N746SW

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 75,665 hrs · 44,639 cycles

RT. OVERWING EXIT FLOURESCENT LIGHT INOP ; / [01] OK TO CONT. PER MEL 33-2-03 SP1 B AUTHORIZATION # <BR>26890; [02] R&R RT. OVERWING EXIT FLUORESCENT LIGHT BALLAST PER AMM 33-21-00; [03] WORK COMPLETED ON LP 1711356

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 75,665 hrs · 44,639 cycles

RT. OVERWING EXIT FLOURESCENT LIGHT INOP ; / [01] OK TO CONT. PER MEL 33-2-03 SP1 B AUTHORIZATION # <BR>26890; [02] R&R RT. OVERWING EXIT FLUORESCENT LIGHT BALLAST PER AMM 33-21-00; [03] WORK COMPLETED ON LP 1711356

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 74,496 hrs · 43,952 cycles

SF AND EA DOOR SLIDE PULL HANDLE SHOWING; ADJUSTED SLIDE PACK PER AMM 256601

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 74,496 hrs · 43,952 cycles

SF AND EA DOOR SLIDE PULL HANDLE SHOWING; ADJUSTED SLIDE PACK PER AMM 256601

Part: SKIN — CRACKED (ZONE 200) · airframe 74,284 hrs · 43,832 cycles

CHEM-MILL POCKET COMMON TO STR2R; STA 574-STA 578 APPPROX. INDACATES CRACKED PER NDT PART 6; 53-30-25 & PART 6; 53-30-18. / REAPIRED LEAK AT S-2R STA 574 TO STA 778 PER EA 21-153-00915.

Part: SKIN — CRACKED (ZONE 200) · airframe 74,284 hrs · 43,832 cycles

CHEM-MILL POCKET COMMON TO STR 1; STA 400-STA398 INDICATES CRACKED PER NDT PART6; 53-30-25 & PART6 53-30-18. / REPAIRED PER EA 21-153-00921 REV IR

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 74,212 hrs · 43,790 cycles

MECHANICAL DAMAGE ON PASSENGER CABIN SEAT TRACK LBL 45 BS 520 WL 208. / REMOVED AND REPLACED ON PASSENGER CABIN SEAT TRACK LBL 45 BS 520 WL 208 PER DWG 143A5300 REV:- AND SRM 51-40-02-0G-0; PER DWG 143A5034 REV: A; SRM 51-40-08-0G-0 SEAT TRACK REPLACED FROM BS 480 - 520 LBL 45 WL 208. 2398C 18MAR21

Part: ANGLE — CRACKED (CENTER WING) · airframe 74,212 hrs · 43,790 cycles

R/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT RBL8 WL167.68 / REPAIRED R/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 8 WL 167.68 PER ATS ER 21-01455 REV IR AND SWA EA # 21-157-00648 REV IR

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

***CORROSION*** ON UPPER SURFACE OF INTERCOSTAL BS 260- BS 268; LBL 11; WL 208 / 'DAMAGE REPAIRED PER EA 21-153-00781 REV IR (ATS ER 21-01445 REV IR); REFER TO NRC U279446 FOR TRACKING.'

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

STRINGER 24 RIGHT IS CRACKED AT B.S. 536. / REMOVED AND REPAIRED CRACKED STRINGER SECTION BS 536 STR. 24 R/H PER SRM 53-00-03-2R-1; SRM 53-00-03-1A-1

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

STRINGER 23 RIGHT IS CRACKED AT B.S. 536. / REPAIRED STR 23 RIGHT AT BS 536 PER ATS ER 21-01457 REV IR AND SWA EA# 21-153-00706 REV IR

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

***CORROSION*** ON UPPER SURFACE OF INTERCOSTAL BS 264- BS 268; RBL 11; WL 208 / 'DAMAGE REPAIRED PER EA 21-153-00781 REV IR (ATS ER 21-01445 REV IR). REFER TO NRC U279446 FOR TRACKING.'

Part: CREASE BEAM — CORRODED (BS 706-727) · airframe 74,212 hrs · 43,790 cycles

***CORROSION*** ON INBD CREASE BEAM CHORD AROUND FLOORPANEL HOLES AND INBD RADIUS BS 706-727 LBL64 WL 208 / CORROSION ON I/B CREASE BEAM CHORD; BS 706-727 LBL 64 WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-40-13-1A-1 REMOVED AND REPLACED I/B CREASE BEAM CHORD BS 670-727+3 PER SRM 51-40-02; SRM 51-40-05; MM 21-23-03; MM 20-60-07; MM 51-21-99 AND DWG# 144A5900 REV -

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

STRINGER 25 LEFT IS CRACKED AT B.S. 536. / REMOVED AND REPLACED CRACKED STRINGER SECTION BS 536 STR 25 LEFT PER SRM 53-00-03-2R-1. SRM 53-00-03-1A-1 APPLIED CTC TO REWORKED REPAIR AREA PER SRM 53-00-03-1A-1

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 74,212 hrs · 43,790 cycles

MECHANICAL DAMAGE TO SEAT TRACK AT BS 544 LBL25 WL 208 / REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK AT BS 540-727B LBL 25 WL 208 IAW DWG 144A5300 AND SOPM 20-50-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

CORROSION ON INBD CREASE BEAM CHORD AROUND FLOORPANEL HOLES BS 706727 RBL64 WL 208 CORROSION ON IB CREASE BEAM CHORD BS 706727 RBL 64 WL 208 FOUND TO BE OUT OF LIMITS PER SRM 5340131A1 REMOVED AND REPLACED IB CREASE BEAM CHORD BS 673 - 727+5' RBL 64 WL 208 PER SRM 514002; SRM 514005; MM 206007; MM 212303; MM 512191 AND DWG# 144A5900 REV

Part: WEB — CRACKED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

DURING COMPLETION OF CCN: 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK TO BE CRACKED AT RBL 42 BS 673 WL 201 AND WBL 41 BS 665 WL 201. / REMOVED DAMAGED PRESSURE WEB AND INSTALLED REPAIR PARTS AND PRESSURE WEB AT BS 663-675 RBL 30-60 WL 201 IAW SRM 53-40-51-2R-2 REP. 2.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 74,212 hrs · 43,790 cycles

***CORROSION*** ON UPPER SURFACE OF FWD; FLANGES OF FLOOR STRUCTURE AT COCKPIT FLOOR PANEL 211AF; LBL 11.2 TO RBL 11.2; STA 259 WL 208 / BS 259 AFT CHORD LBL 11 TO RBL 11 WL 208 REMOVED CORROSION BY BLENDING NO APPLICABLE REPAIRS PER SRM 53-10-51. REPAIRED PER ER 21-01445 REV IR & EA 21-155-00781 REV IR

Part: RETAINER — CRACKED (RT WING SEAL) · airframe 74,212 hrs · 43,790 cycles

RT WING UPPER T/E PANEL JUST AFT ON #2 PYLON; HORIZ. SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED R/WING UPPER T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IAW SRM 51-40-02-0G-0 PARA 4 AND SOPM 20-50-01.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 74,212 hrs · 43,790 cycles

RT HORIZ. STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED RT HORIZ. STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-801 AND 53-31-31-400-801; SOPM 20-50-01 59796C 5MAR21

Part: RETAINER — CRACKED (RT WING SEAL) · airframe 74,212 hrs · 43,790 cycles

RT WING UPPER T/E PANEL JUST AFT ON #2 PYLON; VERT SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED R/WING UPPER T/E PANEL JUST AFT OF #2 PYLON VERT SEAL RETAINER IAW SRM 51-40-02-0G-0 PARA 4 AND SOPM 20-50-01

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 74,212 hrs · 43,790 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 AT BS 255 RBL 4 - LBL 14 WL 208. AS PER EA 1-A53-33179 REV 1

Part: BARRIER — CRACKED (CENTER WING) · airframe 74,212 hrs · 43,790 cycles

R/H BS663 LOWER VAPOR BARRIER IS CRACKED BETWEEN RBL45 AND RBL55 WL161 / REMOVED AND REPLACED R/H BS 663 LOWER VAPOR BARRIER IAW SRM 51-40-02-0G-0; DWG 111A1000; AIPC 11-22-06-01

Part: WEB — CRACKED · airframe 74,212 hrs · 43,790 cycles

DURING COMPLETION OF CCN: 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK TO BE CRACKED AT LBL 31 BS 665 WL 201 / REMOVED DAMAGED PRESSURE WEB AND INSTALLED REPAIR PARTS AND PRESSURE WEB AT BS 663-675 LBL 26-60 WL 201 IAW SRM 53-40-51-2R-2 REP. 2.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,542 hrs · 43,403 cycles

LT EMERGENCY EXIT LIGHT INOPERABLE. RELAMP NO HELP. REMOVED AND REPLACED FLUORESCENT LIGHT BALLAST L751V AT LT EMERGENCY EXIT, REF WDM 33-21-12. OPERSATIONS CHECK NORMAL, REF AMM 33-20-00 W/AMT 24731.

Part: SIGN — LOOSE (CABIN) · airframe 73,293 hrs · 43,256 cycles

FLIGHT ATTENDANT REPORTS FWD EXIT SIGN NOT SECURE. R&R EXIT SIGN ASSEMBLY PER MM 33-51-01. OPERATIONS CK GOOD.

Part: DOOR — OUT OF ADJUST (EXTERNAL POWER) · airframe 73,280 hrs · 43,248 cycles

EXTERNAL POWER DOOR WILL NOT STAY LATCHED. ADJUSTED EXTERNAL POWER DOOR. OPERATIONS CHECK GOOD IAW AMM 52-49-02.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,778 hrs · 42,942 cycles

EXTERIOR EMERGENCY LIGHT AT THE FWD ENTRY DOOR WAS INOPERATIVE. REPLACED THE LAMPS AND TESTED GOOD IAW AMM 33-51-04-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,778 hrs · 42,942 cycles

EMERGENCY LIGHT OUT AT ROW 6 DEF. REPLACED THE LAMP AND TESTED GOOD IAW AMM 33-51-03-960-801.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 72,771 hrs · 42,936 cycles

FIRE ALARM AFT LAV WILL NOT SHUT OFF (SMOKE ALARM) / CLEARING DMA: 0412848 R&R AFT LAV SMOKE DET- ASSY PER AMM 26-14-01 CL# 34609 POS: AFT PN OFF:DU90-499 PN ON:474560-21 SN OFF: ------___SN ON:---------

Part: THRESHOLD — CRACKED (FWD CARGO) · airframe 72,759 hrs · 42,931 cycles

FWD CARGO CENTER THRESHOLD IS CRACKED / REMOVED AND REPLACED FWD CARGO CENTER THRESHOLD IAW AMM 53-11-02

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 72,759 hrs · 42,931 cycles

LEFT WING FIXED UPPER TE PANEL O/B OF #3 CANOE HORIZONTAL SUPPORT BRACKET IS CRACKED / R&R'D LEFT WING FIXED UPPER TE PANEL O/B OF #3 CANOE HORIZONTAL SUPPORT BRACKET REF SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 72,759 hrs · 42,931 cycles

CENTER RIGHT FLOOR SUPPORT AT STA 540 IS CRACKED / REMOVED AND REPLACED CENTER RIGHT FLOOR SUPPORT AT STA 540 IAW AMM 53-21-00 AND SRM 51-40-02

Part: BRACKET — CRACKED (LT WING) · airframe 72,759 hrs · 42,931 cycles

LEFT WING #2 SLAT I/B AUX TRACK COVER ON THE SLAT HAS AN ANGLE BRACKET CRACKED / R7R LEFT WING #2 SLAT I/B AUX TRACK COVER ANGLE BRACKET PER AMM 20-50-11.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 72,738 hrs · 42,919 cycles

ON DESCENT A. FA CALLED TO NOTIFY CREW THAT AFT SMOKE DETECTOR WAS SOUNDING OFF WITH NO OTHER INDICTAIONS AT ALL. / RESET SMOKE ALARM GREEN LIGHT SHOWS GOOD. PERFORMED AFT LAV SMOKE DETECTOR SELF TEST. TEST PASSED. REF AMM 26-14-00. INSPECTED LAV. NO DEFECTS NOTED. FIRE BOTTLE UNDER SINK WAS NOT DISTURBED. HEAT INDICATOR STRIP IS STIL GOOD. NO DEBRIS IN LAV WASTE CONTAINER

Part: COFFEEMAKER — ODOR (FWD GALLEY) · airframe 72,378 hrs · 42,694 cycles

DECLARED EMERGENCY-------------------------------------------------------ADVISE BY FLIGHT ATTENDANT THE SMELL OF BURNING IN FORWARD GALLEY. NO SMOKE NOTED. DECLARED EMERGENCY & LANDED. / R&R FORWARD COFFEE MAKER PER AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 72,178 hrs · 42,556 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 45. REPAIRED BARRIER IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,178 hrs · 42,556 cycles

EXTERIOR FUSELAGE SKIN CORRODED AT BS 350, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER SRM AND EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 72,178 hrs · 42,556 cycles

FORWARD BULKHEAD LOWER CORD CORRODED AT BS 1016, BETWEEN STR 25L TO STR 25R. R&R CHORD PER DWG AND SRM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,717 hrs · 40,989 cycles

RIGHT SIDE EMERG EXIT LOWER LIGHT LIGHT INOP / REPLACED EMERG LIGHT POWER SUPPLY AT R/H EMERG. EXIT IAW AMM

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,717 hrs · 40,989 cycles

LEFT SIDE EMERG EXIT LOWER LIGHT AND EXTERIOR LIGHT INOP / REPLACED EMERG. LIGHT POWER SUPPLY IAW AMM

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,717 hrs · 40,989 cycles

RIGHT SIDE EMERG EXIT EXTERIOR LIGHT INOP / REPLACED EMERG LIGHT POWER SUPPLY IAW AMM

Part: CAP — MISSING (R1 DOOR SLIDE) · airframe 69,717 hrs · 40,989 cycles

R1 DOOR SLIDE COVER MISSING CAP END FOR BUMPER. REPAIRED CAP END IAW SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,717 hrs · 40,989 cycles

R1 DOOR #4 LOWER BEAM CRACKED NEAR RADIUS IN INSPECTION AREA. R&R #4 BEAM IAW CCO.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,717 hrs · 40,989 cycles

AFT CABIN, EMERGENCY EXIT LIGHTS COMMON TO M1673 BATTERY PACK ARE INOP. / REMOVED AFT LEFT EMERGENCY LIGHT BATTERY CHARGER

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 69,717 hrs · 40,989 cycles

PANEL 193B HAS MULTIPLE FASTENER HOLES THAT ARE ELONGATED DUE TO WEAR. / REPAIRED ELONGATED FASTENER HOLES ON PANEL 193B I.A.W. B737 SRM 53-40-70-22-1 AND 51-70-05-2R-8. RESTORED PROTECTIVE FINISH I.A.W. B737 AMM 51-21-81-370-802

Part: BULKHEAD — CORRODED (BS 946) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO COMPARTMENT BULKHEAD PANEL LOWER CURVED SUPPORT CORRODED AT BS. 946, RBL 23, ON LOWER SURFACE. / R&R BULKHEAD ASSEMBLY IAW DWG AND SRM.

Part: FRAME — CRACKED (BS 259) · airframe 69,717 hrs · 40,989 cycles

FLIGHT DECK STA 259 FRAME WEB CRACKED AT BS. 259, BETWEEN STR. 12L TO STR. 13L. / REPAIRED WEB IAW EA AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

INTERCOSTAL CORRODED BETWEEN BS 927 TO BS 947, RBL 3. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 69,717 hrs · 40,989 cycles

FORWARD CABIN FLOOR BOARD 221BF AFT OUTBOARD TAB IS BROKEN. / REMOVED & REINSTALLED FWD CABIN FLOOR BOARD 221BF I.A.W AMM 53-20-00-400-801. REPAIRED FORWARD CABIN FLOOR BOARD 221BF AFT OUTBOARD TAB I/A/W SRM 53-00-50-2R-1 STEP 3 A-M

Part: FLAP — DELAMINATED (LT WING) · airframe 69,717 hrs · 40,989 cycles

LT OUTBOARD AFT FLAP DELAMINATED ON UNDERSIDE INBOARD END. REPAIRED AFT FLAP IAW SRM.

Part: NONE — CRACKED (ECS BAY LH) · airframe 69,717 hrs · 40,989 cycles

L/H A/C BAY UPPER CHORD AT STA 663 LBL 8 CRACKED / REPAIRED L/H A/C BAY UPPER CHORD AT STA 663 LBL8 IAW EA 190208 IR AND SWA EA 1-757-16074 REV IR

Part: FITTING — CORRODED (BS 365) · airframe 69,717 hrs · 40,989 cycles

E&E BAY STA 365 STR 27R HAS CORROSION JUST AFT OF STRINGER END FITTING. R&R FITTING PER SRM.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL PART NUMBER 141A5810-181 FORWARD EDGE DISBONED AND TORN. / RECIEVED NEW FLOOR PANEL; PART # 14A5810-181. FLOOR PANEL INSTALLED ON N/R 39031/2500/0005 S/N. X908747 IAW AMM 53-21-00-400-801. A-TAG # SL0384.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL PART NUMBER 141A5810-181 TOP SURFACE HAS LOOSE FIBERS. / RECIEVED NEW FOOR PANEL; PART # 141A5810-18. FLOOR PANEL INSTALLED ON N/R 39031/2300/0005 S/N. X908747 IAW AMM 53-21-00-400-801. SL0384.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

L1 DOOR CREASE BEAM CORRODED AT BS 328. R&R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO COMPARTMENT BELOW FLOOR INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (BS 374) · airframe 69,717 hrs · 40,989 cycles

MAIN ELECTRONICS & EQUIPMENT BAY AT AFT END OF STRINGER SPLICE CORRODED AT BS. 374, STR. 27L. R&R STRINGER IAW EA.

Part: STRINGER SPLICE — CORRODED (BS 374) · airframe 69,717 hrs · 40,989 cycles

MAIN ELECTRONICS & EQUIPMENT BAY AT AFT END OF STRINGER SPLICE CORRODED AT BS 374, STRINGER 27L. R & R STRINGER SPLICE IAW EA.

Part: SPAR — CORRODED (RT WING) · airframe 69,717 hrs · 40,989 cycles

R\H WING REAR SPAR HAS CORROSION AT TANK #2 BOOST PUMP LOWER BONDING STRAP CONNECTION POINT. / REMOVED CORROSION ON R/H WING REAR SPAR BOOST PUMP LOWER BONDING STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; ORIGINAL .685' LOSS .126' REMAINING .559' OUT OF LIMITS IAW SRM 57-20-10-1A-1. REPAIRED R/H WING REAR SPAR WEB IAW AAR EA 190212 IR AND SWA EA 1-757-16098 REV IR. ORSS STATION 145 P/N 112A1101-4

Part: STRINGER — CORRODED (BS 364-370) · airframe 69,717 hrs · 40,989 cycles

ELECTRONIC & EQUIPMENT COMPARTMENT STRINGER CORRODED BETWEEN BS. 364 TO BS. 370, STR. 28R. / R&R STRINGER IAW SRM.

Part: SPAR — CORRODED (LT WING) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: L\H WING REAR SPAR HAS CORROSION AT TANK #1 BOOST PUMP LOWER BONDING STRAP CONNECTION POINT. / REMOVED CORROSION ON L/H WING REAR SPAR WEB BOOST PUMP LOWER BOND STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS ORIGINAL .685' LOSS .137' REMAINING .548' OUT OF LIMITS IAW SRM 57-20-10-1A-3. REPAIRED L/H WING REAR SPAR WEB IAW AAR EA 190214 IR AND SWA EA 1-757-16093 REV IR P/N 112A1101-3

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

FWD CARGO COMPARTMENT; CAPSTRIP MARKED L/H #3 IS CORRODED ON BOTTOM. / REPLACED FWD CARGO COMPARTMENT L/H #3 CAP STRIP P/N# 453A1611-10 IAW B737 AIPC 25-52-010-01 AND DWG # 453A1600 REV: A ATAG: WN5481

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO; 2EA FLOOR PANEL CAP STRIP SPLICE PLATES ARE CORRODED ON LOWER SURFACE / RECEIVED 2EA AFT CARGO FLOOR PANEL CAP STRIP SPLICE P/N 453A2611-13 IAW BOEING DWG 453A2600 REV- ATAGA32647

Part: VAPOR BARRIER — DEBONDED (LT MLG WW) · airframe 69,717 hrs · 40,989 cycles

LT VAPOR BARRIER WEB PAIR DEBONDED AT BS 663. REPAIRED WEB IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 69,717 hrs · 40,989 cycles

RT VAPOR BARRIER WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 363) · airframe 69,717 hrs · 40,989 cycles

ELECTRONIC & EQUIPMENT COMPARTMENT STRINGER SPLICE CORRODED AT BS. 363, STR. 28L. / R&R STRINGER SPLICE IAW SRM AND DWG.

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO; FLOOR PANEL CAP STRIP P/N 453A2611-9 HAS CORROSION ON LOWER SURFACE / REPLACED AFT CARGO; FLOOR PANEL CAP STRIP P/N: 453A1611-9 IAW B737-700 AIPC 25-52-10-02 AND BOEING DWG #453A2611 REV:D ATAG: SL0359

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO; AFT TIE DOWN PLATE HAS CORROSION ON LOWER SURFACE / REPLACED WITH A NEW AFT CARGO; AFT TIEDOWN PLATE; P/N 453A2611-2; ATAG A82985 I/A/W AIPC 25-52-10-02 ITEM 75 AND BOEING DRAWING 453A2611 REV C A82985

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO; FWD TIEDOWN PLATE HAS CORROSION ON LOWER SURFACE / REPLACED WITH A NEW AFT CARGO FORWARD TIEDOWN PLATE P/N 453A2611-1 ATAG A26873 I/A/W AIPC 25-52-10-02 ITEM 70 AND BOEING DRAWING 453A2611 REV C A26873

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO; 6EA TIE DOWN FITTINGS HAVE CORROSION (HOCKEY PUCKS) / REPLACED WITH 6 EACH TIE DOWN FITTINGS (PLATE-ANCHOR) P/N 40000-11 ATAG A1751 I/AW AIPC 25-52-51-05 ITEM 15 AND AMM 25-52-12-020-801 A17251

Part: BULKHEAD — NONE (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

1016 BULKHD 6L AT STR 2L HAS OUT OF TOLERANCE HOLE / REAMED HOLE 6L AT STR 2L 1016 BULKHD TO (.3905) (1ST OVERSIDE HOLE TOLERANCES)(.3901 - .391) IAW WO # 39032/3000/001 CUSTOMER CARD# I12107 STEP 5C TO 52 PG 12 TOOL ID#22846 DUE: 07/03/19

Part: BULKHEAD — NONE (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

1016 BULKHD STR 5L STR 2L HAS OUT OF TOLERANCE HOLE DIA / REAMED HOLE 5L AT STR 2L 1016 BULKHD TO (.3905) (1ST OUTSIDE HOLE TOLERANCE IS .3901 - .391) IAW WO# 39032/3000/0001 CUSTOMER CARD #I12107 STEP 5B TO 5A PG 11 TOOL ID#22846 DUE:07/03/19

Part: BULKHEAD — NONE (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

1016 BULKHD 6R AT STR 2R HAS OUT OF TOLERANCE HOLE / REAMED HOLE 6R AT OTR 2R 1016 BULKHEAD TO (.406) (2ND OVERSIDE HOLE TOLERANCES IS .4057 - .4067) IAWWO # 37032/3000/0001 CUSTOMER CARD # I12107 STEP 16A TO 16B PG 30 TOOL ID # 22846 DUE:07/03/19.

Part: RETAINER — CRACKED (LT WING) · airframe 69,717 hrs · 40,989 cycles

LH TRAILING EDGE PANEL 551GB; AFT SEAL RETAINER CRACKED ON O/B END / REMOVED DAMAGED SEAL RETAINER INSTALLED NEW RETAINER AS REQUIRED I.A.W BOEING DWG: 115A2714 REV:B SRM 51-40-02-0G-0.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

L1 DOOR CUTOUT THRESHOLD CORRODED. R&R ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 69,717 hrs · 40,989 cycles

LH WING #3 FLAP TRACK FAIRING 542BB O/B MIDDLE SEAL RETAINER IS CRACKED AT FWD FASTNER HOLE / REMOVED + REPLACED L/H #3 FLAP TRACK FARING 542BB SEAL RETAINER. IAW SRM 51-40-02 + IPC 27-51-18-03 ATAG A82021

Part: FAIRING — DELAMINATED (LT WING) · airframe 69,717 hrs · 40,989 cycles

LH WING #2 FLAP TRACK FAIRING 543AB HAS SEVERAL LAYERS OF COMPOSITE MISSING ON LOWER SURFACE / REPAIRED L/H WING #2 FLAP TRACK FWD FAIRING 543AB AT FASTNER HOLE AREAS I/.A/W SRM 51-70-04-2R-9 REV 66.

Part: BULKHEAD — NONE (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

1016 BULKHD 5R AT STR 2R HAS OUT OF TOLERANCE HOLE / BEAMED HOLE 5R AT OTR 2R 1016 BULKHEAD TO (.406) (2ND OVERSIDE HOLE TOLERANCES IS .04057 - .04067) IAW WO # 39034/3000/0001 CUSTOMER CARD 3 I12107 STEP 15A TO 15B PG 27. TOOL ID # 22846 DUE: 07/03/19.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 69,717 hrs · 40,989 cycles

CABIN FLOOR PANEL 241 KF HAS UPPER FIBER DELAMINATION AT AFT LH CORNER. / REMOVED; FABRICATED AND INSTALLED A NEW CABIN FLOOR PANEL 241KF IAW AMM 53-21-00-000-801; SRM 53-00-50-2R-0; BAC5055 8.3-1.2 - 8.4.2-2; AND AMM 53-21-00-400-801

Part: SPAR — CORRODED (LT WING) · airframe 69,717 hrs · 40,989 cycles

L\H WING FWD SPAR AT #2 L\E FLAP; TANK 1 BOOST PUMP; AT UPPER BONDING STRAP ATTACH POINT HAS CORROSION. / REMOVED CORROSION ON L/H WING FWD SPAR #2 L/E BOOST PUMP .485' ORIG .163' LOSS .322' REMAINING OUT OF LIMITS IAW B737 SRM 57-20-10 ALLOWABLE DAMAGE 3. REPAIRED AREA IAW EA 190195 REV P1; IR AND SWA EA 1-757-16092 REV IR

Part: ATTACH FITTING — CORRODED (RT WING) · airframe 69,717 hrs · 40,989 cycles

R/H WING INBOARD LEADING EDGE FUEL PUMP ATTACH STRUCTURE FORWARD SPAR WEB CORRODED. REPAIRED SPAR WEB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,717 hrs · 40,989 cycles

RT HORIZONTAL STABILIZER RIB STAB STA 129.50, CRACKED ON 3RD VERTICAL STIFFENER. R&R RIB IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,717 hrs · 40,989 cycles

RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B LE STA 114.55 RIB CRACKED AT LOWER END. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,717 hrs · 40,989 cycles

LT HORIZONTAL STABILIZER INTERNAL RIB AT LEADING EDGE STA 123.85, 3RD VERTICAL STIFFENER CRACKED NEAR LOWER END. REPAIRED RIB IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT PIT FLOOR SUPPORT STRINGER PREVIOUS REPAIR NUTPLATE CORRODED NUTPLATE AT BS 767+5, RBL 8. R&R STRINGER IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT PIT FLOOR SUPPORT STRINGER PREVIOUS REPAIR CORRODED NUTPLATE AT BS 767+5, LBL 2.5. R&R STRINGER IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT PIT FLOOR SUPPORT STRINGER PREVIOUS REPAIR NUTPLATE CORRODED AT BS 767+5, RBL 2.5. R&R STRINGER IAW SRM & EA.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO COMP.FLOOR PANEL STRAP CORROSION AROUND SEVERAL FASTNER HOLES STA 887 / REMOVED CORROSION ON AFT CARGO COMP FLOOR PANEL STRAP STA 887 I.A.W B737-700 SRM 51-10-02 ORIGINAL THICKNESS .071 MATERIAL LOSS .030 FOUND TO BE OUT OF LIMITS I.A.W B737-700 SRM 53-00-53-1A-2 REPLACED WITH NEW P/N 146A9401-39 ATAG WN 4303 I.A.W B737-700 AIPC 53-42-11-30 LOCATED; DRILLED; AND INSTALLED I.A.W B737-700 SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT PIT RT Z-ANGLE UPPER SURFACE CORRODED BETWEEN BS 727 TO BS 727C+10, RBL 21. R&R Z ANGLE IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

FORWARD CARGO AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN BL 0 TO LBL 12. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO PIT; LH Z-ANGLE HAS CORROSION AROUND NUTPLATES; BS 727C+10 TO 807+10; LBL 21. / REMOVED CORROSION FROM AFT CARGO PIT; LH Z ANGLE BS727C+10 TO 807+10 LBL21; FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02; SRM 53-00-53-1A-2 REPAIR PERFORMED IN W/O 39031/1600/0006 X908136

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

AFT PIT RH Z-ANGLE FROM 727C+10 TO 767; RBL 21; UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. / REMOVED CORROSION ON R/H Z ANEL RBL 21 FROM STA 727C + 10 TO STA 767 IAW B737 SRM 51-10-02-0G-0. ORIGINAL THICKNESS 0.040'. MAT LOSS: 0.009'; MAT REMAINING 0.031' FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2; FIGURE 103. THE FABRICATION AND THE INSTALL OF THE NEW Z ANGLE P/N: 146A7502-2 WAS ON DEFECT # X908135.

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO PIT FLOOR PANEL SPLICE HAS CORROSION UPPER SURFACE; BS: 767+6; LBL3. / REMOVED AND REPLACED WITH NEW P/N 146A9401-4 ATAG WN4237 NET CARGO PIT FLOOR PANEL SPLICE AT BS 767+6 LBL 3; I.A.W B737-700 AIPC 53-42-11-30 AND SRM 51-40-02-0G-0; ORIGINAL .071; LOSS .035; REMAINING MATERIAL .036; OUT OF LIMITS IAW SRM 53-00-53-1A-1. P/N 146A9401-4

Part: CARGO TRACK — CORRODED (BS 927) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO COMPARTMENT FLOOR STRINGER PANEL FASTENER HOLE CORRODED AT BS. 927, LBL 3. / R&R CARGO DECK SUPPORT TRACK ASSEMBLY IAW SRM AND DWG.

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO COMP.VERTICAL ANGLE CRACKED FLOOR LEVEL STA 867 LBL 16' / REMOVED + REPLACED VERT. ANGLE AT STA 867 LBL 16 IAW SRM 51-40-02 + DWG 149A8102 REV B.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,717 hrs · 40,989 cycles

AFT CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 727C+10, LBL 21, AREAS OF CORRODED UPPER SURFACE. REPAIRED Z ANGLE IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 69,717 hrs · 40,989 cycles

LT EMERGENCY STOWBIN LIGHT LENS MISSING AT ROW 22. R&R LENS COVER IAW MM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 69,681 hrs · 40,966 cycles

L1 DOOR SLIDE RUBBING ON FLOOR, GIRT BAR CLIP TENSION LOOSE. SECURED CLIP PER SIP.

Part: NUT PLATE — CORRODED (AFT CARGO BAY) · airframe 69,323 hrs · 40,730 cycles

WHILE REMOVING THE AFT CARGO DOOR INNER SEAL PLATE; FOUND THE 3RD NUT PLATE HOLE AFT FROM FORWARD EDGE (MIDDLE ROW) TO HAVE EXFOLIATION/INNER GRANULAR CORROSION AROUND NUTPLATE HOLE MOD / REMOVED & REPLACED 6 EA. BACN10MT3 & BACW10AU3 WITH BACN11E3 @ LWR MAIN SILL AFT CARGO COMPARTMENT DOOR; BETWEEN STA 790 - 810 IAW BOEING DRWG #: 146 A8120; REV. A & SRM 51-40-02-0G-0.

Part: PANEL — DELAMINATED (RH PYLON) · airframe 68,074 hrs · 39,924 cycles

#2 ENGINE I/B THRUST REV STRUT FAIRING (PANEL 441EL) HAS EROSIOIN/HEAT DAMAGE; FRAYED FIBERS/ DELAMINATION NEAR FASTENER LOCATIONS. / DMA 0415061 -DRILLED AND COUNTERSUNK NEW PANEL PER SRM 51-20-07 AND 51-40-08 -INSTALLED NEW PANEL PER SRM 51-40-02 CLEARING # 98203

Part: LENS — MISSING (EXIT SIGN) · airframe 67,574 hrs · 39,608 cycles

R2 DOOR LOWER EXIT SIGN MISSING. INSTALLED LENS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,861 hrs · 39,158 cycles

LT AFT EMERGENCY EXIT LIGHT BATTERY INOP AT BS 952. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,861 hrs · 39,158 cycles

LT EMERGENCY EXIT LIGHT BATTERY INOP AT ROW 11. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,861 hrs · 39,158 cycles

RT EMERGENCY EXIT LIGHT BATTERY INOP AT BS 603. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,861 hrs · 39,158 cycles

RT AFT EMERGENCY EXIT LIGHT BATTERY INOP AT BS 952. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,861 hrs · 39,158 cycles

LT EMERGENCY EXIT LIGHT BATTERY INOP AT ROW 17. R&R BATTERY PACK IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY M1670 FAILED A CAPACITY TEST. R&R BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY M1668 FAILED A CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY M1673 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY PACK M1673 FAILED A CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: CHANNEL — CRACKED (VERTICAL STABILI) · airframe 66,816 hrs · 39,133 cycles

VERTICAL STAB; PANEL 324AR; VERTICAL CHANNEL AND METAL RETAINER ARE CRACKED / R&R VERTICAL STAB; PANEL 324AR; VERTICAL CHANNEL AND METAL RETAINER REF SRM 51-40-02.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 66,816 hrs · 39,133 cycles

EMERGENCY LIGHT BATTERY M1674 FAILED A CAPACITY TEST. R & R THE BATTERY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 66,602 hrs · 39,003 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS MISSING AT ROW 11. REPLACED THE LENS IAW AMM.

Part: COVER — LOOSE (STRAP) · airframe 66,043 hrs · 38,643 cycles

LEFT OVERWING EMERGENCY DOOR ESCAPE STRAP COVER LOOSE. SECURED THE COVER IAW MM.

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 64,784 hrs · 37,830 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER SIP MM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 64,641 hrs · 37,742 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,632 hrs · 37,738 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 151.75. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,632 hrs · 37,738 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 69.93. R & R THE RIB IAW DWG AND SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,632 hrs · 37,738 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 113. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,632 hrs · 37,738 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 86.66. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,632 hrs · 37,738 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT HSS 95.96 FOUND CRACKED. R & R THE RIB IAW DWG AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,432 hrs · 37,615 cycles

RT WING TRAILING EDGE EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA EMERGENCY EXIT LIGHT HAD A WIRE BROKEN. REPAIRED THE WIRE IAW SWPM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 63,012 hrs · 36,777 cycles

R2 DOOR FORWARD LOWER CORNER BRACKET CRACKED. R&R BRACKET IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 63,012 hrs · 36,777 cycles

AFT CARGO BAY SUPPORT ANGLE CRACKED BETWEEN BS 907 TO 927, BETWEEN STRINGERS 25 TO 27R. R & R SUPPORT ANGLE IAW SRM AND DWG.

Part: PLATE — CORRODED (L2 DOOR) · airframe 63,012 hrs · 36,777 cycles

L2 DOOR EMERGENCY EVAC SLIDE FLOOR PLATE ASSEMBLY CORRODED. R&R PLATE ASSEMBLY IAW AMM.

Part: PLATE — CORRODED (R2 DOOR) · airframe 63,012 hrs · 36,777 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR PLATE ASSEMBLY CORRODED. R&R PLATE ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (AFT BULKHEAD) · airframe 63,012 hrs · 36,777 cycles

AFT BULKHEAD ANGLE CRACKED AT BS 663, RBL 9, ON LOWER FUSELAGE. R &R THE ANGLE IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 63,012 hrs · 36,777 cycles

LEFT WING TRAILING EDGE PLATE ASSEMBLY CRACKED ON IRSS. 199+20. R & R PLATE ASSEMBLY IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 63,012 hrs · 36,777 cycles

AFT BULKHEAD ON LOWER FUSELAGE ANGLE CRACKED AT BS 663, LBL 9. R & R ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 967-986) · airframe 63,012 hrs · 36,777 cycles

FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 967 TO 986, RBL 50. R & R THE FLOOR SUPPORT ANGLE IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 827-867) · airframe 63,012 hrs · 36,777 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 827 TO 867. R & R CARGO TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA WEB INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 312, BETWEEN RBL 25 TO RBL 45.5. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS 727D TO BS 807, STR 25L. REPAIRED SUPPORT ZEE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

AFT CARGO COMPARTMENT WEB INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: GLOWSTRIP — CRAZED (CABIN) · airframe 63,012 hrs · 36,777 cycles

FORWARD STRIP PHOTOLUMINESCENT CRAZED. R&R STRIP IAW DWG AND MT.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 45.5. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (AFT GALLEY) · airframe 63,012 hrs · 36,777 cycles

AFT GALLEY AREA FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA WEB INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45.5. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 270-294) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA FLOOR SUPPORT CRACKED BETWEEN BS 294.5 TO 270, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SIGN — BROKEN (CABIN) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA EMERGENCY EXIT SIGN ASSEMBLY BROKEN. R&R SIGN ASSEMBLY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 63,012 hrs · 36,777 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294.5 - 312, RBL 16. R & R FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA FLOORBEAM CORRODED AT BS 328, RBL 45.5. REPAIRED THE FLOORBEAM IAW SRM.

Part: FLOORBEAM — CRACKED (BS 294) · airframe 63,012 hrs · 36,777 cycles

FORWARD GALLEY AREA FLOORBEAM UPPER TEE CRACKED AT BS 294.5, RBL 45.5. REPAIRED THE FLOORBEAM IAW EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,012 hrs · 36,777 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,012 hrs · 36,777 cycles

RIGHT WING LEADING EDGE NR 7 SLAT SKIN CRACKED. R & R THE SLAT IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R & R THE BATTERY IAW AMM.

Part: SUPPORT BRACKET — CRACKED (FAIRING) · airframe 62,863 hrs · 36,679 cycles

RIGHT FORWARD UPPER WING TO BODY FAIRING 191AR SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY IAW AMM.

Part: BRACKET — CRACKED (FAIRING) · airframe 62,863 hrs · 36,679 cycles

LEFT FORWARD UPPER WING TO BODY FAIRING 191AL SUPPORT BRACKET CRACKED R & R THE BRACKET IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,863 hrs · 36,679 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,166 hrs · 35,691 cycles

LEFT EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 9. R & R LIGHT IAW AMM.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 60,733 hrs · 35,442 cycles

LEFT OTBD TE FLAP, OTBD RIB CRACKED. R & R RIB IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 59,815 hrs · 34,907 cycles

R1 DOOR EMER ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 58,233 hrs · 33,995 cycles

LEFT OVERWING EXIT SIGN LENS AT LOWER LEVEL MISSING. INSTALLED LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,411 hrs · 33,536 cycles

MAIN WW PRESS WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,411 hrs · 33,536 cycles

LEFT WING NR 1 SLAT, LOWER SURFACE LE SKIN CRACKED AT FASTENER HOLE, AT ACTUATOR ATTACHMENT FITTING. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,411 hrs · 33,536 cycles

LEFT WING NR 3 SLAT LOWER SURFACE LE SKIN CRACKED AT FASTENER HOLE, AT ACTUATOR ATTACHMENT FITTING. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,580 hrs · 33,058 cycles

LEFT WING OTBD TE AFT FLAP DELAMINATED AT INBD END. R & R AFT FLAP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,580 hrs · 33,058 cycles

M1672 EMER LIGHT BATTERY PACK CHARGE LOW. R & R BATTERY PACK IAW AMM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 56,580 hrs · 33,058 cycles

RIGHT WING UPPER TE PANEL, AFT SUPPORT BRACKET BETWEEN NR 7 & 8 SPOILER PANELS, OTBD ATTACH BRACKET CRACKED AT OTBD FASTENERS. R & R BRACKET IAW DWG & SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,580 hrs · 33,058 cycles

M1673 EMER LIGHT BATTERY PACK CHARGE LOW. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,580 hrs · 33,058 cycles

RIGHT EXTERIOR OVERWING EXIT EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,580 hrs · 33,058 cycles

RIGHT WING NR 5 SLAT LE LOWER SKIN CRACKED AT ACTUATOR ATTACH BRACKET AFT OTBD FASTENER. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 56,525 hrs · 33,026 cycles

RIGHT EMER EXIT LIGHT LENS MISSING AT ROW 11. INSTALLED LENS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,349 hrs · 31,767 cycles

M1675 EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,349 hrs · 31,767 cycles

FLOOR SUPPORT CRACKED BETWEEN STATION 344 & 360, BL 0. R & R FLOOR SUPPORT IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,349 hrs · 31,767 cycles

RIGHT MAIN WW FWD PRESS WEB CRACKED AT BS 663.75, RBL33.83. REPAIRED WEB IAW SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 54,349 hrs · 31,767 cycles

EEPLS PHOTO LUMINESCENT LIGHT STRIP CRACKED AT ROW 21. R & R EEPLS STRIP SECTION IAW MM.

Part: COVER — MISSING (EVAC SLIDE) · airframe 53,292 hrs · 31,164 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER MISSING. INSTALLED COVER IAW MM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 52,565 hrs · 30,730 cycles

LT AFT BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE. SECURED CONNECTOR IAW WDM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,492 hrs · 30,688 cycles

RT MID CABIN EMERGENCY LIGHT BATTERY CHARGER INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: COVER — MISSING (CABIN) · airframe 52,492 hrs · 30,688 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

LT HORIZONTAL STABILIZER RIB STATION 92.7 1ST VERTICAL STIFFENER AFT OF FWD SPAR CRACKED THROUGH TO OTBD SIDE. REPAIRED STIFFENER IAW SWA SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

RT NR 1 WINDOW FRAME CRACKED AT OTBD FASTENER HOLE. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME WEB CRACKED AT STATION 259, STRINGER 9L. REPAIRED WEB IAW AAR EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

LT NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. R & R WINDOW IAW ACO.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

RT HORIZONTAL STABILIZER RIB 92.7 1ST STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

RT HORIZONTAL STABILIZER RIB 92.7 3RD STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

LT HORIZONTAL STABILIZER RIB 92.7 3RD STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

RT HORIZONTAL STABILIZER RIB 92.7 2ND STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

LT HORIZONTAL STABILIZER RIB 92.7 2ND STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,492 hrs · 30,688 cycles

RT HORIZONTAL STABILIZER RIB 92.7 4TH STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R & STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 727D, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8L TO STRINGER 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGER 8L & STRINGER 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8R TO STRINGER 9R. REPAIRED IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

SEAT TRACKS CRACKED AT STATION 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8L TO STRINGER 9L. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

SEAT TRACKS CRACKED AT STATION 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME 2ND FROM BOTTOM WINDOW ATTACH FASTENER HOLE ON WINDOW FRAME E-F POST CRACKED. R & R FRAME IAW SWA EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 52,492 hrs · 30,688 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,492 hrs · 30,688 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME 2ND FROM BOTTOM WINDOW ATTACH FASTENER HOLE ON WINDOW FRAME E-F POST CRACKED. R & R FRAME IAW SWA EA.

Part: PUMP — FAULTY (CENTER TANK) · airframe 52,481 hrs · 30,683 cycles

DIVERSION BOTH CENTER TANK PUMP LOW PRESSURE LIGHTS REMAIN ILLUMINATED. W/1860 LBS IN CENTER TANK FL390. R & R RT CENTER FUEL BOOST PUMPS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,382 hrs · 30,621 cycles

RT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,382 hrs · 30,621 cycles

LT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,908 hrs · 29,715 cycles

RIGHT OTBD AFT FLAP INBD T/E CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 50,908 hrs · 29,715 cycles

RT OVERWING EXTERIOR EXIT LIGHT INOP. R & R POWER SUPPLY IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,908 hrs · 29,715 cycles

LT NR 1 FLIGHT DECK FIXED WINDOW FRAME UPPER OTBD CORNER CRACKED ON INNER EDGE OF FRAME. REPAIRED DOUBLER IAW EA.

Part: SIGN — INOPERATIVE (CABIN) · airframe 50,908 hrs · 29,715 cycles

RT OVERWING EMERGENCY EXIT LOWER SIGN INOP. R & R SIGN IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,231 hrs · 28,061 cycles

R1 WINDOW FRAME CRACKED AT UPPER RIGHT CORNER. REPAIRED FRAME PER EA.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 48,139 hrs · 28,009 cycles

EMERGENCY EXIT DOOR SIDE WALL LIGHT INOP. REMOVED AND REPLACED BALLAST PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,276 hrs · 26,927 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 21. RELAMPED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,276 hrs · 26,927 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: SENSOR — FAULTY (LE SLAT) · airframe 45,540 hrs · 26,487 cycles

AFTER LANDING FLAPS WOULD NOT RETRACT PAST 5-10 WITH SPLIT FLAP INDICATION. REMOVED AND REPLACED NR 5 SLAP SKEW SENSOR PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,725 hrs · 26,009 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 8. SECURED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 727, WL 201. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 685, STR 8R. REPAIRED FRAME PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, EMERGENCY EXIT LIGHT BATTERY PACK INOP AT BS 322, RBL 7. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 685, STR 8R. REPAIRED FRAME PER EA.

Part: LIGHT — CRACKED (EXIT SIGN) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, L1 DOOR EMERGENCY EXIT SIGN LIGHT CRACKED. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 867 STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 500C STR 8L. REPAIRED FRAME IAW EA.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLIGHT DECK FLOOR PANEL CORRODED BETWEEN STATIONS 260 TO 270 BL 0 ON "C" CHANNEL. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, RT CREASE BEAM CORRODED FROM STA 1006 + 10 TO STA 967+ 10. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, RIGHT SIDE BS 305 TO 350 Z-ANGLE CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 44,061 hrs · 25,616 cycles

DURING SCHEDULED 12Y CHECK FOUND, AFT GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,568 hrs · 28,276 cycles

FRAME CRACKED AT BS 727, WL 201. REPAIRED FRAME IAW EA AND AAR EA.

Part: FASTENER — MISSING (GIRT BAR) · airframe 43,642 hrs · 25,384 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FASTENER MISSING. INSTALLED FASTENER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,066 hrs · 22,729 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,161 hrs · 22,168 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 38,161 hrs · 22,168 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 38,040 hrs · 22,087 cycles

EEPLS STRIP LOOSE AT ROW 7. REMOVED AND REPLACED STRIP PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 35,676 hrs · 20,636 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD UPPER I/B TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG) · airframe 35,676 hrs · 20,636 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD UPPER I/B TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: STRIP — LOOSE (CABIN) · airframe 35,560 hrs · 20,567 cycles

FOUND EEPLS STRIP LOOSE BETWEEN ROW 9 TO ROW 10. SECURED STRIP PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 35,560 hrs · 20,567 cycles

FOUND EEPLS STRIP LOOSE BETWEEN ROW 9 ABC TO ROW 10 ABC. SECURED STRIP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 34,730 hrs · 20,070 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,729 hrs · 20,070 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,729 hrs · 20,070 cycles

DURING SCHEDULED HC2 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,198 hrs · 18,545 cycles

DURING SCHEDULED HC1 CHECK, AFT LEFT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,198 hrs · 18,545 cycles

DURING SCHEDULED HC1 CHECK, FWD LEFT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,198 hrs · 18,545 cycles

DURING SCHEDULED HC1 CHECK, AFT RIGHT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 30,113 hrs · 17,335 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT MLG W/W STIFFENER CRACKED AT BS 663, BETWEEN LBL 6.15 TO LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,113 hrs · 17,335 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 27,406 hrs · 15,814 cycles

DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 27,406 hrs · 15,814 cycles

DURING SCHEDULED HC1 CHECK, LT AFT CABIN EMERGENCY BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 26,049 hrs · 14,991 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER AT FWD CABIN DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,506 hrs · 14,691 cycles

DURING SCHEDULED RON CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 25,163 hrs · 14,502 cycles

EEPLS STRIP COVER LOOSE AT FWD END. SECURED EEPLS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 25,143 hrs · 14,488 cycles

DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,103 hrs · 14,460 cycles

CABIN EEPLS TRACK LENS MISSING. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 24,443 hrs · 14,102 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 24,182 hrs · 13,968 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,942 hrs · 13,266 cycles

FWD ENTRY EMERGENCY EXIT LOWER SIGN BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,906 hrs · 13,251 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,378 hrs · 12,372 cycles

DURING SPV, FOUND LT EMERGENCY EXIT AISLE LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,378 hrs · 12,372 cycles

DURING SPV, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 20,339 hrs · 11,795 cycles

BRAKES VERY INEFFECTIVE WITH INCREASING PEDAL PRESSURE DOWN TO 70 KNOTS WHERE ANTISKID ACTIVATED. BRAKES CHECK WITHIN LIMITS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOORS) · airframe 20,204 hrs · 11,728 cycles

DURING SCHEDULED HC2D CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 17,608 hrs · 10,284 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,608 hrs · 10,284 cycles

DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,608 hrs · 10,284 cycles

DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 16,977 hrs · 9,945 cycles

L1 DOOR SLIDE OUT OF ADJUSTMENT. READJUSTED L1 SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,357 hrs · 9,615 cycles

DURING SCHEDULED C3 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT ASSY INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 15,998 hrs · 9,397 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW NR 7. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (ALL CABIN DOORS) · airframe 13,981 hrs · 8,295 cycles

DURING SCHEDULED C1 CHECK, FOUND ALL CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 13,619 hrs · 8,110 cycles

EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 13,540 hrs · 8,069 cycles

DURING SCHEDULED RON, FOUND AFT CABIN EELPS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: LIGHT — LOOSE (CABIN) · airframe 11,638 hrs · 6,997 cycles

DURING SCHEDULED RON, FOUND EEPLS LOOSE AT ROW NR 1. SECURED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,106 hrs · 4,258 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD CABIN. R&R TRACK COVER PER MM.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 5,972 hrs · 3,603 cycles

IN FLIGHT ENGINE SHUTDOWN. CREW REPORTED NR 1 ENG OIL QUANTITY STARTED DROPPING. THE ENGINE WAS SHUT DOWN. ON FURTHER INSP, IDG FAILURE WAS FOUND. REMOVED AND REPLACED NR 1 ENGINE PER MM. OPS CHECK NORMAL.