N904FD

ATA 5313

Part: STRINGER SPLICE — DAMAGED (BS 667 S7L) · airframe 53,423 hrs · 21,903 cycles

SHORT EDGE MARGIN IN THE 657N3250-18 STRINGER SPLICE AT BS 667, S7L CONDITION COMMON TO THE 657N3250-18 STRINGER SPLICE WAS DETERMINED TO BE ACCEPTABLE TO ENGINEERING IAW MAE EA 757-5331-16-F2599 AND MAE PTF W/C NR 118250277DSSR07, REF EA F-5310-139198 AND FORM 8110-3, DATED 06/25/2010, FOR FIRST STAGE APPROVAL/DTE PENDING, NOT TO EXCEED 12 MONTHS FROM DATE OF 8110-3. MAJOR ALTERATION.

ATA 5311

Part: FRAME — DAMAGED (BS 480 S26-27L) · airframe 53,423 hrs · 21,903 cycles

POTENTIAL SHORT EDGE MARGIN FOUND ON FRAME AT BS 480, BETWEEN S26L / 27L. AT BS 480, S26L / 27L, FRAME ALTERATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C 118250068DSSR07 AND MAE EA 757-5332-16-F2619, REV NEW, DATED 04/07/2010. THIS N/R IS FOR TRACKING PURPOSES ONLY REF EA F-5310-141164 AND FORM 8110-3, DATED 06/26/2010 - FIRST STAGE APPROVAL/ DTE PENDING, NOT TO EXCEED 12 MONTHS FROM DATE OF 8110-3. MAJOR ALTERATION.

ATA 5311

Part: FRAME — DAMAGED (BS 1645) · airframe 53,423 hrs · 21,903 cycles

UNABLE TO TRIM THE FRAME AT BS 1645, LBL 63.125 - EXISTING REPAIR DOUBLER WILL INTERFERE WITH PTF MOD. AT BS 1645, LBL 62.125, WL 208, FRAME ALTERATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118350399EZ2R02, AND MAE EA 757-5362-16-F2644, REV. NEW, DATED 04/15/2010. THIS N/R IS FOR TRACKING PURPOSES ONLY REF EA F-5310-139201 AND FORM 8110-3, DATED 06/26/2010 - FIRST STAGE APPROVAL/ DTE PENDING, NOT TO EXCEED 12 MONTHS FROM DATE OF 8110-3. -MAJOR ALTERATION.

ATA 5320

Part: BRACKET — MISALIGNED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

STA 365, LBL 20-24 CABLE PULLEY BRACKET THAT NEEDS TO SHIMMED DUE TO EXISTING FLOORBEAM REPAIR AT STA 365, LBL 20-24 CABLE PULLEY BRACKET REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE W/C NR 118350472RCBR10 AND MAE EA 757-5315-16-F2645, REV- DATED APRIL 20, 201. THIS N/R IS FOR TIME TRACKING PURPOSES ONLY REF EA F-5310-141161 FIRST STAGE APPROVAL/DTA PENDING AND 8110-3 DATED JUNE 25,2010, MINOR ALTERATION.

ATA 5315

Part: FLOORBEAM — DAMAGED (BS 680) · airframe 53,423 hrs · 21,903 cycles

ELONGATED HOLES IN FLOORBEAM WEB AT STA 680 LBL 24.75 AT STA 680 LBL 24.75 FLOORBEAM WEB REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE MOD W/C 118350497BZ2R04 AND MAE EA NR 757-5335-16-F2674 REV - DATED MAY 11, 2010. THIS N/R IS FOR TRACKING PURPOSES ONLY. REF FED EX EA F-5310-139197 FIRST STAGE APPROVED/DTA PENDING AND 8110-3 DATED JUNE 26,2010.

ATA 5330

Part: SKIN — MISINSTALLED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

MCD-STA 460 BETWEEN S-1 AND S-2L AND S-3L AND S-4L FASTNERS IN (2) AREAS ARE FOUND TO BE MISLOCATED DEVIATION TO SKIN FASTNER PATTERN AT STA 460 FROM S-1 TO S-4L WAS DETERMINED TO BE STRUCTURALLY ACCEPTABLE IAW NON CONFORMITY/REJECTION REPORT MAE/AIDC/118, PAGE 1/5. THIS N/R IS FOR TIME TRACKING PURPOSES ONLY REF EA F-5330-141161, FIRST STAGE APPROVAL/DTA PENDING AND 8110-3 DATED JULY 1, 2010.

ATA 5320

Part: FILLER — MISALIGNED (BS 460) · airframe 53,423 hrs · 21,903 cycles

POTENTIAL BREAK OUT CONDITION ON 143N5407-11 AND 143N5407-16 FILLERS LOCATED AT STA 460, LT SIDE, WL 208.1 AT STA 460 LT SIDE, WL 208.1 POTENTIAL BREAK OUT CONDITION REPAIR WAS ACCOMPLISHED DUE TO DISCREPENCY EFFECTING THE P TO F CONVERSION ON MAE MOD W/C 118350464AZ2R07 AND MAE EA 757-5331-16-F2654, REV - DATED APRIL 23,2010. THIS N/R IS FOR TIME TRACKING PURPOSES ONLY. REF EA F-5310-139196, FIRST STAGE APPROVAL/DTA PENDING AND 8110-3 DATED JUNE 26, 2010. MAJOR ALTERATION.

ATA 5340

Part: FITTING — MISINSTALLED (BS 460) · airframe 53,423 hrs · 21,903 cycles

POTENTIAL SHORT EDGE MARGIN CONDITIONS ON 657N4320-4 FITTING AT BS 460, LBL 62.50. AT BS 460, LBL 62.50, POTENTIAL SHORT EDGE MARGIN CONDITION WAS REWORKED REPAIRED ON MAE PTF W/C 118350028BZ2R04 AND MAE EA 757-5335-16-F2611, REV NEW, DATED 04/01/2010 AND FORM 8110-3, DATED 06/25/2010. EA F-5310-141158 FOR FOLLOW UP DTA. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION

ATA 5330

Part: SKIN — DENTED (BS 1661) · airframe 53,423 hrs · 21,903 cycles

EXTENAL SKIN DENTED AT R-4 DOOR BELOW SCUFFPLATE AT BS 1661,S18R. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL 3, DUE TO PROXIMITY TO SHEAR TIE AT BS 1661, S18R. ACCOMPLISHED DENT REPAIR IAW EA F-5330-139159, DATED 06/03/2010, AND FORM 8110-3, 06/25/2010. DTA PENDING NOT TO EXCEED 12 MONTHS FROM DATE OF 8110-3. MAJOR REPAIR.

ATA 5415

Part: FITTING — MISALIGNED (ZONE 400) · airframe 53,423 hrs · 21,903 cycles

EO F-5450-7-5003, PT 3, FIG 8, PANEL 3, STEP 4, STATES TO REMOVED CODE I, 0.0374-0.375 IN FASTENER FROM L/E SUPPORT FITTING AREA, INCOMING FASTENER. REMOVED IS 0.437-0.438 IN DIA ACCOMPLISHED EA F-5450-131188, CLASSIFIED AS MAJOR REPAIR.

ATA 5415

Part: FITTING — MISALIGNED (ZONE 400) · airframe 53,423 hrs · 21,903 cycles

NR 2 PYLON MID BULKHEAD FWD RT BOLT HOLE MEASURES 0.4021 UPON REMOVAL OF EXISTING FASTNER. EO F-5450-7-5005 P2 WORK STEP 1.9 CALLS OUT A MAXIMUM REAM OF 0.3901- 0.3911 AND INSTALLATION OF 1/64 OVER SIZE FASTNER. ACCOMPLISHED EA NR F-5450-131189, CLASSIFIED AS MAJOR REPAIR.

ATA 5411

Part: SPAR — DAMAGED (NR 2 PYLON) · airframe 53,423 hrs · 21,903 cycles

DURING REMOVAL OF NR2 PYLON OTBD SKIN 1EA NUTPLATE HOLE IN LOWER SPAR IN THE PRECOOLER CUTOUT AREA FOUND ELONGATED COMPLIED WITH EA F-5450-139153 "NACELLES/PYLONS - ELONGATED HOLE IN PYLON LOWER SPAR" DATED 05/21/10. CONSIDERED "MAJOR REPAIR" IAW EA MAJOR REPAIR.

ATA 5311

Part: FRAME — DAMAGED (BS 418 S1-2L) · airframe 53,423 hrs · 21,903 cycles

FRAME AT STA 418, BETWEEN STR. 1 AND 2L HAS HOLES THAT WERE DISCOVERED TO BE OUT OF LIMITS WHEN PARTS WERE REMOVED ASSOCIATED WITH THE TV MONITOR BRACKET MOD. REPAIR ACCOMPLISHED PER EA 757-5332-16-F2660, REV A. CLASSIFED MAJOR REPAIR.

ATA 5311

Part: FRAME — DAMAGED (BS 395 S2L) · airframe 53,423 hrs · 21,903 cycles

TV MONITOR SUPPORT BRACKET MOUNT HOLE ON FRAME AT STA 395 STR 2L ELONGATED. REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON ST AEROSPACE MOBILE NR 43269370001 AND EA 757-5332-16-F2660. CLASSIFIED MAJOR REPAIR.

ATA 5310

Part: SPLICE — DAMAGED (BS 700) · airframe 53,423 hrs · 21,903 cycles

BS 700, LBL 45, AFTER INSTALLING SEAT TRACK ALIGNMENT TOOL, EXISTING FASTENER HOLE IN SEAT TRACK AND FLOORBEAM DO NOT ALIGN. AT BS 700, LBL 45, AN ALTERATION WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 118350496BZ2R02 AND STAM EA 757-5335-16-F2684, REV NEW, DATED 05/19/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. -MAJOR ALTERATION -

ATA 5310

Part: SPLICE — DAMAGED (BS 700) · airframe 53,423 hrs · 21,903 cycles

BS 700, LBL 45.5, FITTING PN 140N2504U1, IF DRILLED, A VARIETY OF FASTENERS WILL LAND IN RADIUS OF FITTING, ON HORZ. AND VERT FLANGES AT BS 700, LBL 45.5, AN ALTERATION WAD ACCOMPLISHED, DUE TO THE DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 118350496BZ2R02, AND STAM EA 757-5335-16-F2684, REV NEW, DATED 05/19/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. -MAJOR ALTERATION-

ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS1180-1290) · corrosion level 2 · airframe 53,423 hrs · 21,903 cycles

FS 1261, STR 17 LT HAS CORROSION ON FLOOR CUSP ANGLE. (NOTE: CREASE BEAM CHORD) REMOVED CORROSION FROM CUSP ANGLE AT LBL-17, LBL 60, STA 1261 IAW SRM 51-10-02. CHECKED LIMITS; ORIG MAT =0.071, MAT LOSS =0.015; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 102 DETAIL VIII. REMOVED CUSP FROM STA 1180 TO 1290,S17L, LBL-60 IAW SRM 51-40-02. FABBED NEW CUSP ANGLE FROM 'PN BAC1515-553, 7075-T6511 IAW SRM 53-60-13 FIG 1, DETAIL III. LOCATED AND DRILLED NEW CUSP ANGLE. IAW SRM 51-40-05. TRENTED AND PRIMMED NEW CUSP ANGLE IAW SRM 51-20-01. INSTALLED NEW CUSP ANGLE, FILLERS' AND NUTPLATES IAW SRM 51-40-02 AT BS 1180-1290, S17L, LBL 60.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,423 hrs · 21,903 cycles

FRAME AT BS 1380, S26L-S27L, IS EXFOLIATED. (IN-PROCESS; REMOVING FRAME, AWP 146N8511-34 AND AWE).

ATA 5311

Part: FRAME — DAMAGED (BS 1600) · airframe 53,423 hrs · 21,903 cycles

FRAME AT BS 1600, S26L, IS DAMAGED. (IN-PROCESS; AWF FOR REPAIR PARTS) DAMAGED FRAME STA 1600 STR 26L FOUND OUT OF LIMITS IAW SRM 53-00-07 PG-103 FIG. 101 DET. II. ORIG. MAT. .063" MAT. REMAIN .053" MAT. LOSS .010" L=1.0" W=2.0" FABBRICATED & INSTALLED J-SECTION W/TRAVELER T10/835210 IAW SRM 53-00-07 PG 204 FIG 201 DET I & SRM 51-40-20. CAT. "B" REPAIR WITH SUPPLEMENTAL INSPECTION REQUIREMENTS. LINITIAL 50,000 F/C, REPEAT EVERY 12,000 F/C, METHOD-HFEC PER 575 NDT MANNAL 51-00-01 PT6. MAJOR REPAIR

ATA 5320

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 53,423 hrs · 21,903 cycles

NR 2 CARGO DOOR LOWER SILL HAS CORRODED NUT PLATES. (IN-PROCESS; REMOVING T-CHORD, AWP)

ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 53,423 hrs · 21,903 cycles

FUSELAGE SKIN DENT, 2EA, AT BS 330, 2" BELOW S22R, ARE OUT OF LIMITS. (IN-PROCESS: REPAIR IS REQUIRED) EVALUATED UPPER DENT IAW SRM 53-00-01, FIG 101,DETAIL 3 AND FOUND TO BE W/I LIMITS ; A=.742",Y=.011",A/Y=67.45. EVALUATED LOWER DENT IAW SRM 53-00-01, FIG 101, DETAIL 3 AND FOUND TO BE OUT OF LIMITS DUE TO BEING LOCATED COMMON TO THE STRINGER. REPAIRED LOWER DENT IAW SRM 53-00-01, FIG 201,REPAIR NR 2 AT BS 330, S22R. CAT. "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING; INITIAL INSP AT 37,500 FC, THEREAFTER EVERY 6,000 FC (HFEC).

ATA 5310

Part: CREASE BEAM — CORRODED (BS 665-775) · corrosion level 2 · airframe 53,423 hrs · 21,903 cycles

INBD CREASEBEAM CHORD CORRODED AT BS 665-755, RBL 58. REMOVED CORROSION ON INBD CHORD, R2 DOOR, BS 665-775, RBL 58, IAW SRM 51-10-02. BLENDED AREA .015", MAX ALLOWED .008"; FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL 2/6. REMOVED INBD CHORD IAW SRM 51-40-02. LOCATED AND DRILLED NEW INBD CHORD IAW SRM 51-40-02. INSTALLED NEW INBD CREASEBEAM INBD CHORD AT BS 665-775, RBL 58, IAW SRM 51-40-02. - MAJOR REPAIR.

ATA 5320

Part: FITTING — DAMAGED (BS 1640) · airframe 53,423 hrs · 21,903 cycles

DWG 657N3160, SH.2, REV. D, FOR AFT PALLET FRAME MOD, SHOWS 4EA. EXISTING FASTENER HOLES TO BE PICKED UP IN THE 657N3161-11 FITTING AT BS 1640. ACFT ACTUALLY HAS 5 EA EXISTING HOLES AT BS 1640, LBL 60, A FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399EZ2R02, AND MAE EA 757-5362-16-F2601, REV NEW. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.

ATA 5310

Part: CREASE BEAM — CORRODED (BS 353-366) · corrosion level 2 · airframe 53,423 hrs · 21,903 cycles

R-1 DOOR OTBD CREASEBEAM IS CORRODED AT BS 353-366, RBL 60. R & R NEW CREASEBEAM IAW SRM 51-40-02, 2 BS 353-366, RBL 60. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 3; BEFORE REWORK: .071", AFTER REWORK: .061", REMOVED; .010". -MAJOR REPAIR

ATA 5320

Part: SUPPORT BRACKET — DAMAGED (BS 1100) · airframe 53,423 hrs · 21,903 cycles

TV MONITOR SUPPORT BRACKET MOUNT HOLE ON FRAME IS WITHOUT PROPER PITCH AT BS 1100, BETWEEN STR 3-R AND 4R. REMOVED DAMAGED SECTION OF FRAME. LOCATED AND DRILLED FRAME AND REPAIR DOUBLERS IAW SRM 53-00-07. TREATED AND PRIMED FRAME AND DOUBLERS IAW SRM 51-21-01. INSTALLED REPAIR FRAME AND DOUBLERS ISW SRM 53-00-07. (MAJOR REPAIR) THIS REPAIR IS A CATEGORY B REPAIR.

ATA 5320

Part: SUPPORT — DAMAGED (BS 1120) · airframe 53,423 hrs · 21,903 cycles

TV MONITOR SUPPORT BRACKET MOUNT HOLE DISTANCE FROM ANOTHER HOLE IS OUT OF LIMITS ON FRAME AT STA 1120 BETWEEN STR 4R, AND STR 3R. REMOVED DAMAGED SECTION, STA 1120, STR. 3R-4R, IAW SRM 53-00-07, REPAIR 3. RECEIVED REPAIR PART FROM FAB SHOP ON T10/830330, BATCH NR 418405A7. NDT CHECK, NO CRACK INDICATIONS FOUND IAW NTM 51-00-19 PT 6. LOCATED, DRILLED, AND INSTALLED REPAIR IAW SRM 53-00-07 REPAIR NR 3. ALL PARTS TREATED AND PRIMED BEFORE INSTALLATION IAW SRM 51-20-01. CAT 'B" REPAIR. INITIAL INSPECTION 10,000 FLIGHT CYCLES. INSPECT PER NOTE "D" OF SRM 53-00-07 PAGE 201. COMPLY WITH A HFEC INSP EVERY 12,000 FLIGHT CYCLE INTERVALS. ALTERNATE COMPLIANCE; DETAILED VISUAL INSP AT 9,000 FLIGHT CYCLE INTERVALS. CLASSIFIED AS A MAJOR REPAIR. CLASS 'B" REPAIR.

ATA 5311

Part: FRAME — DAMAGED (BS 395 S1-2L) · airframe 53,423 hrs · 21,903 cycles

BS 395 FRAME, BETWEEN S1/ 2L, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.

ATA 5311

Part: FRAME — DAMAGED (BS 1100 S3-4R) · airframe 53,423 hrs · 21,903 cycles

BS 1100, FRAME, S3R/ 4R, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.

ATA 5311

Part: FRAME — DAMAGED (BS 1120 S3-4R) · airframe 53,423 hrs · 21,903 cycles

BS 1120 FRAME, BETWEEN S3R/ 4R, HAS MULTIPLE HOLES THAT ARE NOT WITHIN PITCH LIMITS.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 640-780) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK CORRODED AND GOUGED AT BS 640-780, RBL 45.5, IN SEVERAL PLACES. R & R DAMAGED SEAT TRACK AT RBL 45.5, BS 640-780, IAW SRM 53-00-52, AND SRM 51-40-02. CORROSION AND GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 7, PAGE 101-104; L=100",W=3.3",D=.020". -MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — DAMAGED (BS 1160) · airframe 53,423 hrs · 21,903 cycles

THE 144N8007-64 CHORD, LWR FLANGE, AT BS 1160, RBL 8-LBL 8, WILL HAVE SHORT E.D. CONDITION ON 14 EA .250" HOLE LOCATIONS. AT BS 1160, RBL8 - LBL 8, A T-CHORD REPLACEMENT WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING PTF CONVERSION, ON MAE MOD W/C 118350451CZ2R05, AND MAE EA 757-5345-16-F2002, REV NEW, DATED 03/25/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY AND CLASSIFIED AS A MAJOR ALTERATION.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 1640) · airframe 53,423 hrs · 21,903 cycles

MCD SEAT TRACK CROWN CORRODED AT BS 1640, LBL 24. R & R SEAT TRACK BETWEEN BS 1540-1640, LBL 24.50, IAW SRM 53-00- 52 / 51-40-02. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, PAGE 102. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — MISLOCATED (BS 1420-1620) · airframe 53,423 hrs · 21,903 cycles

FRAME STA 1420-1620, LBL 58.22, UNABLE TO LOCATE SEAT TRACK PN 657N3332-10. EXISTING SEAT TRACK BETWEEN BS 1540-1620, LBL 24.75 AND 45.50, MISLOCATED. SEAT TRACK AT BS 1420-1620, LBL 58.22, WAS REPLACED IAW MAE EA 757-5365-16-F2600, DATED 04/08/2010, REV A SEAT TRACK 657N3332-10 WAS INSTALLED ON MAE MOD W/C 118350437EZ2R06, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION. THIS NON- ROUTINE IS FOR TRACKING PURPOSES ONLY AND CLASSIFIED AS A MAJOR ALTERATION.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 780-879) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK GOUGED AND WORN AT BS 780-879, LBL 24. CLEANED AND CHECKED LIMITS ON SEAT TRACK AT BS 780-879, LBL 24; THE GOUGE AND WORN AREA EXCEEDS .260" MINIMUM FOR ACCEPTABLE WEAR AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R- SEAT TRACK AT BS 780-879, LBL24, PER SRM 51-40-02. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 640-780) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK AT BS 640-780, RBL 24, IS GOUGED.

ATA 5310

Part: CREASE BEAM — CORRODED (BS 350) · airframe 53,423 hrs · 21,903 cycles

R1 DOOR CREASE BEAM IS CORRODED AT BS 350, RBL 58.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 780-870) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK AT BS 780-870, RBL 45, IS GOUGED AND WORN. R & R SEAT TRACK, PN BAC 1520-792, 7178-T6, FROM BS 780-879, RBL 45.50, PER SRM 53-00-52 AND 51-40-02. GOUGE/ WEAR FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK GOUGED AND WORN AT STA 879TO 900 RBL24 BLENDED AREA, CHECK LIMITS FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT .225 AFTER REWORK .213 MAT LOSS OF .12 EXCEEDS MAX MAT WEAR OF .004 . REMOVED SEAT TRACK CROWN STA 879 - 900 RBL 24 IAW SRM 51-40-02 . FABBED REPLACEMENT CROWN FROM MAT BAC1520-841 IAW SRM 53-30-52 FIG 1 DETAIL IV , INSTALLED FABBED SEAT TRACK CROWN STA 879 - 900 RBL 24 IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 780-879) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK AT BS 780-879, RBL 24, IS BROKEN AND GOUGED. R & R SEAT TRACK, PN 1520-792, FROM BS 780-879, RBL 24.75, PER SRM 53-00-52, AND SRM 51-40-02. DAMAGE TO SEAT TRACK OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — DAMAGED (BS 575) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK AT BS 575, RBL 24, HAS BROKEN FLANGE. BLENDED AREA IAW SRM 51-10-02. SEAT TRACK DAMAGE AT BS 575, RBL 24 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 2 AND 3; L=6",W=1.3",D=.100". R & R SEAT TRACK AT BS 440-640, RBL 24.75, IAW SRM 51-40-02. -MAJOR REPAIR

ATA 5347

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

SEAT TRACK GOUGED AND WORN AT STA 879 TO 900 RBL 45 BLENDED AERA , CHECKED LIMITS, FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT 225 , AFTER REWORK .203, EXCEEDS MAX MAT LOSS OF .004 , REMOVED SEAT TRACK CROWN STA 879 TO 900 RBL 45 IAW SRM 51-40-02, FABBED REPLACEMENT SEAT TRACK CROWN FROM MAT BAC 1520-841 IAW SRM 53-30-52 FIG 1 DETAIL IV INSTALLED NEW SEAT TRACK CROWN AT STA 879-900 RBL 45 IAW 51-40-02. MAJOR REPAIR.

ATA 5311

Part: FRAME — GOUGED (BS 1280 S10-11R) · airframe 53,423 hrs · 21,903 cycles

FUSELAGE FRAME AT BS 1280, S10R-S11R, FLANGE IS GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P.103. REMOVED AND INSTALLED NEW FRAME SECTION, AND 2EA. CHANNELS, AT BS 1280, S10R TO S11R IAW SRM 51-40-02 / 53-00-07, FIG 202, P.201-206. REPAIR PARTS FABRICATED ON TRAVELERS T10/833037, T10/833036, T10/833035. MAJOR REPAIR.

ATA 5320

Part: SILL — CORRODED (FUSELAGE) · airframe 53,423 hrs · 21,903 cycles

L3 DOOR LOWER SILL IS CORRODED.

ATA 5100

Part: NONE — NONE (NONE) · airframe 53,423 hrs · 21,903 cycles

BS1640 FLOORBEAM PREVIOUS REPAIR INTERFERES WITH PTF CONVERSION. (IN-PROCESS).

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

AT STA 1661 LBL 57 FLOORBEAM UPPER CHORD, UPPER SURFACE CORRODED.

ATA 5320

Part: SUPPORT — CORRODED (BS 365-418) · airframe 53,423 hrs · 21,903 cycles

BS 365-418, RBL 45.5, SEAT TRACK SUPPORT IS CORRODED. REMOVED CORROSION; .020" MATERIAL REMOVED, ORIGINAL MATERIAL .070", FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 7. REMOVED SUPPORT 2 BS 365-418, RBL 45 IAW SRM 51-40-02. RECEIVED NEW SUPPORT IAW TRAVELER NR T10/824299. INSTALLED NEW SUPPORT 2 BS 365-418, RBL 45, IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 53,423 hrs · 21,903 cycles

BS 418-440, RBL 45.5, SEAT TRACK GOUGED, OUT OF LIMITS.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 53,423 hrs · 21,903 cycles

BS 418-440, RBL 24.75, SEAT TRACK GOUGED OUT OF LIMITS.

ATA 5347

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

STA 418-440 RBL 24.5 SEAT TRACK GOUGED. REMOVED .019" FROM .070" ORIGINAL MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 2. REMOVED SEAT TRACK AT BS 418-440, RBL 24.75, IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK FROM MATERIAL PN BAC 1520-792, BATCH 1571736 & INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 53,423 hrs · 21,903 cycles

STA 365 RBL 0-18 HAS EXISTING REPAIR THAT INTERFERS WITH MOD CARD 1183650461AZ2R05 INSTALL, ALSO FOUND CORRODED OUT OF LIMITS LBL 58. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3; ORIGINAL THICKNESS=.125' / AFTER REWORK=.092". FABRICATED NEW UPPER TEE, BAC 1505-100880/7075-T6, BATCH NR 1787163, IAW SRM 53-00-51, FIG 201, REPAIR NR 3. RECEIVED -2 & -3 REPAIR ANGLES ON TRAVELER NR T10/823329, RECEIVED -4 & -5 REPAIR STRAPS ON TRAVELER NR T10/823330. INSTALLED NEW UPPER T-CHORD, REPAIR ANGLES, AND REPAIR STRAPS IAW SRM 53-00-51-FIG 201, REPAIR NR 3. MAJOR REPAIR.

ATA 5320

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,423 hrs · 21,903 cycles

STA 365-418 RBL 45.5 SEAT TRACK SUPPORT CORRODED FWD OUTBD CORNER. REMOVED CORROSION ; .020" MATERIAL REMOVED, ORIGINAL MATERIAL .070" , FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SUPPORT 2 BS 365-418, RBL 45, IAW SRM 51-40-02. RECEIVED NEW SUPPORT IAW TRAVELER NR T10/824299. INSTALLED NEW SUPPORT 2, BS 365-418, RBL 45, IAW SRM 51-40-02. MAJOR REPAIR.

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,423 hrs · 21,903 cycles

FLOORBEAM HAS CORROSION AT STA 345 LBL 12 TO 17. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. FIG 101, DET III. FABRICATED UPPER T-CHORD MAT BAC 1505-100880, REPAIR ANGLES MAE TRAV NR T10/824058, AND REPAIR STRAPS MAE TRAV NR T10/824060. INSTALLED UPPER T-CHORD , REPAIR ANGLES, AND STRAPS STA 345, RBL 70- LBL 52, IAW SRM 53-00-51, FIG 201, CATEGORY "A", REPAIR 3. MAJOR REPAIR.

ATA 5347

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 53,423 hrs · 21,903 cycles

STA 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED .018" FROM .070" ORIGINAL MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT TRACK FROM BS 418-440, RBL 45.5, SRM 51-40-02. FABRICATED NEW SEAT TRACK FROM MATERIAL PN BAC 1520-792, BATCH 157736 & INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.