N734SA

Part: RIB — CRACKED (LT WING) · airframe 78,892 hrs · 46,684 cycles

CLIP-DEFLECTION CONTROL RIB IS CRACKED AT L/H WING TRAILING PANEL JUST OUTBOARD OF NR 3 FLAP TRACK. REMOVED AND REPLACED CLIP-DEFLECTION CONTROL RIB AT L/H WING TRAILING PANEL JUST OUTBOARD OF NR 3 FLAP TRACK PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 78,892 hrs · 46,684 cycles

FWD GALLEY SERVICE DOOR SLIDE GAUGE NOT COMPLETELY VISIBLE. REPOSITIONED FWD GALLEY SERVICE DOOR SLIDE IN COMPARTMENT PER MT725-61-06

Part: LIGHT — INOPERATIVE · airframe 76,559 hrs · 45,181 cycles

LH OVERWING EMERGENCY EXIT LIGHT HAS ONE BULB INOP. / [01] RESCUED LH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 76,045 hrs · 44,865 cycles

SUPPLEMENTAL INFORMATION: SLIDE OUT OF POSITION ; / [01] REPOSITION SLIDE TO LATCH VELCRO TO THE SLIDE CASE PER AMM 25-66-00

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 75,159 hrs · 44,311 cycles

RH OUTBD AFT FLAP; DELAMINATED ON INBD UPPER SURFACE. (HONEYCOMB IS SHOWING) ; / [01] REMOVED RH OUTBOARD AFT FLAP ASSY. PER AMM 27-51-22.; [02] INSTALLED RH OUTBOARD AFT FLAP ASSY.PER AMM 27-51-22; [03] REMOVED AND REPLACED T/E O/B AFT FLAP TRACKS #1;2;3;4 PER M/M 27-51-26

Part: SIGN — LOOSE (CABIN) · airframe 74,391 hrs · 43,875 cycles

PLACARD IN F/O SIDE EMERGENCY EXIT ROW KEEPS FALLING OFF. ; / R+R EMERGENCY EXIT SIGN PER AMM33-51-01

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 74,351 hrs · 43,856 cycles

FLIGHT ATTENDANT REPORTS FORWARD SERVICE DOOR GIRT BAR RETAINING HOLDER/CLIP IS LOOSE. ; / SECURED BRACKET HARDWARE PER AMM 25-66-02.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,269 hrs · 43,804 cycles

R/H EMERGENCY EXIT DOOR LIGHT INOP ; / REMOVED AND REPLACED LIGHT ASSEMBLY FUSE REF AMM 33-21-00

Part: PLATE — CORRODED (AFT CARGO) · airframe 74,151 hrs · 43,733 cycles

FOUND CORROSION ON AFT CARGO AFT SCUFF PLATE PANEL. REMOVED AND INSTALLED NEW PLATE AT AFT CARGO COMPT REF B737700 SRM 5140020G0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,151 hrs · 43,733 cycles

L/H STAB INSPAR RIB ASSY NO.4 AT STA 120.30 FWD LWR EDGE CRACKED / CUT OUT DAMAGE AREA; FABRICATED AND INSTALLED REPAIR AT L/H STAB RIB ASSY NO.4 STA 120.30 FWD LOWER EDGE PER RES-WI 2017205-5 REV P.1 AND IR AND SWA EA 21-155-00999 REV IR

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 74,151 hrs · 43,733 cycles

MAIN CABIN FLOOR PANEL 241DF BOTTON SIDE COMPOSITE DAMAGE AT 3 LOCATION / CLEANED FLOOR PANEL 241DF. REMOVED DAMAGE NO CORE DAMAGE NO WATER FOUND. INSTALLED A PERMANENT REPAIR ON BOTTOM SIDE OF PANEL3 PLACERS AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO# 1480720 PO# 1692653.

Part: CHANNEL — CRACKED (MAIN CABIN) · airframe 74,151 hrs · 43,733 cycles

MAIN CABIN WL 208.1 STA 540 BETWEEN BL 0 TO RBL 24 CHANNEL CRACKED. REMOVED N REPLACED CHANNEL BL0 TO RBL 24 STA 540 MAIN CABIN WL 208.1 REF B737700 SRM 5140020G0 CHANNEL INTERCOS PART NO. 7530771

Part: RIB — CRACKED (VERTICAL STAB) · airframe 74,151 hrs · 43,733 cycles

VERTICAL STAB DORSAL FIN FORWARDMOST RIB CRACKED. REMOVED AND REPLACED VERTICAL STAB DORSAL FIN FORWARDMOST RIB AS PER B737700 NDT PART 6 510000 PROC 23. BC 166317; SRM 5140020G0.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 74,151 hrs · 43,733 cycles

MAIN CABIN FLOOR PANEL 241AF TOP LAYER DELAMINATED / CLEANED AND REPAIRED SMALL AREAS OF TOP SURFACE DAMAGE ON MAIN CABIN FLOOR PANEL 241AF CAUSED BY CARPET REMOVAL AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO# 1486720 AND PO#1692653

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 74,151 hrs · 43,733 cycles

FOWARD CARGO LOWER DOOR CUT OUT AFT CONNER SCUFF PLATE IS CRACK RECIEVED SERVICEABLE REPAIRED AFT CONNER SCUFF PLATE PO# 1713374 AS PER B737 SRM 5330152R1 REPAIR 1. JL WELDING INC.

Part: FLOOR PANEL — DETERIORATED (AFT CARGO) · airframe 74,151 hrs · 43,733 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS DETERIORATED REMOVED; FABRICATED AND INSTALLED FLOOR PANEL 140 AF AT AFT CARGO AS PER B737700 AMM 255210000801; AMM 255201201801 AND AMM 255210400801

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,151 hrs · 43,733 cycles

RH HORIZONTAL STABILIZER LE FAIRING CRACKED @ RIB # 5 MKD DOT. REMOVED AND REPLACED RH HORIZONTAL STAB LE RIB #5 AS PER B7377 SRM 5140020G0 AND DWG#186A1001.

Part: SKIN — CRACKED (BS 291-294 S8-9R) · airframe 74,151 hrs · 43,733 cycles

CRACK INDICATION FOUND AT FASTENER AT R-1 DOOR CUTOUT BETWEEN STA 291.5 AND STA 294.5 BETWEEN STR 8R AND STR 9R. SEE FIG 4 AT FASTENER SHOWING TYPICAL CRACK. / ACCOMPLISHED INTERIM REPAIR PER RES-W1 2017205-2 REV P.1; P.2; IR AND EA 21-153-00875 IR AT R-1 DOOR CUT OUT BETWEEN STA 291.5 AND STA 294.5 BETWEEN STR 8R AND 9R.

Part: FLOOR PANEL — DETERIORATED (AFT CARGO) · airframe 74,151 hrs · 43,733 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF IS DETERIORATED REMOVED; FABRICATED AND INSTALLED FLOOR PANEL 140BF AT AFT CARGO AS PER B737700 AMM 255210000801; AMM 255201201801 AND AMM 255210400801

Part: FLOOR PANEL — DETERIORATED (FWD CARGO) · airframe 74,151 hrs · 43,733 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 120AF IS DETERIORATED REMOVED; FABRICATED & INSTALLED FLOOR PANEL #120AF FWD CARGO COMP AS PER REF B737 700 AMM 255201201801

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 74,151 hrs · 43,733 cycles

MAIN CABIN FLOOR PANEL 232SF TOP LAYER DELAMINATED / CLEANED AND REPAIRED PANEL #232SF AS PER B737-900 ER SRM 53-00-50-2R-1. MATERIALS USED FABRIC P/O #1480720 RESIN P/O 1692653

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 74,151 hrs · 43,733 cycles

MAIN CABIN FLOOR PANEL 231XF TOP LAYER DELAMINATED / REPAIRED DAMAGED AREA AT MAIN CABIN FLOOR PANEL 231XF TOOP LAYER. REF B737-7 SRM 53-00-50-2R-1

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,151 hrs · 43,733 cycles

L/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO. 3 CRACKED / REMOVED AND REPAIRED L/H HORIZONTAL STAB. NO.5 RIB AT STA 129.50 STIFFENER NO.3 AS PER B737-700 SRM 55-10-09-2R-4 REP 4 FIG 202 AND DWG NO. 55100003. REV B.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,151 hrs · 43,733 cycles

RH HORIZONTAL STAB ILIZER LE FAIRING CRACKED @ RIB # 4 MKD DOT. REMOVED AND REPLACED RH HORIZONTAL STAB LE RIB # 4 AS PER B7377 SRM 514002OG0 AND DWG #186A1001.

Part: FLOOR PANEL — DETERIORATED (FWD CARGO) · airframe 74,151 hrs · 43,733 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 120CF IS DETERIORATED REMOVED; FABRICATED & INSTALLED FLOOR PANEL #120CF FWD CARGO COMP. AS PER REF B737 700 AMM 255201201801

Part: TRUNNION — CRACKED (LT MLG) · airframe 74,151 hrs · 43,733 cycles

LEFT WING REAR SPAR FIXED TE LOWER SUPPORT BRACKET CRACKED INB OF MLG FWD TRUNNION MKD DOT. REMOVED AND REPLACE PLATE ASSY-WIGGLE AT LT WING IB OF MLG TRUNNION PER BOEING 737700 SRM 5140020G0.

Part: CUSP WEB — DEBONDED (LT MLGWW) · airframe 74,151 hrs · 43,733 cycles

L/H MAIN WHEEL WELL PRESSURE PANEL UPPER SURFACE IS DISBONDED AT 665667; LBL 6670. WL 203. REMOVED AND INSTALLED NEW CUSP WEB PANEL; CUSP GUSSET AND SEALS AT LH MAIN WHEEL PRESSURE PANEL UPPER SURFACE STA 663.75 TO STA 685 LBL 6670 WL 203 IAW B737700 SRM 5140020G0.

Part: SIGN — LOOSE (CABIN) · airframe 73,936 hrs · 43,603 cycles

EMERGENCY EXIT SIGN LOOSE. / TIGHTENED LOOSE SCREWS @ EMERGENCY EXIT SIGN PER AMM 20-50-11

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 73,133 hrs · 43,126 cycles

CABIN CREW REPORTS FWD SERVICE DOOR SLIDE FALLING OUT. REPOSITIONED FWD SERVICE DOOR SLIDE, IAW WIC 725-61-06.

Part: SLIDE — DISENGAGED (L1 DOOR) · airframe 73,056 hrs · 43,074 cycles

FWD ENTRY DOOR SLIDE LATCH ASSY DISENGAGED. R & R FWD ENTRY DOOR SLIDE, IAW WORK INSTRUCTION 725-61-06 ICT 551469 P/N OFF/ON 63550-101 S/NOFF 0426F, S/NON 0285F.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,027 hrs · 43,056 cycles

AFT SECTRON OF EGRESS LIGHTS INOP. R&R AFT LEFT BATTERY PACK, AS PER AMM 33-51-06.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 71,345 hrs · 42,021 cycles

EMERGENCY EXIT STRIP LIGHTING COVER LOOSE/OFF. ROW 6 L/H SIDE LENS MISSING 26975 BULL NOSE / INSTALLED LENS HOUSING ASSEMBLY PER MM.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 71,345 hrs · 42,021 cycles

EMERGENCY EXIT STRIP LIGHTING COVER LOOSE/OFF. ROW 6 L/H SIDE LENS MISSING 26975 BULL NOSE / INSTALLED LENS HOUSING ASSEMBLY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,095 hrs · 41,863 cycles

FORWARD ENTRY CENTER EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,726 hrs · 41,636 cycles

R/H EMERGENCY EXIT AISLE LIGHTS INOP BETWEEN SEAT ROW 16 TO ROW 17. / R&R POWER SUPPLY IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,725 hrs · 41,635 cycles

R1 DOOR ESCAPE SLIDE EMERGENCY HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

ALL FORWARD R/H EMERGENCY EXIT LIGHTS INOP AT LOCATION M1675. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

FORWARD LT EMERGENCY EXIT LIGHTS INOP AT LOCATION M1674. R&R BATTERY PACK IAW AMM.

Part: HOUSING — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

R2 DOOR EMERGENCY EXIT LIGHT HOUSING DAMAGED. R&R LIGHT HOUSING IAW AMM.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 69,540 hrs · 40,865 cycles

FLOOR PANEL 231YF APPEARS TO BE DISBONDING / REPAIRED FLOOR PANEL 231YF IAW AMM 53-21-00; SRM 53-00-50; AND DWG #144A5810-4

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 69,540 hrs · 40,865 cycles

FLOOR PANEL 241EF APPEARS TO BE DISBONDING / REPAIRED 241EF IAW AMM 53-21-00; SRM 53-00-50; AND DWG# 144A5810-10

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 69,540 hrs · 40,865 cycles

FLOOR PANEL 241BF APPEARS TO BE DISBONDING / REPAIRED FLOOR PANEL 241BF IAW AMM 53-21-00; SRM 53-00-50; AND DWG #144A5810-3T

Part: CREASE BEAM — CRACKED (MAIN CABIN) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM WEB IS CRACKED AT LIGHTNING HOLE; BS 469 RBL 65; WL 208 / REMOVED CRACK ON CREASE BEAM WEB LIGHTNING HOLE EDGE AT BS 469; RBL 65; WL 208 IAW SRM 53-30-13-1A-1 STEP 4A (1)(A) & SRM 51-10-02-0G-0. AFTER EVALUATE REWORK AREA IT WAS FOUND WITHIN LIMITS IAW SRM 53-30-13-1A-1 STEP 4A (E)(A) FIG 103 DETAIL A. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW 53-30-13-1A-1 STEPS 2C (1) & 2C(2). ACCOMPLISHED A HFEC INSP TO REWORKED AREA IAW 737 NDIM PT6 51-00-00 PROC 23; NO CRACKS NOTED.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

PANEL 191D HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE; IN THE CORE AREA. / DELAMINATED DENT ON THE EXTERNAL SURFACE HAS BEEN REPAIRED ON PANEL 191D IAW SRM 51-70-05-2R-2 59313U 05-09-19

Part: PRESSURE PANEL — DEBONDED (LT MLG WW) · airframe 69,540 hrs · 40,865 cycles

LT MAIN WHEEL WELL PRESSURE PANEL UPPER SURFACE DEBONDED BETWEEN BS. 665 TO BS. 667, BETWEEN LBL 66 TO LBL 70. REPAIRED PANEL PER ER & EA.

Part: ATTACH ANGLE — CORRODED (LT OW EXIT) · airframe 69,540 hrs · 40,865 cycles

***CORROSION*** ON L/H OVER WING EXIT LOWER SILL WEB ATTACH ANGLE BS 616-639 LBL68 WL221. / REMOVED AND REPLACED L/H OVERWING EXIT; LOWER SILL WEB ATTACH ANGLE WITH NEW ANGLE AT BS616-639 LBL 68 WL221 SRM 51-10-02-0G-0 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 SRM 51-20-01-0G-0 BOEING DWG 411A2820 AND 411A2854 13656R 11MAY19

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM WEB CORRODED BETWEEN BS. 380 TO BS. 400, LBL 67. REPAIRED CREASE BEAM WEB IAW EA & ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

SHEAR TIE CRACKED AT BS. 887 BETWEEN STR. 17L TO STR. 16L. R&R SHEAR TIE PER SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

MAIN WHEEL WELL ON PRESSURE DECK SHEAR TIE CORRODED BETWEEN BS. 665 TO BS. 668, BETWEEN LBL 65 TO LBL 68. R&R SHEAR TIE IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM WEB UPPER ATTACH ANGLE CORRODED AT BS. 668, RBL 67. R&R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

MAIN WHEEL WELL ON PRESSURE DECK SHEAR TIE CORRODED BETWEEN BS. 665 TO BS. 668, BETWEEN RBL 65 TO RBL 68. R&R SHEAR TIE PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 673 TO BS. 727+5, RBL 65. REPAIRED INNER CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 618 TO BS. 664, LBL 65. R&R INNER CHORD IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

CREASE BEAM WEB CORRODED BETWEEN BS. 710 TO BS. 713, RBL 65. REPAIRED CREASE BEAM WEB IAW EA & ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

UNDERSIDE OF CREASE BEAM WEB CORRODED BETWEEN BS. 658 TO BS. 655, LBL 65. REPAIRED WEB PER EA AND ER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

SEAT TRACK CORRODED BETWEEN BS. 552 TO BS. 727B, RBL 45. R&R SEAT TRACK SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

SEAT TRACK CORRODED AT BS. 520, LBL 45. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FRAME CRACKED AT BS. 312, STR. 5L, ABOVE UPPER SILL WEB. REPAIRED FRAME PER EA & ER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

SEAT TRACK CORRODED BETWEEN BS. 407 TO BS. 471, LBL 45. R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

SEAT TRACK CORRODED BETWEEN BS. 578 TO BS. 727A+6.5, RBL 25. R&R SEAT TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 69,540 hrs · 40,865 cycles

CRACKED INTERCOSTAL AT BS 278 STR 14 R/H I/B SIDE. / REPAIRED CRACKED INTERCOSTAL BS 278 STR 14 R/H I/B SIDE IAW EA# 1-753-34896 REV IR AND ER# 19-03070 REV IR.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

STRAP CORRODED BETWEEN BS. 291 TO BS. 294, STR. 5R. R&R STRAP IAW SRM & DWG.

Part: WEB — DAMAGED (FLIGHT DECK FLOO) · airframe 69,540 hrs · 40,865 cycles

COCKPIT FLOOR DAMAGED ON UPPER SURFACE BS257 270 RBL4-LBL 15 WL208. / REPAIRED DAMAGED COCKPIT FLOOR ON UPPER SURFACE BS 257-270 RBL 4- LBL 15 WL 208 PER EA 1-753-34787 REV IR AND ATS ER #19-02962 REV IR

Part: LIGHT — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

EMERGENCY EXIT LIGHT DAMAGED ON G4 GALLEY. R&R LIGHT IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,540 hrs · 40,865 cycles

LT HORIZONTAL STABILIZER LEADING EDGE CRACKED RIB AT LEADING EDGE STA. 150.20. R&R RIB IAW SRM AND DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 69,540 hrs · 40,865 cycles

RT HORIZ STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED R/H HORIZONTAL STAB UPPER FRONT SPAR CRACKED SLIDING SEAL IAW AMM 53-31-31-000-802 PAR 2D AND E AND 53-31-31-400-802 PAR 3EAND F. 57048U 08MAY19

Part: PANEL — DEBONDED (LH PYLON) · airframe 69,540 hrs · 40,865 cycles

#1 ENGINE PYLON PANEL 431ER LWR CORNER IS DISBONDED. / #1 ENGINE BYLON PANEL 431ER WITH LOWER CORNER DISBOND WAS REPLACED WITH A SERVICEABLE PYLON PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FORWARD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED ON THE FORWARD SIDE AT BS. 500C, RBL 24. REPAIRED BAFFLE CLIP PER SRM AND DWG.

Part: LENS — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

RT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #8. R&R LENS IAW AMM & SIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FORWARD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500C, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.

Part: LENS — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #6. R&R LENS IAW AMM & SIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500B, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.

Part: LENS — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #4. R&R LENS IAW AMM & SIP.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 23. R&R SHIELD PER SRM AND DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 747 TO BS. 807, LBL 23. R&R SUPPORT IAW SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FORWARD CARGO BAY LT FLOOR TO SIDE WALL SUPPORT PLATE CORRODED BETWEEN BS. 500A TO BS. 500C, LBL 23. R&R SUPPORT IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 69,540 hrs · 40,865 cycles

RT HORIZONTAL PRESSURE WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 39 TO RBL 60. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500C, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.

Part: LENS — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #1. R&R LENS IAW AMM & SIP.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 69,540 hrs · 40,865 cycles

LT HORIZONTAL PRESSURE WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 45. REPAIRED WEB IAW SRM.

Part: LENS — DAMAGED (CABIN) · airframe 69,540 hrs · 40,865 cycles

RT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #11. R&R LENS IAW AMM & SIP.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS. 927 TO BS. 947, RBL 3 ON FORWARD END. R&R VERTICAL WEB PER SRM & DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. R&R SUPPORT PLATE PER SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS772 RBL10 TO LBL10 WL156 HAS AREAS OF CORROSION / RECEIVED NEW ACB FLOOR SPLICE STRAP B.S 772 ON PO# 717082 NEW PART WILL BE INSTALLED ON CUST CARD # JPANEL-141-CLOSE

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS727D+6 RBL10 TO LBL10 WL156 HAS AREAS OF CORROSION / RECIEVED NEW ACB FLOOR SPLICE STRAP FOR B.S 727D+6 ON PO# 724358 PART WILL BE INSTALLED ON CUST. CARD # JPANEL-141-CLOSE

Part: RETAINER — CRACKED (RIGHT WING) · airframe 69,540 hrs · 40,865 cycles

RT WING UPPER T/E PANEL HORIZ SEAL RETAINER IS CRACKED; JUST AFT OF #2 PYLON. / REMOVED AND REPLAED R/H WING UPPER T/E PANEL CRACKED HORIZONTAL SEAL RETAINER AFT OF #2 PYLON IAW SOPM 20-50-01; SRM 51-40-02-0G-0 AND IPC 57-50-00-25. 57048U 02MAY19

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY FLOOR SPLICE STRAP CORRODED AT BS. 887, BETWEEN RBL 10 TO LBL 10. R&R FLOOR SPLICE STRAP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,540 hrs · 40,865 cycles

AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS. 827 TO BS. 847, RBL 6. R&R WEB PER SRM & DWG.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 69,540 hrs · 40,865 cycles

RT LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 45 TO RBL 55. R&R BARRIER IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 69,540 hrs · 40,865 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS. 663, LBL 8. REPAIRED ANGLE PER ATS ER AND EA.

Part: COVER — DISCOLORED (EXIT SIGN) · airframe 69,540 hrs · 40,865 cycles

R1 DOOR EXIT LIGHT COVERS DISCOLORED. R&R COVER IAW AMM.

Part: LENS — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

L1 DOOR UPPER EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,540 hrs · 40,865 cycles

RT WING #8 SLAT CRACKED AROUND THE FASTENER AT LOWER SURFACE OF SLAT NOSE SKIN AT ACTUATOR RIBS. REPAIRED #8 SLAT IAW SRM.

Part: SIGN — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

LOWER L2 DOOR EXIT SIGNS DISCOLORED. R&R SIGNS IAW AMM.

Part: COVER — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

L2 DOOR EMERGENCY LIGHT COVER DISCOLORED. R&R COVERS IAW AMM.

Part: COVER — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

R2 DOOR EMERGENCY LIGHT COVER DISCOLORED. R&R COVERS IAW AMM.

Part: SIGN — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

UPPER L2 DOOR EXIT SIGNS DISCOLORED. R&R SIGNS IAW AMM.

Part: LENS — DISCOLORED (CABIN) · airframe 69,540 hrs · 40,865 cycles

L1 DOOR LOWER EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 69,444 hrs · 40,803 cycles

EXT LIGHT LENS NEAR L1 DOOR BROKEN. / R&R EXIT LIGHT LENS PER AMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 69,331 hrs · 40,732 cycles

R2 DOOR SLIDE PACK FELL FROM CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: CIRCUIT BREAKER — TRIPPED (CABIN) · airframe 69,259 hrs · 40,687 cycles

AFT GALLEY CEILING EXIT "EXIT SALIDA" LIGHTS INOP. RESET CIRCUIT BREAKER P18-3 IAW AMM.

Part: CIRCUIT BREAKER — TRIPPED (CABIN) · airframe 69,259 hrs · 40,687 cycles

FORWARD GALLEY OVERWING EXIT "EXIT SALIDA" LIGHTS INOP. RESET CIRCUIT BREAKER P18-3 IAW AMM.

Part: FLAP — DAMAGED (LT WING) · airframe 69,073 hrs · 40,571 cycles

LT WING INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACKED. R&R AFT FLAP IAW AMM.

Part: FLAP — DAMAGED (LT WING) · airframe 69,073 hrs · 40,571 cycles

LT INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACK 21" INBOARD + 2 INCHES FROM TRAILING EDGE. R&R AFT FLAP IAW AMM.

Part: FLAP — CRACKED (LT WING) · airframe 69,073 hrs · 40,571 cycles

LT WING INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACK 21" INBOARD AND 2 INCHES FROM TRAILING EDGE. REPAIRED AFT FLAP IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,387 hrs · 40,132 cycles

LT WING NR 2 SLAT SKIN CRACKED AFT OF ACTUATOR. REPAIRED NR 2 SLAT SKIN PER EA.

Part: COVER — LOOSE (CABIN) · airframe 67,717 hrs · 39,712 cycles

RT EMERGENCY LIGHT COVER LOOSE AT ROW 3. SECURED COVER PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,577 hrs · 39,622 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,577 hrs · 39,622 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 66,667 hrs · 39,014 cycles

RT EMERGENCY EXIT LENS ASSEMBLY BROKEN AT ROW 18. R&R LENS PER SIP.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 66,667 hrs · 39,014 cycles

SUPPLEMENTAL INFORMATION: FWD CORNER SECTION SCUFF PLATE OF THE AFT CARGO COMPARTMENT IS CRACKED. / REMOVED AND REPLACED REF AMM 53-11-02.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,932 hrs · 36,695 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON UPPER SURFACE. R & R THE AFT FLAP IAW AMM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 62,932 hrs · 36,695 cycles

LEFT WING TO BODY FAIRINGS AFT EMERGENCY EXIT LIGHT LENS DIRTY. CLEANED THE LENS IAW SOPM.

Part: GUSSET — CRACKED (BS 500D) · airframe 62,932 hrs · 36,695 cycles

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

Part: STRAP — CORRODED (BS 276-298) · airframe 62,932 hrs · 36,695 cycles

R1 DOOR SILL VERTICAL FLANGE TAPERED STRAP CORRODED BETWEEN BS 276 TO 298. R & R THE STRAP IAW SRM.

Part: WEB — CORRODED (BS 850) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE INTERCOSTAL WEB CORRODED AT BS 850, RBL 24.5. R & R THE WEB IAW DWG & SRM.

Part: STRAP — CORRODED (BS 847) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY DOOR SURROUND STRAP CORRODED AT BS 847, RBL 24.5. R & R THE STRAP IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 867-917) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 917, RBL 24.5. R & R THE SIDEWALL SUPPORT IAW DWG.

Part: SUPPORT — CORRODED (BS 420-440) · airframe 62,932 hrs · 36,695 cycles

FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 420 TO 440, RBL 25. R & R THE SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 62,932 hrs · 36,695 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 25. R & R THE SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 492-500A) · airframe 62,932 hrs · 36,695 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 TO 500A, RBL 25. R&R SIDEWALL SUPPORT IAW SRM.

Part: SHIELD — CORRODED (BS 857) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE AFT SHIELD CORRODED AT BS 857, RBL 24.5. R & R SHIELD IAW SRM.

Part: SHIELD — CORRODED (BS 787) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE FORWARD SHIELD CORRODED AT BS 787, RBL 24.5. R & R SHIELD IAW SRM.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 62,932 hrs · 36,695 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO 500D, LBL 25. R & R THE SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727C-767) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO 767, RBL 24.5. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 62,932 hrs · 36,695 cycles

RIGHT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, RBL 25. R & R THE SUPPORT ANGLE IAW DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 62,932 hrs · 36,695 cycles

LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 TO RBL 25. R & R THE SUPPORT ANGLE IAW SRM.

Part: STRAP — CORRODED (BS 787-797) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE BOTTOM STRAP CORRODED BETWEEN BS 787 TO 797, RBL 24.5. R & R THE STRAP IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727D-807) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO 807, LBL 24.5. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: ATTACH ANGLE — CORRODED (BS 767) · airframe 62,932 hrs · 36,695 cycles

AFT CARGO BAY FRAME ATTACH ANGLE CORRODED AT BS 767, RBL 24.5. R & R THE ATTACH ANGLE IAW SRM.

Part: SIDEWALL SUPPORT — CRACKED (BS 847) · airframe 62,932 hrs · 36,695 cycles

SIDEWALL PANEL SUPPORT ANGLE CRACKED AT BS 847, LBL 9. R & R SIDEWALL SUPPORT ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,932 hrs · 36,695 cycles

AFT EDGE OF COOLING FAN EXHAUST CUTOUT SKIN CRACKED AT BS 380, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER EA.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 62,932 hrs · 36,695 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 62,932 hrs · 36,695 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, RBL 12. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 62,932 hrs · 36,695 cycles

FLOORBEAM UPPER FLANGE TEE CORRODED AT BS 986, WL 208. REPAIRED THE FLOORBEAM TEE IAW ER.

Part: SCUFF PLATE — CRACKED (CARGO DOORWAY) · airframe 62,932 hrs · 36,695 cycles

FORWARD CARGO BAY DOOR CUTOUT CENTER SCUFF PLATE CRACKED AT BS 450. REPAIRED THE SCUFF PLATE IAW EA.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 62,932 hrs · 36,695 cycles

LEFT WING LEADING EDGE NR 3 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING. REPAIRED THE SKIN IAW SRM.

Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 62,932 hrs · 36,695 cycles

AFT LOWERED CEILING EMERGENCY EXIT LIGHT HOUSING CRACKED. R & R THE LIGHT IAW SOPM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,525 hrs · 36,464 cycles

LEFT EMERGENCY AISLE LIGHT BATTERY PACK M1670 FAILED CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,525 hrs · 36,464 cycles

EMERGENCY LIGHT BATTERY PACK M1668 FAILED CHECK AT BS 500C. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,525 hrs · 36,464 cycles

LT ABOVE OVERWING EMERGENCY LIGHT BATTERY PACK M1668 FAILED CHECK AT BS 500C. R&R BATTERY PACK IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,725 hrs · 35,978 cycles

RIGHT CABIN EXIT LIGHT LENS MISSING BETWEEN ROWS 5 & 6. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,651 hrs · 35,344 cycles

RT MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW SIP.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 60,468 hrs · 35,240 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT FITTING. R&R SLIDE ASSEMBLY PER MT.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 60,468 hrs · 35,240 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT FITTING. R&R SLIDE ASSEMBLY PER MT.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 59,148 hrs · 34,470 cycles

AFT PRESS BULKHEAD AREA OF OIL CANNING AT BS 1016, BETWEEN BL 0 & STRINGER 3L, EXTEND FROM UPPER Y CHORD, 10" DOWN & OVER OUTER STRAP. REPAIRED BULKHEAD IAW SRM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 58,951 hrs · 34,354 cycles

DURING CRUISE, CAPTAINS FWD WINDSHIELD L1 ARCED. R & R L1 WINDOW IAW MM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 57,564 hrs · 33,529 cycles

LEFT MAIN WW LT ANGLE STIFFENER CRACKED AT BS 663 BULKHEAD FWD SIDE. R & R STIFFENER IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

AFT SEAT TRACK TO FLOORBEAM, ATTACH FASTENER HOLES OUTBOARD FLANGE HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

FORWARD SEAT TRACK TO SPLICE PLATE ATTACH FASTENER HOLES, INBOARD & OUTBOARD AFT HOLES CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

FORWARD SEAT TRACK TO SPLICE PLATE ATTACH FASTENER HOLES, INBOARD AFT & OUTBOARD FORWARD & AFT HOLES CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

AFT SEAT TRACK TO FLOORBEAM ATTACH FASTENER HOLE, OUTBOARD FLANGE HOLE CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 57,564 hrs · 33,529 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 25.75. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 57,564 hrs · 33,529 cycles

RIGHT WING NR 6 SLAT CRACKED AROUND FASTENERS THAT ATTACH THE ACTUATOR FITTING. REPAIRED NR 6 SLAT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,564 hrs · 33,529 cycles

LEFT MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED IN VERTICAL STIFFENER, 10" AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

NUMBER 3 RIGHT WINDOW FRAME AT E - F POST, AT SECOND LOWER CORNER HOLE CRACKED. REPAIRED POST IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED IN VERTICAL STIFFENER, 20" AFT OF FWD SPAR. REPAIRED STIFFENER IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 101.90, CRACKED IN LOWER SURFACE 20" AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

SKIN CRACKED AT BS 540, LEFT SIDE. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 101.90 IN VERTICAL STIFFENER & LOWER FLANGE 10" AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 129.50 CRACKED IN VERTICAL STIFFENER, 10" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 147.90 CRACKED IN VERTICAL STIFFENER, 30" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70 CRACKED IN VERTICAL STIFFENER, 40" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,564 hrs · 33,529 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70 CRACKED IN VERTICAL STIFFENER, 30" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,564 hrs · 33,529 cycles

RIGHT NR 1 FLIGHT DECK CRACKED IN UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,441 hrs · 32,902 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW WDM & AMM 6.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,441 hrs · 32,902 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW WDM & AMM 6.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 54,968 hrs · 32,058 cycles

L1 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 54,467 hrs · 31,765 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,392 hrs · 31,730 cycles

BULKHEAD CHORD CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,392 hrs · 31,730 cycles

SKIN CRACKED AT BS 540 BELOW STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,392 hrs · 31,730 cycles

SKIN CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,791 hrs · 31,393 cycles

RIGHT LOWER OVERWING EMER EXIT LIGHTS BULB INOPERATIVE. RE LAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,791 hrs · 31,393 cycles

LEFT LOWER OVERWING EMER EXIT LIGHT BULB INOPERATIVE. RE LAMPED LIGHT IAW AMM.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 53,791 hrs · 31,393 cycles

AFT CARGO DOOR CUT OUT LOWER AFT THRESHOLD CRACKED. REPAIRED THRESHOLD IAW EA.

Part: LENS — MISSING (CABIN) · airframe 53,456 hrs · 31,196 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 52,653 hrs · 30,725 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 52,218 hrs · 30,485 cycles

AFT CABIN EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 52,218 hrs · 30,485 cycles

FWD CABIN EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,779 hrs · 30,211 cycles

FLANGE CRACKED AWAY WHERE INTERCOM PANEL DOOR MEETS FUSELAGE ON AFT FUSELAGE EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,844 hrs · 29,646 cycles

LT WING INBD MAIN FLAP DELAMINATED ON UPPER SURFACE. REPAIRED MAIN FLAP IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,844 hrs · 29,646 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME ON E-F POST, SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW SWA EA.

Part: FAIRING — CRACKED (LT WING) · airframe 50,844 hrs · 29,646 cycles

LT WING TE PANEL ATTACH STRUCTURE WAFFLE PLATE CRACKED BEHIND NR 2 PYLON FAIRING. R&R FAIRING IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 50,844 hrs · 29,646 cycles

CENTER WING VERTICAL PRESSURE DECK WEB CRACKED AT STATION 663, BETWEEN RBL 36 - RBL 46. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,844 hrs · 29,646 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME ON E-F POST, SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW SWA EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 49,432 hrs · 28,798 cycles

CRACK ON AFT CARGO DOOR FRAME BOTTOM MOD. FOUND CENTER SCUFF PLATE DAMAGES AT FWD EDGE 1" IN LENGTH X 1/16" WIDTH. OK TO CONTINUE PER EA 1-A53- 2389 PERFORM VISUAL INSPECTION EVERY 10 DAYS OR 100 FLT HRS FOR SPEED TAPE CONDITION. ACCOMPLISH

Part: TIRE — BLOWN (LT MLG) · airframe 46,647 hrs · 27,138 cycles

DECLARED EMERGENCY -- AFTER T/O, FELT VIBRATION DUE TO NR 2 LT MLG BLOWN TIRE. REMOVED AND REPLACED BOTH LT MLG TIRE/WHEEL ASSY'S PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,139 hrs · 26,854 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT PER AMM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 45,998 hrs · 26,770 cycles

WINDSHIELD R1 ARCED AND SHATTERED. REMOVED AND REPLACED R1 WINDOW HEAT CONTROLLER PER MM.

Part: LIGHT — DIRTY (CABIN) · airframe 45,866 hrs · 26,684 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS DIRTY. CLEANED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,866 hrs · 26,684 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,866 hrs · 26,684 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT BATTERY CHARGERS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,866 hrs · 26,684 cycles

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

Part: HOLDER — LOOSE (GIRT BAR) · airframe 45,144 hrs · 26,282 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MT.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM ANGLE CORRODED AT BS 984, RBL 48. REPAIRED ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

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

Part: WEB — CORRODED (CARGO BAY) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND FORWARD CARGO DOOR CUTOUT WEB CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z ANGLE CORRODED BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 747 TO BS 767. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED AT BS 984, RBL 48. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 24. REPAIRED BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,141 hrs · 25,686 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 24. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,141 hrs · 25,868 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 44,141 hrs · 25,868 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,560 hrs · 25,352 cycles

DURING SCHEDULED MV1 CHECK FOUND, RT EEPLS INOP AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: STRIP — DELAMINATED (CABIN) · airframe 42,523 hrs · 24,748 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS DELAMINATED BETWEEN ROW 6 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 40,436 hrs · 23,557 cycles

AIR TURNBACK - AT 41000FT ON CRUISE, LEFT BLEED TRIP OFF LIGHT ILLUMINATED A TOTAL OF 4 TIMES WITH SUCCESSFUL RESETS ON EACH OCCASION. RIGHT BLEED TRIP OFF LIGHT ALSO ILLUMINATED TWICE AND CABIN BEAN CLIMBING. RESET WAS SUCCESSFUL. REMOVED AND REPLACED PRECOOLER CONTROL VALVE SENSOR, NR 2 ENGINE PRECOOLER VALVE, AND AIR CONDITIONING ACCESSORY UNIT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,886 hrs · 23,251 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 37,175 hrs · 21,572 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRIP — DELAMINATED (CABIN) · airframe 37,004 hrs · 21,471 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DELAMINATED AT ROW 22. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 37,004 hrs · 21,471 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN AT FWD BULKHEAD. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 35,246 hrs · 20,397 cycles

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

Part: TRUNNION — CORRODED (LT MLG) · airframe 35,246 hrs · 20,397 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,489 hrs · 19,953 cycles

FOUND L1 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 32,266 hrs · 18,574 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 30,455 hrs · 17,516 cycles

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

Part: SLIDE — FAULTY (L2 DOOR) · airframe 30,332 hrs · 17,439 cycles

L2 DOOR EMERGENCY EVAC SLIDE WILL NOT ARM. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,258 hrs · 17,401 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 30,258 hrs · 17,401 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,258 hrs · 17,401 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, LBL 35. REPAIRED FLOORBEAM CHORD PER ER.

Part: BATTERY — FAILED (CABIN) · airframe 29,925 hrs · 17,213 cycles

DURING SCHEDULED HC2 CHECK, LH OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,925 hrs · 17,213 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,925 hrs · 17,213 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,555 hrs · 17,000 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,928 hrs · 13,537 cycles

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

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 28,057 hrs · 16,147 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,415 hrs · 15,776 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,347 hrs · 15,163 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 25,263 hrs · 14,519 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 24,363 hrs · 14,161 cycles

EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 4 DEF. SECURED LENS PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,663 hrs · 14,188 cycles

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

Part: SLIDE — LOW (R2 DOOR) · airframe 24,594 hrs · 14,142 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,504 hrs · 13,537 cycles

DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 3 AND 5 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,448 hrs · 12,936 cycles

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

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 17,516 hrs · 10,107 cycles

EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS FWD SECTION PER MM.

Part: GIRT BAR — OUT OF ADJUST (SERVICE DOOR) · airframe 14,091 hrs · 8,265 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 12,969 hrs · 7,657 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 12,684 hrs · 7,493 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 12,684 hrs · 7,493 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACE RT ELEVATOR TAB NR 2 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 51,244 hrs · 37,757 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 9,475 hrs · 5,680 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY LENGTH OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,007 hrs · 4,226 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.