N554WN

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,942 hrs · 34,439 cycles

FWD SERVICE DOOR SLIDE NOT SECURE IN SLIDE CONTAINER. REPOSITIONED & REINSTALLED FS DOOR SLIDE, PER MT 725-61-06 STEPS 3B; 3C; 3G & 3I-3K.

Part: COVER — OUT OF POSITION (EMERGENCY LIGHT) · airframe 60,420 hrs · 34,123 cycles

AFT R/H EMER EXIT SIGN BACKWARDS. / R&R AFT R/H EMERGENCY EXIT LIGHT COVER PER AMM 33-51-01.

Part: BATTERY — FAULTY (MEGAPHONE) · airframe 60,413 hrs · 34,120 cycles

FWD MEGAPHONE INTERMITTENT / R&R BATTERIES ON MEGAPHONE PER AMM 25-64-00

Part: BATTERY — NO TEST (EMEGENCY LIGHTS) · airframe 60,412 hrs · 34,119 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M02335 / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION M02335 PER AMM 33-51-06

Part: TRUNNION — CORRODED (RT MLG) · airframe 60,412 hrs · 34,119 cycles

RH MLG FWD TRUNION UPPER OB FITTING; OB FACE AND BORE CORRODED / REPAIRED PER EA1-A57-3246; REF D&M ENTERPRISES A/R WORKORDER SSR #1234

Part: TRUNNION — CORRODED (RT MLG) · airframe 60,412 hrs · 34,119 cycles

RH MLG FWD TRUNION LOWER IB FITTING;IB FACE_AND BORE CORRODED. / REPAIRED PER EA1-A57-3246;REF D&M ENTERPRISES A/R WORK ORDER SSR #1234

Part: TRUNNION — CORRODED (RT MLG) · airframe 60,412 hrs · 34,119 cycles

RH MLG FWD TRUNION UPPER IB FITTING; IB FACE AND BORE CORRODED / REPAIRED PER EA1-A57-3246;REF D&M ENTERPRISES A/R WORKORDER SSR# 1234

Part: LVPS — CORRODED (RT MLG) · airframe 60,412 hrs · 34,119 cycles

RH MLG FWD TRUNION LOWER OB FITTING; OB FACE AND BORE CORRODED. / REPAIRED PER EA1-A57-3246;REF D&M ENTERPRISES A/R WORK ORDER SSR#1234

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,338 hrs · 34,073 cycles

EMERGENCY BATTERY PACKS M1675 AND M1673 INOP REMOVED AND REPLACED EMER BATT PACK M1673 AND EMER BATT PACK + POWER SUPPLY M1675 IAW AMM 33-51-06-960-805, AMM 33-51-06-960-806. PERFORMED EMERGENCY LIGHTS OPS CHECK FOR M1675 AND M1673, CHECKS GOOD IAW AMM 33-51-06-960-806 STEP 5.E.4 AND AMM 33-51-06-960-805 STEP 4.D.5

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,338 hrs · 34,073 cycles

EMERGENCY BATTERY PACKS M1675 AND M1673 INOP REMOVED AND REPLACED EMER BATT PACK M1673 AND EMER BATT PACK + POWER SUPPLY M1675 IAW AMM 33-51-06-960-805, AMM 33-51-06-960-806. PERFORMED EMERGENCY LIGHTS OPS CHECK FOR M1675 AND M1673, CHECKS GOOD IAW AMM 33-51-06-960-806 STEP 5.E.4 AND AMM 33-51-06-960-805 STEP 4.D.5

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,338 hrs · 34,073 cycles

EMERGENCY BATTERY PACKS M1675 AND M1673 INOP / REMOVED AND REPLACED EMER BATT PACK M1673 AND EMER BATT PACK + POWER SUPPLY M1675 IAW AMM 33-51-06-960-805; AMM 33-51-06-960-806. PERFORMED EMERGENCY LIGHTS OPS CHECK FOR M1675 AND M1673; CHECKS GOOD IAW AMM 33-51-06-960-806 STEP 5.E.4 AND AMM 33-51-06-960-805 STEP 4.D.5

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

SHEAR WEB STIFFENER IS DAMAGED @ STA. 986-1006 RBL 47, WL 208 REMOVED AND REPLACED SHEAR WEB STIFFENER IAW SRM 51-40-02-0G-0 AND DWG 147A0000

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

SHEAR WEB CRACKED RBL 20 STA 1009 WL 208 REMOVED AND REPLACED SHEAR WEB RBL 20 STA 1009 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5730, DWG 147A0000

Part: FLAP TRACK — CORRODED (L/H WING) · airframe 60,338 hrs · 34,073 cycles

L/H I/B AFT FLAP O/B TRACK HAS PITTING ON I/B LOWER RACE / REMOVED AND REPLACED L/H I/B AFT FLAP O/B TRACK IAW AMM 27-51-16 57613U 3-5-20

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** ON FLOOR BEAM STA 986.5, RBL 45, WL 208 REMOVED AND REPAIRED DAMAGED SECTION OF FS 986.5 FLOOR BEAM DUE TO OUT OF LIMITS CORRISION IAW SRM 53-70-51-2R-4.

Part: STRAP — CORRODED (AFT CARGO) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** FOUND ON STR 21R; B.S. 986 W.L. 196 STRAP / CORROSION ON STRAP STR 21R BS 986 WL 196 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED STRAP I.A.W. SRM 51-40-02-0G-0. FABRICATED NEW REPLACEMENT STRAP FROM 7075T6 0.063 I.A.W. BOEING DWG 147A8801 REV: M; INSTALLED REPLACEMENT STRAP I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 147A8801. REV:-.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT FROM STA 727 - 787, RBL 22, WL 155 REMOVED AND REPLACED AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT PO# 773423 P/N 146A7502-2 IN REFERENCE WITH BDW# 146A7500 REV B AND 146A7502 REV A, ALSO SRM 51-40-02-0G-0

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727 - 847, LBL 22, WL 155 REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727-847, LBL 22, WL 155 PER SRM 51-40-02-0G-0 AND DWG# 146A7500 57903U 03MAR20

Part: SHIELD — CORRODED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** AFT CARGO BAY SHIELD FWD OF CARGO BAY DOOR FROM STA 787 - 807, RBL 22, WL 155 CORROSION ON AFT CARGO BAY SHIELD FWD OF CARGO BAY DOOR STA 787-807, RBL 22, WL 155 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED WITH NEW SHIELD P.O# 777813 IAW SRM 51-40-02-0G-0 DRG# 146A0081. 57309U 3/3/20

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 60,338 hrs · 34,073 cycles

PAX CABIN FLOOR PANEL 232BF UPPER SURFACE DAMAGED REPAIRED UPPER SURFACE DAMAGED ON PAX CABIN FLOOR PANEL 232BF IAW 737 SRM 53-00-50-2R-0 AND SRM 53-00-50-2R-1. DETERMINED DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW 737 SRM 53-00-50-1A-1 PARA 4E(2)(C)(1). 59606U 27FEB20.

Part: MOUNT — CORRODED (NR 2 VHF ANTENNA) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** FUSELAGE SKIN UNDER VHF #2 ANTENNA BASE HAS CORROSION. BS 727D+5 - 14; WL 148; BL 0 / REPAIRED #2 VHF ANTENNA MOUNT ADAPTER PLATE; BS 727D+10 BL 0. PER ATS ER 20-02040 REV IR AND SWA EA 1-753-36683 REV IR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

***CORROSION*** ON STRINGER AT STA540, STR 23 LEFT (STA540,LBL45,WL159) CORROSION ON STR 23L BS 540 LBL 45 WL 159 FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-03-1A-1 FIG 103 PAGE 8. REMOVED STR 23L I.A.W. SRM 51-40-02-0G-0. STA 515 TO 540. INSTALLED REPLACEMENT STR AND SPLICE I.A.W. SRM 53-00-03-2R-1 REPAIR 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,338 hrs · 34,073 cycles

CRACKED AND CORRODED STRINGER AT STA540, STR 26 LEFT (STA540,LBL31,WL155) REMOVED SECTION OF DAMAGED STR 26L STA 500D+10 TO 540 FOR REPAIR FABRICATED AND INSTALLED STR AND REPAIR SPLICE IAW SRM 51-40-02-0G-0 AND SRM 53-00-03-2R-1. 57828U 3/9/2020. STRINGER 26L REPLACED AT BS 540 - 500D WL 155 56415R 3/09/20

Part: ATTACH BRACKET — BROKEN (RT WING) · airframe 60,338 hrs · 34,073 cycles

R/H WING AFT ATTACH BRACKET FOR PANEL 661AB IS BROKEN / REMOVED AND REPLACED AFT ATTACH BRACKET FOR PANEL 661AB IAW SRM 51-40-02-0G-0. ADJUSTMENT IS GOOD IAW AMM 27-51-21. 57613U 3-8-20

Part: BULKHEAD WEB — CANNING (BS 1016) · airframe 60,338 hrs · 34,073 cycles

OIL CAN CONDITION EXISTED IN RH AFT PRESSURE WEB AT STA 1016; RBL 50; WL 260. / REPAIR DOUBLER INSTALLED OVER OIL CAN PER OEM SRL REPAIR N1440034592. REF SWA EA 1-753-34894 AND 1-753-34907.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 60,338 hrs · 34,073 cycles

RIGHT WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE IS DELAMINATED / UPON INVESTIGATION DAMAGE ON R/H WING O/B AFT FLAP I/B UPPER SURFACE FOUND TO BE BEYOND ALLOWABLE LIMITS PER SRM 57-53-01-1A-4 PARA 4.A.(5). REMOVED DAMAGE AND REPAIRED AREA IAW SRM 51-70-10-2R-0 PARA 7; PARA 14; PARA 15; PARA 20 AND PARA 22.

Part: RIB — CRACKED (RT WING) · airframe 60,338 hrs · 34,073 cycles

RIGHT WING DEFLECTION RIB CRACKED / REMOVED AND REPLACED RIGHT WING DEFLECTION RIB IAW SOPM 20-50-01 FOR ACCESS REMOVED AND REINSTALL BRACKET AND PULLEYS SPOILER SYSTEM AT RIGHT WING. DEFLECTION RIB AREA IAW AMM 20-10-09-000-801 AND 20-10-09-400-801 ACCOMPLISHED SPOILER CABLES RH WING ADJUSTMENT AND OPS CK IAW AMM 27-61-00-820-801 AND 27-61-00-710-801 ADJ. & OPS CK GOOD.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,338 hrs · 34,073 cycles

LEFT HAND WING OUTBOARD AFT FLAP INBOARD CORNER DELAMINATED UPON EVALUATION OF DELAMINATION TO L/H OTBD AFT FLAP FOUND IT BEYOND ALLOWABLE LIMITS OF B737 SRM 57-53-01-1A-4. REPAIRED I.A.W SRM 57-53-01A-2R-4 AND 51-70-10-2R-4 AND 51-70-10-2R-0

Part: BATTERY — FAULTY (FWD MEGAPHONE) · airframe 60,263 hrs · 34,028 cycles

FORWARD MEGAPHONE DIFFICULT TO HEAR. / R&R MEGAPHONE BATTERIES PER AMM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 59,001 hrs · 33,309 cycles

R1 DOOR SLIDE CONTAINER OPENED AND SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 58,407 hrs · 32,929 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 57,882 hrs · 32,608 cycles

L/H OVERWING EXIT SIGN COVER MISSING. SECURED SIGN LENS PER SIP.

Part: LENS — LOOSE (CABIN) · airframe 56,320 hrs · 31,663 cycles

RT OVERHEAD BIN BULLNOSE PANEL EMERGENCY LIGHT LENS LOOSE AT ROW 19. SECURED LENS PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,320 hrs · 31,663 cycles

EMERGENCY LIGHTS BATTERY PACK M1674 FAILED TO ILLUMINATE. R&R BATTERY PACK IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,320 hrs · 31,663 cycles

RT WING INBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. R&R AFT FLAP IAW AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT "L" BRACKET CRACKED AT BS 500B, LBL 24. R&R "L" BRACKET PER SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 480+15, RBL 26. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS 947.5. R&R SUPPORT PER SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY "L" BRACKET UNDERNEATH LT FLOOR TO SIDEWALL SUPPORT CRACKED AT BS 400, LBL 24. R&R BRACKET IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY AFT BULKHEAD SURROUND STRUCTURE CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R&R ANGLE PER SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT M LG WW) · airframe 56,320 hrs · 31,663 cycles

VERTICAL PRESSURE WEB ATTACH ANGLE CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE IAW ER AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY AFT BULKHEAD SURROUND STRUCTURE CORRODED AT BS 500D, RBL 26. R&R ANGLE PER SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT BRACKET CRACKED AT BS 400, RBL 24. R&R BRACKET IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT "L" BRACKET CRACKED AT BS 500C, LBL 24. R&R L BRACKET IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 500. R&R WEB IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT "L" BRACKET CRACKED AT BS 500B. R&R L BRACKET PER SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CARGO BAY AFT BULKHEAD SURROUND STRUCTURE CORRODED AT BS 500D, LBL 26. R&R ANGLE PER SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO FLOOR PANEL SUPPORT SPLICE CORRODED AT BS 887, RBL 19. R&R SUPPORT SPLICE IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO BAY SHIELD FORWARD OF DOOR CORRODED BETWEEN BS 767 TO BS 787+6, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

AFT CARGO BAY FLOOR SUPPORT CRACKED AT BS 747, RBL 14. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 328+9, LBL 45.5. R&R INTERCOSTAL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 312+9, LBL 45.5. R&R INTERCOSTAL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 344+6, LBL 12. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

ENTRY WAY SCUFF PLATE ANGLE SUPPORT CORRODED BETWEEN BS 344 TO BS 312, LBL 63. R&R SUPPORT IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 277+7, BL 0. R&R INTERCOSTAL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 344+6, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

SCUFF PLATE ANGLE SUPPORT CORRODED BETWEEN BS 312 TO BS 344, LBL 60. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 312+12, RBL 32. R&R INTERCOSTAL IAW DWG.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

FORWARD CABIN HARDPOINT MOUNT CORRODED AT BS 344, LBL 59. R&R HARDPOINT IAW DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

R2 DOOR MOP SILL CORRODED. R&R MOPSILL PER SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 56,320 hrs · 31,663 cycles

VAPOR BARRIER STIFFENER CRACKED AT BS 663, BETWEEN RBL 6.15 TO RBL 31.83. R&R STIFFENER IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 56,320 hrs · 31,663 cycles

VAPOR BARRIER ANGLE CRACKED AT UPPER EDGE AT BS 663, RBL 7. REPAIRED ANGLE PER EA & ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,320 hrs · 31,663 cycles

VAPOR BARRIER VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.3. R&R STIFFENER PER SRM AND DWG.

Part: WEB — CRACKED (LT WING) · airframe 56,320 hrs · 31,663 cycles

LT WING UPPER TRAILING EDGE PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB CRACKED ON FORWARD FLANGE. R&R WEB IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 56,320 hrs · 31,663 cycles

RT WING LOWER SURFACE WIGGLE PLATE CRACKED AT RSS 261. R&R WIGGLE PLATE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,320 hrs · 31,663 cycles

RT WING NR 1 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 54,399 hrs · 30,468 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN LOOSE. R & R THE SIGN IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 53,840 hrs · 30,125 cycles

LT EMERGENCY EXIT BULLNOSE LENS MISSING AT ROW 12. INSTALLED LENS PER SIP.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 53,232 hrs · 29,773 cycles

EMERGENCY LIGHTS OVER DOORS AND BINS FAULTY. R & R THE BATTERY CHARGER IAW AM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 52,244 hrs · 29,144 cycles

RT WING OUTBOARD NR 8 FLIGHT SPOILER ACTUATOR LEAKED. R&R ACTUATOR PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,142 hrs · 29,091 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 52,053 hrs · 29,046 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 50,588 hrs · 28,206 cycles

L1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,014 hrs · 27,886 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,634 hrs · 27,653 cycles

L2 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED THE LIGHT IAW MM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 48,281 hrs · 26,876 cycles

LEFT WING UPPER SHELF PANEL ABOVE PYLON CTR AFT SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LATCH — LOOSE (R2 DOOR) · airframe 48,281 hrs · 26,876 cycles

R2 DOOR EMER EVAC SLIDE LATCH LOOSE. SECURED LATCH IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,164 hrs · 26,260 cycles

RIGHT BULLNOSE EMER EXIT LIGHT INOPERATIVE AT ROW 19. R & R LIGHT IAW AMM.

Part: ENGINE — FAILED (RIGHT) · airframe 45,351 hrs · 25,226 cycles

ABORTED TAKEOFF. AT APPROX 50 KNOT ON TAKEOFF ROLL, NR 2 ENG FAILED. R & R NR 2 ENG IAW MT.

Part: SIGN — MISALIGNED (CABIN) · airframe 44,888 hrs · 24,993 cycles

L1 DOOR EMER EXIT SIGN MISALIGNED. R & R SIGN IAW SIP.

Part: SIGN — MISALIGNED (CABIN) · airframe 44,888 hrs · 24,993 cycles

R1 DOOR EMER EXIT SIGN MISALIGNED. R & R SIGN IAW SIP.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT 2ND TO BOTTOM FASTENER HOLE ALONG THE E-F POST. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

LEFT NR 3 WINDOW FRAME CRACKED AT 2ND TO BOTTOM FASTENER HOLE ALONG THE E-F POST. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

FLIGHT DECK LT NR 3 WINDOW FWD FRAME 2ND FASTENER FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 25. REPAIRED FLANGE IAW EA & ER.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 25. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,708 hrs · 24,313 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 45. REPAIRED FLANGE IAW ER & EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,452 hrs · 23,013 cycles

RIGHT EEPLS DAMAGED BETWEEN ROW 2 TO ROW 4. R & R EEPLS IAW MM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 40,381 hrs · 22,374 cycles

DIVERT DECLARED EMERGENCY. HAD A RT BLEED FAIL AT 410 FOLLOWED BY A LT BLEED FAIL. O2 MASKS DEPLOYED AUTOMATICALLY. DURING EMERGENCY DESCENT FOUND NR 1 ENG PRSOV REGULATOR BAD. R & R PRSOV REGULATOR & NR 2 ENG HIGH STAGE VLV IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 40,140 hrs · 22,226 cycles

LT FWD EEPLS LIGHT MISSING AT ROW 1. INSTALLED EEPLS IAW DRAWING.

Part: HANDLE — LACK OF LUBE (COCKPIT WINDOW) · airframe 39,199 hrs · 21,686 cycles

R2 WINDOW EXTERNAL RELEASE HANDLE INOPERATIVE. LUBED HANDLE IAW SIP.

Part: FRAME — BROKEN (EXIT SIGN) · airframe 37,108 hrs · 20,468 cycles

EXIT SIGN FRAME BROKEN FOR AFT GALLEY DOOR. REMOVED AND REPLACED LAMP ASSY PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,857 hrs · 20,329 cycles

(QC) AFT SERVICE DOOR EXIT LIGHT BULB BURNED OUT. RELAMPED AFT SERVICE DOOR EXIT LIGHT BULB PER AMM 33-51-01-960-801 STEPS 2.C.(A.1) & 2.C.4 AND PERFORMED GOOD OPS CHECK PER AMM 33-51-01-960-801 STEP 2.C.2 56138U 27JAN13.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 36,857 hrs · 20,329 cycles

(QC) AFT SERVICE DOOR ESCAPE GIRT IS CONTACTING FLOOR AND BINDING UPON CLOSE. REPOSITIONED AFT SERVICE DOOR SLIDE PACK IAW MT #725-61-06 POS SA 3695U 27JAN13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,857 hrs · 20,329 cycles

(QC) FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED FWD ENTRY EMERGENCY EXIT LIGHT PER AMM 33-35-01-960-801 STEP 2.C. 1(A-4) & 2.C.1(C) & 2.C.4 AND PERFORMED GOOD TEST PER AMM 33-35-01-960-801 STEP 2.C.2 56138U 27JAN13.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

AFT CARGO BAY FWD BULKHEAD ATTACH BRACKET CRACKED BS 727, WL 163, RBL 5. REMOVED AND REPLACED ACB FWD BULKHEAD ATTACH BRACKET AT BS 727, WL 163 RBL 5 WITH NEW BRACKET PART NUMBER 7531203 IAW SRM 51-40-02. 56105U 17JAN13.

Part: STOP PIN — LOOSE (EMERGENCY EXIT) · airframe 36,857 hrs · 20,329 cycles

RIGHT EMERGENCY EXIT DOOR HATCH AFT UPPER STOP PIN IS LOOSE. TIGHTENED RIGHT EMERGENCY EXIT DOOR HATCH AFT UPPER STOP PIN JAM NUT IAW AMM 52-22-00-820-801 STEP 5.F.(1)10).

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 36,857 hrs · 20,329 cycles

FORWARD GALLEY DOOR FWD GIRT BAR RETAINING CLIP IS LOOSE. REMOVED & REPLACED FGD FWD GIRT BAR RETAINING CLIP IAW SRM 51-40-02 STEP 4A,B,C, & E.

Part: CONNECTOR — BROKEN (CABIN) · airframe 36,857 hrs · 20,329 cycles

ELECTRICAL CONNECTOR BS 952 WL 300 LBL 16 IS BROKEN. REMOVED AND REPLACED CONNECTOR D40100J PER SWPM 20-72-24 & WDM 33-51-22, 33-51-14 4631U 09JAN13 8052C 9JAN13 307 09JAN13 PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS PER AMM 33-51-00-710-8.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 1088 RBL 32 O/B T-CHORD CORRODED. REMOVED AND REPLACED T-CHORD PER SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

CORROSION ON RIGHT EDGES OF FLOOR PANEL 140AF. REPLACED PANEL PER DWG SRM.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

CORROSION APU COMPARTMENT RT SIDE BS 1128. REMOVED AND REPLACED T-CHORD PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

STRINGER CLIP IS CRACKED AT STA 360 STRINGER 8R. REMOVED STR CLIP BS 360 STR 8R IAW SRM 51-40-02. INSTALLED NEW STRINGER CLIP PO #LINE 422757 AT STA 360 STR 8R IAW SRM 51-40-02-0G-0.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 36,857 hrs · 20,329 cycles

RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL IS CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL PER MM 55-31-31-000-801, MM 55-31-31-400-801 AND SOPM 20-50-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

FRAME CRACKED STA 293, RBL 54, WL 209 (FSD FWD FRAME). REPAIRED BS 293 FWD SERVICE DOORWAY FWD LOWER STUB FRAME RBL 54 WL 209 IAW ER 13-01020 AND EA 1-753-21496.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 36,857 hrs · 20,329 cycles

BATTERY CHARGER AT STATION 500C, M2335 HAS BLOWN FUSES. INSTALLED FUSES ON M2335 PER WDM 33-51-11 89229U 15JAN13 8052C 15JAN13 267 15JAN13 OPS CHECK OF EMERGENCY EXIT LIGHTS WILL BE ACCOMPLISHED ON DEFECT T169107 SAM 326 A771917 ITEM 1.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 36,857 hrs · 20,329 cycles

BATTERY CHARGER AT STATION 597 RIGHT, M1669 HAS BLOWN FUSES. INSTALLED FUSES ON M1669 PER WDM 33-51-11 89229U 15JAN13 8052C 15JAN13 267 15JAN13 OPS CHECK OF EMERGENCY EXIT LIGHTS WILL BE ACCOMPLISHED ON DEFECT T169104 SAM 326 A 771917 ITEM

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 727D FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 727D FRAME REMOVED AND REPLACED ON CARD T169299.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 440 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED AT BS 440 FRAME AIR CONDITIONING ATTACH BRACKET STR 8L PER EA 1-A53-12114R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 787 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED THE CRACK AT BS 787 STR 8L AT AIR CONDITIONING BRACKET I/B HOLE IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 500A FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED AT BS 500A FRAME AIR CONDITIONING ATTACH BRACKET STR 8L IAW EA 1-A53-12114R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 360 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED BS 360 FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8L IAW EA 13-01010 AND EA 1-753-21499.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 827 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 827 FRAME THAT IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE REPAIRED IAW EA 1-A53-12114 89213C 02JAN13.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 36,857 hrs · 20,329 cycles

CORROSION ON L1 DOOR GIRT BAR FITTING MOUNT STA 344, LBL 58, WL 208. REMOVED AND REPLACED MOUNT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 400 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. REPAIRED BS 400 FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8R IAW EA 1-A53-12114R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 867 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 867 FRAME THAT IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE REPAIRED IAW EA 1-A53-12114. 89213C 02JAN13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 500A FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKED I/B HOLE AT STR 8R. REPAIRED BS 500A FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8R IAW EA 1-A53-12114R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

BS 360 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 360 FRAME AT STRINGER 8R REPAIRED PER EA 1-753-21532.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

"L" ANGLE CRACKED AT STA 500C, LBL 25, WL 154 AFT SIDE OF FRAME. REMOVED & REPLACED "L" ANGLE AT STA 500C, LBL 25, WL 154 AFT SIDE OF FRAME IAW SRM 51-10-02 STEP 9 & SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

L-ANGLE CRACKED AT STA 500C, LBL 25, WL 154 FWD SIDE OF FRAME. 2706C. REMOVED & REPLACED L- ANGLE AT STA 500C, LBL 25, WL 154 FWD SIDE OF FRAME IAW SRM 51-10-02 STEP 9 & SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

"L" ANGLE CRACKED AT STA 500C, RBL 25, WL 154. REMOVED & REPLACED "L" ANGLE AT STA 500C, RBL 25, WL 154 IAW SRM 51-10-02 STEP 9 & STR 51-40-02

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,857 hrs · 20,329 cycles

CORROSION ON UNDER SIDE OF FLOOR TO SIDEWALL SUPPORT STA 859-863, RBL20, WL 160. REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT AT STA 859-863. RBL 20, WL 160 PER B737-700 SRM 51-40-02-0G-0 & DRAWING 146A0081.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,121 hrs · 19,891 cycles

RIGHT EXTERIOR EMERGENCY LIGHT AFT OF WING INOP. REMOVED AND REPLACED BULB PER AMM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 35,566 hrs · 19,547 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SENSOR — FAILED (E&E BAY) · airframe 35,158 hrs · 19,312 cycles

DECLARED EMERGENCY -- AIRSPEED LOW WARNING AND STICK SHAKER ACTIVATED AT FLAPS 25 POSITION WITH L/E TRANSIT LIGHT ILLUMINATED ON FORWARD PANEL. FOUND NR 1 SLAT INBOARD SENSOR FAIL. REPLACED FSEU IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 36,857 hrs · 20,329 cycles

LEFT WHEEL WELL BS 663 VERTICAL SUPPORT ANGLE OUTBOARD OF PACK EXHAUST IS CRACKED 2 INCHES. REPAIRED PER EA 1-753-19534. THIS IS A TIME LIMITED REPAIR REQUIRING PERMANENT REPAIR (REF SRM 51-70-12) OR REPLACEMENT OF PART WITHIN 730 DAYS OR 30

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 36,857 hrs · 20,329 cycles

LEFT W/W BS 663 VERTICAL SUPPORT ANGLE O/B OF PACK EXHAUST CRACKED. REPAIRED PER EA. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 33,924 hrs · 18,639 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 32,912 hrs · 18,053 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 32,293 hrs · 17,691 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: COVER — BROKEN (CABIN) · airframe 31,708 hrs · 17,363 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 31,696 hrs · 17,355 cycles

LT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 11. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,503 hrs · 16,676 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,511 hrs · 16,680 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS INOP AT ROW 11. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,501 hrs · 16,675 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EEPLS INOP AT ROW 18. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,501 hrs · 16,675 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 11. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,501 hrs · 16,675 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 20. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,501 hrs · 16,675 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 2. RELAMPED PER MM.

Part: LENS — LOOSE (CABIN) · airframe 30,501 hrs · 16,675 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,501 hrs · 16,675 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.