N372SW

Part: SENSOR — FAULTY (RT MLG) · airframe 70,340 hrs · 58,195 cycles

AIR TURN BACK, AIR & GND SYS FAILURE. GEAR WOULD NOT RETRACT, TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATED. GEAR WARNING HORN SOUNDED. R & R RT MLG S106 SENSOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,287 hrs · 58,145 cycles

SKIN CRACKED AT BS 912, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,232 hrs · 58,103 cycles

RIGHT EMER AISLE LIGHT INOPERATIVE AT ROW 4. REPAIRED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,232 hrs · 58,103 cycles

RIGHT OVERWING EMER HATCH LIGHT BULB INOPERATIVE. REPAIRED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,232 hrs · 58,103 cycles

LEFT EMER AISLE LIGHTS INOPERATIVE BETWEEN ROW 2 - 6. REPAIRED LIGHT IAW AMM.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 70,232 hrs · 58,103 cycles

AFT CABIN LOWERED CEILING BULLNOSE EMER EXIT LIGHT WIRE BROKEN. REPAIRED LIGHT ASSEMBLY IAW AMM.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 70,232 hrs · 58,103 cycles

AFT BULLNOSE EMER EXIT SIGN LIGHT, ASSEMBLY WIRE BROKEN. REPAIRED SIGN ASSEMBLY IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,232 hrs · 58,103 cycles

RIGHT WING OTBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FORE FLAP IAW MM.

Part: FAIRING — CRACKED (LT WING) · airframe 70,232 hrs · 58,103 cycles

LEFT WING LOWER TE PANEL JUST INBD OF NR 3 FLAP TRACK FAIRING, CRACKED ON UPPER SURFACE. REPAIRED FAIRING IAW SRM.

Part: FITTING — CRACKED (LT WING) · airframe 70,232 hrs · 58,103 cycles

LEFT WING RIB AT WBL 114, STRINGER 2L CRACKED INBD MOST FWD HOLE COMMON TO REAR SPAR CHORD. R & R FITTING IAW DWG & EA.

Part: RIB — CRACKED (LT WING) · airframe 70,232 hrs · 58,103 cycles

LEFT WING WBL 114 RIB UPPER CHORD CRACKED. R & R CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 70,231 hrs · 58,103 cycles

RIGHT WING REAR SPAR, UPPER CHORD CRACKED AT MLG SUPPORT FITTING RSS 224, UPPER INBD. REPAIRED CHORD IAW EA & ER.

Part: SPAR — CRACKED (LT WING) · airframe 70,231 hrs · 58,103 cycles

LEFT WING REAR WING SPAR, UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,231 hrs · 58,103 cycles

SKIN CRACKED AT BS 892, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,232 hrs · 58,103 cycles

AFT VERTICAL CHEM MILL SKIN CRACKED AT BS 907, BETWEEN STRINGER 4R TO 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,232 hrs · 58,103 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 500+15, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,226 hrs · 58,101 cycles

FUSELAGE SKIN CRACKED AT STATION 501B, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,226 hrs · 58,101 cycles

FUSELAGE SKIN CRACKED AT STATION 481, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 70,226 hrs · 58,101 cycles

NUMBER 6 FLIGHT SPOILER PANEL DELAMINATED AT UPPER SURFACE. R & R SPOILER ASSEMBLY IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 70,028 hrs · 57,961 cycles

DIVERSION & DECLARED EMER. FLIGHT ATTENDANTS REPORTED ELEC FUMES IN THE AFT GALLEY. R & R AFT COFFEE MAKER IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 70,028 hrs · 57,961 cycles

DIVERSION & DECLARED EMER. FLIGHT ATTENDANTS REPORTED ELEC FUMES IN THE AFT GALLEY. R & R AFT COFFEE MAKER IAW MM.

Part: SKIN — CRACKED (LT WING) · airframe 69,697 hrs · 57,703 cycles

LEFT WING LOWER SKIN CRACKED ABOVE OTBD PANEL MID SPAR FITTING. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,690 hrs · 57,698 cycles

LEFT WING INBD AFT FLAP TE DELAMINATED. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,367 hrs · 57,431 cycles

R1 DOOR SKIN CUT OUT CRACKED AT BS 244.5, STRINGER 14R, LOWER HINGE. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,367 hrs · 57,431 cycles

SKIN CRACKED AT BS 294.5, STRINGER 14R, STATION 294.5. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 69,367 hrs · 57,431 cycles

RIGHT HORIZONTAL STABILIZER CRACKED JUST FWD OF LOWER AFT SPAR APPROX STAB STATION 97. REPAIRED STABILIZER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,365 hrs · 57,430 cycles

R1 DOOR SKIN LOWER HINGE CUT OUT CRACKED AT BS 294.5, STRINGER 14R. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 69,365 hrs · 57,430 cycles

RIGHT HORIZONTAL STABILIZER CRACKED FWD OF LOWER AFT SPAR, APPROX STABILIZER STATION 97. REPAIRED STABILIZER IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,085 hrs · 57,226 cycles

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

Part: LENS — CRAZED (CABIN) · airframe 68,470 hrs · 56,790 cycles

LEFT FUSELAGE EMER EXIT LIGHT LENS CRAZED. R & R LENS IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 68,470 hrs · 56,790 cycles

RIGHT WING NR 4 SLAT DELAMINATED ON OTBD END. R & R SLAT IAW MM.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 68,445 hrs · 56,775 cycles

AFT CARGO DOOR STIFFENER CRACKED AT A BEAM 12 INCHES AFT OF FWD FRAME. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 68,445 hrs · 56,775 cycles

AFT CARGO DOOR VERTICAL STIFFENER CRACKED AT INNER SKIN ATTACHMENT AFT SIDE OF HANDLE CUT OUT. R & R STIFFENER IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

STRINGER TIE CLIP CRACKED AT BS 360 STRINGER 5L. R & R TIE CLIP IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

LONGITUDINAL FLOORBEAM SEAT TRACK INBD FLANGE CRACKED AT BS 727B RBL 24.8. REPAIRED SEAT TRACK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 500B+4 TO 500B+6, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 500B+4 TO 500B+5, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 373 TO 374, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED AT BS 370, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: PANEL — DELAMINATED (LT MLG WW) · airframe 68,445 hrs · 56,775 cycles

LEFT MAIN WW LOWER FUSELAGE COMPOSITE PANEL CUT OUT DELAMINATED. REPAIRED PANEL IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACK BETWEEN BS 339 TO 381, BETWEEN STRINGER 1 TO 2L. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

INTERCOSTAL CRACKED AT BS 323 RBL 31. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 500A+3 TO 500A+7, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 799 TO 802, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 68,445 hrs · 56,775 cycles

RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, STRINGER 2. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

SKIN CRACKED BETWEEN BS 1009 TO 1011, STRINGER 20L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

FRAME CRACKED AT BS 303, STRINGER 17R. R & R FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

L1 DOOR CUT OUT ANGLE CRACKED AT BS 348.2 STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

AFT GALLEY DOOR FWD OF LOWER HINGE SKIN CUT OUT CRACKED AT BS 951. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

R1 DOOR CUT OUT FWD FRAME ANGLE CORRODED AT STRINGER 17. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

R1 CHORD CORRODED BETWEEN BS 292 TO 328. R & R CHORD IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

MAIN CABIN LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666 RBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

MAIN CABIN LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666 RBL 24.8. REPAIRED CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, LT SIDE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 68,445 hrs · 56,775 cycles

AFT CARGO DOOR AFT END OF CROSSBEAM E, OTBD T CHORD CRACKED. REPAIRED T CHORD IAW CCO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,445 hrs · 56,775 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, RT SIDE. REPAIRED CHORD IAW EA.

Part: LENS — MISSING (CABIN) · airframe 68,205 hrs · 56,583 cycles

RIGHT OVERHEAD BULLNOSE EMER EXIT LIGHT LENS MISSING AT ROW 16. INSTALLED LENS IAW SIP.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 66,776 hrs · 55,547 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOW PRESS INDICATED. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,776 hrs · 55,547 cycles

FUSELAGE SKIN CRACKED AT BS 500+14, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,776 hrs · 55,547 cycles

FUSELAGE SKIN CRACKED AT BS 500+14, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,554 hrs · 55,380 cycles

SKIN CRACKED BETWEEN BS 383.5 TO 385.2, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,554 hrs · 55,380 cycles

FUSELAGE SKIN CRACKED AT BS 727B & 4, STRINGER 1. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,554 hrs · 55,380 cycles

FRAME WEB CRACKED AT BS 291.5, STRINGER 16R. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,554 hrs · 55,380 cycles

FRAME WEB CRACKED AT BS 291.5, STRINGER 16R. REPAIRED WEB IAW ER & EA.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 66,244 hrs · 55,156 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT. R & R SLIDE ASSEMBLY IAW MT.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,102 hrs · 55,056 cycles

RT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FORE FLAP IAW MM.

Part: LUG — BROKEN (RT SPOILER) · airframe 66,094 hrs · 55,050 cycles

RT WING NR 5 GND SPOILER LUG BROKEN. R & R SPOILER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,798 hrs · 54,842 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SEAL DEPRESSOR — CRACKED (LT WING) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SEAL DEPRESSOR ON TRAILING EDGE AT WL 181.15 LT WING. REPLACED SEAL DEPRESSOR ON TRAILING EDGE AT WL 181. 15 LT WING IAW B737-300 SRM 51-10-02 ITEM 8 INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DWG 65-50820.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON BRACKET LOCATED ON BS 312 BETWEEN STRINGER 28L TO STRINGER 27L E/E COMPARMENT. REPLACED BRACKET IAW B737-300 SRM 51-10-02 PAGE 8 ITEM 8 LOCATED ON BS 312 BETWEEN STRINGER 28L TO STRINGER 27L E/E COMPARTMENT.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,123 hrs · 52,869 cycles

DELAMINATION UPPER AND LOWER SKIN ON I/B AFT FLAP LEFT SIDE. REMOVED AND REPLACED AFT FLAP LEFT SIDE I/B IAW AMM 27-51-11.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC ON BS 380 AND STR 9L FWD PAX CABIN. REPLACED TIE CLIP LOC ON BS 380 AND STR 9L FWD PAX CABIN IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK INDICATION FOUND ON THE EXTERNAL FUSELAGE SKIN CHEM-MILLED STEP LOCATED AT THE BS 927+13.5" BELOW STR 21L. REPAIRED EXTERNAL SKIN CHEM-MILLED STEP LOCATED AT THE BS 927+13.5 BELOW STR 21L IAW SRM B737-300 53-00-01-2R-31

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOCATED ON INTERNAL AREA OF THE AFT FAIRING NR 3 RT. REPLACED SUPPORT ANGLE LOCATED ON INTERNAL AREA OF THE AFT FAIRING NR 3 RT WING IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DRAWING

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

SKIN CRACKED AT BS 500+2, STR 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

SKIN CRACKED AT BS 400+14, STR 17L. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC BS 380 AT LEVEL STR 26R E/E COMPARTMENT. REPLACED TIE CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE BS 328+8 AT STR 21L E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOC BS 328+8 AT LEVEL STR 21L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DWG 65-29819.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC BS 380 AT LEVEL STR 21L E/E COMPARTMENT. REPLACED TIE CLIP LOCATED BS 380 AT LEVEL STR 21L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 PAGE 8 ITEM 8 DWG 65-46525.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STIFFENER LOC HORIZONTAL STABILIZER CENTER SECTION LEFT SIDE. REPLACED STIFFENER AND FASTENERS LOCATED HORIZONTAL STABILIZER CENTER SECTION LEFT SIDE IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT CLIP LOC BS 294.5 AT LEVEL STR 23L NOSE WHEEL WELL AREA. REPLACED SUPPORT CLIP LOC BS 294.5 AT LEVEL STR 23L NOSE WHEEL WELL AREA IAW B737-300 SRM 51-10-02 ITEM 8 AND 51-40-02 AND DWG

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE, BS 312+8, STR 21L E/E COMPARTMENT. REPLACED ANGLE LOC BS 312+8 AT LEVEL STR 21L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65-29819.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC BS 380 AT LEVEL STR 20L E/E COMPARTMENT. REPLACED TIE CLIP LOC BS 380 AT LEVEL STR 20L E/E COMPARTMENT IAW B737-300 SRM 5

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC BS 380 AT LEVEL STR 26L E/E COMPARTMENT. REPLACED TIE CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

SKIN CRACKED AT BS 360+16, STR 8L. REPAIRED SKIN IAW EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOC, BS 328 AT STR 21L E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOC BS 328 AT LEVEL STR 21L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DWG

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOC BS 380 AT LEVEL STR 22L E/E COMPARTMENT. REPLACED TIE CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 787 AND STR 24R AFT CARGO COMPARTMENT. REPLACED TIE CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 927 TO 947.5, BBL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (THRUST REVERSER) · airframe 63,123 hrs · 52,869 cycles

CRACK ON RUB STRIP LOCATED ON FWD EDGE OF INBOARD OF INBOARD THRUST REVERSER OF ENGINE NR 1. REPLACED RUB STRIP LOCATED ON FWD EDGE OF INBOARD OF INBOARD THRUST REVERSER OF ENGINE NR 1 IAW SRM B737-300 51-10-02 ITEM 8 AND SRM B737-300 51-40-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 947.5 AND STR 25 R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 947.5 AND STR 25R AFT CARGO COMPARTMENT IAW EO AEM-HC53-605/12R0 AND EA 1-353-21407 R0

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOCATED ON INTERNAL AREA OF ACCESS PANEL 5758L INBOARD SIDE OF ENGINE NR 1. REPLACED SUPPORT ANGLE LOCATED ON INTERNAL AREA OF ACCESS PANEL 5758L INBOARD SIDE OF ENGINE NR 1 IAW B737-300 SRM 51-10-02 M, 51-40-02 AND DRAWING

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

FITTING CRACKED AT BS 727, RBL 45.5. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BSTA 947.5 + 8" BETWEEN STR 24L TO STR 26L OF POTABLE WATER SERVICE AREA AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE PER SRM.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOCATED ACCESS PANEL 9224 R. REPLACED BLADE ASSY LOC ACCESS PANEL 9224R RT HORIZONTAL STABILIZER IAW B737-300 SRM 51-10-02 -0G-0 ITEM 8, SRM 51-0-02-0G-0 AND DRAWING

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BSTA 947.5 +12" AND BETWEEN STR 24L TO STR 26L OF POTABLE WATER SERVICE AREA AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOCATED ON BS 243.7 AT LEVEL OF WL 169.1 RIGHT SIDE IN NOSE WHEEL WELL. REPLACED STIFFENER LOCATED ON BS 243.7 AT LEVEL OF WL 169.1 RIGHT SIDE IN NOSE WHEEL WELL IAW B737-300 SRM 51-10-02 ITEM 8, 51-40-02 AND DRAWING

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CLIP WEB CRACKED AT BS 947.5, STR 25R. REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

LOWER FLANGE FRAME CORRODED AT BS 847, BETWEEN STR 27L TO 27R. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (LT PYLON) · airframe 63,123 hrs · 52,869 cycles

SHOE HORSE FITTING CRACKED AT INTERNAL STRUCTURE ACCESS PANEL 5769L LEFT PYLON. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STIFFENER LOCATED AT STA 727 AND STR 27L AFT CARGO COMPARTMENT. REPLACED STIFFENER LOCATED AT STA 727 AND STR 27L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 AND SRM B737-300 51-10-02 ITEM 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 26R TO 25R. REPAIRED FRAME IAW EO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON BRACKET LOCATED ON WEB AT STA 727A BETWEEN STR 25L TO STR 26L AFT CARGO COMPARTMENT. REPLACED BRACKET PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STIFFENER LOCATED AT STA 727 AND STR 27R AFT CARGO COMPARTMENT. REPLACED STIFFENER LOCATED AT BS 727 AND STR 27R AFT CARGO COMPARTMENT IAW SRM 737-300 51-10-02 PARAGRAFT 8 51-40-02 AND DRAWING

Part: SKATE ANGLE — CRACKED (LT PYLON) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SKATE ANGLE LOCATED ON INTERNAL STRUCTURE OF ACCESS PANEL 5769L OF THE LEFT PYLON. REPLACED SKATE ANGLE LOC ON INTERNAL STRUCTURE OF ACCESS PANEL 5769L OF LEFT PYLON IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DWG

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED AT STA 727A AND STR 26 L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT STA 727A AND STR 26L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 AND DRAWING 65-46595.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 927 AND STR 25R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED ON BS 500C AT LEVEL STR 24R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED ON BS 500C AT LEVEL STR 24R FWD CARGO COMPARTMENT IAW SRM

Part: WEB — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON WEB LOC AT LEVEL OF STR 26R BETWEEN BS 500C TO BS 500B FWD CARGO COMPARTMENT. REPLACED WEB LOC AT LEVEL OF STR 26R BETWEEN BS 500C TO BS 500B FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,123 hrs · 52,869 cycles

DELAMINATION ON UPPER SKIN THE AFT FLAP O/B LEFT WING. REPAIRED UPPER SKIN THE AFT O/B LEFT WING IAW B737-300 SRM 51-70-10-2R-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

LOWER FLANGE FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CORROSION AROUND OF NUT PLATE ON STR 24R BETWEEN BS 500B TO BS 500C FWD CARGO COMPARTMENT. REPAIRED STRINGER 24R BETWEEN BS 500B TO BS 520 FWD CC IAW SRM 53-00-03 REPAIR 1.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON TIE CLIP LOCATED AT STA 727A AND STR 25R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT STA 727A AND STR 25R AFT CARGO COMPARTEMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-46595.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON CLIP LOCATED ON WEB AT BSTA 947.5 AND LEVEL STR 25L AFT CARGO COMPARTMENT. REPLACED CLIP LOC ON WEB AT BS 947.5 AND LEVEL STR 25L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 AND SRM 51-40-02 DWG

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE ON ACCESS PANEL 9503. REPLACED ANGLE OF ACCESS PANEL 9503 IAW B737-300 51-10-02 AND DRAWING

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON CLIP LOCATED AT BS 360 AND STR 8L, FWD ENTRY DOOR SURROUND STRUCTURE. REPLACED CLIP LOCATED AT BS 360 AND STR 8L FWD ENTRY DOOR SURROUND STRUCTURE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON CLIP LOCATED AT BS 360 AND STR 11L, FWD ENTRY DOOR SURROUND STRUCTURE. REPLACED CLIP LOCATED AT BS 360 AND STR 11L, FWD ENTRY DOOR SURROUND STUCTURE IAW B737-300 SRM

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 344 TO BS 360 AND LBL 10 OF UPPER AREA E/E COMPARTMENT. REPLACED ANGLE PER SRM.

Part: DOUBLER — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

CRACK INDICATION FOUND ALONG DOUBLER EDGE ON RIGHT SIDE OF NLG WHEEL WELL WEB LOC BS 259.5 BETWEEN WL 169.1 AND WL 185. REPAIRED AREA BETWEEN BS 232 TO BS 261 AND WL 166 TO WL 188 RIGHT SIDE OF NOSE WHEEL WELL IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOCATED ON WS 537.806 AILERON RT WING. REPLACED ANGLE LOCATED ON WS 537.806 AILERON RT WING IAW B737-300 SRM 51-10-02 ITEM 8 AND 51-40-02 AND DRAWING 65-46460.

Part: WEB — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

RT SIDE NLG W/W WEB CRACKED AROUND FASTENER HEAD AT BS 243.7+2.5 AND WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

CRACK INDICATION FOUND AROUND FASTENER HEAD ON LT SIDE NLG WHEEL WELL WEB LOCATED BS 243.7+3.5 INCH AND WL 169.1. REPAIRED LT SIDE NOSE LANDING GEAR WHEEL WELL WEB LOCATED BS 232.8 TO BS 254.6 AND BETWEEN WL 188 TO WL 166.1 IAW B737-300 SRM 53-10-14.

Part: WEB — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

RIGHT SIDE OF NOSE W/W CRACKED AT BS 259.5, WL 177. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOWER AREA OF AFT ENTRY DOOR. REPLACED ANGLE LOWER AREA OF AFT ENTRY DOOR IAW B737-300 SRM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STOP FITTING PAD LOCATED ON CUTOUT 3 (EA) ON EMERGENCY EXIT HATCH RIGHT SIDE. REMOVED AND REPLACED STOP FITTING PAD LOCATED ON CUTOUT 3 (EA) ON EMERGENCY EXIT HATCH RIGHT SIDE IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EO.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 63,123 hrs · 52,869 cycles

FRAYED ESCAPE SLIDE LATCH CABLE LOCATED ON AFT SERVICE GALLEY DOOR. REPLACED ESCAPE SLIDE LATCH CABLE LOCATED PER MM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STOP PAD (3EA) ON CUTOUT AT EMERGENCY EXIT HATCH LT SIDE. REMOVED AND REPLACED STOP PAD (3EA) ON CUTOUT AT EMERGENCY EXIT HATCH LEFT SIDE IAW SRM 51-10-02.

Part: WEB — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

RIGHT SIDE OF NOSE W/W CRACKED AT BS 259.5, WL 177. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 63,123 hrs · 52,869 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 727 AND RBL 12 INTERNAL AREA MAIN WHEEL WELL RT SIDE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 727 AND RBL 12 INTERNAL AREA MAIN WHEEL RII SIDE IAW SRM

Part: WEB — CRACKED (NLG WW) · airframe 63,123 hrs · 52,869 cycles

CRACK LOCATED ON BS 259.5 AT LEVEL WL 177 RIGHT SIDE OF NOSE WHEEL WELL. REPAIRED AREA BETWEEN BS 232 TO BS 261 AND WL 166 TO WL 188 RIGHT SIDE OF NOSE WHEEL WELL IAW B737-300 SRM 53-10-14 REPAIR 2 FIG 205.

Part: ANGLE — CRACKED (GALLEY DOOR) · airframe 63,123 hrs · 52,869 cycles

CRACK ON ANGLE LOWER AREA OF AFT GALLEY DOOR. REPLACED ANGLE LOC ON LOWER AREA OF AFT GALLEY DOOR IAW SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 63,123 hrs · 52,869 cycles

CRACK ON AFT EDGE FRAME OF FWD GALLEY DOOR. REPLACED EDGE FRAME OF FWD GALLEY DOOR IAW SRM B737-300 51-10-02 ITEM 8 AND INSTALLED IAW SRM B737-300 51-40-02 AND DRAWING

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666.5, RBL 24.8 IN CENTER WING. REPAIRED PER EA AND ATS ER.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 63,123 hrs · 52,869 cycles

FRAYED ESCAPE SLIDE LATCH CABLE LOCATED ON AFT ENTRY DOOR. REMOVED AND REPLACED ESCAPE SLIDE LATCH CABLE PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,123 hrs · 52,869 cycles

CRACK ON STRAP LOCATED BETWEEN BS 727C TO BS 727D AND STR 26R AFT CARGO COMPARTMENT. REPLACED STRAP (CAPSTRIP) LOCATED BETWEEN BS 727 AND BS 727D+3" STR 26R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,032 hrs · 52,069 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED & REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,032 hrs · 52,069 cycles

FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,032 hrs · 52,069 cycles

FUSELAGE SKIN CRACKED AT FWD LEFT CORNER OF CONDITION AIR DOOR CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,032 hrs · 52,069 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 485 TO BS 486, STR 1R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,032 hrs · 52,069 cycles

SKIN CRACKED BETWEEN BS 727B+14 TO BS 727B+15.5, STR 2R. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 61,862 hrs · 51,947 cycles

LEFT WING NR 1 SLAT DELAMINATED UPPER I/B SURFACE. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 61,862 hrs · 51,947 cycles

LEFT WING NR 3 SLAT DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER M/M.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,862 hrs · 51,947 cycles

LEFT WING NR 2 SLAT TRAILING EDGE WEDGE DELAMINATED AT O/B END. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 61,862 hrs · 51,947 cycles

LEFT WING NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 61,862 hrs · 51,947 cycles

R1 DOOR LOWER FRAME CRACKED AFT LOWER CORNER. REMOVED AND REPLACED R1 DOOR PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,476 hrs · 51,639 cycles

SKIN CRACKED AT BS 927 + 4, STR 24L. REPAIRED SKIN PER SRM.

Part: LUG — BROKEN (RT WING SPOILER) · airframe 61,399 hrs · 51,577 cycles

RIGHT WING I/B GROUND SPOILER BOARD LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 61,193 hrs · 51,424 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSTIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,987 hrs · 51,269 cycles

FUSELAGE SKIN CRACKED AT BS 344+1, STR 2L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 60,540 hrs · 50,938 cycles

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

Part: HOUSING — DEFECTIVE (CABIN) · airframe 58,868 hrs · 49,663 cycles

AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,453 hrs · 49,328 cycles

DURING SCHEDULED HC2 CHECK, FOUND, SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 727D, LBL 2. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND CRACK AT STA 957, WL 211 IN HOLE FOR L2 DOOR CUTOUT STUB FRAME. REPAIRED PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EXTERNAL EMERGENCY EXIT LIGHT BY TRAILING EDGE FLAP INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LAMP PER MM.

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHT) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT GROUND WIRE BROKEN. REPAIRED LIGHT ASSY PER MM.

Part: HOUSING — CRACKED (EXIT SIGN) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EMERGENCY EXIT SIGN HOUSING CRACKED. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 979 TO BS 982, STR 21L. REPAIRED SKIN PER SRM AND BAC DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR LOWER AFT CORNER SKIN CRACKED AT STA 328.5. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME DOUBLER CRACKED AT BS 492, STR 25R. REPAIRED DOUBLER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FORWARD CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 664, RBL 24.5. REPAIRED CHORD PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND BULKHEAD UPPER CHORD CRACKED AT BS 178, LBL 24.1. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT O/B FLOOR WEB CRACKED BETWEEN BS 178 TO BS 188, WL 208. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LEFT O/B FLOOR WEB CRACKED BETWEEN BS 178 TO BS 188, WL 208. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND CRACKED STRINGER CLIP AT STA 360 STR 8R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT S 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT S 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEDGE — PUNCTURED (MIDFLAP) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SURFACE PUNCTURED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 813 TO BS 814, STR 4R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,852 hrs · 48,868 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 960 TO BS 964, STR 21L. REPAIRED SKIN PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,723 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,723 hrs · 48,774 cycles

DURING SCHEDULED OTS CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,723 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 515C, STR 4R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,723 hrs · 48,774 cycles

DURING SCHEDULED OTS CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,723 hrs · 48,774 cycles

DURING SCHEDULED OTS CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 21. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,838 hrs · 48,107 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 415, STR 1. REPAIRED SKIN PER EA.

Part: MOUNT — BROKEN (EVAC SLIDE) · airframe 56,838 hrs · 48,107 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR AFT SLIDE MOUNT BRACKET BROKEN. R&R MOUNT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,838 hrs · 48,107 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 767, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,571 hrs · 47,909 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 501.4C, STR 10L. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 56,719 hrs · 48,019 cycles

REPORTED ELECTRICAL SMELL AT MID CABIN. SECURED GASPER & RECIRC FANS, AND ENTRY/ CEILING/ WINDOW LIGHTS PER QRH. SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 502.4 TO BS 504, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 501C TO BS 506C, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 501.4C TO BS 508C, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 504B TO BS 506B, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 503.5B TO BS 503B, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,570 hrs · 47,908 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 391.5 TO BS 397.5, STR 10L. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 56,484 hrs · 47,837 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,964 hrs · 47,423 cycles

DURING SCHEDULED CV CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,964 hrs · 47,423 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 425, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 423, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 415, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500C.4, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D.4, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 912, STR 23R. REPAIRED SKIN PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT EEPLS DAMAGED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — WORN (CABIN) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT EEPLS WORN. REMOVED AND REPLACED EEPLS PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 55,310 hrs · 46,930 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,228 hrs · 46,866 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO PIT DOOR CUTOUT LOWER SILL WEB UPPER STRAP CRACKED BETWEEN BS 837 TO BS 847. REPAIRED STRAP PER SRM.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 55,228 hrs · 46,866 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO PIT, AFT SIDE DOOR CUTOUT FRAME CRACKED AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED FRAME PER ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,228 hrs · 46,866 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING L/E NR 6 SLAT SKIN I/B LOWER SURFACE CRACKED. REPAIRED SLAT SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,228 hrs · 46,866 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT WING L/E NR 3 SLAT LOWER SURFACE CRACKED. REPAIRED NR 3 SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,111 hrs · 46,783 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 516D, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,111 hrs · 46,783 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 516D, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,111 hrs · 46,783 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,111 hrs · 46,783 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510D, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 54,206 hrs · 46,111 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,828 hrs · 45,834 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 501, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,828 hrs · 45,834 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 53,396 hrs · 45,503 cycles

DIVERSION / DECLARED EMERGENCY. PASSING FL 31.7 CABIN PRESSURIZATION WARNING HORN SOUNDED. CABIN ALT WAS 10,000FT. EMERGENCY DESCENT TO 10,000FT. PRESSURE STABILIZED. REMOVED AND REPLACED PRESSURE CONTROL PANEL. REMOVED AND REPLACED NR 1 ENG PNEU BLEED HIGH STAGE VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,230 hrs · 45,384 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 12. RELAMPED PER MM.

Part: HOUSING — DEFECTIVE (FLASHLIGHT) · airframe 52,693 hrs · 45,245 cycles

LT FWD FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 303, STR 16L. REMOVED AND REPLACED FRAME PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, BETWEEN WL 256 TO WL 258. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN FLOORBEAM CORRODED AT BS 947, BL 0. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 9, WL 234. REPAIRED WEB PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 52,644 hrs · 44,955 cycles

DURING SCHEDULED 16Y CHECK, FOUND GIRT BAR ATTACH CHANNEL CORRODED AT FLOORBEAM, BS 344, LBL 62. REMOVED AND REPLACED CHANNEL PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,440 hrs · 44,803 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,440 hrs · 44,803 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 970, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,440 hrs · 44,803 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,440 hrs · 44,803 cycles

DURING SCHEDULED HC2 CHECK, FOUND FRAME CRACKED AT 727D, BL 0. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,440 hrs · 44,803 cycles

DURING SCHEDULED HC2 CHECK, FOUND ANTENNA DOUBLER BELLY SKIN CRACKED BETWEEN BS 727E TO BS 727E. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 52,362 hrs · 44,743 cycles

LT EEPLS LOOSE BETWEEN ROW 7 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,297 hrs · 44,693 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,095 hrs · 43,847 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 178 BULKHEAD) · airframe 51,095 hrs · 43,847 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1. REPAIRED WEB PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 178 BULKHEAD) · airframe 51,095 hrs · 43,847 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. REPAIRED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,504 hrs · 43,386 cycles

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

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,313 hrs · 43,235 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE LUG FITTING CORRODED AT BS RT 685. REPAIRED LUG PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 50,313 hrs · 43,235 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG BEAM CORRODED AT INBOARD FITTING. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,225 hrs · 43,178 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 50,026 hrs · 43,059 cycles

WHEN SELECTING FLAPS TO 5 DEGREES DURING APPROACH A DEFINITE FLUTTER IS FELT, AND AT CRUISE A RAPID YAWING WAS NOTED. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR PER MM.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 50,026 hrs · 43,059 cycles

WHEN SELECTING FLAPS TO 5 DEGREES DURING APPROACH A DEFINITE FLUTTER IS FELT, AND AT CRUISE A RAPID YAWING WAS NOTED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR PER MM.

Part: AILERON — DEBONDED (LT WING) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING AILERON OUTBOARD T/E DISBONDED. REPAIRED AILERON PER SRM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING AILERON TAB DELAMINATED AT UPPER SURFACE T/E. REMOVED AND REPLACED TAB PER MM.

Part: BEARING — WORN (RT AILERON) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 520 TO RT BS 540. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 344 TO LT BS 440. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 520 TO LT BS 540. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 639 TO LT BS 706. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 747 TO RT BS 827. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 400 TO RT BS 440. REMOVED AND REPLACED STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,025 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,025 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,025 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,075 hrs · 42,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: BEARING — WORN (AILERON TAB) · airframe 48,820 hrs · 42,119 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING AILERON TAB INBOARD HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 1 BEARING PER MM.

Part: SKIN — DELAMINATED (NR 4 SPOILER) · airframe 48,820 hrs · 42,119 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 GROUND SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 947 S24L) · airframe 48,338 hrs · 41,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 947 S25R) · airframe 48,338 hrs · 41,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 47,864 hrs · 41,367 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,864 hrs · 41,367 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 47,864 hrs · 41,367 cycles

DURING SCHEDULED C1 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 46,979 hrs · 40,660 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT NR 4 L/E SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 46,979 hrs · 40,660 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT NR 5 L/E SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SKIN — CRACKED (BS 450 S1) · airframe 46,263 hrs · 40,088 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 430 S1) · airframe 46,263 hrs · 40,088 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, STR 1. REPAIRED SKIN PER EA.

Part: BULKHEAD — CRACKED (BS 178) · airframe 46,252 hrs · 40,081 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7, WL 207. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 46,252 hrs · 40,081 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 12, WL 218. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,251 hrs · 40,080 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 45,992 hrs · 39,889 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMIESCENT STRIP MISSING AT ROW 7 ABC. INSTALLED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 45,992 hrs · 39,889 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT INBOARD AFT CORNER. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (BS 510D S11L) · airframe 45,930 hrs · 39,846 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 11L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 45,788 hrs · 39,731 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 44,997 hrs · 39,113 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BOLT — WORN (TAB HINGE) · airframe 44,879 hrs · 39,006 cycles

DURING SCHEDULED MV2 CHECK, RT ELEVATOR TAB FAILS FREE PLAY CHECK. REMOVED AND REPLACED RIGHT NR 1 TAB HINGE BOLT IAW MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 44,589 hrs · 38,794 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: ACTUATOR — SHEARED (SPOILERS) · airframe 44,214 hrs · 38,489 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 9 GROUND SPOILER OUTBOARD ACTUATOR ROD END SHEARED OFF. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,641 hrs · 36,547 cycles

CABIN AFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOP. RECHARGED BATTERY PACKS PER MM.

Part: WEB — CRACKED (BS 663.75) · airframe 41,224 hrs · 36,220 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663.75, RBL 39. REPAIRED BEADED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,224 hrs · 36,220 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 328 R1 DOOR CUTOUT FUSELAGE FRAME CRACKED AT NR 4 STOP FITTING. REPAIRED FRAME PER SRM.

Part: TIRE — BLOWN (NLG) · airframe 40,224 hrs · 35,377 cycles

DECLARED EMERGENCY. LEFT NLG TIRE BLOWN ON T/O. FOUND NLG W/W FWD BULKHEAD & LOWER TCAS ANTENNA DAMAGED. REPAIRED NLG W/W BULKHEAD PER SWA EA. REMOVED AND REPLACED TCAS ANTENNA PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,208 hrs · 35,365 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 21 ABC. RELAMPED EMERGENCY LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,736 hrs · 34,970 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE WEB CRACKS AT BS 178 BLKHD, BETWEEN WL 213 TO WL 214 & BETWEEN LBL 6.7 TO RBL 4.7. REPAIRED FUSELAGE WEB PER SRM.

Part: BOLT — WORN (LT ELEVATOR) · airframe 39,372 hrs · 34,667 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT TAB HARDWARE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,372 hrs · 34,667 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 38,700 hrs · 34,161 cycles

DECLARED EMERGENCY, WHEN LOWERING LANDING GEAR, RT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR, STILL UNSAFE. MANUAL GEAR EXTENSION OK. REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (RT MLG) · airframe 38,636 hrs · 34,112 cycles

RT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR LOWERED FOR LANDING. RECYCLED GEAR, NO CHANGE. USED MANUAL GEAR EXTENSION, NORMAL LANDING. ADJUSTED RT MLG DOWNLOCK SENSOR PER MM.

Part: WARNING LIGHT — FALSE INDICATION (MLG) · airframe 38,550 hrs · 34,049 cycles

RIGHT MLG UNSAFE LIGHT INDICATION DURING GEAR EXTENSION. RECYCLED GEARS AND GREEN LIGHTS ILLUMINATED. INSPECTED MLG POSITION SENSOR. NO DEFECT NOTED. MLG OPS CK GOOD PER MM

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,455 hrs · 33,981 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,455 hrs · 33,981 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,206 hrs · 33,773 cycles

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

Part: COVER — DAMAGED (ROW 8 ABC) · airframe 37,515 hrs · 33,202 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LIGHT COVER AT ROW 8 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,515 hrs · 33,202 cycles

DURING SCHEDULED C2 CHECK, FOUND COCKPIT WINDOW POST SKIN BETWEEN L1 AND L2 WINDOWS UPPER CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,647 hrs · 32,530 cycles

DURING SCHEDULED C1 CHECK, FOUND EQUIPMENT COOLING DUCT EXHAUST CUT OUT SKIN CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,787 hrs · 31,052 cycles

DURING SCHEDULED C3 CHECK, FOUND .5 INCH LONG CRACK AT FUSELAGE SKIN, LOWER FWD CORNER OF AFT ENTRY DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 34,412 hrs · 30,734 cycles

AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT UPPER EMERGENCY FLASHLIGHT PER MM.

Part: RIB — CRACKED (LH WING) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND LH WING UPPER RIB CHORD CRACKED AT STA 114, STR 2. REPAIRED UPPER RIB CHORD PER BFG ER.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 927, WL 160, RT. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, WL 208, LBL 35 TO RBL 22. REPAIRED FLOORBEAM PER SRM.

Part: BRACKET — CORRODED (CABIN FLOOR) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE BIRT BAR ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 360, BETWEEN STRINGERS 8R AND 9R AND BETWEEN STRINGERS 13L AND 14L, AND BS 440, BETWEEN STRINGERS 8R AND 9R. REPAIRED FRAME SECTIONS PER ER AND SRM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208, RBL 1. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO COMPT) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 747, WL 150, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED, BS 867 TO BS 887, WL 208, LBL 65. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, WL 161 AND RBL 19 TO RBL 28. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 188, STR 17L & STR 17R. R&R FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663 AT STR 10R AND BS 706 AT STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: BRACKET — SHEARED (FWD SVC DOOR) · airframe 31,972 hrs · 28,754 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK BRACKET HAS 1 ATTACH RIVET SHEARED. REMOVED AND REPLACED RIVET PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 31,139 hrs · 28,066 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS WORN BETWEEN ROW'S NR 7 AND NR 9. REMOVED AND REPLACED EEPLS BETWEEN ROW'S NR 7 AND NR 9.

Part: HOOK — LOOSE (FWD SVC DOOR) · airframe 28,392 hrs · 25,869 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,757 hrs · 24,478 cycles

EXTERNAL FUSELAGE SKIN DAMAGED BY GROUND EQUIPMENT, BS 346 TO 382, WL 158 TO 172 RT. MX FERRY TO DAL AND REPAIRED SKIN PER SWA RA.

Part: LENS — MISSING (CABIN) · airframe 26,625 hrs · 24,368 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: TRANSMITTER — ERRATIC (RT WING TE FLAP) · airframe 25,859 hrs · 23,763 cycles

DECLARED EMERGENCY, T/E FLAP INDICATORS ERRATIC. REMOVED AND REPLACED FLAP INDICATOR (P/N 2061-14-1) & FLAP POS TRANSMITTER PER MM. OPS CHECK GOOD PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,571 hrs · 23,531 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 494, RBL 22. REPAIRED FRAME PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 23,314 hrs · 21,636 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,278 hrs · 21,600 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED LOOSE WIRES AT ROW 9, OPS CHECK GOOD PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND 4 EEPLS LIGHTS INOP. RECONNECTED WIRING PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT EEPLS INOP. RECONNECTED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (R1 DOORWAY)

DURING SCHEDULED BC2 CHECK, FOUND RI DOOR FRAME UPPER FWD FITTING CRACKED. REPLACED FITTING PER SRM.

Part: STOP — CRACKED (OVERWING DOOR)

DURING SCHEDULED BC2 CHECK, FOUND RT OVERWING EXIT FRAME UPPER AFT STOP PAD CRACKED. REPLACED STOP PAD PER MM.

Part: WIRE — LOOSE (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND SEVERAL FLOOR TRACK LIGHTS INOP. REATTACHED LOOSE WIRING AND OPS CHECKED PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 987, RBL 35 AROUND FLOORBOARD SCREW HOLE, BS 987 FASTENER HOLE TOP FWD SIDE RBL 39 AND BS 987 FASTENER HOLE TOP FWD SIDE RBL 42.5. REPAIRED PER SWA RA 1-353-1830.

Part: ANGLE — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FWD GALLEY DOOR ENTRY Z-ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM HOLES AT BS 312, BL 0 AND BS 344, RBL 1. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FWD BULKHEAD ATTACH ANGLE AT BS 727, RBL 4. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 530)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RT RAM AIR DUCT SUPPORT LOWER Z-ANGLE AND HAS A HOLE AT BS 530. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 294)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FWD GALLEY DOOR ENTRY Z-ANGLE STRAP AT BS 294, RBL 55. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 530)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RT RAM AIR DUCT SUPPORT WEB ANGLE AT BS 530. REMOVED AND REPLACED PER BOEING SRM.