTPLATE HOLES AND OTBD SIDE OF SEAT TRACK FROM BS 774 - 848, LBL 45. REMOVED CORROSION REF SRM 51-10-1, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1, ORIGINAL THICKNESS .090", REMOVED .020", REMAINING .070", REPLACED SEAT TRACK T-CAP SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LWR AFT CARGO PIT, STA 1166 BULKHEAD WALL STRUCTURE. VERTICAL Z-ANGLE IN CENTERLINE, BL 0" ABOVE DIFFERENTIAL PRESSURE VALVE HAS CORROSION AT LWR AND UPPER LT SIDE. REMOVED DAMAGE AREA, DRILLED NEW PART, Z-ANGLE PN NR 65-67250-34, IAW B727 SRM 51-30- 2 PG 1. INSTALLED NEW Z-ANGLE, IAW B727 SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN DECK FLOOR STRUCTURE, ARCHED CLOUSER WEB COVER FWD ATTACH ANGLE IS CRACKED OUT OF NUTPLATE HOLE STA 1178, RBL 50" (VIEW FROM LWR PIT) REMOVED ARCHED CLOSER WEB ASSY. FABRICATED NEW WEB, STIFFENER, AND ANGLE REF DWG 65-29548. TREATED AND PRIMED REF SRM 51-10-2, INSTALLED ARCHED WEB ASSY REF DWG 65-29548 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION ON SEAT TRACK STA 1166 IN CENTERLINE BL 0" AND LBL 2" ON FLANGE REMOVED, FABRICATED NEW TRACK, INSTALLED SEAT TRACK AT BS 1166 BL 0" PER SRM 51-30-2, 51-30-5, 51-30-08, 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLAP TRACK — CORRODED (ZONE 600) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

ON NON-ROUTINE, RIGHT OUTBD FLAP INBD FLAP TRACK HAS CORROSION AT THE OUTBD AND CENTER MOUNT HOLES AT MOUNT PAD. ON NON- ROUTINE, OUTBD FLAP INBD FLAP TRACK MOUNT BOLTS ARE WORN AND GOUGED. ON NON-ROUTINE, FLAP TRACK HAS WEAR ON TOP OF FLAP TRACK ON OUTBD SIDE 13" FROM AFT END. ON NON-ROUTINE, FLAP HAS RUST IN HORIZONTAL HOLES AT THE TRACK MOUNT PAD. REPLACED NR 7 FLAP TRACK, NEW FLAP TRACK IS INSTALLED ON W/C 27X5709-03. REPLACING WITH NEW FLAP TRACK ADDRESSES NON-ROUTINE N00430, N00432, N00433, N00434, THIS IS CLASSIFIED AS A MINOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT CARGO DOOR THRESHHOLD STANCHION FITTINGS STA 950E-990 RBL 22-27 4 EA. FITTINGS CORRODED UPON FURTHER REVIEW 2 FITTINGS WITHIN LIMITS AFTER BLEND OUT PER DWG 69-45577-2 AND 69-45576-3. 2 OUT OF LIMITS. REPLACED AT STA 950F AND 950G, ALL FITTINGS REPLACED, INSTALLED REF SRM 51-30-2.

Part: CREASE BEAM — CRACKED (ZONE 300) · airframe 39,187 hrs · 24,651 cycles

LT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, CREASE ANGLE IS CRACKED UNDER TRIANGULAR RIB, UPPER IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360 THE CREASE CHORD WAS REPAIRED REF EO NR 7-5530-7-2303 PRT 5, REV Q. JPF STEPS 20-30 AND SRM 51-40-03 FIG, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN STA 950 FLOORBEAM BET RBL 45 AND 62 HAS CORROSION ON UPPER AND LWR, AND AROUND FASTENER HOLES REMOVED CORROSION. HFEC NO DEFECT NOTED, ROTO PEENED REF SOPM 20-10-3. TREATED AND PRIMED REF SRM 51-10-2, LEVEL 1 CORROSION.

Part: SKIN — CHAFED (BS 720D S19R) · airframe 39,187 hrs · 24,651 cycles

RT LWR FUSELAGE SKIN CHAFED STA 720D 14" STR 19R FABRICATED AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG 5, PAGE 20-22. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT CARGO DOOR THRESHOLD AREA BEAM WEB CORRODED, STA 950E - 990 RBL 21"-22", WL 145 - 148 REMOVED CORROSION FROM AFT PIT CARGO DOOR THRESHOLD WEB BEAM AREA, FOUND TO BE OUT OF LIMITS. REMOVED Z- ANGLE FWD/AFT FOR ACCESS UPPER CHORD BEAM. FABRICATED AND INSTALLED WEB/CHORD, Z-ANGLES FWD/AFT REF SRM 51-30-2 PG 2GMM7-0-1001 PG 2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT FRAME CORRODED AT STA 1010 BETWEEN STR 29-30R. REMOVED FASTENERS REF SRM 51-30-2. REMOVED CORROSION REF SRM 51-10-1. INSTALLED FASTENERS REF SRM 51-30-2. TREATED AND PRIMED REF MM 51-20-013 AND PAINTED REF MM 51-20-013. CORROSION LEVEL 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

STA 848 FLOORBOARD SUPPORT BET BL 0 AND LBL 24, HAS LIGHT CORROSION AT NUTPLATE HOLES, UPPER AND LOWER FLANGES SURFACES REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOORBOARD SUPPORT BL 0 TO LBL 24 NAD INSTALLED INBD AND OTBD SEAT TRACK FLANGE, STA 780 - 850 FER SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

MAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090 RBL 45 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, .090" REMOVED. VERIFIED MATERIAL BAC1520-792 7178T6511, FABRICATED NEW SEAT TRACK, TREATED AND PRIMED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK REF 27 SRM 51-30-2 PG 4.

Part: FLOORBEAM — MISREPAIRED (BS 620) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 620 FLOORBEAM UPPER CHORD FROM LBL 3" TO 19". EVALUATED AND DETERMINED REPAIR NOT TO CONFORM TO FED EX DWG SR27-53-034. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR ANGLE FROM 17-7 PH .063", HEAT TREATED TO 180-200 KSI , TH 1050 CAD PLATED, PRIMED. [07-30-07] PRIMED AND INSTALLED REPAIR ANGEL AT BS 620 LBL 3" TO 9" . REF. FED EX DWG. SR27-53-034

Part: SKIN — GOUGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

AFT LWR EXTERNAL BELLY SKIN HAS NUMEROUS NICKS, FROM STA 950D BACK TO 1050, STR 26L TO 26R BLENDED BELLY SKINS FOR NICKS AND REMOVED CORROSION, SRM 51-10-1, ORIGINAL METAL .075", METAL REMOVED .010 AND METAL REMAINING .065" THIS IS CLASSIFIED AS A MINOR REPAIR. TREATED AREA, SRM 51-20-21-7.

Part: SPLICE — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

LEFT WING LEADING EDGE OVER WING PANEL 3342, FORWARD SPLICE ANGLE HAS LOOSE/WORKING RIVETS AND IS CRACKED IN HALF. REPLACED FASTENERS AND FAB SPLICE ANGLE REF 51-30-2, GMM 7-0-1001, DWG 65-22555.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN CARGO DOOR, AFT SIDE FRAME, HAS DEEP GOUGE IN PRIOR REPAIR DOUBLER, 19" UP FROME BOTTOM EDGE REMOVED OLD DOUBLER REF SRM 51-30-2, VERIFIED MATERIAL AS 7075-0-.090, FABRICATED REPAIR DOUBLER REF. PF SRM 52-30-2, HEAT TREATED TO 7075-T6, FIT AND DRILLED DOUBLER REF PFSRM52-30-2, TREATED AND PRIMED REF SRM51-10-2, INSTALLED REPAIR DOUBLER REF. PF SRM 52-30-2

Part: FLOORBEAM — CORRODED (BS 643) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 643 AT STR 28R ABOUT RBL 12, FLOOR SUPPORT CORRODED UNDER NUT PLATE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, SRM 51-40 -4 PG 1. FABRICATED REPAIR PARTS SRM 51-40-4 PG 1-5. DRILLED FASTENER HOLES SRM 51-40-4 AND 51-30-2 PG 1- 12. TREATED AND PRIMED REPAIR PARTS SRM 51-10-2 PG 1. INSTALLED REPAIR PARTS SRM 51-40-4, PG 1-5.

Part: SKIN — CHAFED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

RT LWR AFT FUSELAGE EXTERIOR SKIN CHAFED AT AFT CARGO PIT FWD DOOR CUTOUT FWD UPPER CORNER. REMOVED CHAFED DAMAGE IAW SRM 51-10-1, NDT FOR MATERIAL LOSS, IAW NDT MANUAL PART 4 51-00-00 FIG 2, OUT OF LIMITS PER SRM 53-30-1 PG 2C FIG 2, VERIFIED MATERIAL 2024- T3, .050 PER EA NR I070418 P1, STEP 4A. REMOVED FASTENERS FOR NDT INSPECTION OF HOLES, NO DEFECTS NOTED OF HOLES, FAB`D DOUBLER. INSTALLED IAW EA I070418 AT RT AFT FUSELAGE SKIN AT FWD UPPER CORNER OF AFT CARGO PIT DOOR. PRIMED AND TOP COATED AREA OF INSTALLATION IAW EA NR I070418.

Part: FAIRING — CRACKED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

RT WING OB TE NR 8 JACKSCREW FAIRING, CRACK COMING OUT OF FASTENER HOLE AT FWD END. REMOVED DAMAGE AREA REF SRM 57-20-4 FIG 1 PG 5. FAB`D REPAIR PARTS REF SRM 51-30- 05 AND 57-20-4 FIG, 1 PG 5. INSTALLED REPAIR PARTS REF SRM 51-30-02 PG 1 AND REF SRM 57-20-04 FIG 1 PG 5. VERIFIED METAL AS 6061-T4 .050"

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN FLOORBEAM AT STA 950 HAS CORROSION ON UPPER SURFACE BET RBL 24 RBL 45 REMOVED CORROSION FROM FLOORBEAM AT STA 950 RBL 24 TO RBL 45 IAW B727 SRM 51-10-1, ORIGINAL .125", REMAINING .120", HFEC. NO DEFECTS NOTED, ROTO PEENED, TREATED AND PRIMED IAW EA NR 7-5310-113055.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 39,187 hrs · 24,651 cycles

ON AGING AC INSP, FOUND EXISTING REPAIR LOCATED ON NR 3 LOWER CARGO DOOR SKIN 31" FROM BOTTOM EDGE FROM 1" TO 48" FROM FWD EDGE. DID NOT CONFORM TO SRM 52-00-3 FIG 3. REMOVED 2 EXISTING DOUBLER, INSTALLED 1 DOUBLER TO REPAIR AREA REF SRM 52-00-3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN DECK SEAT TRACK HAS CORROSION AT BL- 0, STA 930 LT SEAT TRACK FLANGE. REMOVED OLD SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AT BS 930 BL 0, REF SRM 51-30-02.

Part: BRACKET — CRACKED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

RT WING FWD NAV LIGHT BRACKET CRACKED. REPLACED RT WING FWD NAV LIGHT BRACKET, REF SRM 51-30-02 P.13.

Part: FRAME — CORRODED (BS 1090) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT FRAME STA 1090 CORRODED FWD FACE, OTBD RADIUS BETWEEN STR 19-20R. REMOVED CORROSION PER EA NRI070450 STEP 1, ROTO PEENED AREA PER EA I070450 STEP 3. ALODINED AND PRIMED PER EA NR I070450 STEP 4, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LOWER EDGE OF RIGHT WHEEL WELL AFT BULKHEAD HAS CORROSION BETWEEN FRAME AND FAIRING. CORROSION STARTS AT RBL 11 AND CONTINUES OUTBOARD. THIS AREA IS LOCATED AT THE FWD EDGE OF THE WING TO BODY FAIRING 3622. FABRICATED NEW FRAME ASSY IAW DWG 65-25550 ON LOWER EDGE OF RIGHT WHEEL WELL, AFT BULKHEAD, TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2, 51-30-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LWR. CARGO PIT BILGE, FRAME HAS CORROSION ON FWD SIDE ON SKIN ATTACH FLANGE AND UP VERTICAL SIDE 2", STA 720E BETWEEN STR 27R AND 28R. REMOVED DAMAGED SECTION BS 720E BETWEEN STR 27R - 28R. FABRICATED REPAIR PART, SHEAR TIE PER SRM 53-10-4 PG 43-45.

Part: RIB — CRACKED (ZONE 400) · airframe 39,187 hrs · 24,651 cycles

LT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, TRIANGULAR RIB WEB IS CRACKED AT UPP IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360. (MKD) REMOVED RIB ASSEMBLY, DISASSEMBLED, FABRICATED AND HEAT TREATED NEW WEB, DRILLED UP NEW WEB, ASSEMBLED RIB ASSEMBLY AND INSTALLED REF BAC DRAWING 65-17555 AND SRM 51-30-02.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN FLOOR WEB UPPER SURFACE HAS CORROSION AROUND FASTENERS BS 720 - 720A RBL 48. REMOVED CORROSION, FOUND WEB OUT OF LIMITS REF SRM 53-10-1, REMOVED WEB, VERIFIED MATERIAL 7075 T6-.063 A91989. FABRICATED NEW WEB REF SRM 53-10-2. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED NEW WEB REF SRM 53-10-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

RBL 24 SEAT TRACK BETWEEN STA 804 TO 848 HAS LIGHT CORROSION AROUND NUT PLATE HOLES ON UPPER AND LWR FLANGE SURFACES (DOT 15) REPLACED T-CAP IAW SRM 51-30-2.

Part: INTERCOSTAL — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

MAIN CABIN FLOOR STRUCTURE STA 560 TO STA 580 BL 0 INTERCOSTAL WEB UPPER FLANGE HAS 21 HOLES THAT WERE PREVIOUSLY ELONGATED. REMOVED INTERCOSTAL WEB AND T-ANGLES. FABRICATED NEW INTERCOSTAL AND HEAT TREATED. SEE WORK ORDER 00036352. FABRICATED T-ANGLE AS PER DRAWING 65-59896. INSTALLED AS PER 51-30-2.

Part: ANGLE — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

FWD LWR CARGO PIT CLOSEOUT WEB SUPPORT L-ANGLE AT STA 555 RT SIDE IS CRACKED MANY LOCATIONS. REMOVED AND REPLACED WITH NEW FABRICATED L-ANGLE PER BOEING DRAWING 65-67231 AND SRM 51-30-2 PG 2 AND 3.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN BS 560 FLOORBEAM UPPER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN LBL12 AND LBL 20. REMOVED DAMAGE IAW SRM 51-10-1 MAT WAS .125 REMOVED .005 -.120 REMAINS FOUND TO BE WITHIN LIMITS PERFORMED NDT FOR CRACKS, NEGATIVE RESULTS. ROTO- PEENED IAW SOPM 20-10-03 PG 16. TREATED AND PRIMED IAW SRM 51-10-2 PG 1 EA NR 7-5310713046.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LT WW ABOVE UPLOCK TORQUE TUBE, STR 18 HAS CORROSION ON UPPER SURFACE BETWEEN STA 930 AND 940. REMOVED CORROSION AT LT W/W, STR 18 ON UPPER SURFACE BETWEEN STA 930 TO 940. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 PG 2A. CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER IAW B727 SRM 51-40-2 PG 1. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727SRM 51-10-2, 51-40-2 51-30-2.

Part: FRAME — BENT (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

REWORK: BUCKLE IN BODY FRAME SHEAR TIE WAS STRAIGHTENED USING SRM 51-40-1 (FUSELAGE SKIN) REMOVED SHEAR TIE, FAB NEW SHEAR TIE AND 2 FILLERS, AND INSTALLED AT STA 720B, STRINGER 28 TO STRINGER 28 WL 148 IAW BOEING 727 SRM 53-10-4, PGS 46, 47, 48, 49.

Part: SKIN — DAMAGED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

RT OB FLAP, TRAILING EDGE DAMAGED ON AFT FLAP. REMOVED DAMAGE AND PREPPED FOR REPAIR REF SRM 51-40-20 PARA 7 BONDED ON REPAIR DOUBLER REF SRM 51-40-20 PARA 14, 15, 19, 20, 21, 22. PRIMED AND PAINTED REF M/M 51-20-151-7.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN BS 560 FLOORBEAM UPPER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN LBL 12 AND LBL 20. REMOVED DAMAGE IAW SRM 51-10-1 MAT WAS .125. REMOVED .005 -.120 REMAINS FOUND TO BE WITHIN LIMITS. PERFORMED NDT FOR CRACKS, NEGATIVE RESULTS. ROTO- PEENED IAW SOPM 20-10-03 PG 16. TREATED AND PRIMED IAW SRM 51-10-2 PG 1 EA NR 7-5310713046.

Part: FLOORBEAM — UNKNOWN (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

FOUND REPAIR LOCATED AT BS 1050 FLOORBEAM UPPER CHORD FROM LBL 18" TO 22". REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD REPAIR. REPLACED REPAIR WITH NEW REPAIR. REF FEDEX DWG SR 27-53-034 REV F REPAIR 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN BL 0 SEAT TRACK LEFT FLANGE UPPER SURFACE HAS CORROSION BETWEEN BS 500 AND 580. REMOVED SEAT TRACK AND FABRICATED NEW TRACK FROM BAC1520-792. TREATED PRIMED AND INSTALLED SEAT TRACK REF SRM 51-30-02 P1.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

CABIN MAIN DECK FLOORBEAM AT BS 720 RBL 48" HAS A DOUBLE DRILLED HOLE IN FWD FLANGE OF THE UPPER CHORD. REMOVED DAMAGE AREA'S. FAB 2EA REPAIR ANGLES FAB 3EA SHIMS, FAB CHORD, FAB WEB, FAB T-CHORD PN 65-80690 IAW B727 SRM 51-30-2 FIG NR 8. INSTALLED FAB PARTS AND FASTENERS IAW B727 SRM 51-30-2 PG 5 ALSO REF SRM 53-10-8.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 718, STR 27R ABOUT RBL 12, FLOOR SUPPORT ANGLE IS CORRODED ON REPAIR ANGLE. REMOVED AND INSTALLED NEW REPAIR ANGLE IAW SRM 51-40-3.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 718, STR 27R ABOUT RBL 12, FLOOR SUPPORT ANGLE IS CORRODED ON REPAIR ANGLE. REMOVED AND INSTALLED NEW REPAIR ANGLE IAW SRM 51-40-3.

Part: RIB — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

LEFT OB MID FLAP OB END RIB WEDGE CLIP AND SEAL RETAINER ANGLE ALL CRACKED AT AFT REAR CORNER OF FLAP. REMOVED LT, O/B MIDFLAP, REPLACED WITH SERVICABLE UNIT, REINSTALLED ON NON-ROUTINE #N00234.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

STA 870 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT RBL12 DOT 17. REMOVED CORROSION, ORIGINAL THICKNESS .690, REMAINING .630 REMOVED .060 TOOL NR IN17-1458 DUE 4-24-08 IAW SRM 51-10-1, FOUND TO BE IN LIMITS, ROTO PEENED, CHECKED FOR CRACKS, TREATED, PRIMED, APPLIED BMS 3-23 CORROSION INHIBITOR REF FEDEX EA 7-5310-113048, SRM 51-10-2 AND SOPM 20-10-03. REMOVED AND INSTALLED A FASTENERS THROUGH PULLEY BRACKET IAW SRM 51-03-2. INSTALLED 2 EA NUT PLATES IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 3 · airframe 39,187 hrs · 24,651 cycles

CABIN LBL 25 SEAT TRACK IB AND OB FLANGES UPPER SURFACES HAVE CORROSION BETWEEN BS 560 AND BS 620. REMOVED CORROSION, CHECK FOR MATERIAL LOSS, OUT OF LIMITS. REMOVED SEAT TRACK STA 480-690 LBL 25, FAB NEW SEAT TRACK MATERIAL VERIFIED A-TAG NR A44280 P/O 1023241 BAC1520-792 7178T651. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NUTPLATES AND RADIUS BLOCKS INSTALLED NEW SEAT TRACK STA 480-690 LBL 25 REF SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 650 TO 655, AT STR 28L ABOUT LBL7 STRINGER 28L IS CORRODED. STRINGER SECTION STA 640 11" TO 680 REPLACED ON SNRM N00598. REMOVED STRINGER SECTION FROM STA 680-STA 720 AND INSTALLED NEW SECTION. THE CORRODED STRINGER SECTION WAS OUT OF LIMITS. REF SRM53-10-3/PAGES 1-4B/FIGURE NR 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

STA 740 FLOOR SUPPORT BET BL 0 AND RBL 24 HAS CORROSION AT NUTPLATES HOLES, AND CORROSION BETWEEN BEAM AND FLOOR SUPPORT PLATE AND ALSO A SCRIBE LINE ON TOP SURFACE. REMOVED AND REPLACED FLOOR SUPPORT STRIP REF 51-30-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 718, STR 28R, RBL 8 FLOOR SUPPORT CORRODED ON REPAIR ANGLE. REMOVED CORRODED REPAIR ANGLE, VERIFIED MATERIAL AS BAC1517-1507 7075-T6. FABRICATED NEW REPAIR ANGLE, INSTALLED NEW REPAIR ANGLE, TREATED AND PRIMED NEW REPAIR ANGLE. INSTALLED NEW REPAIR ANGLE REF SRM 51-40-3 FIG 1 SHT 3.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD CARGO AREA, STA 665 TO 675, STR 28L ABOUT LBL 7, STRINGER IS CORRODED REMOVED STRINGER SECTION FROM STA 640 11" TO STA 680 / STR 28L. THE SECTION REMOVED WAS OUT OF LIMITS. INSTALLED NEW SECTION REF SRM 53-10-3/FIGURE NR 1/ PAGES 1-4B.

Part: SHEAR TIE — CORRODED (BS 720C) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720C, STR 28L- 28R WL 148. REMOVED SHEAR TIE DOUBLER, REMOVED CORROSION FROM SHEAR TIE AND DOUBLER. TREATED AND PRIMED SHEAR TIE. INSTALLED NEW SHEAR TIE DOUBLER. NDT FOUND SHEAR TIE WITHIN LIMITS, FOUND SHEAR TIE DOUBLER OUT OF LIMITS REF 51-10-2 PG 7, SRM 51-30-2 PG 2,3 SRM 51-10-6, SRM 53-10-1. SHEAR TIE ORIGINAL MATERIAL THICKNESS IS .063", MATERIAL REMAINING IS .057".

Part: BRACKET — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

A/C DISTRIBUTION BAY BS 740 LBL 6" A/C DUCT SUPPORT BRACKET IS CRACKED ON BULKHEAD ATTACH FLANGE. REMOVED CRACKED SUPPORT BRACKET. VERIFIED MATERIAL AND FABRICATED NEW BRACKET. TREATED, PRIMED, AND INSTALLED NEW BRACKET REF SRM 51-30-2,PG 13-14/ SRM 51-10-2,PG 1, BOEING DRAWING NR 69-47707.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LWR AFT CARGO PIT, STA 1166 BULKHEAD WALL STRUCTURE. UPPER HORIZONTAL L-ANGLE, JUST BELOW FLOORBEAM, 3 FASTENER HOLES HAVE CORROSION ON BACK SIDE. REMOVED ANGLE REF SRM 51-30-2. FABRICATED NEW ANGLE REF DWG 65-67250-2 AND SRM 51-30-5. INSTALLED NEW L-ANGLE REF SRM 51-30-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720D, 2-5" IB OF STR 28L, WL 148 (MKD). REMOVED CORROSION, FOUND TO BE BEYOND LIMITS REF SRM 53-10-1 PG 1&2. REMOVED SHEAR TIE. FABRICATED AND HEAT TREATED SHEAR TIE. INSTALLED NEWLY FABRICATED SHEAR TIE BS 720D IB STR 28L IAW SRM 53-10-4 FIG 15 STEP 12 PG 58.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED BS 720C, STR 25L- 26L, WL 152 (MKD). REMOVED SHEAR TIE BS 720C STR 25L-26L IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE P/N 69-43683-3 A TAG NR A49331 IAW SRM 51-30-2 PAGE 2 AND SRM 51-20-4 PAGE 1.

Part: FRAME — CRACKED (ZONE 400) · airframe 39,187 hrs · 24,651 cycles

NR 2 ENG FWD LT COWL FWD END LWR CORNER CLOSURE COVER ANGLE CRACKED AT OUTER RADIUS. REMOVED DAMAGED CLOSURE COVER ANGLE REF SRM 51-30-2. FABRICATED NEW CLOSURE COVER ANGLE REF SRM 51-30-2 AND DWG 65-19645-199 AND INSTALLED NEW PART REF SRM 51-30-2.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CRACKED BS 720E, 2 "OB OF STR 26L, WL 151 (MKD). REMOVED SHEAR TIE, FORMED, HEAT TREATED, TREATED, PRIMED AND MATCH DRILLED NEW SHEAR TIE. INSTALLED SHEAR TIE REF SRM 51-30-2, REF DRAWING 69-43668, SRM 51-10-2.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME INTERCOSTAL LWR CHORD IS BROKEN/CRACKED BS 720C 19, WL 148. REMOVED CHORD ANGLE REF SRM 51-30-2 PG 2, VERIFIED MATERIAL AS BAC1505-100052. FABRICATED NEW CHORD ANGLE REF BOEING DWG NR 65-58989 ITEM -6. TREATED AND PRIMED REF SRM 51-10-2 PG 2. INSTALLED CHORD ANGLE REF SRM 51-30-2 PG 2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LWR CARGO PIT BILGE STRINGER HAS CORROSION AT END STA 740 STR 27R AT PRESSURE BULKHD TIE. REMOVED SECTION OF STRINGER REF SRM 51-30-2 PG 2, VERIFIED MATERIAL FOR REPAIR. FABRICATED REPAIR PARTS REF SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS REF SRM 51-10-2 PG 2. INSTALLED REPAIR PARTS REF SRM 53-10-3 FIG 1 AND SRM 53-10-2 PG 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION ON LWR O/B FLANGE OF SEAT TRACK STA 950 10" TO 950B 10" RBL 47". REMOVED CORROSION REF SRM 51-10-6 AFTER BLEND. ORIGINAL MATERIAL "T" .081 AFTER BLEND MATERIAL REMAINING .052 FOR A MATERIAL LOSS OF .029 AND WAS OUT OF LIMITS REF SRM 53-10-1 FIG 3. REMOVED TRACK REF SRM 51-30-2. FABRICATED NEW TRACK REF IAW SRM 53-10-5 AND DWG 65-86245. INSTALLED NEW TRACK REF SRM 51-30-2 AND DWG 65-86245

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720, STR 28L- 28R, WL 148 (MKD). REMOVED DAMAGED SHEAR TIE IAW 727 SRM 53-10-4 AND 51-30-2. FAB NEW SHEAR TIE IAW 53-10- 4. INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 AND 51-30-2.

Part: FRAME — UNKNOWN (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FOUND REPAIR LOCATED AT BS 700 ON FRAME BETWEEN STR S-20R AND S-23R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR REF SRM 51-30-2. FABRICATED INNER CHORD REF DWG 65-82614. INSTALLED REPAIR ANGLES REF DWG 65-15938 AND DWG 65-82614 AND SRM 51-30-2.

Part: SKIN — CRACKED (RT WING) · airframe 39,187 hrs · 24,651 cycles

RT WING LEADING EDGE CUTOUT IS CRACKED AT NR 6 SLAT INBD TRACK CUTOUT. INSTALLED DOUBLER REPAIR ON R/ WING LEADING EDGE CUTOUT AT NR 6 SLAT I/B TRACK CUTOUT. REF B727 SRM 51-30-02 PG2 57-30-4 PG 33 FIG II.

Part: CHANNEL — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

LT WING OB TE FLAP WELL LWR FIXED PNL SPPT CHANNEL IS CRACKED AT STRUT ATTACH POINT RSS 501 IB SIDE (MKD). REMOVED AND REPLACED CHANNEL ON LT WING OB TE FLAP P/N 65-21658 USE P/O 1013862, FX 0993 IAW B 727 SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/CORRODED BS 700, STR 28L-28R, WL 148 (MKD) REF SNRM N01157. REMOVED SHEAR TIE, BLENDED CORROSION ON FRAME, NDT FOR CRACKS, FABED NEW SHEAR TIE REF DRWG 69-14871-12. HEAT TREATED PART REF WO N01217. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED SHEAR TIE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LWR FUSELAGE RT SIDE STA 740, RBL 7,KEEL BEAM CORRODED BETWEEN T-CAP FITTING AND SKIN. REMOVED FASTENERS FROM KEEL BEAM, REMOVED KEEL BEAM, DRILLED HOLES IN NEW KEEL BEAM ON SHOP NON ROUTINE NR N01206. INSTALLED BOLTS AT STA 740 IN KEEL BEAM USING TOOL S/N NR 030763468 DUE DATE 3-5-08 REF. DWG 65-2355. INSTALLED FASTENERS IN KEEL BEAM.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LEFT GEAR BODY DOOR AFT STOP FITTING SUPPORT CHANNEL IS CRACKED AND BROKEN AT LWR ATTACH FLANGES AND STRAP. FABRICATED REPAIR CHANNEL AND ANGLES IAW B727 SRM 51-40-3. ALODINE, AND PRIME REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALL FASTENERS IAW B-727 SRM 51-30-2. INSTALLED REPAIR PARTS IAW B-727 SRM51-40-3 PG 1. THIS REPAIR IS CLASSIFIED AS MINOR.

Part: PANEL — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LT MLG WHEEL WELL, AFT LOWER WEB FAIRING ENCLOSURE, AFT SIDE HAS 2 FASTENER HOLES CRACKED LBL40-42, STATION JUST AFT OF 950 WL 147. REMOVED DAMAGED AREA'S IAW B727 SRM 51-10-1. FAB REPAIR FILLER AND DOUBLER IAW B727 SRM 51-40-3. INSTALLED-FAB FILLER AND DOUBLER, IAW B727 SRM 51-40-3. THIS REPAIR IS CLASSIFIED AS MINOR.

Part: BRACKET — GOUGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT STRUCTURE, BS 740, AT FWD END OF DELTA BEAM, "T" BRACKET, WL 150, RBL 5", IS GOUGED IN FWD RADIUS AREA. REMOVED "T" BRACKET REF SRM 51-30-2. INSTALLED NEW "T" BRACKET AND FASTENERS REF SRM 51-30-02.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD LWR CARGO PIT BILGE, FRAME ATTACH ANGLE LWR END HAS CORROSION, STA. 720E OB SIDE AT KEEL BEAM EXTENSION STR 28R REMOVED FRAME ATTACH ANGLE SRM 51-30-2. FABRICATED NEW FRAME ATTACH ANGLE REF BOEING DWG 69-43665-1/1. TREATED AND PRIMED NEW ANGLE, SRM 51-10-2. INSTALLED FRAME ATTACH ANGLE SRM 51-30-2.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/BROKEN BS 720C, STR 27R-28R, WL 148. REPAIRED SHEAR TIE FLOOR SUPPORT AND SHIMS REFERENCING SRM 53-10-4 FIG 11, 51-10- 2, AND 53-10-2, AND BOEING DRAWING 69-43676. TREATED AND PRIMED ALL REPAIR PARTS REF SRM 51-10-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY SKIN STRINGER IS CORRODED BS 720F 17, STR 27L, WL 149 (MKD). REMOVED CORROSION, MEASURED MATERIAL LOSS OUT OF LIMITS, VERIFIED REPAIR MATERIAL. FABRICATED NEW PARTS REF SRM 53-10-3 FIG 1, TREATED AND PRIMED REF SRM 51-10-2 PG 2. INSTALLED REPAIR PARTS REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CRACKED BS 720, 1" I/B OF STR 26L, WL 151 (MKD). REPLACED DAMAGED SHEAR TIE AT FWD PIT STA 720, 1" INBD OF STR 26L. REF SRM 51-30-02 PG 1-12, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/BROKEN BS 720A, STR 26R-27R, WL 150 (MKD). REPLACED DAMAGED SHEAR TIE AT FWD PIT STA 720A , 1" INBD OF STR 26R. REF SRM 51-30-2 PG 1-12, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER — GOUGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY SKIN STRINGER HAS SEVERAL GOUGES BS 720D TO 720E 8, STR 26L, WL 151 (MKD). REMOVED GOUGES, NDT VERIFIED BLENDED AREA OUT OF LIMITS. REMOVED AND INSTALLED STRINGER SECTION FROM STA 720C 10 TO 740 STR 26L, REF SRM 53-10-3 PG 3-4B, SRM 51-30-2, SRM 51-10-2,THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION AROUND NUT PLATE HOLE ON UPPER SURFACE OF UPPER T-CAP STA 950C LBL27.5". REMOVED CORROSION FROM AFT MAIN DECK UPPER SURFACE NUTPLATE HOLE ON T-CAP STA 950C LBL 27.5. HFEC AREA, NO DEFECTS NOTED. SHOT PEEN AREA, TREAT PRIMED, AND APPLIED BMS 3-23 REF SRM 51-10-01, EA 7-5310-113041 THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STA 990 STR 26-27 L SHEAR TIE CORRODED STR 26-27 L. REMOVED 2 EA FASTENERS REF 51-30-2. REMOVED CORROSION REF SRM 51-10-1 NDT'D IAW B727 NDT MAN PART 4 51-00-00 FIG 2 ORIGINAL THICKNESS .063. REMOVED .003 ;.060 MATERIAL REMAINING WITHIN LIMITS REF SRM 51-00-00 FIG 1 DETAIL I. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED 2 EA FASTENERS REF SRM 51-30-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

AFT PIT STRINGER CLIP CRACKED STA 950E STR 28L REMOVED CRACKED STRINGER CLIP REPLACED WITH NEW CLIP PART NR 6611809-2 IAW SRM 51-30-2 PG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — FAILED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 49" DOES NOT CONFORM TO SRM. REMOVED EXISTING REPAIR ANGLES IAW SRM 51-30-2 FABRICATED NEW REPAIR ANGLE FOR BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 48", IAW FED EX DWG SR27-53-034. SENT OUT REPAIR ANGLES FOR HEAT TREAT AND CAD PLATE AND INSTALLED REPAIR REF SR27-53-034 REPAIR NR 1.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

CABIN BS 540 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN RBL2 AND RBL 10 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .125 REMOVAL .005, SELF CONTAINED SHOT PEEN AREA. APPLIED ALODINE AND PRIME, APPLIED CORROSION INHIBITING COMPOUND, REF SRM 51-10-1, 51-10-2, 51-20-5, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113040. CLASSIFIED MINOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

CABIN FLOORBEAM AT BS 480 HAS SCRATCHES ON UPPER SURFACE OF UPPER TEE BETWEEN RBL 27 AND RBL 40 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .130 REMOVAL .008, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND, REF SRM 51-10-1, 51-20-5, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113038. CLASSIFIED MINOR REPAIR.

Part: SKIN — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

PNEU GROUND CONNECTION SERVICE DOOR (#3903) CUTOUT HAS CRACK AT I/B AFT CORNER. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED. REF EA 7-53330-10732, SRM 51-10-2, 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR STOP DRILLED CRACK REF BOEING 727 SRM 51-10-1 AND HFEC, NO DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT SHEAR TIE CORRODED STA 990 STR 28-29L FAB SHEAR TIE AND SHIM REF SRM 53-10-4. TREATED AND PRIMED REPAIR MATERIAL FOR SHEAR TIE 7075-O-071. HEAT TREATED TO T6, CUT OUT DAMAGED AREA, INSTALLED REPAIR PART REF SRM 53-10-3. THIS REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — UNKNOWN (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FOUND REPAIR LOCATED AT STR S-27R FROM BS 674 TO 700 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR IAW BOEING 727 SRM 51-10-2. REPAIRED STRINGER USING NEW STRINGER, SPLICE AND 3 FILLERS. FABRICATED AND INSTALLED AT STA 696, STRINGER 27R USING BOEING 727 SRM 53-10-3 PAGE 4B DETAIL I AND 51-10-2, ALL PARTS TREATED AND PRIMED. ALSO, BEFORE INSTALLATION USING BOEING 727 SRM 51-10-2, PG 1 REF. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT SHEAR TIE CORRODED STA 950D BETWEEN STR 28-29L CUT OUT DAMAGE AREA OF SHEAR TIE AT STA 950D, BETWEEN STRINGER 28-29 L IAW BOEING SRM 53-10-4, REPAIR 3. FABRICATED REPAIR BRACKET AND FILLER IAW BOEING SRM 53-10-4. REPAIR 3. HEAT TREATED REPAIR BRACKET IAW AAR 111HT, REVISION 5-1-07 NR 2007-06-11 AND TO SPECIFICATIONS FOR REPAIR MATERIAL IN BOEING 7272 SRM 53-10-4 REPAIR 3 SHEET (2). LOCATED, DRILLED AND INSTALLED REPAIR BRACKET AND FILLER IAW BOEING 727 SRM 53-10-4 REPAIR 3, 51-30-2, 51-20-4. THIS IS CLASSSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — GOUGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

CABIN BS 500 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN BL 0 AND RBL 25 BLENDED AREA, VERIFIED MATERIAL LOSS, AND NO CRACK BY NDT, FLAP PEENED REF EA 7-5310-113039, TREATED AND PRIMED AREA. APPLIED CORROSION RESISTANT COMPOUND THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

CABIN BS 480 FLOORBEAM UPPER CHORD HAS SCRATCHES BETWEEN RBL 48 AND RBL 60 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .130 REMOVAL .002, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND, REF SRM 51-10-1, 51-10-2 51-20-05, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113038. CLASSIFIED MINOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN STA 940 FLOORBEAM HAS CORROSION BETWEEN BEAM UPPER FLANGE AND SEAT TRACK AT BL 0 REMOVED CORROSION FROM FLOORBEAM AT STA 940 BL 0 IAW B727 SRM 51-10-1, ORIGINAL .125 REMAINING .123. HFEC NO DEFECTS NOTED ROTO PEENED FLOORBEAM. TREATED AND PRIMED REWORKED AREA IAW EA 7-5310-113050. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720A, STR 27L-28L, WL 148. REMOVED CORROSION, ORIGINAL .050", REMAINING- .045", MATERIAL LOSS- .005", WITHIN LIMITS REF SRM 51-10-1 AND 53-10-1, TOOL NR 2221 CAL DUE 4-24-08, STRAIGHTENED SHEAR TIE REF SRM 51-40-1, NDT. NO DEFECTS NOTED REF NDT -00-00 PT 6 FIG 23, TOOL NR IN22-0044, CAL DUE 5-21-08. TREATED AND PRIMED REF SRM 51-10-2, LEVEL 1 CORROSION.

Part: PANEL — CRACKED (ZONE 500) · airframe 39,187 hrs · 24,651 cycles

LT WING OB TE FLAP WELL LWR FIXED PANEL CORRUGATED SUPPORT PLATE IS CRACKED RSS 516-523. REPLACED CORRUGATED SPLICE IAW SRM 51-30-02.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME, SHEAR TIE IS CORRODED, BS 720A, 2" OB OF STR 28R, WL 148. REMOVED CORROSION. ORIGINAL - .050", REMAINING - .046", MATERIAL LOSS - .004", WITHIN LIMITS REF SRM 53-10-1, TOOL NR 18172, CAL DUE 1-19-08. TREATED AND PRIMED REF 51-10-6 AND 51-10-2. LEVEL 1 CORROSION.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE, BODY FRAME SHEAR TIE IS CORRODED, BS 72OF STR 28L- 28R, WL148. REMOVED CORROSION, REFERENCING SRM 51-10-1, ORIGINAL THICKNESS .072", BLENDED TO .067" MATERIAL LOSS .005" WITHIN LIMITS, REFERENCING SRM MEASURED WITH TOOL NR IN17-9593 CAL DUE 5-16-08 TREATED AND PRIMED REF SRM 51-10-2. LEVEL 1 CORROSION

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN, LBL 25 SEAT TRACK IB FLANGE HAS CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 460. REMOVED CORROSION IAW B727 SRM 51-10-1, ORIGINAL .080", REMAINING .059" REF EA NR 7- 5310-113056, ROTO PEENED SEAT TRACK FLANGE AT STA 400-460 LBL 25. TREATED AND PRIMED SEAT TRACK REF EA 7-5310-113056.

Part: FRAME — CORRODED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720B, STR 28L-28R, WL 148. REMOVED CORROSION, ORIGINAL THICKNESS- .063", REMAINING- .058", MATERIAL LOSS- .005". WITHIN LIMITS REFERENCING SRM 51-10-6 AND 53-10-1 USING NR 2221 CAL DUE 4-24-08. STRAIGHTEN SHEAR TIE, REF SRM 51-40-1, NDT, NO DEFECTS NOTED REF NDT 51-00-00 PT 6 FIG 23, TOOL NR IN 22-0044, DUE 5-21-08. TREATED AND PRIMED SHEAR TIE REF SRM 51-10-2. LEVEL 1 CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK , FLOORBEAM TOP CAP HAS CORROSION AND A DRILL START ON UPPER SURFACE, STA 950E, LBL 35. REMOVED DAMAGE AREA OF FLOORBEAM AT STA 950E LBL 35 IAW B727 SRM 53-10-8. FABRICATED REPAIR ANGLES (2 EA) AND FILLER FROM BAC1490-2888 PO NR 10156633 A TAG NR 03969 IAW B272 SRM 51-10-8. TREATED AND PRIMED REPAIR AREA AND REPAIR PARTS IAW SRM 53-10-8.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXTERNAL REPAIR LOCATED AT BS 1120 TO 1130, STR S-18L TO S-19L, DID NOT CONFORM TO SRM 53-30-1. REMOVED EXISTING DOUBLER PER SRM 51-30-2. BLENDED OUT DAMAGE, EXTENDED CUT OUT TO REMOVE FASTENER HOLES WITH NO EDGE DISTANCE, REF 53-30-3 PG 5. FABRICATED DOUBLER TREATED AND PRIMED, AND INSTALLED DOUBLER REF MM 51-20-31-7 AND MM 51-20-21-7.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FUSELAGE BS 720 TO BS 740, S-27L TO S-26L EXTERNAL DOUBLER CORRODED ON BOTH SIDES AROUND DUCT CUTOUT. REMOVED CORROSION REFERENCING SRM 51-10-1 VERIFIED MATERIAL TO BE .125". REMOVED .OO6". REMAINING MATERIAL .119" FOUND TO BE WITH IN LIMITS REFERENCING SRM 53-30-1. TOOL NR IN17-9593 CAL DATE 5/16/08 TREATED AND PRIMED REFERENCING SRM 51-10-2

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE, BODY FRAME SHEAR TIE, IS BUCKLED/CRACKED BS 720B, STR 25L - 26L, WL 152. REPLACED DAMAGED SHEAR TIE AT FWD PIT STA 720B, BETWEEN STR 25L AND 26L, REF SRM 51-30-2 PG 1-12.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 560 ON FRAME BETWEEN STR S-22L AND S-26, DID NOT COMFORM TO SRM 51-40-3 PG 1-6. REMOVED OLD DOUBLER AND FILLER, FABRICATED NEW DOUBLER AND FILLER, HEAT TREATED, ALODINED AND PRIMED REF SRM 51-40-3 PG 1-6.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND REPAIR LOCATED AT BS 1050 FRAME BETWEEN STR S-26R AND S-28R DID NOT CONFORM TO SRM 51-40-3. REMOVED EXISTING REPAIR, REMOVED Z-ANGLE, GUSSET, TIE DOWN BRACKET FOR ACCESS. FABRICATED NEW REPAIR PARTS, REF SRM 51-4O-3 FIG 1. HEAT TREATED PART, DRILLED UP PART, TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR, TIE DOWN BRACKET, GUSSET AND Z ANGLE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

FWD PIT BILGE BODY FRAME, SHEAR TIE, IS CORRODED, BS 720, STR 27L-28L, WL 148. LEVEL 1 CORROSION. REMOVED CORROSION, TREATED AND PRIMED REF SRM 51-10-6 AND 51-10-2. ORIGINAL THICKNESS .050". REMAINING .047" MATERIAL LOSS IS .003" WITHIN LIMITS REF SRM 53-10-1 NR TOOL NR 18172 CAL.

Part: DOOR FRAME — NONE (ZONE 800) · airframe 39,187 hrs · 24,651 cycles

FOUND ON HIDDEN INSPECTION LT AFT SERVICE DOOR, 3RD FRAME, 9" FROM FWD EDGE, LOWER SHEAR TIE, LOWER SURFACE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .045", MATERIAL LOSS OF .001, REMAINING MATERIAL IS .044" TOOL USED IN17-0458 CAL DATE 4-24-08 WITHIN LIMITS REF SRM 52-00-02 TREATED AND PRIMED SRM 51-10-2 '

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 39,187 hrs · 24,651 cycles

HIDDEN DAMAGE INSP LT AFT SERVICE DOOR LOWER AFT STOP FITTING HAS CORROSION. [07-06-07] DRILLED UP NEW STOP FITTING PER. SRM 51-30-5 PG 1, INSTALLED IT, PER SRM 51-10-1 PG. 10 AND 51-30-2 PG. 2-5. INSTALLED CORROSION INHIBITING COMPOUND TO THE LOWER PART OF DOOR PER OHM 52-036-21 PG. 404 AND INSTALLED COVER PANEL PER SRM 51-30-2 PG 2-5

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, BOTTOM FRAME, INNER SURFACE IS CORRODED UNDER LEVELING COMPOUND FROM FWD TO AFT END OF FRAME. [07-06-07] DRILLED UP NEW BEAM PER SRM 51-30-5 PG.1, INSTALLED LOWER BEAM ON AFT SERVICE DOOR, PER SRM 51-10-1 PG.10 51-30-2 PG 1-5 INSTALLED LOWER GATE PER OHM 52-40-07 PG 505 AND INSTALLED COVER PANELS PER SRM 51-30-2 PG 2-5

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 39,187 hrs · 24,651 cycles

HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM AFT EDGE UPPER SURFACE OF LOWER FRAME, SHEAR TIE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE. ORIGINAL MATERIAL IS .050", REMOVED .005", REMAINING MATERIAL IS .045". CHECKED MATERIAL LOSS WITH TOOL IN17-0458 CAL DATE 4/24/07 WITHIN LIMITS REF SRM 52-10-2

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 39,187 hrs · 24,651 cycles

HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR 2ND FRAME, 4" FROM FWD EDGE, UPPER SURFACE OF LOWER FRAME SHEAR TIE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .050", MATERIAL LOSS OF .001", REMANING MATERIAL IS .049", WITHIN LIMITS. TOOL USED IN17-0458 CAL DATE 4-24-08 REF SRM 52-00-2, TREATED AND PRIMED REF 51-10-2.

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 39,187 hrs · 24,651 cycles

HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM FWD EDGE UPPER SURFACE OF LOWER SHEAR TIE IS CORRODED. THIS SDR IS A DUPLICATE OF SDR NR 07-2257 AND INADVERTENTLY ENTERED IN ERROR. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN FLOOR PANEL SUPPORT AT BS 418 HAS CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND RBL 23. REMOVED AND REPLACED SUPPORT REF SRM 51-30-02.

Part: STRUCTURE — CORRODED (BS 720D-720E) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LWR FWD CARGO PIT, CORROSION ON LT AND RT SIDES AT MOUNTING HOLES, FWD OF WORK PLATFORM THATS AT STA 720D TO 720E. ACCOMPLISHED 2 TYPICAL FORMED REPAIRS AT STA 720D AND STA 720E LOWER CARGO PIT WORK PLATFORM PANEL REF SRM 51-40-3 PG 1-6.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

RBL SEAT TRACK HAS CORROSION BETWEEN UPPER CHANNEL AND LWR MOUNT FLANGE STA 783-849. REMOVED CORROSION REF SRM 53-10-1 FIG 3 SHT 5. .015" MAT. REMOVED. OUT OF LIMITS REF SRM 53-10-1 FIG 3. REMOVED FLOORBEAM AND SEAT TRACK BS 740 TO 850 RBL 45. FABRICATED NEW FLOORBEAM OUT OF BAC1506-1108. REF FED EX GMM7-0-1001, SRM 51-30-02 TREATED AND PRIMED FLOORBEAM REF MM 51-20-031-1, 51-20-21-7. INSTALLED FLOORBEAM AND SEAT TRACK REF BAC DWG 65-16279, SRM 51-20-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT SHEAR TIE CORRODED STA 970 BETWEEN STRINGER 28-29L REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT SHEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071, HEAT TREATED TO T-6 CONDITION ON SNRM NR N01032, 8130 TRACKING NR 2007-06-30. DRILLED AND INSTALLED SHEAR TIE REPAIR REF 53-10-4 FIG 15, SRM 51-30-2, SRM 51-10-1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, CORROSION ON SEAT TRACK LWR O/B UPPER SURFACE STA 950 LBL 26K. REMOVED CORROSION REF SRM 51-10-1, VERIFIED REMAINING MATERIAL WITHIN LIMITS REF SRM 53-10-1 FIG 3. TREATED AND PRIMED REF MM 51-20-002-7.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FWD PIT FLOOR SUPPORT STIFFENER STA 580, RBL 9, IS CRACKED REMOVED AND REPLACED STIFFENER AT STA 580 RBL 9, IAW B727 SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STR CLIP/FLOOR SUPPORT ANGLE CORRODED AT STA 990 STR 29L REMOVED CORRODED STIFFENER REF SRM 51-30-2. REMOVED CORROSION FROM STIFFENER REF SRM 51-10-01 PG 14-16. FABED FILLER FROM 7075-T6- .071. TREATED AND PRIMED STIFFENER AND FILLLER REF MM 51-20-021-7 AND MM 51-20-031-7 AND INSTALLED STIFFENER AND FILLER REF SRM 51-30-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT UPPER MAIN DECK, SEAT TRACK HAS CORROSION, ON UPPER INBD FLANGE, STA 1070 2 LBL 45. REMOVED CORROSION ORIG THICKNESS .530. REMOVED .036, REMAINING .494" MATERIAL. REMOVED IS WITHIN LIMITS. TREATED AND APPLIED PRIMER REF SRM 53-10-1 PG 13-17.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

RT WING O/B T/E UPPER SURFACE PANEL JUST INBD OF AILERON, JACKSCREW FAIRING ATTACH ANGLE CRACKED INSIDE FAIRING. REMOVED DAMAGED ANGLE, DRILLED UP, PRIMED AND PAINTED NEW ANGLE ON PANEL INBD OF AILERON, REF SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT SHEAR TIE CORRODED STA 950F STR 25L-29L. REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT SHEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071" SENT TO HEAT TREAT ON SNRM NR N00976 FORM 8130 TRACKING NR 2007-05-157 TO T-6. DRILLED AND INSTALLED SHEAR TIE, REPAIR REF SRM 53-10-4 FIG 15, SRM 51-30-02, SRM 51-10-1 AND SRM 53-10-4 .

Part: SKIN — CORRODED (BS 680-740) · airframe 39,187 hrs · 24,651 cycles

FWD LOWER FUSELAGE BELLY SKIN, BS 680 TO 740 STR 26L TO S-26R NEEDS TO BE REPLACED DUE TO MULTIPLE AREAS OF CORROSION AND DAMAGES. [08-29-07] BELLY SKIN AT STA. 680 TO 740, BETWEEN STR 26L TO 26R, WAS REMOVED. NEW SKIN WAS DRILLED UP TO MATCH EXISTING STRUCTURE. DOUBLER/ TRIPLER WAS INSTALLED AT STA 700 TO 740, STR 26L TO 26R, REF FED EX EA 7-5330-113938. INSTALLED NEW SKIN (65-54590-7) AND RELATED WING TO BODY STRUCTURE. REF' S USED SRM 51-10-1, 51-30-2.

Part: STRINGER CLIP — GOUGED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

MAIN CABIN, STRINGER CLIP GOUGED IN RADIUS AT STA 680 AT STR 7L REPLACED DAMAGED STRINGER CLIP AT BS 680 STR 7L REF SRM 51-30-2 PG 1&2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

UPPER MAIN DECK FLOOR SUPPORT STRUCTURE, INTERCOSTAL LWR STRAP HAS CORROSION (VIEW FROM PIT) FROM STA 1115 TO 1130, RBL 46. REMOVED CORROSION AT STA 1115 TO 1130 RBL 46, IAW B727 SRM 51-10-6. 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. REMOVED DAMAGED SECTION OF FLOOR STABILIZER IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PLATE FROM 7075-T6 .040, TREATED AND PRIMED REPAIR PLATE IAW SRM 51-10-2. INSTALLED REPAIR PLATE IAW SRM 51-40-2.

Part: FLOOR SUPPORT — CORRODED (BS 970) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STR CLIP FLOOR SUPPORT ANGLE CORRODED STR 29L, STA 970 REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT, FABRICATED SHIM AND DRILLED UP NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10-2 PG 1, SRM 51-20-1 FIG 10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STRINGER CLIP FLOOR SUPPORT ANGLE CORRODED STA 950F, STR 29L REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT. FABRICATED SHIM AND DRILLED UP. INSTALLED NEW FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10--2 PG 1, SRM 51-20-1, FIG 10.

Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

NR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET REF, FED EX J/C 76C07500 AND BOEING DWG 65-21795 AND SRM 51-30-2 PG 4&5.

Part: FLAP TRACK — CRACKED (NR 5) · airframe 39,187 hrs · 24,651 cycles

NR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. THIS SDR WAS ENTERED IN ERROR. THIS IS A DUPLICATE OF TRACKING NR 07-2224 KEEP NR 07-2224 AS ORIGINAL AND ACTIVE. THIS SDR WAS SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,187 hrs · 24,651 cycles

FWD ENTRY FLOOR SUPPORT UPPER FLANGE CRACKED BS 310, LBL32. REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 53-30-2.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

FOUND ON AGING A/C INSP EXISTING REPAIR AT STR S-27R FROM BS 610 TO BS 630 DOES NOT CONFORM TO CURRENT SRM 53-10-3 FIG 1. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON STR 27R, BS 610 TO BS 630, REF SRM 53-10-3 PG 3. INSTALLED STRINGER SPLICE REPAIR HAT CHANNEL, REF SRM 53-10-3 PG 3.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING I/B AFT FLAP UPPER SURFACE 30" FROM O/B END, 9" FROM T/E DID NOT CONFORM TO SRM 51-40-20. REMOVED PREVIOUS REPAIR AND BONDED ON REPAIR REF SRM 51-40-20 PARAGRAPHS, 7, 14, 18, 20, 21, AND 22. TAP TEST GOOD. PRIMED AND PAINTED REF.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 39,187 hrs · 24,651 cycles

AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING AFT FLAP UPPER SURFACE 18" FROM I/B END 12" FROM T/E DID NOT CONFORM TO SRM 51-40-20 PARA 7. REMOVED PREVIOUS REPAIR AND BONDED ON NEW REPAIR REF SRM 51-40-20 PARAGRAGHS 7, 14, 15, 18, 20, 21, AND 22 TAP TEST GOOD, PRIMED AND PAINTED REF MM 51-20-151-7.

Part: FLOORBEAM — MISREPAIRED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX DWG SR27-53-034 AT BS 680 LBL 3'' TO 23''. REMOVED OLD REPAIR, FABRICATED NEW PARTS AND INSTALLED REF SRM 51-10-1 AND FED EX DWG SR27-53-034.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STA 950E-950F STR 29L KEEL BEAM CORRODED REMOVED CORROSION, REMOVED .052" MAXIMUM DEPTH ON KEEL BEAM BETWEEN STA 950E AND 950F IS OUT OF LIMITS. SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED REPAIR STRAP, FABRICATED FILLER WASHER AND INSTALLED REPAIR PARTS. REF FED EX STANDARD REWORK DRAWING, LT AND RT KEEL BEAM FLANGE CORROSION, DRAWING NUMBER SR27-53-023A.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STA 950E STR 29L STRINGER CLIP/FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE REF SRM 51-30-2.

Part: FLOORBEAM — MISREPAIRED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

ON AGING AC INSPECTION FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT FED EX SR27-53-034 AT BS STA 720D, LBL27"-43" FLOORBEAM. REMOVED OLD REPAIR, FABRICATED 2 NEW ANGLES, HEAT TREATED, CAD PLATED, PRIMED AND PAINTED. INSTALLED 2 NEW ANGLES AND FILLERS AT STA 720D, LBL 27"- 43" REF SRM 51-30-2, MM 51-20-151-7, AND FED EX DWG SR27-53-034F REPAIR NR 1.

Part: SKIN — CRACKED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

LOWER EXTERNAL SKIN IS CRACKED AT BS 1082, RBL 4. R EMOVED SURROUNDING STRUCTURE TO ACCESS DAMAGE. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL, NO DEFECTS. INSTALLED DOUBLER AND FILLER WHERE DAMAGE WAS REMOVED. INSTALLED SURROUNDING STRUCTURE REF SRM 51-30-2, SRM 53-30-2 FIG 2 AND 3, NDT MAN PART 6 51-00-00, FIG 23.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STR 29L KEEL BEAM CHORD CORRODED STA. 970-990 REMOVED A MAXIMUM OF .048" CORROSION ON KEEL BEAM BETWEEN STA 970 AND 990 AND IS OUT OF LIMITS. SPOT FACED FASTENER HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP AND INSALLATION OF REPAIR PARTS ON SNRM N00644/JPF ITEM 7-18.

Part: DOOR — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LEFT AFT EMERGENCY EXIT HATCH INTERIOR STRUCTURE ATTACH ANGLE AT FWD LWR CORNER OF WINDOW FRAME CORRODED REMOVED OLD ANGLE AT FWD CORNER OF WINDOW FRAME AND FABRICATED AND INSTALLED A NEW ANGLE USING 7075-T-6 .071". ORIGINAL THICKNESS WAS .071" CALIPER GAUGE NR 18238, REF SRM 52-20-1 AND 51-30-1.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT SHEAR TIE CORRODED STA 950E BETWEEN STR 28-29L. REMOVED CORRODED SHEAR TIE AND REPAIRED PER SRM 53-10-4 FIG 15.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STR 29L, KEEL BEAM CHORD CORRODED STA 950F-970 REMOVED A MAXIMUM OF .032" OF CORROSION ON KEEL BEAM BETWEEN STA 950F AND 970 AND IS OUT OF LIMITS. SPOT FACED HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP. INSTALLATION OF REPAIR PARTS ON SNRM N00644/JPF ITEMS 7-18.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT STR 29L/KEEL BEAM CHORD CORRODED BETWEEN STA 950D - 950E REMOVED CORROSION, FABRICATED REPAIR STRAP, SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED FILLER WASHER AND INSTALLED REPAIR PARTS. REF FED EX STANDARD REWORK DRAWING, LT AND RT KEEL BEAM FLANGE CORROSION, DWG NR SR27-53-023.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN FLOOR SUPPORT WEB AT STA 804 RBL 45 IS CRACKED OUT FASTENER HOLE. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT WEB STA 804, RBL 5, SRM 51-30-2, DWG 65-16279.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

AFT PIT ANTENNA DOUBLER CORRODED AT STA 1030-1050 BETWEEN STR 29R-30. REMOVED NR 3 VHF ANTENNA AND DOUBLERS REF SRM 51-30-02. REMOVED HAT CHANNEL. REMOVED CORROSION FROM DOUBLERS. ORIGINAL THICKNESS .196" REMOVED .002 REMAINING .194" WITHIN LIMITS REF SRM 51-10-01. REMOVED CORROSION FROM SKIN. ORIGINAL THICKNESS .071" REMOVED .009", REMAINING .065" FOUND TO BE WITHIN LIMITS REF SRM 53-30-01. FAB`D NEW HAT CHANNEL, AND T-ANGLE REF DWG 65-59591 AND 10136-2004. REINSTALLED HAT CHANNEL REF SRM 51-30-02 NR 3 VHF ANTENNA REINSTALL ON SNRM N00997.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

LOWER FUSELAGE STA 1082 STR 30 HAS CORROSION ON LOWER SURFACE OF STRINGER AT CUT OUT FOR SKIN. REMOVED DAMAGED SECTION OF OF STRINGER 30, AT STA 1082 AND REPAIRED REF SRM 53-10-30 FIG 1.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND FWD RT CORNER OF AIR STAIR CUTOUT DID NOT CONFORM TO FED EX DWG SR27-53-024. REMOVED OLD DOUBLER, HFEC INSP TO VERIFY CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER REF, FED EX DWG 27-53-024.

Part: SKIN — MISREPAIRED (TE FLAPS) · airframe 39,187 hrs · 24,651 cycles

AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20, AT RT WING OB AFT FLAP T/E 8" TO 22" FROM OB END. REMOVED PREVIOUS REPAIR AND REPAIRED AFT FLAP REF SRM 51-40-20 PAR 7, 14, 15, 18, 21, 22. PRIMED AND PAINTED REPAIR REF MM 51-20151-7.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN BS 620, FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE, LBL 37 TO LBL 42 REMOVED CORROSION, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS =.135, REMOVED .013". FLAP PEENED BLENDED AREA. TREATED AND PRIMED AND APPLIED CORROSION INHIBITOR. REF SRM 51-10-2, MM 51-20-151, SOPM 20-10-3 AND EA NR 7-5310-113045.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,187 hrs · 24,651 cycles

CABIN BS 620 FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE FROM LBL 3 TO LBL22 REMOVED CORROSION, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS= .135". REMOVED .017" FLAP PEENED BLENDED AREA, TREATED AND PRIMED AND APPLIED CORROSION INHIBITOR. REF SRM 51-10-6, 51-10-2, MM 20-151, SOP M 20-10-3 AND EA NR 5310-113045.

Part: WEB — GOUGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

AGING A/C INSP. FOUND REPAIR LOCATED AT BS 620 FWD LOWER CARGO DOOR AFT FRAME FWD SURFACE UPPER CORNER, HAS ADDITIONAL DAMAGE ON AFT SIDE. REMOVED EXISTING REPAIR REF SRM 51-30-2. BLENDED DAMAGE AREA, ORG. THICKNESS .071, AFTER BLENDING, THICKNESS .064" TO .068". WITHIN LIMITS PER REF SRM 53-10-1 PG 2. MANUFACTURED NEW DOUBLER REF SRM 51-10-2. INSTALLED DOUBLER AND FASTENERS SRM 51-30-2.

Part: TAB — DENTED (RUDDER) · airframe 39,187 hrs · 24,651 cycles

LWR RUDDER TAB LT SIDE HAS SPOT OF SURFACE DAMAGE, 14" UP FROM BOTTOM AND 8" FWD FROM BACK EDGE. REPAIRED DAMAGE TO LOWER RUDDER TAB LT SIDE REF SRM 51-40-9 PARA 3D. APPLIED CONDUCTIVE COATING REF MM 51-20-051-7. APPLIED PRIMER AND PAINT REF MM 51-20-151-7. NO RE-BALANCING REQUIRED REF SRM 51-80-0 PG.1A

Part: SKIN — DAMAGED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

RT LOWER FUSE STA 380-387 STR 23R, 3 LIGHTNING STRIKES. REMOVED LIGHTNING STRUCK RIVETS, HFEC FOUND CRACKS AROUND RIVET HOLES AND SKIN. REMOVED DAMAGE, SECOND TIME HFEC FOUND NO CRACKS. FAB`D DOUBLER, DRILLED AND INSTALLED, PRIMED AND PAINTED IN REF TO SRM 51-30-2 PG 13-16, SRM 53-30-3 FIG 3, FIG 20. SRM 51-10-2 PG 1. THIS REPAIR WORKED WITH SNRM N00131.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

RT INBD FOREFLAP T/E IS DELAMINATED 36" FROM INBD END. REPAIRED DELAMINATION REF SRM 51-40-21 PG 1 AND 2, TAP TEST GOOD.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 39,187 hrs · 24,651 cycles

ON AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX STD REWORK DWG SR27-53-024. REMOVED OLD DOUBLER SRM 51-30-2, HFEC VERIFY OF CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER PER DWG SR27-53-024, TREATED AND PRIMED DOUBLER REF MM 51-20-151-7. INSTALLED NEW DOUBLER AND FASTENERS RE SRM 51-30-2.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 39,187 hrs · 24,651 cycles

FOUND REPAIR LOCATED AT RT O/B FOREFLAP LWR SURFACE I/B END ON AGING A/C INSP. EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20. REPAIRED RT O/B FOREFLAP AREA REF SRM 51-40-20 PARA 14-20, 21, 22.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM STA 322 CORRODED AT BL0TO LBL45. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW FXB727 SRM 53-10-8 FIG 9. ALODINED AND PRIMED PARTS IAW FX B727 SRM 51-10-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

SEAT TRACK CORRODED STA 480-690 AT LBL 24. REMOVED DAMAGED SEAT TRACK STA 480-690 AT LBL24, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 480 FROM BL0 TO LBL45. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 480 FROM BL0 TO LBL45 ALL IAW FX B727 SRM 53-10-8, 53-10-1 AND 51-10-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

SEAT TRACK CORRODED STA 480-690 AT LBL 45. REMOVED SEAT TRACK STA 480-690 AT LBL 45 IAW FX B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICES IAW FX B727 SRM 53-10-5. ALLODINED, PRIMED AND INSTALLED SEAT TRACK IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM STA 344 HAS CORROSION AT LBL10-RBL16 (PREVIOUS SPLICE AT LBL10). REMOVED DAMAGED AREA PER FE SR27-53-007 FIG 11. FABRICATED AND INSTALLED NEW UPPER CAP BEAM REPAIR IAW FX SR27-53-007 FIG 11. ALLODINED AND PRIMED IAW FX B727 SRM 51-10-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

SEAT TRACK CORRODED STA 720-740 AT BL0. REMOVED CORRODED SEAT TRACK AT STA 720-740 ON BL 0, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INST NEW SEAT TRACK SECTION STA 720-740 AT BL0 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

SEAT TRACK CORRODED STA 690-740 AT LBL24. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK SECTION STA 690-740 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2,51-10-5 AND 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 560 FROM BL0 TO LBL45. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP IAW FX SR27-53-034E FIG 30 SHT 5. FABRICATED, DRILLED AND LOCATED REPAIR "T", SUPPORTS, FILLERS, ANGLES AND "T" CAP REPAIR ANGLES IAW FX SR27-53-034E FIG 30 SHT 5. INSTALLED REPAIR "T" SUPPORT, FILLERS ANGLES AND "T" CAP REPAIR ANGLES IAW FX SR27-53-034E FIG 30 SHT 5. ALODINED AND PRIMED ALL REPAIR PARTS IAW FX SRM B727 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 680 FROM BLO TO LBL 45. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND AREA FROM LBL8 TO LBL12 TO BE OUT OF LIMITS IAW FX P-F SRM 53-10-1. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW FX SR27-53-034E FIG 1. ALODINED AND PRIMED REPAIR PARTS IAW FX SRM B727 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 720A FROM BL0 TO LBL45. REMOVED, FABRICATED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR STA 720A BLO TO LBL 45 ALL IAW FX SR 27-53-034E FIG 5, FX B727 SRM 51-10-2, 53-10-1, BAC5619(H) AND BAC 5701.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

SEAT TRACK CORRODED STA 690-740 AT LBL45. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 690 TO 740 AT LBL45 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 720D FROM RBL 24 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 720D FROM RBL 24 TO LBL 45 ALL IAW FX SR27-53-034E FIG. 1 & 4, FX B727 SRM 51-10-2, BAC5619 (H) AND BAC 5701.

Part: FLOORBEAM — MISDRILLED (ZONE 200) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM STATION 380 HAS PREVIOUS DRILLED HOLES IN RADIUS AND NO EDGE DISTANCE AT LEFT BUTT LINE 50 TO 60. CUT OUT DAMAGE SECTION OF UPPER BEAM CAP IAW FEDEX SR27-53-034E FIGURE 30. REMOVED TIEDOWN, RADIUS STOPS AND VERTICAL STIFFENERS IAW FEDEX SRM 51-30-2. FABRICATED REPAIR FILLER IAW FEDEX SR27-53-03E FIGURE 30. ALODINED AND PRIMED FILLER IAW FX B727 SRM 51-10-2. FABRICATED REPAIR ANGLES IAW FX SR 27-53-034E FIG 30. PRIMED REPAIR ANGLES IAW FX B727 SRM 51-10-20. INSTALLED REPAIR ANGLES AND FILLER IAW FX SR27-53-034E FIG 30. REINSTALLED TIEDOWN RADIUS, STRAPS AND VERTICAL STIFFENER IAW FX SRM B727 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,740 hrs · 23,509 cycles

FLOORBEAM CORRODED STA 620 FROM BL 0 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM BL 0 TO LBL45 ALL IAW FX SR 27-53-034E FIG 1 & 4,FX B727 SRM 51-10-2,BAC5619(H) AND BAC5701.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,100 hrs · 23,016 cycles

STRINGER 22L IS CORRODED AT STA 1180. REPAIRED STRINGER 22L IAW SRM 53-10-3 PG 48 DETAIL 1.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 37,100 hrs · 23,016 cycles

1183 BULKHEAD REPAIR. COMPLIED WITH EA 7531055423 REPAIRED HOLE IN 1183 BULKHEAD.

Part: MOTOR — LEAKING (FLAP DRIVE) · airframe 36,253 hrs · 22,338 cycles

DURING CLIMBOUT OF MEMPHIS, HYDRAULIC PUMP 1 LOW PRESSURE LIGHT FLASHED, FOLLOWED BY AND IMMEDIATE LOSS OF PRESSURE AND QUANTITY. PRESSURE, QUANTITY WAS AT ZERO PRIOR TO PUMPS BEING TURNED OFF. SUSPECT PROBLEM IS IN RIGHT WHEEL DUE TO SKYDROL MIST IN THE AREA. REPLACED RIGHT O/B FLAP DRIVE MOTOR REF 727-200 M/M 27-51-062-4.

Part: SWITCH — FAULTY (L/E FLAP) · airframe 35,439 hrs · 21,706 cycles

AFTER TAKEOFF WHEN RETRACTING FLAPS FROM 5 DEGREES THE PILOTS L/E FLAP AMBER LIGHT ILLUMINATED. S/O PANEL SHOWED THE NR 1 L/E FLAP WAS AMBER. RAN RED TABS RETURNED TO MEM AFTER DUMPING APPROX 4000 LBS FUEL. R&R NR 1 L/E FLAP SWITCH REF B727 MM 27-82-001-4.

Part: STRINGER — CRACKED (VERTICAL STAB)

CRACKED STRINGER AT VERT FIN STRINGER 8 AT RIB NR 2 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1.

Part: STRINGER — CRACKED (VERTICAL STAB)

CRACKED STRINGER AT VERTICAL FIN STA 20, STR LT RIB NR 2. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON FRAME WEB BS 990, STR 24 RT. REPAIRED FRAME BS 990 STR 22-29 RT PER SRM 51-40-2.

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION ON SKIN UNDER WEB/INTERCOSTAL AT BS 950F - 970, LBL 14, WL 148. REPAIRED SKIN BS 950F - 970, LBL 14, WL 148 IAW SRM 53-30-3 FIG 3.

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION AT STR 28L, BS 950F+8, WL 148. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3.

Part: FRAME — CORRODED (FUSELAGE)

FOUND FRAME CORRODED AT BS 720C, RBL 25, WL 148 C53-111-01. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1.

Part: ANGLE — CRACKED (FUSELAGE)

AFT AIRSTAIR RT LWR TORQUE BOX INTERNAL BS 1263 BULKHEAD UPPER FWD SIDE L-ANGLE IS CRACKED, JUST BELOW AIR STAIR ACTUATOR. REMOVED AND REPLACED AFT AIRSTAIR PER SRM 51-30-2 & 51-10-2.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON FRAME AND SHEAR TIE BS 990 BETWEEN STR 28-29 LT. REPAIRED SHEAR TIE & FRAME IAW FEDEX EA 7-5310-64980 & SRM 53-10-4 FIG 15.

Part: BUSHING — WORN

01-317 ON CLIMB GOT AN AMBER LEAD EDGE FLAP LIGHT. R&R WORN BUSHING & ADJ PER MM 27-82-001-4.

Part: BRACKET — CRACKED (NLG) · airframe 33,462 hrs · 20,029 cycles

NOSE LANDING GEAR DOWNLOCK ACTUATOR SUPPORT BRACKET FITTING CRACKED. INSPECTION NOTE: MEASURED CRACK TO BE APPROX 1 IN. FROM RT UPPER MOUNT HOLE PROGRESSING THRU HOLE DOWNWARD. INSTALLED NEW BRACKET ASSY.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

LOWER AFT BODY HEAT LIGHT ILLUM IN FLT. UTILIZED RED TAB PROC. LIGHT REMAINED ILLUM. *S/D* REPLACED CONNECTOR PER 727-200 MM 20-62-14. REMOVED AND REPLACED PANELING PER 727-200 MM 26-14-1. NO FURTHER DEFECTS NOTED. OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT)

99-284 - R2 WINDOW STARTED ARCING. SHUT R2 OFF COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 2 SLIDING WINDOW. ADJUSTED PER MM 56-12-011-5.

Part: STRINGER — CORRODED (BS 683-688)

FWD CARGO BS 683 TO 688, STR 27 LT, CORROSION INSIDE STRINGER UNDER LEVELING COMPOUND. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER SRM 51-10-02. CORROSION REMOVAL ONLY, NO REPAIR REQUIRED.

Part: BELLFRAME — DENTED (BS 500)

NR 0747, NR 0798 71C209-02 - FWD CARGO BS 500, STR 19-25 RT: 11 DENTS ON TOP SIDE OF BELLFRAME. INSTALLED DOUBLERS BS 500 RT PER SRM 51-40-3.

Part: BELLFRAME — BENT (BS 970)

NR 0544 71C70902 - LOWER AFT CARGO COMP, FS 970 BELLFRAME INNER FLANGE BENT OUTWARD BETWEEN STR 25 AND 26 LEFT. REMOVED DAMAGED DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER PER SRM 51-40-30.

Part: BELLFRAME — DENTED (BS 560)

NR 0741 71C209-02 - FWD CARGO BS 560, STR 22-25 LT 8 DENTS IN TOP SURFACE OF BELLFRAME. CUT OUT DAMAGED SECTION OF BELLFRAME PER SRM 53-10-4. INSTALLED BELLFRAME REPAIR PER SRM 53-40-4.

Part: STRINGER — CORRODED (BS 684-687)

NR 0114, NR0280 71C209-02 - CORROSION STR 27 RT, BS 684-687 CORRODED, BLENDED BEYOND LIMITS FOR REMOVAL. REMOVED CORRODED SECTION, SPLICED IN NEW STRINGER SECTION PE153-10-3 SRM.

Part: DOUBLER — CRACKED (BS 720)

NR 0727 W/C 72C235-02 - STR 15L CRACKED AT END STA 720B + 5. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-3 FIG 5.

Part: BELLFRAME — DENTED (BS 680)

NR 0504 71C205-02 FWD CARGO BS 680, STR 21-25 RT, 2 DENTS IN TOP LEG OF BELLFRAME. CUT OUT DAMAGED AREA OF BELLFRAME PER SRM 53-10-4. INSTALLED REPAIR PER SRM 51-40-3.

Part: DOUBLER — DAMAGED (BS 680)

NR 0732 72C235-02 - STR 15L CHANNEL GOUGED AT STA 680 BLENDED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-3 PAGE 5 FIG 3.

Part: FRAME — CORRODED (CARGO DOORWAY)

NR 0310 71C709-02 - LOWER AFT CARGO COMPT NR 2 CARGO DOOR CUTOUT AFT LOWER CORNER SEVERE CORROSION AFFECTING 1.5 BY 1 AREA OF AFT DOOR FRAME AT FS 990 BETWEEN STRINGER 26 AND 27 RT. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED AREA. INSTALLED ANGLE REPAIR PER SRM 51-40-3 USING PROPER FASTENERS.

Part: STRINGER — CORRODED (BS 683-688)

NR 0283 71C209-02, FWD CARGO BS 683-688, STR 27 LT: CORROSION INSIDE STRINGER UNDER LEVELING COMPOUND. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER SRM 51-10-02. CORROSION REMOVAL ONLY. NO REPAIR REQUIRED.

Part: SKIN — CORRODED (BS 680-683)

FWD CARGO BS 680 TO 683, STR 28 LT CORROSION ON FUSELAGE SKIN OUTBD OF STRINGER. REMOVED CORROSION FROM SKIN AT STA 680 TO 683, O/B OF STR 28 LT PER SRM 51-10-6. TREATED AND PAINTED PER SRM 51-20-0. CORROSION REMOVAL ONLY, NO REPAIR REQUIRED.

Part: SKIN — CORRODED (BS 680-683)

NR 0282 71C209-02, FWD CARGO BS 680-683, STR 28 LT: CORROSION ON FUSELAGE SKIN OUTBD OF STRINGER. REMOVED CORROSION FROM SKIN AT BS 680-683 AND OB OF STR 28 LT PER SRM 51-10-6. TREATED AND PAINTED PER SRM 51-20-0. CORROSION REMOVAL ONLY. NO REPAIR REQUIRED.

Part: SKIN — CORRODED (BS 682-686)

NR 0279 71C209-02 FWD CARGO BS 682-686, STR 27 RT HAS CORROSION AROUND AND UNDER LEVELING COMPOUND ON FUSELAGE SKIN. CUT OUT DAMAGED AREA OF FUSELAGE SKIN PER SRM 51-10-6. INSTALLED DOUBLER PER SRM 53-30-3.

Part: STRINGER — CORRODED (BS 620-624)

NR 0278 71C209-02, FWD CARGO BS 620-624, STR 27 RT: CORROSION INSIDE STRINGER UNDER LEVELING COMPOUND. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR OF 7075-T6 .090 PER SRM 53-10-3 FIG 1 DETAIL 1.

Part: STRINGER — CORRODED (BS 620-624)

FWD CARGO BS 620 TO 624, STR 27 RT CORROSION INSIDE STRINGER UNDER LEVELING COMPOUND. CUT OUT DAMAGED AREA AND INST FILLER AND DOUBLER REPAIR OF 70757-6 .090 PER SRM 53-10-3 FIG 1 DETAIL 1.

Part: BELLFRAME — DENTED (BS 660)

NR 0332 71C209-02 - FWD CARGO BS 660, STR 22-25 LEFT, BELLFRAME UPPER LEG DENTED 5 PLACES. INSTALLED DOUBLER AT BELLFRAME AT STA 660, STR 22-25 LEFT PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 500)

NR 0746 71C203-02 - FWD CARGO BS 500 - 3 DENTS ON TOP SURFACE OF BELLFRAME STR 22-23 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 560)

NR 0741 71C209-02 - FWD CARGO BS 560, STR 22-25 LEFT, 8 DENTS IN TOP SURFACE OF BELLFRAME. INSTALL BELLFRAME REPAIR PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 700)

NR 0328 71C209-02 - FWD CARGO BS 700, STR 22-25 LEFT, 7 DENTS IN UPPER LEG OF BELLFRAME. INSTALLED REPAIR PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 520)

NR 0744 71C209-02 - FWD CARGO BS 520, STR 23-25 LEFT 6 DENTS ON TOP OF BELLFRAME. REPAIRED BELLFRAME PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 720)

NR 0319, NR 0525 71C209-02 - FWD CARGO BS 720A, STR 24-25 RT: 2 DENTS IN TOP LEG OF BELLFRAME. DYE CHECKED DENTS, NO CRACKS FOUND PER BACOHM 20-20-02. INSTALLED REPAIR DOUBLER PER 51-40-3.

Part: FRAME — DENTED (BS 680)

71C209-02 NR0330 - FOUND FWD CARGO BS 680, STR 23 - 24LT, HAS 3 DENTS IN UPPER LEG OF BELLFRAME. CUT OUT DAMAGED SECTION OF BELLFRAME, PER SRM 51-40-3, FIG 1. INSTALLED DOUBLER PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 720)

NR 0326 71C209-02 - FWD CARGO BS 720, STR 23-24 LEFT BELLFRAME DENTED UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3.

Part: BELLFRAME — DENTED (BS 540)

NR 0743 71C209-02 - FWD CARGO BS 540, STR 22-25 LEFT, 3 DENTS ON TOP SURFACE OF BELLFRAME. REPAIRED BELLFRAME AT STA 540, STR 22-25 LEFT IAW SRM 51-40-3 FIG 1.

Part: FLOORBEAM — CORRODED (BS 1070)

NR 0381 72C237-02 - CORROSION AT TOP OF UPPER LOBE FLOORBEAM STA 1070, RBL 55. REMOVED CORROSION PER SRM 51-10-6. INSTALLED FLOORBEAM REPAIR PER AARD 53-10-07-2 FIG 2.

Part: MOUNT — CRACKED (NR 3 ENGINE)

FOUND NR 3 ENGINE FWD MOUNT HAS A 3.5 INCH CRACK IN THE UPPER FITTING ROOT. *S/D* REMOVED AND REPLACED NR 3 ENGINE FWD MOUNT PER FED-EX EA 7-5410-34137.