N908FD

ATA 5753

Part: SKIN — DAMAGED (TE FLAP) · airframe 51,202 hrs · 20,978 cycles

PREVIOUS REPAIR INSTALLED REPAIR REQUIRES REPLACEMENT, REPAIR INDENTIFIED AT RT WING OB AFT FLAP LWR SURFACE 40" FROM IB EDGE REMOVED DAMAGE ON RT WING OB AFT FLAP LWR SURFACE AT WS 397-459. CLEANED AND PREPED AREA, FABRICATED REPAIR PN 04-009-0022 BATCH NR 0001698127, BONDED PLIES, SEALED AND PRIMED AREA, AND REPAIRED AREA IAW SRM 51-70-05. MAJOR REPAIR.

ATA 5753

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,202 hrs · 20,978 cycles

PREVIOUSLY INSTALLED REPAIR REQUIRES REPLACEMENT. REPAIR IDENTIFIED AT RT WING, OTBD AFT FLAP, LWR SURFACE, 103" FROM INBD EDGE. REPAIRED AREA IAW SRM 51-70-05. REMOVED DAMAGE, CLEANED AND PREPPED AREA FOR REPAIR. FABRICATED REPAIR PLIES, BONDED REPAIR PLIES, SEALED AND PRIMED IAW SRM 51- 70-05. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

ATA 5510

Part: ATTACH ANGLE — BENT (HORIZONTAL STAB) · airframe 51,202 hrs · 20,978 cycles

LT HORZ STAB PANEL 332CL NUTPLATE ATTACH ANGLE BENT CUT OUT DAMAGE, FABRICATED FILLER, RADIUS FILLERS AND REPAIR ANGLES. IAW EA F-5510-131542. INSTALLED REPAIR PARTS IAW EA F-5510-131542. COMPLIED WITH EA F-5510-131542 DATED 11/23/2009.

ATA 5320

Part: FLOOR SUPPORT — MISALIGNED (ZONE 200) · airframe 51,202 hrs · 20,978 cycles

EXISTING FLOORBEAM REPAIR AT STA 700, LBL 55, TO LBL 65, WILL INTERFERE WITH INSTALLATION OF SECTION 43, SEAT TRACK 657N3332-3, AT LBL-58, STA 660, TO STA 884. REPAIR AT STA 700, LBL 55, TO LBL 65, WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSIONS ON MAE MOD W/C 118350502B22R02, AND MAE EA NR 757-5335-16-F2232, REV B, DATED 09/11/09, THIS N/R IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.

ATA 5754

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 51,202 hrs · 20,978 cycles

LT WING, NR5 L/E SLAT, T/E WEDGE, OTBD END, IS DELAMINATED. REPAIRED LT WING, NR 5 L/E SLAT, IAW SRM 57-43-02; BONDED DOUBLER REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — FAILED (ZONE 200) · airframe 51,202 hrs · 20,978 cycles

2 EA EXISTING HOLES IN THE FLOORBEAM UPPER CHORD AT STA 680 RBL 58 ARE ELONGATED AT BS 680 RBL 58 FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE MOD W/C 118350441BZ2R03 AND MAE EA# 757-5335-16-F2306.

ATA 5315

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 51,202 hrs · 20,978 cycles

2EA EXISTING HOLES IN THE FLOORBEAM UPPER CHORD AT STA 780 RBL 58 ARE ELONGATED AT BS 780 RBL 58 FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE W/C 118350441BZ2R03 AND MAE EA# 757-5335-16-F2306 REV - DATED SEPT 30, 2009.

ATA 5315

Part: FLOORBEAM — NONE (ZONE 200) · airframe 51,202 hrs · 20,978 cycles

EXISTING FLOORBEAM REPAIR INTERFERES WITH INSTALLATION OF DWG FASTENERS, AT F STA 740, RBL 58 AT STA 740, RBL 58 FLOORBEAM REPAIR ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118350441BZR03, AND MAE EA 757-5335-16-F2266 REV B, DATED 11/SEP/09 THIS NON-ROUTINE, FOR TRACKING PURPOSES ONLY, THIS IS A MAJOR ALTERATION

ATA 5340

Part: ATTACH ANGLE — FAILED (ZONE 100) · airframe 51,202 hrs · 20,978 cycles

EXISTING DUCT AND ALL ATTACHING ANGLES, CLIPS AND SSEMBLIES INTERFERE WITH INSTALLAATION OF E 7 RACK AT STA 1640-1681 STR. 26L-28L. AT STA. 1640 -1681 STR. 26L-28L- ASSEMBLIES WERE RELOCATED AND ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C 118150084AL2R03 AND MAE EA 757-5362-F2267 REV. A DATED SEPT. 14, 2009 THIS N/R IS TRACKING PURPOSES ONLY , (MAJOR ALTERATION).

ATA 5315

Part: FLOORBEAM — MISREPAIRED (ZONE 200) · airframe 51,202 hrs · 20,978 cycles

EXISTING FLOORBEAM UPPER CHORD REPAIR AT STA 740, LBL 58 WILL INTERFERE WITH INSTALLATION OF SECTION 43 SEAT TRACK NR 657N3332-2. REPAIR AT STA 740, LBL 58 WAS ACCOMPLSHED EFFECTING PTF CONVERSION ON MAE-MOD W/C 118350502BZR02 AND MAE EA 757-5365-16-F2265 REV. D, DATED ON 09/11/09 THIS N/R IS FOR TRACKING PURPOSES ONLY (MAJOR ALTERATION).

ATA 5310

Part: CREASE BEAM — MISALIGNED (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

DURING INSTALLATION OF INNER CREASE BEAM CHORD AT STA 640, 2 EA EXISTING HOLES WERE FOUND THAT CANNOT BE PICKED UP. COMPLIED WITH EA 757-5331-16-F2284 AT STA 640, LBL 58, ON MAE WORK CARD 118350403BZ2R01. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. (MAJOR REPAIR)

ATA 5347

Part: SEAT TRACK — CORRODED (BS 700-740) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN DECK AT STA 700 TO 740 LBL 45 SEAT TRACK CORRODED. REMOVED CORROSION AT STA 700 TO 740 LBL 45.50 IAW SRM 51-10-2. FOUND OUT OF LIMIT IAW SRM 53-00-52 DETAIL I, REMOVED SEAT TRACK AND FABED A NEW SEAT TRACK USING MAT PN BAC1520-792 BATCH NR 0001544831 IAW SRM 51-10-02 AND 53-30-52. LOCATED AND DRILLED IAW SRM 51-10-02, APPLIED SUPERFICIAL TREATMENT IAW SRM 51-20-01. INSTALLED SEAT TRACK IAW SRM 51-40-02. (MAJOR REPAIR)

ATA 5100

Part: NONE — NONE (NONE) · airframe 51,198 hrs · 20,976 cycles

ACFT DOES NOT MATCH DWG 657N3160 FIG E, SHT 2 , REV D AT STA 1640, LBL 60 -62. DWG SHOWS 4 EA EXISTING FASTENERS BUT THE ACFT HAS 5 EA AT STA 1640; LBL 60 - 62. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399EZ2R02, AND MAE EA 757-5362-16-F2250, REV- DATED 08/18/2009. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. (MAJOR ALTERATION)

ATA 5100

Part: NONE — NONE (NONE) · airframe 51,198 hrs · 20,976 cycles

ACFT DOES NOT MATCH DWG NR 657N3160 FIG. E , SHT 2, REV D AT STA 1640, RBL 60 - 62. DWG SHOWS 4 EA EXISTING FASTENERS, BUT THE ACFT HAS 5 EA AT STA: 1640; RBL 60 - 62 WAS REPAIRED IAW EA 757-5362-16-F2251, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C NR 118350400EZ2R02. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. (MAJOR ALTERATION)

ATA 5100

Part: STRUCTURE — UNKNOWN (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

UPPER CORD AT BL-0;900 -1080 HAS AN EXISTING FASTENER BREAKING OUT ON EDGE OF CHORD AT STA 925. IF THIS HOLE IS PICKED-UP IN THE NEW CHORD PN 111N5207-10 WE WILL DUPLICATE THE PROBLEM. AT STA 925, BL-0 , EA 757-5345-16-F2226, WAS COMPLIED WITH AND ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350451CZ2R04 AND MAE EA 757-5345-16-F2226, REV - DATED AUG 03, 2009. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. (MAJOR ALTERATION)

ATA 5100

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

SEAT TRACK 657N3318-7 AT LBL 24.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 LBL 24, PREVIOUSLY INSTALLED REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. NEW REPAIR WAS ACCOMPLISHED AT STA 1280, DURING PTF CONVERSION ON MAE MOD W/O 4230072, MAE MOD W/C 118350419E22, AND MAE EA 757-5365-16-F2275. REV 09/09/09. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY AND CLASSIFIED A. (MAJOR ALTERATION.)

ATA 5347

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

EXITING SEAT TRACK AT STA 1540-1640 HAS A 1.0 INCH CRACK AT STA 1640 ON INB OF SEAT TRACK AND CROWN AT RBL 45. REMOVED SEAT TRACK STA 1540-1640 BL 45, FABRICATED NEW SEAT TRACK FROM BAC 1520- 792 BATCH NR 00015411987, LOCATED AND DRILLED HOLES, TREATED, PRIMED AND INSTALLED NEW SEAT TRACK STA 1540-1640, RBL 45 IAW SRM 51-10-02, THIS IS A MAJOR REPAIR NO FOLOW-UP INSP REQUIRED.

ATA 5330

Part: SKIN — DAMAGED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

APPROX STA 437, BETWEEN STR'S 17 AND 18 LT 1 EA EXISTING FASTENER HOLE IN ACFT SKIN IS AT A 0.256 DIA AT STA 437, BETWEEN STR'S 17 AND 18 LT, A REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION, ON MAE WC NR 118250073ASSR03, AND MAE EA NR 757-5311-16-F 2225, REV-, DATED 08/03/09, THIS NR IS FOR TRACKING PURPOSES ONLY. ( MAJOR ALTERATION)

ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

INTERCOSTAL CRACKED. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T9/800306. (MAJOR REPAIR)

ATA 5100

Part: SEAT TRACK — NONE (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

SEAT TRACK 657N3318-7 AT LBL 45.5, STA 1280 - 1320 CAN NOT BE LOCATED AND DRILLED DUE TO ACFT CONFIGURATION NOT MATCHING UP TO DWG AT STA 1280 - 1320, SEAT TRACK REPAIR WAS ACCOMPLISHED, DUE TO WRONG CONFIGURATION EFFECTING THE PTF CONVERTION, ON MAE W/C NR 118350420E22R01 ON MAE EA NR 757-5365-16-F2271, REV 09/04/09. (MAYOR ALTERATION)

ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

LWR EXT FUSE STA 645 ABOVE STR 18R SKIN DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-01 FIG.1. REMOVED DAMAGED SKIN AT STA 645; STR 18R IAW SRM 53-00-01, FIG 201, TABLE 1. PERFORMED HFEC IAW NTM 51-00-19 PT 6 ON CUT OUT AREA. NO CRACK INDICATION NOTED. FABRICATED REPAIR DOUBLER IAW SRM 53-00- 01, FIG 201, TABLE 1 MATERIAL ID 2024-T3. 100C BATCH NR 0001551385. LOCATED AND DRILLED REPAIR DOUBLER IAW SRM 51-10-02. TREATED AND PRIMED DOUBLER IAW SRM 51-20-01. INSTALLED NEW REPAIR DOUBLER AT STA 645; STR 18R IAW SRM 51-40-02. CAT "B" REPAIR WITH SUPLEMENTAL INSP. INITIAL INSP 37.500 F/C, REPEAT EVERY 6.000 F/C METHOD HFEC IAW NDT MANUAL 51-00-01 PT 6. (MAJOR REPAIR)

ATA 5311

Part: FRAME — DAMAGED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

AFT CARGO COMPT FRAME 1480 UPPER FLANGE HAS A DENT AT S-25L. REMOVED DAMAGED AREA AND ORIGINAL SPLICE FOR REPAIR IAW SRM 51-40-2; NDT NO CRACK NOTED; FABED NEW SPLICE ON MAE TRAVELER NR T9/800805; LOCATED AND DRILLED IAW SRM 51-40-5; REMOVED STRINGER FOR ACCESS; FABED NEW STRINGER CLIP ON MAE TRAVELER NR T9/801724; LOCATED AND DRILLED IAW SRM 51-40-5; TREATED AND PRIMED REPAIR SPLICE AND NEW STRINGER CLIP IAW SRM 51-20-01; INSTALLED REPAIR AND NEW STRINGER CLIP IAW SRM 51-40-2. (MAJOR REPAIR)

ATA 5311

Part: FRAME — DENTED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

AFT CARGO COMP, STA 1540, STR 26R ATTACH FRAME HAS DENT. FOUND OUT OF LIMITS IAW 53-00-07. CUT OUT DAMAGE IAW SRM 53-00-07. REMOVED CLIP IAW SRM 51-40-02. RECEIVED REPAIR FABED ON TRAVELER NR T9/801702. RECEIVED CLIP IAW TRAVELER NR T9/801701. LOCATED AND DRILLED HOLES ON REPAIR AND CLIP IAW SRM 51-40-05. INSTALLED SUPPORT IAW SRM 53-00-07 REPAIR 5 DETAIL II INSTALLED REPAIR AND CLIP AT STA 1540, STRG 26R IAW SRM 53-00-07 REPAIR 5 DETAIL II.( MAJOR REPAIR)

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN DECK AT STA 765, RBL 45 SEAT TRACK CORRODED. REMOVED SEAT TRACK FROM RBL 45 STA 640 TO 780 IAW SRM 51-40-2. FURTHER INVESTIGATION WEB FROM 700-720 IS CRACKED, REMOVED WEB AT RBL 45, STA 700- 720. FABRICATED AND INSTALLED NEW WEB ON NR N00602; FABRICATED NEW SEAT TRACK, LOCATED, DRILLED AND INSTALLED IAW SRM 52-40-2 ON STA 765, RBL-45. (MAJOR REPAIR).

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN CABIN FLOORBEAM STA 740, LBL 45 TO LBL 62, HAS AREAS OF CORROSION REMOVED FLOORBEAM SEC, FABRICATED A NEW WITH MATERIAL PN 7075-T6- .071C, FABED ANGLES ON MAE TRAVELER NR T9/800801,TR NR T9/800802, INSTALLED ALL REPAIR PARTS STA 740, LBL 45 TO LBL 62. REPAIR NR 3, CAT A. (MAYOR ALTERATION)

ATA 5311

Part: FRAME — DAMAGED (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

MCD CIRCUMFERENTIAL FRAME AT STA 1620, BETWEEN S2L AND S5L, HAS TOO MANY HOLES. REMOVED FRAME SECTION, FABED NEW FRAME ON MAE TRAV NR T9/800999, INSTALLED NEW FRAME SECTION AND REPAIR PARTS AT STA 1620, STR 5R TO 5L, IAW SRM 53-00-07, 51-40-02. CATEGORY "A", MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,198 hrs · 20,976 cycles

MAIN DECK AT STA 865, LBL24 SEAT TRACK WORN/GOUGED. FABRICATED NEW SEAT TRACK PN 60-6549/24 BATCH NR 1511787. LOCATED AND DRILLED IAW SRM 51-40-05. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND SRM 51-20-05.

ATA 5311

Part: FRAME SPLICE — DENTED (ZONE 100) · airframe 51,198 hrs · 20,976 cycles

AFT CARGO COMPT. FRAME 1340 UPPER FLANGE HAS A DENT AT S-25L REMOVED DAMAGED AREA, FABRICATED NEW SPLICE BY MAE TRAVELER NR T9/800920, LOCATED AND DRILLED HOLES, IAW SRM 53-00-07, TREATED AND PRIMED IAW SRM 51-20-01 AND INSTALLED NEW SPLICE IAW SRM 53-00-07 REPAIR 1, THIS A MAJOR REPAIR WITH NO FOLLOW-UP INSPECTIONS REQUIRED.

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN DECK FLOORBEAM AT STA 740, RBL 45 TO 58, UPPER CAP CORRODED. REMOVED SECTION, FABED STRAPS MAT-7075-T6-.063C, AND FABED ANGLES MAE TRAV NR T9/800804, T9/800803, IAW SRM 51-40-02. INSTALLED FLOORBEAM STRAPS AND ANGLES, ALL REPAIR PARTS, AT STA 740, FLOORBEAM , RBL 45-62 IAW SRM 53-00-51. CATEGORY "A", MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

BS 395 RBL 58 FLOOR BEAM CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED UPPER CHORD, FABRICATED NEW CHORD FROM BAC1505- 100617 BATCH 1611790. FABRICATED STRAPS AND ANGLES ON MAE TRAVELER T9/801278 AND T9/801277. INSTALLED REPAIR PARTS IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR CATAGORY 3.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN DECK FLOORBEAM UPPER CAP CORRODED AT STA. 366, BL0 TO RBL24. REMOVED DAMAGED SECTION FOUND TO BE OUT OF LIMITS, FABRICATED TEE CHORD, REPAIR ANGLES AND STRAPS. INSTALLED REPAIR PARTS AT STA 365, LBL 74 -RBL 34 IAW 53-00-51 FIG 201 REPAIR 3, CATEGORY A, MAJOR REPAIR..

ATA 5347

Part: SEAT TRACK — GOUGED (BS 780-879) · airframe 51,198 hrs · 20,976 cycles

MAIN DECK AT STA 865, RBL 45, SEAT TRACK WORN / GOUGE. REMOVED SEAT TRACK , FABRICATED NEW SEAT TRACK FROM MAT- BAC1520-792, IAW SRM 51-10-02. INSTALLED SEAT TRACK STA 780- 879, RBL 45", IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (BS 695) · corrosion level 2 · airframe 51,198 hrs · 20,976 cycles

MAIN DECK FLOOR SUPPORT WEB AT STA 695 LBL 58 CORRODED. REMOVED CORROSION IAW SRM 51-30-02. ORIGINAL MATERIAL THICKNESS IS .056 AFTER REWORK WAS .053 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-04 FIG 101 DETAIL II. REPAIR CLASSIFIED AS MINOR.