N729SW

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,996 hrs · 44,802 cycles

AFT ENTRY ESCAPE SLIDE EMERGENCY LIGHT INOP ; / [01] R+R AFT ENTRY LEFT ESCAPE SLIDE EMERGENCY LIGHT FUSE AT POWER SUPPLY OPS OKAY PER AMM 33-51-06

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,533 hrs · 44,546 cycles

FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW ; / [01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY LIGHT LENS REF AMM 33-51-01.; [02] INSPECTION C/W

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,533 hrs · 44,546 cycles

RIGHT OVERWING EMERGENCY EXIT LOWER FWD LIGHT LENS MISSING DIRECTIONAL ARROW MISSING ; / [01] REMOVED AND REPLACED R/H OVER WING EMERGENCY EXIT FWD LIGHT LENS. REF. AMM. 33-51-01.; [02] INSPECTED

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,282 hrs · 43,810 cycles

LT OWE FWD EMERGENCY EXIT LIGHT, BULB INOPERABLE. RELAMPED LT OWE FWD EMERGENCY EXIT LIGHT BULBS AS NEEDED. PERFORMED GOOD FUNCTIONAL TEST, IAW AMM 33-51-01-960-801 STEPS 2B(1)(A)4);(C);(2) AND (4).

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,282 hrs · 43,810 cycles

RT OWE UPPER EMERGENCY EXIT LIGHT, BULB INOPERABLE. RE-LAMPED RT OWE UPPER EMERGENCY EXIT LIGHT BULBS AS NEEDED. PERFORMED GOOD FUNCTIONAL TEST, IAW AMM 33-51-01-960-801 STEPS 2B(1)(A)2);(C);(2) AND (4).

Part: ISOLATOR — DAMAGED (BS 360 S10L) · airframe 74,282 hrs · 43,810 cycles

DAMAGED ISOLATOR ON FRAME STA 360; AT STR 10 L/H. / REPLACED DAMAGED ISOLATOR ON FRAME STA 360 AT STR 10 L/H PER SRM 51-40-02-0G-0; REF IPC 53-11-00-56.

Part: FRAME — CRACKED (L1 DOOR) · airframe 74,282 hrs · 43,810 cycles

WHILE WORKING CRACK ON FWD ENTRY DOOR DISCOVERED FRAME TO BE CRACKED COMMON TO NR 7 STOP PIN ON AFT FRAME. THE DAMAGE WAS REPAIRED, PER ATS ER 20-03739 REV IR AND SWA EA 20-152-02598; REV IR. REFER TO NRC U251831 FOR TRACKING.

Part: ISOLATOR — DAMAGED (L1 DOOR) · airframe 74,282 hrs · 43,810 cycles

1 EACH DAMAGED ISOLATOR ON FWD ENTRY DOOR FWD MID UPPER COVE PANEL. / REMOVED AND REPLACED DAMAGED ISOLATOR ON FWD ENTRY DOOR; FWD MID UPPER COVE PANEL PER SRM 51-40-02-0G-0

Part: STRINGER — CRACKED (ZONE 100) · airframe 74,282 hrs · 43,810 cycles

FCB STRINGER 25L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 25L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 74,282 hrs · 43,810 cycles

RT NR 2 BIN EMERGENCY LIGHT LENS IS DAMAGED. INSTALLED A NEW RT NR 2 BIN EMERGENCY LIGHT LENS, PER AMM NR 33-51-03-960-801 STEP 2D ITEMS (1)(A)(C) 2666C 17DEC20.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 74,282 hrs · 43,810 cycles

CORROSION ON BS 259.5 LATERAL BEAM AFT FLANGE UPPER SURFACE WL 208.1 LBL 10 TO RBL 10. CORROSION WAS FOUND TO BE OUT OF LIMITS ON BS 259.5 LATERAL BEAM AFT FLANGE UPPER SURFACE WL 208 LBL 10 TO RBL 10. THE AREA WAS REPAIRED, PER EA 20-153-02588 REV IR & ATS ER 20-03719 REV IR. 56040C 04JAN21.

Part: CAP — MISSING (AFT DOOR SLIDE) · airframe 74,282 hrs · 43,810 cycles

AFT ENTRY DOOR SLIDE COVER BUMPER MISSING AFT END CAP. INSTALLED NEW BUMPER END CAP ON AFT ENTRY DOOR SLIDE COVER, PER SRM 51-40-02.

Part: ANGLE — CRACKED (BS 693) · airframe 74,282 hrs · 43,810 cycles

CRACKED VERTICAL ANGLE ON CABLE GUARD INTERCOSTAL BS 693 RBL 1 WL 204-208. / REMOVED AND REPLACED VERTICAL ANGLE ON CABLE GUARD INTERCOSTAL BS693 RBL1 WL204-208 IAW SRM 51-40-02-0G-0 PARA 4(B) AND DWG 273A9110

Part: STRINGER — CRACKED (ZONE 100) · airframe 74,282 hrs · 43,810 cycles

FCB STRINGER 27L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 27L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L.

Part: STRINGER — CRACKED (ZONE 100) · airframe 74,282 hrs · 43,810 cycles

FCB STRINGER 26R CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 26R AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L.

Part: STRINGER — CRACKED (ZONE 100) · airframe 74,282 hrs · 43,810 cycles

FCB STRINGER 26L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 26L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L.

Part: STRINGER — CRACKED (ZONE 100) · airframe 74,282 hrs · 43,810 cycles

FCB STRINGER 25R CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FWD CARGO BAY STR 25 RT AT BS 536 PER ER 20-03717 REV IR AND EA 21-153-00002 REV IR.

Part: WEB — CRACKED (PAX DOOR) · airframe 74,282 hrs · 43,810 cycles

FWD ENTRY DOOR INNER WEB IS CRACKED AFT FRAME AT NR 7 STOP PIN CUTOUT. FWD ENTRY DOOR INNER WEB CRACK AT AFT FRAME AT NR 7 STOP PIN CUTOUT WAS REPAIRED, PER ER 20-03739 REV IR, PER EA 20-152-02598 REV IR. REMOVABLE COMPONENT:P/N:141A6150-2M; S/N#000264.

Part: SKATE ANGLE — CHAFED (BS 1028) · airframe 74,282 hrs · 43,810 cycles

L/H AFT SKATE ANGLE CHAFFED BS 1028; LBL 12; WL 308 / REMOVED & REPLACED L/H AFT SKATE ANGLE BS1028 LBL12 WL308 IAW SRM'S 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; DWG 148A8300 SHT 1 REV C & AMM 51-21-99 56304U 22DEC20

Part: SKATE ANGLE — CHAFED (BS 1028) · airframe 74,282 hrs · 43,810 cycles

R/H AFT SKATE ANGLE CHAFFED BS 1028; RBL 12; WL 308; / REMOVED & REPLACED R/H AFT SKATE ANGLE BS1028 RBL 12 WL 308 IAW SRM'S 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 DWG 148A8300 SHT 1 REV C & AMM 51-21-99 56304U 22DEC20

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 74,282 hrs · 43,810 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255, RBL 4-LBL 14, WL 207.54. THE DAMAGE IS REPAIRED, PER EA 1-A53-33179 REV 1 AND EA 20-153-02588 REV IR. 56040C 04JAN21.

Part: NUT PLATE — BROKEN (RADOME) · airframe 74,097 hrs · 43,702 cycles

BROKEN NUTPLATE ON RADOME AT 6 OCLOCK POSITION / REMOVEED AND REPLACED NUTPLATE AT 6 OCLOCK POSITION IAW AMM 53-52-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,787 hrs · 43,500 cycles

CABIN EMERGENCY LIGHT INOPERABLE AT ROW 13DEF. RELAMPED EMERGENCY LIGHT AT ROW 13DEF IAW AMM 33-51-03.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 73,734 hrs · 43,465 cycles

EXTERNAL GROUND POWER RECEPTICAL DOOR SURROUND DOUBLER DAMAGED. REPAIRED PER SRM 53-10-15-2R-4. SEE ATTACHED SAM 326 FOR WORK IN PROGRESS DETAILS

Part: LENS — LOOSE (CABIN) · airframe 73,436 hrs · 43,270 cycles

EMERGENCY EXIT LIGHT LENS IS LOOSE 4ABC. SECURED LOOSE EMERGENCY LIGHT LENS PER AMM 33-51-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,994 hrs · 42,997 cycles

RES NRC D393391 CRACK IND FROM BS 706+7 TO 706+10 1' TO 2' ABOVE S-4L USING C SCAN 737 NDT MANUAL PART 6; 53-30-25 AND 737 NDT MANUAL PART 6; 53-30-18 / C/W EA 1-753-36731 REV IR; THIS IS A STAGE 1 APPROVED; CONTACT SERVICE ENGINEERING PRIOR TO THRESHOLD FOR STAGE 2 AND 3 REQUIREMENTS

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 71,995 hrs · 42,373 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 71,995 hrs · 42,373 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 71,995 hrs · 42,373 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 71,995 hrs · 42,373 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R&R BATTERY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,531 hrs · 42,079 cycles

LOGBOOK DEFECT NO.1250576 AIRCRAFT N729SW FOUND CORROSION AT STA.364 ON STRINGER 27R / FOUND CORROSION ON STR 27R TO BE 100% MATERIAL LOSS ON STR AND STR END FITTINGS REMOVED FABRICATED AND INSTALLED STR END FITTINGS IAW SRM 51-40-05 AND DWG 141A8513 SH 3 REV F CUT AND REMOVED DAMAGED STR AT STA 360+14' AND REPAIRED IAW EA 190834 REV P1 REV IR AND SWA EA 1-753-35756 REV IR NOTE STA 364 STR 27R AND W/L 160 P/N'S 141A8513-49 141A8513-51 AND 143A3241-5

Part: STRINGER — CORRODED (BS 364) · airframe 71,532 hrs · 42,079 cycles

STRINGER CORRODED AT BS. 364, STR. 27R. / REPAIRED STRINGER IAW EA.

Part: RETAINER — CRACKED (LT WING) · airframe 69,930 hrs · 41,035 cycles

LEFT WING TRAILING EDGE FIXED PANEL BEHIND NACELLE STRUT FAIRING CENTER SEAL RETAINER CRACKED / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 69,930 hrs · 41,035 cycles

RIGHT WHEEL WELL; RBL 26 VERTICAL STIFFENER CRACKED AT LOWER END. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02.

Part: LENS — MISSING (CABIN) · airframe 69,805 hrs · 40,955 cycles

RT EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 69,574 hrs · 40,798 cycles

RIGHT WING INBOARD LEADING EDGE JUST AFT OF #4 KRUGER FLAP HAS CRACKED SEAL RETAINER / REMOVED CRACKED SEAL RETAINER ON RIGHT WING I/B LEADING EDGE AFT OF #4 FRUGER FLAP. FACRICATE & INSTALLED NEW 116A2917-10 SEAL REATAINER IAW SRM 51-40-02-0G-0; 51-40-05-06-0; AMM 51-21-41-370-803; 51-21-72-370-804; 51-21-99-300-801; & DRG 116A2917 SHT 5

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, FORWARD WEB, LOWER SIDE INBOARD LOWER FLANGE FORWARD END FASTENER HOLE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

RT HORIZONTAL STABILIZER RIB STA 120.3, 4TH FROM FORWARD VERTICAL STIFFENER CRACKED. REPAIRED RIB IAW SRM.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 69,574 hrs · 40,798 cycles

WTB FAIRING PANEL 195CR HAS CRACK AT FWD END IN RADIUS / REPAIRED WTB FAIRING PANEL 195CR AT FWD END IN RADIUS IAW 3737-700-SRM 53-6070-2R-1 REPAIR 1 REV 66

Part: SUPPORT CHANNEL — CRACKED (RT WING) · airframe 69,574 hrs · 40,798 cycles

RT WING AFT LOWER PANEL SUPPORT CHANNEL CRACKED NEAR ORRS 288. R&R CHANNEL IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 69,574 hrs · 40,798 cycles

LT WING AFT SPAR WIGGLE PLATE CRACKED AT ORRS 261. R&R WIGGLE PLATE IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

RT HORIZONTAL STABILIZER RIB 120.30, THIRD FROM FORWARD VERTICAL STIFFENER CRACKED. R&R RIB IAW SRM & DWG.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

FORWARD CABIN FRAME FACTORY SPLICE CORRODED AT BS 294.5, STR 1. R&R SPLICE IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 69,574 hrs · 40,798 cycles

R/H A/C BAY STA 663; RBL 8 VERTICAL ATTACH ANGLE CRACKED / REMOVED VERTICAL STIFFNER RBL 8 STA 663 FWD SIDE OF VAPOR BARRIER IAW B737-700 SRM 51-40-02-0G-0. RECEIVED ANGLE P/N #38839-1700-0001. W/O: 38839-1700-0001; LOCATED AND DRILLED NEW ANFLE IAW B737-700 SRM 51-40-05-0H-0; INSTALLED THE NEW ANGLE IAW B737-700 SRM 51-40-02-0G-0 AND DWG #144A71 REV: A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

STRINGER CORRODED AT BS 365, STR 28L. REPAIRED STRINGER IAW SRM AND EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

E&E COMPARTMENT STRINGER SPLICE CORRODED AT BS 370, STR 25L. R&R SPLICE IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

E&E COMPARTMENT VERTICAL INTERCOSTAL CORRODED BETWEEN BS 351 TO BS 360, STR 28L. R&R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CORRODED (E & E COMPT) · airframe 69,574 hrs · 40,798 cycles

E/E COMPARTMENT STUB FRAME STA 336 ABOVE STR 23L WEB HAS CORROSION / EVALUATED CORROSION + FOUND TO BE 100% MATERIAL LOSS. OUT OF LIMITS. REMOVED STUB FRAME AT STA 336 ABOVE STR 23L WEB. FABRICATED AND INSTALLED NEW 141A1180-25 WEB IAW SRM 51-10-02-0G-0; 51-40-02-0G-0; AMM 51-21-41-370-803; 51-21-72-370-804 + DWG 141A1180 SHT 12 REV B P/N: 141A1180-25

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

E&E COMPARTMENT STUB FRAME LOWER CHORD ON VERTICAL AND SKIN FLANGE CORRODED AT BS 336, STR 23L. REPAIRED CHORD IAW SRM, DWG, AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

FLIGHT DECK BULKHEAD WEB AFT SIDE CRACKED AT BS 259.5, BETWEEN STR 12L TO STR 13L. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL STABILIZER RIB 67" OUTBOARD OF FUSELAGE CRACKED AT 4TH STIFFENER FROM FORWARD SPAR. REPAIRED RIB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

LT REAR SPAR VERTICAL PRESSURE DECK AT LOWER ANGLE CRACKED AT LBL 35. REPAIRED ANGLE IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, LBL 30. REPAIRED WEB IAW SRM.

Part: PANEL — CORRODED (LEFT WING) · airframe 69,574 hrs · 40,798 cycles

WING FUEL ACCESS PANEL 532BB HAS CORROSION ON EXTERIOR LIP. / EVALUATED LH WING FUEL ACCESS PANEL 532BB CORROSION ON EXTERIOR LIP IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7. REWORK WOULD EXCEED ALLOWABLE LIMITS ON ELECTRICAL BOND SURFACE AREA. ORDERED AND RECEIVED SERVICABLE PANEL FOR LH WING FUEL ACCESS PANEL 532BB. IAW B737 SRM 51-10-02-0G-0 STEP 9A(1) AND IPC 28-11-11-02. ATAG# NB1031

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL STAB LEADING EDGE PANEL 331B, NR 2 RIB FROM INBOARD TO OUTBOARD CRACKED. R&R NR 2 RIB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY AFT BULKHEAD SUPPORT ANGLE STRUCTURE CORRODED AT BS 947.5, BETWEEN RBL 20 TO RBL 10. R&R ANGLES PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY RT FORWARD FLOOR SHIELD CORRODED BETWEEN BS 767 TO BS 787+5. R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY AREA INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 807, RBL 6. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY BETWEEN STA 727B AND 727D R/H Z ANGLE IS CORRODED TOP SURFACE AS MARKED / REMOVED CORROSION I/A/W B737 SRM 51-10-02-0G-0. CHECKED LIMITS. ORIGINAL .040; LOSS .009 REMAINING .031 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIGURE 103D. REMOVED AND REPLACED WITH A NEW Z ANGLE BS727-BS767 R/H ON NRC 38837/1600/0018; DEFECT # X884264 P/N 146A7502-2

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY RT Z ANGLE CORRODED BETWEEN BS 727C TO BS 767. R&R Z ANGLE IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331B, NR 4 RIB FROM INBOARD TO OUTBOARD CRACKED. R&R RIB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

AFT CARGO BAY LT Z ANGLE CORRODED BETWEEN BS 727C TO BS 747+10. R&R Z ANGLE IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331B, NR 3 RIB FROM INBOARD TO OUTBOARD CRACKED. R&R RIB IAW SRM AND DWG.

Part: PANEL — CORRODED (RIGHT WING) · airframe 69,574 hrs · 40,798 cycles

WING FUEL ACCESS PANEL 632FB HAS CORROSION ON EXTERIOR LIP. / EVALUATED CORROSION ON EXTERIOR LIP OF RH WING FUEL ACCESS PANEL 632FB IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7. REWORK WOULD EXCEED ALLOWABLE LIMITS ON ELECTRICAL BOND SURFACE AREA. ORDERED AND RECEIVED SERVICABLE PANEL FOR RH WING FUEL ACCESS PANEL 632FB IAW B737 SRM 51-10-02-0G-0 STEP 9A(1) AND IPC 28-11-11-02. ATAG # NB1035

Part: ANGLE — CRACKED (FWD CARGO) · airframe 69,574 hrs · 40,798 cycles

FWD CARGO COMPARTMENT STA 500A LBL 22; INTERCOSTAL SUPPORT ANGLE IS CRACKED. / REMOVED AND REPLACED FWD CARGO INTERCOSTAL SUPPORT ANGLE STA 500A LBL 22 IAW B737 SRM 51-40-02-0G-0 PARA 4; DWG 143A 7SOS IP 0007 REV-

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

FORWARD CARGO COMPARTMENT LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 22 TO RBL 22. R&R SUPPORT IAW SRM.

Part: FLAP — DELAMINATED (L/H WING) · airframe 69,574 hrs · 40,798 cycles

DELAM FOUND ON L/H WING I/B MAIN FLAP LOWER SKIN LOCATED 10' FWD OF AFT EDGE AND 1.5' FROM O/B EDGE / UPON EVALUATION NOTED DISBOND ON L/H WING FLAP LOWER SKIN. ON FWD EDGE REPAIRED I.A.W. B737 SRM 51-70-10-2R1 AND 51.70.10.2R.0. RESTORED FINISH I.A.W AMM 51-21-99-300-801. DENT

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,574 hrs · 40,798 cycles

AFT PIT FLOORBOARD 140CF IS CORRODED / RECEIVED NEW AFT PIT FLOOR BOARD #140CF A-TAG# WN4156 PN #453A2610-2; ORIGINAL PANEL FOUND TO BE OUT OF LIMITS OF 100% IAW 53-00-53-1A-1 ALLOWABLE DAMAGE OF MORE THAN 3.0 INCHES MAXIMUM OF CORROSION STEP 5(1)B

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,574 hrs · 40,798 cycles

LT HORIZONTAL STABILIZER 67" FROM FUSELAGE, 27 1/8" AFT FROM FRONT SPAR, CRACKED IN THE RIB LOWER END 1" UP FROM SKIN. REPAIRED STABILIZER IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,574 hrs · 40,798 cycles

PASSENGER CABIN FLOORBOARD 231YF 2 EA CORNERS HAVE COMPOSITE DAMAGE / REPAIRED 2EA CORNER DAMAGE ON FLOOR PANEL 231YF IAW B737 SRM 53-00-50-2R-4.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT COMPARTMENT CAPTAINS FORWARD INBOARD SEAT TRACK BOTTOM LT SIDE SURFACE CORRODED. R&R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT DECK FIRST OFFICER INBOARD FORWARD SEAT TRACK CORRODED ON LOWER SIDE. R&R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT COMPARTMENT CAPTAINS FORWARD OUTBOARD SEAT TRACK LT SIDE SURFACES CORRODED. R&R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT COMPARTMENT CAPTAINS FORWARD OUTBOARD SEAT TRACK RT SIDE SURFACES CORRODED. R&R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT COMPARTMENT CAPTAINS FORWARD INBOARD SEAT TRACK BOTTOM RT SIDE SURFACE CORRODED. R&R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT DECK FIRST OFFICER OUTBOARD AFT SEAT TRACK CORRODED ON LOWER SIDE. R&R SEAT TRACK IAW AMM.

Part: TRACK — CORRODED (FLIGHT DECK FLOO) · airframe 69,574 hrs · 40,798 cycles

FLIGHT DECK. F/O INBOARD AFT SEAT TRACK CORRODED ON LOWER SIDE. / REMOVED AND REPLACED F/O I/B AFT SEAT TRACK IAW AMM 25-11-11-400-801 STEP 3. D WN3837

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 69,574 hrs · 40,798 cycles

FWD CARGO COMPARTMENT STA 420-440 RBL 21.5 RH Z-ANGLE HAS CORROSION ON UPPER SURFACE AT FASTENER HOLES; MARKED. / REMOVED CORROSION IAW SRM 51-10-02-0G-0; ORIGINAL MATERIAL .040'; LOSS .008'; MATERIAL REMAINING .032' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND INSTALLED A NEW SHIELD AT FORWARD CARGO COMPARTMENT IAW B737 SRM 51-40-02-0G-0 AND BNOEING DRAWING 143A0080 REV -; 143A8126 REV A P/N 143A8126-21

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,574 hrs · 40,798 cycles

FLIGHT DECK FIRST OFFICER OUTBOARD FORWARD SEAT TRACK CORRODED ON LOWER SIDE. R&R SEAT TRACK IAW AMM.

Part: WEB — DELAMINATED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

LT LOWER VAPOR BARRIER WEB HAD PREVIOUS REPAIR DELAMINATED AT BS 663. REPAIRED WEB IAW SRM.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,574 hrs · 40,798 cycles

RH WING LOWER LEADING EDGE PANEL 621DB IS DAMAGED / DELAMINATED ALONG FWD EDGE; MARKED. / REPAIRED DELAM DAMAGE ALONG FWD EDGE ON LWR WING PANEL 621DB I.A.W. B737 SRM 57-41-01-2R-1 AND 51-70-04-2R-10. REPAIRED ALUMINUM FOIL I.A.W. SRM 51-70-14-2R-3

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 69,574 hrs · 40,798 cycles

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

Part: COVER — MISSING (CABIN) · airframe 68,755 hrs · 40,269 cycles

RT EMERGENCY AISLE LIGHT COVER MISSING AT ROW 5. R&R COVER IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 68,714 hrs · 40,244 cycles

OVERWING CEILING EXIT SIGN FELL OFF. REINSTALLED LENS PER AMM.

Part: NONE — CRACKED (LWR FUSELAGE) · airframe 68,139 hrs · 39,874 cycles

SUPPLEMENTAL INFORMATION: WING TO BODY FAIRING PANEL 193B IS CRACKED AT FWD RIGHT CORNER / CLOSING DMA 0237600 REMOVED AND REPLACED PANEL 193B IAW AMM 53-51-21_CLR 94763

Part: NONE — CRACKED (LWR FUSELAGE) · airframe 68,139 hrs · 39,874 cycles

SUPPLEMENTAL INFORMATION: WING TO BODY FAIRING PANEL 193B IS CRACKED AT FWD RIGHT CORNER / COMPLIED WITH EA 1-753-33111. TRANSFERRED TO LOG PAGE# 0775210.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,116 hrs · 39,858 cycles

RT OVERWING EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 67,634 hrs · 39,539 cycles

IN DESCENT AS THE PLANE WAS LEVELING OFF AT FL 340 AND THROTTLES COMING UP, RIGHT ENGINE STAYED AT 40% AND BEGAN TO STALL (MILD CHUGGING) FROOM RIGHT ENGINE. R&R HYDRO MECHANICAL UNIT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,257 hrs · 38,708 cycles

FORWARD SERVICE DOOR EMERGENCY EGRESS LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 66,088 hrs · 38,610 cycles

LEFT WING NR 3 LEADING EDGE SLAT CRACKED OUT OF FASTENER HOLE. REPAIRED THE SLAT IAW EA.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 64,927 hrs · 37,903 cycles

R1 DOOR SLIDE GIRT BAR LOOSE IN HOLDER. SECURED THE GIRT BAR IAW SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,052 hrs · 37,380 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,052 hrs · 37,380 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,052 hrs · 37,380 cycles

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

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 64,052 hrs · 37,380 cycles

RIGHT VERTICAL PANEL 323CR HORIZONTAL RETAINER CRACKED / REMOVED AND REPLACED RIGHT VERTICAL PANEL 323CR HORIZONTAL RETAINER PER SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 64,052 hrs · 37,380 cycles

LEFT FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328. R & R THE FLOOR SUPPORT IAW SRM.

Part: BATTERY PACK — NO TEST (CABIN) · airframe 64,052 hrs · 37,380 cycles

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

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 64,052 hrs · 37,380 cycles

RIGHT VERTICAL PANEL 324AR VERTICAL RETAINER CRACKED / REMOVED AND REPLACED RIGHT VERTICAL PANEL 324AR VERTICAL RETAINER PER SRM 51-40-02

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 64,052 hrs · 37,380 cycles

RIGHT VERTICAL PANEL 324AR HORIZONTAL RETAINER CRACKED / REMOVED AND REPLACED RIGHT VERTICAL PANEL 324AR HORIZONTAL RETAINER PER SRM 51-40-02

Part: BATTERY PACK — DAMAGED (CABIN) · airframe 63,058 hrs · 36,739 cycles

RT EMERGENCY EXIT LIGHT INOP BETWEEN BS 380 TO BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,058 hrs · 36,739 cycles

LT EMERGENCY EXIT LIGHT INOP AT REAR WING TO BODY FAIRING. RECHARGED BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,058 hrs · 36,739 cycles

AFT GALLEY AREA EMERGENCY EXIT LAVATORY B LIGHT BULB INOP. R&R BULB IAW AMM.

Part: STRUCTURE — BROKEN (EMERGENCY LIGHT) · airframe 63,058 hrs · 36,739 cycles

FORWARD EMERGENCY EXIT CEILING PANEL BASE BROKEN AT BS. 627.5. R & R BASE IAW MM.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 63,058 hrs · 36,739 cycles

RIGHT WING INBD AND OTBD FLAP INBD AFT FLAP TRACK CORRODED. REPAIRED AFT FLAP TRACK IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 63,058 hrs · 36,739 cycles

RT WING FIXED TRAILING EDGE SUPPORT BRACKET CRACKED ON ORSS 273. R&R BRACKET IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

AFT GALLEY AREA ANGLE CORRODED AT BS 986.5, LBL 40. R&R ANGLE IAW SRM AND DWG.

Part: PLATE — CORRODED (CABIN) · airframe 63,058 hrs · 36,739 cycles

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

Part: PLATE — CORRODED (CABIN) · airframe 63,058 hrs · 36,739 cycles

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

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,058 hrs · 36,739 cycles

RT MAIN WHEEL WELL COMPARTMENT PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675.05, RBL 43. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,058 hrs · 36,739 cycles

LT WING LEADING EDGE NR 3 SLAT SKIN CRACKED ON LOWER SURFACE ACTUATOR AREA. R&R NR 3 SLAT PER AMM.

Part: STRUCTURE — CORRODED (BS 344-360) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA STRUCTURE CORRODED BETWEEN BS 344 TO 360, LBL 56. R & R THE STRUCTURE IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA FLOORBEAM CRACKED AT BS 294.5, RBL 52. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

R1 DOOR SUPPORT ANGLE CRACKED AT BS 294.5, STR 17R. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA WEB INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, LBL 34. REPAIRED INTERCOSTAL IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA INNER CHORD CORRODED BETWEEN BS 294.5 TO BS 328, RBL 56. R&R CHORD IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

STUB FRAME CRACKED AT BS 294.5, STR 17R. R&R STUB FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA FLOORBEAM CORRODED AT BS 987, BETWEEN LBL 45 TO RBL 45. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (BS 312-326) · airframe 63,058 hrs · 36,739 cycles

WEB STRUCTURE CRACKED BETWEEN BS 312 TO 326, RBL 29. R & R THE STRUCTURE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (GALLEY AREA) · airframe 63,058 hrs · 36,739 cycles

FLOORBEAM TEE FITTING CORRODED AT AFT GALLEY AREA RBL 47. R& R THE TEE FITTING IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FRAME CRACKED AT BS 907, BETWEEN STR 26R TO STR 25R. REPAIRED FRAME WEB IAW EA.

Part: INTERCOSTAL — CRACKED (BS 312-326) · airframe 63,058 hrs · 36,739 cycles

WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO 326, LBL 47. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD GALLEY AREA FLOOR BEAM CORRODED AT BS 328, RBL 45. REPAIRED FLOOR BEAM IAW EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 63,058 hrs · 36,739 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, LBL 25.2. R&R ANGLE IAW SRM AND DWG.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,058 hrs · 36,739 cycles

AFT GALLEY EMERGENCY LIGHT LENS BROKEN. R & R THE LENS IAW AMM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS 460 TO BS 500D, LBL 21.8. REPAIRED SUPPORT ZEE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, LBL 25.2. R&R ANGLE IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 63,058 hrs · 36,739 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,058 hrs · 36,739 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS 727C TO BS 807, LBL 21. R&R ZEE CHANNEL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO BAY SUPPORT CORRODED BETWEEN BS 727 TO 767, RBL 21. R & R THE SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRAP — CORRODED (BS 767) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO BAY STRAP CORRODED AT BS 767+5, BETWEEN STRINGERS 25L & 25R. R & R THE STRAP IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO COMPARTMENT STRAP CORRODED AT BS 887, BETWEEN STR 26L TO STR 25R. R&R STRAP IAW SRM AND DWG.

Part: STRAP — CORRODED (BS 727D) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO BAY STRAP CORRODED AT BS 727D+5, BETWEEN STRINGERS 25L & 25R. R & R THE STRAP IAW SRM AND DWG.

Part: ANGLE — CRACKED (WING TO BODY) · airframe 63,058 hrs · 36,739 cycles

WING TO BODY FAIRING SUPPORT STRUCTURE RT SIDE AT LOWER FUSELAGE ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,058 hrs · 36,739 cycles

AFT CARGO COMPARTMENT RT FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 63,058 hrs · 36,739 cycles

RIGHT SIDE EXTERNAL TAIL CONE SKIN DELAMINATED AT BS 1156+10. REPAIRED THE SKIN IAW SRM.

Part: LIGHT — CRAZED (CABIN) · airframe 63,058 hrs · 36,739 cycles

FORWARD EMERGENCY LIGHT CRAZED. R & R THE LIGHT IAW AMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 63,026 hrs · 36,720 cycles

R2 DOOR SLIDE LOOSE. REPOSITIONED THE SLIDE IAW MM.

Part: RIB — CRACKED (RT WING AILERON) · airframe 62,195 hrs · 36,236 cycles

RIGHT WING AILERON RIB CRACKED. REPAIRED RIB IAW EA.

Part: SUPPORT CHANNEL — CRACKED (LT WING) · airframe 62,195 hrs · 36,236 cycles

LEFT WING LOWER SUPPORT CHANNEL CRACKED. R & R THE SUPPORT CHANNEL IAW SRM AND SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,018 hrs · 34,992 cycles

LT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BUMPER — MISSING (R1 DOOR) · airframe 60,018 hrs · 34,992 cycles

R1 DOOR ESCAPE SLIDE COMPARTMENT BUMPER MISSING END CAP. INSTALLED END CAP PER SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

AFT SEAT TRACK AT FLOORBEAM OTBD ATTACH FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 57,379 hrs · 33,472 cycles

RIGHT MAIN WW REAR SPAR VAPOR BARRIER BETWEEN WW & RT A/C BAY, VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

FORWARD SEAT TRACK AT FLOORBEAM, SEAT TRACK TO SPLICE STRAP ATTACH FLANGES, INBD AFT, INBD FWD & OTBD AFT ATTACH FASTENER HOLES CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

SEAT TRACK OUTER ATTACH FLANGES, INBD & OTBD ATTACH FASTENER HOLES CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

AFT SEAT TRACK TO FLOORBEAM INBD ATTACH FLANGE ATTACH FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,379 hrs · 33,472 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 32 - 3. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

SEAT TRACK TO SPLICE STRAP ATTACH FLANGES, INBD & OTBD AFT ATTACH FASTENER HOLES CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

FUSELAGE FRAME CRACKED AT BS 559, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

FORWARD SEAT TRACK, OUTER ATTACH FLANGES TO SPLICE STRAP OTBD AFT, INBD FWD & INBD AFT ATTACH FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,379 hrs · 33,472 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 57,379 hrs · 33,472 cycles

LEFT WING NR 2 SLAT CRACKED AT FASTENER HOLE IN LOWER SKIN. REPAIRED NR 2 SLAT IAW SRM.

Part: WEB — CRACKED (L/H TNG) · airframe 57,379 hrs · 33,472 cycles

LEFT WING AFT OTBD, WING TO BODY FAIRING 193CL MOD WEB BETWEEN CHORDS CRACKED. R & R WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,379 hrs · 33,472 cycles

RIGHT WING NR 7 SLAT SKIN CRACKED AT LOWER FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 57,379 hrs · 33,472 cycles

RIGHT WING AFT OTBD, WING TO BODY FAIRING 193CR MOD WEB BETWEEN CHORDS CRACKED. R & R WEB IAW SRM.

Part: DOUBLER — CRACKED (LE SLAT) · airframe 57,379 hrs · 33,472 cycles

RIGHT WING NR 8 SLAT DOUBLER CRACKED AT FASTENER HOLE IN LOWER SKIN. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,379 hrs · 33,472 cycles

LEFT WING NR 1 SLAT CRACKED AT FASTENER HOLE IN LOWER SKIN, BELOW ACTUATOR. REPAIRED NR 1 SLAT IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,379 hrs · 33,472 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 57,379 hrs · 33,472 cycles

RIGHT WING OTBD AFT FLAP INBD LOWER CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,077 hrs · 33,304 cycles

RIGHT WING NR 6 SLAT CRACKED AT FASTENER HOLES IN LOWER SKIN. REPAIRED NR 6 SLAT IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,852 hrs · 32,592 cycles

R1 DOOR EXIT LIGHT FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,852 hrs · 32,592 cycles

RIGHT OVERWING EXIT LIGHT FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 55,100 hrs · 32,166 cycles

RIGHT OVERWING EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 53,420 hrs · 31,211 cycles

AFT EMERGENCY EXIT LIGHT BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,398 hrs · 31,200 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,341 hrs · 31,166 cycles

RT HORIZONTAL STABILIZER INTERCOSTAL RIB INBD FOURTH FROM FWD VERTICAL RIB INBD CRACKED AT STATION 92.7. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,341 hrs · 31,166 cycles

RT HORIZONTAL STABILIZER INTERCOSTAL RIB INBD THIRD FROM FWD VERTICAL RIB INBD CRACKED AT STATION 92.7. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,341 hrs · 31,166 cycles

RT HAND HORIZONTAL STABILIZER INTERCOSTAL RIB CRACKED AT STATION 92.7, LOWER FLANGE BELOW 1ST VERTICAL STIFFENER AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

FRAME CRACKED AT BS 540, STRINGER 22R. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,341 hrs · 31,166 cycles

RT HORIZONTAL STABILIZER INTERCOSTAL RIB INBD SECOND FROM FWD VERTICAL RIB INBD CRACKED AT STATION 92.7. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME AT EF POST CRACKED AT FASTENER HOLE FOURTH FROM BOTTOM. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME AT EF POST FASTENER HOLE, SECOND FROM BOTTOM, CRACKED. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,341 hrs · 31,166 cycles

LT WING OTBD AFT FLAP INBD DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

SKIN CHORD SPLICE CRACKED AT BS 540, STRINGER 22R. REPAIRED SPLICE IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

FLIGHT DECK RT NR 3 WINDOW FRAME EF POST CRACKED AT FASTENER HOLE SECOND FROM BOTTOM. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,341 hrs · 31,166 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,669 hrs · 30,179 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 50,506 hrs · 29,501 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 50,247 hrs · 29,336 cycles

LOWER EXIT SIGN LENS COVER L1 DOOR LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,997 hrs · 27,948 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

Part: HOOK — LOOSE (R2 DOOR) · airframe 47,997 hrs · 27,948 cycles

R2 DOOR EMERGENCY EVACE SLIDE CASE AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK ASSY PER SRM.

Part: LENS — CRACKED (EVAC SLIDE) · airframe 47,997 hrs · 27,948 cycles

R1 DOOR EMERGENCY EVAC SLIDE LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,091 hrs · 27,395 cycles

LEFT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BEAM — DAMAGED (RT HORIZ STAB) · airframe 46,848 hrs · 27,260 cycles

RIGHT HORIZONTAL STABILIZER CENTER SECTION FORWARD BEAM DAMAGED. REPAIRED IAW STABILIZER ASSY PER SRM.

Part: COVER — MISSING (EVAC SLIDE) · airframe 45,495 hrs · 26,446 cycles

R1 DOOR EMERGENCY EVAC SLIDE MANUAL RELEASE HANDLE VELCRO COVER MISSING. REMOVED AND REPLACED SLIDE IAW MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,784 hrs · 26,042 cycles

LEFT AFT EMER CHPR" CIRCUIT BREAKER POPPED. REMOVED AND REPLACED BATTERY CHARGER AND CONTROLLER PER MM.

Part: CONTROLLER — FAILED (CABIN) · airframe 44,785 hrs · 26,042 cycles

BATTERY RETAINERS FAILED AT EGRESS LIGHT CHARGER CONTROLLER M1672. REMOVED AND REPLACED CONTROLLER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 5 TO RBL 5. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 27 TO RBL 44. REPAIRED T-CAP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK FOUND, SKIN CORRODED AT BS 500 B+12 BETWEEN STRINGERS 27L AND 27R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX STA 540 RBL 32. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX STA 540 LBL 32. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX STA 540 LBL 52. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX STA 540 LBL 7. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX, STA 540 RBL 7. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX STA 540 LBL 14.5. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX, STA 540 RBL 14.5. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (CENTER WING BOX) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK VERTICAL BEAM SHEAR TIE WING BOX, STA 540 RBL 41. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

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

Part: BRACKET — MISSING (GIRT BAR) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET MISSING. INSTALLED BRACKET PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM INSIDE OF L1 DOOR CORRODED. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,920 hrs · 25,543 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,920 hrs · 25,543 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING O/B AFT FLAP I/B CORNER UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,666 hrs · 24,827 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,666 hrs · 24,827 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 42,101 hrs · 24,502 cycles

LT EMERGENCY EXIT LIGHT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 40,873 hrs · 23,804 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 39,398 hrs · 22,935 cycles

RIGHT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: ACTUATOR — FAULTY (ELEVATOR TAB) · airframe 38,856 hrs · 22,584 cycles

HYDRAULIC SYSTEM "A" REFILL SIGN ILLUMINATED. REMOVED AND REPLACED ELEVATOR TAB CONTROL ACUTATOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,495 hrs · 22,367 cycles

RIGHT EEPLS LOOSE FROM ROW 7 TO ROW 9. SECURED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 37,510 hrs · 21,752 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 36,385 hrs · 21,047 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,345 hrs · 21,021 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 36,079 hrs · 20,869 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 36,079 hrs · 20,869 cycles

R1 EMERGENCY EVAC DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: LUG — CORRODED (RT MLG) · airframe 35,649 hrs · 20,611 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION LOWER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,649 hrs · 20,611 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION UPPER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: STRIP — LOOSE (CABIN) · airframe 35,589 hrs · 20,569 cycles

FOUND EEPLS STRIP LOOSE BETWEEN ROW 6 TO ROW 7. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,305 hrs · 19,745 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS TRACK PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 34,305 hrs · 19,745 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM.

Part: BEARING — FAILED (LT ELEVATOR) · airframe 33,562 hrs · 19,303 cycles

DURING SCHEDULED HC1 CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR CONTROL BEARING PER MM.

Part: STRINGER — CRACKED (BS 520 S26L) · airframe 33,562 hrs · 19,303 cycles

DURING SCHEDULED HC1 CHECK, STRINGER 26L CORRODED AT BS 520. REPAIRED STRINGER PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,850 hrs · 18,256 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 31,386 hrs · 18,001 cycles

EEPLS LENS MISSING AT ROW 8 ABC. INSTALLED LENS PER MM.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 30,911 hrs · 17,699 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 39 TO RBL 41. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986, RBL 42 TO LBL 42. REPAIRED FLOORBEAM CHORD PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, BETWEEN RBL 7.5 AND LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 987, LBL 36. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1016, RBL 10. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,417 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1001, RBL 38. REMOVED AND REPLACED WEB PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 30,226 hrs · 17,293 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 29,908 hrs · 17,110 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 19 ABC. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,648 hrs · 14,677 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 25,582 hrs · 14,641 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,900 hrs · 12,588 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 19,032 hrs · 10,993 cycles

DURING SPV, FOUND BULKHEAD ANGLE STIFFENER AT BS 663, LBL 10 TO LBL 24, CRACKED. REMOVED AND REPLACED STIFFENER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,991 hrs · 10,969 cycles

DURING SPV, FOUND FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 17,802 hrs · 10,306 cycles

EEPLS STRIP COVER LOOSE AT ROW 1. SECURED EEPLS STRIP COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,866 hrs · 9,207 cycles

DURING SCHEDULED CHECK, FOUND EEPLS INOP AT ROW NR 18. RELAMPED EEPLS PER MM.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 15,633 hrs · 9,053 cycles

ABORTED TAKEOFF, WITH POWER LEVERS FWD, TAKEOFF WARNING HORN SOUNDED WITH SPEED BRAKES EXTENDED AND LIGHT ILLUMINATED. REMOVED AND REPLACED NR 9 SPOILER ACTUATOR AND SPEED BRAKE EXTEND LIGHT SWITCH PER MM.

Part: GIRT BAR — OUT OF ADJUST (L2/R2 DOORS) · airframe 14,397 hrs · 8,327 cycles

BOTH AFT CABIN DOOR EVACUATION SLIDE GIRT BARS WOULD NOT GO IN BRACKETS. REMOVED AND REPLACED BOTH EVACUATION SLIDE ASSY'S PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 13,838 hrs · 8,029 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55) FOUND RT ELEVATOR TAB NR 3 ATTACH HINGE BUSHING WORN. REMOVED AND REPLACED NR 3 ATTACH HINGE BUSHING PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 13,838 hrs · 8,029 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55) FOUND LT ELEVATOR TAB NR 4 ATTACH HINGE BUSHING WORN. REMOVED AND REPLACED NR 4 ATTACH HINGE BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 12,953 hrs · 7,535 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BEARING — WORN (ELEVATOR) · airframe 8,262 hrs · 4,887 cycles

DURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BEARINGS AT ELEVATOR TORQUE TUBE PER MM.

Part: LENS — MISSING (CABIN) · airframe 7,039 hrs · 4,204 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS RED LENS MISSING. INSTALLED RED LENS PER MM.

Part: PROBE — INOPERATIVE (EMPENNAGE) · airframe 6,411 hrs · 3,853 cycles

DIVERSION, LEFT ELEVATOR PITOT HEAT INOP. DIVERTED DUE TO DESTINATION WEATHER. REMOVED AND REPLACED PITOT HEAT PROBE PER MM. LEAK & OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 3,998 hrs · 2,439 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.