N782FD

Part: SLIDE — DETACHED (R2 DOOR) · airframe 75,524 hrs · 28,955 cycles

WITH THE R2 DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRD BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R&R R1 DOOR SLIDE IAW B757 AMM 25-66-01-4.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 75,513 hrs · 28,945 cycles

WITH THE R2 (UPDATED TO REFLECT R1) DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRT BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R & R DOOR ESCAPE SLIDE IAW AMM 25-66-01-4, ASSIST BOTTLE NEEDS REPLACED AND DOOR COVER ALSO DAMAGED WITH LEFT HAND HINGE PULLED OUT. SLIDE COVER WILL BE PLACED BEHIND BARRIER WALL WITH COVER PER MEL. R&R DOOR BOTTLE IAW B757 AMM 52-11-30-4 OK FOR SERVICE, R&R R1 DOOR SLIDE IAW B757 AMM 25-66-01-4. COMPLETED AMM STEPS UP TO I. (2) DOOR COVER HAS DAMAGE AND NEEDS REPAIR OR REPLACEMENT. PART INFO AS FOLLOWS 757 EVACUATION SLIDE ASSEMBLY AIR CRUISERS CO. P/N D31038-201FX S/N 1013.

Part: ADC — FAILED (COCKPIT) · airframe 75,111 hrs · 28,660 cycles

PDIS 782 34-11 4300 23FEB21 MDT FACT U LOG PAGES: 2980148 FO AIR DATA INSTRUMENTS WENT BLANK DURING TO ROLL. R/I 23FEB21 05:38 MDT U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 4040800-912 POS: 2 SRL: 90032121 TAG NBR: 6852G2 ON MPN: 4040800-912 CPN: 3414864 SRL: 90022096 TAG NBR: 5627C1 FACT 23FEB21 05:38 MDT U FOUND RIGHT AIR DATA COMPUTER FAULTED, REMOVED AND REPLACED RIGHT ADC REF AMM 34-12-01-4. ACCOMPLISHED TEST 30 REF AMM 22-10-00-5. NO CURRENT FAULTS NOTED AT THIS TIME. OPS CHECK GOOD.

Part: SPRING — BROKEN (LT MLG) · airframe 75,031 hrs · 28,607 cycles

LT GEAR SPRING RETAINER ASSEMBLY BROKEN AT THE START OF LT GEAR OPERATION CHECK. SDR ENTERED IN ERROR AGAINST WRONG TAIL NUMBER.

Part: INTERCOSTAL — DAMAGED (BS 1420-1440) · airframe 74,612 hrs · 28,334 cycles

FUSELAGE SKIN BULGE FROM BS 1420 TO BS 1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , B757 SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCOSTAL TO BE ELONGATED IAW SRM 53-00-04-1A, FIG 101, DETAIL I.

Part: INTERCOSTAL — DAMAGED (BS 1420-1440) · airframe 74,612 hrs · 28,334 cycles

FUSELAGE SKIN BULGED FROM BS 1420 TO 1440, AT INTERCOSTAL BETWEEN STRINGERS 28R AND 29R. REMOVED, FABRICATED, AND INSTALLED THE NEW INTERCOSTAL IAW DWG 146N5398, REV P, A , DWG 146N5425 REV -, AND SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCOSTAL TO BE ELONGATED IAW SRM 53-00-04-1A, FIG 101, DETAIL I. NO BULGE CONDITIONS EXHIST.

Part: INTERCOSTAL — UNKNOWN (BS 1420-1440) · airframe 74,612 hrs · 28,334 cycles

FUSELAGE SKIN BULGE FROM BS1420 TO BS1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCOSTAL TO BE ELONGATED IAW SRM 53-00-04-1A, FIG 101, DETAIL I. NO BULGE CONDITIONS EXHIST.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 73,850 hrs · 27,831 cycles

RAMP REPORTED SMALL PUNCTURE IN FLOOR OF AFT CARGO COMPARTMENT. HOLE IS LOCATED AT APPROX STA 1372 RT SIDE APPROX 8 INCHES FWD OF LOWER AFT CARGO DOOR OPENING. COMPLIED WITH EA F-5321-T0349330 PT1. PATCH III INSTALLED OVER PUNCTURE.

Part: CIRCUIT CARD — FAILED (MLG) · airframe 73,682 hrs · 27,714 cycles

INTERMITTENT GEAR NOT DOWN WARNING FOR DURATION OF FLIGHT UNTIL GEAR EXTENDED SHGN 11JUN19 16:26 MEM U PERFORMED BITE PROCEDURE FOR PSEU PER 757 FIM 32_09 F/T_802 NO FAULTS STORED. PERFORMED PSEU GROUND TEST FOR SYS #1 AND SYS #2 LDG GEAR SYSTEMS ; BOTH TESTS PASSED WITH NO FAULTS DETECTED. ITEM REQIRES FURTHER TROUBLESHOOTING. SHGN 11JUN19 17:01 MEM U TROUBLESHOT PER 757 FIM 31-51 F/T 817 BOX 1-6; ACCOMPLISHED BITE CHECK OF LEFT RAD ALT IAW AMM 34-33-00-5. BITE CHECK GOOD. ACCOMPLISHED BITE CHECK OF EGPWS IAW AMM 34-46-98-5. NO CURRENT FAULTS OR FAULT HISTORY DATA LOGGED IN EGPWS. FACT 11JUN19 21:38 MEM U TROUBLESHOT PER 757 FIM 31-51 FAULT TREE 817. PER FIM SYSTEM TEST OK. PERFORMED OPERATIONAL TEST OF RADIO ALTIMETER SYSTEM IAW AMM 34-33-00-5, TEST PASSED. PERFORMED BITE CHECK AND TEST OF ALL 3 FSEU'S AS PER AMM 27-51-01-2-0. NO FAULTS FOUND AND TEST PASSED. AS PRECAUTION, REMOVED AND REPLACED (M983) LANDING CONFIGURATION WARNING MODULE AS PER AMM 31-51-04-4 AND PERFORMED LANDING CONFIGURATION WARNING MODULE TEST PER AMM 31-51-04-4. OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,957 hrs · 27,183 cycles

DENT ON OUTER FUSELAGE SKIN BETWEEN STA 420 & STA 440 BETWEEN S-17L & S-18L. MEASURED, CUT OUT AND REPAIRED DENTED AREA ON FUSELAGE SKIN IAW SRM 5-40-02-0G, SRM 51-40-05-0G AND SRM 53-00-00-01-2R REPAIR 16.

Part: FRAME — CORRODED (BS 1400) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO BAY, BS 1400 STRINGERS 29R - 29L FRAME WEB CORRODED, BOTH FRONT AND AFT SURFACE. FRAME REMOVED AND REPLACED IAW DWG 146N1011 SHT 3 REV E. FRAME FABRICATED IAW DWG 146N1028 SHT 8 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO BAY, BS 1460-1480 CARGO DOOR LOWER SILL WEB CORROSION. SILL WEB R&R WITH NEW FABRICATED STA 1460-1480 CARGO DOOR SILL LOWER SILL WEB IAW DWG 146N8522, SHT 7, REV C. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522-42, SHT 7, REV C. REPAIR CLASSIFIED AS MAJOR.

Part: DOME NUT — CORRODED (L1 DOOR) · airframe 71,362 hrs · 26,122 cycles

CABIN L1 DOOR INTERNAL UPPER WEB, 03 EA DOME NUTS FOUND CORRODED.

Part: SKIN — CHAFED (RT WING) · airframe 71,362 hrs · 26,122 cycles

RT WING, UPPER INTERSPAR SKIN, UPPER SURFACE FOUND CHAFE MARK AT WBL 76-78, 20" LONG FROM SKIN T/E, WING TO BODY FAIRING MATING AREA. MINOR CHAFE MARK BLEND OUT ON 112N3101-12, AFT MACHINED SKIN AT APPROX WBL 76.00 TO 78.00. TRACE FROM REAR SPAR TO STRINGER 7. REPAIR CLASSIFIED AS MAJOR

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, STA 1480, STR 27R-26R, FRAME WEB CORROSION FOUND AFTER ATTACHED ANGLE REMOVED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

AFT CARGO BAY BS 1460 STRINGER 30 STRINGER SPLICE HAS CORROSION. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW DWG 146N3400 SHT 2 REV C. STRINGER SPLICE FABRICATED IAW DWG 146N3820 SHT 01 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, BS 1520, STR 22R-STR 23R. FRAME WEB HAS GOUGE MARKS.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, STA 1618, STR 21L, STRINGER HAS CORROSION. STRINGER REMOVED AND REPAIR IAW SRM 51-40-02 AND SRM 53-00-03, REPAIR 2, REV 118. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

FUSELAGE RT SIDE, THERE IS A LIGHTNING STRIKE AT BS 680 - BS 700 BETWEEN STR 24- STR 25. LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 101, DETAIL II, REV 118. REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 118. THIS IS A CAT B REPAIR. THRESHOLD 29000 F/C FROM TIME OF REPAIR, REQUIRE LFEC REPEAT INSPECTION AT 3000 F/C REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, BS 1460, STR 26R-28L, FRAME WEB CORROSION. R & R WITH NEW FABRICATED FRAME WEB IAW DWG 146N1014, SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT STATION 1510 - 1530, STRINGER 29R, STRINGER CORROSION. CORROSION OUT OF LIMITS, R & R WITH NEW STR STA 1460-STA 1620, STR 29R IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F IN REF TO JOB CARD N02233 IAW WORK DETAIL ATTACHED. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT STATION 1460 - 1480, STRINGER 29R, STRINGER CORROSION. AFT CARGO COMPARTMENT OUT OF LIMIT, STR STA 1460-STA 1620, STR 29R. R & R WITH NEW STR STA 1460-STA 1620 IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

FUSELAGE RIGHT SIDE THERE IS A LIGHTNING STRIKE AT BS 500 - 520 BETWEEN STRINGER 25 - 26 WITH STICKER 633. LIGHTNING STRIKE MARK REMOVED AREA FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX, AD REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 7, REV 118. THIS REPAIR IS CATEGORY B. REPAIR AND INSPECTION THRESHOLD IS 24000 FLIGHT CYCLES AND REPEAT INTERVAL 12000 FLIGHT CYCLES BY USING HIGH FREQUENCY EDDY CURRENT METHOD. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

FUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 480 - 500, BETWEEN STRINGER 25 - 26 WITH STICKER 630. FUSELAGE EXTERIOR SKIN AT BS 480-500, STR 25R-26R LIGHTING STRIKE MARK. REMOVED AREA, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-00, FIG 201, REPAIR 7, REV 118. THIS REPAIR IS CATEGORY B REPAIR AND INSPECTION THRESHOLD 24000 FLIGHT CYCLE AND REPEAT INTERVAL 12000 FLIGHT CYCLES BY USING HIGH FREQUENCY EDDY CURRENT METHOD. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

FUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 460 - 480, BETWEEN STRINGER 25 - 26 WITH STICKER 613. REMOVED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 7, REV 118. THIS REPAIR IS CATEGORY B, REPAIR AND INSPECTION THRESHOLD IS 24,000 FLIGHT CYCLES AND REPEAT INTERVAL 12,000 FLIGHT CYCLES BY USING HIGH FREQUENCY EDDY CURRENT. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT STATION 1560, STRINGER 30 - 29L, FRAME WEB CORROSION.

Part: SKIN — CHAFED (TE FLAP) · airframe 71,362 hrs · 26,122 cycles

RIGHT WING OTBD TE MAIN FLAP, NOSE SKIN FOUND CHAFE MARK AT 2.5" FROM OTBD EDGE.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD CHANNEL, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CHANNEL REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD CHANNEL FABRICATED IAW DWG 146N5317, SHT 1, REV AND INSTALLED IAW DWG 146N5300, SHT 23, REV K. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD ANGLE, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CABIN, STA 1720, LBL 65-RBL 65 DECK PLATE ATTACHED CHORD ANGLE WITH ELONGATED HOLE REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD ANGLE INSTALLED IAW DWG 146N5300, SHT 44, REV AND 146N5300, SHT 23, REV K. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, STATION 1460, STRINGER 28L, STRINGER SPLICE HAS CORROSION. R & R WITH NEW FABRICATED STA 1460, STR 28L, STRINGER SPLICE IAW DWG 146N3400, SHT 02, REV C. NEW STRINGER FABRICATED IAW DWG 146N3820, SHT 01, REV C.

Part: FRAME SPLICE — GOUGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

AFT CARGO COMPARTMENT, STATION 1520, STRINGER 24R, FRAME SPLICE HAS GOUGE MARKS. FRAME SPLICE REMOVED AND REWORKED AREA TREATED IAW SRM 51-10-02 AND SRM 51-20-01, REV 118. MATERIAL REMOVED 0.027" OUT OF LIMIT. FRAME SPLICE R & R WITH NEW FABRICATED FRAME SPLICE, STA 1520, STR 24R IAW DWG 146N1017, SHT 03, REV D. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1681, RBL 10 - 47, FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVAL. CABIN, STA 1681, RBL 10-47 FLOORBEAM UPPER FLANGE CORROSION REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA ORIGINAL THICKNESS 0.158" MATERIAL THICKNESS. REMAINING 0.119" AND MATERIAL THICKNESS REMOVED 0.039" FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-51-1A, REV 117. FLOORBEAM FABRICATED IAW SRM DWG 146N5111, SHT 1, REV B AND INSTALLED IAW DWG 146N5091, SHT II, REV-146N5300, SHT 23, REV K AND 146N8712, SHT 2, REV K. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

EMPANNAGE, LEFT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP FOUND CORROSION LT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP. REMOVED AND NEW PIVOT STRAP FABRICATED IAW DWG NR:182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601 SHT, REV C. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

EMPENNAGE, RT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP. FOUND CORROSION RT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP REMOVED AND NEW PIVOT FABRICATED IAW DWG NR: 182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

LEFT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRICATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

RIGHT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRCIATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1621, STRINGER 13L INTERCOSTAL WEB FOUND CORROSION. INTERCOSTAL WEB CORROSION REMOVED IAW SRM 51-12-02 REV 117. FOUND 50% MATERIAL LOSS. INTERCOSTAL WEB R & R WITH FABRICATED WEB IAW SRM 51-40-02 REV 117 & DWG 146N8734 SHT 1 REV C. INTERCOSTAL WEB FABRICATED IAW 146N8734 SHT 1 REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: PAN — CHAFED (L1 DOOR) · airframe 71,362 hrs · 26,122 cycles

CABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 117. FOUND EXCEEDS LIMIT IAW SRM 52-10-01-1A REV 117. HANDLE PAN REMOVED IAW SRM 51-40-02 REV 117 & REPLACED IAW DWG 141N6100 SHT 8 REV K & SHT 14 REV F. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DECK PLATE — CORRODED (BS 1681) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

BS 1681 LBL 10 - 17 DECK PLATE UPPER SURFACE FOUND CORRODED. COMPLIED WITH EA F-5310-T0325421 PART 1 P1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1550 - 1570, LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEAN UP DEPTH ON THE LIP OF SEAT TRACK CROWN 0.040" AFTER REMOVAL THE MAXIMUM DIAMETER BETWEEN THE LIPS 0.504" EXCEED THE MAXIMUM LIMIT 0.48" IAW SRM 53-00-52-1A, REV 117. SEAT TRACK REMOVED BETWEEN STA 1540-1600 LBL 24.75 REMOVED IAW SRM 51-40-02, REV 117. NEW SEAT TRACK FABRICATED IAW DWG 146N5137, SHT 2, REV AND INSTALLED IAW DWG 146N5120, SHT 30, REV. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1440, RBL 19, FLOORBEAM UPPER FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-51-2R FIG 201 REPAIR 5 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1316, RBL 45.5, SEAT TRACK OTBD FLANGE HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 OPTION 1 REV 117. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1475, LBL 24.75, SEAT TRACK INBD FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 REPAIR 1 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 1590, RBL 45.5 SEAT TRACK INBD FLANGE CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEANED UP DEPTH OF 0.021" MATERIAL ORIGINAL, THICKNESS 0.080" AND REMAINING THICKNESS 0.059" FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-52-1A, REV 117. SEAT TRACK REMOVED BETWEEN STA 1540- STA 1600, RBL 45.5 IAW SRM 51-40-02, REV 117. NEW SEAT TRACK FABRICATED IAW DWG 146N5137, SHT 2, REV AND INSTALLED IAW DWG 146N5120, SHT 30, REV. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

CABIN 1360 - 1380 RT CREASE BEAM WEB UPPER SURFACE FOUND CORROSION. CORROSION, REMOVED IAW SRM 51-10-02, REV 117. MATERIAL REMOVED 0.010" FOUND EXCEED LIMIT IAW SRM 53-60-13-1A, REV 117. CORRODED CREASEBEAM WEB. R & R IAW SRM 51-40-02, REV 117 & DWG 146N5590, SHT 8, REV B. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 940 - 960 RT CREASE BEAM WEB FOUND CORROSION. R & R IAW SRM 51-40-02 REV 117 & DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 71,362 hrs · 26,122 cycles

CABIN STATION 680 - 698, RBL 24.75, SEAT TRACK SUPPORT FOUND CRACK & CORROSION. COMPLIED WITH EA F-5310-T0325422A PART: 1, P1 TITLE: FUSELAGE, MAINFRAME SEAT TRACK SUPPORT INSTALLATION, BETWEEN STA 640 AND STA 700, RBL 24.75. REPAIR CLASSIFIED AS MAJOR.