N951FD

Part: STRAP — CORRODED (ZONE 300) · airframe 36,796 hrs · 25,761 cycles

STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. DOT 10/012. COMPLIED WITH EA # F-5330-T0376272 A P1 FUSELAGE - PLATES OF SKINS - APU DOOR SURROUND STRUCTURE FABRICATION OF SUPPORT ANGLES ALTERNATIVE SURFACE FINISH. MAJOR REPAIR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 36,796 hrs · 25,761 cycles

STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. DOT 10/012. COMPLIED WITH EA # F-5330-T0376272 A P1 FUSELAGE - PLATES OF SKINS - APU DOOR SURROUND STRUCTURE FABRICATION OF SUPPORT ANGLES ALTERNATIVE SURFACE FINISH. MAJOR REPAIR.

Part: STRAP — CORRODED (ZONE 300) · airframe 36,796 hrs · 25,761 cycles

STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. COMPLIED WITH EA F-5330-T0376272 A P1.

Part: FILLER — GOUGED (ZONE 300) · airframe 36,796 hrs · 25,761 cycles

LH AFT FUSE STA 1801 BTW STR 16L-17L HAS GOUGE ON FUSE SKIN. DOT 10/008. EVALUATED AREA,FOUND FILLER TO BE GOUGED ONLY. REMOVED AND REPLACED FILLER ONLY IAW SRM 53-80-70-2R REPAIR 2, FIG 201 AND TABLE 201 DETAIL I ON LH AFT FUSELAGE STA 1801 BETWEEN STR 16L-17L. MAJOR REPAIR.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 36,316 hrs · 25,429 cycles

L1 DOOR SLIDE RAFT UNABLE TO BE ARMED. FOUND ATTACH SURVIVAL KIT STRAP D RING UNDER GIRT BAR (NO DAMAGE), REINSTALLED SURVIVAL KIT STRAP D RING IAW AMM FIG 405. L1 DOOR SLIDE ARMS AND DISARMS NORMAL IAW AMM 25-66-01-4.

Part: NONE — CRACKED (ZONE 400) · airframe 35,472 hrs · 24,852 cycles

#2 ENG I/B T/R EXTERNAL SURFACE FWD LOWER CORNER IS CRACKED. REPAIRED CRACK IN FIBERGLASS LAYERS OF #2 ENGINE I/B T/R EXTERNAL SURFACE FWD LOWER END ACTORATOR ACCESS PANEL IAW RR RB211 535-E4-37110 EM 78-31-300-084 PARA 17.

Part: NONE — CRACKED (N/A) · airframe 35,472 hrs · 24,852 cycles

#9 SLAT, INTERNAL COVE PANEL IS CRACKED @ OSS 604 REMOVED & REPLACE COVE PANEL ASSY IAW BAC DWG 114N4003 REV G & BAC DWG 114N4076 REV C

Part: NONE — DELAMINATED (ZONE 400) · airframe 35,472 hrs · 24,852 cycles

RIGHT ENGINE FAN CASE ATTRITION LINER AT 6 O,CLOCK POSITION HAS APPROX 2.5" BY 2" HOLE/HONEYCOMB MISSING. REMOVED AND INSTALLED NEW ATTRITION LINER IAW RB211 EM 72-34-14-300-007 AND REMOVED AND INSTALLED NEW ICE BREAKER PANELS IAW RB211 EM 72-34-14-300-014. WRI CARD 72107874

Part: NONE — CRACKED (N/A) · airframe 35,472 hrs · 24,852 cycles

#9 SLAT INTERNAL COVE PANEL IS CRACKED @ OSS 574 REMOVED & REPLACED COVE PANEL IAW BAC DWG 114N4003, REV G & BAC DWG 114N4076 REV C

Part: NONE — NONE (655) · airframe 35,472 hrs · 24,852 cycles

RH WING INB FWD FLAP LEADING EDGE WORN APPROX 73" OUTB OF THE INB EDGE REPAIRED RH WING INB FLAP LEADING EDGE NOSE SKIN DOUBLER IAW B757-200 SRM 57-53-01- 2R REPAIR 3

Part: NONE — DELAMINATED (ZONE 600) · airframe 35,472 hrs · 24,852 cycles

RH I/B FWD FLAP UPPER SURFACE IS DELAMINATED APPROX 38" I/B OF THE O/B EDGE REPAIRED RH WING I/B FWD FLAP UPPER SKIN DELAM IAW B757 SRM: 57-53-01-2R FIG. 201 SHEET 2 AND 51-70-10-0G. MAJOR REPAIR.

Part: NONE — DELAMINATED (ZONE 600) · airframe 35,472 hrs · 24,852 cycles

RH WING I/B FLAP UPPER SURFACE IS DELAMINATED APPROX 47" I/B OF O/B EDGE REPAIRED R/H WING I/B FWD FLAP UPPER SURFACE DELAM IAW B757 SRM: 57-53-01-2R FIG. 201 SHEET 2 AND 51-70-10-0G. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (N/A) · airframe 35,472 hrs · 24,852 cycles

MAIN DECK FLOOR PANEL 241MAF, UPPER SURFACE IS PUNCTURED ON FWD, INBD SIDE REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201 REPAIR 1

Part: SKIN PANEL — NONE (ZONE 300) · airframe 35,472 hrs · 24,852 cycles

LEFT HORIZONTAL STABILIZER UPPER SKIN INBOARD OF LOGO LIGHT IS DENTED REPAIRED HORIZONTAL STABILIZER UPPER SKIN PANEL IAW B757 SRM 51-70-10-2R REPAIR 3 AND 4.

Part: FLOOR PANEL — NONE (N/A) · airframe 35,472 hrs · 24,852 cycles

MAIN DECK FLOOR PANEL 242MAF, UPPER SURFACE IS DENTEDON FWD, INBD SIDE REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201, REPAIR 1

Part: FLOOR PANEL — NONE (N/A) · airframe 35,472 hrs · 24,852 cycles

MAIN DECK FLOOR PANEL 241MGF, UPPER SURFACE IS DENTED IN 2EA PLACES REPAIRED 2EA DENTS IAW B757 SRM 53-00-50-2R, FIG 201, RPEAIR 1

Part: FLOOR PANEL — NONE (N/A) · airframe 35,472 hrs · 24,852 cycles

MAIN DECK FLOOR PANEL 242MBF, UPPER SURFACE IS DENTED IN 2EA LOCATIONS REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201, REPAIR 1

Part: FRAME — CRACKED (N/A) · airframe 35,472 hrs · 24,852 cycles

CRACK INDICATION NOTED AT THE LOWER, OUTBD HOLE AT STATION 1640 FRAME WEB, COMMON TO STRINGER 14L AS FOUND WHILE ACCOMPLISHING EO F-5310-E0344602 REPAIRED HOLE IAW FEDEX EA F-5310-T0364795

Part: NONE — CRACKED (N/A) · airframe 35,472 hrs · 24,852 cycles

STATION 580 FLOORBEAM HAS A CRACK IN AFT UPPER FLANGE RADIUS @ APPROXIMATE LBL 40 REPAIRED FLOOR BEAM IAW FEDEX DRAWING SR57-53-004 & EA # F-5310-T0364849-P1

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 33,985 hrs · 23,797 cycles

FOUND DURING WRI# 05-50/6574. ANTISKID/AUTOBRAKE CONTROL UNIT HAS MSG "BOX 1-5" THAT WILL NOT CLEAR. DURING TRANSDUCER SPINUP TEST, TRANSDUCER #1 SPINUP DOES NOT RESULT IN RELEASE OF BRAKE #5. REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT REF B757 MM 32-42-01-4. CONTROL UNIT INSTALLATION TEST PASSED. NEED TO ACCOMPLISH ANTISKID TRANSDUCER SPINUP TEST PER MM 32-42-00-5 ACCOMPLISHED ANTISKID TRANSDUCER SPINUP TEST PER MM 32-42-00-5 . OPS CHECKED NORMAL

Part: SKIN — GOUGED (EPENNAGE) · airframe 33,854 hrs · 23,717 cycles

L\H SIDE OF EMPENNAGE HAS 2 EACH SMALL GOUGES AT STABILIZER LOWER SLIDING SEAL AREA BETWEEN B.S. 1800 AND B.S. 1810 BLENDED GOUGES ON L\H SIDE OF EMPENNAGE STA 1800 TO 1810 IAW B757 SRM 51-10-02. AFTER FURTHER EVAL FOUND STA 1810 TO BE OUT OF LIMITS IAW B757 SRM 53-80-70-1A FIG 101 DET IV. CUT OUT DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW B757 SRM 53-80-70-2R REP 2 FIG 201

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 33,854 hrs · 23,717 cycles

RIGHT SIDE HORIZONTAL STABILIZER EXTERIOR UPPER SKIN ALONG FRONT SPAR LOOSE AND AND FLAKING PAINT WITH BARE METAL AS MARKED. COMPLIED WITH EA # F-5510-T0350281 P1. TITLE: STABILIZES-HORIZON STABILIZER-RH HORIZONTAL STABILIZER FWD TORQUE BOX UPPER SKIN BLEND REPAIR.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 33,854 hrs · 23,717 cycles

LEFT SIDE HORIZONTAL STABILIZER EXTERIOR UPPER SKIN ALONG FRONT SPAR LOOSE AND FLAKING PAINT WITH BARE METAL AS MARKED. COMPLIED WITH EA # F-5510-T0350222 P1 TITLE: STABILIZERS - HORIZON STABILIZER - LH HORIZONTAL STABILIZER FWD TORQUE BOX UPPER SKIN BLEND REPAIR.

Part: INDICATOR — FAILED (TE FLAPS) · airframe 33,421 hrs · 23,417 cycles

WHEN EXTENDING FLAPS FROM 15 DEGREES TO 20 DURING APPROACH, TRAILING EDGE LIGHT ILLUMINATED, AND THE TE FLAP DISAGREE EICAS MESSAGE APPEARED. DELARED EMERGENCY, COMPLIED WITH THE QRH AND LANDED. ARFF RESPONSED TO THE EMERGENCY. TROUBLESHOT IN REF TO FIM 27-51 FAULT TREE 805 FOUND FAULT CODE ON #1 FSEU CODE 305 ON FLIGHT LEG #9 CHECKED FLAP OVERLOAD INDICATORS FOUND LEFT OUTBOARD TRANSMISSION P/N # 25IN4022-34, S/N # 0053 OVERLOAD INDICATOR POPPED RE-SET INDICATOR CYCLED FLAPS IN BOTH ALTN AND WITH HYDRAULIC'S FLAPS OP'S CHECKED NORMALLY. OK FOR SERVICE.

Part: ADC — FAILED (NR 1) · airframe 33,143 hrs · 23,231 cycles

AT 4000FT IN THE TURN TO JOIN 36L LOC THE CAPTAINS AIRSPEED BECAME UNRELIABLE. TEMP WAS 13 DEGREES C WITH ENG TAI OFF. AN EMERGENCY WAS DECLARED. ATC PROVIDED VECTORS TO ALLOW US TIME TO RUN THE AIRSPEED UNRELIABLE CHECKLIST. THE CHECKLIST WAS FOLLOWED AND DETERMINED FIRST OFFICERS INFORMATION AND STANDBY WAS CORRECT. FIRST OFFICER BECAME PF AND FLEW ILS 36C TO LANDING KMEM. WHEN AIRSPEED BECAME UNRELIABLE THE L ENG EEC AND R ENG EEC BOTH DISPLAYED AS CAS MESSAGES AND THE TRANSPONDER WOULD NOT WORK IN NR 1 POSITION. CONFIRMED FAILED L ADC. REMOVED AND REPLACED L AIR DATA COMPUTER REF MM 34-12-01-4. REQUIRED ADC OPS CKS ALL NORMAL. L (NR 1) ATC TRANSPONDER CKS NORMAL REF MM 34-53-99-5. OK FOR SERVICE.

Part: GUIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,214 hrs · 22,574 cycles

UNABLE TO CLOSE THE L1 DOOR. DOOR PROGRAMMING INCORRECT. TIGHT AT FRONT, GAP AT TOP AFT CORNER. REMOVED THE L1 DOOR SLIDE COVER IAW AMM 52-11-00-5. ADJUSTED THE L1 DOOR GUIDE ARM AND HANDLE MECHANISM IAW AMM 52-11-04-2, AND 52-11-13-2. OPS CHECKED GOOD IAW AMM 52-11-00-5. REINSTALLED L1 DOOR SLIDE COVER IAW AMM 52-11-00-5.

Part: COVER — BROKEN (R1 DOOR SLIDE) · airframe 31,595 hrs · 22,170 cycles

R1 DOOR SLIDE COVER BOTTOM EDGE BROKEN POTTED NEW INSERTS IN R1 DOOR SLIDE COVER IAW AMM 25-00-00-8. REMOVED SAFTEY PIN AND INSTALLED R1 DOOR SLIDE COVER IAW AMM 52-11-02-4. OK FOR SERVICE

Part: COVER — BROKEN (R1 DOOR SLIDE) · airframe 31,578 hrs · 22,160 cycles

R1 DOOR SLIDE COVER BOTTOM EDGE BROKEN. POTTED NEW INSERTS IN R1 DOOR SLIDE COVER IAW AMM 25-00-00-8. REMOVED SAFTEY PIN AND INSTALLED R1 DOOR SLIDE COVER IAW AMM 52-11-02-4. OK FOR SERVICE.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 304 hrs · 21,400 cycles

RIGHT WING INBD FLAP UPPER SURFACE IS DELAMINATION AT WS 258. REPAIRED RT WING, INBD FLAP UPPER SURFACE WS 258 BY HOT BONDING REPAIR PLYS IAW SRM 57-53-01-2R REPAIR 1 FIG 201 & SRM 51-70-07 PARA 4 G & EA F-5750-TO320630.

Part: WEB — CORRODED (BS 420-440) · corrosion level 2 · airframe 29,133 hrs · 20,363 cycles

FLOOR WEB CORRODED UPPER SURFACE LBL 12 BS 420-440. REMOVED CORROSION FROM WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5.4.3.

Part: SEAT TRACK — CORRODED (BS 420-440) · corrosion level 2 · airframe 29,133 hrs · 20,363 cycles

SEAT TRACK SPLICE CORRODED, LBL 24, BS 420-440. REMOVED DAMAGED SEAT TRACK SPLICE. FABRICATED AND INSTALLED IAW DRAWINGS 3505,3475 REV G, AND 3458 REV K.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 28,459 hrs · 19,979 cycles

LEFT FWD ENTRY DOOR DIFFICULT TO GET DOOR TO ARM PROPERLY, IN ARM POSITION, BUT TAKE REPEATED ATTEMPTS TO GET SLIDE ARMED LIGHT TO ILLUMINATE. CLEANED DEBRIS FROM LT FWD ENTRY DOOR , OPERATED SLIDE ARM SYSTEM IAW MM REF 25-66-00-5. ACFT OK TO CONTINUE.

Part: SEAL — DIRTY (COCKPIT WINDOW) · airframe 28,035 hrs · 19,690 cycles

DURING DESCENT OUT OF 35000, PSID APPROX 8.0-7.8, A LOUD SQUEAL FROM F/O'S WINDOW. ONCE PSID GOT LOWER THAN 7.8 SQUEAL WENT AWAY. CLEAN WINDOW SEAL IAW MM 56-11-53-4 AND RETORQUED. FASTENERS ON FO'S SLIDING WINDOW IAW MM 56-11-02-4. PRESSURIZED ACFT UP TO 8.0, NO SQUEAL AT THIS TIME. OPS CHECK GOOD. FINAL CLOSED.

Part: WIRE — DAMAGED · airframe 27,905 hrs · 19,606 cycles

DURING CLIMB OUT, AT FL 330 RT HYD PRESSURE DROPPED TO ZERO, EICAS RT HYD SYS PRESSURE ILLUMINATED RT RF ON STATUS PAGE. PRESSURE RETURNED TO NORMAL AND EICAS WARNING EXTINGUISHED. FOUND THAT WHEN WIRE W4220-1001-22 AT ABOUT 3" FROM D42134P IS MOVED, THE RT HYD QTY IN THE EICAS PAGE BECOMES VERY ERRATIC AND MOST OF THE TIME WILL GO TO 0.00 RF. SPLICED IN A NEW SECTION OF WIRE REF SWPM 20-10-13. VERIFIED OPERATION OF BRAKE PRESSURE INDICATION, WHEEL WELL LIGHTS, PARKING BRAKE SYS, GROUND GEAR DOOR CLOSE SYSTEM AND HYD QTY SYSTEM, REF AMM 32-41-15-4, 33-31-00-2, 32-44-00-5, 32-00-15-2 AND 29-33-00-5. RAN RIGHT ENGINE IAW JRH. HYD QTY REMAINS STEADY WITH NO LOSS OF INDICATION. OK FOR SERVICE.

Part: GIRT BAR — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 27,500 hrs · 19,382 cycles

DOOR SLIDE DOES NOT ENGAGE WHEN ARMED. SLIDER FOUND NOT ATTACED TO GIRT BAR. REINSTALLED SLIDER AND GIRT BAR ASSY ONTO L1 DOOR AND PERFORMED ADJUSTMENT TESTS IAW MM 52-11-25-5. WITH DOOR CLOSED, GIRT BAR SLIDERS ENGAGE FLOOR FITTINGS AND SLIDE ARMS PROPERLY.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 27,497 hrs · 19,379 cycles

L1 DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 52-11-01-A.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 27,493 hrs · 19,376 cycles

L1 ENTRY DOOR SLIDE LIGHT IS BURNED OUT. RELAMPED L1 ENTRY DOOR SLIDE LIGHT IAW MM 33-13-00-2, CHECKED GOOD AT THIS TIME.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 27,456 hrs · 19,356 cycles

LT WING OTBD T/E FLAP OTBD L/E CHAFING MARK FOUND. DAMAGED SKIN PANEL REPAIRED IAW EA F-5730-152588. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1460. REPAIR CARRIED OUT ON LT CARGO TIE DOWN FITTING AT STA 1460 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (BS 1300) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1300. REPAIR CARRIED OUT IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY LT TIE DOWN FITTING HAS CORROSION AT STA 520. CORROSION REPAIR CARRIED OUT ON TIE DOWN FITTING AT STA 520 IAW EA F-5340-152585. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY LT TIE DOWN FITTING HAS CORROSION AT STA 580. CORROSION REPAIR ON LT TIE DOWN FITTING CARRIED OUT IAW EA 5340-152585. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 540. CORROSION REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 540 IAW EA F-5340-152585. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP RT TIE DOWN FITTING HAS CORROSION AT STA 1240. REPAIR CARRIED OUT ON RT CARGO TIE DOWN FITTING IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 1280 CORROSION. REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 1280 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP TIE DOWN FITTING LT HAS CORROSION AT STA 1620. CORROSION REPAIR ON CARGO TIE DOWN FITTING CARRIED OUT IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (ZONE 200) · airframe 27,456 hrs · 19,356 cycles

FUSELAGE EXTERIOR SKIN WITH EXISTING DENT AT BS 1701, BETWEEN STR 14L TO STR 15L. DENT REPAIR CARRIED OUT IAW EA F-5330-152589. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY, LT TIE DOWN FITTING HAS CORROSION AT STA 620. REPAIR CARRIED OUT ON LT TIE DOWN FITTING AT STA 620 IAW EA F-5340-152585. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 520. CORROSION REPAIR CARRIED OUT ON FWD LWR CARGO COMP. RT TIE DOWN FITTING IAW EA F-5340-152585. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP RT TIE DOWN FITTING HAS CORROSION AT STA 1220. REPAIR CARRIED OUT ON RT CARGO TIE DOWN FITTING IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 1600. REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 1600 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1240. REPAIR CARRIED OUT ON LT TIE DOWN FITTING AT STA 1240 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1220. REPAIR CARRIED OUT ON AFT CARGO COMPARTMENT LT TIE DOWN FITTING AT STA 1220 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY LT TIE DOWN FITTING HAS CORROSION AT STA 560 CORROSION REPAIR ON LT TIE DOWN FITTING AT STA 560 CARRIED OUT IAW EA F-5340-152585. REPAIR CLASSIFIED AS MAJOR.

Part: TIE DOWN — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

FWD LWR CARGO BAY LT TIE DOWN FITTING HAS CORROSION AT STA 600. CORROSION REPAIR CARRIED OUT ON LT TIE-DOWN FITTING AT STA 600 IAW EA F-5340-152585. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 790-810) · airframe 27,456 hrs · 19,356 cycles

SEAT TRACK AT BS 790 TO 810, RBL 45, HAS DAMAGE TO CROWN AND CHANNEL. REMOVED AND REPLACED IAW SRM 51-40-02 REV.103. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 834-841) · airframe 27,456 hrs · 19,356 cycles

SEAT TRACK AT BS 834 TO 841, RBL 45, DAMAGED TO CROWN AND CHANNEL. R & R IAW SRM 51- 40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 27,456 hrs · 19,356 cycles

CABIN SEAT TRACK AT STA 834 TO STA 841 LBL 45 HAS SEAT FITTING DAMAGE TO CROWN AND CHANNEL. DAMAGED SEAT TRACK FROM STA 780 TO STA 880, LBL 45 WAS R & R IAW SRM 51-40-02 REV 103 (REFER SNRM N00796). REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

FUSELAGE EXTERIOR SKIN STA 620-640 BETWEEN STRINGER 26R TO 28R HAS NUMEROUS SCRATCHES. REPAIR CARRIED OUT IAW SRM 53-00-01 FIG.201, REPAIR 16, REV.104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SPAR — DAMAGED (ZONE 500) · airframe 27,456 hrs · 19,356 cycles

LT WING REAR SPAR UPPER FITTING FOUND SHIM MIGRATION AT LBL 70.5. REPAIR CARRIED OUT ON LEFT WING REAR SPAR AT LBBL 70.5 AS PER E.A. F- 5740-152567 PT 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP. RT UPPER SILL UPPER INNER FLANGE HAS CORROSION AT ANCHOR NUT, BS 1400-1440. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP LWR SILL, CORROSION FOUND ALONG UPPER SURFACE UNDER TRANSITION PANEL FROM BS 1380-1440. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (BS 1440 S25-26L) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP FRAME UPPER SURFACE HAS DENT AT BS 1440, BETWEEN S25-26L. REPAIRED AS PER EA F-5310-153431 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 1340 S26-27R) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO FRAME UPPER SURFACE HAS CORROSION BS 1340 BETWEEN S26-27R. CORROSION REMOVED AS PER EA F-5310-153433. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (BS 1420 S23-24L) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP FRAME HAS DENT ON UPPER SURFACE AT BS 1420 BETWEEN STRINGERS S-23L- S-24L. REPAIR CARRIED OUT AS PER EA F-5310-153430 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME SPLICE — GOUGED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO COMP FRAME SPLICE PLATE AFT SIDE HAS GOUGE MARK AT STA 1480, BETWEEN STRINGERS S24R AND S25R. DAMAGED FRAME SPLICE AT STA 1480, BETWEEN S-24R AND S-25R. R & R IAW SRM 51-40-02 REV 103. REPAIR IS CLASSIFIED AS MAJOR.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO NR 2 DOOR CUTOUT LWR CHORD HAS CORROSION ON OTBD SIDE JUST AFT OF FWD SUPPORT FITTING AT STA 1386.5. REPAIR CARRIED OUT IAW EA F-5310-152578. REPAIR CLASSIFIED AS MAJOR.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

AFT LWR CARGO, FWD LWR CORNER OF DOOR CUTOUT AT STA 1381.5 HAS CORROSION ON LOCK FASTENER COLLAR 1 EA AND CORROSION ON SURFACE AREA SURROUNDING THE DISCREPANT FASTENER. REPAIR CARRIED OUT IAW EA F-5310-152578. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CRACKED (BS 1580 S3R) · airframe 27,456 hrs · 19,356 cycles

CABIN, AFTER BRACKET REMOVAL FOUND BS 1580 ADJACENT TO S3R CRACK IN FRAME AT FASTENER LOCATION. FRAME R & R IAW SRM 53-00-07, REPAIR 3, FIG 201, REV 103. REPAIR CLASSIFIED AS MAJOR.

Part: BUSHING — DAMAGED (NR 1 NACELLE) · airframe 27,456 hrs · 19,356 cycles

NR 1 PYLON NAC STRUT DIAGONAL BRACE FITTING BUSHINGS FOUND WITH SCORING MARKS DURING PYLON REMOVAL. DAMAGED BUSHINGS REMOVED AND REPLACED IAW SRM 54-50-90 REPAIR 5 FIG.201 REV. 103. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

RT WING OVERWING FILL PORT CUTOUT FOUND CORRODED. REPAIR CARRIED OUT ON RT OVERWING FILL PORT CUTOUT IAW EA F-5730-152583. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

LT WING OVERWING FILL PORT CUTOUT FOUND CORRODED. REPAIR CARRIED OUT ON LT OVERWING FILL PORT CUTOUT IAW EA F-5730-152583. REPAIR CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 27,456 hrs · 19,356 cycles

NR 1 PYLON NAC STRUT UPPER SPAR FITTING AT PPSTA 174.0 FOUND WITH OTBD AND INBD SIDE HORIZONTAL SHIMS MIGRATED OUTWARDS AND AFT DIRECTIONS. R & R IAW EA F-5450-152592. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (ZONE 200) · airframe 27,456 hrs · 19,356 cycles

FRAME AT BS 1280 HAS CHAFE MARKS AT S10R AND 2" BELOW S11R. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG. 201, REV 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 27,456 hrs · 19,356 cycles

NR 2 PYLON NAC STRUT UPPER SPAR FITTING AT PPSTA 174.0 FOUND WITH OTBD SIDE HORIZONTAL SHIMS MIGRATED OUTWARDS. SHIMS REPLACED IAW EA F-5450-152597. REPAIR CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 27,456 hrs · 19,356 cycles

NR 2 PYLON MID BULKHEAD LOWER FLANGE OTBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW EA F-5450-152597. REPAIR CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (ZONE 400) · airframe 27,456 hrs · 19,356 cycles

NR 2 PYLON MID BHEAD LOWER FLANGE INBD AFT SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW EA F-5450-152597. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 27,456 hrs · 19,356 cycles

AFTER REMOVAL OF CABIN FLOORBEAM REPAIR AT STA 720, RBL 45 TO RBL 64, OBSERVED FRAME INNER CHORD AREA WITH DAMAGE ADJACENT S17R. DAMAGED FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (NR 1 NACELLE) · airframe 27,456 hrs · 19,356 cycles

NR 1 PYLON MID-BULKHEAD LOWER FLANGE OTBD FWD AND AFT SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW EA F-5450-152592. REPAIR IS CLASSIFIED AS MAJOR.

Part: SHIM — MIGRATED (NR 1 NACELLE) · airframe 27,456 hrs · 19,356 cycles

NR 1 PYLON MID BULKHEAD LOWER FLANGE INBD FWD AND AFT SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW EA F-5450-152592. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,456 hrs · 19,356 cycles

CABIN DECK PLATE AT STA 1717, RBL 64 TO LBL 64 HAS CORROSION. R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 27,456 hrs · 19,356 cycles

CABIN, SEAT TRACK AT STA 862 TO STA 876 RBL 45, HAS DAMAGE TO CROWN AND CHANNEL. R & R IAW SRM 51-40-02 REV 103. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 27,456 hrs · 19,356 cycles

CABIN, SEAT TRACK AT STA 862 TO STA 876, LBL 45 HAS SEAT FITTING DAMAGE TO CROWN AND CHANNEL. R & R IAW SRM 51-40-02, REV 103 AND EA F-5100-152584. REPAIR IS CLASSIFIED AS MAJOR.