N402WN

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,499 hrs · 38,939 cycles

EMERGENCY LIGHTS BATTERY FAILED CAPACITY CHECK AT L/H MIDDLE LOCATION (M1669). / R&R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,499 hrs · 38,939 cycles

R2 DOOR SLIDE REQUIRED ADJUSTMENT. / INSTALLED SLIDE PER MT AND AMM.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,390 hrs · 38,876 cycles

RT TRAILING EDGE IN BD FLAP HAS CRACK WITH A DENT. R&R RT INBOARD AFT FLAP PER AMM 27-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,489 hrs · 38,281 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSEMBLY PER AMM.

Part: COVER — BROKEN (EMERGENCY EXIT) · airframe 64,379 hrs · 37,537 cycles

R/H EMERGENCY EXIT DOOR HANDLE CRADLE/INTERLOCK BROKEN. SECURED DOOR STRAP PULL COVER IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,146 hrs · 36,758 cycles

AFT LEFT WINDSCREEN FLASHLIGHT INOP. R&R BATTERY IAW AMM.

Part: BALANCE WEIGHT — CORRODED (L/H ELEVATOR) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** L/H ELEVATOR BAY #5 CENTER BALANCE WEIGHT HAS PITTING AND CORROSION / REMOVED AND REPLACED 2EA FIXED LOWER BALANCE WEIGHTS ON L/H ELEVATOR BAY #5. IAW SRM 51-61-04-0G-0 5.(5) (A) TRHU (D). 59083U 01/28/19 FIGURE 4. SHEET 1 VIEW B-B. DRAWING: 183A6000 REV P. ID: 0020 ZONE 20DG THE FIXED LOWER BALANCE WEIGHTS WERE REPLACED WITH THE SOME WEIGHT IT DOESN'T AFFECT THE MOMENT. WEIGHT AND BALANCE NO RQUIRED. 59083U 01/28/19. WEIGHT OUT OF LIMIST DUE TO NO LIMITS IN AMM OR SRM. 59083U 01/28/19

Part: WEB — DAMAGED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT BULKHEAD LOWER SEAL ATTACH WEB DAMAGED AT RBL 26. R&R WEB PER SRM AND DWG.

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,146 hrs · 36,758 cycles

LT OVERWING EMERGENCY EXIT LIGHT CONNECTOR LOCKING TAB BROKEN. R&R CONNECTOR PER AMM.

Part: SUPPORT — CRACKED (RT WHEEL WELL) · airframe 63,146 hrs · 36,758 cycles

FAIRING SUPPORT AT BS 663 LOWER VAPOR BARRIER FOUND CRACKED AT INBOARD SIDE RBL30 / REPAIRED FAIRING SUPPORT AT BS 663 RBL 30 IAW ER 19-01217 REV IR AND SWA EA 1-753-34079 REV IR

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 460 TO BS 480, LBL 21. R&R INTERCOSTAL IAW SRM & DWG.

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,146 hrs · 36,758 cycles

LT OVERWING EMERGENCY EXIT LIGHT CONNECTOR FORWARD SIDE ON OVER DOOR PANEL LOCKING TAB BROKEN. R&R CONNECTOR PER AMM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 63,146 hrs · 36,758 cycles

LOWER LT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE IAW ER AND EA.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 63,146 hrs · 36,758 cycles

LOWER RT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE IAW ER AN EA.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** SEAT TRACK LBL45.50 BS 500B -5' TO BS 500B -1' WL 208 HAS CORROSION IN 1 PLACE. CORROSION IS MARKED. / SEAT TRACK LBL 45.5 BS 500B-5' TO BS 500B-1' WL 208 TO BE REPLACED ON CUSTOMER CARD # N180107

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 500A TO BS 500B, LBL 21. R&R BAFFLE IAW ER & EA.

Part: FLOOR SUPPORT — CORRODED · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** FOUND ON UNDER SIDE OF FLOOR SUPPORT AT STA 951 RBL 45.5-53 WL 208 / CORROSION FOUND ON UNDER SIDE OF FLOOR SUPPORT AT STA 951 RBL 45.5-53 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS FOUND AND IS ONLY REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; 9C. REMOVED AND REPLACED FLOOR SUPPORT AT STA 951 RBL 45.5-53 WL 208 IAW SRM 51-40-02-0G-0; 7D AND BOEING DWG 147A5760 SHEET 11. 57901U 14JAN19

Part: SHEAR WEB — CORRODED · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** SHEAR WEB AT STA 986-1016 LBL 33-45 HAS CORROSION AT STA 1016 LBL 36 WL 208 / CORROSION ON SHEAR WEB AT STA 1016 LBL 36 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS FOUND AND IS ONLY REPAIRABLE BY REPLACEMENT. LOCATED AND DRILLED REPLACEMENT SHEAR WEB MPM 147A5620011 IAW SRM 51-40-05-0G-0 AND BOEING DWG 147A5600 5420 REV -. SHEAD WEB WILL BE INSTALLED ON CUSTOMER DEFECT# N179725 SA-M 326 A1231318 ITEM #4

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 63,146 hrs · 36,758 cycles

L/H LWR 663 VAPOR BARRIER STIFFENER ON THE FWD SIDE FOUND CRACKED/BROKEN P/N 111A1301- 5 / REPLACED L/H LWR 663 VAPOR BARRIER STIFFER ON THE FWD SIDE P/N 111A1301-5 WITH NEW PO# 684835/2 PER SRM 51-40-05 AND DWG 111A1000

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

ANGLE CORRODED AT BS 663+4, RBL 69. R&R ANGLE PER DWG & SRM.

Part: SUPPORT BRACKET — CORRODED (AFT CARGO BAY) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** AFT CARGO BAY FWD WALL PANEL SUPPORT BRACKET AT STA 727 RBL 6 HAS CORROSION ON LOWER AFT SURFACE / REMOVED DAMAGED AFT CARGO BAY FWD WALL PANEL SUPPORT BRACKET AND REPLACED WITH NEW PO# 704606 IAW SRM 51-40-02-0G-0. 57403U 01/06/2019 AND BOEING D-WG# 144A2600 AT STA 727 RBL 6. DAMAGE TO BE OUT OF LIMITS DUE TO NO LIMITS LISTED IN SRM.

Part: FLOOR SPLICE — CORRODED (AFT CARGO BAY) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** AFT CARGO BAY FLOOR SPLICE SUPPORT AT STA 887 HAS MULTIPLE SPOTS OF CORROSION ON UPPER SURFACE FROM RBL 22 TO LBL 6 / REMOVED CORROSION AFT CARGO BAY FLOOR SPLICE SUPPORT STA 887 RBL 22 TO LBL 6 NO SRM ENTRYS AVAILABLE; REPLACED WITH NEW PART PER SRM 51-10-02-0G-0. LOCATED AND DRILLED NEW SPLICE SUPPORT IAW SRM 51-40-05-0G-0; DWG# 146A9401. P.O.# 725077 RECEIPT# 5078496 PN# 146A9401U21 INSTALLED NUTPLATES IAW DWG# 146A9401 REV A AND SRM 51-40-02-0G-0. PART TO BE INSTALLED ON JPANEL-141-CLOSE CARD

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO FLOOR SHIELD CORRODED BETWEEN BS 500+2 TO BS 500+14, RBL 25. R&R SHILLED IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT CARGO BAY RT CARGO DOOR CUTOUT THRESHOLD CORRODED ON UPPER SURFACE BETWEEN BS 800 TO BS 847, RBL 22. R&R THRESHOLD WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT CARGO BAY RT FORWARD FLOOR Z CHANNEL CORRODED BETWEEN BS 727E TO BS 767, RBL 22. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT CARGO BAY LT FORWARD FLOOR Z CHANNEL CORRODED BETWEEN BS 727B TO BS 727E, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO Z ANGLE CORRODED AT BS 400+14, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO FLOOR Z ANGLE CORRODED BETWEEN BS 500A+1 TO BS 500A+6, RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT CARGO BAY LT AFT FLOOR Z CHANNEL CORRODED BETWEEN BS 727E TO BS 847, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 28. R&R THRESHOLD WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FORWARD CARGO FLOOR Z ANGLE CORRODED BETWEEN BS 460+14 TO BS 500B+14, LBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT CARGO BAY RT FORWARD CARGO DOOR CUTOUT FLOOR SUPPORT CORRODED BETWEEN BS 767 TO BS 787, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FWD CARGO BAY) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** FWD CARGO FLOOR AFT BULKHEAD ATTACH ANGLE MULTIPLE AREAS LBL1; RBL12 WL156 STA 500D / FWD CARGO FLOOR AFT BULKHEAD ATTACH ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS STATEMENT IN SRM REMOVED DAMAGED ATTACH ANGLE; REPLACED WITH P/N 7530142 PO#708714 IAW DWG 143A7962 & SRM 51-40-02-0G-0 51146U 1/4/19

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

LT SIDE LOWER FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

RT SIDE LOWER FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME PER EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

R1 DOOR CUTOUT ATTACH ANGLE TO INNER CHORD CORRODED BETWEEN BS 294.5+11 TO BS 312 +12, RBL 57. R&R ATTACH ANGLE PER SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

L1 DOOR CUTOUT SURROUND STRUCTURE ANGLE ATTACH TO INNER CHORD CORRODED BETWEEN BS 312+3 TO BS 328+13, S17L. REPAIRED ANGLE IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

R1 DOOR CUTOUT INNER CHORD CORRODED BETWEEN BS 294.5 TO BS 328, RBL 57. R&R INNER CHORD PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

R1 DOOR CUTOUT STRAP CORRODED AT BS 294.5+4, RBL 57. R&R STRAP PER SRM AND DWG.

Part: SKIN — CORRODED (LOWER EXT FUSELA) · airframe 63,146 hrs · 36,758 cycles

***CORROSION*** TOILET SERVICE DOOR SKIN INTERIOR LOWER SURFACE STR 847+10 LBL27 6' BELOW STRINGER 24 / REMOVED CORRISION ON TOILET SERVICE DOOR INTERRIOR SKIN 3.7'L X 2.4'W X .045D FOUND TO BE OUT OF LIMITS 52-40-01-1A-4. REMOVED AND REPLACED LAV SERVICE DOOR IAW AMM 52-49-07-000-801 AND 52-49-07-400-801. BOND CHECK GOOD

Part: ANGLE — CORRODED (L1 DOOR) · airframe 63,146 hrs · 36,758 cycles

FWD. ENTRY DOOR CUT OUT SURROUND STRUCTURE; STA 312 +3 TO STA 328 +9 ; S17L SCUFF PLATE SUPPORT ANGLE HAS CORROSION. / FOUND CORROSION ON SCUFF PLACE SUPPORT ANGLE AT STA 312 + 3 TO STA 328 + 9 S17L TO BE OUT OF LIMITS DUE TO DAMAGE FASTENER HOLES IAW SRM 53-10-15-1A-1 FIG 108 D. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE MPN 141A8112-2 IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A6720. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8110

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

INTERCOSTAL CORRODED BETWEEN BS 294.5+7 TO BS 294.5+13, RBL 15. R&R INTERCOSTAL PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE WEB CRACKED AT BS 1016 +11, RBL 27. R&R WEB PER ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FLOOR STRUCTURE WEB CORRODED BETWEEN BS 1016 TO BS 1016+12, BETWEEN LBL 6 TO LBL 37. R&R WEB PER SRM AND DWG.

Part: STRAP — CORRODED (CABIN) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE; STA 1016 +13 WL 208 LBL 3 STRAP HAS CORROSION / REMOVED DAMAGED STRAP AT 1016+13 WL 208 LBL 3 AND INSTALLED NEW STRAP ITEM 147A5620U3 P.O. 725693 PER SRM 51-40-02 AND BOEING DWG 147A5600 REV H AND BOEING DWG 147A5730 REV: A TRM 57373U 1-20-19 DAMAGD STRAP FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE DOOR INNER CHORD CORRODED BETWEEN BS 947.5+11 TO BS 967+18, STR 17L. R&R INNER CHORD IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE STRAP CORRODED BETWEEN BS 1016 TO BS 1016+8, RBL 3. R&R STRAP PER DWG AND SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

TRANSVERSE BEAM CORRODED AT BS 344, BETWEEN LBL 10 TO LBL 16. R&R TRANSVERSE BEAM IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

INNER CHORD CORRODED AT BS 344 -1, LBL 61. R&R CHORD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FLOORBEAM METAL DAMAGED FROM FASTENER CLIP AT BS 328, RBL 39. REPAIRED BEAM IAW ER AND SWA EA.

Part: INTERCOSTAL — DAMAGED (CABIN) · airframe 63,146 hrs · 36,758 cycles

INTERCOSTAL MATERIAL MISSING BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 32. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

INTERCOSTAL CRACKED UNDER PASSENGER FLOOR _PANEL 221AF; STA 278-294; WL 208; BL0. / REMOVED AND REPLACED INTERCOSTAL STA 278-294; WL 208 IAW SRM 51-40-02-0G-0 AND DWG# 141A5400 57111U 1-8-2019

Part: PANEL — ELONGATED (RIGHT WING) · airframe 63,146 hrs · 36,758 cycles

SCREW HOLE ELONGATED & MATERIAL SHOWING ON R/H WING L/E PANEL #621QB / REPAIRED ELONGATED HOLE & MATERIAL SHOWING ON R/H WING L/E PANEL 621QB I.A.W 737 SRM 57-41-01-2R-1 TABLE 202 250 DEGREES FAHRENHEIT CURE PER 737 SRM 51-70-05-2R-8; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 57-41-01-1A-1 PARA 1; 4C(5)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 5 TO RBL43. REPAIRED FLOORBEAM IAW ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE MOPSILL INNER CHORD CORRODED AT BS 927+17, STR 17R. R&R INNER CHORD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE CORRODED AT BS 947.5+9, BETWEEN RBL 15 TO RBL 30. R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

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

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 63,146 hrs · 36,758 cycles

VAPOR BARRIER TEMP REPAIR CRACKED AT BS 663, RBL 28. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 63,146 hrs · 36,758 cycles

VAPOR BARRIER CRACKED AT BS 663, LBL 8. REPAIRED BARRIER PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,146 hrs · 36,758 cycles

AFT CABIN FLOORBOARD PANEL 241ADF DELAMINATED ON __CORNER / REPAIRED DELAMINATED CORNER ON AFT CABIN FLOORBOARD PANEL 241ADF IAW SRM 53-00-50-2R-9 + SRM 53-00-50-2R-0. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. DELAMINATION IS NOT PERMITTED 807334 03JAN19

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,146 hrs · 36,758 cycles

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

Part: BRACKET — CRACKED (LEFT WING) · airframe 63,146 hrs · 36,758 cycles

_SEAL RETAINER BRACKET CRACKED ON LEFT WING _DEFLECTION WEB PANEL APPROX. ORSS 269 / REMOVED + REPLACED SEAL RETAINER BRACKET WEB ASSY IAW SRM 51-40-02-0G-0 PAR 4 + DWG# 115A2930

Part: BRACKET — CRACKED (RIGHT WING) · airframe 63,146 hrs · 36,758 cycles

BRACKET ATTACHING RIGHT WING O/B FIXED TRAILING EDGE PANEL TO DEFLECTION RIB CRACKED APPROX. ORSS 269 / REMOVED AND REPLACED BRACKET ATTACHING RIGHT WING OB FIXED TE PANEL TO DEFLECTION CONTROL RIB AT APPROX ORSS 269 PER SRM 51-40-02-0G-0 AND DRAWING 115A6200 REV B.

Part: PLATE — CRACKED (LT WING) · airframe 63,146 hrs · 36,758 cycles

LT WING TRAILING EDGE WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE IAW SRM & DWG.

Part: PANEL — CRACKED (SLAT) · airframe 63,146 hrs · 36,758 cycles

_____PANEL 623DB CRACKED ON RIGHT WING SLAT / REMOVED; FABRICATED AND INSTALLED NEW COVER PANEL 623DB IAW SOPM 20-50-01; DRAWING 114A8131 FROM 7075T0 .063 LOT 5042804 81012U 24JAN19

Part: SKIN — CORRODED (LH NACELLE) · airframe 63,146 hrs · 36,758 cycles

CORROSION AROUND MULTIPLE FASTENERS ON THE UPPER SKIN OF #1 ENGINE INLET COWL / REMOVED AND REPLACED #1 ENGINE INLET COWL LEAK AND OPS CHECK GOOD IAW AMM 71-11-01 (POS:#2; TAG NO:ROB TAG; P/N OFF:0710037; S/N OFF:1484001; P/N ON:0710037; S/N ON:3658001)

Part: SKIN — CRACKED (SLAT) · airframe 63,146 hrs · 36,758 cycles

LT WING; LOWER SURFACE OF L/E SLAT #2; NOSE SKIN AT SLAT ACTUATOR; HAS 02 E/A WORKING FASTENERS. / TRIMMED OUT DAMAGED AREA ON LT WING LOWER SURGACE OF L/E #2 SLAT AT NOSE SKIN SLAT ACTUATOR AND REPAIRED IAW SRM 57-42-01-2R-8 81146U 1/11/19

Part: BATTERY — FAILED (CABIN) · airframe 62,773 hrs · 36,530 cycles

AFT GALLEY RIGHT SIDE EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: SKIN — CRACKED (TE FLAP) · airframe 62,099 hrs · 36,100 cycles

LT WING INBOARD TRAILING AFT FLAP LOWER SURFACE CRACKED. REPAIRED AFT FLAP PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,160 hrs · 35,496 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,151 hrs · 35,489 cycles

RT AISLE EMERGENCY LIGHTS INOP BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,978 hrs · 35,380 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 60,724 hrs · 35,222 cycles

RUDDER BALANCE WEIGHT CORRODED. / REMOVED AND REPLACED RUDDER BALANCE WEIGHT PER CMM 55-40-09

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 60,724 hrs · 35,222 cycles

LEFT CABIN EMERGENCY LIGHT FAILED 15 MINUTE RUN TIME CHECK, BETWEEN BS 603 TO 727C+13. R & R THE BATTERY PACK IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 60,724 hrs · 35,222 cycles

BULKHEAD WEB CRACKED AT BS 663, RBL 44. REPAIRED THE BULKHEAD WEB IAW EA.

Part: GAUGE — OUT OF POSITION (L2 DOOR DOOR) · airframe 59,169 hrs · 34,210 cycles

L2 DOOR SLIDE GAUGE OUT OF POSITION. R & R THE SLIDE IAW MT & AMM.

Part: BRACKET — CRACKED (RT WING TE) · airframe 58,718 hrs · 33,899 cycles

RIGHT WING FIXED TRAILING EDGE L-BRACKET CRACKED. R & R THE BRACKET IAW SRM.

Part: BEAM — CRACKED (FSD) · airframe 58,718 hrs · 33,899 cycles

SUPPLEMENTAL INFORMATION: FWD SERV DOOR HAS .75 INCH CRACK ON BEAM IN RADIUS ABOVE CAM BOX ASSY NEXT TO FWD I/B MOUNTING BOLT. / R&R FWD GALLEY SERVICE DOOR PER AMM 52-41-00. TAG NO: 267630 PN ON: 141A6516-4 SN ON: 000092 PN OFF: SN OFF: 0008111

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 58,718 hrs · 33,899 cycles

SUPPLEMENTAL INFORMATION: R/H WING TO BODY PNL 196CR AFT TRAILING EDGE RADIUS HAVE A APPROX. 3 IN. CRACK. / REPAIRED DAMAGE PER SRM 53-40-70-2R-1.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 58,347 hrs · 33,678 cycles

RIGHT HORIZONTAL STABILIZER CRACKED. R & R THE STABILIZER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,749 hrs · 33,337 cycles

R2 DOOR EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,918 hrs · 32,823 cycles

RIGHT EMERGENCY EXIT OVERWING DOOR SIDEWALL LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 56,612 hrs · 32,653 cycles

AFT CARGO DOOR CORRODED ON THE BOTTOM FORWARD INTERNAL SKIN. R&R AFT CARGO DOOR PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 56,484 hrs · 32,572 cycles

RT BULLNOSE BIN EMERGENCY LIGHT LENS LOOSE AT ROW 16. REPAIRED LIGHT ASSEMBLY PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,484 hrs · 32,572 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,484 hrs · 32,572 cycles

AFT CENTER CEILING EMERGENCY EXIT SIGN INOP AT LOCATION M01672. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,484 hrs · 32,572 cycles

L2 DOOR EMERGENCY EXIT SIGN INOP AT LOCATION M01672. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,484 hrs · 32,572 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,484 hrs · 32,572 cycles

FUSELAGE SKIN CORRODED AT BS 355, BL 0. REPAIRED SKIN PER SWA EA.

Part: CARGO TRACK — CORRODED (BS 787) · airframe 56,484 hrs · 32,572 cycles

CARGO TRACK CORRODED AT BS 787, RBL 14. R & R THE CARGO TRACK IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,484 hrs · 32,572 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · airframe 56,484 hrs · 32,572 cycles

FLOOR SUPPORT CORRDED AT BS 727 TO 767 OUTBOARD SIDE. R & R THE FLOOR SUPPORT IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 56,484 hrs · 32,572 cycles

RIGHT MLG WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,484 hrs · 32,572 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE LAMP IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,484 hrs · 32,572 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 9 TO 13. R & R THE BATTERY IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,484 hrs · 32,572 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,605 hrs · 32,066 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON INBD AFT CORNER. R & R AFT FLAP IAW AMM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 53,556 hrs · 30,907 cycles

AFT PRESS BULKHEAD INITIAL STIFFENER Z ANGLE DAMAGED IN THE RADIUS AT BS 1016, RBL 35. REPAIRED BULKHEAD IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,387 hrs · 30,269 cycles

FLOOR SUPPORT FRAME CRACKED, BETWEEN BS 344 - 360, LT OF CTR. R & R FRAME IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 51,712 hrs · 29,860 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN CRACKED. R & R SIGN MM.

Part: SIGN — LOOSE (CABIN) · airframe 51,694 hrs · 29,849 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 50,867 hrs · 29,362 cycles

MID CABIN CEILING EMER EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

SKIN CRACKED AT BS 1016, STRINGER 14L. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,092 hrs · 28,940 cycles

LEFT WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 32 ON INBD SIDE OF PRESS BALL CUT OUT. REPAIRED WEB IAW EA.

Part: DOUBLER — DEBONDED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FRAME DOUBLER DISBONDED AT RIB LOCATION BS 727A, BETWEEN STRINGER 1 TO 4R. REPAIRED DOUBLER IAW DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 44.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 44.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 46.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 23.75. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 44.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

AFT SEAT TRACK OUTBOARD FLANGE CRACKED AT BS. 727B, LBL 46.5. / REPAIRED SEAT TRACK PER ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

AFT SEAT TRACK OTBD FLANGE CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FLOORBEAM UPPER FLANGE CRACKED AT BS 727B, LBL 22.75. REPAIRED FLOORBEAM IAW ACO.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,092 hrs · 28,940 cycles

INTERIOR SIDE OF WW SPAR VERTICAL WEB CRACKED AT LBL 40. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 46.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK INBD FLANGE AFT FASTENER CRACKED AT BS 727B, RBL 44.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK OTBD FLANGE CRACKED AT BS 727B, LBL 46.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,092 hrs · 28,940 cycles

FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW ACO.

Part: FAN — MALFUNCTIONED (AC BAY) · airframe 49,544 hrs · 28,626 cycles

AT CRUISE GOT A REPORT OF SMOKE FROM THE AFT CABIN FROM FLIGHT ATTENDANT & DEADHEADING PILOT. FOUND RECIRC FAN CABIN AIR CB POPPED. R & R RECIRC FAN IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 49,514 hrs · 28,608 cycles

RIGHT EMER EXIT LIGHT LENS MISSING AT ROW 3. INSTALLED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 49,514 hrs · 28,608 cycles

RIGHT EMER EXIT LIGHT LENS LOOSE AT ROW 3. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 44,242 hrs · 25,590 cycles

LT OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE AT ROW 1. SECURED LENS IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 43,344 hrs · 25,071 cycles

RIGHT OVERWING EMERGENCY EXIT COVER MISSING. INSTALLED LENS PER M/M.

Part: FUSE — INOPERATIVE (CABIN) · airframe 43,269 hrs · 25,016 cycles

EMERGENCY LIGHTING BATTERY PACK CHARGING ASSEMBLY (M1669) AT STA 603 RIGHT FUSES INOP. REMOVED AND REPLACED FUSES IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,269 hrs · 25,016 cycles

PASSENGER CABIN CENTER CABIN EMERGENCY PROXIMITY LIGHTING INOP. REMOVED AND REPLACED LIGHT IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 43,269 hrs · 25,016 cycles

AFT LAVATORY EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

INTERCOSTAL CLIP STA 500C STRINGER 25L IS CRACKED. REMOVED CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND DEBURRED NEW CLIP P/N 143A7502-5 A50282 INSTALLED NEW CLIP AT STA 500C STR 25L IAW BOEING DWG 143A7505 AND SRM 51-40-02 APPLIED CIC IAW AMM 51-21-91.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

PANEL 141PW LOWER ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 43,269 hrs · 25,016 cycles

LT W/W BULKHEAD AT INBD CORNER OF PANEL 193AL, VERTICAL STIFFENER CRACKED. R & R STIFFENER IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

MAIN CABIN STA 400 TO 420, RBL 65 CREASE BEAM WEB ANGLE CRACKED ON BOTTOM SIDE. R & R ANGLE IAW SRM AND DWG.

Part: FLANGE — CRACKED (RT HORIZ STAB) · airframe 43,269 hrs · 25,016 cycles

RIGHT HORIZONTAL STAB - STATION 147.90 - FWD I/B LOWER FLANGE IS CRACKED. REPAIRED FLANGE IAW SWA EA 1-755-1810 AND AAR EA 13013 IR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

MAIN CABIN SERVICE DOOR CREASE BEAM BETWEEN STA 294 AND 328, RBL 65 WL 208 HAD CORROSION. R & R BEAM IAW SRM AND DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CO-PILOTS NR 3 WINDOW FRAME 2ND HOLE FROM BOTTOM OF E-F WINDOW POST HAS CRACK INDICATIONS. REMOVED AND REPLACED FRAME IAW BOEING DRAWINGS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

MAIN CABIN BETWEEN FUSELAGE STA 277 AND 294 RBL 2 CRACKED INTERCOSTAL ON SCREW HOLE. REMOVED AND INSTALLED NEW INTERCOSTAL AT STA 277-294 277-294 RBL 2 IAW SRM 51-40-02-0G-0 AND DWG 141A5400

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE UPPER SURFACE STA 889 RBL 4 ONE AREA OF CORROSION AROUND FASTENER HOLE AS MARKED. REMOVED AND REPLACED SUPPORT IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FRAME CRACKED AT STA 480, STR 8R. R & R FRAME IAW SWA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO COMP FLOOR STRUCTURE UPPER SURFACE CORRODED AT BS 889, LBL 4. REMOVED AND REPLACED STRUCTURE IAW SRM AND BOEING DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AD DRIVEN ACO 8323-53 PASSENGER CABIN STATION 787 FRAME CRACKED AT INBOARD FASTENER OF AIR CONDITIONING BRACKET ATTACHMENT AT STRINGER 8R. INSTALLED REPAIR DOUBLERS AT STA 787 FRAME AT STRINGER 8 RT IAW EA 1-A53-12114 REV 2

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CARGO COMP LT Z-ANGLE STA 727D TO 807 HAD CORROSION. R & R Z-ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO COMP, RIGHT Z-ANGLE STA 893 TO 924 HAS NUMEROUS AREAS OF CORROSION AS MARKED. INSTALLED NEW Z ANGLE A-TAG A49641 IAW BOEING DWG 147A7500. ORIGINAL Z ANGLE FOUND TO BE "OUT OF LIMITS". ORG MAT. .032", REMOVED 0.10". REMIANING .022". REPAIR MATERIAL VERIFIED AS A-TAG A49641 IAW SRM 53-00-53-2R-5 FABRICATED NEW Z ANGLE IAW SRM 53-00-53-2R-5 TREATED NEW Z ANGLE IAW AMM 51-21-41-370-802. PRIMED NEW Z ANGLE IAW AMM

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FRAME CRACKED AT STA 867, STR 8R. R & R FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

STATION 360 FRAME CRACKED AT STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FRAME CRACKED AT STA 400, STR 8L. R & R FRAME IAW SWA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO COMPARTMENT, STATION 727A+10, RBL 13, CARGO FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AD DRIVEN ACO # 8212-53 PASSENGER CABIN STATION 480 FRAME CRACKED AT INBOARD FASTENER OF AIR CONDITIONING BRACKET ATTACHMENT AT STRINGER 8L. REPAIRED CRACKED PORTION OF FRAME AT STA 480 STR 8L AND INSTALLED REPAIR ANGLES AT 8 IAW EA 1-A53-12114 REV 2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO COMP RIGHT Z-ANGLE, STA 727D TO 767 NUMEROUS AREAS OF CORROSION AS MARKED. VERIFIED LIMITS ON Z-ANGLE ORG 0.040, REMOVED 0.006 REMAIN 0.034. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-2. REMOVED OUT OF LIMITS AREA AND REPAIRED IAW SRM 53-00-53-2R-6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FRAME CRACKED AT STA 747, STR 8L. REPAIRED FRAME EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

STIFFENER HAD AREAS OF CORROSION AT STA 951 AND RBL 33 AND RBL 38. R & R STIFFENER IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FWD CARGO ANGLE ATTACHED TO INTERCOSTAL AT STA 500C LBL 25" CRACKED AS MARKED. REMOVED AND REPLACED INTERCOSTAL CLIP STA 500C AT LBL 25 IAW SRM 51-40-02 & BOEING DRAWING 143A7502.

Part: SUPPORT BRACKET — CORRODED (L1 DOOR) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA L-1 DOORWAY AFT GIRT BAR FITTING SUPPORT BRACKET CORRODED STA 344 LBL 59. REMOVED AND REPLACED AFT GIRT BAR FITTING SUPPORT BRACKET AT L-1 DOORWAY, STA 344 LBL 59 IAW SRM 51-40-02 AND IPC 53-42-00-29.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CABIN HAD WET AREA FLOOR SUPPORT CORRODED STA 312-328 RBL10. R & R SUPPORT IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA FLOORBOARD 221GF UPPER SURFACE DELAMINATED. REPAIRED DAMAGE TO CABIN FWD WET AREA FLOORBOARD 221GF IAW SRM 53-00-50-2R-0, 53-00-50-2R-1. TAP TEST GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CARGO STA 500B, LBL 25 ANGLE ATTACHED TO INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM AND BOEING.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA FLOORBOARD 222BF FWD OUTBOARD EDGE DELAMINATED. REPAIRED FLOORBOARD IAW SRM 53-00-50-01-1 SRM 53-00-50-1A-1 SRM 53-00-50-2R-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT STA 344-360 BL 0. REMOVED CRACKED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL AT STA 344-360 IAW SRM 51-40-02, 51-40-05- AND DRAWING 141A5400

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT PIT STA 847 TO STA 867 RBL 22 Z-ANGLE CLOSURE HAS CORROSION (AS SEEN FROM BOTTOM) AND MISSING NUT PLATE. REMOVED CORROSION FROM Z-ANGLE CLOSURE. ORIGINAL THICKNESS .050", AMOUNT REMOVED .009", AMOUNT REMAINING .041". FOUND TO BE "OUT OF LIMITS" IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE CLOSURE IAW BOEING DWG 164A8127 APPLIED CIC TO AREA IAW SRM 51-20-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FORWARD CABIN R-1 DOORWAY FWD FRAME WEB CRACKED AT STA 312 RBL 53.5 WL 209. REMOVED DAMAGED AREA, HAD NDT INSPECT AREA TO ENSURE NO MORE DAMAGE EXISTS, AND INSTALLED NEW REPAIR DUE TO FWD CABIN R1 DOORWAY FWD FRAME WEB CRACK IAW SRM 51-70-11-2R-0. REPAIRED PART IS NOT ON FCBS LIST NO DTE REQUIRED IAW SRM 51-00-04-0G-0 TABLE 7 IDENTIFIED AS STUB FRAME IAW SRM 53-10-15-01-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

CABIN HAD WET AREA FLOOR SUPPORT CORRODED STA 294-312 RBL10. R & R SUPPORT IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

AFT CARGO PIT STA 767 TO STA 793, RBL 22 "Z" ANGLE CLOSURE WEB HAS CORROSION. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA FLOORBOARD 221GF FWD OUTBOARD CORNER BROKEN. REPAIRED DAMAGE TO CABIN FWD WET AREA FLOORBOARD PANEL 221GF IAW SRM 53-00-50-2R-4, 53-00-50-2R-0 TAP TEST GOOD.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

FWD CARGO STA 420 TO 440 ABOVED STR 26 RBL 25" Z- CHANNEL CRACKED, AS MARKED. REMOVED AND REPLACED FWD CARGO STA 420-440 RBL 25" Z-CHANNEL IAW 737-700 SRM 51-40-02-0G-0.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 43,269 hrs · 25,016 cycles

CABIN FWD WET AREA FLOORBOARD 222DF OUTBOARD UNDERSIDE EDGE PUNCTURED. REMOVED AND INSTALLED INSERT FOR ACCESS, AFTER COMPLETING WET LAYUP REPAIR ON FLOORBOARD 222DF REPAIR TAP TESTS GOOD IAW SRM 53-00-50.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

PASSENGER CABIN STA 727D FRAME CRACKED I/N FASTENER OF AIR CONDITIONING AT STR 8R. R & R FRAME IAW SWA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,269 hrs · 25,016 cycles

SERVICE DOOR R2 THRESHOLD/ CREASE BEAM HAD CORROSION BETWEEN BS 951R AND 992.8R. R & R BEAM IAW SRM AND DWG.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,269 hrs · 25,016 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED IN SKIN, INBOARD OF STA 101.90 RIB, 9.75" TO 10.75" FROM T/E OF PANEL. REMOVED AND REPLACED SKIN PER CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,269 hrs · 25,016 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED, INBOARD OF STA 129.50 RIB, 9.5" TO 10.0" FROM T/E OF PANEL. REMOVED AND REPLACED SKIN PER CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,269 hrs · 25,016 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED, INBOARD OF STA 138.70 RIB, 9.25" TO 9.55" FROM L/E OF PANEL. REMOVED AND REPLACED SKIN PER CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,269 hrs · 25,016 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED, INBOARD OF STA 120.30 RIB, 9.5" TO 10.0" FROM L/E OF PANEL. REMOVED AND REPLACED SKIN PER CCO.

Part: SLAT — CRACKED (RT WING) · airframe 41,561 hrs · 23,951 cycles

RIGHT WING NR 7 SLAT CRACKED. REMOVED & REPLACED NR 7 SLAT PER AMM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 41,366 hrs · 23,832 cycles

LEFT EEPLS INOP BETWEEN ROW 3 TO ROW 5. CONNECTED WIRE TO LIGHT ASSEMBLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 40,954 hrs · 23,583 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 40,834 hrs · 23,515 cycles

CENTER OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER M/M.

Part: LATCH — LOOSE (R1 DOOR) · airframe 40,468 hrs · 23,311 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER BOTTOM LATCH BRACKET LOOSE. SECURED LATCH ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,099 hrs · 23,117 cycles

LT EMERGENCY LIGHT ASSY AT ROW 13 INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: COVER — CRACKED (CABIN) · airframe 39,412 hrs · 22,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS COVER CRACKED AT ROW 18. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,412 hrs · 22,704 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT M01672 AND M01675. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CAP — MISSING (CABIN) · airframe 39,412 hrs · 22,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS END CAP MISSING. REMOVED AND REPLACED END CAP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 39,412 hrs · 22,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 39,412 hrs · 22,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS DAMAGED AT ROW 5. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 37,055 hrs · 21,351 cycles

LT EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 36,787 hrs · 21,189 cycles

EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, RBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, RBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, LBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B FORE FLAP I/B LOWER CORNER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,489 hrs · 21,023 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547, LBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: ENGINE — STALLED (NR 1) · airframe 35,255 hrs · 20,316 cycles

AIR TURNBACK/ DECLARED EMERGENCY. COMPRESSOR STALL ON NR 1 ENGINE AFTER TAKEOFF AT 4000FT. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,021 hrs · 20,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,021 hrs · 20,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: COVER — CRACKED (CABIN) · airframe 34,853 hrs · 20,070 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 15. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 34,853 hrs · 20,070 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 16 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 33,672 hrs · 19,374 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER CRACKED AT ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 33,462 hrs · 19,265 cycles

DURING SCHEDULED MV3 CHECK FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 33,462 hrs · 19,265 cycles

DURING SCHEDULED MV3 CHECK FOUND EEPLS COVER MISSING AT ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 33,462 hrs · 19,265 cycles

LT EEPLS COVER LOOSE AT ROW 2. SECURED COVER PER EA.

Part: COVER — LOOSE (CABIN) · airframe 32,706 hrs · 18,819 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,598 hrs · 18,757 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 32,531 hrs · 18,711 cycles

FWD EEPLS LENS MISSING AT ROW 10. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 32,531 hrs · 18,711 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 10. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 31,940 hrs · 19,349 cycles

BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 30,136 hrs · 17,269 cycles

LT FWD CABIN EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,016 hrs · 17,192 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986, BETWEEN RBL 50 TO LBL 50, WL 208. REPAIRED BEAM PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 29,754 hrs · 17,039 cycles

R2 COCKPIT WINDOW ARCED AT LOWER FWD CORNER NEAR HANDLE. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,763 hrs · 17,045 cycles

DURING SCHEDULED OTS CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,662 hrs · 16,986 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 29,247 hrs · 16,733 cycles

EEPLS TRACK LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 28,898 hrs · 16,523 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT COVER BROKEN AT BETWEEN ROW 1 TO ROW 3. REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 28,898 hrs · 16,523 cycles

EEPLS LIGHT COVER BROKEN BETWEEN ROW 1 TO ROW 3. REPAIRED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,876 hrs · 16,511 cycles

LT EEPLS LIGHT STRIP COVER LOOSE. SECURED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,876 hrs · 16,511 cycles

RT EEPLS LIGHT STRIP COVER LOOSE. SECURED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,250 hrs · 16,124 cycles

DURING SCHEDULED MV2 CHECK, FOUND EGRESS LENS COVER MISSING AT LT FLOOR ROW 10. INSTALLED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,621 hrs · 5,129 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,583 hrs · 14,481 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 23,803 hrs · 13,409 cycles

EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 17,208 hrs · 9,603 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS COVER CRACKED AT ROW 17 ABC. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 21,878 hrs · 12,270 cycles

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

Part: COVER — MISSING (CABIN) · airframe 21,803 hrs · 12,232 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,064 hrs · 11,809 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LT EEPLS INOP. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 20,786 hrs · 11,638 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,673 hrs · 11,580 cycles

AFT LEFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,673 hrs · 11,580 cycles

FWD RT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INSTALLED (EMERGENCY LIGHT) · airframe 20,673 hrs · 11,580 cycles

MID RIGHT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RIVET — SHEARED (R1 DOOR) · airframe 20,350 hrs · 11,394 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK HAS A SHEARED RIVET. REMOVED AND REPLACED RIVET PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 18,482 hrs · 10,354 cycles

EEPLS COVER BROKEN AT FWD END. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,316 hrs · 9,717 cycles

EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 17,282 hrs · 9,703 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,022 hrs · 9,575 cycles

EEPLS LENS MISSING AT FWD END. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,430 hrs · 9,264 cycles

EEPLS TRACK LOOSE AT ROW 1 ABC. SECURED EEPLS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 15,898 hrs · 8,968 cycles

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

Part: LIGHT — BROKEN (FWD CABIN) · airframe 14,974 hrs · 8,443 cycles

FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 12,481 hrs · 7,022 cycles

DURING SCHEDULED C3 CHECK, FWD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 11,606 hrs · 6,508 cycles

DURING SPV, FOUND SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. DEEP CYCLED AIRCRAFT EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: GIRT BAR — OUT OF ADJUST (FWD CABIN DOORS) · airframe 9,491 hrs · 5,350 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH CABIN DOOR SLIDES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 5,891 hrs · 3,381 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM.