N992FD

Part: LAMP — FAILED (N/A) · airframe 82,010 hrs · 41,606 cycles

PDIS 992 32-60 8410 23DEC21 MEM OPEN U ON APPROACH AFTER GEAR WAS SELECTED DOWN THE NOSE GEAR DOWN LIGHT DID ILLUMINATE. NO GEAR UNSAFE OR OTHER INDICATIONS RECEIVED. EXECUTED A GO AROUND AND DECLARED AN EMERGENCY FOR POTENTIAL GEAR ISSUE. CONTINUED TO A NORMAL LANDING AND TAXIED TO THE GATE. FACT 23DEC21 07:14 MEM UPON DEBRIEF OF CREW MX NOTED THAT THE NOSE GEAR DOWN LOCK GREEN LIGHT ON THE FWD P3 PANEL WAS NOT ILLUMIATED. PERFORMED LIGHT TEST AND LIGHT DID NOT ILLUMINATE. RELAMPED NOSE GEAR DOWN LOCK LIGHT IAW AMM 33-16-02-2 AND LIGHT IMMEDIATELY ILLUMINATED AND RE-PERFORMED LIGHT TEST WITH SATISFACTORY RESULTS. PEFORMED BITE TEST OF PSEU WITH NO FAULTS ON NOSE GEAR DOWN OR NOSE GEAR LOCK SENSORS IAW AMM 32-61-03-2. INSPECTED SECURITY, CONDITION, AND GAPS OF NOSE GEAR DOWN SENSORS S10066 AND S10079, AS WELL AST NOSE GEAR LOCK SENSORS S10065 AND S10078 IAW AMM 32-61-03-2. ALL CHECKS GOOD. A/C OK TO CONTINUE SERIVCE AT THIS TIME.

Part: CIRCUIT CARD — FAILED (CONFIG WARNING) · airframe 81,981 hrs · 41,582 cycles

DURING TAKEOFF AT ABOUT 110KNOTS TAKEOFF, CONFIGURATION WARNING ILLUMINATED. PERFORMED RTO. FLAPS WERE SET TO 5 AND TRIM WAS IN THE GREEN. AIRCRAFT WAS PROPERLY CONFIGURED FOR TAKEOFF. R&R TAKEOFF CONFIG. WARNING CARD IAW MM 31-51-04-4. PERFORMED TAKEOFF CONFIG. WARNING SIGNALS TEST IAW MM 31-51-00-5. ALL TESTS PASSED.

Part: NONE — NONE (N/A) · airframe 81,981 hrs · 41,582 cycles

PERFORMED RTO AT 120 KIAS. CONSULTED QRH BRAKE COOLING CHART WHICH DIRECTED A 57 MINUTE BRAKE COOLING TIME. REF WRI 31-50 8385. PEFORMED HIGH ENERGY STOP INSP, REF AMM 05-51-14-2. ALL BRAKE READING AT TIME OF INSP 3.0 AND DROPPING. NO ABNORMALITIES NOTICED WITH BRAKING SYSTEM. A/C OK FOR SERVICE

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 81,708 hrs · 41,373 cycles

DISBOND INDICATION FOUND ON #4 SLAT, BOTH UPPER AND LOWER SURFACES 20 INCHES FROM INBOARD EDGE AND 6 INCHES BELOW TRAILING EDGE. REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #4 SLAT IAW B757 AMM 27-81-02-4. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (NR 8 SLAT) · airframe 81,708 hrs · 41,373 cycles

DISBOND FOUND 36" INBOARD OF OUTBOARD EDGE, 8" FROM AFT EDGE ON #8 SLAT UPPER SURFACE REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #8 SLAT PER B757 AMM 27-81-02-4

Part: FLOORBOARD — DAMAGED (456-462) · airframe 81,708 hrs · 41,373 cycles

MAIN EQUIPMENT CENTER RH SIDE THRU ACCESS DOOR 119 FLOORBOARD EDGE IS DAMAGED ABOVE THE DOOR LATCH PLATE. FAB NEW PANEL IAW FED EX SRZ -25-005 REV R.

Part: SKIN — CRACKED (L2 DOOR) · airframe 81,708 hrs · 41,373 cycles

L2 INNER SKIN IS CRACKED AT LIGHTENING HOLE FLANGE JUST BELOW UPPER LATCH TORQUE TUBE, APPROXIMATELY STA 716 STR 10LH REMOVED DAMAGE IAW B757-200 SRM 52-10-01-1A, FOUND TO BE WITHIN LIMITS PER DETAIL XI, MATERIAL REMOVED .100" MAXIMUM ALLOWED .100", RESTORED FINISH IAW B757 SRM 51-20-01- 0G

Part: DOOR FRAME — CRACKED (R1 DOOR AREA) · airframe 81,708 hrs · 41,373 cycles

R1 DOOR CUTOUT - FWD UPPER CORNER - INNER FRAME CRACKED ACCOMPLISHED FEDEX EA # F-5310-T036230-P1 : FUSELAGE - MAINFRAME - STUB FRAME STA 330 S-9R, CRACK AND DEFORMATION DAMAGE

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 81,708 hrs · 41,373 cycles

RIGHT WING INBOARD MAIN FLAP LOWER SURFACE HAS AREA OF DELAMINATION REPAIRED RIGHT WING INBOARD MAIN FLAP LOWER SKIN IAW B757 SRM 57-53-01-2R FIG 201 AND 51-70-10- 2R REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 825 LBL 45) · corrosion level 2 · airframe 81,708 hrs · 41,373 cycles

MAIN CABIN STA 825 LBL 45 SEAT TRACK HAS MILD CORROSION REVOVED CORROSION IAW B757 -2 SRM 53-00-52-1A DETAIL I, FOUND TO BE WITHIN LIMITS, MATERIAL REMOVED .017", ORIGINAL .230", REMAINING .213". RESTORED FINISH IAW B757-2 SRM 51-20-01 AND 53-00-52-1A

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 81,708 hrs · 41,373 cycles

L/H WING OTBD FWD FLAP UPPER SURFACE HAS 4EA LOCATIONS OF DELAMINATION APPROX 70 OTBD OF THE INBD EDGE ALL CONTAINED WITHIN APPROX 20" OF EACH OTHER REPAIRED L/H WING O/B FWD FLAP UPPER SURFACE IAW B757-SRM 57-53-01-2R & 51-70-07-0G.

Part: SKIN — DAMAGED (BS 603 S19L) · airframe 81,581 hrs · 41,281 cycles

MAINFRAME - HOLE IN A/C FUSELAGE REPAIR COMPLY WITH E..A. F-5310-T0361682 REV NO. POS. P1 DURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE IMPACT AREA (STA 603.5 AND STRINGER 19L) JUST ABOVE A SKIN SPLICE NEAR THE AFT CORNER OF THE MCD. MINOR REPAIR TO THE FUSELAGE SKIN (EA F-5310-T0361682 PART 1, ERS 21-01979) AS THE REPAIR CONSIST OF A FREEZE PLUG REPAIR WITH SPECIAL CONDITIONS DUE TO THE LOCATION OF THE DAMAGE TO THE LAP JOINT. THIS REPAIR WAS COORDINATED WITH THE STC HOLDER VTMAE AND IS APPROVED BY AN 8110-3. PERMANENT REPAIR TO BE DONE AT C-CHECK

Part: SKIN — DAMAGED (BS 603 S19L) · airframe 81,580 hrs · 41,280 cycles

DURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE IMPACT AREA (STA 603.5 AND STRINGER 19L) JUST ABOVE A SKIN SPLICE NEAR THE AFT CORNER OF THE MCD. MINOR REPAIR TO THE FUSELAGE SKIN AS THE REPAIR CONSIST OF A FREEZE PLUG REPAIR WITH SPECIAL CONDITIONS DUE TO THE LOCATION OF THE DAMAGE TO THE LAP JOINT. THIS REPAIR WAS COORDINATED WITH THE STC HOLDER VTMAE AND IS APPROVED BY AN 8110-3. PERMANENT REPAIR TO BE DONE AT C-CHECK.

Part: SENSOR — FAILED (L1 DOOR) · airframe 80,574 hrs · 40,601 cycles

L FWD ENT DOOR EICAS MSG DISPLAYED IN FLT DURING CRUISE AT FL 360 INTERMITTENTLY THEN EXTINGUISHED ON DECENT. R/R L1 DOOR LOCKED SENSOR S10094 - REF M/M 52-71-00-4. PERFORMED ADJUSTMENT/TEST WITH NO FAULTS - REF M/M 52-71-00-5. NO FAULTS PER PSEU BITE - REF FIM 32-09 FT 803. A/C O.K. FOR SERVICE.

Part: FRAME — CORRODED (BS 700) · airframe 80,347 hrs · 40,446 cycles

FORWARD CARGO COMPARTMENT - CORROSION ON UPPER FLANGE OF FRAME AT BS 700 RBL1 COMPLIED WITH FEDEX EA # F-5310-T0349986 P1. FUSELAGE - MAINFRAME - STA 700 FRAME REPAIR BETWEEN STRINGERS S-28R AND S-28L

Part: FLOOR SUPPORT — CORRODED (BS 665) · corrosion level 2 · airframe 80,347 hrs · 40,446 cycles

FORWARD CARGO COMPARTMENTM CORROSION ON INTERCOSTAL BS 655 RBL 25. REMOVED INTERCOSTAL FWD CARGO COMP BS 655 RBL 25. EVALUATED INTERCOSTAL FOUND OUT OF LIMITS IAW B757 SRM 51-40-02-0G AND 53-00-04-1A FIG 101 DET II. FORMED, TRIMMED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW BOEING PL 143N5367 REV F AND DWG # 143N5353 REV -

Part: SKIN — GOUGED (BS 513) · airframe 80,347 hrs · 40,446 cycles

LOWER FUSELAGE HAD A DENTED AREA AT BS 513, BETWEEN STRINGERS 28L AND 29L. EVALUATED DENTED AREA AND FOUND THE AREA TO HAVE TWO GOUGES IAW IAW SRM 51-10-02-0G, AND BLENDED AREA AND FOUND MINIMUM THICKNESS REMAINING OF SKIN AREA .030. FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 01-1A DET II. CUT OUT AREA OF DAMAGE IAW SRM 53-00-01-2R, FIG 1, DET I, REPAIR 28. FABRICATED A DOUBLER AND FILLER. INSTALLED THE REPAIR IAW SRM 53-00-01-2R, REPAIR 28.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,347 hrs · 40,446 cycles

BOTTOM EXT FUSELAGE SKIN UPPER SURFACE HAS 2 SQUARE INCHES OR CORROSION AND BULGING LOCATED AT THE MAIN E&E BAY DOOR 119BL FWD CUTOUT BETWEEN 2EA STOP FTGS. COMPLIED WITH EA F-5330-T0349870, P1.

Part: SHEAR TIE — CORRODED (BS 1460) · corrosion level 2 · airframe 80,347 hrs · 40,446 cycles

AFT CARGO SHEAR TIE BS 1460 CORRODED. FOUND WITH 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-00-07-1A, FIG 101, DET II, REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 146N1014, REV D.

Part: FLOORBEAM — CRACKED (BS 580) · airframe 80,347 hrs · 40,446 cycles

STUB FLOORBEAM STA. 580 LBL 45.5 CRACK AT AFT INNER RADIUS COMPLIED WITH FEDEX EA # F - 5310-T0349768 P1 , TITLE: STUB FLOOR BEAM STA. 580 LBL 45.5 CRACK AT AFT INNER RADIUS.

Part: FUSE — LEAKING (A/SKID MANIFOLD) · airframe 80,146 hrs · 40,305 cycles

AFTER BLOCK IN. RIGHT HYDRAULIC LEAK. LOST RIGHT HYDRAULIC QUANITY REMOVED AND REPLACED #4 BRAKE NORMAL ANTISKID MANIFOLD BRAKE FUSE REF AMM 32-42-03-4-0. LEAK AND OPS CK GOOD.

Part: TARGET — OUT OF LIMITS (DOOR SENSOR) · airframe 79,667 hrs · 39,974 cycles

L AFT EMERGENCY DOOR EICAS LIGHT. RAN QRH. GOOD PRESSURE, CONTINUED. WITH DOOR CLOSED FOUND GAP BETWEEN SENSOR AND TARGET OUT OF LIMITS. ADJUSTED TARGET IAW AMM 57-71-00-5. OPS CHECKS NORMAL.

Part: COLLAR — NOT REPORTED (L1 DOOR) · airframe 79,598 hrs · 39,920 cycles

L1 DOOR WILL NOT CLOSE, GUST LOCK BUSHING SEIZED UP, POSSIBLE CRACKED OR TOOTH BROKE OFF. REPLACED L1 DOOR HOLD OPEN LOCK COLLAR PER MM 52-11-08-8. OPS CHECK NORMAL. A/C OK FOR SERVICE. P/N REPLACED WAS 654N0244-7, NO SERIAL NUMBER ON PART.

Part: BATTERY PACK — INOPERATIVE (INOPERATIVE) · airframe 79,134 hrs · 39,600 cycles

L1 DOOR INTERIOR EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51-07-2-0.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 79,134 hrs · 39,600 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSY IAW MM 33-51-06-2-1. OPS CHECKED GOOD.

Part: GUST LOCK — OUT OF ADJUST (L1 DOOR) · airframe 79,031 hrs · 39,515 cycles

L1 DOOR HOLD OPEN LOCK IS VERY STIFF TO OPERATE. IAW AMM: 52-11-08-8, ADJUSTED THE L1 DOOR HOLD OPEN LOCK AMM 52-11-08-4-0 AND ALIGNED THE PAX DOOR HOLD OPEN LOCK IAW AMM 52-11-08-8-0. OPS CHECKED NORMAL.

Part: LIGHT — UNKNOWN (EXTERIOR) · airframe 79,024 hrs · 39,508 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. COULD NOT DUPLICATE PROBLEM. PERFORMED EMERGENCY LIGHT TEST AND LIGHT OP'S CHECKED GOOD IAW MM 33-51-00-5.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 79,024 hrs · 39,508 cycles

RESEATED EMERGENCY EXIT SIGN AND PERFORMED EMERGENCY LIGHT TEST AND LIGHT OP'S CHECKED GOOD IAW 757 MM 33-51-00-5.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,859 hrs · 39,385 cycles

ON REMOVAL OF THE SEAT TRACK FROM BS 440 TO 640, RBL 45 FOUND CRACKED. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05-0G AND DWG 143N5080, REV A.

Part: FRAME — CRACKED (BS 1640) · airframe 78,859 hrs · 39,385 cycles

BS 1640 FRAME AT LONGERON 14L IS CRACKED. REPAIRED IAW EA F-5310-T0335764, P1.

Part: CREASE BEAM — CORRODED (BS 370-377) · airframe 78,859 hrs · 39,385 cycles

BS 370 - 377, RBL 64, LOWER SURFACE OF CREASE BEAM INBD ANGLE HAS SIGNS OF CORROSION. REMOVED THE CREASE BEAM IAW SRM 51-10-02. OUTT OF LIMITS IAW SRM 53-30-13-1A. REMOVED THE WEB IAW SRM 51-40-02. FABRICATED A NEW WEB IAW DWG 141N8322, REV K. INSTALLED THE WEB IAW SRM 51-40- 02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 78,859 hrs · 39,385 cycles

STA 231 FRAME HAS A HOLE IN IT. REPAIRED 231 FRAME IAW SRM 53-00-07-2R REP 7. PERFORMED SATISFACTORY OPS CHECK OF DOOR SWITCH IAW AMM 52-71-00-5.

Part: SPRING — FAILED (GIRT BAR) · airframe 78,714 hrs · 39,287 cycles

WHEN CLOSING L1 DOOR, EMERGENCY SLIDE GIRT BAR FELL OUT FOUND LEAF SPRINGS BAD. REMOVED AND REPLACED GIRT BAR ASSY IAW MM 25-66-10-2. DOOR SLIDE ARMS AND DISARMS NORMAL.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 78,611 hrs · 39,214 cycles

AFTER PREFLIGHT WAS COMPLETED, COULD NOT CLOSE L1 DOOR. FOUND GIRT BAR HANGING FROM BOTTOM OF DOOR. REMOVED AND REPLACED THE L1 GIRT BAR ASSY IAW AMM 25-66-10-2. DOOR ARMS & DISARMS GOOD.

Part: COLLAR — DAMAGED (L1 DOOR) · airframe 77,706 hrs · 38,588 cycles

AIRCRAFT L1 DOOR WILL NOT CLOSE. GUST LOCK DOESN’T OPEN, SO DOOR WON’T OPEN. R & R L1 DOOR GUST LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONAL CHECK OF L1 ENTRY DOOR NORMAL, RII PROCEDURES COMPLIED WITH.

Part: ARM — DIRTY (R1 DOOR SLIDE) · airframe 769 hrs · 38,073 cycles

MAIN CABIN R1 EXIT DOOR SLIDE ARM POPPED OUT. INDICATOR INTERMITTENTLY STICKS IN & OUT OF VIEW. FOUND DEBRIS IN UPPER PORTION OF RETRACTABLE DOOR CUT OUT CAUSING INDICATOR NOT TO EXTEND PROPERLY. CLEANED CUT OUT AREA OF DEBRIS & INDICATOR WORKS CORRECTLY.

Part: SWITCH — TRIPPED (LE SLAT) · airframe 76,640 hrs · 37,811 cycles

LE SLAT ASM EICAS MSG WHILE RETRACTING FLAPS DURING TAKEOFF. COMPLIED WITH QRH, LANDED NOTICED NO ROLLING OR CONTROL DIFFICULTY. LT ALTN FLAP & FLAPS AT 20 DEGREES. FOUND UPPER EICAS WITH AMBER LE SLATS ASYM MSG DISPLAYED BUT NO LOWER EICAS OR SELECTED EICAS MSG FAULT. NO FURTHER TIME TO WORK, PREPPING TRANSLOAD ACFT. TROUBLE SHOT IAW FIM. FOUND RT WING OTBD SLAT LOSS SWITCH TRIPPED. RESET SWITCH INSPECTED CABLE, NO DEFECTS NOTED. DID FIND ADEQUATE LUBE ON CABLE RUN. INSPECTED RT INBD SLAT LOSS SWITCH & NO DEFECTS NOTED IT ALSO HAD ADEQUATE LUBE. CYCLED SLATS & FLAPS NUMEROUS TIMES NO FAULTS DETECTED. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: SKIN — DENTED (TE FLAP) · airframe 76,479 hrs · 37,682 cycles

HAIL DAMAGE, LT WING MAIN FLAP UPPER SURFACE INBD SIDE HAS 2 DENTS. ACCOMPLISHED EA F-5750-T0308600 PT1 WINGS, LT WING INBD MAIN FLAP UPPER SKIN REPAIR.

Part: WEDGE — DENTED (LE SLAT) · airframe 76,479 hrs · 37,682 cycles

HAIL DAMAGE NR 4 SLAT TE WEDGE. ACCOMPLISHED EA F-5750-T0308597 PT 1 FLIGHT CONTROL, LE SLATS & FLAPS NR 4 SLAT TE WEDGE REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 76,479 hrs · 37,682 cycles

HAIL DAMAGE LT OTBD FLAP HAS 2 DENTS DELAMINATED. ACCOMPLISHED EA F-5750-T0308601 PT 1, WINGS, LT WING OTBD MAIN FLAP UPPER SKIN REPAIR.

Part: WEDGE — DENTED (LE SLAT) · airframe 76,479 hrs · 37,682 cycles

HAIL DAMAGE NR 2 SLAT TE WEDGE. ACCOMPLISHED EX EA F-5750-T0308596 PT1 FLIGHT CONTROLS, LE SLATS & FLAPS, NR 2 SLAT TE WEDGE REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 76,479 hrs · 37,682 cycles

HAIL DAMAGE LT WING INBD AFT FLAP UPPER SURFACE. COMPLIED WITH EA F-5750-TO308549 SEE COPY ATTACHED LT WING AFT FLAP UPPER SKIN REPAIR RSC.

Part: PANEL — DEFECTIVE (ENTRY DOOR) · airframe 76,460 hrs · 37,673 cycles

RIGHT ENTRY DOOR ARMED SLIDE PLACARD REMAINS IN DISARMED POSITION WHEN SLIDE WAS ARMED. PLACARD HAS TO BE BE MANUALLY MOVED TO THE ARMED POSITION. FOUND ARMED POP OUT INDICATOR RUBBING CUT OUT PANEL, REMOVED EXCESS FROM PANEL. OPERATIONS CHECKED DOOR ARMING & DISARMING IAW AMM 52-11-00-6. OPERATIONS CHECKED GOOD.

Part: WIRE — OPEN (EMERGENCY LIGHTS) · airframe 76,371 hrs · 37,602 cycles

L1 SLIDE EMERGENCY LIGHT INOPERATIVE. FOUND OPEN GROUND WIRE W3532-0001-20. TERMINATED WIRE AT GROUND POINT GD478-DC REF AWD 33-51-12. EMERGENCY LIGHT SYSTEM TESTS NORMAL IAW MM 33-51-00-5.

Part: SIGN — INOPERATIVE (CABIN) · airframe 76,258 hrs · 37,514 cycles

L1 EMERGENCY EXIT LIGHT SIGN INOPERATIVE. RELEASED FOR SERVICE PER MEL 33-51-01-01 CATEGORY D EXPIRATION 4MAY14.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 75,498 hrs · 36,955 cycles

SLIDE ARMED LIGHT FOR L1 DOOR IS INOPERATIVE, RELAMPED L1 "SLIDE" LIGHT. SLIDE LIGHT ILLUMINATES NORMAL, ACFT OK FOR SERVICE.

Part: HANDLE — SEPARATED (PARKING BREAK) · airframe 75,048 hrs · 36,627 cycles

ON COMPLETION OF PUSH BACK, PARKING BRAKE HANDLE CAME OFF, UNABLE TO ENGAGE PARKING BRAKE. RECONNECTED HANDLE BY TIGHTENING SET SCREWS, PERFORMED WORK IAW SMP.

Part: SKIN — MISREPAIRED (BS 1640-1661) · airframe 74,746 hrs · 36,427 cycles

FUSELAGE SKIN REPAIR AT BS 1640-1661, STR 20L, LAP SEAM MISREPAIRED. ACCOMPLISHED IAW-EA F-5330-152637, REF FAA FORM 8100-9, FIRST STAGE APPROVAL, DTA DUE WITHIN 24 MONTHS, "CAT A, MAJOR REPAIR".

Part: GATE — CORRODED (L1 DOOR LOWER) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

L1 DOOR LOWER GATE BOTTOM EDGE IS CORRODED. REMOVED AND REPLACED LOWER GATE ON L1 DOOR, IAW-A.M.M-52-11-38, ADJUSTED DOOR ,IAW-AMM 52-11-00-5, OPS CHECKED GOOD. FOUND TO BE OUT OF LIMITS IAW SRM-52-10-02. CAT.A, MAJOR REPAIR.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 74,746 hrs · 36,427 cycles

CORROSION AT STA 425 STR 30 AT TOILET DUMP VALVE, INSIDE E/E BAY. DOT # 82149.

Part: SKIN — MISREPAIRED (BS 1460-1480) · airframe 74,746 hrs · 36,427 cycles

SKIN REPAIR AT BS 1460-1480 BL 0, REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REPLACED REPAIR IAW EA F-5330-147734, MAJOR REPAIR.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

R-4 DOOR UPPER GATE UPPER EDGE HAS CORROSION. R & R R4 DOOR UPPER GATE ASSY IAW AMM 52-11-38. PERFORMED R4 DOOR ADJUSTMENT CHECK IAW AMM 52-11-00. CHECKED GOOD. ORIGINAL MATERIAL: .200", REMOVED: .050", REMAINING: .150", CORROSION FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL 4. MAJOR REPAIR.

Part: FRAME SPLICE — DAMAGED (ZONE 100) · airframe 74,746 hrs · 36,427 cycles

FWD PIT,BS 760 S-27L, FRAME SPLICE BOTTOM FASTENER MISDRILLED. ACCOMPLISHED REPAIR IAW EA F-5310-147727. MAJOR REPAIR.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

DOOR LOWER GATE BOTTOM EDGE CORRODED. REMOVED CORROSION PER SRM 51-10-02. ORIGINAL MATERIAL: .200", REMOVED: .015", REMAINING: .185", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L2 LOWER GATE ASSY PER AMM 52-11-38, AND DWG 143N6106. ADJUSTMENT/RIG ACCOMPLISHED PER AMM 52-11-00-5. CHECKED GOOD. MAJOR REPAIR.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

DOOR LOWER GATE BOTTOM EDGE FWD AND AFT CORNER ARE CHAFED. REMOVED CORROSION PER SRM 51-10-02. BEFORE: 0200", AFTER: .150", LOSS: .050", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L4 DOOR LWR GATE ASSY PER AMM 52-11-38, AND DWG 146N6106. ADJUSTED/RIGGED GATE ASSY PER AMM 52-11-00-5, CHECKED GOOD. MAJOR REPAIR.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

R2 DOOR LOWER GATE HAS CORROSION ON THE BOTTOM EDGE. FOUND OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4; EXCEEDS .100" FROM EDGE. REMOVED AND REPLACED R2 DOOR LOWER GATE ASSY PER AMM 52-11-38. PERFORMED R2 DOOR ADJUSTMENT CHECK PER AMM 52-11-00-5. ADJUSTMENT CHECKED GOOD. MAJOR REPAIR.

Part: FRAME SPLICE — MISREPAIRED (BS 720) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE REPAIR AT BS 720, S29L- S29R, REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. FRAME SPLICE REPAIR REPLACED IAW EA F-5310-147720. MAJOR REPAIR.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

R1 DOOR LOWER GATE BOTTOM EDGE IS CORRODED. REMOVED CORROSION; ORIGINAL MATERIAL WAS: .200", REMAINING MATERIAL: .170", LOSS: .030". FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL 4. R & R R1 DOOR LOWER GATE ASSY IAW SRM 51-40-02, SRM 52-11-38, AND DWG 141N6220. ADJUSTED LOWER GATE ASSY IAW AMM 52-11-00-825-050. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 400 S14-16L) · airframe 74,746 hrs · 36,427 cycles

FUSELAGE SKIN REPAIR DOUBLER AT STA 400, STR 14L-16L NOT IAW APPROVED DATA. R & R DOUBLER IAW SRM 51-40-02 & SRM 53-00-01. REPAIR 16, FABRICATED NEW DOUBLER.

Part: STRINGER — CORRODED (BS 1462 S29R) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

STRINGER 29R AT BS 1462, CORRODED. REMOVED AND REPLACED CORRODED STRINGER SECTION IAW SRM 53-00-03 REPAIR 2. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (R4 DOOR) · airframe 74,746 hrs · 36,427 cycles

REPAIR DOUBLER ON R-4 SERVICE DOOR SKIN NOT REPAIRED IAW APPROVED DATA. R & R DOUBLER AND FILLER, IAW SRM 52-10-01, REPAIR NR 7, AND SRM 51-40-02. CAT. "B" MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 74,746 hrs · 36,427 cycles

FOUND SCRIBE LINE AT BS 663.438 THROUGH BS 671.750 & S-19L LAP JOINT. COMPLIED WITH EX F-5330-147698, AD2007-19-07, & EO F-5330-7-5000, MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 720 - 781) · airframe 74,746 hrs · 36,427 cycles

FOUND SCRIBE LINE AT BS 759.531 TO BS 765.375, AT S14R LAP JOINT. ACCOMPLISHED EA F-5330-147702, PART 1 ONLY; VERIFICATION OF NO ADDITIONAL SCRIBE LINES AT BUTT JOINT, BS 720 TO BUTT JOINT, BS 781. PART 2 OF EA REQUIRED AT 1,500 FC AFTER PART 1 AND PART 3 OF EA REQUIRED AT 1,500 FC AFTER PART 2. (CAT. "B") MAJOR REPAIR.

Part: SKIN — GOUGED (NR 1 NACELLE) · airframe 74,746 hrs · 36,427 cycles

LT NACELLE STRUT RT SIDE NAC STA 100 FWD FAIRING UNDERNEATH SKIRT PANEL HAS DEEP GOUGE. COMPLIED WITH EA F-5450-147713. MAJOR REPAIR.

Part: SEAT TRACK — OUT OF TOLERANCE (BS 640) · airframe 74,746 hrs · 36,427 cycles

STA 640, RBL 24.75 SEAT TRACK WILL NOT JIG. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52 FIG 201 ITEM 2. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT IAW SRM 51-20-00. INSTALLED SEAT TRACK AND SPLICES AND STRAP IAW SRM 53-00-52 FIG 201. MAJOR REPAIR.

Part: SEAT TRACK — OUT OF ALIGNMENT (BS 640) · airframe 74,746 hrs · 36,427 cycles

STA 640 LBL 24.75 SEAT TRACK WILL NOT JIG. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 610-640, LBL 24.75 IAW SRM 53-00-52, FIG 201, ITEM 2. RECEIVED NEW SEAT TRACK MAT BAC 1502-792 BATCH NR 001904663 IAW SRM 53-00-52, PG 203, FIG 201, SHT 3 OF 5. LOCATED AND DRILLED FASTENER HOLES IAW SRM 51-40-05. APPLIED TOP COAT IAW AMM 51-20-00. INSTALLED NEW SEAT TRACK SECTION BETWEEN STA 610-640, LBL 24.75 AND -3 STRAP AND SPLICES -2 (2EA) IAW SRM 53-00-52, FIG 201, SH 1 OF 5, REPAIR 1. CATEGORY "A" MAJOR REPAIR.

Part: UNKNOWN — CORRODED (BS 750) · airframe 74,746 hrs · 36,427 cycles

FWD CARGO COMPT STA 750, STR 21R EXFOLIATED.

Part: FRAME — MISREPAIRED (BS 1300 S25-26R) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE REPAIR AT STA 1300 STR 25R TO 26R REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APROVED DATA. REMOVED AND REPLACED FRAME IAW SRM-51-40-02, NEW FRAME FABRICATED AND INSTALLED NEW SPLICE ON FRAME IAW SRM-51-40-02. SPLICE FABRICATED. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1460) · airframe 74,746 hrs · 36,427 cycles

AFT CARGO PIT STA 1460, BL0 CORROSION ON FRAME. REMOVED FRAME BS 1460, S24L-S24R AND FOUND TO BE OUT OF LIMITS AT BL0' BEFORE: .063", AFTER: .053", LOSS: .010", AS PER SRM 53-00-07, DETAIL 2, FIG.101. REPLACED FRAME AND SPLICE AS PER SRM 51-40-02. MAJOR REPAIR

Part: FRAME — MISREPAIRED (BS 1340 S24-26R) · airframe 74,746 hrs · 36,427 cycles

FRAME AT STA 1340, STR 24R-26R MISREPAIRED. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-02 AND DWG.146N1042. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1420) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE REPAIR AT STA 1420, STR 24L-26L REQUIRES REPLACEMENT DUE NOT COMPLYING WITH APPROVED DATA. REMOVED FRAME AND PRODUCTION SPLICE PER SRM 51-40-02. FABRICATED FRAME AND SPLICE. INSTALLED NEW FRAME AND SPLICE PER SRM 51-40-02 AND DRAWING 146N1028. MAJOR REPAIR

Part: FRAME — MISREPAIRED (BS 1520) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE AT STA 1520, STR 23L-25L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R SPLICE, AND R & R FRAME, IAW SRM 51-40-02 AND SRM 51-10-02. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1500 S24-27L) · airframe 74,746 hrs · 36,427 cycles

EXISTING FRAME SPLICE REPAIR AT BS 1500, STR 24L-27L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REMOVED AND REPLACED FRAME BS 1500 STR. 24L-24R, AS PER SRM 51-40-02 & DWG 146N1030. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1320 S23-26L) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE REPAIR AT STATION 1320, STR 23L-26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R FRAME, AT STA 1320, STR. 24L TO STR 24R, IAW SRM-51-40-02. NEW FRAME FABRICATED AND INSTALLED. NEW SPLICE IAW-SRM-51-40-02, SPLICE FABRICATED. "CAT A, MAJOR REPAIR".

Part: SKIN — MISREPAIRED (BS 1708-1718) · airframe 74,746 hrs · 36,427 cycles

EXISTING FUSELAGE SKIN EXTERNAL DOUBLER REPAIR AT STA 1710, STR 24L REQUIRES REPLACEMENT DUE TO NOT BEING IN COMPLIANCE WITH KNOWN APPROVED DATA. REMOVED EXISTING DOUBLER, CUT-OUT DAMAGE SKIN AND INSTALLED NEW DOUBLER/ FILLER, BS 1708-1718, S23L-S24L, IAW SRM 51-40-02 AND SRM 53-00-01, REPAIR NR 15. ZONE "A" CAT "B" MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1440 S24-29L) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE REPAIR AT STA 1440, STR 23L-26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. REMOVED AND REPLACED FRAME AND SPLICE, BS 1440, S29R - S24L, PER SRM 51-40-02, AND DRAWING 146N1028.

Part: FRAME — MISREPAIRED (BS 1480) · airframe 74,746 hrs · 36,427 cycles

FRAME SPLICE AT STA 1480, STR 23L- 26L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R FRAME STA 1480 FROM STR.24L-24R IAW SRM-51-40-02, AND SPLICE. "CAT A, MAJOR REPAIR".

Part: FRAME — CRACKED (RT NACELLE) · airframe 74,746 hrs · 36,427 cycles

RT ENG PYLON OTBD SIDE STA 193 FRAME CRACKED. REMOVED SUPPORT CLAMPS 4 EA HYDR LINES 3 EA TO BE FOM IAW AMM 20-10-09. FABRICATED NEW SUPPORT ANGLE FRAME ON TRAVELER. LOCATED AND DRILLED NEW SUPPORT ANGLE AND INSTALLED IAW SRM SRM 51-40-05 AND 51-40-02 INSTALLED HYD LINES 3 EA AND SUPPORT CLAMPS IAW AMM 20-10-09. LEAK CHECK ACCOMPLISHED ON CARD EF-2910-7-5004, STEP 8 (D).

Part: CREASE BEAM — GOUGED (ZONE 200) · airframe 74,746 hrs · 36,427 cycles

RT CREASE BEAM INBD CHORD, STA 1180-1400 GOUGED AT AND AROUND NUMEROUS FASTENER HOLES EVALUATED DAMAGES ON CREASEBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, FIG 101, SH 3, DETAIL 2 ( L= .5 W=.1 D=.015) ORIG .080 DAMAGED AREA .065 REMOVED CREASEBEAM RT 1180-1400 IAW SRM 51-40-02 FABRICATED NEW CREASEBEAM PN BAC1515-3553-24, BATCH 0001896249, INSTALLED NEW CREASEBEAM RT 1180-1400 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 100) · airframe 74,746 hrs · 36,427 cycles

RIGHT SIDE WALL ANGLE BS 740, S24-27R CORRODED.

Part: SUPPORT ANGLE — CORRODED (BS 650-750) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

L-2 DOOR SILL DRAIN PAN SUPPORT ANGLE HAS CORROSION APPROX BETWEEN STA 680 TO 730. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS; L=4", W=2", D=.071, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-13, FIG 101, DETAIL 2. REMOVED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1711 S15R) · airframe 74,746 hrs · 36,427 cycles

BS 1711 S15R HAS A DENT IN SKIN. REMOVED DAMAGED SKIN IAW SRM 53-00-01, FABRICATED DOUBLER IAW SRM 53-00-01, TABLE I. REPAIR 16. HFEC CHECK CUT-OUT, HOLES IAW NDTM 51-00-19, NO CRACKS NOTED. INSTALLED DOUBLER IAW SRM 51-40-02, CATEGORY "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1681) · airframe 74,746 hrs · 36,427 cycles

EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STA 1681, STR 2L-3L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R REPAIR DOUBLER IAW SRM 53-00-01, REPAIR NR 15, MAJOR REPAIR, CAT "B", AT BS 1681, S2L- S3L.

Part: ATTACH ANGLE — GOUGED (ZONE 100) · airframe 74,746 hrs · 36,427 cycles

FWD PIT RT SIDE WALL ATTACH ANGLE AT FRAME 640 S25R- S26R CORRODED AND GOUGED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF SIDE WALL ANGLE AT FS 640 S25R-S26R. MATERIAL THICKNESS .050 REMOVED MAT .015 REMANING MAT .035 FOUND TO BE OUT OF LIMITS IAW 53-00-53, FIG 101, DETAIL 5 FABRICATED NEW ANGLE ON TRAVLER TII/ 882795. INSTALLED NEW ANGLE AT FS 640 S25R -S26R IAW SRM 51-40-02.

Part: SKIN — MISREPAIRED (BS 1700-1720) · airframe 74,746 hrs · 36,427 cycles

EXISTING EXTERNAL FUSELAGE REPAIR AT STA 1700-1720, STR 16L REQUIRES REPLACEMENT DUE TO NOT COMPLING WITH APPROVED DATA. REMOVED AND REPLACED DOUBLER PER SRM 53-00-01, REPAIR 15. MAJOR REPAIR, CAT. "B" .

Part: SEAT TRACK — GOUGED (BS 1180-1320) · airframe 74,746 hrs · 36,427 cycles

RBL 45, SEAT TRACK, DIRTY AND GOUGED AT NUMEROUS SPOTS STA 1180 TO 1320. REMOVED CORROSION AND GOUGES IAW SRM 51-10-02 CHECKED LIMITS OF SEAT TRACK AT RBL 45, FS 1180-FS 1320 MATERIAL THICKNESS .230 REMOVED MAT .051 REMAINING MAT .179, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 74,746 hrs · 36,427 cycles

DENT STA 1700 S23R RT SIDE SKIN. FOUND OUT OF LIMITS IAW SRM 53-00-01, PG 101, DET III. CUT-OUT DAMAGED SKIN. INSTALLED DOUBLER, FILLER IAW SRM 51-40-02 AND SRM 53-00-01 ZONE A,CAT B REPAIR. MAJOR REPAIR.

Part: FLOORBEAM — NONE (ZONE 200) · airframe 74,746 hrs · 36,427 cycles

FLOORBEAM STA 680 REQUIRES REPLACEMENT DUE TO INCOMING REPAIRS THAT WILL INTERFERE WITH SEAT TRACK INSTALL. REMOVED FLOORBEAM STA 680 IAW SRM 51-40-02. REMOVED BRACKETS STA 680 RBL 17-62 (4EA) AND LBL 24-62 (2EA) PER SRM 51-40-02. RECEIVED EXTRUSION PN BAC 1518-338/18A. BATCH 1944014 AND FABRICATED NEW FLOORBEAM IAW SRM 53-30-51. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED, PRIMED AND TOP COATED IAW SRM 51-20-01 AND AMM 51-21-00. PART MARKED PN FX-143N5013 IAW GMM 7-0-1001. INSTALLED BRACKETS STA 680, RBL 17-62 AND LBL 24-62 IAW SRM 51-40-02. INSTALLED FLOORBEAM PN FX-143N5013 IAW SRM 51-40-02 AT STA 680 RBL 70 TO LBL 70. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 760-785) · airframe 74,746 hrs · 36,427 cycles

MAIN DECK SEAT TRACK HAS NUMEROUS GOUGES AT RBL 24 BETWEEN BS 760 TO BS 785. REMOVED GOUGE IAW SRM 51-10-02 MEASURED OUT OF LIMITS ORIGINAL .300 REM .250 LOSS .050 DETAIL 1 FIG 101 PAGE 103 IAW SRM 53-00-52. FABRICATED SEAT TRACK IAW SRM 53-30-52. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 . MAJOR REPAIR.

Part: SKIN — DENTED (BS 519-530) · airframe 74,746 hrs · 36,427 cycles

DENT ON SKIN STA 521, STR 24R. REMOVED DAMAGE AND FOUND OUT OF LIMITS PER SRM 53-00-01, DETAIL 3, FIG.101. FABRICATED DOUBLER AND FILLER AS PER SRM 53-00-01, TABLE 1, P.203, FIG.201, REPAIR 15. HFEC CHECKED CUTOUT AND HOLES WITH NO CRACKS NOTED. INSTALLED DOUBLER AND FILLER AS PER SRM 53-00-01, REPAIR 15 AND SRM 51-40-02. CAT. "B" MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 1620-1670) · airframe 74,746 hrs · 36,427 cycles

CHECKED LIMITS AND FOUND STRINGER CRACKED, OUT OF LIMITS IAW SRM 53-00-03, REPAIR 2, PG 102, FIG 101, DETAIL 1. R & R STRINGER IAW SRM 53-00-03, REPAIR 2. MAJOR REPAIR

Part: SEAT TRACK — WORN (BS 1090-1110) · airframe 74,746 hrs · 36,427 cycles

MAIN CABIN SEAT TRACK BS 1090-1110 RBL 25 IS WORN. BLENDED WORN AREA WITH .032". REMOVED FROM TOP SURFACE. MAX ALLOWED IS .020". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, SH 2, P 102. R & R SEAT TRACK IAW SRM 51-40-02, 51-20-01, 51-40-05, AND GMM 7-0-1001-1. MAJOR REPAIR.

Part: FIREWALL — GOUGED (APU BAY) · airframe 74,746 hrs · 36,427 cycles

APU COMPARTMENT, FWD FIREWALL HAS GOUGES, 8" FROM BOTTOM EDGE OF WALL. FOUND GOUGE TO BE .003" DEEP, DETERMINED TO BE OUT OF LIMIT IAW SRM 53-80-01, FIG 101 DET IX PG 109, REPAIRED DAMAGE PER SRM 53-80-08, FIG 201, SHEET 1 PG 201. MAJOR REPAIR.

Part: FIREWALL — CHAFED (APU BAY) · airframe 74,746 hrs · 36,427 cycles

APU COMPARTMENT FWD FIRE WALL HAS CHAFING MARKS 20" FROM BOTTOM EDGE OF COMPARTMENT. CHAFE MARK FOUND TO .004" DEEP, DETERMINED TO BE OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL IX PG 109. REPAIRED DAMAGE IAW SRM 53-80-08, FIG 201, SHEET 1, PG 201, STA 1885, LBL-14". MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1140) · airframe 74,746 hrs · 36,427 cycles

MAIN DECK STA 1140, RBL 45 SEAT TRACK CORRODED.

Part: SEAT TRACK — GOUGED (BS 1170) · airframe 74,746 hrs · 36,427 cycles

MAIN CABIN COMPARTMENT STA 1170, LBL 45 SEAT TRACK GOUGED. R & R SEAT TRACK IAW SRM 51-40-01, 51-40-02, AND 51-40-05. MAJOR REPAIR.

Part: FLOORBEAM — GOUGED (BS 1600) · airframe 74,746 hrs · 36,427 cycles

FLOORBEAM AT STA 1600 HAS NUMEROUS GOUGES BETWEEN RBL 60 TO LBL 60. REMOVED AND REPLACED FLOORBEAM, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51 FIG.101 DETAIL 3. LOCATED AND DRILLED FASTENER HOLES IN NEW FLOORBEAM PER SRM 51-40-02. APPLIED TOP COAT PER SRM 51-20-01. PART MARKED PER GMM 7-0-1001 AND INSTALLED PER SRM 53-00-51, FIG.1, SHEET 5OF 8, AND SRM 51-40-02. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1120) · airframe 74,746 hrs · 36,427 cycles

MAIN CABIN STA 1120, LBL 25 SEAT TRACK CORRODED. BLENDED AREAS OF CORROSION WITH MATERIAL LOSS OF .070. CLEAN UP MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R SEAT TRACK IAW SRM 51-10-02, 51-40-02, 51-40-05.

Part: SEAT TRACK — CORRODED (BS 1155) · airframe 74,746 hrs · 36,427 cycles

MAIN DECK STA 1155, RBL 45 SEAT TRACK CORRODED. REMOVED CORROSION WITH .070" MATERIAL LOSS. MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R TRACK IAW SRM 51-40-01, 51-40-05, 51-40- 02. MAJOR REPAIR.

Part: FLOORBEAM — GOUGED (BS 1200) · airframe 74,746 hrs · 36,427 cycles

STA 1200, FLOORBEAM UPPER FLANGE GOUGED BL 0 TO LBL 64. FOUND OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REPAIRED FLOORBEAM AT STA 1200 LBL 19.5 IAW SRM 53-00-51 DETAIL 1, AND REPAIR 3. BLENDED GOUGES; L=2.5, W=1.0, D=.002, ORIGINAL MATERIAL WAS .125, FOUND TO BE WITHIN LIMITS PER SRM 53- 00-51, FIG.101, DETAIL 3. MAJOR REPAIR

Part: FLOORBEAM — DAMAGED (BS 480) · airframe 74,746 hrs · 36,427 cycles

MAIN DECK FLOORBEAM UPPER TEE FITTING HAS 2 EA. ELONGATED FASTENER HOLES AT STA 480 BETWEEN RBL 45 TO RBL 63. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG.101. REMOVED AND INSTALLED ANGLES, BS 480, RBL 50, PER SRM 51-40-02, FOR ACCESS. REMOVED DAMAGED TEE FITTING, FABRICATED REPAIR ANGLES. INSTALLED NEW TEE FITTING PER SRM 53- 00-51, FIG.201, AND SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 900) · airframe 74,746 hrs · 36,427 cycles

MAIN CABIN STA 900 RBL 45 SEAT TRACK CORRODED. BLENDED CORROSION . ORIGINAL MATERIAL .230, MATERIAL REMOVED .050. MATERIAL REMAINING .180 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101. R & R SEAT TRACK AT STA 900, RBL 45 IAW SRM 51-40-02, PG 8. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1400) · airframe 74,746 hrs · 36,427 cycles

AFT CARGO FRAME BS 1400 HAS CORROSION UNDER DOOR SILL AREA. CORROSION FOUND OUT OF LIMITS IAW 53-00-07, PG 104, FIG 101, DET V, RECEIVED NEW FRAME & SPLICE. R & R FRAME IAW SRM 51-40-02 & DWG 146N1028. MAJOR REPAIR.

Part: SEAT TRACK — BROKEN (BS 1200) · airframe 74,746 hrs · 36,427 cycles

LBL 24 SEAT TRACK SCALLOP BROKEN AT BS 1200. TRANSFERED FROM N00741, REMOVED SEAT TRACK FS 1180-1320 LBL 24 IAW SRM 51-40-02, FABBED NEW SEAT TRACK FROM BAC1520- 792, BATCH 1904663, LOCATED AND DRILLED IAW SRM 51-10-02 AND 51-10-55, TREATED, PRIMED AND TOP COATED IAW SRM 51-20-01, INSTALLED NEW SEAT TRACK FS 1180- 1320 LBL 24 IAW SRM 51-40-02, DAMAGE ON SEAT TRACK WAS OUT OF LIMITS IAW SRM 53-00-52. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 460) · airframe 74,746 hrs · 36,427 cycles

MAIN DECK FLOORBEAM UPPER T-CHORD HAS 2 EA ELONGATED FASTENER HOLES BETWEEN RBL 45 AND RBL 63 AT STA 460. FOUND TO BE OUT OF LIMITS .250 MAX DIA. AFTER .310 IAW SRM 53-00-51 FIG 101. REPAIRED FLOORBEAM AT STA 460 RBL 33- 63 IAW SRM 53-00-51 FIG 201. CAT- A, REPAIR 5. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 760-879) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

CABIN SEAT TRACK STA 760-879 LBL 24, CORRODED. REMOVED AND REPLACED SEAT TRACK AT STA 760 - 879 LBL 24 IAW SRM 51-40-02 P/N BAC1520-792 BATCH 1904663, FABRICATED WITH SEAT TRACK WAS FOUND OUT OF LIMITS IAW 53-00-52 FIG 101 DETAIL I. ORG MATERIAL .188 AFTER REWORK .150. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 877) · airframe 74,746 hrs · 36,427 cycles

MAIN CABIN SEAT TRACK CROWN HAS GOUGE AT STA 877 RBL 45 REMOVED AND REPLACED SEAT TRACK STA 760- 879 RBL 45 IAW 51-10-02, PN BAC1520-792, BATCH 1904663. SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1; ORIGINAL MATERIAL .145", AFTER REWORK .080", LOSS .065". MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 74,746 hrs · 36,427 cycles

STA. 365, FLOORBEAM CORRODED BL-0 - 24L. REMOVED CORROSION AT STA 365 LBL 6 ORGINAL MAT .125 MATERIAL REMOVED .060 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. FABERICATED FLOORBEAM IAW SRM 53-10-51 FIG 101 DETAIL II PART MARKED IAW GMM 7-0-1001. INSTALLED FLOORBEAM AT STA 365 IAW SRM 51-40-02 THIS IS A CATEGORY "A" MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 345) · airframe 74,746 hrs · 36,427 cycles

FLOOR BEAM AT STA. 345, LBL10 CORRODED. REMOVED; .040", FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, DETAIL 3. REMOVED FLOORBEAM PER SRM 51-40-02. FABRICATED NEW FLOORBEAM PER SRM 53-10-51 & INSTALLED PER SRM 51-40-02. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,746 hrs · 36,427 cycles

STA. 377 FLOORBEAM CORRODED BL 24 - 45 L. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL III. ORIG. MAT. .125 AFTER REWORK .107 MAT. LOSS EXCEED MAX. ALLOWED. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-10-51 FIG. 1 DETAIL II. INSTALLED FLOORBEAM IAW SRM 51-40-02.