N989DN

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 35,695 hrs · 34,789 cycles

VERTICAL STABILIZER LEFT FRONT SPAR CAP DAMAGED, BELOW ZFS 52.267. REPAIRED THE SPAR CAP IAW ERA 565658-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,878 hrs · 33,546 cycles

FRAME 1225 CRACKED AT TAIL CONE ALIGNMENT PIN 7 O'CLOCK POSITION. REMOVED DAMAGED AREA REF 497316-14MA. MANUFACTURED DOUBLER AND DRILLED REF 497316-14MA. INSTALLED REPAIR PER RI 559273-14.

Part: LIGHT — CONTAMINATED · airframe 33,774 hrs · 33,477 cycles

OVERWING AISLE OVERHEAD EMERGENCY EXIT SIGN PARTIALLY OBSCURED. REMOVED DEBRIS FROM INSIDE BOTH LENS, OPS CHECKED GOOD.

Part: CONNECTOR — FAILED (CABIN) · airframe 31,631 hrs · 31,957 cycles

THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS FOR THE OVERWING LIGHTS AND REPLACED THAT CONNECTOR PLUG. THE FUNCTIONAL CHECK OF THE SYSTEM WAS GOOD.

Part: POWER SUPPLY — UNKNOWN (CABIN) · airframe 31,631 hrs · 31,957 cycles

THE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT P1-119 AND THE FUNCTIONAL CHECK OF THE SYSTEM WAS GOOD.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 31,610 hrs · 31,940 cycles

THE PILOT REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AIRCRAFT HAD ILLUMINATED UNCOMMANDED. MAINTENANCE REPLACED AN INTERMITTENT EMERGENCY LIGHT SWITCH S1-177 IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,610 hrs · 31,940 cycles

THE F/A REPORTED THAT THE EEPL AT THE LOWER SIDEWALL OVERWING AND THE TAIL EXIT LIGHTS HAD ILLUMINATED UNCOMMANDED DURING FLIGHT. MAINTENANCE CYCLED THE EEPL SWITCH IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,017 hrs · 31,445 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: FRAME — CRACKED (BS 696) · airframe 30,653 hrs · 31,179 cycles

UPPER RADIUS BS 696 OF OVERWING FRAME TAB RT CRACKED. REPLACED FRAME AT RT BS 696 IAW SRM 51-41-02, 51-41-05, DWG SR95530013, REV: A, PN SA95530034-9.

Part: VANE — PUNCTURED (RT WING TE FLAP) · airframe 30,653 hrs · 31,179 cycles

RIGHT WING, INBD FLAP VANE, INBD END HAS A PUNCTURE HOLE. REMOVED DAMAGE ON RT WING INBD FLAP VANE INBD END IAW SRM 57-53-01 REPAIR NR 1. MATERIAL REMOVED .75" DIA CIRCLE. FABRICATED .75" FILLER FROM 7075-T6 BARE .016", FABRICATED 11.5" X 4.25" DOUBLER FROM 7075-T6 .020" IAW SRM 57-53-01, REPAIR 1, REPAIR PARTS INSTALLED IAW SRM 57-53-01.

Part: CARGO TRACK — CORRODED (BS 427-655) · corrosion level 2 · airframe 32,248 hrs · 32,411 cycles

FWD CARGO BAY. CARGO TRACK CORRODED AT BS 427 - 655. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE BEYOND LIMITS IAW SRM 53-20- 52. REPLACED THE CARGO TRACK IAW SRM 53-20-52 AND DWG 5965411 REV AW.

Part: LONGERON — DAMAGED (BS 908) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

AFT CARGO COMPARTMENT CENTER LONGERON 30 HAS CHIPPED PAINT, POSSIBLE LIGHT CORROSION FRAME BS 908. REMOVED CORRODED IAW SRM 51-10-04 AT AFT CARGO BS 908, L30. EVALUATED AND FOUND ORIG .093" LOSS .040" REM .053" OUT OF LIMITS IAW SRM 53-00-00 REMOVED, FABRICATED AND INSTALLED NEW SPLICE IAW SRM 51-41-05 AND DWG NR S940866, REV:Y.

Part: DUCT — DENTED (A/C PACK) · airframe 30,826 hrs · 31,284 cycles

AFT ACCESSORY COMPARTMENT, GROUND AC DUCT LOWER SIDE HAS DENT.

Part: CARGO TRACK — CORRODED (BS 813-1028) · corrosion level 2 · airframe 32,244 hrs · 32,407 cycles

AFT CARGO BAY, CARGO TRACK CORRODED BS 813 TO 1028 S26L. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 AND 51-30-07 AND DWG 5956331 REV BS. REPLACED FWD CARGO TRACK IAW DWG 5956331 REV BS & BE.

Part: SLAT TRACK — GOUGED (RT WING) · airframe 30,653 hrs · 31,179 cycles

RIGHT WING FIXED L/E INBD SIDE OF SLAT TRACK NR 2 HAS GOUGE ON DOUBLER. ASSOCIATED ER/A 14-542808 ADDED FOR AC 9589. REPLACED EXISTING REPAIR AT RT WING FIXED L/E INBD SIDE OF TRACK NR 2 SLAT IAW SRM 51-40-02 AND COMPLIED WITH ER/A 542808-14, REV: ORIGINAL. REPLACED EXISTING REPAIR AT RT WING FIXED L/E INBD SIDE OF TRACK NR 2 SLAT IAW SRM 51-40-02 AND COMPLIED WITH ER/A 542808-14, REV: ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 813-1028) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

AFT CARGO BAY CARGO TRACK AT BS 813 - 1028, CORRODED, REMOVED CORROSION IAW SRM 51-10-04 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101 & 51-30-07, FIG 18. REPLACED THE CARGO TRACK IAW SRM 51-41-01, 51-41-02, AND DWG 59366 63, REV: W.

Part: CUSP WEB — CRACKED (BS 674-696) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN CUSP WEB CRACKED AT LT BS 674 AND 696 BETWEEN LBL 44 -54. CUT OUT DAMAGE, FABRICATE AND INSTALLED CUSP WEB 7075-T6 .020, 2 EA SPLICES 7075-T6 .032 IAW SRM 51-41-02 AND 53-00-55, FIG 223.

Part: SEAT TRACK — DAMAGED (BS 237-589) · corrosion level 2 · airframe 30,669 hrs · 31,193 cycles

MAIN CABIN SEAT TRACK HAS CORROSION, SCRATCHES AND GOUGES BETWEEN BS 237-589, RBL 22. REPLACED MAIN CABIN SEAT TRACK AT RBL 22, FS 237-589 IAW SRM 51-41-01. DAMAGE REMOVED IAW SRM 53-20-52. ORIGINAL MATERIAL 0.100", MATERIAL REMOVED 0.060", MATERIAL REMAINING 0.040", FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-20-52. REPLACED MAIN CABIN SEAT TRACK AT RBL 22, FS 237-589 IAW SRM 51-41-01. DAMAGE REMOVED IAW SRM 53-20-52. ORIG MATERIAL 0.100" MATERIAL REMOVED 0.060" MATERIAL REMAINING 0.040" FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-20-52, NO FOLLOW ON INSPECTION.

Part: ANGLE — CRACKED (BS 1152) · airframe 30,653 hrs · 31,179 cycles

AFT ACCESSORY COMPARTMENT BS 1152 HAS CRACKED ANGLE L2R. REPLACED ANGLE IAW SRM 51-41-05 AND DWG 9911860, REV L.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 32,244 hrs · 32,407 cycles

BS 200 FLOORBEAM IS CORRODED BETWEEN RBL 44 & 52. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53- 00-00. THE FLOORBEAM WAS REPLACED IAW DWG 9936534 REV BW & SRM 51-41-02.

Part: FORMER — CORRODED (BS 715) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

LEFT KEEL BEAM BARREL, BS 715, OTBD END CORRODED FORMER. REPLACED LT KEELBEAM FORMER BS 715 IAW SRM 51-41-05, DWG 9923454, REV: F. REMOVED CORROSION & EVALUAED DAMAGE ORIGINAL MATERIAL .063 REMAINING .000 AND IS OUT OF LIMITS IAW SRM 53-00-00.

Part: LONGERON — CRACKED (BS 1133) · airframe 30,653 hrs · 31,179 cycles

AFT ACCESSORY COMPARTMENT, BS 1133, LONG 2R CRACKED. REMOVED EWIS PROTECTION FROM WORK AREA IAW SWPM 20-10-10. CUTOUT DAMAGED AREA AT AFT ACCESSORY COMPARTMENT BS 1133, LONG 2R, DIM 15" IAW SRM 20-10-10, FABRICATED, LOCATED, AND DRILLED LONGERON SECTION FROM S2912727, DIM 15" AND SPLICE FROM S00045-1200, DIM 13" IAW SRM 53-00-05 AND 51-40-08, INSTALLED REPAIRS PARTS IAW SRM 53-00-05, REP 2. INSTALLED ID TAG IAW DPS 900-5-1-N04.

Part: DOOR FRAME — CRACKED · airframe 30,653 hrs · 31,179 cycles

CRACKED DOOR LANDING AT FWD OTBD CORNER OF GROUND CONDITIONED AIR SUPPLY DOOR CUTOUT. REMOVED DOOR ASSY FOR CONDITIONED AIR GROUND CONNECTION IAW SRM 51-41-01. REMOVED DOOR LANDING IAW SRM 51-41-02. REMOVED AIR GROUND CONNECTION IAW SRM 51-41-02. FABRICATED NEW DOOR LANDING FROM 7075-T6 IAW SRM 51-40-08 AND DWG 5911429, REV DZ. APPLIED FINISH AS REQUIRED IAW SRM 51-10-04. INSTALLED PAN AND NEW DOOR LANDING IAW SRM 51-41-02, INSTALLED DOOR ASSY IAW SRM 51-41-01.

Part: FORMER — CRACKED (BS 696) · airframe 30,653 hrs · 31,179 cycles

LEFT KEELBEAM BARREL BS 696, OTBD END OF FORMER CRACKED. REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.

Part: FORMER — NOT REPORTED (BS 696) · airframe 30,653 hrs · 31,179 cycles

REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.

Part: FORMER — CRACKED (BS 1116) · airframe 30,653 hrs · 31,179 cycles

AFT ACCESSORY COMP BS 1116 BELOW LONGERON 15R FORMER CRACKED. REPLACED FORMER BS 1116 BELOW LONGERON 15R IAW SRM 51-41-02.

Part: ANGLE — CORRODED (BS 202) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

FWD GALLEY SERVICE DOOR LOWER JAMB AREA, Z-ANGLE IS CORRODED FWD OF RBL 54 SEAT TRACK AT FS 202. REMOVED CORROSION FWD GALLEY GALLEY SERVICE DOOR LOWER JAMB AREA "Z" ANGLE FWD OF RBL 54, SEAT TRACK AT FS 202 IAW SRM 51-10-04. EVALUATED AREA AND FOUND ORIG MATERIAL .070", MATERIAL LOSS .027, MATERIAL REM .043" AND IS FOUND TO BE OUT OF LIMITS IAW SRM 53-0-0. REMOVED DAMAGED ANGLE IAW SRM 51-41-02. LOCATED DRILLED AND DEBURRED NEW FLOOR SUPPORT IAW SRM 51-40-08 AND DWG 5952262, REV K. INSTALLED NEW SUPPORT IAW SRM 51-40-04.

Part: FORMER — CRACKED (BS 1116) · airframe 30,653 hrs · 31,179 cycles

AFT ACCESSORY COMPARTMENT BS 1116 BELOW LONG 15L FORMER CRACKED. REMOVED FORMER BS 1116, BELOW LONGERON 15L IAW SRM 51-41-02 LOCATED, DRILLED, AND DEBARRED NEW FORMER IAW SRM 51-40-08 AND DWG 5913596, REV AN. INSTALLED NEW FORMER BS 1116 BELOW LONGERON 15L IAW SRM 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,237 hrs · 32,401 cycles

LOWER FUSELAGE ANTENNA INTERNAL DOUBLER IS CORRODED AT FS 212 BETWEEN L229L & LONGERON 30 IN E&E COMPARTMENT. APPLIED TOP COAT ON AREA IAW AMM 51-10-00 701. REMOVED CORROSION FROM INTERNAL DOUBLER STA 212 BETWEEN 629L & L30L IAW SRM 51-10-04. NO LIMITS IN SRM FOR AREA COMPLIED WITH ER/A 542799-14 REV ORIGINAL.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 30,653 hrs · 31,179 cycles

AFT FUSELAGE BS 1022 BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 6L AND L7L, MARKED. REMOVED SHEAR TIE AT AFT FUSELAGE FS 1022 BETWEEN LONG 6L TO L7L IAW SRM 51-40-02, LOCATED, DRILLED, AND DEBURRED NEW SHEAR TIE IAW SRM 51-40-08. INSTALLED NEW SHEAR TIE IAW SRM 51-41-05 & DWG 9912243, REV HF.

Part: SUPPORT — CHAFED (RUDDER) · airframe 30,653 hrs · 31,179 cycles

RUDDER L/E PANEL 370GL CENTER MOUNTING SUPPORT IS CHAFED, MARKED. REMOVED DAMAGED SUPPORT AT RUDDER L/E IAW SRM 51-41-02 LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-08 AND DWG 9971306, REV, INSTALLED NEW SUPPORT ON L/E OF RUDDER IAW SRM 51-41-02.

Part: FORMER — CRACKED (BS 674) · airframe 30,653 hrs · 31,179 cycles

LEFT KEEL BEAM FORMER BS 674 CRACKED ON OTBD END. INSTALLED NEW FORMER IAW SRM 51-41-02, 51-41-05 AND DWG 9923453, REV C, REV A. REPLACED KEEL BEAM FORMER BS 674 IAW SRM 51-41-02 AND 51-41-05 COMPLIED WITH ER/A 542797-14, REV O FOR ALL OTHER WORK REQUIRED. ASSOCIATED ER/A 14-542797 ADDED FOR AC 9589.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,237 hrs · 32,401 cycles

LT KEEL BEAM PANEL BETWEEN STA 715-747 LONG 30 TO OB SIDE OF CONT KEEL EDGE CORRODED. INSTALLED FASTENERS LT KEEL BEAM STA 715-747 IAW SRM 51-41-02. REMOVED CORROSION LT KEEL BEAM STA 715-747 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04 C/W NDT UT INSPECTION OF THE BLENDED AREA IAW NDT SPM PT 04-00-07. ORIG MAT .071" REMAINING MAT .053". COMPLIED WITH ER/A 542804-14 FOR ALL OTHER WORK REQUIRED. NO FURTHER ACTIONS REQUIRED AT THIS TIME.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,237 hrs · 32,401 cycles

LT KEEL BEAM BARREL, BETWEEN STA 715-696 LONG 30 TO OB SIDE OF CANT KEEL EDGE CORRODED. TOPCOATED LT KEEL BEAM BARREL IAW SRM 51-10-04. REMOVED CORROSION LT KEEL BEAM STA 696-715 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04. C/W NDT UT INSPECTION OF THE BLENDED AREA IAW NDTM PT 4 CH 04-00-07, ORIG MAT .071" MAT REMAINING .053". COMPLIED WITH ER/A 542804-14.

Part: FLOOR SUPPORT — CORRODED (BS 994) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

AFT CARGO - SIDE PLATE FLOOR SUPPORT CORRODED AT BS 994, S 28L MARKED. REMOVED CORROSION AFT CARGO SIDE PLATE FLOOR SUPPORT BS 994 S28L, EVALUATED AREA FOUND ORIGINAL MATERIAL .063, MATERIAL REMOVED .015, MATERIAL REMAINING .048 AND IS FOUND TO BE BEYOND LIMITS IAW SRM 53-00-0. REMOVED AFT CARGO SIDE PLATE FLOOR SUPPORT IAW SRM 51 -41-05. LOCATED AND DRILLED NEW SPLICE IAW SRM 51-40-08 AND DWG 9957917, REV BY. INSTALLED NEW SPLICE BS 994, S28L IAW SRM 51-41-05. APPLIED FINISH AS REQUIRED IAW SRM 51-10-04.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD NR 222GF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222GF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222GF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688 REV H.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD NR 211ASF. IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222ASF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 211, ASF DIM 11" X 15" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV AB.

Part: SHEAR TIE — CORRODED (BS 674) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

UPON REMOVAL OF RT KEEL BEAM BARREL FORMER BS 674 FOUND SEVERAL AREAS OF CORROSION ON THE FORMER SHEAR CLIP. REMOVED SHEAR CLIP FROM RT KEELBEAM FORMER BS 674 IAW SRM 51-41-02 FROM SHEAR CLIP AND EVALUATED AREA FOUND ORIGINAL MATERIAL .062", MATERIAL LOSS .025", REM MATERIAL .037" AND IS FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00 AND DWG S1242526, REV A. LOCATED, DRILLED, AND DEBURRED NEW SHEAR CLIP IAW SRM 51-40-08. RESTORED FINISH AS REQUIRED IAW SRM 51-10-04.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222 AEF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222AEF DIM 21" X 41" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936640, REV D.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 221 IS DELAMINATED. MAIN CABIN FLOOR PANEL 221KF FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221KF, DIM 36" X 56" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936552, REV: K.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD, 211ALF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ALF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 211ALF DIM 40" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936537, REV AG.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 211 ARF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211 ARF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 211ARF DIM 11" X 15" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV: AG.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 221WF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221WF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED FLOOR PANEL 221 WF DIM 21" X 76" IAW SRM 53-20-50, REPAIR 3 AND 9936585, REV: G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 221LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221LF DIM 21" X 56" IAW SRM 53-20-50, REPAIR 3. DWG 9936553, REV: C.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221EF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221EF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221EF DIM 40" X 9" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936549, REV K.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221CF IS DAMAGED. MAIN CABIN FLOOR PANEL 221CF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE. FABRICATED NEW FLOOR PANEL NR 221CF DIM 40" X 12" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936546, REV C.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222DF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222DF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222DF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV: H.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211 AND FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 211ANF DIM 22" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539 REV AB.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221BF IS DAMAGED. MAIN CABIN FLOOR PANEL 221BF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221 BF DIM 40" X 36" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936545, REV M.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221 AF IS DAMAGED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50. ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 221AF DIM 36" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936544, REV: G.Q.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222APF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222APF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222APF DIM 21" X 76" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV: G.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221JF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221JF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 60" X 8" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936551, REV: AN.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222FF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50. REPAIR 3 AND DWG 9936583, REV: E.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD NR 211ATF IS DELAMINATED. FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG DWG 9936539, REV AB.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD NR 222AVF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222AVF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222AVF DIM 42" X 65" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585 REV: G.

Part: FLOOR PANEL — PUNCTURED (AFT CABIN) · airframe 30,653 hrs · 31,179 cycles

AFT CABIN FLOOR PANEL UPPER SKIN IS PUNCTURED AT FS 986 BETWEEN RBL 44 AND RBL 54. REPAIRED AFT CABIN FLOOR PANEL UPPER SKIN AT FS 986, RBL 44-54 IAW SRM 53-20-50, REPAIR 2 AND DWG 9956320, REV: G.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221DF IS DAMAGED. MAIN CABIN FLOOR PANEL 221DF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 221DF DIM 20" X 36" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV: W.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 223DF IS DELAMINATED. MAIN CABIN FLOOR PANEL 223DF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 223DF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV: H.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOOR PANEL 221FF IS DAMAGED. MAIN CABIN FLOOR PANEL 221FF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 20" X 36" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936585, REV: W.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222ACF IS DELAMINATED. MAIN CABIN FLOOR 222ACF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222ACF DIM 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222RF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222RF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222RF DIM 21" X 76" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV: G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN FLOORBOARD 222LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222LF DIM 21" X 76" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV G.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 30,653 hrs · 31,179 cycles

AFT FUSELAGE BS 1022, BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 7 & 8R. REPLACEDTHE SHEAR TIE IAW SRM 51-41-02 AND 51-41-05, DWG 9912243, REV HF.

Part: SUPPORT — CORRODED (BS 946) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

AFT CARGO COMPT; SIDE PLATE ON FRAME, SUPPORT CORRODED, BS 946 STRINGERS 27 - 28L. REMOVED CORROSION AFT CARGO FRAME SUPPORT BS 946 S28L TO S27L. EVALUATED DAMAGE FOUND ORIGINAL MATERIAL .063" MAT LOSS .020" REMAINING MAT .043" AND IS FOUND TO BE BEYOND SERVICEABLE LIMITS. REMOVED SPLICE IAW B717 SRM 51-41-05, LOCATED AN DRILLED NEW SPLICE IAW SRM 51-40-08 AND DWG 9919603, REV CC. INSTALLED NEW SPLICE IAW SRM 51-41-05. APPLIED FINISH AS REQUIRED IAW SRM 51-10-04.

Part: FORMER — CRACKED (BS 696) · airframe 30,653 hrs · 31,179 cycles

RT KEEL BEAM BARREL, BS 696 OTBD END OF FORMER CRACKED. REPLACED RT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG NR 9923453, REV A AND C.

Part: SUPPORT — CORRODED (BS 946) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

AFT CARGO BAY SIDE PLATE ON FRAME, SUPPORT CORRODED, BS 946 STRINGERS 27 - 28L. REMOVED CORROSION AFT CARGO FRAME SUPPORT BS 946, S28L TO S27L. EVALUATED DAMAGE FOUND ORIG MAT .063", MAT LOSS .020", REMAINING MATERIAL .043" AND IS FOUND TO BE BEYOND SERVICEABLE LIMITS . REMOVED SPLICE IAW SRM 51-41-05, LOCATED AN DRILLED NEW SPLICE IAW SRM 51-40-08 AND DWG NR 9919603, REV CC. INSTALLED NEW SPLICE IAW SRM 51-41-05. APPLIED FINISH AS REQUIRED IAW SRM 51-10-04.

Part: FORMER — CRACKED (BS 715) · airframe 30,653 hrs · 31,179 cycles

RT KEELBEAM BARREL BS 715 OTBD END OF FORMER CRACKED. REPLACED RT KEELBEAM FORMER IAW SRM 51-41-02 AND 51-41-05.

Part: SUPPORT BRACKET — CRACKED (BS 715) · airframe 30,653 hrs · 31,179 cycles

RT KEELBEAM BARREL, BS 715 SUPPORT BRACKET ASSY CRACKED. REPLACED RT KEELBEAM SUPPORT BRACKET BS 715 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923454, REV F.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 30,653 hrs · 31,179 cycles

FS 1022 BULKHEAD TO SKIN AFT SHEAR TIE IS CRACKED BETWEEN LONGERON 13R AND L14R MARKED. REPLACED FS 1022 BULKHEAD TO SKIN AFT ATTACHING SHEAR TIE BETWEEN LONGERON 13R AND 14R IAW SRM 51-41-05 AND DWG 9912243, REV JS.

Part: CUSP WEB — CRACKED (BS 598-617) · airframe 30,653 hrs · 31,179 cycles

MAIN CABIN CUSP WEB CRACKED BETWEEN BS 598-617, LT SIDE. CUT OUT DAMAGED AREA OF MAIN CABIN CUSP WEB BS 598-617 LT SIDE, FABRICATED, AND INSTALLED REPAIR FILLER & DOUBLER MADE FROM 7075T6 .032", DOUBLER AND 7075T6 .020, FILLER IAW SRM 53-00-55, REP 4.

Part: FLOOR SUPPORT — CORRODED (BS 160-190) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

FWD WET AREA FLOOR SUPPORT IS CORRODED AROUND FASTENER HOLES AT RBL 52, FS 160 TO FS 190. REMOVED CORROSION AT M/C FLOOR SUPPORT FS 160-190 RBL 52 AND ALODINED IAW SRM 51-10-07. C/W UT INSP OF BLENDED AREA FOR MATERIAL LOSS IAW B717 NDTSPM PT 4, 07-00-07 ORIGINAL "T" .070 LOWEST REM MAERIAL .049 ASSET 15251. EVALUATED LIMITS AND FOUND FLOOR SUPPORT TO BE OUT OF LIMITS MATERIAL LOST: .021. REMOVED FLOOR SUPPORT IAW SRM 51-41-02. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-08 & DWG 9936534, REV BW. ALODINED AND PRIMED HOLES IAW SRM 51-10-4. INSTALLED NEW FLOOR SUPPORT AT M/C, FS 160-190, RBL 52 IAW SRM 51-41-02 AND DWG 9936534, REV BW.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,237 hrs · 32,401 cycles

PRESSURE BULKHEAD FWD FACE LOWER DOUBLER IS CORRODED BELOW THE FLOOR AT FS 1053. EVALUATED DOUBLER AND FOUND MAT TO BE EXFOLIATED BEYOND LIMITS ORIG MAT .080" IAW SRM 53-00-00. REMOVED DOUBLER IAW 51-41-05 AND 51-41-02. LOCATED, DRILLED, AND INSTALLED DOUBLER IAW DWG 5930760 REV DL PART NR 5910130U61.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 30,653 hrs · 31,179 cycles

FWD GALLEY AREA FLOORBEAM HAS CORROSION AT BS 200 BETWEEN RBL 10 - 44. REPLACED IAW SRM 51-41-02. AND DWG 9936534, REV BW.