N730SW

Part: HANDLE — OUT OF POSITION (R2 DOOR SLIDE) · airframe 76,793 hrs · 45,227 cycles

R2 DOOR SLIDE PULL TO INFLATE HANDLE IS VISIBLE. REPOSITION R2 DOOR SLIDE HANDLE FLAP IAW AMM 25-66-01; OK FOR SERVICE.

Part: SEAT TRACK — INOPERATIVE (COCKPIT) · airframe 75,583 hrs · 44,545 cycles

F/OS SEAT SLIDE ADJUSTMENT INOP. REMOVED OBSTRUCTION FROM SEAT TRACK PER. SIP MM 20-00-00 OPS CHECK NORMAL

Part: COVER — MISSING (CABIN) · airframe 75,080 hrs · 44,255 cycles

AFT SERVICE EXIT LENS FELL OFF / CLEARING DMA LOG PAGE# 0180851 R/R EMERGENCY LIGHT LENS COVER AT R2 DOOR PER AMM 33-51-03. OPS OK. MDDR CL# 72211

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 74,542 hrs · 43,942 cycles

FWD RT EXTERIOR EMERGENCY LIGHT INOPERABLE. R & R LAMP AT FWD RT EXTERIOR EMERGENCY LIGHT, PER AMM 33-51-04.

Part: BATTERY — INOPERATIVE (EXTERIOR LIGHT) · airframe 74,542 hrs · 43,942 cycles

EXTERIOR EMERGENCY LIGHT AT AFT RT CABIN DOOR INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND BATTERY CHARGER M1672 AND PERFORMED GOOD OPERATIONS CHECK, PER AMM 33-51-00-960-806 AND AMM 33-51-06-960-805 59889U 05DEC20.

Part: CHARGER — INOPERATIVE (EXTERIOR LIGHT) · airframe 74,542 hrs · 43,942 cycles

EXTERIOR EMERGENCY LIGHT AT AFT RT CABIN DOOR INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND BATTERY CHARGER M1672 AND PERFORMED GOOD OPERATIONS CHECK, PER AMM 33-51-00-960-806 AND AMM 33-51-06-960-805 59889U 05DEC20.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 74,542 hrs · 43,942 cycles

EMERGENCY LIGHTS POWERED FROM CHARGER M1673 STAY ON FOR APPROXIMATELY ONE MINUTE, THEN GO OUT. REPLACED POWER SUPPLY M1673 AND PERFORMED SATISFACTORY, PASSING TEST OF NEW POWER SUPPLY, PER AMM 33-51-06-960-806.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 74,542 hrs · 43,942 cycles

M1674 FAILS BATTERY PACK CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK FOR M1674 WITH SERVICEABLE UNIT AND TESTED GOOD, PER AMM 33-51-06-960-805. 59019U 04DEC20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,542 hrs · 43,942 cycles

G-4 EMERGENCY EXIT LOCATOR SIGN HAS LAMPS INOPERABLE. REMOVED AND REPLACED G-4 EMERGENCY EXIT LOCATOR SIGN LAMP AND PERFORMED GOOD INSTALLATION TEST. ALL WORK PERFORMED, PER AMM 33-51-01-960-801 STEP 2B (1)(A) (2); (2) AND (4). 57574U 03DEC20.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 74,542 hrs · 43,942 cycles

LEFT OVER WING HATCH SLIDE LIGHT INOPERABLE. RELAMPED LT OVERWING HATCH SLIDE LIGHT AND TESTED GOOD, PER AMM 33-51-04-960-801. 59019U 04DEC20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,542 hrs · 43,942 cycles

RIGHT OVER WING HATCH AFT EMERGENCY LAMP INOPERABLE. RELAMPED RIGHT OVERWING HATCH AFT EMERGENCY EXIT LAMP AND TESTED GOOD, PER AMM 33-51-01-960-801. 59019U 04DEC20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,542 hrs · 43,942 cycles

LEFT HAND OVER WING EXIT FWD LOWER EMERGENCY EXIT LOCATOR SIGN HAS LAMPS INOPERABLE. RELAMPED INOPERABLE BULBS IN THE LT OVERWING EXIT LOWER LOCATOR SIGN AND TESTED GOOD, PER AMM 33-51-01-960-801. 59019U 04DEC20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,542 hrs · 43,942 cycles

FWD ENTRY DOOR EMERGENCY LAMPS INOPERABLE. RELAMPED INOPERABLE LAMPS IN FWD ENTERY DOOR EMERGENCY EXIT SIGN AND TESTED GOOD, PER AMM 33-51-01-960-801. 59019U 04DEC20.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 74,542 hrs · 43,942 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727B-787 LBL 23 WL 156. REMOVED AND INSTALLED NEW AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT, IAW SRM 53-00-53 SRM 51-40-02 DWG 146A7500 AT BS 727+4 TO 847 LBL 23 WL 156.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 74,542 hrs · 43,942 cycles

PASSENGER CABIN FLOOR PANEL 221BF AFT OUTBOARD TAB IS CRACKED. PASSENGER CABIN FLOOR PANEL 221BF WITH CRACKED AFT OUTBOARD TAB WAS REPLACED WITH A SERVICEABLE FLOOR PANEL, DUE TO AMOUNT OF ALLOWABLE DAMAGE, PER SRM 51-10-02-0G-0 PARA 9A(1).

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 74,542 hrs · 43,942 cycles

PASSENGER CABIN FLOOR PANEL 222AF AFT OUTBOARD CORNER HAS INNER CORE AND LOWER SURFACE DAMAGE. / REPAIRED AFT O/B CORNER ON PASSENGER CABIN FLOOR PANEL 222AF PER SRM 53-00-50-2R-10 AND SRM 53-00-50-2R-0.

Part: WEB — CORRODED (FUSELAGE) · airframe 74,542 hrs · 43,942 cycles

CORROSION ON VERTICAL WEB BS 259 LBL 4 TO RBL 6 WL 207. CORROSION ON VERTICAL WEB BS 259 LBL 4 TO RBL 6 WL 207 WAS FOUND TO BE OUT OF LIMITS, PER SRM 53-10-51-1A-1 FIG 105(E). AREA WAS REPAIRED, PER EA 20-153-02333 REV IR & ER 20-03616 REV IR.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 74,542 hrs · 43,942 cycles

CORROSION ON CREASEBEAM WEB ATTACH ANGLE STA 665 RBL 67 WL 208 UPPER SURFACE. REMOVED CORROSION ON CREASE BEAM WEB ATTACH ANGLE STA 665 RBL 67 WL 208, PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS .016' 1' X .5' FROM .056'. AND OF LIMITS, PER SRM 53-40-13-1A-1. REMOVED DAMAGED ATTACH ANGLE AND FABRICATED NEW FROM 7075T6 CLAD 7075T6 .056' LOT NR 1331117-2, PER DWG 144A5930, SRM 51-40-02-0G-0, SRM 51-30-01-0G-0. LOCATED & DRILLED AND APPLIED CHEM CONV COATING AND PRIMED, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-20-01-0G-0; SOPM 20-43-03. INSTALLED PER SRM 51-40-02-0G-0 AND DWG 144A5920.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 74,542 hrs · 43,942 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS 540-BS 727B RBL 45 WL 208, MARKED. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK AT BS 540-727B RBL 45 WL 208, IAW DWG 144A5300 AND SOPM 20-50-01.

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 74,542 hrs · 43,942 cycles

CRACKED BREAK PANEL STA 540; BL0-RBL 25; WL 207. / REMOVED AND REPLACED BREAK PANEL ASSY AT STA 540; BL0 - RBL 25; WL 207; PER SRM 51-40-02-0G-0; PARAGRAPH 7.

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 74,542 hrs · 43,942 cycles

CRACKED BREAK PANEL STA 540; BL0-LBL 25; WL 207. / REMOVED AND REPLACED BREAK PANEL ASSY AT STA 540; BL0 - LBL25; WL 207; PER SRM 51-40-02-0G-0.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,542 hrs · 43,942 cycles

CORROSION ON CREASEBEAM INNER CHORD STA 675-727 RBL 65 WL 208 UPPER SURFACE. REMOVED DAMAGED CREASE BEAM INNER CHORD AND INSTALLED NEW CREASE BEAM INNER CHORD AT BS 675-727 RBL 65 WL 208, IAW SRM 51-40-02-0G-0 AND DWG 144A5900.

Part: THRESHOLD — CRACKED (FWD CARGO) · airframe 74,542 hrs · 43,942 cycles

FORWARD CARGO FORWARD CORNER THRESHOLD IS CRACKED / FORWARD CARGO BAY FORWARD CORNER THRESHOLD WAS REPAIRED PER SRM 53-30-15-2R-1. FWD CORNER SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD# U240230.

Part: THRESHOLD — CRACKED (AFT CARGO) · airframe 74,542 hrs · 43,942 cycles

AFT CARGO FORWARD CORNER THRESHOLD IS CRACKED / AFT CARGO BAY; FORWARD CORNER THRESHOLD WAS REPAIRED PER SRM 53-60-15-2R-1. FWD CORNER SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD# U240229.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 74,542 hrs · 43,942 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS 540-BS 727B LBL 25 WL 208, MARKED. REMOVED CORROSION FROM SEAT TRACK STA 540-727B LBL 25 WL 208, PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED OF 0.50' BETWEEN TEETH FOUND TO BE OUT OF LIMITS, PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK AT STA 540-727B LBL 25 WL 208, PER SOPM 20-50-01, REFERENCING BOEING DWG 144A5300 SHEET 1.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 74,542 hrs · 43,942 cycles

CORROSION BS 270 FWD CHORD RBL 4-RBL 10 WL 208. THE DAMAGE IS REPAIRED, PER EA 1-A53-13812 REV 3 AND ER 20-03616 REV IR.

Part: STRUCTURE — CORRODED (LAV SERVC DOOR) · airframe 74,542 hrs · 43,942 cycles

LAV SERVICE DOOR HAS CORROSION AROUND BONDING JUMPER STUD ON DOOR SIDE / FOUND CORROSION ON LAV SERVICE DOOR OUT OF LIMITS; ORIGINAL THICKNESS .060; REMOVED .020 MATERIAL 1' X 1'; OUT OF LIMITS PER SRM 52-40-01-1A-4; SRM 52-40-01-0I4. REMOVED CORRODED DOOR PER AMM 52-49-07-000-801. INSTALLED NEW LAV SERVICE PANEL; PERFORMED A GOOD BONDING RESISTANCE CHECK PER AMM 52-49-07-400-801.

Part: ISOLATOR — DAMAGED (L1 DOOR) · airframe 74,542 hrs · 43,942 cycles

FWD ENTRY DOOR SURROUND FWD UPPER MID COVE PANEL HAS DAMAGED ISOLATOR. / REMOVED AND REPLACED FED SURROUND UPPER MID COVE PANEL ISOLATOR PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. 59525U 11/21/20

Part: ATTACH ANGLE — CRACKED (BULKHEAD) · airframe 74,542 hrs · 43,942 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 7 WL 164. REPAIRED PER ARS ER 20-03606 REV IR AND SWA EA 20-157-02385 REV IR.

Part: PANEL — DAMAGED (L1 DOOR) · airframe 74,542 hrs · 43,942 cycles

FWD ENTRY DOOR SURROUND AFT UPPER MID COVE PANEL HAS DAMAGED ISOLATOR. / REMOVED AND REPLACED FED SURROUND AFT UPPER MID COVE PANEL ISOLATOR PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0. 59525U 11/21/20

Part: ISOLATOR — BROKEN (L1 DOOR) · airframe 74,542 hrs · 43,942 cycles

FWD ENTRY DOOR CUTOUT; FWD MID COVE PANEL HAS 2 BROKEN ISOLATORS. / REMOVED AND REPLACED FWD CUTOUT; FWD MID COVE PANEL 2 ISOLATORS PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. 59525U 11/21/20

Part: CREASE BEAM — CORRODED (RIGHT) · airframe 74,542 hrs · 43,942 cycles

CORROSION CREASE BEAM WEB RT BS 663-685 AT CENTER LIGHTNING HOLE INBOARD SIDE RBL 65 WL 208. REMOVED CORROSION ON CREASE BEAM WEB RT RBL 65, WL 208 STA 663-685 AT CENTER LIGHTNING HOLE INBOARD SIDE. MAX MATERIAL REMOVED ON WEB WAS .008' 1' X 2' FROM .040' OUT OF LIMITS. REMOVED DAMAGED WEB AND FABRICATED NEW WEB, PER CUSTOMER PO NR 808015-SWA, PER SRM 51-40-02-0G-0; SRM 53-40-13-1A-1; SRM 51-10-02-0G-0. APPLIED CHEMICAL CONV COATING AND PRIMED & INSTALLED PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SOPM 20-43-03; SRM 51-20-01-0G-0; DWG NR 144A5900.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 74,542 hrs · 43,942 cycles

CORROSION BS 259 FWD CHORD LBL 10- RBL 4 WL 208. REMOVED AND REPLACED BS 259 FWD CHORD LBL 32-RBL 32 WL 208, IAW BOEING DWGS 141A0631, 141A7430, 141A7434 AND SRM 51-40-02-0G-0.

Part: STRUCTURE — CORRODED (CABIN) · airframe 74,542 hrs · 43,942 cycles

CORROSION BS 259 AFT CHORD LBL 8-RBL 4 WL 208. DAMAGE REPAIRED, PER EA 20-153-02333 REV IR (ATS ER 20-03616 REV IR). REFER TO NRC U240471 FOR TRACKING.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 74,542 hrs · 43,942 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4 LBL 14 WL 207.54. DAMAGE REPAIRED, PER EA 1-A53-33179 REV 1 AND ER 20-03616 REV IR AND EA 20-153-02333 REV IR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,385 hrs · 43,840 cycles

R/H OVERWING EXIT EMERGENCY LIGHT INOP / RELAMPED PER AMM 33-51-04

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 74,067 hrs · 43,641 cycles

ESCAPE SLIDE MANUAL PULL HANDLE COVER NOT IN POSITION ON L1 DOOR; R1 DOOR; AND L2 DOOR. REPOSITIONED L1; R1 & L2 ESCAPE SLIDE HANDLE COVERS PER SIP

Part: COVER — OUT OF POSITION (L2 DOOR) · airframe 74,067 hrs · 43,641 cycles

ESCAPE SLIDE MANUAL PULL HANDLE COVER NOT IN POSITION ON L1 DOOR; R1 DOOR; AND L2 DOOR. / REPOSITIONED L1; R1 & L2 ESCAPE SLIDE HANDLE COVERS PER SIP

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 74,067 hrs · 43,641 cycles

ESCAPE SLIDE MANUAL PULL HANDLE COVER NOT IN POSITION ON L1 DOOR; R1 DOOR; AND L2 DOOR. / REPOSITIONED L1; R1 & L2 ESCAPE SLIDE HANDLE COVERS PER SIP.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 73,152 hrs · 43,068 cycles

RIGHT WING OUTBOAR AFT FLAP INBOARD CORNER SEPARATED 2 INCHES BY 1 INCH / ACCOMPLISHED PERMANENT REPAIR PER SRM 57-53-01-1A4

Part: FLAP — DELAMINATED (LT WING) · airframe 72,714 hrs · 42,798 cycles

LT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 72,714 hrs · 42,798 cycles

LT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 72,007 hrs · 42,335 cycles

DIVERSION-------------------------------------------------------------#1 ENGINE INDICATED 37% OIL QUANTITY AND DECREASING. OIL QUANTITY DOWN TO 19% ON FINAL APPROACH. #1 ENGINE OIL PRESSURE AND TEMPERATURE WERE NORMAL THROUGH LANDING AND #1 ENGINE SHUTDOWN. / FOUND OIL LEAK COMING FROM INTEGRATED DRIVE GENERATOR AND ENGINE DRIVEN HYDRAULIC PUMP OIL DRAINS. R&R INTEGRATED DRIVE GENERATOR AND ENGINE DRIVEN PUMP SEALOL SEAL IAW AMM

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 71,873 hrs · 42,238 cycles

L2 DOOR SLIDE GIRT OUT OF ADJUSTMENT. / ADJUSTED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 71,873 hrs · 42,238 cycles

R2 DOOR SLIDE GIRT OUT OF ADJUSTMENT. / ADJUSTED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,873 hrs · 42,238 cycles

R1 DOOR SLIDE GIRT OUT OF ADJUSTMENT. / ADJUSTED SLIDE PER MT

Part: STRUCTURE — SEPARATED (RT TE FLAP) · airframe 71,869 hrs · 42,234 cycles

R/H WING OUTBOARD AFT FLAP INBOARD CORNER SEPARATED. / REPAIRED AFT FLAP PER SRM.

Part: SUPPORT — CRACKED (LOWER EXT FUSELA) · airframe 71,869 hrs · 42,234 cycles

LOWER FUSELAGE KEEL BEAM PANEL 191F FORWARD LH SUPPORT CLIP CRACKED / R&R LOWER FUSELAGE KEEL BEAM PANEL 192F FORWARD LH SUPPORT CLIP PER SRM 51-40-02

Part: LENS — UNSECURE (EXIT SIGN) · airframe 70,929 hrs · 41,604 cycles

OVERWING EMERGENCY EXIT SIGN NOT SECURE. SECURED LENS IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 70,680 hrs · 41,438 cycles

R/H LIGHTING STRIP ON FLOOR BY LOOSE AT ROW 10. SECURED FLOOR TRACK LIGHTING STRIP PER M/M 33-51-12

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,619 hrs · 40,776 cycles

FORWARD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LAMP INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — DISLODGED (CABIN) · airframe 69,619 hrs · 40,776 cycles

PHOTO LUMINESCENT LIGHT STRIP DISLODGED AT ROW 10. SECURED STRIP PER AMM.

Part: CONTROL LEVER — CRACKED (COCKPIT) · airframe 69,615 hrs · 40,774 cycles

NR 1 ENGINE THRUST LEVER HAD A .25" CRACK AT THE NECK OF KNOB ATTACH POINT. REPAIRED LEVER PER EA.

Part: LIGHT — DISCONNECTED (EXIT SIGN) · airframe 69,470 hrs · 40,669 cycles

RT OVERWING EXIT AFT EMERGENCY EXIT SIGN INOP AT BS 651. RECONNECTED LIGHT IAW WDM & AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,470 hrs · 40,669 cycles

LT SIDE A/C SLIDE EMERGENCY LIGHT AFT OF WING INOP. R&R LIGHT IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

RT HORIZONTAL STABILIZER LEADING EDGE PANEL, 3RD RIB CRACKED INBOARD. R&R RIB IAW DWG AND SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

RT HORIZONTAL STABILIZER LEADING EDGE PANEL, 9TH RIB CRACKED INBOARD. R&R RIB IAW DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LH HORIZONTAL L/E HAS A CRACKED RIB # 1 INBOARD / REMOVED DAMAGED LH HORIZONTAL L/E #1 RIB AND INSTALLED NEW RIB PART # 186A1301-1 IAW BOEING DWG # 186A1001 ID: 0004 REV: A ATAG # RI0121

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LH HORIZONTAL L/E HAS CRACKED RIB #3 INBOARD / REMOVED DAMAGED LH HORIZONTAL L/E #3 RIB AND INSTALLED NEW RIB PART # 186A1303-1 IAW BOEING DWG # 186A1001 ID: 0004 REV: A ATAGT # WN8358

Part: RIB — CRACKED (RT WING) · airframe 69,470 hrs · 40,669 cycles

R/H WING FIXED L/E RIB AT STA KRAS 125.75 HORIZONTAL FLANGE CRACKED / CUTOUT CRACK ON R/H WING FIXED L/E RIB AT STA KRAS 125.75 HORIZONTAL FLANGE IAW B737-700 SRM 51-21-06. ACCOMPLISHED HFEC INSPS. IAW NDT PT6 51-00-00 P23; EA190008 P1 STEPS 4 & 5. NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR IAW EA 19008 IR AND EA 1-757-15827 REV IR.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

R/H HORIZONTAL STAB RIB AT STA 120 VERTICAL FLANGE CRACKED AT FWD SPAR / CUT OUT AND REMOVED DAMAGED SECTION OF R/H HORIZONTAL RIB AT STA 120 VERTICAL WEB AT FWD SPAR. ACCOMPLISHER HFEC OF CUTOUT AND OPEN HOLES NO DEFECT NOTED. FABRICATED REPAIR PARTS AND INSTALLED IA/W/ EA 1900005 REV 34 AND SW 1-755-4297 REV IR.

Part: HOOK — CORRODED (CABIN) · airframe 69,470 hrs · 40,669 cycles

RT EMERGENCY EXIT ESCAPE STRAP HOOK SURFACE CORRODED. R&R STRAP IAW AMM.

Part: HOOK — CORRODED (CABIN) · airframe 69,470 hrs · 40,669 cycles

LT EMERGENCY EXIT ESCAPE STRAP HOOK SURFACE CORRODED. R&R STRAP IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120, 4TH VERTICAL STIFFENER FROM FORWARD END. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 120, 4TH VERTICAL STIFFENER FROM FORWARD END. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LT HORIZONTAL RIB CRACKED AT STA 120. R&R WEB IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LT HORIZONTAL RIB CRACKED AT STA 120. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LT HORIZONTAL STABILIZER RIB STA 120, 3RD VERTICAL STIFFENER FORWARD END CRACKED. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LT HORIZONTAL STABILIZER RIB STA 120, RIB CRACKED AT 2ND, VERTICAL STIFFENER FROM FORWARD END. REPAIRED RIB PER SRM.

Part: ANGLE — CRACKED (WHEEL WELL LH) · airframe 69,470 hrs · 40,669 cycles

HORSE SHOE ATTACH ANGLE AFT SIDE OF STA 663 L/H VAPOR BARRIER WEB CRACKED / REMOVED AND REPLACED HORSE SHOE ATTACH ANGLE AFT SIDE OF STA 663 LH VAPOR BARRIER WEB IAW SRM 51-40-02-0G-0 AND 111A1000 REV.B RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802

Part: STIFFENER — CRACKED (ECS BAY LH) · airframe 69,470 hrs · 40,669 cycles

45 DEGREE ATTACH ANGLE FWD SIDE OF STA 663 L/H VAPOR BARRIER WEB CRACKED / P/N FOR 663 VAPOR BARRIER STIFFNERS 45 DEGREE 111A1301U5 IAW BOEING DWG 111A10001 REV F LOCATED AND DRILLED 45 DEGREE STIFFNER IAW BOEING DWG 111A1001 REV F; INSTALLED 45 DEGREE STIFFNER 663 VAPOR BARRIER IAW BOEING DWG 111A1001 REV F

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, 3RD VERTICAL STIFFENER FROM FORWARD END. REPAIRED RIB IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,470 hrs · 40,669 cycles

FLIGHT COMPARTMENT CAPTAIN FORWARD INBOARD SEAT TRACK CORRODED BOTTOM AND SIDES. R&R TRACK IAW W.I.C.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,470 hrs · 40,669 cycles

FLIGHT COMPARTMENT CAPTAIN FORWARD OUTBOARD SEAT TRACK CORRODED SIDES AND BOTTOM. R&R SEAT TRACK IAW WIC.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,470 hrs · 40,669 cycles

FLIGHT COMPARTMENT FIRST OFFICER FORWARD INBOARD SEAT TRACK CORRODED BOTTOM AND SIDES. R&R TRACK IAW W.I.C.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 69,470 hrs · 40,669 cycles

FLIGHT COMPARTMENT FIRST OFFICER FORWARD OUTBOARD SEAT TRACK CORRODED BOTTOM AND SIDES. R&R TRACK IAW W.I.C.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

STRINGER CLIP CRACKED AT BS 294, STR 13L. R&R CLIP IAW DWG & AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

FUSELAGE SKIN DENT AT BS 380+2, STR 17L. REPAIRED SKIN IAW EA & SRM.

Part: FITTING — CRACKED (LT WING) · airframe 69,470 hrs · 40,669 cycles

LT WING RIB 27 AFT SPAR TENSION FITTING CRACKED. REPAIRED FITTING PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

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

Part: FAIRING — CRACKED (LEFT WING) · airframe 69,470 hrs · 40,669 cycles

#2 FLAP TRACK FAIRING 543BB HAS 3/8 LONG CRACK AT LOWER RADIUS ON FWD MOUNTING BRACKET / REPLACED #2 FLAP TRACK FAIRING 543BB AND REMOVED FAILING LINKAGE FROM OLD 543BB AND INSTALLED ON NEW FAIRING. PER B737 AMM 27-51-28-000-804; AMM 27-51-28-400-804. ON NEW FAIRING. PER B737 AMM 27-51-28-000-804; AMM 27-51-28-400-804. REMOVED TAIL CONE FROM OLD FAIRING AND INSTALLED ON NEW FAIRING PER B737 AMM 27-51-28-000-804 AND AMM 27-51-28-400-804. INSTALLED FAIRING 543BB AND AJDUSTED ON GOOD NO JPANEL-540-CLOSE. ADJUSTMENT GOOD. POS 2 TAG / GRB NO. 137291 P/N OFF 113A9250-13 S/N OFF N50038 P/N ON 113A9250-13 S/N ON WN0104

Part: RETAINER — CRACKED (RIGHT WING) · airframe 69,470 hrs · 40,669 cycles

#6 FLAP TRACK FAIRING FORWARD OUTBOARD BULB SEAL RETAINER IS CRACKED / REMOVED AND REPLACED #6 FLAP TRACK FAIRING FWD OUTBOARD BULB SEAL RETAINER IAW B737 SRM 51-40-02-0G-0. ISSUE TAG # A73257

Part: PANEL — DELAMINATED (LT WING) · airframe 69,470 hrs · 40,669 cycles

NACELLE STRUT PANEL 431 ER HAS DELAM AT EDGE. MARKED. / REPAIRED DELAM AT EDGE OF NACELLE START PANEL 431ER I.A.W B737 SRM 54-50-70-2R-2 AND 51-70-04-2R-10. RESTORED FINISH I.A.W AMM 51-21-99-300-801

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 69,470 hrs · 40,669 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

INTERCOSTAL CORRODED AT BS 616+2, STR 5L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

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

Part: COVER — CRACKED (RT WING) · airframe 69,470 hrs · 40,669 cycles

R/H AILERON #1 & #4 OUTBD HINGE COVERS ARE CRACKED. / INSTALLED R/H AILERON #1 AND #4 O/B HINGE COVERS I/A/W B737 AMM 27-11-21-400-801 STEP 3E3(D) ATAGS - A71397 + A71422

Part: COVER — CRACKED (LT WING) · airframe 69,470 hrs · 40,669 cycles

L/H AILERON TAB #1 HINGE COVER CRACKED. / REPLACED L/H AILERON BALANCE TAB #1 HINGE COVERS IAW B737 AMM 27-11-21-400-801 STEP 3.E. (4) (D). A-TAG # A71407; A71411.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

INTERCOSTAL CORRODED AT BS 616+2, STR 5R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

SHEAR TIE CORRODED AT BS 667, BETWEEN RBL 63 TO RBL 70. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 69,470 hrs · 40,669 cycles

MID CABIN FLOOR HORIZONTAL BULKHEAD SHEAR TIE STIFFENER CORRODED AT BS 666, BETWEEN RBL 63 TO RBL 67. R&R STIFFENER IAW SRM & DWG.

Part: FAIRING — CRACKED (LT HORIZ STAB) · airframe 69,470 hrs · 40,669 cycles

LH HORIZ STAB TE PNL 333CB FAIRING STRIP HAS 10 CRACKS AT FASTENERS. / REMOVED AND REPLACED LH HORZ STAB TE PANEL 333CB FAIRING STRIP IAW SRM 51-40-02 AND DWG 185A1702-61 REV D. STRIP P/N: 185A1702-43; A73798 / 185A1702-43; ND1041 / 185A1702-43; A92240

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 69,470 hrs · 40,669 cycles

AFT CARGO COMPT; FLR PNL 140CF HAS CORROSION JUST FWD OF THRESHOLD. / VERIFIED AFT CARGO FLOOR PANEL 140CF ALLOWABLE DAMAGE LIMITS. CORROSION MAX LENGTH 3' INCHES FOUND CORROSION ON PANEL TUBE 10' INCHES OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-1 VERIFIED RECEIVED NEW FLOOR PANEL 140CF P/N 453A2610-2/7252490 A TAG # WN7678 IAW B737-700 DWG 453A2610.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,470 hrs · 40,669 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, RBL 40. REPAIRED WEB IAW EA.

Part: MODULE — FAULTY (CABIN PRESSURE) · airframe 69,171 hrs · 40,484 cycles

WHILE LEVEL FL390 CABIN ALT WARN HORN SOUNDED, PRESS MODE SELECTOR MOVED TO MANUAL AND OUTFLOW VALVE CLOSED CABIN RECOVERED. CABIN ALTITUDE INDICATED 10000' AT TIME OF EVENT. R&R CABIN PRESSURE CONTROL MODULE PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,302 hrs · 39,922 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,302 hrs · 39,922 cycles

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

Part: LENS — UNSECURE (EXIT SIGN) · airframe 68,302 hrs · 39,922 cycles

AFT GALLEY EXIT SIGN FELL OFF. SECURED LENS PER AMM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 68,222 hrs · 39,868 cycles

***CORROSION*** ON INTERNAL DOUBLER BELOW STR 28 L/H BS 362-380 / REMOVED CORROSION IN MULTIPLE AREAS ON INTERNAL DOUBLER BELOW STR 28 L/H AT BS 362 - 380 PER SRM 53-00-01-1A-5 AND EA 1-753-33016 REV. IR. LARGEST BLENDOUT MEASURES 1' X 14'; MAX DEPTH .005'. FOUND TO BE IN LIMITS PER EA 1-753-33016 REV IR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,222 hrs · 39,868 cycles

STRINGER CORRODED AT BS 373, STR 28L. REPAIRED STRINGER IAW EA & SRM.

Part: RETAINER — CRACKED (L/H VERTICAL STA) · airframe 68,220 hrs · 39,867 cycles

VERTICAL STAB. L/H PANEL #323CL;; RETAINER IS CRACKED / R&R VERTICAL STAB. L/H PANEL #323CL;; RETAINER PER SRM 51-40-02

Part: RETAINER — CRACKED (R/H VERTICAL STA) · airframe 68,220 hrs · 39,867 cycles

VERTICAL STAB. R/H PANEL #323CR; RETAINER IS CRACKED / R&R VERTICAL STAB. R/H PANEL #323CR; RETAINER REF SRM 51-40-02.

Part: CHANNEL — CRACKED (R/H VERTICAL STA) · airframe 68,220 hrs · 39,867 cycles

VERTICAL STAB. R/H PANEL #323CR; VERTICAL CHANNEL IS CRACKED / R&R VERTICAL STAB. R/H PANEL #323CR; VERTICAL CHANNEL PER SRM 51-40-02

Part: PANEL — CRACKED (L/H VERTICAL STA) · airframe 68,220 hrs · 39,867 cycles

VERTICAL STAB. L/H SIDE; PANEL #324AL RETAINER IS CRACKED / R&R VERTICAL STAB. L/H SIDE; PANEL #324AL RETAINER PER SRM 51-40-02

Part: RETAINER — CRACKED (R/H VERTICAL STA) · airframe 68,220 hrs · 39,867 cycles

VERTICAL STAB. R/H SIDE; PANEL #324AR RETAINER IS CRACKED / R&R VERTICAL STAB. R/H SIDE; PANEL #324AR RETAINER REF SRM 51-40-02.

Part: ACTUATOR — LEAKING (RT WING SPOILER) · airframe 67,170 hrs · 39,159 cycles

RIGHT WING NR 8 FLIGHT SPOILER ACTUATOR LEAKING. R & R THE NR 8 FLIGHT SPOILER ACTUATOR IAW AMM.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 66,686 hrs · 38,866 cycles

RIGHT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE HAS A SMALL AREA OF DELAM / REPAIRED DELAM OF RIGHT OUTBD AFT FLAP INBOARD TRAILING EDGE IAW B737 SRM 51-70-10-2R-1 AND SRM 51-70-10-2R-0 AND SRM 57-53-01-2R-4

Part: BRACKET — CRACKED (LT WING) · airframe 66,258 hrs · 38,594 cycles

LEFT WING UPPER FIXED TRAILING EDGE PANEL (AFT OF ENGINE PYLON) FWD. SEAL BRACKET CRACKED / REMOVED AND REPLACED LEFT WING UPPER FIXED TRAILING EDGE PANEL (AFT OF ENGINE PYLON) FWD. SEAL BRACKET PER SRM 51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 66,258 hrs · 38,594 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M01670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,258 hrs · 38,594 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M01672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,258 hrs · 38,594 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PER AMM.

Part: PLATE — CRACKED (LT WING) · airframe 66,258 hrs · 38,594 cycles

LT WING LOWER FIXED TRAILING EDGE PANEL AFT OF ENGINE PYLON WIGGLE PLATE CRACKED. R&R WIGGLE PLATE PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,587 hrs · 38,157 cycles

RT INTERIOR EMERGENCY OVERWING EXIT SIGN INOP. RELAMPED SIGN IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,297 hrs · 37,966 cycles

CABIN AISLE EMERGENCY LIGHT LENS MISSING. INSTALLED THE LENS IAW MM.

Part: SPACER — MISSING (GIRT BAR) · airframe 63,442 hrs · 36,858 cycles

R1 DOOR SLIDE GIRT BAR NYLON SPACER MISSING. R & R THE SLIDE ASSEMBLY IAW MT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,005 hrs · 36,586 cycles

RIGHT OVERWING EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK ASSY IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,005 hrs · 36,586 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK ASSY IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R INTERCOSTAL IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

R1 DOOR CREASE BEAM WEB CORRODED BETWEEN BS 334 TO BS 348. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

CREASE BEAM CRACKED AT BS 303, STR 17L. R&R CREASE BEAM IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,005 hrs · 36,586 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE INTERCOSTAL CORRODED AT BS 956, RBL 27. R&R INTERCOSTAL IAW DWG & AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE CREASE BEAM INNER CHORD CORRODED BETWEEN BS 907 TO BS 998, BETWEEN RBL 47 TO RBL 55. R&R BEAM IAW DWG AND SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

R1 DOOR FORWARD STUB BEAM CRACKED AT BS 295.5. R&R STUB BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

CREASE BEAM CORRODED BETWEEN BS 344 TO BS 360, STR 17L. R&R CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE LT SIDE CREASE BEAM INNER CHORD CORRODED BETWEEN BS 907 TO BS 998, BETWEEN LBL 55 TO LBL 47. R&R CHORD IAW DWG AND SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE FLOOR WEB CORRODED BETWEEN BS 987 TO BS 1016, BETWEEN RBL 34 TO RBL 45. R&R WEB IAW DWG & AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 460, BL 0. R&R INTERCOSTAL IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE FLOOR STRUCTURE WEB CORRODED BETWEEN BS 1016 TO BS 1030, BETWEEN BL 0 TO LBL 37. R&R WEB IAW DWG AND SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE FLOOR STRUCTURE STRAP CORRODED BETWEEN BS. 1006 TO BS. 1029, BETWEEN LBL 2 TO LBL 5. R&R STRAP IAW DWG AND SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

CREASE BEAM ATTACH ANGLE CRACKED AT BS 295.5, STR 17R. R&R ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE FLOOR WEB CORRODED BETWEEN BS 987 TO BS 1016, BETWEEN LBL 34 TO LBL 45. R&R WEB IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

FORWARD PASSENGER CABIN L1 DOOR THRESHOLD WEB CORRODED. R&R ZEE ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT WET AREA FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 7.5 TO LBL 45. REPAIRED T-CAP IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO FLOOR T CHORD SPLICE CORRODED AT BS 887. R&R SPLICE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO RT Z ANGLE CORRODED BETWEEN BS 727E TO BS 767+8, RBL 22. REPAIRED Z ANGLE PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO, FLOOR SUPPORT CHANNEL CORRODED AT BS 767+5, LBL 12.5. REPAIRED CHANNEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO FRAME CORRODED AT BS 787, RBL 18. REPAIRED FRAME IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO FLOOR RAIL SUPPORT CHANNEL CORRODED BETWEEN BS 727 TO BS 727C, LBL 17. R&R SUPPORT IAW SRM & DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,005 hrs · 36,586 cycles

RT WING OUTBOARD FLAP LOWER INBOARD CORNER DELAMINATED. REPAIRED FLAP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 767+5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO, RT Z ANGLE CORRODED BETWEEN BS 727 TO BS 727, RBL 22. R&R Z ANGLE IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO COMPARTMENT SUPPORT BRACKET CRACKED AT BS 867, BETWEEN STR 26L TO STR 27L. R&R BRACKET IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO LT Z ANGLE CORRODED BETWEEN BS 727 TO BS 807, LBL 22. R&R Z ANGLE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 767+5, LBL 3" UPPER AND LOWER SIDE. R&R CHANNEL IAW EA.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

AFT CARGO, FLOOR SUPPORT CHANNEL CORRODED AT BS 767+5, RBL 14. R&R SUPPORT IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,005 hrs · 36,586 cycles

SKIN CORRODED AT BS 500A+12, BL0. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,005 hrs · 36,586 cycles

RT WING NR 6 SLAT LOWER SKIN CRACKED AT FASTENER COUNTERSINK BELOW ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,491 hrs · 36,257 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED AT LOWER INBOARD CORNER. REPAIRED THE FLAP IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R &R THE BATTERY PACK IAW AMM.

Part: HOOK AND LOOP — WORN (EMERGENCY EXIT) · airframe 62,491 hrs · 36,257 cycles

LEFT EMERGENCY EXIT RED PULL STRAP COVER HOOK AND LOOP WORN. R & R THE STRAP ASSEMBLY IAW SIP.

Part: STRAP — WORN (EMERGENCY EXIT) · airframe 62,491 hrs · 36,257 cycles

RT EMERGENCY EXIT RED PULL STRAP COVER HOOK AND LOOP WORN. R & R THE STRAP ASSEMBLY IAW SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,491 hrs · 36,257 cycles

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

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 62,491 hrs · 36,257 cycles

FORWARD GALLEY EXIT SIGN COVER NEAR R1 DOOR FELL OFF. INSTALLED COVER IAW SIP.

Part: LIGHT — WORN (CABIN) · airframe 61,340 hrs · 35,580 cycles

LEFT FWD EMERGENCY LIGHT STRIP WORN. R & R EMERGENCY LIGHT IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 60,254 hrs · 34,958 cycles

R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 59,587 hrs · 34,573 cycles

MID CABIN CEILING EMER LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,301 hrs · 33,822 cycles

L1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,101 hrs · 33,719 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,101 hrs · 33,719 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1675. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,101 hrs · 33,719 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,101 hrs · 33,719 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,447 hrs · 33,341 cycles

R1 DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,238 hrs · 33,222 cycles

RIGHT AFT LOWER EXTERNAL EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 57,105 hrs · 33,142 cycles

L1 DOOR EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 57,069 hrs · 33,124 cycles

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

Part: LENS — MISSING (CABIN) · airframe 58,016 hrs · 33,679 cycles

EXIT LIGHT LENS MISSING AT ROW 11 DEF. R & R LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 56,933 hrs · 33,042 cycles

RIGHT EGRESS BULLNOSE LIGHT LENS MISSING AT ROW 11. R & R LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 56,933 hrs · 33,042 cycles

RIGHT EMER BULLNOSE LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,658 hrs · 32,890 cycles

LEFT INBD SEAT TRACK CORRODED AT BS 400. R & R SEAT TRACK FROM IAW DWG & SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 56,658 hrs · 32,890 cycles

RIGHT WING SUPPORT CLIP JUST UNDER WING TO BODY FAIRING 195CR CRACKED. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,658 hrs · 32,890 cycles

CENTER WING BOX FRONT SPAR SHEAR FITTING CRACKED AT BS 540, LBL 6. R & R FITTING IAW DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,658 hrs · 32,890 cycles

AFT CARGO COMPARTMENT STATION 796 TO 844, DOOR THRESHOLD WEB CORRODED. REPAIRED WEB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,658 hrs · 32,890 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,658 hrs · 32,890 cycles

FLOOR SUPPORT ANGLE INBD OF THRESHOLD WEB CORRODED BETWEEN BS 796 TO 844. R & R ANGLE IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,658 hrs · 32,890 cycles

FORWARD CARGO SCUFF PLATE SILL WEB CORRODED BETWEEN BS 450 TO 495. R & R WEB IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,658 hrs · 32,890 cycles

MAIN LANDING GEAR WW UPPER PRESS WEB, BS 663, RBL 42 CRACKED. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (LE SLAT) · airframe 56,658 hrs · 32,890 cycles

RIGHT WING NR 7 SLAT ACTUATOR TO SLAT ATTACH FITTING CRACKED AT OTBD MOST AFT RIVET. REPAIRED FITTING IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,658 hrs · 32,890 cycles

LEFT WING NR 3 LE SLAT LOWER SURFACE CRACKED AT OTBD ACTUATOR CUT OUT. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,658 hrs · 32,890 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT LOWER SURFACE AT ACTUATOR FITTING. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,658 hrs · 32,890 cycles

RIGHT WING NR 8 SLAT SKIN ACTUATOR TO SLAT ATTACH FITTING CRACKED AT INBD MOST AFT RIVET. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,658 hrs · 32,890 cycles

LEFT WING NR 2 LE SLAT LOWER SURFACE CRACKED AT OTBD ACTUATOR CUT OUT. REPAIRED SLAT IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 56,585 hrs · 32,850 cycles

RIGHT OVERHEAD BIN EMER EXIT LIGHT LENS COVER LOOSE AT ROW 11. SECURED COVER IAW MM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 56,482 hrs · 32,800 cycles

R1 DOOR EMER EXIT SIGN ARROW OUT OF POSITION. REPOSITIONED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,190 hrs · 32,635 cycles

LEFT OVERWING EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,190 hrs · 32,635 cycles

FWD CABIN LT EMER BATTERY PACK FAILED TIME CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,190 hrs · 32,635 cycles

MID CABIN RT EMER BATTERY PACK FAILED TIME CHECK. R & R BATTERY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,190 hrs · 32,635 cycles

AFT CABIN LT EMER BATTERY PACK FAILED TIME CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,190 hrs · 32,635 cycles

AFT CABIN RT EMER BATTERY PACK FAILED TIME CHECK. R & R BATTERY IAW MM.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 55,947 hrs · 32,488 cycles

NUMBER 2 ENG COMPRESSOR STALL AT FL 410 IN CRUISE. R & R NR 2 ENG HYDRO MECHANICAL UNIT IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 55,572 hrs · 32,257 cycles

LEFT EMER EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,399 hrs · 32,161 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,399 hrs · 32,161 cycles

SKIN CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,399 hrs · 32,161 cycles

FUSELAGE SKIN CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED SKIN IAW EA.

Part: COVER — MISSING (CABIN) · airframe 55,252 hrs · 32,074 cycles

LEFT AFT DOOR EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW AMM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 54,521 hrs · 31,674 cycles

R1 DOOR SLIDE GIRT BAR BRACKET LOOSE. R & R BRACKET ASSEMBLY IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

LT NR 1 WINDOW FRAME CRACKED AT EXISTING FASTENER HOLE. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

RT NR 1 COCKPIT WINDOW FRAME CRACKED IN UPPER OTBD CORNER AT WINDOW CUTOUT. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

FRAME WEB CRACKED AT STATION 259.5, STRINGER 9L. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

SET TRACK CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 45.5. R & R SEAT TRACK IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

FS FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

FS FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 52,752 hrs · 30,671 cycles

NR 4 GALLEY EMERGENCY EXIT SIGN NEAR DOOR LOOSE ON THE GALLEY WALL. SECURED SIGN IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 52,752 hrs · 30,671 cycles

RT HORIZONTAL STABILIZER, STAB STATION 129.50 RIB CRACKED ON THE LOWER FLANGE AT 14.5", 20", 24.5", 26.5", 27.5" & 29.75" AFT OF THE FRONT SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,752 hrs · 30,671 cycles

LT NR 3 WINDOW, E-F POST, 2ND & 3RD HOLES FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: BRACKET — CRACKED (NR 2 NACELLE) · airframe 51,911 hrs · 30,164 cycles

NR 2 ENGINE AFT RT STRUT BRACKET CRACKED HYDRAULIC LINE STAND OFF. REPAIRED BRACKET IAW EA.

Part: HINGE — CRACKED (LT MLG DOOR) · airframe 51,911 hrs · 30,164 cycles

LT MLG INNER DOOR AFT HINGE CRACKED. R&R LT MLG INNER DOOR IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 51,549 hrs · 29,944 cycles

RIGHT FWD EEPLS COVER BROKEN. R & R LIGHT ASSY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 51,002 hrs · 29,630 cycles

LENS COVER ON EMERGENCY EXIT LIGHT ON OVERHEAD BIN ROW 11 MISSING. INSTALLED LENS PER MM.

Part: LENS — UNSECURE (CABIN) · airframe 50,581 hrs · 29,378 cycles

AFT SERVICE DOOR EMERGENCY LIGHT LENS NOT SECURE. SECURED LENS IAW MM.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 49,973 hrs · 29,008 cycles

RIGHT ELEVATOR LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EVAC SLIDE) · airframe 48,472 hrs · 28,097 cycles

L1 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER AMM.

Part: LENS — LOOSE (EVAC SLIDE) · airframe 48,472 hrs · 28,097 cycles

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

Part: HOOK — LOOSE (L1 DOOR) · airframe 48,472 hrs · 28,097 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR HOOK LOOSE. SECURED HOOK ASSY PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 48,472 hrs · 28,097 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR HOOKS LOOSE. SECURED HOOK ASSY PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,793 hrs · 27,712 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 47,218 hrs · 27,376 cycles

L1 DOOR SKIN CRACKED UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: COVER — MISSING (CABIN) · airframe 47,176 hrs · 27,356 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 47,176 hrs · 27,356 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 46,134 hrs · 26,757 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,969 hrs · 26,056 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,969 hrs · 26,056 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,100 hrs · 25,544 cycles

DURING SCHEDULED 12Y CHECK, FOUND CRACK LT STA 727 FRAME, AFT SIDE OF WEB. REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,100 hrs · 25,544 cycles

DURING SCHEDULED 12Y CHECK, FOUND LEFT OVERWING EXIT SIDEWALL LIGHT DOES NOT ILLUMINATE. REMOVED AND INSTALLED OVERWING EMERGENCY EXIT LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,101 hrs · 25,544 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 44,101 hrs · 25,544 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN BASE BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM Z-ANGLE CORRODED BETWEEN BS 291.5 TO BS 348. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,101 hrs · 25,544 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,044 hrs · 32,545 cycles

FRAME ANGLE CRACKED AT BS 727 WL 201. REPAIRED FRAME IAW EA.

Part: LENS — MISSING (CABIN) · airframe 41,269 hrs · 23,910 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 3. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,975 hrs · 23,144 cycles

RT EEPLS LOOSE AT ROW 18. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — FADED (EMERGENCY LIGHT) · airframe 39,460 hrs · 22,852 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — FADED (EMERGENCY LIGHT) · airframe 39,460 hrs · 22,852 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,708 hrs · 21,770 cycles

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

Part: RIB — CRACKED (HORIZ STAB) · airframe 37,572 hrs · 21,687 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED AT STA 138. REPAIRED RIB PER EA.

Part: RIB — CRACKED (HORIZ STAB) · airframe 37,572 hrs · 21,687 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED AT SAT 138.7. REPAIRED PER AAR EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,572 hrs · 21,687 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT LOWER OVERWING EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM

Part: FITTING — CORRODED (RT MLG) · airframe 35,563 hrs · 20,511 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT MLG) · airframe 35,563 hrs · 20,511 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 31,266 hrs · 17,911 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,621 hrs · 17,535 cycles

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

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,267 hrs · 17,337 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,267 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 43 AND LBL 43. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,267 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 773, BETWEEN LBL 12 AND RBL 12. REMOVED AND REPLACED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,267 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED BETWEEN BS 793 AND BS 847, RBL 14. REMOVED AND REPLACED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,267 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,267 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 773, LBL 17. REPAIRED FLOORBEAM PER SWA EA.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 27,603 hrs · 15,844 cycles

EEPLS LIGHT COVER LOOSE AT ROW 7 DEF. SECURED LIGHT COVER PER MM.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 26,344 hrs · 15,103 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 1 ENGINE HPC 6TH STAGE BLADE WITH MISSING MATERIAL ON THE L/E IN DIMENSION -B- AREA OF THE AIRFOIL THAT MEASURES 058 INCH DEEP. REMOVED AND REPLACED NR 1 ENGINE PER SWA MT.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 26,335 hrs · 15,099 cycles

DURING SCHEDULED HC2 CHECK, ALL EMERGENCY EXIT LIGHT BATTERY PACKS FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACKS PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 26,335 hrs · 15,099 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 26,215 hrs · 15,036 cycles

EEPLS COVER LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 23,389 hrs · 13,457 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 21,974 hrs · 12,657 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,861 hrs · 12,009 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,802 hrs · 10,877 cycles

DURING SCHEDULED 5Y CHECK, FOUND EMERGENCY EXIT LIGHTS AT R1 AND L1 DOORS INOP. REMOVED AND REPLACED R1 AND L1 EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: ATTACH FITTING — LOOSE (ENTRY DOOR) · airframe 16,561 hrs · 9,642 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACHMENT FITTING LOOSE. SECURED ATTACHMENT FITTING PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,769 hrs · 8,616 cycles

EEPLS COVER MISSING IN AFT CABIN. INSTALLED EEPLS COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,061 hrs · 7,626 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW 4. REMOVED AND REPLACED COVER PER MM.

Part: FLAP — CRACKED (LT WING) · airframe 11,851 hrs · 6,943 cycles

DURING SCHEDULED PM CHECK, FOUND LT INBD T/E AFT FLAP CRACKED ON LOWER SURFACE. REPAIRED LT INBD T/E AFT FLAP PER SWA RA.

Part: BEARING — WORN (LT ELEVATOR) · airframe 11,558 hrs · 6,792 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LH ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR NR 2, 3 AND 4 TAB HINGE BEARINGS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 9,484 hrs · 5,660 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 1, 2 ,3, 5, 6, 16, AND 17. REMOVED AND REPLACED COVERS PER MM.

Part: FASTENER — LOOSE (ENTRY DOOR) · airframe 9,131 hrs · 5,466 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK HAS LOOSE FASTENER. REMOVED AND REPLACED GIRT BAR FASTENER PER SRM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 8,890 hrs · 5,308 cycles

DURING SCHEDULED RON SI # 11038-55, FOUND RH ELEVATOR TAB BUSHINGS WORN AT # 1 & # 4 HINGES. R&R BUSHINGS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 7,346 hrs · 4,348 cycles

DURING SCHEDULED SERVICE CHECK , SWA SI 11038-55, FOUND BOTH LT & RT ELEVATOR, NR 3 & NR 4 TAB HINGE BUSHINGS WORN. R&R BUSHINGS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,962 hrs · 4,148 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 5,557 hrs · 3,322 cycles

EEPLS COVER MISSING. REPLACED EEPLS COVER PER MM.

Part: INDICATOR — OUT OF POSITION (DOOR SLIDE) · airframe 4,967 hrs · 2,971 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR SLIDE INDICATOR OUT OF POSITION. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,967 hrs · 2,971 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED LAMP PER MM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 4,967 hrs · 2,971 cycles

DURING SCHEDULED C1 CHECK, FOUND CREASE IN AFT CARGO DOOR 2.5 LONG. REPAIRED DOOR SKIN PER SRM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT DURING DOOR OPENING. (DID NOT DEPLOYED). REMOVED AND REPLACED SLIDE ASSY PER MM.