N987AT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,966 hrs · 30,714 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY INOPERATIVE AT LOCATION B5-260. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-55. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,603 hrs · 29,769 cycles

ON SERVICE CHECK FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-227 AND BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,155 hrs · 29,435 cycles

DURING SERVICE CHECK, FOUND FWD CEILING EMERGENCY LIGHTS COME ON MOMENTARILY DURING TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT BIN 4R / SEAT ROW 11R PER AMM 33-51-03. EMERGENCY LIGHT TEST NORMAL.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.

Part: SKIN — DELAMINATED (SPOILER)

DURING UNSCHEDULED MAINTENANCE CHECK, RT OTBD SPOILER FOUND DELAMINATED.

Part: SKIN — DELAMINATED (SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK RT INBD SPOILER FOUND DELAMINATED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,311 hrs · 28,845 cycles

RT CUSP WEB JUST FORWARD OF FRAME STA 505 IS CRACKED AROUND RIVET AND AREA OF CORROSION. REMOVED DAMAGE PART OF CRACKED CUSP WEB. FABRICATED NEW PARTS. INSTALLED NEW PARTS IAW SRM 53-00-55 REPAIR 4 PG 257 & SRM 51-40-02 AT STA 505.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,286 hrs · 28,825 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: CUSP WEB — CORRODED (BS 1002-1022) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

RIGHT CUSP WEB HAS CORROSION BETWEEN BS 1002-1022. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-51 FIG 1 ITEM 2. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: FRAME — CORRODED (BS 908) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

FRAME AT BS 908 HAS CORROSION ON UPPER AND LOWER AREAS ON LOWER FLANGE BETWEEN STRINTERS 29 AND 30L. BLEND CORRODED AREA IAW SRM 53-00-00 FIG 103, AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-20-07 REPAIR 3.

Part: SEAT TRACK — CORRODED (BS 200-590) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

SEAT TRACK FOUND TO BE CORRODED BEYOND LIMITS, AT RBL 56 IN MULTIPLE AREAS BS 200-590. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5 AND 51-41-01.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,629 hrs · 29,068 cycles

CORR SKIN AT STA 1002 STR 28R-25R. BLENDED CORROSION ON INTERNAL DOUBLER "SKIN" AT STA 1002 L25R-L28R FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15 NOMINAL .071 .040. REMAINING REPAIRED OUT OF LIMITS AREA IAW ER/A 549633-14.

Part: INTERCOSTAL — CRACKED (BS 665) · airframe 41,190 hrs · 28,745 cycles

INTERCOSTAL AT BS 665 UNDER LEFT INBOARD SEAT TRACK CRACKED. REPLACED IAW DWG 9911751 REV Z.

Part: STRINGER — CORRODED (BS 908) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

STRINGER 30 CORRODED AT BS 908. BLENDED CORROSION IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED THE STRINGER IAW SRM 53-20-05 REPAIR 1, AND SRM 53-20-05 103.

Part: SEAT TRACK — DAMAGED (BS 813-908) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

RIGHT OTBD SEAT TRACK RBL 56 IS GOUGED AND CORRODED IN SEVERAL AREAS FROM BS 813 - 908. BLENDED, AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01.

Part: SEAT TRACK — DAMAGED (BS 500-600) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

RIGHT OUTBOARD SEAT TRACK HAS KNICKS AND CORROSION BS 500 - 600. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 AND SRM 53-20-52 REPAIR 5.

Part: INTERCOSTAL — CRACKED (BS 665) · airframe 41,190 hrs · 28,745 cycles

INTERCOSTAL AT BS 665 UNDER THE RIGHT INBOARD SEAT TRACK CRACKED. REPLACED THE INTERCOSTAL IAW DWG 9911751 REV 2.

Part: CUSP WEB — CRACKED (BS 218) · airframe 41,190 hrs · 28,745 cycles

CUSP WEB AT BS 218 WAS FOUND CRACKED. REMOVED AND REPLACED THE CUSP WEB BS 218-236 IAW SRM 51-41-00 ITEM 1, SRM 51-40-08, SRM 51-41-02, AND 51-41-05.

Part: FRAME — CORRODED · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

NR 2 RT AIR GRILL FRAME IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 A.D. GENERAL FIG 103. INSTALLED REPAIR DOUBLERS IAW SRM 51-70-11-B1.

Part: CUSP WEB — CORRODED (BS 218) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

CORROSION ON CUSP WEB AT BS 218. RBL 56. CUT OUT CORROSION DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2, AMM 51-10-00 370-803, AND SRM 51-41-08.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 41,190 hrs · 28,745 cycles

VERTICAL STAB LEADING EDGE AT VSS ZFS 52.267 SPLICE HAS NUMEROUS LOOSE SCREWS & SCREWS PULLING INTO SKIN & ELONGATED HOLES. REPAIRED THE VERTICAL STAB LEADING EDGE SKIN IAW DWG SR95550001 AND JC 5530-01048-03. FABRICATED NEW SPLICE BAN IAW ER/A 549632-14 REV O AND INSTALLED IAW SR95550001.

Part: CUSP WEB — CRACKED (BS 655) · airframe 41,190 hrs · 28,745 cycles

CUSP WEB AT BS 655 CRACKED. REPLACED THE CUSP WEB IAW SRM 51-41-02 AND 51-41-05.

Part: LONGERON — CORRODED (BS 1002) · airframe 41,190 hrs · 28,745 cycles

CORROSION LONGERON 25R BS 1002. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 51-41-02 PAGE 1-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

CUSP WEB CORRODED ON FWD AND AFT SIDE OF FLOORBEAM AT FS 389 ON UNDERSIDE OF WEB. REPAIRED CORRODED CUSP WEB AT FS 389 BY REMOVING DAMAGED SECTION AND REPAIRING IAW SRM 53-00-55 REPAIR 4 FIG 224.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,190 hrs · 28,745 cycles

DENT IN FUSELAGE AT C-1 UPPER CORNER CUTOUT. EVALUATED DENT IN FUSELAGE AT C-1 UPPER FWD CORNER CUTOUT IAW SRM 53-01-01 AD3 DENT IS OUT OF LIMITS. REPAIRED DENTED AREA AT C1 DOOR CUTOUT IAW SRM 53-20-15 REPAIR 1. REPLACED FWD HINGE BRACKET IAW SRM 51-41-05.

Part: CUSP WEB — CRACKED (BS 657) · airframe 41,190 hrs · 28,745 cycles

RT CUSP WEB AT BS 657 CRACKED. REPAIRED THE CUSP WEB IAW SRM 51-70-10 REP 2 & SRM 53-00-55 REP 4.

Part: CUSP WEB — CRACKED (BS 579-598) · airframe 41,190 hrs · 28,745 cycles

LEFT CUSP WEB FOUND CRACKED BETWEEN BS 579 & 598. REPLACED THE CUSP WEB IAW SRM 51-41-05 PG 17 STEP 8.

Part: CUSP WEB — CRACKED (BS 374) · airframe 41,190 hrs · 28,745 cycles

CUSP WEB AT BS 674 CRACKED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

RIGHT INBD SEAT TRACK BS 200-256, FOUND THREE SPOTS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-05 PG 1.

Part: FRAME — CRACKED (BS 1022) · airframe 41,190 hrs · 28,745 cycles

BS 1022 FRAME ABOVE LONGERON 14R WAS FOUND CRACKED. REPLACED THE FRAME IAW SRM 51-41-02 PG 1-4, & 51-41-05 PG 1.

Part: STRINGER — CORRODED (BS 908-927) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

STRINGER 29L CORRODED BETWEEN BS 908 - 927. BLENDED THE STRINGER IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED THE STRINGER IAW SRM 53-00-05 REPAIR 3.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 41,190 hrs · 28,745 cycles

RT WING UPPER ACCESS PANEL 620CT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.

Part: FRAME — CRACKED (BS 1022) · airframe 41,190 hrs · 28,745 cycles

CRACK IN BS 1022 MAIN FRAME, AFT SIDE AT STRINGER 7R. REPAIRED THE FRAME IAW SRM 51-70-11 REPAIR 1.

Part: FRAME — CRACKED (BS 1022) · airframe 41,190 hrs · 28,745 cycles

CRACK IN BS 1022 MAIN FRAME AT STRINGER 7L. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1.

Part: BRACKET — CRACKED (BS 735) · airframe 41,190 hrs · 28,745 cycles

CRACKED BRACKET UNDER UPPER CABIN FLOOR, ABOVE CENTER WING FUEL TANK AT APPROXIMATE BS 735 RBL 48. REMOVED AND REPLACED THE BRACKET IAW SRM 51-41-05.

Part: SEAT TRACK — DAMAGED (BS 1020-1053) · corrosion level 2 · airframe 41,190 hrs · 28,745 cycles

LEFT OTBD SEAT TRACK LBL 56 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 1020 - 1053. BLENDED THE AREAS OF CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 PG 105 FIG 103. FABRICATED A NEW SEAT TRACK IAW DWG 9981474 REV.L. AND INSTALLED THE NEW SEAT TRACK IAW SRM 51-41.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 41,190 hrs · 28,745 cycles

RT WING UPPER ACCESS PANEL 620FT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,063 hrs · 28,661 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT A SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,459 hrs · 28,150 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 39,744 hrs · 27,545 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. A MISRIGGED, IMPROPERLY MISSING BUSTLE CABLE CLIP FOR THE SLIDE COVER WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYS AND IS NOT INCOMPLIANCE WITH 14 CFR, PART 121.703. THE TAILCONE SLIDE COVER CABLE CLIP WAS INSTALLED CORRECTLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,583 hrs · 26,647 cycles

SEVERAL EMERGENCY EXIT SIGNS DO NOT ILLUMINATE; 2 BY RT SERVICE DOOR, 1 OVERHEAD FWD CABIN & 1 AFT CABIN BY AFT PRESSURE BULKHEAD. REPLACED EMERGENCY LIGHT BATTERY PACKS B5-118 & B5-260 IAW AMM 33-51, OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,271 hrs · 26,378 cycles

DURING SERVICE CHECK, FOUND OVERHEAD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACKS B101, 102, 104 & B106. CHECKED GOOD.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 36,796 hrs · 25,195 cycles

DURING TAILCONE CHECK, FOUND LT UPPER AND LOWER TAILCONE LATCH ASSEMBLIES WORN. REPLACED LT UPPER AND LOWER LATCH ASSYS IAW AMM 53-52.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,074 hrs · 24,653 cycles

FORWARD LT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — LOOSE (AC BAY) · airframe 36,074 hrs · 24,653 cycles

CAT WALK CEILING EMER LIGHT WIRING LOOSE. SECURED LIGHT IAW SWPM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,677 hrs · 24,377 cycles

RIGHT EXTERIOR OVERWING EMER EVACUATION LIGHTS INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,677 hrs · 24,377 cycles

LEFT EXTERIOR OVERWING EMER EVACUATION LIGHTS INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,677 hrs · 24,377 cycles

LEFT FWD EMER EXIT OVERWING IDENTIFIER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM & WDM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,677 hrs · 24,377 cycles

FORWARD OVERHEAD EMER LIGHT BATTERY CHARGER INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,677 hrs · 24,377 cycles

RIGHT FWD EMER EXIT OVERWING IDENTIFIER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM & WDM.

Part: SIGN — CRACKED (CABIN) · airframe 35,677 hrs · 24,377 cycles

LEFT FWD OVERWING EXIT SIGN LIGHT HOUSING CRACKED. R & R SIGN IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 35,677 hrs · 24,377 cycles

RIGHT FWD OVERWING EXIT SIGN LIGHT HOUSING LIGHT BOARD LOCK CLIP BROKEN. R & R SIGN IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 35,677 hrs · 24,377 cycles

LEFT AFT OVERWING EXIT SIGN LIGHT HOUSING BROKEN ON LIGHT BOARD LOCK CLIPS. R & R SIGN IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

SPLICE CRACKED AT FS 1012 LONGERON 30. R & R SPLICE IAW SRM & DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

LONGERON CHANNEL CORRODED AT BS 954 LONGERON 30L. REMOVED CHANNEL IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

LEFT WING TO BODY FORMER CORRODED AT BS 832. REPAIRED FORMER IAW SRM.

Part: RIB — CRACKED (LE SLAT) · airframe 35,677 hrs · 24,377 cycles

RIGHT WING OTBD END OF SLAT NR 5 RIB CRACKED. R & R NR 5 RIB IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD PANEL 221CF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 222VF PANEL DELAMINATED. R & R PANEL IAW SRM & AMM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 221AF PANEL DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 221KF PANEL DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 221GF PANEL DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 221EF PANEL DELAMINATED. R & R PANEL IAW SRM & AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 222WF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,677 hrs · 24,377 cycles

MAIN CABIN FLOORBOARD 221FF PANEL DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 35,677 hrs · 24,377 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTING AFT CORRODED. R & R FITTING IAW SRM & DWG.

Part: TRIM PANEL — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

R1 DOOR THRESHOLD CLOSE OUT TRIM PANEL CORRODED BETWEEN BS 168 TO 200 RBL 56. R & R PANEL IAW SRM & DWG.

Part: ANGLE — CRACKED (SLAT TRACK) · airframe 35,677 hrs · 24,377 cycles

LEFT WING ON SLAT TRACK 12 INBD SIDE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

R1 DOOR THRESHOLD PLATE CORRODED BETWEEN BS 168 TO 200 RBL 56. R & R PLATE IAW SRM & DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 35,677 hrs · 24,377 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTING FWD CORRODED. R & R FITTING IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

C2 DOOR JAMB LOWER SECTION CORRODED. R & R JAMB PAN IAW AMM & SRM.

Part: DOOR — CRACKED (RT MLG WW) · airframe 35,677 hrs · 24,377 cycles

RIGHT WW DOOR LOWER FWD END CRACKED. REPAIRED DOOR IAW SRM.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

C1 DOOR JAMB SEAL DEPRESSOR LOWER SPLICE PLATE CORRODED. R & R SPLICE IAW SRM & DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,677 hrs · 24,377 cycles

LEFT FUSELAGE SKIN DOUBLER CORRODED BETWEEN BS 851 TO 891. REPAIRED DOUBLER IAW SRM.

Part: HINGE — BROKEN (R1 DOOR) · airframe 24,790 hrs · 24,790 cycles

R1 DOOR SLIDE COVER HINGE BROKEN. R & R DOOR IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,775 hrs · 24,441 cycles

EMERGENCY EXIT ROW LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 33,417 hrs · 22,969 cycles

FWD FLIGHT AFT FLASHLIGHTS INOPERATIVE. CONNECTED BATTERIES TO FLASHLIGHTS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,450 hrs · 22,360 cycles

EMERGENCY EXIT LIGHT BATTERY PACK ASSY INOP AT BS 118. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,955 hrs · 22,680 cycles

LOWER LEFT FUSELAGE SKIN CORRODED BETWEEN STA 851 TO STA 891. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

CUSP WEB CRACKED AT STA 418, LBL 54. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

CUSP WEB CRACKED AT STA 323, LBL 54. REPAIRED WEB IAW SRM.

Part: MOUNT FITTING — CRACKED (CARGO BAY) · airframe 32,450 hrs · 22,360 cycles

FORWARD CARGO AT C1 DOOR WEB LOWER CUT OUT THE SEAT TRACK MOUNTING CLIP CRACKED AT STA 370. REMOVED AND REPLACED CLIP IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 32,450 hrs · 22,360 cycles

RIGHT EMERGENCY LIGHT LENS MISSING AT ROW 20. INSTALLED LENSES IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 32,450 hrs · 22,360 cycles

RIGHT EMERGENCY LIGHT LENS MISSING BETWEEN ROW 12 TO ROW 17. INSTALLED LENSES IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

LOWER LEFT FUSELAGE SKIN CORRODED BETWEEN STA 851 TO STA 891. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 32,450 hrs · 22,360 cycles

RIGHT FWD OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,450 hrs · 22,360 cycles

MAIN CABIN FLOOR PANEL 222 ABF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

LEFT CABIN CUSP WEB CRACKED BETWEEN BS 655 TO BS 674. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

SEAT TRACK CORRODED BETWEEN BS 908 TO BS 998, RBL 54.5. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

SEAT TRACK CORRODED AT STA 379, LBL 54.5. REMOVED AND REPLACED TRACK PER SRM.

Part: LENS — MISSING (CABIN) · airframe 32,450 hrs · 22,360 cycles

EMERGENCY PATH LIGHTING MISSING COVER AT TAILCONE LEFT. INSTALLED LENS IAW AMM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 32,450 hrs · 22,360 cycles

LEFT WING AT WING TO BODY AREA BONDING STRAP CRACKED. REMOVED AND REPLACED STRAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 32,450 hrs · 22,360 cycles

RIGHT ROW 20 MISSING EMERGENCY PATH RED LENS. INSTALLED LENS IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

RIGHT CABIN STA 560-579 CUSP WEB CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

FORWARD LOWER CARGO COMPARTMENT DOOR THRESHOLD JAMB WEB CORRODED BETWEEN STA 403 TO STA 416, RBL 28. REMOVED AND REPLACED WEB IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 32,450 hrs · 22,360 cycles

RIGHT WING AT WING TO BODY AREA UPPER & LOWER BONDING STRAPS CRACKED. REMOVED AND REPLACED STRAP IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

RIGHT CABIN CUSP WEB CORRODED BETWEEN BS 696 TO BS 715. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 465 TO BS 503. REMOVED AND REPLACED WEB PER SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

AFT ACCESSORY COMPARTMENT LONGERON CRACKED AT BS 1194, LONGERON 2L. REMOVED AND REPLACED LONGERON PER SRM.

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 32,450 hrs · 22,360 cycles

AFT CARGO FWD BULKHEAD GILLINER SUPPORTS CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 32,450 hrs · 22,360 cycles

RIGHT OVERWING FORWARD EXIT LIGHT LENS BROKEN. INSTALLED COVER IAW AMM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

AFT ACCESSORY LONGERON CRACKED AT BS 1144, LONGERON 2R. REMOVED AND REPLACED LONGERON IAW SRM.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 32,450 hrs · 22,360 cycles

LEFT WING LEFT APRON CRACKED AT AFT UPPER COWLING LATCH HINGE CUTOUT. REPAIRED CUTOUT PER SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 32,450 hrs · 22,360 cycles

FORWARD CARGO DOOR JAMB CORRODED. REMOVED AND REPLACED PAN IAW SRM.

Part: STRUCTURE — CRACKED (LT COWLING) · airframe 31,775 hrs · 21,948 cycles

LTW(1) MDDR 211779 - LEFT APRON CRACKED AT AFT UPPER COWLING LATCH HINGE CUTOUT SECTION 1 OF TRA 17-54-TR00192. REPAIRED PER SRM.

Part: STRUCTURE — CRACKED (LT COWLING) · airframe 31,775 hrs · 21,948 cycles

LTW(2) MDDR 211779T - LEFT APRON CRACKED AT AFT UPPER COWLING LATCH HINGE CUTOUT SECTION 1 OF TRA 17-54-TR00192. REPAIRED PER SRM.

Part: INVERTER — FAULTY (E&E BAY) · airframe 29,837 hrs · 20,653 cycles

BUS A/C EMERGENCY OFF ALERT ILLUMINATED WHEN TURNING EMERGENCY POWER SWITCH TO ARM. REMOVED AND REPLACED INVERTER PER MM.

Part: LENS — DEFECTIVE (CABIN)

RED EPL LIGHT OUT AT 20DEF SEAT ROW. REPLACED RED EPL LIGHT LENSE AT 20DEF SEAT ROW AS REQUIRED BY MM 33-50-00. OPS CHECKED OK.

Part: COVER — MISSING (CABIN)

ROW 2D, 18 F,E,D EMERGENCY LIGHT COVERS ARE MISSING. INSTALLED EMERGENCY LIGHT COVERS AT ABOVE LOCATIONS - IAW W/B717 AMM 33-50.

Part: LIGHT — MISSING (CABIN)

ESCAPE PATH LIGHTING MISSING BULBS, ROWS 10, 11. INSTALLED BULBS, AS REQUIRED. OPS CHECKED GOOD REF AMM 33-51.

Part: WIRE HARNESS — UNSECURE (CABIN)

SEAT 23F EMERGENCY LIGHTING ELECTRICAL HARNESS HANGING DOWN UNDER SEAT 23F. SECURED ELECTRICAL HARNESS AT 23F IAW B717 AMM 25-23.

Part: WIRE HARNESS — UNSECURE (CABIN)

EMERGENCY LIGHTING ELECTRICAL HARNESS HANGING DOWN UNDER SEAT 24F. SECURED EMERGENCY LIGHTING ELECTRICAL HARNESS AT 24F IAW B717 AMM 25-23.

Part: SPLICE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD LOWER JAMB DOUBLER SPLICE ANGLE, CORROSION. ACCOMPLISHED DOOR CUTOUT FORWARD LOWER JAMB DOUBLER SPLICE ANGLE REPLACEMENT PER B717 SRM 51-10-04 53-00-00, 51-41-02 AND 51-41-05.

Part: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR CUTOUT AFT LOWER JAMB PAN DOUBLER, CORROSION. ACCOMPLISHED DOOR CUTOUT AFT LOWER JAMB PAN DOUBLER REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-05.

Part: BULKHEAD — CORRODED (FUSELAGE)

AFT CARGO FORWARD FACE AFT PRESSURE BULKHEAD, STA 1053, RBL 2, CORROSION. ACCOMPLISHED AFT PRESSURE BULKHEAD DOUBLER REPAIR PER B717 SRM 51-41-05.

Part: CHANNEL — CORRODED (FUSELAGE)

AFT CARGO BILGE AREA, STA 986, LONG 30, CORROSION. ACCOMPLISHED BILGE AREA CHANNEL REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 53-00-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 9 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 179, RBL 22 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FORWARD CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER BOEING DWG SR09530085.

Part: FITTING — CORRODED (GIRT BAR)

GALLEY DOOR FWD GIRT BAR FITTING, CORROSION. ACCOMPLISHED GIRT BAR FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: FITTING — CORRODED (GIRT BAR)

GALLEY DOOR AFT GIRT BAR FITTING, CORROSION. ACCOMPLISHED GIRT BAR FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 256, LBL 8 TO RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-05 AND BOEING DWG PL5930544.

Part: WEB — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR WEB, STA 200, LBL 7 TO RBL 7, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 53-00-00, 51-70-10 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT TRACK, STA 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT TRACK REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK, STA 237, RBL 45, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 51-10-04, 53-20-52 AND BOEING DWG SR09530085.

Part: WEB — CORRODED (FUSELAGE)

E/E COMPARTMENT CEILING FLOOR WEB, STA 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 53-00-00, 51-70-10 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT, STA 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: CHARGER — MALFUNCTIONED (MASTER BATTERY)

BATTERY CHARGER FAIL ALERT AGAIN WITH SMOKE FROM E/E COMPT. REMOVED AND REPLACED 3 SHIPS BATTERIES AND BATTERY CHARGER AS OUTLINED IN 717 M/M 24-34, AND ASSOCIATED SYSTEMS OPERATE NORMALLY AS OUTLINED IN 717 M/M 24-34.

Part: COVER — MISSING (CABIN)

EPL LIGHT COVER MISSING AT ROW 10 AND 11. REPLACED COVER IAW AMM 33-51.

Part: COVER — MISSING (CABIN)

EPL WHITE COVER MISSING AT 3DEF SEAT ROW. REPLACED WHITE COVER AT 3DEF SEAT ROW IAW MM 33-51-00. OPS CHECK OK.

Part: COVER — MISSING (CABIN)

EPL RED COVER MISSING AT 21DEF SEAT ROW. REPLACED RED COVER AT 21DEF SEAT ROW FOR EPL LIGHT IAW MM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN)

ESCAPE PATH LIGHTING AT 10D IS BROKEN. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD. REF MM 33-51.

Part: PLACARD — MISSING (CABIN)

R1 EXIT PLACARD IS MISSING. INSTALLED R1 EMERGENCY EXIT IDENTIFIER LENS, REF 33-51-18.

Part: CABLE — MISSING (DOOR L1 SLIDE)

L1 SLIDE PACK SECONDARY RELEASE CABLE IS MISSING. REMOVED AND REPLACED L1 SLIDE PACK MM 25-61.

Part: SLIDE — UNSERVICEABLE (TAIL CONE)

TAIL CONE EVACUATION SLIDE PRESSURE GAUGE FELL DOWN INSIDE OF CONTAINER. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY IAW B717 MM 25-61-02.

Part: SKIN — DAMAGED (FUSELAGE)

LIGHTNING STRIKE LT SIDE FUSELAGE. REPLACED WINDOW BELT SKIN PANELS STA 313 - STA 403 PER B717 SRM 51-41-02. REPLACED CABIN WINDOWS SAME AREA.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR LOWER PAN CORRODED BEYOND LIMITS FS 954.0 TO 594.0. INSTALLED AFT CARGO LOWER PAN NEW SECTION IAW SRM 52-20-15 TASK 201.

Part: PAN — CORRODED (CARGO DOOR FRAME)

AFT CARGO COMPARTMENT LOWER DOOR FRAME PAN CORRODED BEYOND LIMITS. TRIMMED OUT AFT CARGO AREA, PERFORMED HFEC INSTALLED SPLICES AND NEW PAN PER B717 SRM 52-20-15.

Part: PAN — CRACKED (AFT CARGO DOOR)

WHILE PREPARING TO TAXI A/C FOUND AFT PIT DOOR FWD PAN CRACKED. FABRICATED .063" 2024-T42 REPAIR ANGLE AND .050" 301 1/2 HARD DOUBLER. INSTALLED REPAIR PARTS WITH HLT 434-6 AND HLT 334-6 REFERENCE EA 17-52-01010IR AND SRM CHAPTER 51.

Part: DISPLAY — MALFUNCTIONED (COCKPIT)

AFTER TAKEOFF AIRCRAFT NAVIGATION SYSTEMS WERE UNRELIABLE. COULD NOT INPUT ANY DATA ON MCDU, AUTOPILOT AND THROTTLES WOULD NOT ENGAGE. NO NAVIGATION. REBOOTED AIRCRAFT PWR, PERFORMED RTS ON FCC 1 & 2, GPC, MMR 1 & 2, DME 1 & 2, VIA 1 & 2, VOR 1 & 2, ALL CHECKS GOOD REF'S 22-00, 34-35, 34-35, 34-52, 31-43, 34-32.

Part: WIRE — BROKEN (CABIN)

ROW 17 DEF EMERGENCY EXIT LIGHT INOP (E-PATH). REPAIRED BROKEN WIRE AT SEAT DISCONNECT IAW SWPM 20-10-01, OPS CHECK NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT SEATS 11-19 AND 25-31 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER B717 M/M 33-51-03 AT STATION 804R, OPS CHECK GOOD.