N735SA

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 79,163 hrs · 46,539 cycles

L/H AFT EMERGENCY LIGHTS DID NOT PASS CAPACITY CHECK. REMOVED AND REPLACED M01673 BATTERY PACK IAW AMM 33-51-06; OPS TESTED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 79,163 hrs · 46,539 cycles

L/H AFT EMERGENCY LIGHTS DID NOT PASS CAPACITY CHECK (M01670) / [01] REMOVED AND REPLACED M01670 BATTERY PACK PER AMM 33-51-06; OPS TEST NORMAL

Part: SLIDE — LOOSE (PAX DOOR) · airframe 78,985 hrs · 46,432 cycles

FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE MOTORIAL IS LOOSE AND HANGING DOWN BELOW BAR / [01] RE ATTACHED VELCRO ON THE FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE PER S.I.P OPS CHECK GOOD..

Part: NONE — MISSING · airframe 78,601 hrs · 46,168 cycles

AFT SVC DOOR EMER SIGN LENS MISSING / [01] R/R AFT SVC DOOR EMER SIGN LENS PER AMM 33-51-01. OPS. CHECK GOOD.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 78,306 hrs · 45,963 cycles

SEVERAL EMERGENCY LIGHTS OUT IN FWD CABIN ON RIGHT SIDE / [01] REMOVED AND REPLACED RIGHT HAND FWD. EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (R/H FUSELAGE) · airframe 77,992 hrs · 45,759 cycles

EMERGENCY LIGHT ABOVE L2 DOOR AND EXTERIOR EMERGENCY LIGHT AFT OF R2 DOOR INOP / [01] REMOVED AND REPLACED AFT RIGHT HAND EMERGENCY BATTERY PACK PER AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE · airframe 77,797 hrs · 45,629 cycles

EMERGENCY LIGHT BATTERY M1675 DEAD / [01] R&R M1675 BATT + CHARGER REF AMM 33-51-06. OPS CHK GOOD.

Part: SKIN — CRACKED (LH WING TE FLAP) · airframe 77,548 hrs · 45,478 cycles

LH INBD T/E AFT FLAP LOWER SKIN PUNCTURE /CRACK LH INBD T/E AFT FLAP LOWER SKIN PUNCTURE & CRACK 24.5 IN. FROM OB END AND 6 IN. FROM TE. / [01] INSTALLED PERMANENT TO FLAP LOWER SKIN PER SRM 51-70-10 AND SRM 57-53-01-2R-4. PERMANENT REPAIR

Part: BATTERY PACK — FAULTY (AFT GALLEY) · airframe 77,234 hrs · 45,270 cycles

AFT GALLEY L/H UPPER EMERGENCY BATTERY PACK BAD / [01] R/R BATTERY PACK @ M1673 POWER SUPPLY PER MM: 33-51-06.

Part: MODULE — FAILED · airframe 76,483 hrs · 44,808 cycles

LANDING GEAR LEVER JAMMED IN THE UP POSITION. LANDING GEAR EXTENDED PER THE CHECKLIST USING THE OVERRIDE TRIGGER. ; / [01] R&R LANDING GEAR CONTROL LEVER MODULE; REF AMM 32-31-11. ACCOMPLISHED LANDING GEAR SWING; REF AMM 32-61-00. LANDING GEAR SYSTEM OPERATES AS REQUIRED; NO DEFECTS NOTED.; [02] INSPECTED INSTALLATION AND OP?S CHECK OF LANDING GEAR MODULE. REF AMM 32-31-11.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 76,376 hrs · 44,736 cycles

SUPPLEMENTAL INFORMATION: SLIDE OUT OF POSITION ; FWD SERVICE DOOR SLIDE LOWER PORTION STICK OT. / [01] REPOSITION SLIDE TO LATCH VELCRO TO SLIDE CASE PER AMM 25-66-00; [02] ENTERED IN ERROR. WRONG AIRCRAFT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,287 hrs · 44,685 cycles

20 ABC EMERGENCY LIGHT INOP ; / [01] RELAMPED PER AMM 33-51-01.

Part: BULB — INOPERATIVE (EXIT SIGN) · airframe 74,508 hrs · 43,627 cycles

L1 LOWER EXIT IDENTIFIER HAS 1 BURNED OUT BULB / RELAMPED L1 LOWER EXIT IDENTIFIER AND PERFORMED GOOD OPS CHECK PER AMM 33-51-04-960-801 59889U 24APR21 59889U

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 74,508 hrs · 43,627 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP / RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT AND PERFORMED GOOD OPS CHECK PER AMM 33-51-01-960-801 59889U 24APR21

Part: FLOOR SUPPORT — CRACKED (BS 380-400 BL0) · airframe 74,508 hrs · 43,627 cycles

INTERCOSTAL AT BS 380-400 BL 0 WL 208 UPPER ATTACH ANGLE IS CRACKED. / REMOVED DAMAGED INTERCOSTAL BS380 - 400 BL0 WL 208 AND LOCATED AND DRILLED NEW I.A.W BOEING DWG 143A5400 AND SRM 51-40-05-0G-0 OK TO INSTALL 80512R 13APR21 INSP 18 13APR21 INSTALLED NEW INTERCOSTAL BS380 - 400 BL0 WL208 I.A.W BOEING DWG 143A5400 AND SRM 51-40-02-0G-0

Part: SKIN — DENTED (BS 360 S17L) · airframe 74,508 hrs · 43,627 cycles

DENT OF FUSELAGE SKIN BS 360 + 2; 1.5' ABOVE 17L / THE DAMAGE WAS REPAIRED PER ATS ER 21-01672 REV IR AND SWA EA 21-153-01120 REV IR. REFER TO NRC U299215 FOR TRACKING

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 74,508 hrs · 43,627 cycles

STUB FRAME IS CRACKED AT BS 296; RBL 60; WL 265.

Part: SEAT TRACK — DAMAGED (BS 520 LBL25) · airframe 74,508 hrs · 43,627 cycles

MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 520; LBL 25; WL 208 / REMOVED SEAT TRACK BS 480 - BS 520 LBL 25 WL 208 AND INSTALLED NEW SEAT TRACK I.A.W BOEING DWG 148A5300 AND SRM 51-40-02-0G-0

Part: SEAT TRACK — CORRODED (BS 370-445 LBL25) · airframe 74,508 hrs · 43,627 cycles

***CORROSION*** ON SEAT TRACK CROWN BS 370- BS 445; LBL 25; WL 208 VARIOUS SPOTS (MARKED) / REMOVED CORROSION ON SEAT TRACK CROWN STA 370 - 445 LBL 25; WL 208 MAX MATERIAL REMOVED WAS .057' 1' X 1' IN WELL. OUT OF LIMITS PER SRM 51-10-02-0G-0; SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK BS 370 - 480 LBL 25 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5300

Part: SEAT TRACK — DAMAGED (BS 500D RBL25) · airframe 74,508 hrs · 43,627 cycles

MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 500D + 14; RBL 25; WL 208 / REMOVED SEAT TRACK BS 480 - BS 520 RBL 25 WL 208 AND INSTALLED NEW SEAT TRACK I.A.W BOEING DWG 143A5300 AND SRM 51-40-02-0G-0.

Part: SEAT TRACK — DAMAGED (BS 520 LBL 45) · airframe 74,508 hrs · 43,627 cycles

MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 520; LBL 45; WL 208 / REMOVED DAMAGE SECTION OF SEAT TRACK AND SPLICE BS 500C+10 - BS 520 AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE I.A.W SRM 53-20-52-2R-4 REPAIR 4; BOEING DWG 143A5300

Part: BEAR STRAP — CRACKED (BS 293-294 S8-9R) · airframe 74,508 hrs · 43,627 cycles

UPON COMPLETION OF CCN: 15021 FOUND 2 EA CRACKS COMMON TO THE BEAR STRAP; 1 EA ADJACENT TO THE EDGE AND 1 EA AROUND THE MIDDLE OF THE BEAR STRAP AT STA 293-294 BETWEEN STR 8R-9R / REPAIRED DAMAGE ON BEAR STRAP BS293-294; STR 8R-9R PER ER 21-01662 REV IR AND EA 21-153-01088 REV IR.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,508 hrs · 43,627 cycles

LT HORIZ. STAB RIB AT STAB STA 120.30 4TH VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZONTAL STABILIZER RIB AT STAB STA 102.30 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.

Part: INDICATOR — DAMAGED (EMERGENCY LIGHTS) · airframe 74,508 hrs · 43,627 cycles

FWD ATTENDANT ANNUNCIATOR LIGHT BAR IS DAMAGED. / REMOVED AND REPLACED DAMAGED FWD ATTENDANT ANNUNCIATOR LIGHT BAR AND EXIT SIGN LIGHT ASSEMBLY I.A.W. AMM 33-51-01-960-802 3. C. (5)(A)(6)(A)(C)(E) (10) SOPM 20-50-01 OPS CHECK WILL BE PERFORMED ON CARD U298669

Part: FLOORBEAM — CRACKED (BS 540 LBL1) · airframe 74,508 hrs · 43,627 cycles

CRACKED BREAK PANEL STA 540; LBL 1; WL 207. / REMOVED DAMAGED BREAK PANEL BS540 LBL1 - LBL25 WL207 I.A.W SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW BREAK PANEL I.A.W AIPC 53-31-00-05 AND SRM 51-40-05-0G-0 OK TO INSTALL 80512R 13APR21 INSP 18 13APR21 INSTALLED NEW BREAK PANEL BS540 LBL1 - LBL25 WL 207 I.A.W AIPC 53-31-00-05 AND SRM 51-40-02-0G-0

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 74,508 hrs · 43,627 cycles

ATTACH ANGLE ON THE FWD SIDE OF THE BS663 VAPOR BARRIER IS CRACKED AT LBL25 WL154 / REMOVED & REPLACED ATTACH ANGLE ON THE FWD SIDE OF BS 663 VAPOR BARRIER LBL 25; WL 154 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; AIPC 53-42-00-91.

Part: ANGLE — CRACKED (BS 692 RBL 1) · airframe 74,508 hrs · 43,627 cycles

CRACKED ANGLE COMMON TO CABLEGUARD INTERCOSTAL STA 692; RBL 1; WL 204-206 / REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE COMMON TO CABLEGUARD INTERCOSTAL STA. 692 RBL 1 WL 204-206 IAW SRM 51-40-02-0G-0 & DWG 273A9112

Part: SEAT TRACK — DAMAGED (BS 500D RBL45) · airframe 74,508 hrs · 43,627 cycles

MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 500D + 14; RBL 45; WL 208 / REMOVED SEAT TRACK BS 480 - BS 520 RBL 45 WL 208 AND INSTALLED NEW SEAT TRACK I.A.W BOEING DWG 143A5300 AND SRM 51-40-02-0G-0

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 74,508 hrs · 43,627 cycles

MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 520; LBL 45; WL 208 / REMOVED DAMAGE SECTION OF SEAT TRACK AND SPLICE BS 500C+10 - BS 520 AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE I.A.W SRM 53-20-52-2R-4 REPAIR 4; BOEING DWG 143A5300

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 74,508 hrs · 43,627 cycles

HORIZONTAL STIFFENER ON FWD SIDE BS663 VAPOR BARRIER IS CRACKED AT LBL8 WL152 / REMOVED DAMAGED STIFFENER AND INSTALLED NEW HORIZONTAL STIFFENER BS 663 LBL 6-32 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 & 111A1001

Part: SUPPORT FRAME — CORRODED (BS 727D-787) · airframe 74,508 hrs · 43,627 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE AS HAS OF CORROSION BS727D TO BS787+13 LBL25 WL156 / EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT; BS 727D - 787+13; REMOVED .020' FROM .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. FABRICATED REPAIR PARTS; LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; ALL IAW SRM 53-00-53-2R-5. MATERIAL BAC1496-377; LOT# 1442411-1. AND INSTALLED; ALL IAW SRM 53-00-53-2R-5. DWG 146A7500; AND PRIMED; REPAIR PARTS SRM 53-00-53-2R-5 7081R 12APR21

Part: STRINGER — CRACKED (BS 536 S26R) · airframe 74,508 hrs · 43,627 cycles

STR26R IS CRACKED AT BS536 / REMOVED DAMAGED STRINGER SECTION BS500D+10' - BS536 STR26R PER SRM 53-00-03-2R-1 & REPAIRED PER SRM 53-00-03-2R-1 STEP 4K & DWG 143A3230

Part: STRINGER — CRACKED (BS 536 S26L) · airframe 74,508 hrs · 43,627 cycles

STR26L IS CRACKED AT BS536 / REMOVED DAMAGED STRINGER SECTION BS500D+10' - BS536 STR26L AS PER SRM 53-00-03-2R-1 & REPAIRED PER SRM 53-00-03-2R-1 STEP 4K & DWG 143A3230

Part: FRAME — CRACKED (BS 312 S6L) · airframe 74,508 hrs · 43,627 cycles

BS 312 FRAME IS CRACKED ABOVE STRINGER 6L WL286 / REMOVED 1.3' LONG X 0.16 WIDE MATERIAL & CRACK FROM INNER CHORD FLANGE OF BS 312 FRAME JUST ABOVE STRINGER 6L; AS PER SRM 51-10-02-OG-0 AND REPAIRED PER ER 21-01695 REV IR & EA 21-153-01072 REV IR

Part: STRAP — CORRODED (BS 887 LBL7-13) · airframe 74,508 hrs · 43,627 cycles

AFT CARGO BAY FLOOR STRAP AT BS887 HAS AREAS OF CORROSION LBL7 TO LBL13 WL156 / EVALUATED CORROSION ON ACB FLOOR STRAP; BS887; FOUND TO BE; OUT OF LIMITS; DUE TO NO LIMITS IN SRM. REMOVED DAMAGED FLOOR STRAP; LOCATED; DRILLED; AND INSTALLED NEW FLOOR STRAP; ALL IAW; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A7500.

Part: STRINGER — CORRODED (BS 536 S27L) · airframe 74,508 hrs · 43,627 cycles

STR27L HAS CORROSION AT BS536 LBL16 WL151 / REMOVED DAMAGED STRINGER SECTION BS500D+11 - BS536 STR27L AS PER SRM 53-00-03-2R-1 & REPAIRED PER SRM 53-00-03-2R-1 STEP 4.K & DWG 143A3230

Part: STRINGER — CRACKED (BS 536 S24L) · airframe 74,508 hrs · 43,627 cycles

STR24L IS CRACKED AT BS536 / REMOVED DAMAGED STRINGER SECTION BS500D+11' - BS536 STR24L AS PER SRM 53-00-03-2R-1 & REPAIRED PER SRM 53-00-03-2R-1 STEP 4K & DWG 143A3230

Part: PRESSURE DECK — CRACKED (BS 666) · airframe 74,508 hrs · 43,627 cycles

UPON COMPLETION OF CCN: 753-201-00-02 FOUND CRACK AT STA 666 LBL 33 WL 203. AREA MARKED / REMOVED DAMAGE PART OF THE BEADED PRESSURE DECK WCB BS 663-675 LBL 30 - LBL 60 WL203 AND REPAIRED I.A.W SRM 53-40-51-2R-2 REPAIR 2 FIG 203.

Part: STRINGER — CRACKED (BS 536 S23R) · airframe 74,508 hrs · 43,627 cycles

STR23R IS CRACKED AT BS536 / STR 23R CRACK AT B.S 536 WAS REPAIRED PER ATS ER 21-01629 REV IR AND SWA EA #21-153-01105 REV IR

Part: STRINGER — CRACKED (BS 536 S24R) · airframe 74,508 hrs · 43,627 cycles

STR24R IS CRACKED AT BS536 / REMOVED DAMAGE STRINGER SECTION STR 24R BS500D+10' - BS536 & REPAIRED PER SRM 53-00-03-2R-1 STEP 4K & DWG 143A3230.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 74,508 hrs · 43,627 cycles

FWD CARGO BAY SHEILD AFT OF THE DOOR HAS AREAS OF CORROSION AROUND NUTPLATE HOLES BS493 TO BS500A RBL25 WL156 / EVALUATED CORROSION ON FWD CARGO BAY SHIELD AFT OF DOOR BS493 - 500A; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM. REMOVED DAMAGED SHIELD; DRILLED; LOCATED; DEBURRED; AND INSTALLED NEW SHIELD; IAW SRM51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A0080.

Part: STRINGER — CORRODED (BS 536 S25R) · airframe 74,508 hrs · 43,627 cycles

STR25R HAS CORROSION AT BS536 RBL30 WL152 / STR 25R AT B.S 536 WAS REPAIRED PER ATS ER 21-01628 REV IR AND SWA EA # 21-153-01141 REV IR

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,508 hrs · 43,627 cycles

LT HORIZ. STAB RIB AT STAB STA 120.30 2ND VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 2ND. VERTICAL STIFFENER IAW SRM 55-10-09-2R-5; SRM 51-40-02-0G-0; AMM 27-31-41-400-801; DWG #'S: 182A1500; 182A3001; 002A0001; 182A2401. 59796C 5APR'21

Part: BEAM — CRACKED (R1 DOOR) · airframe 74,508 hrs · 43,627 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) AND #5 (UPPER) BEAM TO BE BOTH CRACKED IN THE RADIUS / FWD SVC DOOR REPAIRED AND MODIFIED PER CMM 52-41-05; REV 39; 01NOV'10; AND SWA EO 5241-C-14093-NG; REV 2; 27AUG'20. WORK ACCOMPLISHED ON ATS WORK ORDER 538533. 56085U 15APR21

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,508 hrs · 43,627 cycles

LT HORIZ. STAB RIB AT STAB STA 120.30 3RD VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZONTAL STAB RIB AT STAB STA 120.30 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 74,508 hrs · 43,627 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REMOVED PREVIOUS REPAIR ON FLIGHT DECK FLOOR AND INSTALLED NEW REPAIR I.A.W EA 1-A53-33179 REV 1 BS 259 - BS 270 LBL 18 - RBL 10 WL 207.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 74,104 hrs · 43,403 cycles

LT HORIZONTAL STAB ;FWD LOWER L/E SLIDE CRACK. / REMOVED AND REPLACED LT HORIZONTAL STAB FWD LOWER SLIDER SEAL REF MM 53-31-31

Part: SLIDING WINDOW — LOOSE (COCKPIT) · airframe 73,515 hrs · 43,069 cycles

ON TAKEOFF ROLL CAPTAIN'S WINDOW SLID OPEN. REJECTED TAKEOFF AND WINDOW WOULD NOT SHUT. HANDLE SEEMS LOOSE. FOUND CAPTAIN`S SLIDE WINDOW HANDLE UNLOCK BUTTON INOPERATIVE. WINDOW CAN OPEN WITHOUT PUSHING UNLOCK BUTTON. R & R CAPTAIN`S SLIDING WINDOW, PER MT 756-12-01. OPERATIONS CHECKS NORMAL RAR 74551 POS; L2 PN OFF; 141A4810-37EFB SN OFF; 406 PN ON; 141A4810-24EFB1025 SN ON; 05314H7330.

Part: BRACKET — DAMAGED (EMER EXIT SIGN) · airframe 73,455 hrs · 43,029 cycles

CEILING EXIT SIGN BRACKET DAMAGED AT 12F. R & R EIT SIGN, REF 33-51-01.

Part: ANGLE — CRACKED (RT WING) · airframe 72,716 hrs · 42,545 cycles

R/H WING AFT TRAILING EDGE UPPER PANEL ABOVE #2 ENG AFT FAIRING COVE SEAL ANGLE IS CRACKED / REMOVED AND REPLACED SEAL ANGLE IAW SRM 51-40-02.

Part: RADOME — DAMAGED (NOSE) · airframe 72,716 hrs · 42,545 cycles

NOSE RADOME HAS FIBER DAMAGE / REPLACED RADOME REF MM 53-52-00 TAG NO: 663058 PN ON: 10010027B SN ON: C152308 PN OFF: SN OFF: 9810012C

Part: FUSE — INOPERATIVE (CABIN) · airframe 72,716 hrs · 42,545 cycles

RT EMERGENCY EXIT SIDEWALL LIGHT IS INOP. R&R RT EMERGENCY EXIT LIGHT FUSE PER AMM 33-21-00.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 72,656 hrs · 42,510 cycles

LT MLG WHEEL WELL HAS A 12' CRACK IN THE VAPOR BARRIER NEAR LBL 10. ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 71,969 hrs · 42,104 cycles

FORWARD BULKHEAD VAPOR BARRIER CRACKED THE L/H WHEEL WELL NEAR "A" ELECTRICAL HYDRAULIC PUMP CRACK LOCATED IN MOD. / REPAIRED BARRIER PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,773 hrs · 41,981 cycles

L1 DOOR SLIDE HAD EXCESS HANGING. REPOSITIONED SLIDE IN COMPARTMENT PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,650 hrs · 41,896 cycles

L/H EMERGENCY LIGHT INOP AT SEAT 24. / RELAMPED LIGHT PER AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 71,228 hrs · 41,650 cycles

EXIT SIGN AT FORWARD ENTRANCE BROKEN. / SECURED LENS PER SIP.

Part: SIGN — UNSECURE (CABIN) · airframe 70,589 hrs · 41,225 cycles

OVERHEAD/OVERWING EXIT SIGN KNOCKED OUT OF BRACKET. SECURED EXIT SIGN PER MM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 70,285 hrs · 41,023 cycles

L2 DOOR EMERGENCY EXIT LENS CAME OFF. R&R LENS IAW AMM.

Part: HOUSING — LOOSE (EMERGENCY LIGHT) · airframe 70,285 hrs · 41,023 cycles

L2 DOOR EMERGENCY EXIT LENS CAME OFF. R&R BASE ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 70,201 hrs · 40,966 cycles

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

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 69,861 hrs · 40,739 cycles

R2 DOOR SLIDE DEPLOYMENT HANDLE LOOSE. SECURED COVER PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 69,711 hrs · 40,640 cycles

R1 DOOR ABOVE EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER EA.

Part: PANEL — DELAMINATED (RT WING) · airframe 69,690 hrs · 40,625 cycles

RIGHT WING LOWER L/E PANEL 621YB FWD SECTION DELAMINATED (231-513-1) / CLEANED THE DAMAGED AREA OF RIGHT WING LOWER L/E PANEL 621YB REF B737-700 SRM 51-70-06-2B-6 REPAIR 6-4B; FILL THE DAMAGE WITH LAMINATING RESING; CURED ITS AND APPLIED FINISH REF B737-700 SRM 51-70-06-2B-6 REPAIR 6-4G MAT USED EA-934NA PO# 1590993.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO AFT BULKHEAD INTERCOSTAL CORRODED. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (AFT CARGO BAY) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO INTERCOSTAL BETWEEN BS. 927-947 AND S-26R CRACK FOUND. / REPLACED AFT CARGO INTERCOASTAL BETWEEN BS 927-947 AND 3-26R AFTER THE FABRICATION ON N/R . W101959-2014926-1000-0116. INSTALLATION ACCOMPLISHED IAW B737 SRM 51-40-02-0G-0 AND DWG 147A7580

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

AFT PRESSURE WEB AT FLOOR LEVEL INTERCOSTAL CORRODED AT BS. 1016. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (AFT PRESS BULKHE) · airframe 69,690 hrs · 40,625 cycles

STA 1016 AFT PRESSURE WEB AT FLOOR LEVEL INTERCOSTAL P/N: 65-54862-17 HAS CORROSION AND IT REQUIRES TO BE FABRICATED / AFTER EVALUATION OF CORRISION AT THE AFT PRESSURE BULKHEAD LOWER LOBE INTERCOASTAL P/N 65-54862-17 BETWEEN LB-0 TO LB2-28 FOUND TO BE OUT OF LIMITS .IAW B737-700 SRM53-80-48-1A-1.REMOVED INTERCOASTAL P/N 65-54862-17.IAWB737-700 SRM 51-40-02.FABRICATIONINTERCOASTAL P/N 65-54862-17.IAW BOEING DWG #148A0922. INSTALLED INTERCOASTAL P/N65-54862-17 AFTER FABRICATION .IAWB737-700 SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

AFT PRESSURE WEB LOWER SECTION INTERCOSTAL CORRODED AT BS. 1016, BETWEEN LBL 0 TO LBL 28. REPAIRED INTERCOSTAL IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

FLOOR PANEL CRACKED ON LOWER SURFACE 232SF. REPAIRED FLOOR PANEL # 232SF IAW SRM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 69,690 hrs · 40,625 cycles

CABIN FLOOR PANEL CRACKED ON UPPER EDGE AREA 241EF. REPAIRED FLOOR PANEL IAW SRM.

Part: PANEL — CRACKED (VERTICAL STAB R/) · airframe 69,690 hrs · 40,625 cycles

PANEL ASSY #323CR VERTICAL FAN R/H FLANGE CRACKED MKD DOT 60-120 / REMOVED & REPLACED FLANGE AT PANEL # 323CR VERTICAL FAN R/H IAW B737-700 SRM 51-40-02-0G-0

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 69,690 hrs · 40,625 cycles

CABIN FLOOR PANEL HAS CRACK ON LWR SURFACE 242DF 8-32 / CLEANED THE REPAIR AREA OF CABIN FLOOR PNL 242DF AND INSTALLED FIBER GLASS REPAIR REF B737-700 SRM 53-00-50-2R-2. REPAIR 2-3L MATERIALS USED EY3804AB PO# 1608199 AND HCS2410-030 PO# 1150387

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,690 hrs · 40,625 cycles

FWD CARGO CTR SCUFF PLATE CRACKED AT WELD SPOT. 8-37 / SENT OUT FOR WELDING BY J.L. WELDING CUSTOMER ORDER NUMBER 412325. RECEVIED WITH ISSHED TAG AF 7627 PARTS CONTROL TAG 364286 CP 18533 5-21-19

Part: SCUFF PLATE — BROKEN (FWD CARGO BAY) · airframe 69,690 hrs · 40,625 cycles

FWD CARGO FWD CORNER SCUFF PLATE BROKEN. 8-38 / LOCATED AND DRILLED NEW SCUFF PLAE AT FWD CARGO DOOR (FWD CORNER POSITION) IRW 737-700 SRM 51-40-05-0G-0; 51-20-01-0G-0

Part: ANGLE — CRACKED (RT MLG WW) · airframe 69,690 hrs · 40,625 cycles

R/H WHEEL WELL FORWARD LOWER WEB UPPER SUPPORT ANGLE CRACKED AT BS. 663.75, RBL 44. REPAIRED ANGLE PER EA.

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 69,690 hrs · 40,625 cycles

WING TO BODY FAIRING 192BL HAS A CRACK ON OUTER SURFACE 1' LONG. 8-3 / REMOVED DAMAGE AREA ON WING TO BODY FAIRING 192 BL OUTERSURFACE CLEANED ;PREPARED AND INSTALLED REPAIR PLIES IAW B737-7 SRM 51-70-05-2R-1 TOTAL REPAIR SIZE 3' DIAMETER

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 69,690 hrs · 40,625 cycles

L/H WHEEL WELL FORWARD LOWER WEB UPPER SUPPORT ANGLE CRACKED AT BS. 663.75, LBL 44. / REPAIRED ANGLE PER EA.

Part: STRINGER — CORRODED (BS 960) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO COMPARTMENT STRINGER CORRODED AT RIVET TAIL AT BS. 960, STR. 25L. REPAIRED PARTIAL STRINGER IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS. 887, BETWEEN STR. 26L TO STR. 26R. REPAIRED FLOOR SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO TRACK CORRODED BETWEEN BS. 827 TO 787, 15 INCHES RT OF CENTER LINE AROUND NUT PLATES. R&R TIE DOWN TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED BETWEEN BS. 727D TO BS. 807, BETWEEN LBL 21 TO LBL 22. R&R SUPPORT ZEE IAW SRM.

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 69,690 hrs · 40,625 cycles

AFT CARGO FLOOR SUPPORT ZEE CHANNEL HAS CORROSION AROUND NUT PLATES 22 INCHES RIGHT OF CENTER LINE FROM 727A TO 787. / REMOVED AND REPLACED ZEE CHANNEL FROM STA 727A TO 767 RBL 21.0; TREATED AND PRIMED AND INSTALLED. BLENDED AND REMOVED CORROSION FROM SHIELD FROM STA 767-787 RBL 21.0 WITHIN LIMITS IAW B737-700 SRM 51-10-02-0G-0 SRM 53-60-15-1A-1 FIG 103 DETAIL D; SRM 53-00-53-1A-2 FIG 103 DETAIL D; SRM 53-70-53-01-2; SRM 51-40-02-0G-0 AND SRM 51-20-01-0G-0 AND DWG 146A7500

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

MAIN CABIN AFT PRESSURE BULKHEAD LOWER LOBE WEB CORRODED AT BS. 1016, BETWEEN LB 0 TO LBL 28 (P/N 65-54862-19). R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

MAIN CABIN AFT PRESSURE BULKHEAD LOWER LOBE WEB AREA CORRODED AT BS. 1016, BETWEEN RBL 25 TO RBL 41. R&R INTERCOSTAL IAW SRM.

Part: PANEL — CRACKED (SLAT) · airframe 69,690 hrs · 40,625 cycles

LH WING SLAT #1 PANEL 525AB HAS CRACK / REMOVED PANEL 525 AB AND FABRICATED PER BOEING DRAWING; PL 114A8111; TREATED+PRIMED & INSTALLED PANEL 525 AB AT LT; WING SLAT # 1 PER REF. B737-700 AMM 51-21-72-370-801 AND SRM 51-40-02-0G-0

Part: ANGLE — BROKEN (VERTICAL STABILI) · airframe 69,690 hrs · 40,625 cycles

R/H VERTICAL STABILIZER; ACCESS PNL 324AR WITH SUPPORT ANGLE BROKEN / REMOVED AND REPLACED ANGLES (CHANNEL AND RETAINER) AT R/H VERTICAL STABILIZER; ACCESS PANEL 324 AR AS PER REF B737-700 SRM SRM 51-40-02-06-0

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

MAIN CABIN AFT PRESSURE BULKHEAD LOWER LOBE WEB CORRODED AT BS. 1016, BETWEEN LB 0 TO LBL 28 (P/N 65-54862-17). R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

MAIN CABIN AFT PRESSURE BULKHEAD LOWER LOBE WEB CORRODED AT BS. 1016, BETWEEN LB 0 TO LBL 28 (P/N 65-54862-18). R&R INTERCOSTAL IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

BULKHEAD PRESSURE WEB CRACKED AT BS. 663.75, LBL 35. REPAIRED BULKHEAD IAW SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,690 hrs · 40,625 cycles

PRESSURE WEB ON EDGE OF STIFFENING BEAD CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 38.0 TO RBL 60.0. REPAIRED WEB IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,217 hrs · 40,336 cycles

R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R POWER SUPPLY BATTERY PACK PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INNER FACE CORRODED. REPAIRED LUG PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — LOOSE (LT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOOSE. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,941 hrs · 40,159 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FORCE CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 68,786 hrs · 40,071 cycles

L2 DOOR SLIDE LOOSE. REINSTALLED SLIDE IAW MT.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,010 hrs · 39,581 cycles

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

Part: SIGN — UNSECURE (L1 DOOR) · airframe 67,569 hrs · 39,307 cycles

L1 DOOR EMERGENCY EXIT SIGN CAME OFF. REINSTALLED SIGN PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 67,013 hrs · 38,954 cycles

L1 DOOR ESCAPE SLIDE GIRT STRAP LOOSE. REINSTALLED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 65,625 hrs · 38,065 cycles

RT OVERWING EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM.

Part: STRAP — CRACKED (EMERGENCY EXIT) · airframe 65,071 hrs · 37,718 cycles

RT OVERWING EMERGENCY EXIT ASSIST STRAP BOX CRACKED. R&R STRAP BOX AND COVER PER SIP.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 63,404 hrs · 36,679 cycles

LT EMERGENCY ESCAPE GROUND FLOOR LIGHT INOP. SECURED CONNECTOR PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,084 hrs · 36,472 cycles

RT OVERWING EMERGENCY EXIT DOOR ESCAPE HATCH LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,084 hrs · 36,472 cycles

RIGHT WING TRAILING EDGE ANGLE CRACKED AT ORSS. 261+11 AFT POSITION. R & R THE ANGLE IAW SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 63,084 hrs · 36,472 cycles

LT WING INBOARD FLAP WEDGE ASSEMBLY DELAMINATED ON LOWER EDGE. REPAIRED FLAP WEDGE ASSEMBLY IAW SRM AND EA.

Part: WEB — CRACKED (BS 312-328) · airframe 63,084 hrs · 36,472 cycles

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

Part: ANGLE — CRACKED (LEFT WING) · airframe 63,084 hrs · 36,472 cycles

LEFT WING TRAILING EDGE ANGLE CRACKED AT REAR SPAR WS 94.24. R & R THE ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,084 hrs · 36,472 cycles

LEFT WING SUPPORT ANGLE CRACKED BETWEEN WS 204.25 TO 228.25, REAR SPAR LOWER SURFACE. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 63,084 hrs · 36,472 cycles

L1 DOOR EMERGENCY EVAC SLIDE FLOOR DOOR MOUNTED BRACKET CORRODED. R&R BRACKET IAW AMM.

Part: BRACKET — CORRODED (R1 DOOR SLIDE) · airframe 63,084 hrs · 36,472 cycles

R1 DOOR SLIDE MOUNTED BRACKET CORRODED. R & R THE BRACKET IAW AMM.

Part: WEB — CRACKED (RT WING) · airframe 63,084 hrs · 36,472 cycles

RIGHT WING OTBD FIXED LEADING EDGE WEB CRACKED AT FSS. 630. R & R THE WEB IAW SRM AND DWG.

Part: SUPPORT — CRACKED (BS 312-326) · airframe 63,084 hrs · 36,472 cycles

WEB SUPPORT CRACKED BETWEEN BS 312 - 326, RBL 30.5. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CRACKED (BS 344-360) · airframe 63,084 hrs · 36,472 cycles

WEB SUPPORT CRACKED BETWEEN BS 344 TO 360, LBL 11. R & R THE SUPPORT IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 344-360) · airframe 63,084 hrs · 36,472 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 326-344) · airframe 63,084 hrs · 36,472 cycles

FLOOR SUPPORT CRACKED AT BS 326 TO 344, LBL 45. R & R THE FLOOR SUPPORT IAW SRM.

Part: LIGHT — BROKEN (GALLEY) · airframe 63,084 hrs · 36,472 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT BROKEN AT GALLEY 1. R & R LIGHT IAW AMM.

Part: SUPPORT — CRACKED (LT WING) · airframe 63,084 hrs · 36,472 cycles

LT WING TO BODY FAIRING SUPPORT STRUCTURE CRACKED AT BS 500D. R&R SUPPORT IAW SRM AND DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 63,084 hrs · 36,472 cycles

EMERGENCY LIGHT CRACKED. R & R THE EMERGENCY LIGHT IAW AMM.

Part: ANGLE — CORRODED (BS 767-787) · airframe 63,084 hrs · 36,472 cycles

AFT CARGO BAY WEB ANGLE CORRODED BETWEEN BS 767 TO 787+5, STRINGER 25R. R & R THEWEB ANGLE IAW SRM AND DWG.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 62,559 hrs · 36,183 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE IN BRACKETS. R&R BRACKET ASSEMBLY PER AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,047 hrs · 34,662 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 59,029 hrs · 34,075 cycles

RIGHT OVERWING EMER EXIT LENS LOOSE. SECURED LENS IAW SIP.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 58,538 hrs · 33,811 cycles

CROSS FEED VLV CB OPEN. R & R FUEL CROSS FEED VLV IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,077 hrs · 33,554 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 57,406 hrs · 33,163 cycles

EMERGENCY LIGHT BATTERY PACK FAILED OPERATIONS TEST AT M1674. R & R BATTERY IAW AMM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 57,406 hrs · 33,163 cycles

NUMBER 3 COCKPIT WINDOW FRAME CRACKED AT BS 259.5, STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 57,406 hrs · 33,163 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

FORWARD SEAT TRACK, OUTBOARD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW FAS EA.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 57,406 hrs · 33,163 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 57,406 hrs · 33,163 cycles

FORWARD SEAT TRACK OUTBOARD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 57,406 hrs · 33,163 cycles

FORWARD SEAT TRACK OUTBOARD & INBOARD FLANGES CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,406 hrs · 33,163 cycles

LEFT NUMBER 3 FLIGHT DECK WINDOW FRAME CRACKED AT THE SECOND LOWER FASTENER HOLE FROM THE BOTTOM. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,406 hrs · 33,163 cycles

LEFT WING NR 1 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,406 hrs · 33,163 cycles

RIGHT WING NR 7 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,406 hrs · 33,163 cycles

RIGHT WING NR 6 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,406 hrs · 33,163 cycles

LEFT WING NR 5 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 57,232 hrs · 33,070 cycles

FWD EMERGENCY LIGHT STRIP WAS FOUND DAMAGED. R & R THE EMERGENCY LIGHT STRIP IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,232 hrs · 33,070 cycles

THE EMERGENCY BATTERY M01669 FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 57,232 hrs · 33,070 cycles

THE AFT EMERGENCY LIGHT STRIP WAS FOUND DAMAGED. R & R THE EMERGENCY LIGHT STRIP IAW MM.

Part: SWITCH — LOOSE (CABIN) · airframe 56,136 hrs · 32,473 cycles

AFT EMER LIGHT PANEL SWITCH LOOSE. R & R LIGHT ASSEMBLY IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,952 hrs · 31,777 cycles

LEFT OVERWING CABIN EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 54,952 hrs · 31,777 cycles

RIGHT MLG WW VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,952 hrs · 31,777 cycles

RIGHT OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,952 hrs · 31,777 cycles

CEILING AFT ENTRY EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,952 hrs · 31,777 cycles

FORWARD ENTRY EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,952 hrs · 31,777 cycles

MID CABIN EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.

Part: LENS — LOOSE (CABIN) · airframe 54,952 hrs · 31,777 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 54,515 hrs · 31,524 cycles

RIGHT OVERWING EMER EXIT LENS COVER MISSING. INSTALLED LENS IAW AMM.

Part: HANDLE — LOOSE (EVAC SLIDE) · airframe 53,579 hrs · 30,979 cycles

R2 DOOR EMER EVAC SLIDE MANUAL INFLATION HANDLE LOOSE. SECURED HANDLE IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,581 hrs · 30,395 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 52,193 hrs · 30,165 cycles

RT SIDE EMERGENCY EXIT ROW, EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,517 hrs · 29,161 cycles

LEFT NR 3 WINDOW E&F FRAME 2ND HOLE FROM BOTTOM HFEC HOLE PROBE CRACKED. REPAIRED FRAME IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,517 hrs · 29,161 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT THE SECOND LOWER FASTENER HOLE FROM THE BOTTOM. REPAIRED FRAME IAW SWA EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,517 hrs · 29,161 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT THE THIRD LOWER FASTENER HOLE FROM THE BOTTOM. REPAIRED FRAME IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,093 hrs · 27,109 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,981 hrs · 27,041 cycles

RIGHT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: PLATE — MISSING (CABIN) · airframe 46,443 hrs · 26,735 cycles

LOWER EXIT LIGHT FORWARD GALLEY BY R1 DOOR MISSING FACE PLATE. REPLACED LIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 45,735 hrs · 26,325 cycles

FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 45,735 hrs · 26,325 cycles

FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,000 hrs · 25,888 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — CRACKED (CABIN) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT SIGN LIGHT LENS MOUNTED ON FWD LAV WALL CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB PER EA AND ER.

Part: CONNECTOR — CRACKED (CABIN) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EEPLS CONNECTOR CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED CONNECTOR PER WDM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME SUPPORT ANGLE CORRODED AT BS 787, BETWEEN STR 22L TO STR 25L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: PLATE — CORRODED (GIRT BAR) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT SUPPORT CORRODED AT BS 312, LBL 55. REMOVED AND REPLACED PLATE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, BETWEEN RBL 6 TO RBL 11. REMOVED AND REPLACED BEAM PER SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR WEB SUPPORT CHANNEL CORRODED BETWEEN BS 260 TO BS 270, BL 0. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: ATTACH FITTING — MISSING (GIRT BAR) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULE 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT THREADED INSERT MISSING. REMOVED AND REPLACED ATTACH ASSY PER DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR THRESHOLD SUPPORT Z CORRODED BETWEEN BS 312 TO BS 344, LBL 63. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,840 hrs · 25,212 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,766 hrs · 26,918 cycles

BULKHEAD WEB CRACKED AT BS 663 , RBL 35. REPAIRED WEB PER EA AND ER.

Part: LIGHT — BROKEN (CABIN) · airframe 43,829 hrs · 25,204 cycles

R2 DOOR EEPLS ASSY BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 43,683 hrs · 25,117 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 41,276 hrs · 23,689 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 40,903 hrs · 23,477 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 40,344 hrs · 23,152 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,234 hrs · 23,094 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,211 hrs · 22,534 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 39,006 hrs · 22,398 cycles

L1 COCKPIT WINDOW ARCED TWICE IN FLIGHT. REMOVED AND REPLACED WINDOW PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,348 hrs · 20,799 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,348 hrs · 20,799 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,348 hrs · 20,799 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,348 hrs · 20,799 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 35,574 hrs · 20,343 cycles

RT WING OVERWING EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,788 hrs · 19,858 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP INOP AT ROW 11. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,788 hrs · 19,858 cycles

DURING SCHEDULED HC2 CHECK, LT AFT GALLEY EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 33,285 hrs · 18,960 cycles

DIVERSION/DECLARED EMERGENCY, CLIMBING THROUGH 3000' AGL NR 1 ENGINE COMPRESSOR STALLED, VIBRATION OCCURRED, ENGINE FLUCTUATED. R&R NR 1 ENGINE PER MT.

Part: WIRE HARNESS — ARCED (COCKPIT) · airframe 31,958 hrs · 18,159 cycles

AIR TURNBACK, FLIGHT DECK L1 WINDOW ELECTRICAL CORD ARCED. REMOVED AND REPLACED ELECTRICAL HARNESS PER MM.

Part: FRAME — CRACKED (BS 295 S15L) · airframe 30,485 hrs · 17,319 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CRACKED AT BS 295, STR 15L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (BS 986) · airframe 30,485 hrs · 17,319 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 986, RBL 45. REPAIRED FLOORBEAM WEB PER MM.

Part: FLOORBEAM — CRACKED (BS 986) · airframe 30,485 hrs · 17,319 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 986, LBL 35. REPAIRED FLOORBEAM WEB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,485 hrs · 17,319 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 47. REPAIRED FLOORBEAM PER SRM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 25,032 hrs · 14,206 cycles

LEFT FWD CABIN EEPLS COVER LOOSE. SECURED LT FWD CABIN EEPLS COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,978 hrs · 14,167 cycles

EEPLS TRACK LOOSE AT FWD LT SIDE. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,944 hrs · 14,149 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 24,944 hrs · 14,149 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 24,944 hrs · 14,149 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 23,680 hrs · 13,433 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 13 DEF. SECURED LENS PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,993 hrs · 13,066 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,063 hrs · 11,995 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON LT OVERWING DOOR & CENTER AISLE. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 20,016 hrs · 11,398 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 18,722 hrs · 10,671 cycles

DURING SCHEDULED 5Y CHECK, FOUND CABIN SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 18 DEF, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 18,197 hrs · 10,392 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, MISSING. REPLACED LIGHT LENS PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 17,891 hrs · 10,228 cycles

EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — CRACKED (ROW 1 ABC) · airframe 17,558 hrs · 10,046 cycles

EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,500 hrs · 10,000 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EEPLS INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM.

Part: INDICATOR — MALFUNCTIONED (SLIDE BOTTLE) · airframe 17,273 hrs · 9,884 cycles

L1 DOOR EVAC SLIDE LOW PRESS IND. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 16,968 hrs · 9,719 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (MID CABIN) · airframe 14,193 hrs · 8,218 cycles

EEPLS INOP AT MID CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,035 hrs · 7,594 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED (4 EA) AT ROW NR 11, ROW NR 12, ROW NR 20 AND ROW NR 21. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 8,343 hrs · 4,965 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN ( 8 EA ). R&R COVERS PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 8,201 hrs · 4,893 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.