N7816B

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 66,080 hrs · 30,273 cycles

SUPPLEMENTAL INFORMATION: FWD SAC DOOR SLIDE LOOSE ; / [01] COMPLETED INSPECTION OF FWD SVC DOOR SLIDE. REPOSITIONED GIRT BAR IN SLIDE APRON. REF AMM 25-66-01

Part: RETAINER — BROKEN (R1 GIRT BAR) · airframe 64,603 hrs · 29,425 cycles

GIRTBAR RETAINER ON FORWARD SERVICE DOOR BROKEN ; / RESECURED GIRTBAR RETAINER ON FWD SRV DOOR WITH 2 NEW RIVETS REF SRM 51-40-02. <BR>REF MT 725-61--06FOR SLIDE REMOVAL ANFD INSTALLATION TO FOM<BR>E136889

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,949 hrs · 29,044 cycles

AFT SERVICE DOOR SLIDE GIRT BINDS IN DOOR WHEN CLOSING / RETUCKED AFT SERVICE DOOR SLIDE GIRT 2 - FOLD USING HAND PRESSURE. GIRT NOW CLEARS SCUFF PLATE WHEN CLOSING DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,949 hrs · 29,044 cycles

EMERGENCY ISLE ILLUMINATION LIGHT AT BIN 6 LH DOES NOT ILLUMINATE / RELAMPED AND REPLACED LENS OF ROW 6 LH EMERGENCY AISLE ILLUMINATION LIGHT PER AMM 33-51-03-960-801 AND PERFORMED A GOOD INSTALLATION TEST OF ROW 6 LH EMER LIGHT PER AMM 33-51-03-960-801

Part: DEPRESSOR — CRACKED (R1 DOOR SEAL) · airframe 63,949 hrs · 29,044 cycles

FSD CUTOUT FWD FRAME UPPER SEAL DEPRESSOR IS CRACKED BETWEEN WL 220 TO 230 / REMOVED & REPLACED FSD CUTOUT FWD FRAME UPPER SEAL DEPRESSOR BETWEEN WL220 TO WL230. PER SRM 51-40-02-0G-0 & IPC 53-11-00-80 PO#814612

Part: STUB FRAME — CRACKED (R1 DOOR) · airframe 63,949 hrs · 29,044 cycles

FWD SERVICE DOOR CUTOUT UPPER STUB FRAME IS CRACKED / REMOVED AND INSTALLED NEW FSD UPPER STAB FRAME; ALL WORK ACCOMPLISHED ON CUSTOMER CARD # U271289. SA-M 326 # A1289821

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 63,949 hrs · 29,044 cycles

VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BS 1090-1120 LT SIDE / REMOVED & REPLACED L/H VERTICAL STAB TO FUSELAGE SKATE ANGLE FROM BS1016-BS1132 PO#809203 PER SRM 51-40-02 & DWG# 148A8310

Part: SIDEWALL PANEL — CRACKED (CABIN) · airframe 63,949 hrs · 29,044 cycles

FWD SERVICE DOOR ; FWD SURROUND SIDEWALL PANEL IS CRACKED AT THE ELECTRICAL OUTLET CUTOUT / REPAIRED FWD SERVICE DOOR; FWD SURROUND PANEL IAW AMM 25-00-00-300-801 STEP 2.I. 59310U 01FEB21

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

CORROSION MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACKS AT BS 727B-887; L.BL 24.5; WL 208.1.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

DURING INSPECTIONS ON CUSTOMER CARD 15021 A 1 INCH CRACK IN THE BEAR STRAP WAS NOTED AT BS 294. THREE INCHES BELOW STR 8R. ENGINEERING DISPOSITION REQUIRED.

Part: ATTACH BRACKET — BROKEN (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

ROD ATTACH BRACKET IS BROKEN; LOCATED 5' O/B OF O/B HINGE FOR ACCESS PANEL 551DB / REMOVED AND INSTALLED NEW COLLARS (2) AND ROD ATTACH BRACKET LOCATED 5' O/B OF O/B HINGE FOR ACCESS PANEL 551DB IAW SRM 51-40-02-0G-0 57015U 08FEB21

Part: RETAINER — CRACKED (LT WING SEAL) · airframe 63,949 hrs · 29,044 cycles

LH WING FIXED SEAL RETAINER IS CRACKED AT UPPER FLANGE; ORSS 272; AFT OF LH PYLON TRAILING EDGE FAIRING / REMOVED & REPLACED L/H WIND FIXED SEAL RETAINER AT UPPER FLANG; ORSS 272 AFT OF L/H PYLON TRAILING EDGE FAIRING IAW SRM 51-40-02-0G-0 & DWG # 115A2930

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 63,949 hrs · 29,044 cycles

***CORROSION*** MULTIPLE AREAS OF CORROSION GOUGES ON PASSENGER CABIN SEAT TRACKS AT B.S. 727B-887; R.B.L. 45; W.L. 208.1. / REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK AT BS727B TO 887; RBL45; WL208.1 PER SRM 51-40-02-0G-0 AND BOEING DWG #146A5300

Part: SEAT TRACK — CORRODED (PASS CABIN) · airframe 63,949 hrs · 29,044 cycles

CORROSION MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACKS AT BS 727B-887; LBL. 45; WL. 208.1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 TO L.B.L. 24.5; W.L. 208.1. / REMOVED AND REPLACED FLOOR SUPPORT AT B.S.540 B.L.0. LBL24.5 W.L.208.1 IAW SRM 51-40-02-0G-0 & SRM 51-40-05 & DWG 143A5240

Part: STRINGER — CRACKED (ZONE 100) · airframe 63,949 hrs · 29,044 cycles

CRACKED STRINGER AT B.S. 540; STRINGER 23 LEFT. / CRACKED STRINGER AT BS 540; STRINGER 23 LEFT REPAIRED IAW ATS ER 21-01193 REV IR. AND PER EA NO:21-153-00353 REV IR. 55981U 11FEB21

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

CORROSION ON FUSELAGE SKIN AT BS 860-1016; LBL 14 TO RBL 14; WL 306.

Part: FASTENER — CRACKED (#2 ENGINE) · airframe 63,949 hrs · 29,044 cycles

SEVERAL FASTENERS PULLING THROUGH ONE FASTENER CRACKED 6 O'CLOCK POSITION #2 ENGINE INLET / REPAIRED SEVERAL FASTENERS PULLING THROUGH AND ONE FASTENER CRACKED AT 6 O'CLOCK POSITION ON #2 ENGINE INLET PER SRM 54-10-01-1A-2 ALLOWABLE DAMAGE 2.

Part: FLOOR SUPPORT — BENT (ZONE 100) · airframe 63,949 hrs · 29,044 cycles

SUPPORT INTERCOSTAL IS BENT AT BS 500D+8 LBL 7; WL 156 / REMOVED AND REPLACED INTERCOSTAL SUPPORT AT BS 500D TO 520 WL156 PER SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,949 hrs · 29,044 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR # 4 (LOWER) BEAM WAS REPLACED ON WORK ORDER: 537115.

Part: NUT PLATE — BROKEN (ZONE 100) · airframe 63,949 hrs · 29,044 cycles

NUT PLATE BROKEN AT BS 494 AT STRINGER 24R / REMOVED AND REPLACED NUT PLATE AT BS 494 STRINGER 24R FCB IAW AMM INTRODUCTION STEP 2SIP AND DWG 143A8321

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,949 hrs · 29,044 cycles

***CORROSION*** ON INTERCOSTAL SUPPORT CHANNEL FWD O/B CORNER BS 260 LBL 3 WL 208 / REMOVED AND REPLACED INTERCOSTAL SUPPORT CHANNEL BS360 TO BS270 LBL3 WL208 PER SRM 51-40-02; SRM 51-40-05 AND DWG 141A5210

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 63,949 hrs · 29,044 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR DENT AT BS 255; RBL 4 - LBL 14; WL 207; PER SWA EA 1-A53-33179 REV 1

Part: PANEL — DENTED (NR 2 NACELLE) · airframe 63,949 hrs · 29,044 cycles

#2 ENGINE INLET COWL OUTER BARREL PANEL HAS DENT WITH GOUGE AT 3 O'CLOCK POSITION 8 INCHES FORWARD OF PANEL AFT EDGE / REPAIRED #2 ENGINE INLET COWL BARREL PANEL DENT WITH GOUGE PER SRM 54-10-01-2R-6 REPAIR 6

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,913 hrs · 29,020 cycles

GIRT BAR TAB HANGING TO LOW AFT SERVICE DOOR. REPOSITIONED AFT SERVICE DOOR SLIFE, PER SWA MT 725-61-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,446 hrs · 28,119 cycles

AFT EMERG. BATTERY PACK INOP / R/R AFT EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CK. GOOD.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 62,396 hrs · 28,089 cycles

R2 DOOR SLIDE LOOSE / SECURED R2 DOOR SLIDE REF MT 725-61-06; AMM 25-66-01

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,151 hrs · 27,929 cycles

"Z" FOLD HAS COME OUT OF CONTAINER AT LH AFT SLIDE GIRT REPOSTIONED L2 SLIDE THAT IS HOOKED TO THE GERT BAR REF MM 25-66-01 (DID NOT REMOVE SLIDE FROM COVER) REF SA-M 767 H24793-3

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 60,841 hrs · 27,092 cycles

EXIT DOOR SIGN ARROW POINTED AWAY FROM DOOR. / R&R LENS PER AMM.

Part: SPLICE — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,081 hrs · 25,956 cycles

R/H OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. / FOUND JIFFY SPLICE D11076 DISCONNECTED. CONNECTED SPLICES IAW AMM & WDM.

Part: TRACK — DEFECTIVE (AFT CARGO COMPT) · airframe 59,081 hrs · 25,956 cycles

DTIP- PREVIOUS OPERATOR; F000888; SPLICE REPAIR ON AFT CARGO COMPARTMENT FLOOR TRACK REPAIR SPLICE AT LBL 17.2 BS 767+11-787+13 REQUIRES REPLACEMENT DUE TO FASTENER COUNT 4 VERSUS 5 AND THICKNESS OF THE LOWER FLANGE OF THE TRACK SPLICE 0.080' VERSUS 0.090' IN ADDITION TO FASTENER SPACING IS BELOW THE MINIMUM OF .750' / REMOVED AND REPLACED CARGO TRACK STA 865 TO STA 756 LBL 17.2 PER DWG 146A7500 REV B. ACCOMPLISHED CARGO TRACK SPLICE REPAIR AT STA 756 PER SRM 53-00-53-2R-3

Part: RETAINER — CRACKED (LT WING) · airframe 59,081 hrs · 25,956 cycles

LEFT WING MIDSPAN FIXED TRAILING EDGE BULKHEAD AFT VERTICAL CURVED SEAL RETAINER IS CRACKED WITH PIECE BROKEN OFF / REMOVED AND REPLACED SEAL RETAINERS IAW B737 AIPC 57-50-00-25 AND B737 SRM 51-40-02-0G-0

Part: CREASE BEAM — OUT OF TOLERANCE (MAIN CABIN) · airframe 59,081 hrs · 25,956 cycles

DTIP PREVIOUS OPERATOR STRAP REPAIR (T402405) ON RH PASSENGER CABIN CREASE BEAM FROM BS 650 TO 673 - REQUIRES REPLACEMENT / PREVIOUS REPAIR AT STA 650-673 IAW EA 190095 IR AND SWA EA 1-753-34321 REV IR DATED 25MAR19.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 59,081 hrs · 25,956 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, RBL 41. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 59,081 hrs · 25,956 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, LBL 31, AT FORWARD SECTION OF BEAD. / REPAIRED DECK IAW EA AND SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

FLOOR SUPPORT L-ANGLE ATTACH WEB CRACKED AT BS 540, BETWEEN LBL 26 TO LBL 45. R&R SUPPORT BREAK ASSEMBLY IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

CABIN FLOOR STRUCTURE RT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 716 TO BS 727. R&R RT CREASE BEAM WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

CIRCUIT BREAKER ATTACH ANGLE CRACKED IN RADIUS AT BS 259.5+1.5, STR 8L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

COMMON TO STRINGER CIRCUIT BREAKER ATTACH ANGLE CORRODED AT BS 259.5+1.5, STR 12L, SLOTTED HOLE. R&R STRINGER CLIP IAW SRM AND DWG.

Part: PANEL — ELONGATED (VERT. STAB.) · airframe 59,081 hrs · 25,956 cycles

VERTICAL STABILIZER PANEL 322A HAS ELONGATED HOLE. MARKED. / VERTICAL STAB PANEL 322 A HAS ELONGATED HOLE EVALUATED HOLE SIZE AS .450' MAX ALLOWED HOLE SIZE = .312' IS OUT OF LIMITS IAW 737-700 SRM 51-40-0G-05-0 FIG 3 VERIFIED NEW VERTICAL STAB PANEL 322 A AS P/N 176A3009U9 IAW 737-700 AIPC 65-33-11-02 AND A TAG WN3941 PICKED UP HOLES IN NEW PANEL 322 A IAW 737-700 SRM 51-40-05-0G-0 *ABOVE PANEL WILL BE INSTALLED ON JPANEL-320-CLOSE SN # 1388 WO # 38939-3300-0015*

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

STUB FRAME CRACKED AT BS 294, WL 208, COMMON TO INNER CREASE BEAM ANGLE. R&R STUB FRAME IAW DWG AND SRM.

Part: ATTACH ANGLE — CRACKED (MAIN CABIN) · airframe 59,081 hrs · 25,956 cycles

PASSENGER CABIN; STA 294; FLOOR LINE; ATTACH ANGLE CRACKED IN RADIUS; COMMON TO CREASE BEAM WEB AND CREASE BEAM INNER CORD / REMOVED AND REPLACED PASSENGER CABIN STA 294; FLOOR LINE ATTACH ANGLE COMMON TO CREASE BEAM WEB AND INNER CHORD IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 SHT 1 REV: D ATAG# 141831203 A06555

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 727 TO STA 747+15; LBL 21; Z-ANGLE HAS CORROSION / AFT CARGO LH Z-ANGEL REPLCED ON WORK CARD X896022. Z-ANGE REPLACED FROM STA 727-847

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

CENTER CABIN INBOARD RAIL ATTACH FASTENER CRACKED AT BS 827, STR 8L. REPAIRED FRAME IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED AT BS 947, LBL 13, AFT BULKHEAD. R&R BRACKET IAW SRM.

Part: BAFFLE — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 727A+19; LBL 23; BAFFLE ANGLE HAS CORROSION ON LOWER SURFACE UNDER NUTPLATE / REMOVED AND EVALUATED CORROSION ORIGINAL THICKNESS .045' LOSS OF .011' WITH .034' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 REMOVED AND REPLACED BAFFLE STA 727A - 727B LBL 23 PART # 146A7505-1 PER SRM 51-40-02-0G-0 AND DWG 146A7500 REV B

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO FLOOR PANEL 140CF HAS CORROSION AROUND PERIMETER OF PANEL / PANEL 14OCF REPLACED ON CARD # X895804

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 767 TO 794; RBL 24; SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED AND EVALUATED CORROSION. ORIGINAL THICKNESS .051' LOSS OF .011' WITH .040' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO FWD SHILED PART # 146A8127-1 PER SRM 51-40-02-0G-0 AND DWG 146A0081 REV C P/N 146A8127-1 ATAG # WN1704

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 787+5; STR 24L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 792 STR 24L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 AND AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED PLATE P/N 146A9403-13 AND VERIFIED IT CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 24L IAW SRM 51-40-02-0G-0 AND BOEING 146A9401 REV D.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO, FLOOR SUPPORT RAIL CORRODED AROUND NUTPLATE HOLES BETWEEN BS 794 TO BS 847, RBL 14. R&R CARGO TRACK PER DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 787; STR 23L TO 25L; SIDEWALL SUPPORT ANGLE HAS CORROSION AT NUT PLATE HOLES / SIDEWALL SUPPORT ANGLE (-89) DOES NOT HAVE ENTRIES IN SRM. PART REPAIRABLE BY REPLACEMENT. PE SRM 51-10-02-0G-0 STEP 9.C. REMOVED AND REPLACED ANGLE PER SRM 51-40-02-0G-0 AND DWG 146A1262 REV -. ANGLE PART# 146A9403-89 P/N 146A9403-89

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 787+5; STR 22L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 792 STR 22L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW BOEING DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 AND AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED PLATE P/N 146A9403-13 CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 22L IAW SRM 51-40-02-0G-0 AND BOEING 146A9401 REV D.

Part: CHANNEL — CORRODED (MAIN CABIN) · airframe 59,081 hrs · 25,956 cycles

PAX CABIN LH SIDE AT STA-616 TO STA-639 AT STR-7L CHANNEL ASSY. IS CORRODED AT BOTH ENDS AND IN LIGHTENING HOLES. / REMOVED CHANNEL ASSY AT PASSENGER CABIN L/H SIDE AT STA 616 TO STA 639 STR 7L IAW B737-700 DWG 412A2250 REV: -; SRM 51-40-02-0G-0 AND INSTALLED CHANNEL. EA 190189 P1 CANCELLED ATAG # A24409

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO; STA 787+5; STR 23L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 787 STR 23L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW BOEING DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 A+D AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION ON PLATE P/N 146A9403-13 AND VERIFIED IT CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 23L IAW SRM 51-40-02-0G-0 AND 146A9401 REV D.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO STA 727 TO 767; RBL 21; Z-ANGLE HAS CORROSION / REMOVED AND EVALUATED CORROSION. ORIGINAL THICKNESS .040' LOSS OF .015' WITH .025' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO RH Z-ANGEL STA 727-767 PER SRM 51-40-02-0G-0 AND DWG 146A7502 REV A

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO Z-ANGLE CORRODED BETWEEN BS 747+15 TO BS 807+5, LBL 21. R&R AFT CARGO Z-ANGLE PER SRM.

Part: FLAP — DELAMINATED (R/H WING) · airframe 59,081 hrs · 25,956 cycles

RIGHT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE CORNER HAS EVIDENCE OF DELAM / REPAIRED R/H WING O/B FLAP; I/B CORNER ON UPPER SURFACE OF SKIN IAW SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-0

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

FORWARD CARGO PIT L/H BAFFLE CLIP FORWARD SIDE OF STA 500C LBL25 IS CRACKED / REMOVED INTERCOSTAL FROM STA 500B-500C LBL25 IAW SRM 51-40-02-09-0. REMOVED CLIP IAW SRM 51-40-02-09-0. RECEIVED NEW CLIP P/N 143A75024159 ON ATAS #A56050 IAW BOEING DWG#143A7505 REV A. LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05-09-0 AND BOEING DWG #143A7505 REV A. INSTALLED NEW CLIP FWD CARGO AT STA 500C LBL25 IAW BOEING DWG#143A7505 REV A. INSTALLED INTERCOSTAL AT STA 500B-500C LBL25 IAW BOEING DWG#143A7505 REV A. A TAG# A56050

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

FORWARD CARGO PIT LT BAFFLE CLIP AFT SIDE OF FRAME CRACKED AT BS 400, LBL 25. R&R CLIP IAW SRM & DWG.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,081 hrs · 25,956 cycles

PAX CABIN FLOOR 231XF HAS MISSING FIBERS ON UPPER SURFACE / REPAIRED PAX CABIN FLOOR 231XF UPPER SURFACE IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 66

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO COMPARTMENT THRESHOLD; FWD OF DOOR; FLOOR TIE DOWN PLATE CORRODED / REPLACED PARTS ON TABLE P/N 450A1611-1 ON ATAG# A02816 IAW IPC 25-52-10-02P/N 456A2611-1 ATAG# A02816

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

FORWARD CARGO PIT DOOR SURROUND AFT SHIELD ON UPPER AND LOWER SURFACE CORRODED BETWEEN BS 492 TO BS 500A, RBL 24. R&R SHIELD IAW SRM & DWG.

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

AFT CARGO COMPARTMENT THRESHOLD; AFT OF DOOR; FLOOR TIE DOWN PLATE CORRODED / REPLACED PART ON TABLE 143A2611-2 ON ATAG #A69675 IAW IPC 25-52-10-02

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,081 hrs · 25,956 cycles

FORWARD CARGO PIT LT BAFFLE CLIP FORWARD SIDE CRACKED AT BS 500B, LBL 25. R&R CLIP IAW SRM & DWG.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 59,081 hrs · 25,956 cycles

FORWARD CARGO PIT L/H BAFFLE CLIP AFT SIDE OF STA 500C LBL25 IS CRACKED / REMOVED CLIP FWD CARGO STA 500C LBL 25 IAW SRM 51-4-02-09-0. RECEIVED NEW CLIP P/N -143A750245 ON A TAG# A17245 IAW BOEING DWG #143A7505 REV. A LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05-09-0 AND BOEING DWG #145A7505 REV A. INSTALLED NEW CLIP FWD CARGO AT STA 500C LBL 25 IAW BOEING DWG #143A7505 REV A. A TAG# A17245

Part: FAIRING — CRACKED (RT WING) · airframe 59,081 hrs · 25,956 cycles

RH OVER WING TO BODY FAIRING 195CR FWD EDGE AT RADIUS HAS CRACK / REPAIRED RH OVERWING TO BODY FAIRING 195CR EDGE AT RADIUS IAW B737-700 SRM 53-60-70-2R-1 REPAIR 1 REV 66

Part: LENS — MISSING (CABIN) · airframe 59,081 hrs · 25,956 cycles

CABIN SIDEWALL PANEL 231YHW MISSING ESCAPE LENS. R&R SIGN LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,612 hrs · 25,630 cycles

LT OVERWING EXIT SIGN INOP. R&R BATTERY PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,612 hrs · 25,630 cycles

RT OVERWING EXIT SIGN INOP. R&R BATTERY PER AMM.

Part: FAIRING — DELAMINATED (RIGHT WING) · airframe 58,486 hrs · 25,549 cycles

#6 FLAP TRACK FAIRING TAILCONE SEPERATING;MULTIPLE LOOSE FASTENERS / REPLACED FLAP TRACK FAIRING TAILCONE (#6) IAW AMM 27-51-28

Part: NONE — DELAMINATED (R/H WING) · airframe 58,276 hrs · 25,411 cycles

SUPPLEMENTAL INFORMATION: R/H WING; I/B MAIN FLAP O/B LOWER SKIN IS SEPARATED; 23.5' W X 10.0' D / REMOVED AND REPLACED R/H I/B T/E FLAP WEDGE MPN 113A2500-14 ATAG WN5499 IAW BOEING DWG 113A2100 REV B737-700 SRM 51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 57,276 hrs · 24,766 cycles

EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 15 DEF. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 57,276 hrs · 24,766 cycles

EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 16 DEF. R&R BATTERY PER MM.

Part: PANEL — CRACKED (LT HORIZ STAB) · airframe 57,276 hrs · 24,766 cycles

TAIL LEFT ELEVATOR BAY #3 BALANCE BAY PANEL VERTICAL SIDE CRACKED UPPER RIGHT SIDE NEAR HINGE ASSY. / REMOVED AND REPLACED CRACKED PANEL ON L/H ELEVATOR #3 BALANCE BAY PANEL AND HINGE ASSY PER SRM 51-10-02. INSTALLED L/H ELEVATOR #3 BALANCE BAY PANEL AND HINGE ASSY PER AMM 27-31-41

Part: BATTERY — FAILED (CABIN) · airframe 57,276 hrs · 24,766 cycles

EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 6 DEF. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 57,276 hrs · 24,766 cycles

EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 3 DEF. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 57,276 hrs · 24,766 cycles

EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 1 ABC. R&R BATTERY PER MM.

Part: STOP — BROKEN (R1 DOOR GIRT BAR) · airframe 55,991 hrs · 23,978 cycles

R1 DOOR SLIDE GIRT BAR STOP BROKEN. INSTALLED A GIRT BAR STOP IAW MT.

Part: SWITCH — FAULTY (L1 DOOR) · airframe 55,560 hrs · 23,711 cycles

AIR TURNBACK, LEFT OVERWING LIGHT ILLUMINATED DURING TAKE OFF ROLL. CLIMBED TO 19,000 FEET PRESSURIZATION ABNORMALITY FELT. R&R FORWARD EMERGENCY EXIT DOOR INDICATION SWITCH.

Part: SWITCH — FAULTY (L1 DOOR) · airframe 55,560 hrs · 23,711 cycles

AIR TURNBACK, LEFT OVERWING LIGHT ILLUMINATED DURING TAKE OFF ROLL. CLIMBED TO 19,000 FEET PRESSURIZATION ABNORMALITY FELT. R&R AFT EMERGENCY EXIT DOOR INDICATION SWITCH.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 55,270 hrs · 23,534 cycles

R/H WING FIXED TRAILING EDGE UPPER PANEL ABOVE #2 PYLON AFT FAIRING HAS CRACKED VERTICAL SEAL RETAINER / R/R RETAINER IAW SRM 51-40-02.

Part: LENS — MISSING (CABIN) · airframe 54,657 hrs · 23,154 cycles

LT EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 9. INSTALLED LENS PER SIP.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 54,649 hrs · 23,150 cycles

DECLARED EMERGENCY, TRAILING EDGE FLAPS DID NOT EXTEND PAST 5 DEGREES WHEN FLAP LEVER WAS PLACED TO 15 AND 30 DEGREES ALTERNATE FLAP SWITCH USED TO EXTEND FLAP TO 15 DEGREES. R&R RIGHT FLAP POSITION TRANSMITTER PER AMM.

Part: SIGN — DETACHED (CABIN) · airframe 54,004 hrs · 22,745 cycles

AFT GALLEY EMERGENCY EXIT SIGN PARTIALLY DETACHED FROM CEILING. R&R SIGN PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 53,908 hrs · 22,691 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. INSTALLED LENS IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 52,693 hrs · 21,975 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE ON BOTTOM. SECURED THE SLIDE IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 52,693 hrs · 21,975 cycles

L2 DOOR SLIDE LOOSE ON BOTTOM. SECURED SLIDE IAW MT.

Part: SIDEWALL SUPPORT — CORRODED (BS 500-500D) · airframe 52,693 hrs · 21,975 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 - 500D, LBL 23. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500-500A) · airframe 52,693 hrs · 21,975 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 - 500A, RBL 23. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT ANGLE CRACKED AT BS 727A+6. R&R SUPPORT IAW SRM AND DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH CLIP CORRODED AT BS 768, RBL 25. R&R ATTACH CLIP IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY RT FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 847-867) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 847 - 867, RBL 25. R & R THE SHIELD IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 767-847) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO 847, LBL 25. R & R SIDWALL SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,693 hrs · 21,975 cycles

LT FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 867-947) · airframe 52,693 hrs · 21,975 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 - 947, RBL 25. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,693 hrs · 21,975 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 52,693 hrs · 21,975 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SRM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 51,685 hrs · 21,392 cycles

FORWARD GALLEY FLASH LIGHT STRAP BROKEN. R&R STRAP IAW SIP.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,459 hrs · 21,248 cycles

R1 DOOR EXIT SIGN AT FLOOR LEVEL INOPERATIVE. R & R THE SIGN IAW MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 51,154 hrs · 21,068 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOOK LOOSE. R & R HOOK ASSY IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,523 hrs · 20,708 cycles

FORWARD NR 2 EMERGENCY FLASHLIGHT STATUS LIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: BRACKET — BROKEN (R1 DOOR) · airframe 48,737 hrs · 19,654 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR BRACKET BROKEN. R & R BRACKET IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,848 hrs · 18,540 cycles

L1 DOOR EMER EVAC SLIDE LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,848 hrs · 18,540 cycles

R2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — DIRTY (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT LENS DIRTY, FWD AFT CARGO BAY. CLEANED LENS IAW AMM.

Part: WIRE — BROKEN (COCKPIT) · airframe 46,848 hrs · 18,540 cycles

DOME LIGHT BEHIND PILOTS SEAT GOING TO EMER EXIT LIGHT FIXTURE, WIRE BROKEN. R & R LIGHT IAW AMM.

Part: BATTERY PACK — OUT OF ADJUST (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT STOW BIN EMER EXIT LIGHT INOPERATIVE AT ROW 12. ADJUSTED BATTERY PACK IAW AMM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

AFT CARGO BAY FLOOR STRAP CORRODED AT BS 727D+5.6 BETWEEN LBL 20 - RBL 20. R & R STRAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,848 hrs · 18,540 cycles

LEFT WING OTBD AFT FLAP OTBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

WHILE WORKING LT FILLET FAIRING MOD FOUND WEB ASSEMBLY TO BE CRACKED. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

RIGHT CREASE BEAM WEB CORRODED AT BS 685, LOWER SURFACE NUTPLATE HOLE. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 639 - 663, LOWER SURFACE NUTPLATE HOLES. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

LEFT CREASE BEAM WEB CORRODED AT BS 685, LOWER SURFACE NUT CLIP HOLE. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

LEFT CREASE BEAM INNER CHORD CORRODED AT BS 650, UPPER SURFACE. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

AFT OF AFT CARGO BAY INTERCOSTAL CORRODED AT FWD SIDE OF FRAME BS 967.5, STRINGER 24R. R & R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

AREA AFT OF AFT CARGO BAY ON SUPPORT ANGLE CORRODED AT BS 967.5, BETWEEN STRINGER 27L - 27R. R & R ANGLE IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

RIGHT CREASE BEAM ANGLE CORRODED AT BS 698. R & R ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

LEFT CREASE BEAM INNER CHORD CORRODED AT BS 639, UPPER SURFACE. R & R CREASE BEAM IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

AFT OF AFT CARGO BAY ON FRAME INNER FLANGE CORRODED AT BS 986.5, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

LEFT CREASE BEAM INNER CHORD CORRODED AT BS 727, UPPER SURFACE. REPAIRED CHORD IAW SRM.

Part: FITTING — CORRODED (RT WING) · airframe 46,848 hrs · 18,540 cycles

RIGHT WING SPAR FWD TRUNNION FITTING UPPER & LOWER INBD & OTBD BORE CHAMFERS CORRODED. REPAIRED FITTING IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727 - 847, LBL 22. R & R ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FRAME CORRODED AT BS 727D, STRINGER 23L. REPAIRED FRAME IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FRAME TO FLOOR SUPPORT ANGLE CRACKED AT BS 827, RBL 20. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 - 767, RBL 22. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FRAME TO FLOOR SUPPORT ANGLE CRACKED AT BS 807, RBL 20. R & R ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 25. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 45. REPAIRED FLANGE IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE SKIN EXTERNAL SURFACE DAMAGED UNDER FWD END OF DORSAL FIN BETWEEN BS 855 - 873, BETWEEN LBL 4 TO RBL 4. REPAIRED SKIN IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

STRINGER CLIP CRACKED AT BS 480+15, STRINGER 24L. R & R CLIP IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

INTERCOSTAL WEB CORRODED AT BS 990, STRINGER 20L. R & R WEB IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 46,848 hrs · 18,540 cycles

LEFT WING NR 6 FLAP TRACK CANOE FAIRING CRACKED AT THE NR 10 FASTENER HOLE AFT END OF LOCATION. REPAIRED FAIRING IAW SRM & EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 46,848 hrs · 18,540 cycles

LEFT WING NR 6 FLAP TRACK CANOE FAIRING CRACKED AT THE NR 13 FASTENER HOLE AFT END OF LOCATION. REPAIRED FAIRING IAW SRM & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

BULKHEAD TO FLOOR WEB CORRODED AT BS 1016, BETWEEN RBL 17 - 27. R & R WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FLOOR BULKHEAD WEB CRACKED AT BS 1016, RBL 35. R & R WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

BULKHEAD TO FLOOR WEB CORRODED AT BS 1016, BETWEEN RBL 8 - 16. R & R WEB IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,848 hrs · 18,540 cycles

R1 DOOR EMER EVAC SLIDE Z FOLD OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: CAP — MISSING (L2 DOOR) · airframe 46,848 hrs · 18,540 cycles

L2 DOOR EMER EVAC SLIDE CASE END CAP ON BUMPER MISSING. R & R END CAP IAW SRM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11326 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT CONNECTOR D11336 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11100 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11088 DAMAGED. R & R D11088 IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT CONNECTOR D11332 DAMAGED. R & R CONNECTOR IAW WDM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11330 DAMAGED. R & R CONNECTOR IAW WDM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT CONNECTOR D11102 DAMAGED. R & R CONNECTOR IAW WDM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11342 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT EMER EXIT LIGHT CONNECTOR D11338 DAMAGED. R & R CONNECTOR IAW WDM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT CONNECTOR D11098 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: HOUSING — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

LEFT CEILING PANEL EMER EXIT LIGHT HOUSING DAMAGED AT BS 627. R & R LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,848 hrs · 18,540 cycles

RIGHT EMER EXIT LIGHT CONNECTOR D11328 DAMAGED. R & R CONNECTOR IAW WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN RBL 6 TO LBL 56. REPAIRED FLOORBEAM IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS 294, RBL 12. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 45 - 58, UPPER & LOWER SURFACE. REPAIRED FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 - 360, RBL 1. REPAIRED INTERCOSTAL IAW ER & EA.

Part: SKIN — CRACKED (RUDDER) · airframe 46,848 hrs · 18,540 cycles

LEADING EDGE OF RUDDER SKIN CRACKED NEAR NR 5 HINGE LOCATION ON RT SIDE. REPAIRED RUDDER IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,848 hrs · 18,540 cycles

FUSELAGE LOWER BULKHEAD CHORD CRACKED AT BS 540, STRINGER 22L, FWD HOLE 2ND FROM TOP. REPAIRED CHORD IAW ER & EA.