N776WN

Part: BRACKET — LOOSE (R1 DOOR) · airframe 71,012 hrs · 42,066 cycles

FWD GALLEY GIRT BAR BRACKET LOOSE / [01] ADJUSTED GIRT BAR BRACKET PER SIP

Part: NONE — INOPERATIVE (L1 DOOR) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: CUSTOMER WALK - EMERGENCY EXIT LIGHT ABOVE L1 DOOR HAS SEVERAL BULBS INOP ; / [01] RELAMPED SEVERAL BULBS ABOVE L1 DOOR EMERGENCY EXIT LIGHT AS PER REF B737 AMM 33-51-01-960-801. TEST OK.; [02] VERIFIED STEP1.

Part: NONE — INOPERATIVE (OVERWING EXIT) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: R/H PASSENGER CABIN OVER-WING DOOR EMERGENCY LIGHT AFT POSITION INOP. ; / [01] RELAMPED R/H PASSENGER CABIN OVER-WING DOOR EMERGENCY EXIT SIGN LIGHT AFT POSITION; OPS CHECK NORMAL REF B737 AMM 33-51-01-960-801; [02] VERIFIED STEP 1

Part: NONE — CRACKED (R2 DOOR) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: R-2 DOOR EXIT LIGHT LENS CRACKED. ; / [01] REPLACED R-2 EXIT DOOR LIGHT ASSY PER B737 AMM 33-51-02-801 OPS CHECK NORMAL.<BR><BR>AAR TAG JV1164 P/N 702409-1007; [02] VERIFIED STEP 1

Part: NONE — INOPERATIVE · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY LIGHT ROW # R/H INOP. ; EMERGENCY LIGHT ROW #3 RH INOP. / [01] RELAMPED #3 RH EMERGENCY LIGHT AS PER REF B737 AMM 33-51-03-960-801 PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER REF B737 AMM 33-51-00-710-801 FOUND NORMAL; [02] VERIFIED STEP 1

Part: NONE — INOPERATIVE · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LT DOOR R1 INOP. / [01] RELAMPED R1 DOOR EMERGENCY LIGHT BULB AS PER REF B737 AMM 33-51-01-960-801 PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST FOUND NORMAL; [02] VERIFIED STEP 1

Part: NONE — CRACKED (OVERWING EXIT) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: R/H OVER WING EMERGENCY EXIT LIGHT LENS CRACKED. ; / [01] REMOVED AND REPLACED R/H OVER WING EMERGENCY EXIT LIGHT LENS IN REF. B737-700 AMM 33-51-01-960-801; [02] VERIFIED

Part: SCUFF PLATE — CRACKED · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO DOOR SCUFF PLATE FWD CORNER CRACK AT EDGE ; / [01] RECEIVE NEW PART 654A0004-337; PO# 1728471. THIS PART WILL BE INSTALL ON TASK CARD TTG8Q0030AYF.AS PER REF SRM 51-10-02-0G-0; [02] PART WILL BE INSTALLED ON TASK CARD TTG8Q0030AYF.

Part: BAFFLE — DAMAGED (FWD CARGO BAY) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO FLOOR SUPPORT STRUCTURE BAFFLE DAMAGE BETWEEN STA 500 AND STA 500A L/H STRG 25 ; / [01] REMOVED AND REPLACED BAFFLE AT FWD CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE BETWEEN STA 500 AND STA 500A AS PER B-737-700 SRM 51-40-02-OG-0; [02] VERIFIED STEP1

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO FLOOR STRUCTURE BAFFLE BETWEEN STA500B AND STA 500C APROX STR25L CRACKED AT AFT UPPER CORNER ATTACHING AREA ; / [01] REMOVED AND REPLACED BAFFLE AT FWD CARGO COMPARTMENT FLOOR STRUCTURE BETWEEN STA 500B AND STA 500C APROX STR 25L AS PER B-737-700 SRM 51-40-02-OG-0; [02] VERIFIED STEP 1

Part: FRAME — CRACKED (FWD GALLEY) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: FOUND FRAME CRACKED AT GALLEY DOOR PANEL CUT OUT ; / [01] REMOVED FRAME AT GALLEY DOOR PANEL CUT OUT. <BR>REF. B737-7 SRM-51-40-02-0G-0.; [02] RECEIVED NEW FRAME P.O.#1728471. LOCATED IT AND DRILLED. AS PER B-737-7 SRM-51-40-05-0G.; [03] OK TO INSTALL NEW FRAME AT GALLEY DOOR; [04] INSTALLED NEW FRAME AT GALLEY DOOR UP TO 95%. REF. B737-7 SRM-51-40-02-0G-0; [05] COMPLETED NEW FRAME INSTALLATION AT FWD GALLEY DOOR AS PER SRM 51-40-02-0G-0; [06] C/W; [07] VERIFIED STEP 5 AND 6

Part: ANGLE — CRACKED (KEEL BEAM) · airframe 68,765 hrs · 40,619 cycles

SMALL ANGLE CRACKED AT AFT KEEL BEAM LOWER BS 727 AND LBL 21. CRACK CONFIRMED IAW NDTM PART 6 ;51-00-00 PROCEDURE 23. CRACK LENGTH: 0.669'. REMOVED SMALL ANGLE AT AFT KEEL BEAM IAW SRM 51-40-02-OG-0. FABRICATEA NEW ANGLE IAW DWG 149A7692. LOCATED AND DRILLED THE NEW ANGLE IAW SRM 51-10-02-0G-0. TREATED AND PRIMED IAW AMM-51-21-72-370-801. ACCOMPLISHED ANGLE INSTALLATION AT AFT KEEL BEAM LOWER STA. 727 AND LBL21 IAW DWG 149A7692 AND BAC 5602.

Part: STIFFENER — CRACKED (WHEEL WELL) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: STIFFENER CRACKED @ WHEEL WELL FWD VERTICAL BULKHEAD LOWER AT STA 663.75 RBL 25 MKD DOT ; / [01] CRACK CONFIRMED IAW NDTM PART 6 ;51-00-00 PROCEDURE 23. CRACK LENGTH: 1.496'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE-10/22]; [02] REMOVED FAIRING PANEL #193AR LWR. CENTER AREA FOR ACCESS AREA WORK; AS PER SRM. 51-40-01-0G-0-A00767.; [03] VERIFIED STEP 2; [04] REMOVED DAMAGE STIFFENER AT WHEEL WELL STA 663.75 IN REF SRM 51-40-02; [05] VERIFIED STEP 4; [06] RECIVED; LOCATED AND DRILL HOLES IN NEW STIFFENER AS PER SRM. 51-20-07-0G-0.; [07] VERIFIED STEP 6; [08] OK TO INSTALL NEW STIFFENER AT W/W STA663.75; [09] INSTALLED NEW STIFFENER AT WHEEL WELL STA 663.75IN REF SRM 51-40-02; [10] VERIFIED STEP 9<BR>OK TO INSTALL FAIRING PANEL 193AR; [11] INSTALLED WING TO BODY FAIRING 193AR AS PER AMM 53-51-21-400-802; [12] VERIFIED STEP 11

Part: FLOOR PANEL — CORRODED (FLIGHT DECK) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: CORROSION ** FLIGHT DECK ENTRY FLOOR ACCESS PANEL 211AF LOWER SKIN SURFACE ; / [01] REMOVED CORROSION AT FLOOR ACCESS PANEL #211AF LOWER SKIN. ORIGINAL MATERIAL .050' REMOVED .007' MAT. REMAINING .043' FOUND OUT OFF LIMITS AS PER SRM. 53-10-51-1A-1-A00060. USED TOOL MICROMETER B/C 17784 DUE: 18-MAY-22.; [02] RECEIVED NEW PANEL P.NO. 141A5133U 15. PANEL WILL BE INSTALL TASK CARD TTG8Q006JDQ0.; [03] C/W; [04] VERIFIED STEPS 1; 2 AND 3

Part: SLAT — CRACKED (RH WING) · airframe 68,765 hrs · 40,619 cycles

RIGHT WING MOVEABLE L/E SLAT NR 5 NOSE SKIN, ACTUATOR RIB APPEAR SMALL CRACK AND FASTENERS HEADS PULLED. FABRICATED AND LOCATED NEW FASTENER HOLES AT REPAIR DOUBLER IAW SRM 57-42-01-2R-8. CUT OUT DAMAGED AREA IAW SRM 57-42-01-2R-8. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. FABRICATED AND LOCATED NEW FASTENER HOLES AT REPAIR FILLER IAW SRM 57-42-01-2R-8. TREATED AND PRIMED REPAIR AND AREAS IAW SOPM 20-41-02. INSTALLED REPAIR DOUBLR, FILLER, AND REPAIR WASHERS IAW SRM 57-42-01-2R-8.

Part: BEAR STRAP — CRACKED (R1 DOOR) · airframe 68,765 hrs · 40,619 cycles

CRACK FOUND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT THE R1 DOOR BEAR STRAP BETWEEN BS 291.5 & 294.5, S8-9R. LENGTH OF CRACK 1.339'. PERFORMED CUT OUT AT BEARSTRAP IAW SRM 53-10-01-2R-6, REPAIR 6. STEP 4-C. FABRICATED REPAIR IAW SRM 53-10-01-2R-6, REPAIR-6, PROCEDURE 4, STEP E-1. TABLE 201. INSTALLED COUNTERSINK REPAIR WASHERS. COMPLETED INSTALATION OF DOUBLER AND TRIPLER IAW SRM 53-10-01-2R-6 REPAIR 6.

Part: FITTING — CRACKED (LH WING) · airframe 68,765 hrs · 40,619 cycles

SUPPLEMENTAL INFORMATION: L/W REAR SPAR FIXED T/E DEFLECTION CONTROL PANEL VERTICAL SEAL FITTING CRACKED I/B SIDE MKD DOT ; / [01] REMOVED AND REPLACED VERTICAL SEAL FITTING; AT L/W REAR SPAR FIXED T/E DEFLECTION; CONTROL PANEL; PER B737-700 SRM 51-40-02-OG-0; [02] VERIFIED STEP 1

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,260 hrs · 40,298 cycles

RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE RT AFT POWER SUPPLY IAW AMM 33-51-06, OPS CHECKED NORMAL.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,172 hrs · 39,576 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG CORRODED ON INNER FACE. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,172 hrs · 39,576 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION LOWER OUTBOARD LUG CORRODED ON OUTER FACE. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG BORE CORRODED. REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG INNER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,172 hrs · 39,576 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG CORRODED ON OUTER FACE. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,172 hrs · 39,576 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INNER FACE CORRODED. / REPAIRED LUG BORE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,172 hrs · 39,576 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG CORRODED ON OUTER FACE. / REPAIRED LUG PER EA.

Part: RIB — CRACKED (LH MLG) · airframe 67,172 hrs · 39,576 cycles

LT MLG STRUT DOOR CRACKED THROUGH RIB FWD OF LOWER FWD MOUNT / REMOVED AND REPLACED L/H MLG STRUT DOOR PER W.I. 732-11-01 POS 1 PN OFF/ON 113A8200-5 SN OFF WN776 PN ON 113A8200Y9 SN ON WN0862

Part: RETAINER — CRACKED (LEFT WING) · airframe 65,916 hrs · 38,799 cycles

LEFT WING UPPER FIXED TRAILING EDGE PANEL SEAL SUPPORT FORWARD RETAINER CRACKED / R&R'D LEFT WING UPPER FIXED TRAILING EDGE PANEL SEAL SUPPORT FORWARD RETAINER REFERENCE SRM 51-40-02

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01672. R&R BATTERY PACK PER AMM & DWG.

Part: RETAINER — CRACKED (LEFT WING) · airframe 65,916 hrs · 38,799 cycles

LEFT WING UPPER FIXED TRAILING PANEL SEAL SUPPORT AFT RETAINER CRACKED AT FASTENER HOLES / R&R'D LEFT WING UPPER FIXED TRAILING PANEL SEAL SUPPORT AFT RETAINER REF SRM 51-40-02

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01674. R&R BATTERY PACK PER AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PACK PER AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01669. R&R BATTERY PACK PER AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,916 hrs · 38,799 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01668. R&R BATTERY PACK PER AMM & DWG.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 64,046 hrs · 37,626 cycles

R1 DOOR GIRT BAR HOLDER LOOSE. ADJUSTED LATCHES PER AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 63,127 hrs · 37,018 cycles

LT EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT ASSEMBLY PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

WEB CORRODED AT BS 808, RBL 65. R&R WEB PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 18R TO STR 13R. R&R FRAME IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

WEB CORRODED AT BS 828, RBL 65. R&R WEB PER SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

CLIP CORRODED AT BS 817.55, RBL 65. R&R CLIP PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

ANGLE CORRODED AT BS 808, RBL 65. R&R ANGLE PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

WEB CORRODED AT BS 830, RBL 65. R&R WEB PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FRAME CORRODED AT BS 827, RT AT WL 200 TO 205. REPAIRED FRAME IAW SRM AND DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 62,841 hrs · 36,825 cycles

RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IS CRACKED / REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL PER MM 53-31-31-000-802 AND 53-31-31-400-802

Part: STABILIZER — DELAMINATED (HORIZONTAL STAB) · airframe 62,841 hrs · 36,825 cycles

RH HORIZ STAB TIP HAS AREA OF DELAMINATION ON UPPER SURFACE APPROX. 11' FROM T/E. / REPLACED RIGHT HORIZONTAL STAB TIP WITH SERVICABLE UNIT DUE TO EXCESSIVE DAMAGE IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 55-10-52-01K ITEM 40

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 62,841 hrs · 36,825 cycles

MAIN WHEEL WELL BULKHEAD STIFFENER CRACKED AT BS 663, BETWEEN LBL 31.83 TO LBL 6.13. R&R STIFFENER IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO DOOR UPPER MAIN SILL WEB CORRODED BETWEEN BS 820 TO BS 827, WL 195. R&R WEB IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 62,841 hrs · 36,825 cycles

ACB AFT SCUFF PLATE IS CRACKED / AFT CARGO BAY AFT SCUFF PLATE REPAIRED PER EA 1-A53-2076 REV 11

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 62,841 hrs · 36,825 cycles

LOWER LT VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 7 TO LBL 15. REPAIRED BARRIER PER SRM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 500A TO BS 500B, STR 25L. R&R BAFFLE IAW SRM AND DWG.

Part: NONE — CRACKED (LH WING) · airframe 62,841 hrs · 36,825 cycles

SUPPLEMENTAL INFORMATION: LT WING INBD FLAP INBD LOWER PANEL NUT PLATE STRIP COMMON TO SEAL PLATE ATTACH POINT IS CRACKED / REPLACED LT WING I/B FLAP I/B LOWER PANEL NUT PLATE STRIP IAW SOPM 20-50-01 57431U 16MAY18

Part: PANEL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** IN AFT CARGO BAY ON FLOOR PANEL SUPPORT AT B.S; 771; R.B.L. 12. / REMOVED & REPLACED AT AFT CARGO BAY ON FLOOR PANEL SUPPORT AT BS 771 LBL TO RBL 12 IAW DRW 146A7500 & SRM 51-40-02-0G-0

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL PANEL SUPPORT CORRODED AT BS 944, RBL 20. R&R SUPPORT IAW DWG AND SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FLOORBEAM CRACKED AT BS 328, RBL 21. REPAIRED FLOORBEAM PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON CARGO TRACK CORRODED AT BS 934, RBL 13.8. R&R TRACK IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON CARGO TRACK CORRODED AT BS 934, LBL 3. R&R TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R&R SUPPORT IAW DWG AND SRM.

Part: SUPPORT STRAP — CORRODED (AFT CARGO BAY) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** IN AFT CARGO BAY ON FLOOR PANEL SUPPORT STRAP AT B.S; 887. / REMOVED AND REPLACED ACB FLOOR PANEL SUPPORT STRAP DUE TO NO ALLOWABLE DAMAGE FOUND ON THE SRM PER SRM 51-10-02-0G-0; SRM 51-40-05-0G-0; DWG. NO. 146A9401; AMM 51-21-41-370-802; AMM 51-21-72-370-804 AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 792, RBL 20. R&R SHIELD IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 20. R&R SUPPORT IAW SRM & DWG.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

PANEL 195CL AFT EDGE RADIUS IS CRACKED. / REPAIRED PANEL 195CL AFT EDGE RADIUS CRACK IAW SRM 51-70-05-2R-6

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

PANEL 194CR OUTER SKIN HAS DISBONDED DENT. (MARKED) / REPAIRED OUTER SKIN OF PANEL 194CR IAW SRM 53-60-70-2R-1 AND SRM 51-70-05-2R-1 55974U 16MAY18

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

SEAT TRACK CORRODED BETWEEN BS 663 TO BS 727, RBL 45. R&R SEAT TRACK PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 706 TO BS 727, LBL 65. R&R CHORD PER SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

L1 DOOR SURROUND STRUCTURE INBOARD THRESHOLD INBOARD SILL ANGLE CORRODED AT BS 312, LBL 60. R&R ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,841 hrs · 36,825 cycles

PRESSURE DECK ABOVE MAIN WHEEL WELL CRACKED AT BS 665, RBL 41. REPAIRED DECK PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FORWARD CARGO BAY FLOOR TO BULKHEAD PANEL SUPPORT CORRODED AT BS 500D, BETWEEN LBL 21 TO RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO BS 500D, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

L1 DOOR SURROUND STRUCTURE CENTER THRESHOLD SILL ANGLE CORRODED AT BS 312, LBL 63. R&R ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 683 TO BS 727, RBL 65. R&R CHORD IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

SEAT TRACK CORRODED BETWEEN BS 663 TO BS 727, LBL 45. R&R SEAT TRACK PER SRM.

Part: ANGLE — CORRODED (FWD SERVICE DOOR) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** FWD SERVICE DOOR THRESHOLD TO MOP SILL ANGLE HAS CORROSION AT FASTENER HOLES / LOCATED AND DRILLED NEW FSD THRESHOLD TO MOPSILL ANGLE IAW DWG # 141A8310; OK TO INSTALL LEAD 122; 18MAY18 INSP 316 18MAY18. INSTALLED NEW FSD THRESHOLD TO MOP SILL ANGLED BETWEEN BS 294 & 2 TO BS 328. IAW SRM 51-40-02 AND DWG # 141A8310. 80002U 21MAY18. DISCREPANCY MOPSILL ANGLE CORROSION BEYOND LIMITS. PART TO BE REPAIR BY REPLACEMENT PER SRM 51-10-02-0G-0 89263C 22MAY18 INSP 340 5-22-18

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

BOTTOM OF FLOORBEAM UPPER CHORD CRACKED AT BS 294, RBL 53. REPAIRED CHORD IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

RT FORWARD MOP SILL CORRODED BETWEEN BS 312 TO BS 360, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

INTERCOSTAL CRACKED AT BS 344, LBL 47.5. R&R INTERCOSTAL IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

LT MOPSILL UPPER SURFACE CORRODED BETWEEN BS 967 TO BS 986. R&R MOPSILL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

INTERCOSTAL CRACKED AT BS 321, LBL 47.5. R&R INTERCOSTAL IAW SRM DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 62,841 hrs · 36,825 cycles

LT WING TRANSVERSE WEB SEAL RETAINER CRACKED / REMOVED LEFT WING TRANSVERSE WEB SEAL RETAINER WITH CRACK DAMAGE AND INSTALLED NEW PART SAME LOCATION ABOVE. IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 907 TO BS 927. R&R CREASE BEAM WEB PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

INTERCOSTAL CRACKED AT BS 286, RBL 1. R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 34.75. R&R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

AFT SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1016, RBL 45. R&R SHEAR WEB IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

LT FORWARD MOP SILL CORRODED BETWEEN BS 312 TO BS 360, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: RIB — CRACKED (LT WING) · airframe 62,841 hrs · 36,825 cycles

LT WING INBOARD LEADING EDGE MOST INBOARD WING TO BODY SUPPORT RIB CRACKED. R&R RIB IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 62,841 hrs · 36,825 cycles

RT WING WIGGLE PLATE JUST OUTBOARD OF SWING DOWN PANEL 651DB CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: WEB — CORRODED (MAIN CABIN) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** AFT SHEAR WEB BS 1027 LBL6 WL 208 CORRODED / REMOVED SHEAR WEB AT BS 1016 TO 1027 TO LBL 45 WL 208 IAW SRM 51-40-02. INSTALLED NEW SHEAR WEB ITEM #75 31067. IAW SRM 51-40-02 AND DWG 147A5600 88324U 22MAY18

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 33 TO RBL 45. REPAIRED FLOOR BEAM IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** AFT SHEAR WEB STRAP BS 1016 LBL3 WL 208 CORRODED / AFT SHEAR WEB STRAP BS 1016; LBL 3; WL 208. REMOVED CORROSION 1.2' X 2.9'. MORE THAN 50% OF MATERIAL THICKNESS IAW 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. STEP 4.G (2). REMOVED AND REPLACED STRAP IAW SRM 51-10-02-0G-0 STEP 9 AND DWG # 147A5600

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

LT SHEAR WEB CORRODED AT BS 1010, LBL 42. R&R SHEAR WEB IAW DWG AND SRM.

Part: WEB — CORRODED (R2 DOOR) · airframe 62,841 hrs · 36,825 cycles

***CORROSION*** ASD DOOR CUTOUT LOWER WEB BS 967 - 992 CORRODED WL 208 RBL 62 / ASDOOR CUTOUT LOWER WEB BS967-992 FOUND TO BE OUT OF LIMITS IAW SRM 53-20-15-1A-1 AD1FIG 103 DET. E. REMOVED AND REPLACED ASD WEB FROM BS 947 TO BS 992 RBL 62 WL208 IAW DWG 147A8501 AND SRM 51-40-02

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,841 hrs · 36,825 cycles

RT MOPSILL UPPER SURFACE CORRODED BETWEEN BS 967 TO BS 986, WL 908. R&R MOPSILL IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,841 hrs · 36,825 cycles

FWD SERVICE DOOR #4 BEAM CRACKED PARALLEL TO THE I/B RADIUS. / FWD SERVICE DOOR #4 BEAM THAT WAS CRACKED WAS REPLACED ON WORK ORDER; 506410.

Part: O-RING — LEAKING (HYD PUMP) · airframe 62,814 hrs · 366,805 cycles

AIR TURNBACK DUE TO LOSS OF THE HYD SYSTEM -A- PRESSURE. FOUND THE 1 HYDRAULIC PUMP HAD LEAKED AROUND PRESSURE LINE. R & R THE O-RING IAW AMM.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 62,658 hrs · 36,705 cycles

DELAMINATION ON INTERIOR PNL AT HOLES 21;34;35 (PNL 193B) / REPLACED PANEL 193B WITH ROBBED PART FROM A/C 719 REF AMM 53-51-21

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 61,818 hrs · 36,171 cycles

CENTER AISLE OVERHEAD CEILING EMERGENCY EXIT SIGN LIGHT BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 61,011 hrs · 35,675 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. R&R HOOK PER SRM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 59,497 hrs · 34,773 cycles

EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED THE LENS IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 58,775 hrs · 34,326 cycles

AFT MID CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED SIGN PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,089 hrs · 33,313 cycles

EMERGENCY EXIT LIGHT INOP AT BS 639, BETWEEN STR 14L TO STR 15L. R & R LAMP IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,089 hrs · 33,313 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,089 hrs · 33,313 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STABILIZER STA 92.70. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,089 hrs · 33,313 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON STABILIZER STA 120.30. REPAIRED RIB IAW SRM.

Part: PLATE — CRACKED (BS 1104) · airframe 57,089 hrs · 33,313 cycles

RIGHT HORIZONTAL STABILIZER AFT TRACK ASSEMBLY ON SEAL PLATE CRACKED AT BS 1104. R & R THE PLATE IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 907) · airframe 57,089 hrs · 33,313 cycles

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

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 57,089 hrs · 33,313 cycles

RIGHT HORIZONTAL STABILIZER SEAL PLATE CRACKED. R & R PLATE IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

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

Part: RIB — CRACKED (VERTICAL STAB) · airframe 57,089 hrs · 33,313 cycles

VERTICAL STABILIZER RIB CRACKED ON FORWARD POSITION ON DORSAL FIN. R & R RIB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 727B) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (BS 500A) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (BS 907) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGERS 7 & 9R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 787) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 57,089 hrs · 33,313 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 57,089 hrs · 33,313 cycles

LT EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 57,089 hrs · 33,313 cycles

RIGHT EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: WEB — CRACKED (WIND TO BODY) · airframe 57,089 hrs · 33,313 cycles

WING TO BODY FAIRING SUPPORT STRUCTURE AT LOWER FUSELAGE WEB CRACKED AT BS 727, RBL 14. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,089 hrs · 33,313 cycles

FRAME CRACKED AT BS 727, BETWEEN STR 17L TO STR 18L. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 57,089 hrs · 33,313 cycles

RIGHT WING NR 6 SLAT LEADING EDGE NOSE SKIN CRACKED AT WS 202.45, ON LOWER SURFACE. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING LE) · airframe 57,089 hrs · 33,313 cycles

LEFT WING NR 2 LEADING EDGE NOSE SKIN CRACKED AT WS 322.71, ON LOWER SURFACE. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 57,089 hrs · 33,313 cycles

L/H WING LEADING EDGE NR 1 SLAT NOSE SKIN CRACKED ON LOWER SURFACE AT STA. 451.97. / REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 57,089 hrs · 33,313 cycles

FUSELAGE FRAME CRACKED AT BS 727, BETWEEN STRINGER 17 - 18R. REPAIRED THE FRAME IAW EA.

Part: COVER — MISSING (EXIT SIGN) · airframe 56,536 hrs · 32,977 cycles

LEFT EMER EXIT SIGN COVER MISSING AT ROW 11. R & R SIGN IAW SIP.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 55,884 hrs · 32,613 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED, JUST INBD OF STAB STATION 129.5, AFT OF FRONT SPAR. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

FLOORBEAM SEAT TRACK CRACKED AT BS 727B, RBL 24, BOTH FWD FASTENER HOLES ON INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

FLOORBEAM SEAT TRACK CRACKED AT BS 727B, LBL 45, FWD FASTENER HOLE ON INBD FLANGE. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

SEAT TRACK FWD OF BS 727B, LBL 24 CRACKED AT BOTH FWD OF AFT FASTENER HOLES ON INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

SEAT TRACK FWD OF BS 727B, RBL 24 CRACKED AT BOTH FWD OF AFT FASTENER HOLES ON INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

FLOORBEAM SEAT TRACK FITTING CORRODED AT BS 727B, LBL 24. R & R FITTING IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

SEAT TRACK FWD OF BS 727B, LBL 45 CRACKED AT BOTH FWD OF AFT FASTENER HOLES ON INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

SEAT TRACK FWD OF BS 727B, RBL 45 CRACKED AT BOTH FWD OF AFT FASTENER HOLES ON INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

LEFT NR 3 WINDOW FRAME E - F POST, 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,851 cycles

LEFT NR 3 WINDOW FRAME E - F POST, 3RD FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: LENS — MISSING (CABIN) · airframe 52,359 hrs · 30,617 cycles

FORWARD LOWER EMER EXIT LIGHT LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 52,359 hrs · 30,617 cycles

AFT LOWER EMER EXIT LIGHT LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: AILERON — BINDING · airframe 52,245 hrs · 30,551 cycles

BINDING FELT DURING AILERON OPERATION. COMPLIED WITH MT 727-10-00.

Part: LIGHT — CRACKED (CABIN) · airframe 51,338 hrs · 30,047 cycles

LEFT EEPLS CRACKED AT ROW 24. R & R EEPLS IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 50,765 hrs · 29,703 cycles

RIGHT LOWER EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,405 hrs · 29,485 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5, 9 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,405 hrs · 29,485 cycles

MAIN WW SPAR VERTICAL PRESS WEB INTERIOR SIDE CRACKED AT BS 663 LBL 41.0. REPAIRED WEB IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 50,053 hrs · 29,298 cycles

RIGHT EMER EXIT DOOR LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 49,028 hrs · 28,692 cycles

R1 DOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING. R & R SIGN ASSEMBLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 46,601 hrs · 27,212 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSY IAW AMM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 45,504 hrs · 26,550 cycles

RIGHT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED & INSTALLED NEW RIGHT OVERWING DOOR SIDEWALL LIGHT BALLAST PER AMM. OPS CHECK

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 44,911 hrs · 26,185 cycles

ALL SEVEN EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. FWD L/H, FWD R/H, CTR L/H, CTR R/H, ROW 16 L/H, AFT L.H, AFT R/H. REMOVED AND REPLACED ALL SEVEN EMERGENCY LIGHT BATTERIES PER MM. FWD L/H, FWD R/H, CTR L/H, CTR R/H, ROW 16 L/H, AFT L.H, AFT R/H.

Part: BRACKET — BROKEN (L1 DOOR) · airframe 43,608 hrs · 25,370 cycles

L1 DOOR EMERGENCY EVAC SLIDE LATCH BRACKET ASSY BROKEN. REMOVED AND REPLACED SLIDE IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 43,608 hrs · 25,370 cycles

AFT LAV MOUNTED EMERGENCY EXIT LIGHT BROKEN. REMOVED AND RELACED LENS IAW AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 43,608 hrs · 25,370 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1. SECURED CONNECTOR IAW WDM & AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 43,608 hrs · 25,370 cycles

L2 DOOR EMERGENCY EXIT SIGN ON AFT LAV INOP. SECURED CONNECTORS IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 43,608 hrs · 25,370 cycles

FORWARD LAV LOWER EMERGENCY EXIT SIGN LIGHT ASSY BROKEN. REMOVED AND REPLACED SIGN IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

FRAME CRACKED AT BS 867, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW IR AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,608 hrs · 25,370 cycles

FORWARD CARGO PIT DOOR CUTOUT LOWER THRESHOLD WEB CORRODED BETWEEN BS 460 TO BS 477, RBL 32. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,608 hrs · 25,370 cycles

LEFT WING O/B AFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,608 hrs · 25,370 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STAB STA 101.9. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,608 hrs · 25,370 cycles

CAPTAIN WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 43,389 hrs · 25,232 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 42,914 hrs · 24,956 cycles

RT EMERGENCY EXIT LIGHT ASSY DAMAGED AT ROW 13. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 40,181 hrs · 23,346 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,812 hrs · 25,488 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 40,181 hrs · 23,346 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,813 hrs · 21,375 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB PER EA.

Part: LIGHT — CORRODED (CABIN) · airframe 36,813 hrs · 21,375 cycles

DURING SCHEDULED 10Y CHECK, FOUND EEPLS CORRODED. REMOVED AND REPLACED EEPLS PER MM.

Part: FITTING — CORRODED (RT WING TRUNNION) · airframe 35,156 hrs · 20,413 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: FITTING — CORRODED (LT WING) · airframe 35,156 hrs · 20,413 cycles

DURING SCHEDULED MV2 CHECK, FOUND L/H WING MLG TRUNNION FITTING LUG FACES CORRODED. R&R FITTING PER SWA EA.

Part: LENS — BROKEN (CABIN) · airframe 34,535 hrs · 20,028 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,407 hrs · 18,698 cycles

R1 DOOR EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 31,296 hrs · 18,011 cycles

FOUND R1 DOOR EGRESS SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,201 hrs · 17,318 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,201 hrs · 17,318 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,201 hrs · 17,318 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 29 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 30,201 hrs · 17,318 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 30,201 hrs · 17,318 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 29,601 hrs · 16,957 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,461 hrs · 16,869 cycles

DURING SCHEDULED MV1 CHECK, FOUND MID CABIN EMERGENCY BULLNOSE AND LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,175 hrs · 15,515 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,411 hrs · 15,052 cycles

DURING SCHEDULED MV2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: CAP — LOOSE (CABIN) · airframe 25,807 hrs · 14,711 cycles

EEPLS END CAP LOOSE AT ROW 3 DEF. SECURED END CAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 25,783 hrs · 14,699 cycles

EEPLS COVER LOOSE AT ROW 5 ABC. SECURED COVER PER MM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 24,905 hrs · 14,178 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER SRM.

Part: COVER — DAMAGED (CABIN) · airframe 24,593 hrs · 13,990 cycles

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

Part: COVER — DAMAGED (CABIN) · airframe 24,593 hrs · 13,990 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER DISCOLORED AT ROW 7 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 24,593 hrs · 13,990 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER DISCOLORED AT ROW 8 DEF. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,291 hrs · 11,011 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,037 hrs · 10,845 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,336 hrs · 9,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT MID, LT & RT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,408 hrs · 9,325 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BALLAST PER MM.

Part: CAP — BROKEN (EMERGENCY LIGHT) · airframe 13,657 hrs · 7,833 cycles

EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 12,893 hrs · 7,445 cycles

FWD EEPLS COVER OUT OF POSITION. REPOSITIONED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,472 hrs · 7,249 cycles

EEPLS COVER MISSING BETWEEN ROWS 11 AND 12. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,431 hrs · 7,218 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: ACTUATOR — FAULTY (NR 3 LE SLAT) · airframe 12,009 hrs · 6,967 cycles

AIR TURN BACK, NR 3 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED ALL L/E SLAT ACTUATORS PER MM.

Part: ACTUATOR — FAULTY (NR 5 LE SLAT) · airframe 11,945 hrs · 6,920 cycles

AIR TURN BACK, ON FLAP RETRACTION L/E LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED NR 5 L/E SLAT ACTUATOR PER MM.

Part: COVER — CRACKED (CABIN) · airframe 8,961 hrs · 5,244 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 4,300 hrs · 2,563 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED ( 23 EA ) THROUGH OUT CABIN. R&R COVERS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 4,300 hrs · 2,563 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.