N712SW

Part: GUIDE ARM — DEFECTIVE (L1 DOOR) · airframe 76,390 hrs · 45,780 cycles

FORWARD ENTRY DOOR WILL NOT OPEN. R&R GUIDE ARM PIN AND HARDWARE PER MM 52-11-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 76,172 hrs · 45,655 cycles

LEFT AFT PORTION OF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-51-06. OPS CHECK OK.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 75,946 hrs · 45,531 cycles

AFT LAV SMOKE ALARM CAME ON WITH NO OTHER INDICATIONS / R/R AFT LAV SMOKE DETECTOR PER AMM # 26-14-01 P/N 475571-2 INSTALLED

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,912 hrs · 45,512 cycles

APEX AREA OF THE AFT PRESSURE BULKHEAD BSTA 1016 HAS A CRACK INDICATION FROM PROD WEB FASTENER INWARD CNTR-LOCATED BSTA 1016 BL 0 +R1 APPROX. 18.25' FROM CENTER OF INNER CIRCLE TEAR STRAP 154.5 ' FROM FUSELAGE UPPER SKIN REF PROVIDED PICTURES-REF NRC D378847 / AFT BULKHEAD BS 1016 CRACK AT FASTENER BL 0 + R1 FOUND TO BE OUT OF LIMITS PER SRM 53-80-08-1A-1. REPAIRED CRACK DAMAGE PER ER 20-02363 REV IR AND EA 20-153-00223 REV IR

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,909 hrs · 45,511 cycles

SUPPLEMENTAL INFORMATION: APEX AREA OF THE AFT PRESSURE BULKHEAD BSTA 1016 HAS CRACK INDICATION FROM PROD WEB FASTENER INWARD CNTR - LOCATED BSTA 1016 BL 0 + R1 APPROX 18.25' FROM CENTER OF INNER CIRCLE TEAR STRAP/54.5' FROM FUSELAGE UPPER SKIN REF PROVIDED PICTURES - REF NRC D378847 - / TRANSFERRED TO NRC N256256

Part: FAIRING — CRACKED (RT FLAP TRACK) · airframe 75,880 hrs · 45,495 cycles

RIGHT WING OUTBOARD AFT FLAP #2 TRACK LOWER FAIRING IS CRACKED. / R&R RIGHT WING OUTBOARD AFT FLAP #2 TRACK LOWER FAIRING PER SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 75,880 hrs · 45,495 cycles

RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL PER SRM 51-40-02 AND AMM 53-31-31 .

Part: FAIRING — CRACKED (RT FLAP TRACK) · airframe 75,880 hrs · 45,495 cycles

RIGHT WING OUTBOARD AFT FLAP #3 TRACK LOWER FAIRING IS CRACKED. / R&R RIGHT WING OUTBOARD AFT FLAP #3 TRACK LOWER FAIRING PER SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,626 hrs · 45,338 cycles

RIGHT HAND EMERGENCY EXIT FORWARD LOWER LAMP WAS INOPERATIVE. / RELAMPED LAMP PER AMM.

Part: LENS — DAMAGED (CABIN) · airframe 75,626 hrs · 45,338 cycles

FORWARD GALLEY LOWER EMERGENCY EXIT INDICATOR SIGN LENS WAS DAMAGED. / R&R LENS PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,626 hrs · 45,338 cycles

EMERGENCY EXIT LIGHT ASSEMBLIES L1189 HAD BULBS OUT. R&R LIGHT BULBS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,626 hrs · 45,338 cycles

ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1674 BATTERY PACK WERE INOPERATIVE. / R&R BATTERY PACK M1674 PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,626 hrs · 45,338 cycles

EMERGENCY EXIT LIGHT ASSEMBLIES L1188 HAD BULBS OUT. / R&R LIGHT BULBS IAW AMM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 75,626 hrs · 45,338 cycles

ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 BATTERY PACK TURN ON MOMENTARILY. / R&R BATTERY PACK M1672 PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,626 hrs · 45,338 cycles

EMERGENCY EXIT LIGHT ASSEMBLIES L1070 HAD BULBS OUT. / R&R LIGHT BULBS IAW AMM.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 75,626 hrs · 45,338 cycles

FLOOR BEAM VERTICAL WEB CORRODED AT BS. 259, BETWEEN RBL 3.5 TO RBL 7. / REPAIRED WEB PER EA.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 75,626 hrs · 45,338 cycles

WHILE ACCESSING FWD CABIN FLOOR PANEL #221BF FOR COCKPIT REPAIR; FOUND PANEL TO HAVE SURFACE DAMAGE. REPAIRED SURFACE DAMAGE ON FLOOR PANEL 221BF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-4.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 75,626 hrs · 45,338 cycles

FLOOR BEAM AFT CHORD CORRODED AT BS. 259, BETWEEN LBL 3 TO RBL 5. / REPAIRED FLOOR BEAM AFT CHORD PER ER AND EA.

Part: STRAP — CORRODED (BS 270) · airframe 75,626 hrs · 45,338 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS. 270, BETWEEN LBL 3 TO RBL 5. / R&R FLOOR BEAM UPPER CHORD STRAP IAW EA.

Part: WEB — CORRODED (BS 259) · airframe 75,626 hrs · 45,338 cycles

VERTICAL WEB CORRODED AT BS. 259, RBL 3.5. / REPAIRED WEB PER EA.

Part: WEB — CORRODED (BS 927-947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY VERTICAL WEB HAD CORROSION BETWEEN BS. 927 TO BS. 947, RBL 13 ON LOWER FLANGE. / R&R VERTICAL WEB IAW SRM & DWG.

Part: ATTACH BRACKET — CRACKED (BS 947 LBL 8) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY FLOOR SUPPORT TO FRAME ATTACH BRACKET IS CRACKED IN THE RADIUS BS947 LBL8 / REMOVED & REPLACED ACB FLOOR SUPPORT TO FRAME ATTACH BRACKET BS947; LBL8 IAW SRM 51-40-02; SRM 51-40-05; DWG #147A7500; DWG #147A1047; DWG #147A7580

Part: FLOORBEAM — CORRODED (BS 260) · airframe 75,626 hrs · 45,338 cycles

UPPER FLOOR BEAM CHORD CORRODED AT BS. 260, BETWEEN LBL 34 TO RBL 34. / R&R FLOOR BEAM CHORD IAW DWG AND SRM.

Part: BAFFLE — CRACKED (BS 927-947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY R/H AFT FLOOR TO SIDEWALL SUPPORT PLATE BAFFLE WAS CRACKED ON AFT LOWER EDGE BETWEEN BS. 927 TO BS. 947, RBL 21. / R&R BAFFLE IAW SRM & DWG.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 75,626 hrs · 45,338 cycles

FLOOR PANEL 241EF DISBONDED UPPER SURFACE. / DUE TO THE EXTENT OF DAMAGE TO FLOOR PANEL 241EF; OPTED TO FABRICATE A NEW FLOOR PANEL USING BMS 4-23TY2 LOT #: 1416426-1. INSTALLED ALL THROUGH INSERTS USING BMS 5-107 LOT #:AK9FP3008K AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A 'NOTE' AND PARA 5S AND DWG 144A5810-10. 59198U 1.31.20.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 75,626 hrs · 45,338 cycles

SEAT TRACK CROWN ON TOP AND IN WELL CORRODED BETWEEN BS. 480 TO BS. 520, LBL 25. / R&R SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 75,626 hrs · 45,338 cycles

SEAT TRACK CROWN ON TOP AND IN WELL CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 75,626 hrs · 45,338 cycles

FLOOR PANEL 241AF DISBONDED UPPER SURFACE. / FLOOR PANEL 241AF WITH DISBONDED UPPER SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0. PARA. 9.A.(1).

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 75,626 hrs · 45,338 cycles

SEAT TRACK CROWN ON TOP AND IN WELL CORRODED BETWEEN BS 480 TO BS. 520, LBL 45. / R&R SEAT TRACK PER SRM.

Part: WEB — CORRODED (BS 847-867) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY VERTICAL WEB HAD AREA OF CORROSION BETWEEN BS. 847 TO BS. 867, RBL 6 ON LOWER EDGE OF LIGHTNING HOLE. / REPAIRED WEB IAW SRM, AMM, AND DWG.

Part: GUSSET — CRACKED (BS 847) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY LOWER LAV SUPPORT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 847, LBL 10. / R&R GUSSET PER SRM & DWG.

Part: WEB — CORRODED (BS 767) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY CLIP COMMON TO VERTICAL WEB BS767+8 RBL20 WL152 HAS CORROSION / REPLACED AFT CARGO BAY CLIP COMMON TO VERTICAL WEB BS647+8' RBL20 WL152 SRM 51-40-05-0G-0. SRM 51-40-02-0G-0; DWG# 146A8125-6

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 75,626 hrs · 45,338 cycles

R/H BS663 VAPOR BARRIER EXHAUST RING DOUBLER IS CRACKED AT RBL25 WL144 / REMOVED AND REPLACED RH BS663 VAPOR BARRIER EXHAUST RING DOUBLE RBL25 WL144 IAW SRM 51-40-05; SRM 51-40-02; AIPC 57-11-00-02 AND DWG 111A1000.

Part: LENS — DISCOLORED (CABIN) · airframe 75,626 hrs · 45,338 cycles

FORWARD ENTRY CENTER PANEL EXIT LENS DISCOLORED. / R&R LENS PER AMM.

Part: WEB — CORRODED (BS 927-947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY VERTICAL WEB HAD CORROSION BETWEEN BS. 927 TO BS. 947, LBL 3. / R&R WEB IAW SRM & DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 75,626 hrs · 45,338 cycles

R1 DOOR #4 (LOWER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / REPAIRED #4 BEAM ON CARD #14079 & PO # 0520055-GIR.

Part: SUPPORT — CORRODED (BS 947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY LOWER CENTER BULKHEAD SUPPORT HAD CORROSION AT BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 75,626 hrs · 45,338 cycles

AFT ENTRY CENTER EXIT LIGHT LENSES DISCOLORED. / R&R LENS PER AMM.

Part: WEB — CORRODED (BS 787) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY VERTICAL WEB HAD AREA OF CORROSION AT BS. 787+4, RBL 6 ON LOWER EDGE OF LIGHTNING HOLE. / R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 847, LBL 23, AROUND NUT PLATE HOLES. / R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 492-550A) · airframe 75,626 hrs · 45,338 cycles

FORWARD CARGO BAY R/H SHIELD AFT OF CARGO DOOR HAS AREAS OF CORROSION AROUND NUT PLATE BETWEEN BS. 492 TO BS. 550A, RBL 21. / R&R SHIELD PER SRM AND DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION BS767+5 RBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP FOR B.S 767+5 ON CUST.PO# 771569 NEW PART WILL BE REINSTALLED ON CUST.CARD# JPANEL-141-CLOSE

Part: CARGO TRACK — CORRODED (BS 927) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY RH CARGO TIE DOWN TRACK AT BS. 927+7, RBL 13 HAD CORROSION AROUND NUT PLATE HOLE. / R&R TIE DOWN IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAD AREAS OF CORROSION AROUND NUT PLATE HOLES BETWEEN BS. 727 TO BS. 767, RBL 23. / R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 887-947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAD AREAS OF CORROSION BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 947) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY BULKHEAD SUPPORT HAD CORROSION AT BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 927) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY L/H CARGO TIE DOWN TRACK AT BS. 927+7, LBL 3 HAD CORROSION AROUND NUT PLATE HOLE. / R&R TIE DOWN TRACK IAW SRM & DWG.

Part: SHIELD — CORRODED (BS 767-794) · airframe 75,626 hrs · 45,338 cycles

SHIELD FORWARD OF THE DOOR HAD AREAS OF CORROSION BETWEEN BS. 767 TO BS. 794, RBL 23. / R&R SHIELD PER SRM AND DWG.

Part: SHIELD — CORRODED (BS 420-440) · airframe 75,626 hrs · 45,338 cycles

FORWARD CARGO BAY R/H SHIELD FORWARD OF CARGO DOOR HAD AREAS OF CORROSION AROUND NUT PLATE BETWEEN BS. 420 TO BS. 440, RBL 21. / R&R SHIELD PER SRM & DWG.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 75,626 hrs · 45,338 cycles

FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR HEADER PANEL EXIT LENSES ARE DISCOLORED. / R&R LENSES IAW AMM.

Part: STRAP — CORRODED (BS 887) · airframe 75,626 hrs · 45,338 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAD CORROSION AT BS. 887, RBL 10. / R&R STRAP IAW SRM.

Part: BOOT — DAMAGED (RADOME) · airframe 75,626 hrs · 45,338 cycles

NOSE RADOME BOOT DAMAGED / DAMAGED RADOME BOOT WAS REMOVED & REPLACED ON SWA EA 1-A53-9144 REV 1. RADOME WAS REMOVED FROM THE AIRCRAFT & WILL BE REINSTALLED ON NRC U119853.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 75,626 hrs · 45,338 cycles

LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 8 TO RBL 15. / R&R VAPOR BARRIER PANEL PER SRM & DWG.

Part: FITTING — LOOSE (L2 DOOR GIRT BAR) · airframe 74,671 hrs · 44,733 cycles

L2 DOOR SLIDE GIRT BAR FORWARD CLIP LOOSE. / ADJUSTED CLIP PER SIP.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 74,128 hrs · 44,382 cycles

R/H WHEEL WELL VAPOR BARRIER FORWARD CRACKED IN BAY 2R AT BS. 663, APPROX. 10.0 RBL. / REPAIRED BARRIER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,441 hrs · 43,298 cycles

EXTERNAL POWER PLUG IN CRACKED. REPAIRED CUTOUT PER SRM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 72,021 hrs · 43,036 cycles

RT OVERWING EMERGENCY ESCAPE LIGHT INOP. RECONNECTED CONNECTOR PER WDM.

Part: SCREW — LOOSE (R2 DOOR) · airframe 70,642 hrs · 42,127 cycles

R2 DOOR SLIDE COVER FORWARD SCREW LOOSE. SECURED SCREW PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,095 hrs · 41,155 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: WEB — CRACKED (RT WING) · airframe 69,095 hrs · 41,155 cycles

RT WING WEB ASSEMBLY CRACKED AT APPROX ORSS 268. R&R WEB ASSEMBLY PER DWG AND SRM.

Part: STRINGER — CORRODED (BS 351-366) · airframe 69,095 hrs · 41,155 cycles

STRINGER 28R CORRODED BETWEEN BS 351 TO 366.01. R & R THE STRINGER IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,095 hrs · 41,155 cycles

RT HORIZONTAL STABILIZER RIB CRACKED FORWARD UPPER INBOARD FLANGE AT STAB STA 120.3. REPAIR RIB IAW ER AND EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,095 hrs · 41,155 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.3. REPAIRED THE RIB IAW EA.

Part: SPLICE STRAP — CORRODED (BS 358) · airframe 69,095 hrs · 41,155 cycles

SPLICE STRAP CORRODED AT BS 358, RBL 2. REPAIRED SPLICE STRAP IAW ER AND EA.

Part: SHEAR TIE — CORRODED (BS 358) · airframe 69,095 hrs · 41,155 cycles

SHEAR TIE CORRODED AT BS 358, RBL 2. REPAIRED THE SHEAR TIE IAW ER AND EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,095 hrs · 41,155 cycles

L2 DOOR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA & AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 69,095 hrs · 41,155 cycles

LT WING SUPPORT STRUCTURE JUST INBOARD OF DEFLECTION RIB FITTING ANGLE BRACKET CRACKED ORSS 621+ 12. R&R BRACKET IAW SRM & DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 69,095 hrs · 41,155 cycles

AFT CARGO BAY RT SIDE SHIELD CORRODED BETWEEN BS 767 TO 787. R & R THE SHIELD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 727D-767) · airframe 69,095 hrs · 41,155 cycles

AFT CARGO BAY RT SIDE CHANNEL CORRODED BETWEEN BS 727D TO 767. R & R THE CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 767-787) · airframe 69,095 hrs · 41,155 cycles

AFT CARGO BAY LT SIDE CHANNEL CORRODED BETWEEN BS 767 TO 787. R & R THE CHANNEL IAW SRM.

Part: WEB — CORRODED (BS 490) · airframe 69,095 hrs · 41,155 cycles

FORWARD CARGO DOOR SUB THRESHOLD WEB CORRODED AT BS 490, RBL 25. R & R THE WEB IAW SRM AND DWG.

Part: WEB — CRACKED (BS 663-675) · airframe 69,095 hrs · 41,155 cycles

PRESSURE WEB FOUND CRACKED BETWEEN BS 663 TO 675, LBL 40. REPAIRED THE WEB IAW EA.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 69,095 hrs · 41,155 cycles

RIGHT WING LOWER SURFACE OF THE LEADING EDGE NR 7 SLAT NOSE SKIN CRACKED AT WS. 542. REPAIRED THE SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,095 hrs · 41,155 cycles

RT WING NR 5 SLAT NOSE SKIN CRACKED AT LOWER SURFACE OF THE LEADING EDGE OUTBOARD OF ACTUATOR RIBS, APPROX WS 307. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,095 hrs · 41,155 cycles

LT WING LEADING EDGE NR 1 SLAT NOSE SKIN CRACKED AT LOWER SURFACE AT ACTUATOR RIBS APPROX WS 643. REPAIRED NR 1 SLAT NOSE SKIN IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,095 hrs · 41,155 cycles

LOWER LEFT BULKHEAD WEB CRACKED AT BS 663. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,095 hrs · 41,155 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,095 hrs · 41,155 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,839 hrs · 39,157 cycles

RIGHT OVERWING EMERGENCY EXIT LOWER LENS MISSING. INSTALLED THE LENS IAW AMM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,206 hrs · 38,783 cycles

L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW AMM.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 63,568 hrs · 37,839 cycles

AIR TURN BACK. NR 1 SPARE VLV CLOSED LT ILLUMINATED BRIGHT ON CLIMB OUT. R & R NR 1 ENG SPARE VLV IAW AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,870 hrs · 37,430 cycles

RIGHT MLG FWD TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 62,810 hrs · 37,396 cycles

RIGHT AFT OVERHEAD EMER EXIT SIGN INOPERATIVE. RECONNECTED CONNECTOR IAW WDM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 - 787, RBL 8. R & R INTERCOSTAL IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,810 hrs · 37,396 cycles

CARGO TRACK CORRODED AT BS 798, RBL 15. R & R CARGO TRACK IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

LEFT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 747+10 - 847. REPAIRED SUPPORT IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

BULKHEAD SUPPORT STIFFENER LOWER ATTACH ANGLE CRACKED AT BS 865, LBL 16. R & R ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

FORWARD SERVICE DOOR THRESHOLD SUPPORT CORRODED, BETWEEN BS 294 - 28, RBL 60. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

INTERCOSTAL CORRODED AT BS 929, RBL 2. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

ANGLE ON FLOOR SUPPORT SHIELD CORRODED AT BS 852, RBL 19. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

STRINGER SPLICE CORRODED AT BS 887, STRINGER 27R. R & R SPLICE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

INTERCOSTAL CORRODED AT BS 727+8, BETWEEN RBL 6 TO LBL 6. R & R INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

R1 DOOR FWD FRAME CRACKED IN INNER FLANGE AT BS 294, RBL 53. REPAIRED FRAME IAW EA & ER.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

FORWARD SERVICE DOOR MOP SILL CORRODED, BETWEEN BS 294 - 360, RBL 55. R & R MOP SILL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

FLOOR SUPPORT CORRODED AT BS 947+4, RBL 32. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

FLOORBEAM UPPER FLANGE CORRODED, AT BS 328, BETWEEN RBL 40 - 55. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

L1 DOOR AFT GIRT SUPPORT FITTING CORRODED AT BS 344, LBL 60. R & R FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 45 - RBL 31. REPAIRED FLOORBEAM IAW EA & ER.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 62,810 hrs · 37,396 cycles

L1 DOOR FWD GIRT SUPPORT FITTING CORRODED AT BS 312, LBL 58. R & R FITTING IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 61,999 hrs · 36,928 cycles

L2 DOOR EMER EXIT SIGN ON AFT BULKHEAD INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 61,493 hrs · 36,645 cycles

AFT ENTRY EMER EXIT MARKER LENS COVER BROKEN. R & R COVER IAW SIP.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 61,482 hrs · 36,640 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING LUG CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 61,482 hrs · 36,640 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING LUG CORRODED. REPAIRED FITTING IAW EA.

Part: CLAMP — LEAKING (COALESOR BAG) · airframe 60,969 hrs · 36,349 cycles

DECLARED AN EMERGENCY, CABIN ALTITUDE WARNING HORN SOUNDED AT FL 340, CABIN ALTITUDE REACHED 10,000 FT, NO LIGHTS OR INDICATIONS FROM ANY SYSTEMS ILLUMINATED. RESET THE CIRCUIT BREAKER IAW AMM. FOUND LEAK IN RIGHT A/C PACK BAY AT THE COALESOR BAG WATER SEPARATOR HOUSING. R & R THE CLAMP ON HOUSING IAW AMM.

Part: DUCT — BROKEN (AC BAY) · airframe 60,969 hrs · 36,349 cycles

DECLARED EMER. CABIN ALT WARNING HORN SOUNDED AT FL 340, CABIN ALT REACHED 10,000' NO LIGHTS OR INDICATIONS FROM ANY SYSTEMS ILLUMINATED. FOUND BROKEN DUCT IN AIR DISTRIBUTION BAY IN AFT FWD CARGO COMPARTMENT RT SIDE. R & R DUCT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,666 hrs · 36,183 cycles

LEFT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,614 hrs · 36,149 cycles

L1 DOOR SLIDE PRESS INDICATES LOW. R & R SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,501 hrs · 35,510 cycles

LEFT EMER EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT IAW SIP.

Part: LENS — CRACKED (CABIN) · airframe 58,555 hrs · 34,974 cycles

FORWARD LAVATORY WALL EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: LIGHT — FAULTY (CABIN) · airframe 58,535 hrs · 34,964 cycles

DIVERSION AT FL380 FLIGHT ATTENDANT REPORTED ODOR OF SMOKE AROUND ROW 2 ABC &DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 57,712 hrs · 34,491 cycles

L1 DOOR EMER EXIT SIGN COVER BROKEN. R & R COVER ASSEMBLY IAW AMM.

Part: COVER — LOOSE (L2 DOOR) · airframe 57,236 hrs · 34,216 cycles

L2 DOOR EMERGENCY EVAC SLIDE PACK COVER LOOSE. SECURED COVER IAW AMM & MT.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,208 hrs · 33,626 cycles

RT CREASE BEAM ANGLE CORRODED AT BS 639. REPAIRED BEAM IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,208 hrs · 33,626 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,208 hrs · 33,626 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 36. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,208 hrs · 33,626 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

LT DOUBLER FOR NR 4 & 5 WINDOW CRACKED AT FASTENER HOLE. REPAIRED DOUBLER IAW EA & SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

LT NR 1 WINDOW FRAME CRACKED AT UPPER 2 FASTENER ON INNER SIDE ATTACHMENT. R&R FRAME IAW ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

NR 3 WINDOW WEB CRACKED AT STATION 259, STRINGER 8L. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,746 hrs · 32,771 cycles

LT HORIZONTAL STABILIZER IN-SPAR RIB CRACKED AT STATION 92.7 IS CRACKED 20 INCHES AFT OF FRONT SPAR AT VERTICAL LEG. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,746 hrs · 32,771 cycles

LT HORIZONTAL STABILIZER LOWER IN SPAR RIB CRACKED AT STATION 92.7, 10 INCHES AFT OF FWD SPAR ON VERTICAL LEG. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

NR 1 LT WINDOW FRAME CRACKED. R&R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,746 hrs · 32,771 cycles

RT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED AT STATION 92.70. REPAIRED CHORD IAW AAR EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

RT NR 1 WINDOW FRAME TOP OTBD CORNER CRACKED IN FRAME. R&R FRAME IAW ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R&R CLIP IAW DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

FRAME CRACKED AT STATION 440 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

RT FS FRAME CRACKED AT STATION 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

FRAME CRACKED AT STATION 480 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

FS FRAME CRACKED AT STATION 827 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

LT FS FRAME CRACKED AT STATION 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

RT FS FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

RT FS FRAME CRACKED AT STATION 867, STRINGER 8R. R&R FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

LT FS FRAME CRACKED AT STATION 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

RT FS FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

FS FRAME CRACKED AT STATION 907 STRINGER 8L. REPAIR FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,746 hrs · 32,771 cycles

LT NR 3 WINDOW FRAME CRACKED SECOND FASTENER HOLE LOWER CORNER. R&R FRAME IAW EA & DRAWING & SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,695 hrs · 31,563 cycles

RIGHT OVERWING EMERGENCY EXIT INTERIOR & EXTERIOR LIGHTS INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT BATTERY PACK PANEL AT STA 603 RBL 67. OPS CHECK GOOD. ALL WORK IAW MM.

Part: RING — WORN (THRUST REVERSER) · airframe 51,567 hrs

CMM 78-31-37 REV 24 01JUL2012 SB 737-78-1072 REV 00 16JUN2005 INSPECTION FINDING OF 1 MISSING BACB30LE6K29 BOLT (FIGURE 12, ITEM 100) COMMON TO THE LOWER AFT HOLE OF THE 315A2222-5 CASCADE RING AND THE 315A2402-6 BEAM ASSY AND 1 EA BACB30LE6K29 COMMON TO THE FWD HOLE OF THE CASCADE SUPPORT RING AND THE LATCH BEAM IS LOOSE. THE 2 .375/.379 HOLE LOCATIONS FOR BACB30LE6K29 BOLTS C/T THE 315A2222-5 CASCADE RING ASSY ARE ELONGATED. CORRESPONDING .375 / .379 HOLE LOCATION FOR THE FWD MOST BACB30LE6K29 BOLT C/T THE 315A2402-6 LATCH BEAM FITTING (FIG 22, ITEM 325C) IS ELONGATED. ALSO A DEEP AREA OF WEAR AROUND THE FWD HOLE LOCATION C/T THE -6 BEAM INBOARD SURFACE. CORRESPONDING .4040 / .4160 HOLE LOCATION FOR THE AFT MOST BACB30LE6K29 BOLT C/T THE 315A2402-6 LATCH BEAM FITTING IS ELONGATED. THERE IS ALSO A DEEP AREA OF WEAR AROUND THE FWD HOLE LOCATION C/T THE -6 BEAM INBOARD SURFACE.

Part: ACTUATOR — LEAKING (NR 4 SPOILER) · airframe 51,235 hrs · 30,640 cycles

NR 4 FLIGHT SPOILER LEAKED. REMOVED AND REPLACED ACTUATOR PER AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,235 hrs · 30,640 cycles

LEFT WING NR 1 SLAT SKIN CRACKED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,235 hrs · 30,640 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 3 SLAT PER AMM.

Part: SLAT — CRACKED (RT WING) · airframe 51,235 hrs · 30,640 cycles

RIGHT WING NR 8 SLAT CRACKED. REMOVED AND REPLACED NR 8 SLAT PER M/M.

Part: SLAT — CRACKED (RT WING) · airframe 51,235 hrs · 30,640 cycles

RIGHT WING NR 6 SLAT CRACKED. REMOVED AND REPLACED NR 6 SLAT ASSY PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,788 hrs · 29,787 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SOPM.

Part: CHARGER — FAILED (CABIN) · airframe 49,018 hrs · 29,324 cycles

DURING SCHEDULED HC1 CHECK, BATTERIES AT LOCATION M1669 FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — FAILED (CABIN) · airframe 49,018 hrs · 29,324 cycles

DURING SCHDEULED HC1 CHECK, BATTERIES AT LOCATION M1675 FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 48,671 hrs · 29,114 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 36,407 hrs · 21,761 cycles

INFLIGHT SHUTDOWN/AIR TURNBACK/DECLARED EMERGENCY. PRECAUTIONARY RETURN FOR LOW OIL QUANTITY AND PRESSURE INDICATION IN NR 2 ENGINE. ADDED OIL TO NR 2 ENGINE PER BOEING FTD AND SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,292 hrs · 25,955 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EVAC SLIDE LIGHT INOP. RELAMPED PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 951 TO BS 995. REPAIRED BEAM PER SRM & EA.

Part: ANGLE — CORRODED (COCKPIT) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND COCKPIT FLOOR PANEL ANGLE CORRODED AT BS 270, RBL 10 TO LBL 7. REPAIRED ANGLE PER EA.

Part: LIGHT — WORN (CABIN) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS STRIPS WORN. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: COVER — CRACKED (L1 DOOR) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,055 hrs · 25,812 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,055 hrs · 25,812 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,227 hrs · 25,335 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 9 TO ROW 11. REMOVED AND REPLACED BATTERY PER MM.

Part: CABLE — OUT OF POSITION (EVAC SLIDE) · airframe 41,729 hrs · 24,645 cycles

L1 DOOR EVAC SLIDE DEPLOY CABLE OUT POSITION. REPOSITIONED CABLE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,772 hrs · 25,051 cycles

FWD EMERGENCY FLASH LIGHT BATTERY INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 40,445 hrs · 24,233 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,673 hrs · 21,917 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,089 hrs · 20,944 cycles

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

Part: TRUNNION — CORRODED (RH WING) · airframe 35,063 hrs · 20,408 cycles

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

Part: TRUNNION — CORRODED (LT WING) · airframe 35,063 hrs · 20,408 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,206 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 33,651 hrs · 20,118 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,931 hrs · 19,694 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,931 hrs · 19,694 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,931 hrs · 19,694 cycles

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

Part: SENSOR — FAULTY (AIRSPEED) · airframe 31,315 hrs · 18,744 cycles

AIRTURN BACK, CLIMBING THRU FL 250, NR 1 IAS DISAGREE LIGHT ILLUMINATED WITH FLUCTUATIONS IN AIRSPEED AND ALTITUDE. REMOVED AND REPLACED ADM SENSOR PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 31,200 hrs · 18,679 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,217 hrs · 17,555 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, AT LBL 5 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,217 hrs · 17,555 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5 TO RBL 43, WL 207. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 26,301 hrs · 15,866 cycles

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

Part: BATTERY — WILL NOT TEST (EMERGENCY LIGHT) · airframe 25,874 hrs · 15,631 cycles

DURING SCHEDULED HC1 CHECK, R1 DOOR, L1 DOOR, L2 DOOR & LT OVERWING HATCH EMERGENCY LIGHTS BATTERIES FAILED TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,133 hrs · 14,096 cycles

DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED OVERWING LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 22,064 hrs · 13,478 cycles

DURING SCHEDULED RON, FOUND EXTERIOR EMERGENCY EXIT GROUND ILLUMINATION LIGHTS WEAK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1,R1,R2 DOORS) · airframe 20,749 hrs · 12,768 cycles

DURING SCHEDULED C4 CHECK, FOUND R1, L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED ALL 3 DOOR EVAC SLIDES PER MM.

Part: LENS — MISSING (CABIN) · airframe 19,795 hrs · 12,261 cycles

EMERGENCY EXIT LIGHT LENS MISSING NEXT TO R2 DOOR. SECURED LIGHT ASSY PER MX NOTE.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 18,543 hrs · 11,545 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,292 hrs · 11,390 cycles

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

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 17,554 hrs · 10,987 cycles

EEPLS LIGHTS AT TWO SECTIONS ILLUMINATED WHEN SWITCH IN AUTO POSITION. RESEATED CONNECTORS AT FWD BATTERY PACKS PER MM.

Part: HYDRAULIC LINE — CRACKED (HYD SYSTEM) · airframe 17,524 hrs · 10,967 cycles

DECLARED EMERGENCY, DURING FLIGHT A-SYSTEM HYDRAULIC QUANTITY IND WENT TO ZERO. FOUND LINE ON HYD MUFFLER CRACKED. REMOVED AND REPLACED HYD LINE, NR 1 ENG HYD PUMP, CASE DRAIN FILTER & A-SYSTEM MAIN FILTER PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 16,920 hrs · 10,628 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11035-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: CASTING — CRACKED (LT/RT WINGS) · airframe 16,060 hrs · 10,128 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH LT/RT WING FLAP CASTING CRACKED (BETWEEN FLAP AND AILERON) OTBD OF OTBD FLAP. REPAIRED CASTINGS PER SWA EA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,602 hrs · 9,874 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW NR 1 AND NR 2. REPAIRED LOOSE CONNECTOR PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 64,871 hrs · 54,448 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (FWD SVC DOOR) · airframe 13,268 hrs · 8,572 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SMOKE — DETECTED (CABIN) · airframe 12,521 hrs · 8,139 cycles

(DECLARED EMERGENCY) STRONG SMELL OF ELECTRICAL FIRE AND SOME SMOKE (ALTHOUGH LIMITED AS REPORTED BY FLIGHT ATTENDANT) UNKNOWN SOURCE. INSP OVERHEAD CABIN (DROPPED PANELS). REMOVED AND REPLACED BOTH PACK COALESCER BAGS, CHECKED CHIP DETECTORS BOTH ENG (LEAK CK OK ). REMOVED AND REPLACED RECIRC FILTER, INSP DISTRIBUTION BAY, INSP GASPER AND RECIRC FANS, CHECKED ALL CABIN LIGHTS AND EMERG LIGHTS AND INSP GALLEYS. NO DECREPANCIES FOUND, ODOR HAS DISSIPATED AND NO SMOKE EVIDENT, ALL CK'S PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,493 hrs · 8,116 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 1, 7, 18, 19, 20, & 23. R&R COVERS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 10,446 hrs · 6,870 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND LT & RT ELEVATOR TABS LOOSE AT INBD HINGES. R&R ELEVATOR TAB BUSHINGS & HARDWARE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,438 hrs · 6,860 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT FWD SECTION. RELAMPED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 10,075 hrs · 6,634 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,307 hrs · 4,903 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROWS 7,12, 20 AND 22. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: HOOK — LOOSE (SLIDE)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: FUSE — FAILED (NLG WW)

AFTER LANDING GEAR EXTENSION, NLG RED LIGHT ILLUMINATED. C/W QRH AND EXTENDED GEAR NORMALLY. REMOVED AND REPLACED NLG HYD FUSE AND NLG DOWN LOCK ACTUATOR PER MM.

Part: NLG — MALFUNCTIONED (NOSE)

NLG WOULD NOT EXTEND, USED MANUAL EXTENSION PER QRH. BLED NLG EXTENSION RATE FUSE PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED PER MM.

Part: MANIFOLD — FAILED (NLG)

DECLARED EMERGENCY, NLG WOULD NOT EXTEND. MANUAL EXTENSION PROCEDURES USED. REMOVED AND REPLACED NLG LOCK ACTUATOR RELIEF MODULE PER MM.