N733SA

Part: PIN — LOOSE (ZN 800 DOOR) · airframe 79,929 hrs · 47,207 cycles

FWD ENTRY DOOR SLIDE CASE PIN LOOSE / [01] SECURED PIN IN REF TO 25-66-01 A.M.M.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,381 hrs · 46,835 cycles

FWD SVC DOOR EXT EMER LIGHT INOP / [01] RELAMPED FWD SVC DOOR EXT EMER EXIT LIGHT REF AMM 33-51-04

Part: SCUFF PLATE — DAMAGED (FWD CARGO BAY) · airframe 79,314 hrs · 46,790 cycles

FWD CARGO DOOR LOWER SILL INNER STRAP SCUFF PLATE REQUIRES REPLACEMENT; REF TTG8Q00F0TV5; EA 22-153-02897 TLD. / [01] REMOVED AND REPLACED FWD CARGO CENTER SCUFF PLATE PER AMM 25-52-10.;[02] ADDED LP# PER ERIC YOUNG 36461.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 79,308 hrs · 46,787 cycles

FUEL LEAK BY DRIP STICK#8; 27 DROPS IN 60 SECONDS / [01] R&R FUEL TANK ACCESS PANEL 632QB. REF AMM 28-11-11-400-801. LEAK CHECK GOOD

Part: LIGHT — MISSING (PAX CABIN) · airframe 78,979 hrs · 46,573 cycles

R/H SIDEWALL EMERGENCY EXIT LIGHT LENS COVER FOR OVERWING EXIT MISSING / [01] INSTALLED NEW LENS COVER IAW SIP

Part: COVER — LOOSE (R2 DOOR) · airframe 78,903 hrs · 46,520 cycles

AFT SERVICE DOOR SLIDE INFLATION FLAP COVER FOR HANDLE IS NOT VISIBLE. / [01] RESECURED AFT SERVICE DOOR INFLATION FLAP COVER REF S.I.P.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 78,686 hrs · 46,386 cycles

L1 DOOR SLIDE FELL OUT / [01] REFERENCE AMM 25-66-01 REPOSITION SLIDE INTO COVER. OK FOR SERVICE

Part: BRACKET — LOOSE (R1 DOOR) · airframe 77,579 hrs · 45,661 cycles

FWD SERVICE GIRT BAR LOOSE / [01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT BAR BRACKET <BR>PER M/M S.I.P.

Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 77,118 hrs · 45,400 cycles

FA REPORT FORWARD GIRT BAR LATCH DOOR L1 INOP ; / [01] REMOVED AND INSTALLED GIRT BAR LATCH PER AMM. 25-66-02

Part: LATCH — STUCK (FWD DOOR) · airframe 77,113 hrs · 45,398 cycles

FLIGHT ATTENDANTS REPORT FWD GIRT BAR LATCH IS STICKY AND DOESNT STAY UP ; / [01] LUBRICATED LATCH; OPS CHECK PER AMM 28-66-02. OPS CHECK GOOD AT THIS TIME

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,304 hrs · 44,914 cycles

POSSIBLE CRACK INDICATION AT S10R BETWEEN STA. 500A AND 500B ; POSSILE CRACK INDICATION AT S10R ETWEEN STA. 500A AND 500B / [01] INSPECTED AREA AS REQUIRED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 75,719 hrs · 44,566 cycles

FOUND FWD ENTRY DOOR EXIT SIGN COVER OFF OF LIGHT ASSEMBLY ; / [01] FOUND LIGHT ASSY DAMAGED; REPLACED LOWER EXIT SIGN ASSY AND PWR SUPPLY FUSE FOR LIGHT. OPS GOOD PER M/M 33-51-01 AND 33-51-06.

Part: RETAINER — OUT OF ADJUST (R1 DOOR GIRT BAR) · airframe 75,523 hrs · 44,448 cycles

GIRT BAR RETENTION CLIP ON FWD SERVICE DOOR WILL NOT HOLD GIRT BAR IN PLACE. / [01] ADJUSTED GIRT BAR RETENTION CLIPS ON FWD SERVICE DOOR IN REF TO AMM 25-66-01. OPS TEST NORMAL AT THIS TIME

Part: PANEL — DAMAGED (NOT REPORTED) · airframe 75,172 hrs · 44,226 cycles

PANEL 193D HAS SEVERAL OBLONG AND OVERSIZED HOLES. ; / INSTALLED PNL PER AMM 53-51-21

Part: PANEL — PULLED (NOT REPORTED) · airframe 75,172 hrs · 44,226 cycles

PANEL 194E HAS SEVERAL HOLES WHERE THE SCREW HAS PULLED THROUGH THE COUNTER SINKS. ; / INSTALLED PNL PER AMM 53-51-21

Part: BEZEL — LOOSE (EMERGENCY LIGHT) · airframe 74,514 hrs · 43,855 cycles

O/H BIN EMERGENCY LIGHT BEZEL AT L/H ROW 9 LOOSE. / RESECURED O/H BIN EMERGENCY LIGHT BEZEL AT L/H ROW 9 AS PER REF B737 AMM 33-51-03-960-802.

Part: SIGN — CRACKED (CABIN) · airframe 74,514 hrs · 43,855 cycles

EMERGENCY EXTIT SIGN AT AFT. LOWER CEILING PANEL BASE WITH CRACK. / REPLACED EMERGENCY EXIT SIGN AT AFT LOWER CEILING PANEL IAW B737 AMM 33-51-01-960-802. PERFORMED OPERATIONAL TEST (CHECK) FOUND NORMAL PER AMM 33-51-00-720-801

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 74,514 hrs · 43,855 cycles

**CORROSION** AFT CARGO FLOOR STRUCTURE L/H ZEE PLATE UPPER SURFACE VARIOUS CORROSION SPOTS BETWEEN STA 727D AND 787. / REMOVED AND REPLACED ZEE CHANNEL AT AFT CARGO COMPT. L/H SIDE STA 727D TO STA 792 REF B737-700 SRM 51-40-02-0G-0

Part: RIB — CRACKED (VERTICAL STAB) · airframe 74,514 hrs · 43,855 cycles

VERTICAL DORSAL FIN FWD RIB CRACKED / REMOVED AND INSTALLED NEW RIB FROM VERTICAL STRAP DORSAL FIN IAW B-737-700 SRM 51-40-02-0G-0

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 74,514 hrs · 43,855 cycles

FOUND LH WING O/B AFT FLAP I/B CORNER DELAMINATED / REMOVED AND REPLACED O/B AFT FLAP AT LT WING AS PER B737-700 AMM 27-51-22-400-801. INSTALLATION TEST OK

Part: BULKHEAD WEB — CRACKED (MID) · airframe 74,514 hrs · 43,855 cycles

R/H STA 663 VAPOR BARRIER WEB IS CRACKED AT RBL 12 / REPAIRED R/H STA 663 VAPOR BARRIER WEB AS PER B737-700 SRM 51-70-04-2R-10.

Part: PRESSURE DECK — DAMAGED (COCKPIT) · airframe 74,514 hrs · 43,855 cycles

FLIGHT DECK FLOOR DAMAGED / ACCOMPLISHED PERMANENT REPAIR AT FLIGHT DECK FLOOR IAW EA # 1-A53-33179 REV 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,905 hrs · 42,860 cycles

2(EA) OVERHEAD BIN EMERGENCY LIGHTS INOP. / RELAMPED 2(EA) EMERGENCY LIGHTS IAW AMM 33-51-03. OPS CHECKS GOOD.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 72,623 hrs · 42,675 cycles

RT WING I/B TRAILING UPPER PANEL FOUND CRACKED INTERCOASTED BESIDE FIXED TRAILING EDGE DEFECTION CONTROL RIB / REMOVED AND REPLACED RT WING I/B FIXED TRAILING EDGE PANEL INTERCOASTAL BESIDE FIXED TRAILING EDGE REF SRM 51-40-00 REF SA-M 326 - A1073133

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 72,343 hrs · 42,479 cycles

EXIT ROW EMERGENCY COVER FELL OFF. / REINSTALLED EMERGENCY EXIT CEILING LIGHT COVERS REF M/M 33-51-03.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 71,622 hrs · 42,019 cycles

PANEL 193B FASTNER HOLES ARE ENLARGED AND ELONGATED. / REMOVED AND REPLACED PER AMM.53-51-21

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1674. R&R BATTERY IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1669. R&R POWER SUPPLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1669. R&R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1668. R&R BATTERY IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1674. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1675. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1668. R&R POWER SUPPLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 69,862 hrs · 40,888 cycles

FLIGHT DECK TO OVERWING EXIT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED AT M1675. R&R BATTERY IAW AMM.

Part: INTERCOSTAL — ELONGATED (AFT FUSELAGE) · airframe 69,862 hrs · 40,888 cycles

REF: N/R X784577 1 EACH ELONGATED HOLE ON REAR PRESSURE BULKHEAD COMMON TO INTERCOSTAL P/N 65-54862-23 / REMOVED 1 EA ELONGATED HOLE FROM REAR PRESSURE BULKHEAD COMMON TO INTERCOSTAL P/N 65-5486-23 TO 247 AND INSTALLED REPAIR FASTENER IAW AAR EA 190359 IR AND SWA EA 1-753-34882 REV IR

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 69,827 hrs · 40,871 cycles

AFT UPPER L/H LIGHTING EMERGENCY CHARGER FORWARD CIRCUIT BREAKER AT P18-3 FOUND POPPED ON PREFLIGHT. R&R POWER SUPPLY IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 69,827 hrs · 40,871 cycles

RT EMERGENCY EXIT LIGHT LOOSE AT ROW 8. REATTACHED LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,349 hrs · 40,581 cycles

L1 DOOR EGRESS LIGHT FAILED TO ILLUMINATE. R&R LAMP IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,349 hrs · 40,581 cycles

RT SIDE EMERGENCY EXIT LOWER EXTERIOR ESCAPE SLIDE LIGHT FAILED TO ILLUMINATE. R&R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,349 hrs · 40,581 cycles

LT STOWBINS EGRESS LIGHTS FAILED TO ILLUMINATE BETWEEN ROW 9 TO ROW 13. R&R LIGHT LAMP IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,349 hrs · 40,581 cycles

LT SIDE EMERGENCY EXIT LOWER EXTERIOR ESCAPE SLIDE LIGHT FAILED TO ILLUMINATE. R&R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,349 hrs · 40,581 cycles

RT SIDE OVERWING EXIT UPPER SIDEWALL PANEL EXIT LIGHT FAILED TO ILLUMINATE. R&R LIGHT IAW AMM.

Part: TIP CAP — CRACKED (LT HORIZ STAB) · airframe 69,349 hrs · 40,581 cycles

LH HORIZONTAL STAB TIP CAP IS CRACKED AT FASTNER HOLE; UPPER SIDE; 6TH FASTNER FROM THE FWD EDGE. / REMOVED AND REPLACED L/H HORIZONTAL STAB TIP CAP IAW SRM 51-40-02-0G-0

Part: FLAP — DELAMINATED (L/H WING) · airframe 69,349 hrs · 40,581 cycles

LEFT WING OUTBD AFT FLAP INBD CORNER HAS DELAM / REPAIRED AND APPLIED DECORATIVE FINISH ON LEFT WING O/B AFT FLAP I/B CORNER IAW B737 SRM 51-70-10-2R-0 AND B737 AMM 51-21-99-300-801

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 69,349 hrs · 40,581 cycles

LT WING INBOARD LOWER TRAILING EDGE SUPPORT STRUCTURE ATTACH FITTING AT REAR SPAR STATION 211 CRACKED. R&R FITTING IAW SRM AND DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

RT LOWER BULKHEAD FOR EXHAUST DUCT HORSESHOE DOUBLER CRACKED AT BS 663. R&R DOUBLER IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,349 hrs · 40,581 cycles

AFT CARGO COMPARTMENT PANEL 140CF HAS CORROSION ON THE UPPER AND LOWER SURFACES AS MARKED. / REPLACED AFT CARGO COMPARTMENT PANEL 140CF P/N 453A2610 7252490 WN9139 IAW B737-700 AIPC 25-52-10-02 & DWG 453A2610 REV. K

Part: PANEL — CRACKED (LEFT WING) · airframe 69,349 hrs · 40,581 cycles

FUEL PANEL 533AB PANEL IS CRACKED AT NUT PLATE CAP. / REPLACED L/H WING FUEL TANK PANEL 533AB IAW B737 SRM 51-10-02-0G-0 STEP. REPLACED WITH NEW PANEL. PART ON PART PACK ATAG# NO0666

Part: STIFFENER — CRACKED (RH NACELLE) · airframe 69,349 hrs · 40,581 cycles

#2 O/B FAN ENGINE OIL ACCESS DOOR AFT VERTICAL STIFFNER CRACKED. UPPER CORNER. / REPLACED ON #2 O/B FAN ENGINE OIL ACCESS DOOR AFT VERTICAL STIFFENER SHIELD P/N 3142259-1 ISSUE TAG# A10570 IAW B737-700 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0; GOODRICH AEROSTRUCTURES 71-13-30

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

ELECTRONICS AND EQUIPMENT BAY INTERCOSTAL WEB CORRODED BETWEEN BS 350 TO BS 360, STR 28L. R&R WEB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,349 hrs · 40,581 cycles

LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT LEADING EDGE AT STA 105.26. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,349 hrs · 40,581 cycles

LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT LEADING EDGE AT STA 86.66. R&R RIB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (AFT CABIN) · airframe 69,349 hrs · 40,581 cycles

PASSENGER CABIN FLOOR WET AREA AT STA 312-328 LBL 47 INTERCOSTAL IS CRACKED / REPLACED PASSENGER CABIN FLOOR WET AREA AT STA 312-328 LBL 47 INTERCOSTAL IAW B737 SRM 51-40-02 DWG 141A5400 REV- TAG: A90009

Part: REPAIR — DETERIORATED (LT MLG WW) · airframe 69,349 hrs · 40,581 cycles

LT WEB PREVIOUS REPAIR DETERIORATED AT VAPOR BARRIER BS 663. REPAIRED WEB IAW SRM AND SRM DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,349 hrs · 40,581 cycles

LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT LEADING EDGE STA 95.96. R&R RIB AT IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

R1 DOOR CUTOUT UPPER STUB FRAME CRACKED AT BS 294, BETWEEN STR 8R TO STR 9R, OUTBOARD OF LATCH RECEIVER. R&R STUB FRAME IAW SRM AND DWG.

Part: FRAME — GOUGED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

INTERIOR FUSE FRAME AT INNER CHORD FORWARD EDGE GOUGED AT BS 694, ABOVE LT CREASE BEAM. REPAIRED FRAME IAW SRM AND EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

R1 DOOR CUTOUT BEAR STRAP CRACKED BETWEEN BS 291.5+2 TO BS 294, BETWEEN STR 8R TO STR 9R. R&R DOUBLER IAW EA.

Part: RETAINER — CRACKED (RT WING) · airframe 69,349 hrs · 40,581 cycles

RH WING TRAILING EDGE 11' INBD OF DEFLECTOR RIB;MID BULB SEAL RETAINER CRACKED / REPLACED R/H WING TRAILING EDGE 11' INBD OF DEFLECTOR RIB IAW B737 SRM 51-40-02 DWG: 115A2930 REV: - TAG: A86357

Part: LENS — LOOSE (CABIN) · airframe 69,349 hrs · 40,581 cycles

RT STOWBIN EMERGENCY LIGHT LENS LOOSE ABOVE SEAT 18. SECURED LENS IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: RETAINER — CRACKED (LT WING) · airframe 69,349 hrs · 40,581 cycles

LH WING TRAILING EDGE SEAL RETAINER L-BRACKET 11' INBD OF DEFLECTOR RIB CRACKED AT LOWER FASTNER / REMOVED AND REPLACED DAMAGED SEAL RETAINER -BRAKET L-BRAKET 11' INBD OF DEFLECTOR RIB IAW DWG # REV- 115A2930 REV- & SRM 51-40-02-0G-0 - APPLIED CIC IAW AMM 51-21-91-620 L/H TRAILING EDGE

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

FRAME CRACKED AT BS 312 STR 5L, INBOARD LOWER RADIUS. REPAIRED FRAME IAW EA AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: RIB — BUCKLED (RT HORIZ STAB) · airframe 69,349 hrs · 40,581 cycles

RH HORIZONTAL STAB LEADING EDGE; STA 78.29 RIB IS BUCKLED IN 2EA PLACES / REPLACED R/H HORIZ STAB LEADING EDGE; STA. 78.29 RIB IAW B737 DWG: 186A1001 REV: A TAG: WN6890

Part: RETAINER — CRACKED (RT WING) · airframe 69,349 hrs · 40,581 cycles

RH WING TRAILING EDGE 11' INBD OF DEFLECTOR RIB; AFT SEAL RETAINER L-BRACKET CRACKED BOTTOM FASTNER / REMOVED AND REPLACED RH WING TRAINLING EDGE AFT SEAL RETAINER L-BRACKET PN: 115A2982-10 IAW B737-700 SRM 51-40-02-06; + DWG# 11542930 ID:0006 REV:- A-TAG#A9450

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,349 hrs · 40,581 cycles

LT MAIN LANDING GEAR HORIZONTAL PRESSURE DECK CRACKED AT BS 665, BETWEEN LBL 30 TO LBL 60. R&R WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,349 hrs · 40,581 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 69,349 hrs · 40,581 cycles

LT WING SLAT STA 451.97, NR 1 SLAT LOWER SURFACE OF LEADING EDGE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,349 hrs · 40,581 cycles

LT WING SLAT STA 322.71, NR 2 SLAT LOWER SURFACE OF LEADING EDGE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRIP — DELAMINATED (CABIN) · airframe 68,774 hrs · 40,195 cycles

RT FORWARD ESCAPE PATH STRIP DELAMINATED AT SEAT 1. R&R STRIP PER DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,774 hrs · 40,195 cycles

RT OVERWING EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,774 hrs · 40,195 cycles

LT OVERWING EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,774 hrs · 40,195 cycles

RT FORWARD EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,483 hrs · 40,000 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,483 hrs · 40,000 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,483 hrs · 40,000 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,483 hrs · 40,000 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 68,141 hrs · 39,785 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 67,693 hrs · 39,486 cycles

RT MAIN LANDING GEAR WHEEL WELL UPPER BEADED PRESSURE DECK CRACKED BETWEEN BS 663.75 TO BS 675, BETWEEN RBL 38 TO RBL 60. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,342 hrs · 38,660 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 17. R&R BULB IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,342 hrs · 38,660 cycles

AFT RT FLASHLIGHT DIM. R&R BATTERIES PER AMM.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 66,342 hrs · 38,660 cycles

AFT LEFT FLASHLIGHT DIM. R & R THE BATTERIES IAW AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 66,342 hrs · 38,660 cycles

AFT CARGO CENTER THRESHOLD CRACKED AT SECOND FROM AFT LOWER FASTENER LOCATION / REMOVED AC.B. CENTER THRESHOLD (SCUFF PLATE) IAW AMM 53-11-02-020-801. 56011U. 13-MAR-18 3115C 13MAR18 OK TO INSTALL A.C.B CENTER THRESHOLD 88225C 14MAR18 INSP # 10 14MAR18 INSTALLED A.C.B CENTER THRESHOLD I.A.W AMM 53-11-02-420-801; PARA.3.D(4) STEPS (A) THRU (I) 88225C 14MAR.18 INSP # 362 14MAR18 SEALED (SCUFF-(PLATE) CENTER THRESHOLD. IAW AMM. 53-11-02-420-801. STEPS 4(5).A-B.C. 56011U.14-MAR-18 AFT CARGO SCUFF PLATE REPAIRED IAW EA 1-A53-2076 REV 11

Part: WINDOW — ARCED (COCKPIT) · airframe 65,516 hrs · 38,122 cycles

LT FORWARD WINDOW HEAT ELEMENT ARCED AT BASE OF WINDOW. R&R L1 WINDOW IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 65,451 hrs · 38,084 cycles

RT OVERWING EXIT EMERGENCY BATTERY PACK INOP. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,451 hrs · 38,084 cycles

L/H OVERWING EXIT EMERGENCY BATTERY PACK INOP. / R&R BATTERY PACK PER MM.

Part: ACTUATOR — FAULTED (LT MLG UPLOCK) · airframe 62,732 hrs · 36,435 cycles

LEFT MAIN LANDING GEAR RED INDICATOR REMAINED ILLUMINATED AFTER TAKEOFF. R & R THE MAIN LANDING GEAR ACTUATOR UP LOCK IAW AMM.

Part: ACTUATOR — FAULTY (LEFT MLG) · airframe 62,732 hrs · 36,435 cycles

LEFT MAIN LANDING GEAR RED INDICATOR REMAINED ILLUMINATED AFTER TAKEOFF. R & R LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW MM.

Part: CYLINDER — FAILED (LT MLG) · airframe 62,705 hrs · 36,414 cycles

AFTER GEAR RETRACTION WITH GEAR HANDLE UP, THE LT MAIN GEAR RED LIGHT ILLUMINATED, OVERHEAD LT MAIN GEAR LIGHT BLANK. CYCLED LANDING GEAR. R & R THE LEFT MAIN GEAR TRANSFER CYLINDER IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

LEFT EMERGENCY STOWAGE BIN BULLNOSE LIGHT INOPERATIVE AT ROW 14. REPLACED THE LAMPS IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

RIGHT LOWER SIDEWALL EMERGENCY EXIT SIGN INOPERATIVE. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,696 hrs · 36,408 cycles

RIGHT SIDE STOWAGE BIN EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 8. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

RIGHT EMERGENCY STOWAGE BIN BULLNOSE LIGHT INOPERATIVE AT ROW 13. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

LEFT OVERWING EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,696 hrs · 36,408 cycles

LEFT SIDEWALL PANEL EMERGENCY EXIT LIGHTS INOPERATIVE. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,696 hrs · 36,408 cycles

LEFT SIDEWALL PANEL EMERGENCY EXIT LIGHTS INOPERATIVE. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

RIGHT EMERGENCY STOWAGE BIN BULLNOSE LIGHT INOPERATIVE AT ROW 11. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 62,696 hrs · 36,408 cycles

LEFT LOWER SIDEWALL EMERGENCY EXIT SIGN INOPERATIVE. CHARGED THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,696 hrs · 36,408 cycles

RIGHT OVERWING EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500C, STR 25L. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

FORWARD CARGO PIT BAFFLE CORRODED BETWEEN BS 500 TO BS 500A, LBL 20. R&R BAFFLE IAW SRM 0 AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 988 TO BS 995, RBL 44. R&R WEB IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

R1 DOOR SURROUND STUB FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 62,696 hrs · 36,408 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR SUPPORT CRACKED BETWEEN BS 312 & 328, RBL 32. R & R THE FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CRACKED (BS 275-294) · airframe 62,696 hrs · 36,408 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 275 TO 294.5, BL 0. R & R THE FLOOR SUPPORT IAW DWG.

Part: ANGLE — CORRODED (BS 727C-794) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO LT ZEE ANGLE CORRODED BETWEEN BS 727C+10 TO 794. R & R THE ANGLE IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

R1 CREASE BEAM ATTACH ANGLE CORRODED. R&R ANGLE IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

R1 CREASE BEAM CORRODED. R&R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R INTERCOSTAL IAW DWG & SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO SILL WEB CORRODED. R&R WEB IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 727E-767) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO RT ZEE ANGLE CORRODED BETWEEN BS 727E+10 TO 767. REPAIRED THE ANGLE IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO RT TIE DOWN TRACK CRACKED BETWEEN BS 727D TO BS 767, RBL 14. R&R TRACK IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO RT Z ANGLE CORRODED BETWEEN BS 727D+10 TO BS 727E+10. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

FORWARD CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 500A TO BS 500C. REPAIRED Z ANGLE IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 62,696 hrs · 36,408 cycles

LT WING AFT SPAR DEFECTOR RIB BRACKET CRACKED AT LOWER BOLT HOLE. R&R BRACKET IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 62,696 hrs · 36,408 cycles

RIGHT WING FIXED TRAILING EDGE PANEL SUPPORT ANGLE CRACKED AT LOWER FORWARD ATTACH FITTING. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 767-794) · airframe 62,696 hrs · 36,408 cycles

AFT CARGO RIGHT ZEE ANGLE CORRODED BETWEEN BS 767 TO 794. R & R THE ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,696 hrs · 36,408 cycles

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

Part: ANGLE — CRACKED (RT WING) · airframe 62,696 hrs · 36,408 cycles

RIGHT WING FIXED TRAILING EDGE PANEL INTERCOSTAL ANGLE CRACKED AT LOWER FORWARD ATTACH OUTBOARD END. REPAIRED THE ANGLE IAW SRM AND DWG.

Part: SPAR — CORRODED (RT WING) · airframe 62,696 hrs · 36,408 cycles

RIGHT WING AFT SPAR CORRODED AT THE MAIN LANDING GEAR WHEEL WELL AREA. REPAIRED THE SPAR IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,696 hrs · 36,408 cycles

R2 CREASE BEAM CORRODED. R&R CREASE BEAM IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 62,693 hrs · 36,407 cycles

RIGHT WHEEL WELL RAM AIR DUCT SUPPORT STIFFENER CRACKED AT BS 663, RBL 15.54. R & R THE STIFFENER IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,693 hrs · 36,407 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,693 hrs · 36,407 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,693 hrs · 36,407 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST AT LOCATION M01669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,693 hrs · 36,407 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,693 hrs · 36,407 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 62,555 hrs · 36,327 cycles

RT OVERWING EXIT LOWER FORWARD LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,104 hrs · 35,484 cycles

AFT CARGO COMPARTMENT STRAP CORRODED AT BS 795, RBL 20. R & R STRAP IAW DWG & SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,104 hrs · 35,484 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT T/E. REPAIRED FLAP IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,104 hrs · 35,484 cycles

AFT CARGO COMPARTMENT TIE DOWN TRACK CORRODED AT BS 792+8, RBL 14. R & R TIE DOWN TRACK IAW DWG AND SRM.

Part: COVER — MISSING (CABIN) · airframe 59,846 hrs · 34,734 cycles

RIGHT OVERWING LOWER EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 59,588 hrs · 34,586 cycles

LEFT WING OVERWING EXIT LIGHT LENS BROKEN. REPAIRED LENS IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 58,813 hrs · 34,123 cycles

RIGHT OVERHEAD BIN BULLNOSE EMER LENS BROKEN AT ROW 11. R & R LENS IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 58,186 hrs · 33,768 cycles

L1 DOOR LOWER EXIT LIGHT COVER FELL OFF. R & R COVER IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 57,496 hrs · 33,359 cycles

LEFT FWD OVERWING EMER EXIT LIGHT LENS COVER BROKEN. R & R LENS IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 480) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500A) · airframe 57,299 hrs · 33,245 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,299 hrs · 33,245 cycles

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

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 57,267 hrs · 33,227 cycles

R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,119 hrs · 33,146 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 56,826 hrs · 32,987 cycles

AFT GALLEY CEILING EXIT SIGN LIGHT MOUNT BRACKET BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: LIGHT — DETACHED (CABIN) · airframe 56,405 hrs · 32,762 cycles

MID CABIN OVERHEAD EXIT LIGHT DETACHED. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 56,311 hrs · 32,707 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW AMM & MT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,637 hrs · 32,326 cycles

ANGLE CRACKED AT BS 727B RBL 24.7. R & R ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,637 hrs · 32,326 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,637 hrs · 32,326 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,637 hrs · 32,326 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,637 hrs · 32,326 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 55,056 hrs · 32,002 cycles

EMERGENCY EXIT LIGHTS IN FWD CABIN ILLUMINATES WITH SYS ARMED. FOUND CB AT P18 2 11 POPPED. RESET CB IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,325 hrs · 31,571 cycles

AFT LT CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 52,057 hrs · 30,207 cycles

AFT EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY FUNCTION CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 52,057 hrs · 30,207 cycles

FWD EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY FUNCTION CHECK. R & R BATTERY IAW AMM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 51,184 hrs · 29,679 cycles

LT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 50,839 hrs · 29,463 cycles

RT AFT EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 50,839 hrs · 29,463 cycles

LT OVERWING EMERGENCY LIGHT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,839 hrs · 29,463 cycles

RT AFT EMERGENCY OVERWING DOOR HANDLE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,839 hrs · 29,463 cycles

LT FWD EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 50,556 hrs · 29,309 cycles

LT HORIZONTAL STABILIZER STIFFENER CRACKED AT STA 663, BETWEEN LBL8 TO LBL 38. R & R STIFFENER IAW SRM. (STATION NUMBERS NO NOT MATCH HORIZ STAB LOCATION, BUT WRITTEN FOR STAB, JSG)

Part: STRUCTURE — LOOSE (LT MLG WW) · airframe 50,556 hrs · 29,309 cycles

LT WHEEL WELL LOOSE AT STA 663. REPAIRED FIBER GLASS IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,556 hrs · 29,309 cycles

LEFT E-F WINDOW POST FRAME CRACKED INDICATION AT THE SECOND LOWER FASTENER HOLE. REPAIRED FRAME IAW EA.

Part: WINGLET — DELAMINATED (RT WING) · airframe 50,556 hrs · 29,309 cycles

RIGHT WING WINGLET DELAMINATED. R & R WINGLET IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 52,649 hrs · 30,551 cycles

CAPTAIN`S NR 1 WINDOW POST CRACKED IN UPPER OTBD CORNER. REPAIRED POST IAW ATS ER & EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 48,396 hrs · 27,950 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: WIRE — LOOSE (COCKPIT) · airframe 44,349 hrs · 25,593 cycles

DURING CLIMB WITH GEAR HANDLE OFF 3 RED GEAR LIGHTS ILLUMINATED WITH GEAR HANDLE UP 3 RED LIGHTS CYCLED RANDOMLY. FOUND WIRES LOOSE IN GROUND BLOCK 6D201B. SECURED WIRES PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, BETWEEN LBL 40 TO LBL 45.57. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 40 TO RBL 45.57. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,189 hrs · 25,500 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 5. REPAIRED BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,364 hrs · 23,300 cycles

LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 11. SECURED LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,007 hrs · 22,508 cycles

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

Part: LENS — MISSING (CABIN) · airframe 37,792 hrs · 21,732 cycles

RIGHT EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,416 hrs · 21,503 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,416 hrs · 21,503 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,416 hrs · 21,503 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 37,267 hrs · 21,411 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS COVER LOOSE BETWEEN ROW 1 TO ROW 3. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 37,267 hrs · 21,411 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING BETWEEN ROW 14 TO ROW 15. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 37,267 hrs · 21,411 cycles

EEPLS COVER MISSING FROM ROW 14 TO ROW 15. REMOVED AND REPLACED EEPLS PER MM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, LBL 41.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, LBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, RBL 41.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 37,238 hrs · 21,394 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING UPPER FITTING FWD STIFFENER CRACKED AT BS 540, LBL 54.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 36,878 hrs · 21,168 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING SUPPORT FITTING I/B LOWER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING SUPPORT FITTING O/B UPPER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT WING TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING FWD TRUNNION BEARING SUPPORT FITTING I/B LOWER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING SUPPORT FITTING O/B LOWER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING SUPPORT FITTING I/B UPPER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING SUPPORT FITTING O/B UPPER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING SUPPORT FITTING I/B UPPER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,042 hrs · 20,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING FWD TRUNNION BEARING SUPPORT FITTING O/B LOWER LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,530 hrs · 20,328 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,808 hrs · 19,878 cycles

CENTER CEILING EMERGENCY LIGHT ASSY UNSECURED. SECURED LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,511 hrs · 19,705 cycles

DURING SCHEDULED HC2 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,511 hrs · 19,705 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,511 hrs · 19,705 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,511 hrs · 19,705 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,511 hrs · 19,705 cycles

DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 33,146 hrs · 18,902 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK OUT OF ADJUST. ADJUSTED GIRT BAR HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,146 hrs · 18,902 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 32,987 hrs · 18,815 cycles

FWD RIGHT CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 32,624 hrs · 18,584 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 22 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,968 hrs · 18,197 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — MISSING (CABIN) · airframe 31,968 hrs · 18,197 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 22 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,968 hrs · 18,197 cycles

DURING SCHEDULED HC1 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,968 hrs · 18,197 cycles

DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,457 hrs · 17,281 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, RBL 11 TO RBL 12. REPAIRED FLOORBEAM CHORD PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,457 hrs · 17,281 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 5. REPAIRED FLOORBEAM CHORD PER ER.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 28,897 hrs · 16,407 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 28,162 hrs · 16,003 cycles

FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,152 hrs · 16,000 cycles

EEPLS COVER MISSING AT ROW 14 ABC. INSTALLED COVER PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,244 hrs · 15,494 cycles

DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,244 hrs · 15,494 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,244 hrs · 15,494 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 23,694 hrs · 13,513 cycles

BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 10. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 22,791 hrs · 13,019 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,230 hrs · 12,693 cycles

DURING SCHEDULED HC1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 5 DEF. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,936 hrs · 11,395 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 18,962 hrs · 10,817 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 18,610 hrs · 10,617 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 15,994 hrs · 9,209 cycles

EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS TRACK COVER PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 15,345 hrs · 8,857 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION CRACKED AND LENS MISSING. REMOVED AND REPLACED EEPLS SECTION AND INSTALLED LENS.

Part: FITTING — LOOSE (GIRT BAR) · airframe 14,035 hrs · 8,148 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENER LOOSE. SECURED FASTENER PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 13,499 hrs · 7,867 cycles

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

Part: HINGE — WORN (ELEVATOR TAB) · airframe 11,246 hrs · 6,637 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AT ALL HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 11,116 hrs · 6,550 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB 2 HINGE WORN. REMOVED AND REPLACED NR 2 HINGE BUSHING PER MM.

Part: COVER — CRACKED (CABIN) · airframe 8,255 hrs · 4,926 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT SEVERAL LOCATIONS IN CABIN. R & R TRACK COVERS PER MM.

Part: TORQUE TUBE — WORN (TAIL) · airframe 8,255 hrs · 4,926 cycles

DURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. R&R ELEVATOR CONTROL BUS TORQUE TUBE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 8,255 hrs · 4,926 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW 1 & ROW 11. R&R COVERS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 8,255 hrs · 4,926 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 7,007 hrs · 4,223 cycles

EEPLS TRACK WIRES EXPOSED AT ROW 1. SECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 7,007 hrs · 4,223 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS WIRES EXPOSED AT ROW 1. SECURED WIRES PER MM.

Part: COVER — CRACKED (ROW 1) · airframe 3,912 hrs · 2,449 cycles

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

Part: LENS — MISSING (CABIN) · airframe 3,612 hrs · 2,265 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING AT FWD END. INSTALLED LENS ASSY PER MM.

Part: INDICATOR — DISLODGED (SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.