N987DN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,267 hrs · 37,195 cycles

MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS OUT IN THE CABIN DURING THE TURN AROUND CHECK. TROUBLE SHOOTING PER MD88 SSM 33-51 FOUND THE BATTERIES B5-123, B5-259, B5-118, B5-121, AND B5-119 TO BE BAD AND REPLACED THEM PER B717 AMM 33-52. ALL OPERATIONS ARE NOW NORMAL. (LP #5591017)

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 36,524 hrs · 35,258 cycles

THE AFT EMERGENCY EXIT LIGHT CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE FOUND A LOOSE WIRING AND SECURED IT. THE EMERGENCY EXIT LIGHT WORKS PROPERLY.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 36,509 hrs · 35,247 cycles

CORROSION ON THE SPLICE OF THE DOOR FRAME AT THE AFT CARGO BAY, BS 954 AND 994. THE SPLICES WERE REPLACED IAW SRM 53-20-15-2R FIG 201.

Part: TAB — DELAMINATED (RT WING TRIM)

DURING NON ROUTINE UNSCHEDULED CHECK, FOUND THE AILERON TAB TO BE DELAMINATED.

Part: TAB — DELAMINATED (LT WING AILERON)

CUSTOMER FOUND DURING INSPECTION CHECK DELAMINATION ON LOWER AND UPPER SURFACE- FULL SKIN REPLACEMENT REQUIRED

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,533 hrs · 31,506 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — DENTED (RUDDER TAB) · airframe 31,529 hrs · 31,500 cycles

DENT ON RUDDER TAB L/H SIDE, 33" FROM LOWER EDGE AND 5" FROM AFT EDGE. CUT OUT DAMAGED AREA IN RUDDER TAB LT SIDE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01.

Part: SKIN — DENTED (RUDDER TAB) · airframe 31,529 hrs · 31,500 cycles

DENT ON RUDDER TAB RT SIDE, 35" FROM LOWER EDGE AND 6.5" FROM AFT EDGE. CUTOUT DAMAGED AREA ON RUDDER TAB RT SIDE 35" FROM LOWER EDGE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01, REPAIR 1 AND TC 2000-8149-04.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222ATF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936584, REV AH.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222YF IS DELAMINATED WITH 2 EA DAMAGED STIFFENERS AND 1 EACH COVER DAMAGED. MAIN CABIN FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 51-41-08, 51-40-08, 53-20-50, REPAIR 3, AND DWG 9936639, REV P.

Part: KEELBEAM — CRACKED (BS 696) · airframe 31,529 hrs · 31,500 cycles

RT KEELBEAM BARREL FORMER CRACKED AT BS 696 OTBD END. RELACED RT KEELBEAM FORMER AT BS 696 OTBD END. CRACK DIM. 4.0" IAW SRM 51-41-02, 51-41-05, DWG 9923418, REV AB, AND 9923453, REV A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222ADF IS DELAMINATED WITH DAMAGE TO LT COVER AND RT STIFFENER. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL WITH 1 EA NEW STIFFENER AND 1 EACH NEW COVER, DIM. OF NEW PANEL 60" X 38" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936639, REV P.

Part: SKIN — CORRODED (BS 946-954) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT INTERIOR FWD LOWER CORNER BS 946-954 SKIN HAS CORROSION LOWER SURFACE HAS CORROSION AT 4 EA SEAT TRACK N/P'S. CORROSION DAMAGE ON CLOSEOUT WEB AT AFT CARGO COMPARTMENT DOOR CUTOUT INTERIOR SIDE AT 4 EA SEAT TRACK NUTPLATES, ORIGINAL THICKNESS .040", MATERIAL LOSS .011", MATERIAL REMAINING .039", OUT OF LIMITS IAW SRM 53-00-00 AND 53-20-15. CUT OUT DAMAGED SECTION OF WEB DIM. 20.5" X 16.5", FABRICATED NEW WEB SECTION, REPAIR SPLICE DIM. 8.5" X 4", AND INSTALLED REPAIR PARTS IAW SRM 53-20-15 AND 51-70-10, REPAIR 1.

Part: KEELBEAM — CORRODED (BS 622) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

UNDER WING BARREL KEELBEAM BS 662 LONG 29LT CORRODED. CORROSION DAMAGE ON UNDER WING KEELBEAM LONGERON 29LT, FITTING, FOUND OUT OF LIMITS. REPAIRED IAW SRM 51-41-05, DWG 5971090, REV AB AND REV AF.

Part: KEELBEAM — CORRODED (BS 695) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

UNDER WING BARREL KEELBEAM BS 695, LONG 29R CORRODED. UNDER WING BARREL KEELBEAM LONGERON 29RT, FITTING FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-00. REPLACED LONGERON FITTING IAW SRM 51-41-05, DWG 5971090, REV AB, AND REV AF.

Part: KEELBEAM — CORRODED (BS 679) · airframe 31,529 hrs · 31,500 cycles

UNDER WING BARREL KEELBEAM AT BS 679 OTBD END OF FORMER CRACKED RT SIDE. REMOVED FORMER AND SHEAR CLIP FROM RT OF UNDER WING BARREL KEELBEAM AT BS 679, AND LOCATED, DRILLED, AND DEBURR NEW FORMER AND SHEAR CLIP IAW SRM 51-40-08, AND FABRICATED REPAIR ANGLE TO NEW FORMER IAW ER/A. 542825-14. REV ORIGINAL, ALODINED, PRIMED PARTS IAW SRM 51-10-04 INSTALLED NEW FORMER, SHEAR CLIP, AND REPAIR ANGLE IAW SRM 51-41-05 AND IAW ER/A 542825-14, REV ORIGINAL.

Part: KEELBEAM — CRACKED (BS 679) · airframe 31,529 hrs · 31,500 cycles

UNDERWING BARREL KEELBEAM-BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. PLEASE DISREGARD SCEPTRE LOG PAGE 2398032 CLOSED IN ERROR. ASSOCIATED ER/A 14-544128 ADDED FOR AC 9587. REMOVED WING TO BODY FAIRING SUPPORT AND KEELBEAM FORMER AT BS 679 LT SIDE, LOCATED AND DRILLED NEW FORMER AND SHEAR CLIP ALL IAW SRM 51-41-02, 51-41-05, AND 51-40-08, C/W FORMER REPAIR IAW ER/A 544128-14, REV O, INSTALLED WTB FAIRING IAW SRM 51-41-05 AND INSTALLED NEW FORMER IAW DWG 5971090, REV AB AND 9923453, REV C+A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD NR 222GF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936688, REV H, AND AMM 53-21-01.

Part: KEELBEAM — CRACKED (BS 679) · airframe 31,529 hrs · 31,500 cycles

UNDERWING BARREL KEELBEAM BS 679 OTBD END OF FORMER CRACKED LT. INSTALLED FOR FORMER AT BS 679 IAW SRM 51-41-02, 51-41-05, AND DWG 9923453, REV A. ASSOCIATED ER/A 14-544128 ADDED FOR AC 9587.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 31,529 hrs · 31,500 cycles

FWD CARGO COMPARTMENT DOOR UPPER FWD INT DOOR STOP FITTING IS CRACKED. REPLACED STOP FITTING FROM FWD CARGO DOOR UPPER FWD INT. ARA IAW SRM 51-41-01, IAW DWG 9957664 REV N AND ALODINED, PRIMED, AND TOP COATED FITTING IAW SRM 51-10-04, AMM 51-10-00.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD NR 222DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936688 REV H, AND AMM 53-21-01.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD NR 222LF IS DELAMINATED. FLOORBOARD FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW 53-20-50, REPAIR 3, DWG 9936585, REV G, AND AMM 53-21-01.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 31,529 hrs · 31,500 cycles

FLIGHT COMPARTMENT FLOOR PANEL 211AJF IS DAMAGED. CUTOUT DAMAGED AREA ON FLOOR PANEL NR 211AJF DIM. 2.1250" X 3" IAW SRM 53-10-50 REPAIR 1. FABRICATED REPAIR DOUBLER DIM. 4.3750" X 3.5" X .032", AND FILLER DIM. 2.1250" X 3" X .025", AND INSTALLED REPAIR PARTS IAW SRM 53-10-50, REPAIR 1.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221HF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9965855, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221JF IS DELAMINATED. FLOORBOARD 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 NR 9936551, REV AN.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD NR 221KF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 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 9936552, REV K.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222JF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED AND INSTALLED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG NR 9936585, REV G, AND AMM 53-21-01.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221EF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936549 REV K.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221DF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936547, REV W.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222AVF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED AND FABRICATED A NEW FLOORBOARD. INSTALLED THE FLOORBOARD IAW SRM 53-20-50, REPAIR 3, DWG 9936584, REV AH, AND AMM 53-21-01.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 211ALF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936537, REV AG.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD NR 221LF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936553, REV C.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221CF IS DELAMINATED. FLOORBOARD 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 9936546, REV C.

Part: SEAT TRACK — DAMAGED (BS 798-898) · airframe 31,529 hrs · 31,500 cycles

SCRATCHES AND GOUGES THROUGHOUT SEAT TRACK CROWN AND INNER FLAT SURFACES AT AFT CABIN FLOOR, FROM BS 798 - 898 AND RBL 56.0. REMOVED SCRATCHES AND GOUGES THROUGH OUT SEAT TRACK INNER FLAT SURFACE AND EVALUATED ORIGINAL MATERIAL .100, AND MAT LOSS .045" AND REM MAT .055 FOUND TO BE OUT OF LIMIT IAW SRM 53-20-52 AND REPLACED SEAT TRACK FROM BS 798 TO 898, RBL 56.0" IAW SRM 51-41-01, DWG 500482, REV A AND ALODINED AND PRIMED AND TOP COATED IAW SRM 51-10-04 AND AMM 51-10-00.

Part: STOP FITTING — CRACKED (FWD CARGO DOOR) · airframe 31,529 hrs · 31,500 cycles

FWD CARGO DOOR MID FWD STOP BRACKET IS CRACKED. REMOVED , LOCATED, DRILLED, AND INSTALLED A NEW BRACKET ALL IAW SRM 51-41-05, 51-40-08 AND DWG 5910141, REV FE, DIM OF CRACK 1.5".

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221AF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 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 9936544, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221FF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936547, REV W.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222BF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. REMOVED, FABRICATED A NEW FLOORBOARD AND INSTALLED IAW SRM 53-20-50 REPAIR 3, DWG NR 9936585, REV G, AND AMM 53-21-01.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221BF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936545, REV M.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222AGF IS DELAMINATED. FLOORBOARD 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 9936585, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222AMF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222AHF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 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 9936585, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222AAF IS DELAMINATED. FLOORBOARD FOUND TO BE 50 PERCENT DELAMINTED 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 9936640, REV D.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222ABF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 PERCNET 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 9936640, REV D.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222PF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 221UF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 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 9936585, REV G.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. FLOORBOARD FOUND TO BE 40 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 9936539, REV AB.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

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

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOORBOARD 222APF IS DELAMINATED. FLOORBOARD 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 9936585, REV G.

Part: DOOR FRAME — CORRODED (BS 994) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

AFT CARGO COMP DOOR JAMB BS 994 FRAME LOWER DOUBLER/TRIPLER SPLICE PLATES HAVE CORROSION. REMOVED SPLICE PLATES FROM AFT CARGO DOOR JAMB BS 994 AT DOUBLER/TRIPLER AND FABRICATED NEW SPLICES IAW SRM 53-20-15R-7, AND ALODINED, PRIMED, AND TOPCOATED IAW SRM 51-10-04, AMM 51-10-00, INSTALLED NEW SPLICES IAW SRM 51-41-05, AND 53-20-15 R-7.

Part: DOOR FRAME — CORRODED (BS 954) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

AFT CARGO COMPARTMENT DOOR JAMB FWD FRAME BS 954 LOWER DOUBLER, TRIPLER SPLICE PLATES HAVE CORROSION. REMOVED SPLICES PLATES AT AFT CARGO DOOR JAMB FWD FRAME BS 954, LOWER DOUBLER, TRIPLER AND FABRICATED NEW SPLICES PLATES IAW SRM 53-20-15-R-7 AND ALODINED AND PRIMED AND TOP COATED NEW SPLICES PLATES IAW SRM 51-10-04, AMM 51-10-00, INSTALLED NEW SPLICES PLATES IAW SRM 51-41-05 AND 55-20-15 R-7.

Part: CUSP WEB — CRACKED (BS 655) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN CUSP WEB LT SIDE HAS A CRACK AT BS 655. ASSOCIATED AA 5310-01436 ADDED FOR AC 9587. ASSOCIATED ER/A 14-544114 ADDED FOR AC 9587. REPLACED MAIN CABIN CUSP WEB LT SIDE BS 655 IAW SRM 51-41-02, 51-41-05, DWG NR 9910151, REV BV AND CG, ER/A 544114-14, REV 0, AND DELTA ER/A NR 544114-14, REV ORIGINAL.

Part: FITTING — CRACKED (BS 1053) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN BS 1053 LONGERON 15R DOOR FRAME FITTING CRACKED. REPLACED FITTING AT MAIN CABIN BS 1053, DOOR FRAME L-15R IAW SRM 51-41-02, DWG 3917624-511, REV EE, LENGTH OF CRACK WAS .500".

Part: FRAME — CRACKED (BS 1022 BULKHEAD) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN BS 1022, LONG 7L BULKHEAD FORMER CRACKED. INSTALLED REPAIRS PARTS IAW ERA 544111-14, REV "O". REPAIRED MAIN CABIN LONGERON 7L BULKHEAD FORMER IAW ER/A 544111-14 REV ORIGINAL, BY FABRICATING -1 AND -2 REPAIR ANGLE, TAPER SHIM, AND FILLER. INSTALLED ALL REPAIR PARTS IAW SRM 51-41-05 AND ER/A 544111-14, REV O, LENGTH OF CRACK 1.1". ASSOCIATED ER/A 14-544111 ADDED FOR AC 9587.

Part: CUSP WEB — CRACKED (BS 717-724) · airframe 31,529 hrs · 31,500 cycles

RIGHT CUSP WEB SECTION FOUND TO HAVE TWO CRACKS BS 717 - 724. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4, FIG 204 AND SRM 51-41-02.

Part: CUSP WEB — CRACKED (BS 656-696) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN CUSP WEB LT SIDE CRACKED, BS 656, 674, AND 696. CUTOUT DAMAGE IAW SRM 53-00-55, REPAIR 4, FIG 226. FABRICATED A REPAIR AND INSTALLED IAW SRM 53-00-55, REPAIR 4, FIG 226.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN FLOOR PANEL 222ZF CRACKED. CUTOUT CRACKED AREA ON MAIN CABIN FLOOR PANEL IAW SRM 53-20-50, REPAIR 2 AND 53-20-50. FABRICATED A REPAIR DOUBLER, FILLER AND INSTALLED REPAIR IAW SRM 53-20-50, REPAIR 2.

Part: CUSP WEB — CORRODED (BS 208-215) · corrosion level 2 · airframe 31,529 hrs · 31,500 cycles

CORROSION FOUND AT CUSP WEB SKIN APPROXIMATELY FROM BS 208 TO BS 215 AND RBL 56. INSTALLED EWIS PROTECTION IAW AMM 20-30-00, REMOVED CUSP WEB IAW SRM 51-40-02, DUE TO 100 PERCENT MATERIAL LOSS, LOCATED, AND DRILLED AND DEBURR NEW CUSP WEB IAW SRM 51-40-08. ALODINED & PRIMED IAW SRM 51-10-04 HOLES, INSTALLED NEW CUSP WEB IAW SRM 51-40-02 AND DWG NR 9930538, REV CC, CF. REMOVED EWIS PROTECTION IAW AMM 20-30-00.

Part: SUPPORT FITTING — CRACKED (BS 737) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN TANK BS 737, RBL 44. SEAT TRACK SUPPORT FITTING CRACKED. REMOVED CRACKED SEAT TRACK SUPPORT FITTING AT STR 737, RBL 44, IAW SRM 51-41-05. LOCATED, DRILLED, AND DEBURRED NEW SUPPORT IAW SRM 51-40-08. ALODINED AND PRIMED NEW HOLES IAW 51-10-04. INSTALLED NEW SUPPORT FITTING IAW SRM 51-41-05. INSTALLED AND REMOVED EWIS PROTECTION IAW AMM 20-30-00.

Part: SUPPORT FITTING — CRACKED (BS 737) · airframe 31,529 hrs · 31,500 cycles

MAIN CABIN BS 737, LBL 44 SEAT TRACK SUPPORT FITTING CRACKED. REPLACED MAIN CABIN CENTER WING TANK BS 737, LBL 44 SEAT TRACK SUPPORT FITTING IAW SRM 51-41-02 AND SRM 51-41-05.