N745SW

Part: NONE — CRACKED (FUSELAGE) · airframe 75,338 hrs · 44,633 cycles

VERTICAL CLIP CRACKED ON AFT SIDE OF LEFT WHEEL WELL UNDER 193D PANEL ; REMOVED AND REPLACED VERTICAL CLIP REF. B737 SRM 51-40-02.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 75,338 hrs · 44,633 cycles

193D PANEL NEEDS TO BE REPLACED DUE TO IT BEING DELAMINATED ; 193D PANEL NEEDS TO E REPLACED DE TO DELAMINATED / [01] REMOVED AND REPLACED PANEL REF. B737 AMM 53-51-21 .

Part: NONE — CRACKED (FUSELAGE) · airframe 75,338 hrs · 44,633 cycles

TEE ANGLE CLIP IS CRACKED ON AFT SIDE OF LEFT WHEEL WELL UNDER 193D PANEL. REMOVED AND REPLACED ?T? ANGLE CLIP REF B737 SRM 51-40-02.

Part: NONE — OUT OF ADJUST (L1 DOOR) · airframe 74,927 hrs · 44,385 cycles

FWD ENTRY DOOR GIRT BAR SPRING CLIPS LOOSE ; / [01] ADJUSTED SPRING CLIPS PER SIP

Part: RADOME — DAMAGED (NOSE) · airframe 74,275 hrs · 44,002 cycles

RADOME HAS DAMAGE DOWN TO FIBERGLASS IN MULTIPLE PLACES. REPLACED NOSE RADOME REF. AMM 53-52-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,381 hrs · 43,478 cycles

L/H FORWARD EMERGENCY BATTERY IS DEAD / REMOVED AND REPLACED L/H FORWARD EMERGENCY BATTERY REFERENCE AMM 33-51-06. OPS CHECK GOOD

Part: SKIN — CRACKED (BS 685 S1L) · airframe 73,381 hrs · 43,478 cycles

REF LP 1306118 FOUND CRACK INDICATION ON FUSELAGE CROWN SKIN AT STATION 685 + 2 STRINGER 1L 1' CRACK MEASURES APPROXIMATELY 1' / REPAIRED FUSELAGE CRACK AT STA 685 + 2 ADJACENT TO RO STR 1L. REPAIR REQUIRER LFCC INSPECTION OF FUSELAGE SKIN AND EXTERNAL DVI OF STRUCTURE AT 1380 FLT CYCLES WITH REPEAT INSPECTIONS EVERY 1380 FLTCYCLES REF EA 21-153-00605 SEE SA-M 326 #A1223927

Part: SKIN — CRACKED (FUSELAGE CROWN) · airframe 73,379 hrs · 43,477 cycles

FOUND CRACK INDICATION ON FUSELAGE CROWN SKIN AT STATION 685 +2' STRINGER 1 L 1' CRACK MEASURES APPROXIMATLEY 1' IN LENGHT W/INSPECTOR A13 (36468) / TRANSFERRED TO LP 1306118

Part: SIGN — MISSING (CABIN) · airframe 73,243 hrs · 43,398 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT SIGN MISSING. DMA NR 0416118 R & R L1 EMERGENCY EXIT SIGN ASSY REF AMM 33-51-01 CL NR 69010.

Part: SIGN — DETACHED (LT OVERWING) · airframe 73,243 hrs · 43,398 cycles

LEFT OVERWING EXIT SIGN CAME LOOSE. VERIFIED ALL EXIT SIGNS AT OVERWING EXITS ARE SECURE AND OPERATING NORMALLY. REF AMM 33-51-01. AIRCRAFT OK FOR SERVICE.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 72,918 hrs · 43,203 cycles

LEFT FWD UPPER WTB FAIRING 191AL AFT LOWER SUPPORT BRACKET CRACKED. / R&R'D LEFT FWD UPPER WTB FAIRING 191AL AFT LOWER SUPPORT BRACKET PER SRM 51-40-02 AND SRM 51-10-02.

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR LIGHT) · airframe 72,583 hrs · 42,996 cycles

EXTERIOR RT OVERWING EXIT EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED POWER SUPPLY CHARGER POSITION M1669, REF. B737 AMM 33-51-06-960-806. RELAMPED EXTERIOR RT OVERWING EMERGENCY LIGHT, REF. B737 AMM 33-51-04-960-801. PERFORMED OPERATIONS TEST, REF. B737 AMM 33-51-06-710-005, FOUND NORMAL.

Part: RIB — WORN (LT WING) · airframe 72,583 hrs · 42,996 cycles

LEFT WING TRAILING EDGE ORSS261 STRUCTURE DEFLECTION CONTROL RIB SHOWS SIGNS OF WEAR AT LOWER REAR SPAR ATTACH POINT (MKD 20- 055). ACCOMPLISHED PERMANENT REPAIR AT LT WING TRAILING EDGE STRUCTURE DEFLECTION CONTROL RIB, IAW B737-700 SRM 57-51-02-2R-4 SRM 57-51-02-2R-1 (REPAIR 4 ADN REPAIR 1); AMM 57-50-01-820-801.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 72,583 hrs · 42,996 cycles

** CORROSION ** FWD CARGO COMPMT. SIDE WALL CIRCUMFERENTIAL SUPPORT AT S-26R STA 500D MKD DOT 60-012 / REMOVED AND REPLACED NEW CIRCUMFERENTIAL AT FWD CARGO STA 500D S-26 TO 17R AS PER B-737-700 SRM 51-40-02-06-0 / DRWG 143A9481

Part: CHANNEL — CORRODED (BS 747-847) · airframe 72,583 hrs · 42,996 cycles

CORROSION AFT CARGO COMPARTMENT LT FLOOR SUPPORT Z CHANNEL S-26L FROM STA 747 TO STA 847 MKD DOT 60-002. REMOVED CORROSION AT AFT CARGO COMPART LT FLOOR SUPPORT Z CHANNEL FROM STA 747 TO STA 847 AND FOUND TO BE OUT OF LIMITS, AS PER REF B737 SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-2. REMOVED AND REPLACED Z CHANNEL AT AFT CARGO COMPARTMENT LT FLOOR Z CHANNEL, AS PER REF B737 SRM 53-00-53-2R-6 AND SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CRACKED (BS 927 S26R) · airframe 72,583 hrs · 42,996 cycles

AFT OF AFT CARGO COMPARTMENT BILGE SUPPRT CLIP CRACKED AT S-26R AND STA 927 MKD DOT 60-008 / REMOVED AND REPLACED CLIP AT AFT CARGO COMPARTMENT BILGE SUPPORT AREA S-26R AND STA 927 AS PER REF B737 SRM 51-40-02-0G-0

Part: CHANNEL — CORRODED (BS 500-500A) · airframe 72,583 hrs · 42,996 cycles

CORROSION FWD CARGO COMPARTMENT. RT SIDE FLOOR SUPPORT Z CHANNEL AT S-26R STA 500 TO STA 500A WL 156 AT RBL 25' MKD DOT 60-013. REMOVED AND REPLACED FLOOR SUPPORT AT FWD CARGO S-26R STA 500 TO 500A, AS PER B737-700 SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 500D) · airframe 72,583 hrs · 42,996 cycles

** CORROSION ** FWD CARGO COMPARTMENT AFT BULKHEAD LOWER FLOOR SUPPORT ANGLE AT STA 500D FROM S-26L TO S-26R MKD DOT 60-010 WL 156 / REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE AT FWD CARGO STA 500D FROM S-26L TO S-26R IN REF SRM 51-40-02-0G-0 AND DRAWING 143A9481.

Part: WEB — CORRODED (BS 440-480) · airframe 72,583 hrs · 42,996 cycles

** CORROSION ** FWD CARGO COMPMT. DOOR CUTOUT LOWER SILL WEB PLATE;WL 156 STA 440 TO STA 480+12' RBL 25'. / REMOVED AND REPLACED LOWER SILL WEB PLATE AT FWD CARGO DOOR CUTOUT AS PER B737-700 SRM 51-40-02-0G-0

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 72,583 hrs · 42,996 cycles

** CORROSION ** FWD CARGO COMPMT. L/ H SIDE WALL CIRCUMFERENTIAL SUPPORT AT S-25L STA 500D MKD DOT 60-011 / REMOVED AND REPLACED L/H SIDEWALL CIRCUMFERNTIAL SUPPORT AT STA 500D STR 25L - STR 19L - FWD CARGO COIMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 / 53-00-53-1A-2 FIG 103 / 51-20-01-0G-0

Part: CHANNEL — CORRODED (BS 500A-500D) · airframe 72,583 hrs · 42,996 cycles

CORROSION FWD CARGO COMPARTMENT. RT SIDE FLOOR SUPPORT Z CHANNEL AT S-26R STA 500A TO STA 500D MKD DOT 60-014. REMOVED AND INSTALLED NEW FLOOR SUPPORT Z CHANNEL (SIDE PLATE) AT FWD CARGO STR 26R FROM STA 500A TO STA 500D RBL 22', IN REF SRM 51-40-02-0G-0 AND DRAWING 143A7500.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 72,583 hrs · 42,996 cycles

PANEL192BL DELAMINATED AT THE LOWER FWD EDGE / CLEANED&REPAIRED DAMAGE L/E AREA 2 EA ON PANEL 192 BL FWD AREA OUTER&SURFACE AS PER B737 SRM 51-70-04-2R-6 REPAIR 6. TOUCH UP PAINT REPAIR ON REPAIRED AREA AS PER B737 AMM 51-21-99-300-802

Part: WEB — CORRODED (FWD CARGO) · airframe 72,583 hrs · 42,996 cycles

**CORROSION** FWD CARGO THRESHOLD; TOP SIDE OF WEB WITH SURFACE CORROSION ON SEVERAL SPOTS / THIS ITEM WILL BE ACCOMPLISHED ON W/O 2016169 ITEM 1000/0065; W169376

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,583 hrs · 42,996 cycles

RT HORIZONTAL STABILIZER LEADING EDGE CAP 341B RIB NR 3 IS CRACKED, (DOT 124-005). REMOVED AND REPLACED RIGHT HORIZ STAB LEADING EDGE CAP NR 341B RIB NR 3 IN REF WITH B737 SWA SRM 51-40-02-0G-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,583 hrs · 42,996 cycles

LT HORIZONTAL STABILIZER LEADING EDGE CAP 331B RIB NR 16 IS CRACKED (DOT 124-004). REMOVED AND REPLACED LEFT HORIZ STAB LEADING EDGE CAP NR 331B RIB NR 16 IN REF WITH B737 SWA SRM 51-40-02-0G-0.

Part: WEB — CORRODED (AFT CARGO) · airframe 72,583 hrs · 42,996 cycles

**CORROSION** AFT CARGO COMPARTMENT THRESHOLD; UPPER SIDE OF WEB WITH SURFACE CORROSION ON SEVERAL SPOTS / THIS TASK CARD TO BE ACCOMPLISHED ON TASK CARD # W169365 AND WORK ORDER 2016169/1000/0047.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 72,583 hrs · 42,996 cycles

LT WHEEL WELL STA 663 LBL 37' 2.5' FROM TOP HAS .250' CRACK EMITTING FROM FASTENER, MARKED LOCATION. REPAIRED DEFECT AT LT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB STA 663 LBL 37' 2.5' FROM TOP, IAW B737-700 SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 1. THIS IS A CATEGORY B REPAIR, SEE TABLE 203.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,583 hrs · 42,996 cycles

EMERGENCY LIGHTS AT SEATS 3 AND 6 DEF INOP. REMOVED AND REPLACED BATTERY PACK POS M1674, AS PER REF B737 AMM 33-51-06-960-805. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS AT SEATS 3 AND 6 DEF AND FOUND NORMAL.

Part: RIB — WORN (RT WING) · airframe 72,583 hrs · 42,996 cycles

RIGHT WING TRAILING EDGE STRUCTURE DEFLECTION CONTROL RIB. SHOWS SIGNS OF WEAR AT LOWER REAR SPAR ATTACH POINT (MKD 26-001). ACCOMPLISHED PERMANENT REPAIR AT RT WING TRAILING EDGE STRUCTURE CONTROL RIB, IAW B737-700 SRM 57-51-02-02R-4 REPAIR 4 SRM 57-51-02-2R-1 REPAIR 1 AND AMM 57-50-1-820-801.

Part: FLOOR PANEL — DETERIORATED (MAIN CABIN) · airframe 72,583 hrs · 42,996 cycles

CABIN FLOOR PANELS 231XF, 241EF, AND 241FF WITH UNDERSIDE FOAM DETERIORATED. REMOVED AND REPLACED UNDERSIDE FOAM AT CABIN FLOOR PANELS 231XF, 231EF, AND 241FF AS PER REF B737 AMM 53-21-00-400-801.

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 72,550 hrs · 42,981 cycles

FO SEAT HARD TO SLIDE FOR/AFT CLEANED F/OS SEAT TRACKS AND LUBED. OPS CHECK OK PER "SIP"

Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 72,482 hrs · 42,942 cycles

FWD CARGO FLOORBOARD 120BF HAS A 3 INCH CRACK AT THE AFT LEFT CORNER. / R&R FWD CARGO FLOORBOARD 120BF PER AMM 25-52-10.

Part: SKIN — DEFORMED (BS 837 S4-5L) · airframe 72,482 hrs · 42,942 cycles

FUSELAGE SKIN HAS A OUT OF CONTOUR PROTRUSION APPROX STA 837 BETWEEN S-4L AND S-5L MEASURES 4'X6' APPROX .045' HIGH. / C/W EA 1-753-36674

Part: BATTERY PACK — FAILED (CABIN) · airframe 72,482 hrs · 42,942 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1669, M1670, M1672 AND M1673 IN CABIN. R&R BATTERY PACKS AT M1669, M1670, M1672 AND M1673 PER AMM 33-51-06.

Part: FASTENER — LOOSE (L1 GIRT BAR) · airframe 70,543 hrs · 41,703 cycles

L1 DOOR SLIDE GIRT BAR RETAINER CLIP LOOSE, DOOR OPENED-LEFT CLIP. R&R FASTENER PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,827 hrs · 41,251 cycles

R2 DOOR EXIT SLIDE LOOSE AND OUT OF POSITION IN CONTAINER. REPOSITIONED SLIDE FLAP PER AMM.

Part: FAIRING — DELAMINATED (LEFT WING) · airframe 68,934 hrs · 40,675 cycles

#3 FLAP SUPPORT FAIRING HAS DAMAGE TO OUTBOARD SIDE OF TAILCONE. DAMAGE CONSISTS OF A HOLE MEASURING .40' IN DIAMETER AND .300' IN DEPTH; EXTENDING THROUGH PILES TO CORE. DELAMINATION EXTENDS TO 2.5' IN DIAMETER AROUND THE HOLE; DAMAGE IS OUT OF LIMITS PER SRM 57-53-70-1A-1 PAR 4(A) 5. / INSTALLED TAIL CONE SUPPORT FAIRING IAW SIP CLEARING# 39728 DMA# 0278981

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,410 hrs · 40,333 cycles

FORWARD ENTRY FUSELAGE EMERGENCY LIGHT BATTERY PACK FAILED THE CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,000 hrs · 40,065 cycles

R2 DOOR EMERGENCY SLIDE LIGHT INOP AT M1672. R&R CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,000 hrs · 40,065 cycles

G4 GALLEY EMERGENCY EXIT LOCATOR LIGHT INOP AT M1672. R&R CHARGER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,000 hrs · 40,065 cycles

LT CENTER EMERGENCY LIGHTS INOP BETWEEN BS 603 TO BS 727C. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,000 hrs · 40,065 cycles

RT CENTER EMERGENCY LIGHTS INOP BETWEEN BS 603 TO BS 727C. R&R BATTERY PACK IAW AMM.

Part: STRIP — BROKEN (FWD CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

FWD CARGO AFT DOOR REVEAL CAP STRIP IS BROKE / VERIFIED AND REPLACED FWD CARGO AFT DOOR REVEAL CAP STRIP PN# 453A1411-2 IAW BOEING DWG #453A1400 REV C 'REPLACED ONLY' ATG# A27377

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 68,000 hrs · 40,065 cycles

RT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB INTERCOSTAL ATTACH ANGLE CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO FRAME CLIP CRACKED AT BS 500C, LBL 25. R&R CLIP IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 68,000 hrs · 40,065 cycles

FORWARD LOWER CEILING CLOSEOUT PANEL, EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: INTERCOSTAL — ELONGATED (FWD CARGO LH) · airframe 68,000 hrs · 40,065 cycles

FWD PIT; STA 480+1; AT STR:25L HAS AN ELONGATED HOLE; O/B SIDE OF CHANNEL COMMON TO INTERCOSTAL. / REMOVED AND INSTALLED NEW INTERCOSTAL AND INSTALLED ONE OVERSIZED HOLE FASTENER AT FWD PIT STA 480+1 AT STR 25L I/A/W E.A. # 18052 P1 AND SWA E.A. # 1-753-3336 REV: IR

Part: FRAME — CRACKED (RIGHT WING) · airframe 68,000 hrs · 40,065 cycles

WHILE REMOVING R/H AFT FLAP TRACK DOOR FOUND STRUCTURE CRACKED. P/N 149A7331-6. / FABRICATED AND APPLIED CHEMICAL CONVERSION COATING AND APPLIED PRIMER AT R/H AFT FLAP TRACK DOOR I/A/W E.A. # 180524 P1 AND SWA E.A. 1-757-15524 REV: IR

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

STRINGER CORRODED AT BS 539, STR 25R. R&R STRINGER IAW EA.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 68,000 hrs · 40,065 cycles

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

Part: SUPPORT FITTING — CRACKED (AFT CARGO BAY) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT STATION 947; STRINGER 26L; ON TOP OF FRAME FREE FLANGE; CORNER SUPPORT FITTING IS CRACKED ON THE VERTICAL FLANGE AS MARKED. / REMOVED & REPLACED FITTING AT AFT CARGO STA. 947 STR 26L. IAW B737-700 SRM 51-40-02-0G-0 AND DWG NO. 149A8103 REV - A16805

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FLOORBEAM FLANGE CRACKED AT BS 294, RBL 51. R&R ANGLE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

E&E COMPARTMENT FRAME WEB CORRODED AT BS 351.2, BETWEEN STR 21L TO STR 22L. R&R FRAME WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 663, BETWEEN RBL 45 TO RBL 60. R&R SUPPORT IAW DWG AND AMM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

BRACKET CORRODED BETWEEN BS 360 TO BS 370, STR 28L. R&R BRACKET IAW DWG AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

ATTACH ANGLE CLIP CRACKED AT BS 260+2, STR 8L. R&R CLIP IAW DWG & SRM.

Part: PANEL — DELAMINATED (LT WING) · airframe 68,000 hrs · 40,065 cycles

LH WING L/E PANEL 521 WB HAS DELAM / REPAIRED DELAM ON L/E PNL 521WB I.A.W B737 SRM 57-46-01-2R-1 AND 51-70-04-2R-10; REPAIRED ALUMINUM FOIL I.A.W SRM 51-70-14-2R-3 AND TOP COAT I.A.W AMM 51-21-99-300-801

Part: ANGLE — CORRODED (LT WING) · airframe 68,000 hrs · 40,065 cycles

L/H WING FWD SPAR BOOST PUMP UPPER ANGLE IS CORRODED / REMOVED CORROSION FROM LH WING FWD SPAR BOOST PUMP; 50% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0. LOCATED; DRILLED; AND INSTALLED NEW ANGLE IAW DWG 112A2004 REV. A RESTORED CIC IAW AMM 51-21-91-620-802

Part: PANEL — DELAMINATED (LT WING) · airframe 68,000 hrs · 40,065 cycles

#1 ENGINE 431 ER DELAMED AT CORNER. MARKED. / REPAIRED DELAMED CORNER ON #1 ENGINE PNL 431ER IAW B737 SRM 54-50-70-2R-2 AND 51-70-04-2R-10 RESTORED FINISH IAW B737 AMM 51-21-99-300-801

Part: BEAM — CRACKED (R1 DOOR) · airframe 68,000 hrs · 40,065 cycles

R1 DOOR UPPER BEAM NR 5 ASSEMBLY CRACKED. R&R BEAM IAW DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

STRINGER CLIP CORRODED AT BS 312, STR 2L. R&R STRINGER CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

STRINGER CLIP CRACKED AT BS 360, STR 8R. R&R STRINGER CLIP IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

CREASE BEAM WEB ATTACH ANGLE CRACKED AT BS 294, STR 17R. R&R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — DENTED (FLIGHT DECK FLOO) · airframe 68,000 hrs · 40,065 cycles

FLIGHT DECK FLOOR HAS 3 EA DENTS / VERFIED DENTS AT FLIGHT DECK FLOOR; ' OUT OF LIMITS' DENTS .155' IAW B737-700 SRM 53-10-51-1A-1 FIG 105 SHEET 2 REMOVED MATERIAL DAMAGED AT FLIGHT DECK FLOOR STA 252-270 BLO-LBL 20 IAW B737-700 SRM 53-10-51-2R-2 REPAIRED FABRICATED & INSTALLED REPAIR PARTS AT FLIGHT DEK FLOOR STA 252-370 BLO-LBL2 IAW B737-700 SRM 53-10-51-2R-2 TAG: A82719; A43751

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

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

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT AFT NET TIE DOWN PLATE HAS CORROSION ON LOWER SURFACE / EVALUATED TIE DOWN AT AFT CARGO AFT OF CARGO DOOR FOUND NO LIMITS FOUND IN SRM FOUND OUT OF LIMITS REPLACED TIE DOWN PLATE IAW BOEING DWG 453A2600 ATAG #A85826

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT FWD NET TIE DOWN PLATE HAS ORROSION CORROSION ON LOWER SURFACE / EVALUATE TIE DOWN PLATE AT AFT CARGO FWD OF CARGO DOOR NO LIMITS ALLOWABLE FOUND IN SRM REPLACED TIE DOWN PLATE IAW BOEING DWG 453A2600 ATAG#A13102

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 26R. R&R FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FRAME CRACKED AT BS 500C, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,000 hrs · 40,065 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.30, 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW DWG & SRM.

Part: SHIELD — CORRODED (FWD CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

FWD CARGO COMPARTMENT FWD SHIELD HAS SURFACE CORROSION. / EVALUATED CORRODED AREA; FOUND CORROSION DAMAGE TO E 100% THROUGH MATERIAL THICKNESS; FOUND TO BE OUT OF LIMITS IAW B737 SRM53-30-15-1A-1. REMOVED DAMAGED SHIELD IAW B737 SRM51-40-02. IDENTIFIED NEW SHIELD AS P/N 143A8126U21 PER BOEING ENG. DWG. NO. 143A0080 REV:-. LOCATED AND DRILLED IAW B737 SRM51-40-05-0G-0; INSTALLED NUTPLATES IAW B737 SRM51-40-02-0G-0 AND BOEING ENG. DWG. NO. 143A0080; REV:-. INSTALLED NEW SHIELD IAW BOEING ENG. DWG. NO. 143A0080 REV:- AND B737-700 SRM 51-40-02. APPLIED CIC IAW B737 AMM 51-21-91-620-802. A-TAG # WN7609

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT FLOOR PANEL 140AF UPPER HORSESHOE CAP STRIP HAS CORROSION ON UPPER AND LOWER SURFACES / ORDERED AND RECEIVED NEW CAPSTRIP ASSY P/N 453A2611-25-REF: BAC DWG 453A2611 REV. F PART TO BE INSTALLED ON CARD JPANEL-141-CLOSE (38146-1600-0022).

Part: FLAP — DELAMINATED (LT WING) · airframe 68,000 hrs · 40,065 cycles

LT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. R&R AFT FLAP IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

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

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 767-793; RH Z-ANGLE HAS CORROSION ON UPPER AND LOWER SURFACE. / EVALUATION OF CORROSION ON R/H Z-ANGLE AFT CARGO STATION 767 TO STA 793 WAS 100% MAT LOSS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE IAW SRM 51-40-02 AND DWG 146A0081 REV C ATAG: WN5340

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 68,000 hrs · 40,065 cycles

NOSE WHEEL WELL PANEL 114 BW HAS CORROSION ON INNER UPPER SURFACE AT FASTENER HOLES; MARKED. / REMOVED CORROSION FROM NOSE WHEEL WELL PANEL 114BW ON INNER UPPER SURFACE ORIGINAL 'T' .192'; REMOVED .007'; .185' REMIANING BOEING FINDS IT TO BE STRUCTURELY ACCEPTABLE; RESTORED SURFACE FINISH IAW EA 1-753-33228 REV IR AND EA 180490 IR

Part: SHIELD — CORRODED (FWD CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

FWD CARGO COMPARTMENT AFT SHIELD HAS SURFACE CORROSION. / REMOVED FWD PIT AFT SHIELD IAW B737 SRM 51-40-02. BLENDED CORROSION IAW B737 SRM 51-10-02 AND SRM 53-30-15-1A-1. ORIG 'T' .032'; LOSS OF .018'; REMAINING 'T' .014'; FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-30-15-1A-1. IDENTIFIED NEW SHIELD ASSY. AS P/N 143A8126U31 PER BOEING ENG. DWG NO. 143A0080 REV:- LOCATED AND DRILLED IAW B737 SRM 51-40-05-0G-0 AND BOEING ENG. DWG NO. 143A0080 REV:- APPLIED CIC TO SHIELD IAW B737 AMM 51-21-91-620-802. A-TAG#WN7300

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 847, LBL 6. R&R STRINGER CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 943-947 LBL9; LH SIDEWALL LOWER SUPPORT ANGLE HAS CORROSION ON LOWER SURFACE. / REMOVED CORROSION AT AFT CARGO COMPARTMENT STA 943-947 LBL 9 L/H SIDEWALL LOWER SUPPORT ANGLE ON LOWER SURFACE I/A/W SRM 53-00-53-1A-2; VERIFIED MATERIAL LOSS; ORIG .090 REMOVED .028 REMAINING .063 MATERIAL IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 ACCOMPLISHED E.A. # 18531 P1 AND SWA E.A. # 1-753-33349 REV: IR

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO COMPARTMENT LT "Z" ANGLE CORRODED BETWEEN BS 460 TO BS 500D. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 727C+4 TO BS 767. R&R Z-ANGLE IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT FLOOR PANEL 140CF HAS CORROSION ALONG EDGES / REMOVED CORROSION AT AFT CARGO FLOOR PNL 140CF ALONG EDGES IAW SRM 51-10-02 VERIFIED MATERIAL LOSS ORIGINAL .080 REMOVED .019 REMAIN .061 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #9800 DUE DATE 10/10/2018 IAW SRM 53-00-53-1A-1 REPLACES PNL 140CF IAW BOEING DWG 453A2600

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 727D+6 LBL21 - RBL21; FLOOR PANEL SPLICE STRAP HAS CORROSION. / REMOVED CORROSION AT AFT CARGO SPLICE TRAP STA 727D + 6LBL 21 TO RBL 21 IAW SRM 51-10-02-0G-00 VERIFIED MATERIAL LOSS FOUND TO BE 100% FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 RECEIVED STRAP IAW IPC 53-42-11-30 FLOOR STRAP INSTALLED PN CUSTOMER CARD JPANEL-141-CLOSE PANEL 140AF. ATAG # A12809

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 934-936 RBL13.5; FLOOR TRACK HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION IAW SRM 53-00-53-1A-2. ORIG. THICKNESS .075'; AFTER REWORK .063' .012' MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. AAR TOOL = 36649; DAL DUE : 05 AUG 19. REMOVED OUT OFF LIMITS CARGO TRACK FROM STA 947 TO 887 RBL 13.5 AND INSTALLED NEW CARGO TRACK ALL IAW SRM 51-40-02-0G-0 AND DWG: 147A7500 REV -. ATG: LP1146

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 765 RBL22.5; Z-AANGLE SUPPORT INTERCOSTAL HAS CORROSSION AT AFT END OF UPPER FLANGE. / REMOVED CORROSION ON INTERCOSTAL AT AFT CARGO STA 765 RBL 22.5; ORIG. 'T' .037' REM. .027' LOSS .005' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 146A7505 REV -

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT BULKHEAD SIDEWALL SUPPORT ANGLE CORRODED AT BS 947, BETWEEN RBL 22 TO RBL 26. R&R ANGLE IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 21R. R&R GUSSET IAW DWG & SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

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

Part: SUPPORT — CRACKED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STA 865 LBL16; SUPPORT CLIP AT BASE OF SIDEWALL VERTICAL SUPPORT IS CRACKED; MARKED. / REMOVED & REPLACED AFT CARCO FROM STA 865 LBL16 SUPPORT CLIP IAW B737-700 DWG 149A8102 REV:- ATAG: A85252

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500B, STR 25L. R&R CLIP IAW SRM AND EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT FORWARD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO PIT FWD CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11

Part: PLATE — CRACKED (AFT CARGO COMPT) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO PIT FLOOR PANEL 140AF LOWER HORSESHOE SUPPORT ANGLE IS CRACKED / ORDERED AND RECEIVED NEW STIFFENER PLATE P/N 453A2611-12 A 78725. REF: BAC DWG 453A2600 REV. E. PART TO BE INSTALLED ON CARD JPANEL-141-CLOSE (38146-1600-0022)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED BETWEEN BS 793 TO BS 810, RBL13.8. R&R FLOOR TRACK IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500C, STR 25L. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 727B+10 TO BS 727E. R&R "Z" ANGLE IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 827, STR 27L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 22. R&R ANGLE IAW SRM AND DWG.

Part: SPAR — CORRODED (LEFT WING) · airframe 68,000 hrs · 40,065 cycles

LEFT WING INBOARD LEADING EDGE CAVITY; FWD SPAR HAS CORROSION UNDER TOP BONDING WIRE ATTACH POINT FOR #1 TANK FWD BOOST PUMP. / BLENDED CORROSION ON L/H WING FWD BOOST PUMP AT UPPER BONDING WIRE ATTACH POINT. MEASURED AREA BY V.T. METHOD IN 1/4' AND FOUND REMAINING THICKNESS AT DEEPEST AREA TO BE .311'. BOEING FINDS THIS TO BE STRUCTURALLY ACCEPTABLE RESTORED SURFACE FINISH IAW EA 1-757-15469 REV IR AND EA 180470 IR. PERFORMED OPS CHECK OF BOOST PUMP IAW AMM 28-22-41-710-801 OPS CHECK GOOD.

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 68,000 hrs · 40,065 cycles

PASSENGER CABIN FLOOR BOARD 241BF IS CRUSHED AT FORWARD OUTBOARD CORNER / REPAIRED PASSENGER CABIN FLLOR BOARD 241BF AT FWD O/B CORNER I/A/W 737-700 SRM 53-00-50-2R-4 REV 65; SRM 53-00-50-2R-0 GENERAL REV 65.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 68,000 hrs · 40,065 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS 663, LBL 37. R&R WEB IAW EA.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 68,000 hrs · 40,065 cycles

RT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB INTERCOSTAL CRACKED. R&R INTERCOSTAL PER SRM AND DWG.

Part: ANGLE — CRACKED (LEFT WING) · airframe 68,000 hrs · 40,065 cycles

LEFT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB; UPPER FIXED PANEL; MID VERTICAL INTERCOSTAL; CURVED ANGLE IS CRACKED. / REMOVED AND REPLACED LEFT WING TRAILING EDGE INBD OF INBD DEFLECTOR RIB; UPPER FIXED PANEL; MID VERDICAL INTERCOSTAL; CURVED ANGLE IAW DWG 115A2953 REV- AND SRM 51-40-02

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 68,000 hrs · 40,065 cycles

PASSENGER CABIN FLOOR BOARD 231YF IS CRUSHED AT FORWARD INBOARD CORNER / REPAIRED PASSENGER CABIN FLOORBOARD 231YF AS MARKED I.A.W. SRM 53-00-50-2R-4 REV. 65, SRM 53-00-50-2R-0 REV 65

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 68,000 hrs · 40,065 cycles

RT WING NR 7 SLAT UPPER TRAILING EDGE WEDGE AT OUTBOARD MAIN TRACK DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,000 hrs · 40,065 cycles

RT AIR CONDITION PACK BAY AFT WALL BULKHEAD ANGLE STIFFENER CRACKED AT BS 663. R&R STIFFENER IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 68,000 hrs · 40,065 cycles

LT WING TRAILING EDGE PANEL ATTACH WAFFLE PLATE INBOARD OF PYLON COMMON TO REAR SPAR LOWER CHORD CRACKED. R&R WAFFLE PLATE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 68,000 hrs · 40,065 cycles

RIGHT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB; UPPER FIXED PANEL; MID VERTICAL INTERCOSTAL; CURVED ANGLE IS CRACKED. / REMOVED AND CRACKED CURVED ANGLE AT R/H WING TRAILING EDGE I/B OF I/B DEFECT OR REB UPPER FIXED PNL MID VERTICAL INTERCOSTAL IAW SRM 51-40-02-0G-0G-00. DRILLED NEW ANGLE IAW SRM 51-40-05-0G-00 AND BOEING DWG 115A2930. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-00 AND BOEING DWG 115A2930

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 68,000 hrs · 40,065 cycles

LT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB, INTERCOSTAL ATTACH ANGLE CRACKED. R&R CLIP IAW SRM & DWG.

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 68,000 hrs · 40,065 cycles

PASSENGER CABIN FLOOR BOARD 242AF IS CRUSHED ALONG AFT EDGE / REMOVED PASSENGER CABIN FLOORBOARD 242AF AT AFT EDGE AS MARKED I/A/W 737-700 SRM 53-00-50-2R-4 REV 65; SRM 53-00-50-2R-0 GENERAL REV 65.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 68,000 hrs · 40,065 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW EA.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 68,000 hrs · 40,065 cycles

RIGHT WING OUTBOARD LOWER LEADING EDGE DEFUEL PANEL 621EB INNER FWD SURFACE HAS DAMAGE TO THE COMPOSITE SURFACE (DELAM); MARKED. / REMOVED DOOR 621 EB AND REPAIR IAW BOEING 51-70-04-2R-13 REINSTALLED PANEL AND BOND TEST IAW BOEING 737 SRM 51-40-02-0G-0 AND SWPM 20-20-00 TABLE 53 BOND TEST PASSED METE AAR 30317 DUE 9-20-19

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 68,000 hrs · 40,065 cycles

LT HORIZONTAL STABILIZER 6TH RIB OUTBOARD FROM ROOT, 3RD STIFFENER BACK CRACKED AT STAB STA 120.3. REPAIRED RIB PER SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,000 hrs · 40,065 cycles

LT WING NR 4 SLAT AT ACTUATOR SLAT STATION 85.19 CRACKED AT FASTENER LOCATIONS. REPAIRED NR 4 SLAT SKIN IAW EA.

Part: FRAME — CRACKED (LWR FUSELAGE) · airframe 67,033 hrs · 39,445 cycles

EXTERNAL POWER RECEPTACLE SHROUD FWD SUPPORT FRAME CRACKED AT UPPER CORNER / REMOVE AND REPLACE PER SRM 51-10-02.

Part: SHROUD — CRACKED (LWR FUSELAGE) · airframe 67,030 hrs · 39,442 cycles

EXTERNAL POWER RECEPTACLE SHROUD CRACKED LOWER AFT CORNER SIDE WALL 2.5 INCHES LONG AROUND FASTENER HOLE / REMOVED AND REPLACED EXT PWR RECEPTACLE SHROUD PER SRM 51-40-02.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 66,904 hrs · 39,357 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE IAW MM.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 66,517 hrs · 39,106 cycles

RAMP REPORTS CRACK ON FLOOR PANEL 120CF IN FWD CARGO COMPARTMENT. / DMA # 0064610 R+R'D FLOOR LINER PER AMM 25-52-10 CL # 54703.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,199 hrs · 38,915 cycles

AFT GALLEY EMERGENCY LIGHT LENS BROKEN. R & R THE LENS SIP.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 65,699 hrs · 38,606 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE ASSEMBLY PER MT.

Part: RETAINER — OUT OF ADJUST (GIRT BAR) · airframe 65,410 hrs · 38,413 cycles

R1 DOOR SLIDE GIRT BAR HOOK OUT OF ADJUST. ADJUSTED THE RETAINER IAW AMM.

Part: BLEED VALVE — LOOSE (RT ENGINE) · airframe 65,351 hrs · 38,373 cycles

DURING CLIMB, AT APPROX. 25000 FT, THE RIGHT ENGINE EGT ROSE TO MID AMBER, EGT 875 DEGREE, AT CRUISE EGT ON RIGHT APPROX. 80 DEGREE HOTTER. ALSO CLIMB FROM 33000 TO 37000 RIGHT THROTTLE HAD TO BE RETARDED TO 95 DEGREE N, TO KEEP EGT OUT OF AMBER. DIVERTED. R & R VARIABLE BLEED VALVE IAW MT.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 64,959 hrs · 38,120 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD LOWER VERTICAL STIFFENER CRACKED AT BS 663. R & R THE STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 64,959 hrs · 38,120 cycles

LEFT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD LOWER VERTICAL STIFFENER CRACKED AT BS 663. R & R THE STIFFENER IAW SRM.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 64,629 hrs · 37,919 cycles

R2 DOOR EVACUATION SLIDE MANUAL PULL TAB COVER LOOSE. SECURED THE COVER IAW SIP.

Part: PROBE — FAULTY (RT ENGINE) · airframe 64,291 hrs · 37,711 cycles

DIVERSION, OIL QUANTITY INDICATION ON RT ENGINE. R&R EXHAUST GAS TEMPERATURE PROBE PER AMM.

Part: LENS — MISSING (CABIN) · airframe 62,337 hrs · 36,546 cycles

RT AFT EXIT LIGHT LENS MISSING. INSTALLED LENS PER AMM.

Part: FRAME — CRACKED (BS 294) · airframe 61,576 hrs · 36,102 cycles

RT SIDE STUB FRAME CRACKED AT BS 294, WL 208. R & R THE STUB FRAME IAW SRM.

Part: FRAME — CRACKED (BS 311) · airframe 61,576 hrs · 36,102 cycles

FRAME CRACKED AT BS 311, BETWEEN STRINGERS 5 - 6L. REPAIRED THE FRAME IAW EA.

Part: ATTACH BRACKET — CRACKED (RT WING FLAP) · airframe 61,576 hrs · 36,102 cycles

RIGHT WING FLAP DEFLECTOR BEAM INBOARD ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

L2 DOOR CREASE BEAM CORRODED BETWEEN BS 947+3 TO BS 986.5. R & R CREASE BEAM IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 61,576 hrs · 36,102 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, RBL 31. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 500) · airframe 61,576 hrs · 36,102 cycles

FORWARD CARGO BILGE ANTENNA SUPPORT CHANNEL CORRODED AT BS 500+11, BL 0. R & R THE CHANNEL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

RIGHT CREASE BEAM CORRODED BETWEEN BS 328 TO BS 344. R & R CREASE BEAM IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,576 hrs · 36,102 cycles

AFT CARGO JUST AFT OF THE FORWARD BULKHEAD LT SIDE TIE DOWN TRACK CORRODED AT BS 727B. R & R TIE DOWN TRACK IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

FLOORBEAM T-CAP CORRODED AT BS 986.5, BETWEEN RBL 45 TO RBL 17. R & R T-CAP IAW SRM.

Part: PLATE — CRACKED (AFT CARGO FRAME) · airframe 61,576 hrs · 36,102 cycles

AFT CARGO DOOR CUTOUT UPPER AFT STOP PLATE CRACKED. R & R THE STOP PLATE IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

FORWARD CARGO RT Z-ANGLE CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R & R Z-ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS 967-10 TO BS 987.5+3. R & R CREASE BEAM IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,576 hrs · 36,102 cycles

FORWARD CARGO TRACK TIE DOWN CORRODED AT BS 440-4, LBL 18. R & R FLOOR TRACK IAW SRM AND DWG.

Part: MOUNT BRACKET — CORRODED (L1 DOOR) · airframe 61,576 hrs · 36,102 cycles

L1 DOOR AFT GIRT BAR FLOOR FITTING MOUNT CORRODED AROUND THE FASTENER HOLES. R & R BRACKET IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

FLOORBEAM T-CAP CORRODED AT BS 986.5, LBL 45 TO LBL 24. REPAIRED T-CAP IAW EA AND SRM.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 61,576 hrs · 36,102 cycles

AFT CARGO RIGHT UNDER CARGO DOOR SCUFF PLATE CARGO TRACK CORRODED. R & R THE CARGO TRACK IAW SRM AND EA.

Part: DOOR FRAME — CORRODED (BS 303) · airframe 61,576 hrs · 36,102 cycles

L1 DOOR FORWARD FRAME CORRODED AT BS 303, BETWEEN STRINGERS 11 - 12L. R & R THE DOOR FRAME IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,576 hrs · 36,102 cycles

L1 DOOR CREASE BEAM CORRODED BETWEEN BS 344 TO BS 360. R & R CREASE BEAM IAW DWG AND SRM.

Part: MOUNT BRACKET — CORRODED (L1 DOOR) · airframe 61,576 hrs · 36,102 cycles

L1 DOOR FORWARD GIRT BAR FLOOR FITTING MOUNT CORRODED ROUND THE FASTENER HOLES. R & R BRACKET IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 61,576 hrs · 36,102 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 - 328, LBL 45. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 61,576 hrs · 36,102 cycles

MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD CRACKED AT BS 727, RBL 60. REPAIRED THE BULKHEAD IAW EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,945 hrs · 35,750 cycles

LEFT WING OTBD TE AFT FLAP LOWER SKIN DELAMINATED. REPAIRED FLAP IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 60,218 hrs · 35,329 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT LENS BROKEN. REPAIRED LENS IAW EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,988 hrs · 35,188 cycles

RIGHT OVERWING EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: ACTUATOR — FAULTY (NLG) · airframe 59,398 hrs · 34,861 cycles

NOSE LANDING WOULD NOT EXTEND. RECYCLED GEAR HANDLE & EXTENDED MANUALLY. R & R NLG LOCK ACTUATOR PART MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,438 hrs · 33,717 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

PANEL BRAKE ASSEMBLY CHANNEL CRACKED AT BS 540, BETWEEN RBL 0 TO RBL 24.5. R & R CHANNEL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 56,305 hrs · 33,053 cycles

RIGHT BULKHEAD WEB CRACKED AT BS 663.09. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LEFT SUPPORT ANGLE CRACKED ON WEB BULKHEAD INTERNAL AREA OF AIR CONDITIONING BAYS & BETWEEN LBL 6.15 TO LBL 43.80. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LEFT STIFFENER CRACKED AT WEB BULKHEAD BETWEEN LBL 6.15 TO 31.83. R & R STIFFENER IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,305 hrs · 33,053 cycles

LEFT BULKHEAD WEB CRACKED AT BS 663.09. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,305 hrs · 33,053 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,305 hrs · 33,053 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 633, LBL 35. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+2, RBL 24.75. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FLOORBEAM UPPER CHORD FWD SEAT TRACK CRACKED AT BS 727B+1, RBL 24.75. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+1, SIDE LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+1, RBL 45.5. REPAIRED CHORD IAW EA & EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+2, RBL 45.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FLOORBEAM FWD SEAT TRACK CRACKED AT BS 727B+1, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FRAME CRACKED AT BS 727B, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+1, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+1, RBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+2, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B+1, RBL 24.75. REPAIRED CHORD IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 907, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: LENS — BROKEN (EXIT SIGN) · airframe 56,305 hrs · 33,053 cycles

BROKEN EXIT SIGN LENS ON WALL AT AFT LAVATORY. R & R LENS ASSEMBLY IAW MM.

Part: SKIN — CRACKED (LT WING) · airframe 56,305 hrs · 33,053 cycles

LEFT WING NR 3 AFT FAIRING LOWER SURFACE CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

WEB CRACKED BETWEEN BS 344 TO 360, BL 0. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,305 hrs · 33,053 cycles

LEFT WING NR 3 LE SLAT SKIN CRACKED ON LOWER SURFACE AT ACTUATOR RIB STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,305 hrs · 33,053 cycles

EXTERNAL GND POWER ACCESS CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 56,305 hrs · 33,053 cycles

LEFT EEPLS CRACKED. R & R EEPLS IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 56,305 hrs · 33,053 cycles

RIGHT EEPLS CRACKED. R & R EEPLS IAW MM.

Part: LIGHT — FAULTY (CABIN) · airframe 56,197 hrs · 32,988 cycles

AFT LT EMER EXIT LIGHT MODULE FAULTY. R & R LIGHT IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,442 hrs · 32,531 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,345 hrs · 31,887 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,296 hrs · 31,856 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: GASKET — DAMAGED (NR 1 ENGINE) · airframe 54,093 hrs · 31,737 cycles

AIR TURN BACK, INFLIGHT SHUTDOWN, DECLARED ROLL BACK, NR 1 ENG ON CLIMB OUT UNABLE TO RESTART. R & R GASKET MAIN ENG FUEL LINE TO HMU IAW MM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 54,093 hrs · 31,737 cycles

AIR TURNBACK NR 1 LT ENG WAS SLIGHTLY MISMATCHED, ABOVE 1.5%, ON TAKEOFF. ON CLIMB OUT, LT ENG WOULD NOT GO ABOVE 86.3%. R & R MAIN FUEL PUMP IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 53,676 hrs · 31,486 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

NR 1 LT COCKPIT WINDOW POST FRAME CRACKED IN UPPER FASTENER HOLE. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,153 hrs · 31,176 cycles

RT HORIZONTAL STABILIZER RIB AT STATION 92.70, 4TH FROM FWD VERTICAL IN SPAR RIB CRACKED. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

FLIGHT DECK RT NR 1 FIXED WINDOW FRAME CUTOUT IN FRAME, UPPER OTBD CORNER, FRAME CRACKED. R & R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,153 hrs · 31,176 cycles

RT HORIZONTAL STABILIZER RIB AT STATION 92.70, 3 RD FROM FWD VERTICAL IN SPAR RIB CRACKED. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME, WINDOW CUTOUT IN FRAME, UPPER OTBD CORNER FRAME CRACKED. R & R FRAME IAW ACO. CORRECTED ATA & PART DEFECT LOCAL.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,153 hrs · 31,176 cycles

RT HORIZONTAL STABILIZER, RIB AT STATION 92.70, 2ND FROM FWD VERTICAL IN SPAR RIB CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,153 hrs · 31,176 cycles

RT HORIZONTAL STABILIZER RIB AT STATION 101.90, FIRST VERTICAL IN SPAR RIB CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,153 hrs · 31,176 cycles

LT HORIZONTAL STABILIZER RIB STABILIZER STATION 92.70, 18" AFT OF FWD SPAR, RIB CRACKED 1" ABOVE LOWER CHORD AT VERTICAL. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME CRACKED BETWEEN 2ND TO 4TH FROM LOWER FASTENER LOCATION ON EF POST. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,153 hrs · 31,176 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT 2ND FROM LOWER FASTENER LOCATION ON EF POST. REPAIRED FRAME IAW ACO.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,830 hrs · 30,989 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE IAW MT.

Part: BRACKET — BROKEN (RT WING) · airframe 52,683 hrs · 30,902 cycles

RT WING ANGLED BRACKET ATTACHED TO MID SPAN DEFLECTION CONTROL RIB BROKEN. R & R CLIP IAW DRAWING & SRM.

Part: SIGN — LOOSE (CABIN) · airframe 52,416 hrs · 30,738 cycles

EMERGENCY EXIT SIGN IN MID CABIN LOOSE. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,966 hrs · 29,288 cycles

RIGHT FIXED LANDING LIGHT INOP OKAY TO CONTINUE PER MEL 33-8-02 SP1 TRACKING #89195. REMOVED AND REPLACED RIGHT FIXED LANDING LIGHT BULB PER M/M. OPS CHECK GOOD. CLEARING #89413.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,307 hrs · 28,250 cycles

RIGHT WING O/B AFT FLAP DELAMINATED ON UPPER SURFACE I/B END. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 47,925 hrs · 28,019 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,328 hrs · 27,659 cycles

MID CABIN CEILING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,989 hrs · 26,271 cycles

DURING SCHEDULED BWI CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR CREASE BEAM Z-ANGLE CORRODED AT BS 967+12. REPAIRED Z-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 270 TO RBL 10. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: RAIL — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT ZEE RAIL CORRODED AT BS 727+15, RBL 3. REPAIRED ZEE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY CREASE BEAM CORRODED. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR CREASE BEAM Z-ANGLE CORRODED BETWEEN BS 947 TO BS 992.8. REPAIRED Z-ANGLE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 320. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING ADAPTER PLATE CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING ADAPTER PLATE CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERWING EMERGENCY EXIT SLIDE EXTERIOR LIGHT INOP. CONNECTED CONNECTOR PER MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK ON FLOOR SUPPORT STA 727E, LBL 17.4. REPAIRED CRACK PER SRM AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,559 hrs · 25,439 cycles

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

Part: ENGINE — FAILED (NR 1) · airframe 42,815 hrs · 25,015 cycles

ON CLIMBOUT NR 1 ENGINE FAILED. SHUTDOWN, AIR TURNBACK & DECLARED EMERGENCY. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LENS — MISSING (CABIN) · airframe 41,394 hrs · 24,163 cycles

LT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LENS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 39,715 hrs · 23,175 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT BATTERY CHARGING UNIT INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,715 hrs · 23,175 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEARING — WORN (AILERON CONTROL) · airframe 38,344 hrs · 22,356 cycles

ROLL CONTROL VERY STIFF WITH AUTOPILOT OFF, RUDDER TRIM ALSO SEEMS TO STICK BEFORE YOKE ADJUSTS TO INDEX. REMOVED AND REPLACED BEARINGS IN AILERON CONTROL WHEEL DRUM PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND UPPER CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED SHEAR TIE FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 12. REMOVED AND REPLACED BEAM PER AAR EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 BETWEEN LBL 7 TO LBL 8. REMOVED AND REPLACED BEAM PER AAR EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 BETWEEN RBL 2 TO RBL 3. REMOVED AND REPLACED BEAM PER AAR EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 BETWEEN LBL 2 TO LBL 3. REMOVED AND REPLACED BEAM PER AAR EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 BETWEEN RBL 7 TO RBL 8. REMOVED AND REPLACED BEAM PER AAR EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOOR ANGLE CORRODED AT BS 767, BETWEEN RBL 12 TO RBL 13. REPAIRED ANGLE PER SWA EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 37,290 hrs · 21,714 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOOR ANGLE CORRODED AT BS 767, LBL 20. REPAIRED ANGLE PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,566 hrs · 21,280 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,405 hrs · 21,183 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 35,258 hrs · 20,485 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE AFT ANCHOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,693 hrs · 20,106 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,574 hrs · 20,038 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,575 hrs · 20,038 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: CONTROL CABLE — BROKEN (LT SPOILER) · airframe 33,701 hrs · 19,505 cycles

CREW REPORTED CABLE SEEN DURING FLIGHT HANGING OUT AT LT WING. FOUND LT SPOILER CONTROL CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,125 hrs · 17,383 cycles

DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 ABC. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,125 hrs · 17,383 cycles

DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,125 hrs · 17,383 cycles

DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,125 hrs · 17,383 cycles

DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. R&R LIGHT BULB PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,125 hrs · 17,383 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOOR BEAM UPPER CHORD CRACKED AT BS 294.5, RBL 52. REPAIRED CHORD PER ER.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,125 hrs · 17,382 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CHAFED UNDER DORSAL FIN BS 925. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,125 hrs · 17,382 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAIRED FRAME PER SRM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 26,847 hrs · 15,528 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT ON TAKEOFF, DID NOT DEPLOY. RE-INSTALLED EVAC SLIDE PER MM.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 24,460 hrs · 14,195 cycles

L2 DOOR EVACUATION SLIDE CONTAINER ATTACH FASTENER LOOSE. SECURED FASTENER PER MM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 23,505 hrs · 13,659 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 21,304 hrs · 12,391 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,670 hrs · 10,335 cycles

RIGHT SIDE OVER WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 14,474 hrs · 8,579 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 AND NR 4 HINGE HARDWARE AND BUSHINGS PER SWA SI AND MM.

Part: COVER — CRACKED (CABIN) · airframe 13,853 hrs · 8,249 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, NR 5, NR 8, NR 13, NR 16 AND NR 18. REMOVED AND REPLACED COVERS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,727 hrs · 6,462 cycles

DURING SCHEDULED RON, FOUND EMERGENCY EXIT LIGHT INOP AT AFT OVERHEAD BULLNOSE. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 9,258 hrs · 5,563 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2. R&R COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 8,971 hrs · 5,379 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: INDICATOR — OBSCURED (ESCAPE SLIDE)

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LENS OBSCURED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: WIRE — CHAFED (LT MLG WW)

ABORTED TAKEOFF, 80 KNOTS DURING TAKEOFF, WARNING HORN SOUNDED. FOUND CHAFING WIRES TO NR 4 SKEW SENSOR CONNECTOR IN LT WHEEL WELL. REPAIRED WIRES PER WDM.

Part: SENSOR — ACTIVATED (EMERGENCY EXIT)

ABORTED TAKEOFF, PSEU LIGHT ILLUMINATED WHEN FLAP EXTENDED AND THRUST POWER APPLIED. C/W BITE CK, FAULT INFO SHOWED OVERWING DOORS DISAGREE PROBLEM. CYCLED BOTH OVERWING DOORS AND C/W FIM TASK. OPS CK GOOD.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE)

WHEN REDUCING POWER LEVERS FROM CLIMB TO CRUISE THRUST, ENGINES DEVELOPED A HARMONIC RESISTANCE RESULTING IN AIRCRAFT SHAKING AGGRESSIVELY. SHAKING STOPPED WHEN POWER WAS PULLED BACK DOWN TO 85 PERCENT N1. REMOVED AND REPLACED NR 2 ENGINE HMU AND AIRCRAFT VIBRATION MONITOR, (P/N 6672M213), (S/N DA72) PER MM.