N924AT

Part: ACM — SEIZED · airframe 58,081 hrs · 42,183 cycles

SHIP 9575 FUME EVENT ON DESCENT. ACM WAS FOUND SEIZED, REPLACED RT ACM AND BOTH COALESCER BAG ASSY. (8047459)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,835 hrs · 41,959 cycles

AFT OVER WING EXIT LIGHTS OUT ON BOTH SIDES OF A/C. T/S PER B717 FIM 33-50-00-201 R/R BATTERY ASSY P/N 803949-1 PER B717 AMM 33-51-03 (6532441)

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 57,750 hrs · 41,880 cycles

SHIP 9575 AFT BULKHEAD DOOR CAUTION MESSAGE ON DECENT 26000 AND CLEARED AT 7000, REAPPEARED ON LANDING. CORRECTIVE ACTION: T/S PER B717 FIM 52-70 TASK 809. FOUND "A CABIN DR" AT 86%/NEAR ADJUSTMENT RECCOMMENDED. (7816676)

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 57,750 hrs · 41,880 cycles

SHIP 9575 AFT BULKHEAD DOOR MESSAGE ILLUMINATED ON DECENT THROUGH FL180- 8000 CAME ON AGAIN DUREING APPROACH. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN DOOR PROX SENSOR PER B717 AMM 52- 70. (7816682)

Part: LATCH — DIRTY (GIRT BAR) · airframe 57,750 hrs · 41,880 cycles

SHIP 9575 1L DOOR GRIT BAR VERY DIFFICULT TO ARM SLIDE. CORRECTIVE ACTION: FOUND BOTH 1L DOOR RETENTION LATCHES STICKY AND DIRTY. CLEANED AND VERIFIED NORMAL OPERATION REF B717 AMM 25-61. (7816646)

Part: HINGE FITTING — EXCESS PLAY (ZONE 600 FLAP) · airframe 57,697 hrs · 41,841 cycles

RT WING FLAP O/B HINGE HAS EXCESSIVE PLAY. REPAIRED PER ERA/PRI 629650-14 REV. A (1274899).

Part: BRACE — NOT REPORTED (ZONE 500) · airframe 57,193 hrs · 41,361 cycles

SHIP 9575 LH WING BRACE FITTING BEING REPLACED. CORRECTIVE ACTION: BRACE FITTING INSTALLED ON ERA622844-14AD (1047886)

Part: NONE — NONE (NONE) · airframe 57,193 hrs · 41,361 cycles

SHIP 9575 DTE, 624256-14AD. CORRECTIVE ACTION: ACCOMPLISH DTE FOR ERA 622844-14AD (1033944)

Part: INSPECTION — NONE (NONE) · airframe 57,189 hrs · 41,356 cycles

SHIP 9575 AMOC, ERA 624259-14AD. CORRECTIVE ACTION: CURRENT AMOC APPROVAL IS LIMITED TO 24 MONTHS. ADDITIONAL ERA REVISION IS REQUIRED FOR AMOC APPROVAL BEYOND 17-JUN-2027 FOR ERA 624259-14AD (1033908)

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,155 hrs · 41,328 cycles

R/H FRAME ON STATION Y1133 DAMAGED NEAR LONGERON R8. REMOVED DAMAGED FRAME REF B717 SRM 53-20-07-2R PROCEDURE 1. FABRICATED, ALODINE, PRIMED, AND PAINTED REPAIR FRAME SPLICE PARTS FOR SPLICE R4-R5 LONGERON. FRAME GOES DOWN TO PRODUCTION SPLICE RIGHT PER B717 SRM 53-20-07-02R PROC 1 REPAIR 1. INSTALLED COMPLETED SPLICE REPAIR PER B717 SRM 53-20-07-02R PROC 1 REPAIR 1. (LP #0637929)

Part: LONGERON — DAMAGED (ZONE 200) · airframe 57,150 hrs · 41,322 cycles

LONGERON R8 AT STATION Y1133 DAMAGED. REMOVED DAMAGED R8 LONGERON 16.5 INCHES OF MATERAL SURROUNDING Y1133 REF 53-00-05-2R PROCEDURE 2. PERFORMED DAMAGE CONTAMENT HFEC IAW MDC93K0393-NDT SPM. NO FURTHER DAMAGE FOUND. FABRICATED, PAINTED, AND INSTALLED R8 REPAIR SPLICE PER B717 SRM 53-00-05-2R PROC 2. RII COMPLETE. (LP #0623114)

Part: FIRE DETECTOR — FALSE INDICATION (APU) · airframe 56,317 hrs · 40,585 cycles

SHIP 9575 -ATB/DE- AS THE AIRCRAFT CLIMBED OUT ON DEPARTURE, THE APU FIRE WARNING (LEVEL 2) ACCOMPANIED BY THE MASTER CAUTION, ALL ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT BACK TO DTW. THE LANDING WAS UNEVENTFUL AND ARFF SCANNED THE AIRCRAFT WITH NO HOTSPOTS LOCATED. NORMAL TAXI TO THE GATE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU FIRE DETECTION CONTROL UNIT. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #5892292)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 55,838 hrs · 40,170 cycles

AD -- OPEN HOLE HFEC (BHEC) INDICATED CRACK 2 FASTENER HOLES BELOW EXISTING DOUBLER ON RT VERT L/E. MARKED. FOUND ON STEP 12 OF AA 5530-01048 AD 2018-10-08. SEPERATED EXTERIOR LATERS ON R/H VERT STAB FRONT SPAR CAP PER AA 5530-01048-02 STEP 13. PERFORMED OPEN HOLE HFEC (BHEC) AND NO LONGER HAVE CRACK INDICATION PER AA 5530-01048-02 STEP 14 & 17. (LP #5306111)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,363 hrs · 39,746 cycles

DURING SERVICE CHECK FOUND AFT OVER WING (RT/LT) EMERGENCY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726 AND STA 803 IAW B717 AMM 33-51-03. PERFORMED OPERATIONAL CHECK IAW B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #0159634)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,189 hrs · 39,602 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5549256)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,991 hrs · 39,441 cycles

WHILE WORKING AD TASK CARD 2540-01288-01, NOTED FWD LAV & AFT RT LAV WASTE RECEPTACLE FLAPPER DOORS WILL NOT FULLY CLOSE. ADJUSTED SPRING TENSION ON BOTH SPRINGS OF AFT LAV FLAPPER DOOR AND REPLACED BROKEN SPRING IN FWD LAV FLAPPER DOOR PER B717 AMM 25-40. OPERATIONAL CHECK WAS GOOD. BOTH FLAPPER DOORS NOW CLOSE FULLY. (LP #9563228)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,860 hrs · 39,337 cycles

THE EMERGENCY EXIT LIGHT COVER OVER ROW 29 FELL OFF. MAINTENANCE REPLACED THE EXIT LIGHT LENS. (LP #4997060)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,170 hrs · 38,720 cycles

AFTER REMOVAL OF THE RECHARGEABLE BATTERY ASSEMBLY, THE RECEPTACLE PINS WERE FOUND DAMAGED. THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REMOVED PER B717-200 AMM 33-51-06 000-801. SUMMARY OF NRC 00257: THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS INSTALLED PER B717 AMM 33-51-06. SATISFACTORY TEST. (LP #2855587)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053. SUMMARY OF NRC 00367: CORROSION LEVEL 2. FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053 WAS REPAIRED PER PRI 609849-14 REV 0 AND REV 1 AND ERA 609849-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-609849 ADDED FOR AC 9575. (LP #2851152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00633: CORROSION LEVEL 2. CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 REPAIR 3. (LP #2849667)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

DURING REMOVAL OF FLOOR SUPPORT, CRACK AND CORROSION ON CUSP WEB Y=199 TO Y=160 X54 (CPAX) WAS FOUND. SUMMARY OF NRC 00598: CORROSION LEVEL 2. CUSP WEB WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2847871)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT OF MAIN ENTRANCE DOOR FROM STA Y=162 TO STA Y=194 & LBL 54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00381: CORROSION LEVEL 2. SUPPORT WAS FABRICATED AND REPLACED PER DWG S00074, B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2847508)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON MEMBRANE (LWR SEAT TRACK AREA) IN STA Y=220 AND X=55 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00648: MEMBARANE WAS REPLACED PER B717-200 SRM 53-00-55-0R PROCEDURE 4 REPAIR 4 AND 53-20-51-0I PROCEDURE 1. (LP #2847901)

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 55,558 hrs · 39,920 cycles

CORROSION ON INBD/OUTBD ATTACHMENT POINTS OF CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR. SUMMARY OF NRC 00167: CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR WAS REPLACED PER B717 AMM 57-55-25. LEVEL N/A BECAUSE IS NOT A PRIMARY STRUCTURE. (LP #2845100)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON FRAME STA 1037 BTW LONGERON 17 LH AT CABIN. SUMMARY OF NRC 00239: FRAME STA 1037 BTW LONGERON 17 LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2844142)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

FLOOR PAN BTW RBL 43 AND LBL 0 BTW STA Y=160 AND STA Y=193 AT CPAX CABIN WAS FOUND WITH CORROSION DAMAGE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PARAGRAPH 4. C. FIGURE 103 AND DC-MD/BOEING NDT SPM PART 4 FIG 9. (REFERENCE TO NRC 211). SUMMARY OF NRC 00607: CORROSION LEVEL 2. FLOOR PAN BTW RBL 43 AND LBL 0 BTW STA Y=160 AND STA Y=193 WAS MANUFACTURED AND REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 IDENTIFICATION 2, 51-41-02-0G, AND 51-41-05-0G. (LP #2841557)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR FITTING BTW STA Y=218 AND RBL 9 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00614: CORROSION LEVEL 2. FLOOR FITTING BTW STA Y=218 AND RBL 9 AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 5968021 REV AND B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2840730)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00452: CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 WAS REPAIRED PER PRI 608991-14 REV 2 AND ER/A 608991-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-608991 ADDED FOR AC 9575. (LP #2838518)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON RH SEAT TRACK X-22 BTW STA Y=197 TO STA Y=266 AT PAX CABIN WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.100 IN. REMAINING THICKNESS IS 0.050 IN. THEREFORE, AREA IT IS OUT OF LIMITS PER B717-200 SRM 53-20-52-1A ALLOWABLE DAMAGE 1 PARAGRAPH 4. C. FIGURE 101. SUMMARY OF NRC 00486: CORROSION LEVEL 2. SECTION OF SEAT TRACK X-22 BTW STA Y=197 TO STA Y=266 AT PAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5, 51-41-01-0G, AND 51-41-05-0G. (LP #2830725)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON SEAT TRACK X=-44 BTW STA 197- 217, OUT OF LIMIT. SUMMARY OF NRC 00606: CORROSION LEVEL 2. SECTION OF SEAT TRACK X=- 44 BTW STA 197-217 WAS REPLACED AND INSTALLED PER B717-200 SRM 51-40-02-0G AND 51-41-01-0G. (LP #2830727)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORTS (2EA) STA Y:148 APPROX BTW -X:22 TO -X:56 AT CABIN PAX. SUMMARY OF NRC 00473: CORROSION LEVEL 2. FLOOR SUPPORT (1EA) STA Y:148 APPROX -X:56 AT CABIN PAX WAS REPLACED AND INSTALLED PER DWG 9936533 REV. CM AND B717-200 SRM 51-41-02-0G AND 51-41-08-0G AND FLOOR SUPPORT (1EA) STA Y:148 APPROX BTW -X:22 AT CABIN PAX WAS ATTENDED WITH NRC 00215. (LP #2830715)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION FOUND ON MENBRANE STA Y=200 TO STA Y=218 AND X=60 TO X=22 AT PASSENGER CABIN. SUMMARY OF NRC 00645: CORROSION LEVEL 2. MEMBRANE STA Y=200 TO STA Y=218 AND X=60 TO X=22 WAS FABRICATED AND REPLACED PER DWG 9936535-3 REV CS. (LP #2831368)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TRACKS (2 EA) BTW LBL 8 AND RBL 8 BTW STA Y=148 AND STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR TRACKS (2 EA) BTW LBL 8 AND RBL 8 BTW STA Y=148 AND STA Y=193 AT CPAX CABIN WERE REPLACED AND INSTALLED PER B717-200 SRM 53-10-51-01-2 AND 51-41-01-0G PAR 6. (LP #2828449)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00212: CORROSION LEVEL 2. FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT CPAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-05-0G. (LP #2828746)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2827439)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMPARTMENT C-1. SUMMARY OF NRC 00447: FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02 -0G AND 51-41-02-0G. (LP #2824613)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON INNER SURFACE OF CUSP WEB MEMBRANE LH STA Y=655. SUMMARY OF NRC 00223: CUSP WEB MEMBRANE LH STA Y=655 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2822605)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

SEVERAL AREAS OF CORROSION ON FLOOR SUPPORT BTW RBL 9 AND RBL 39 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00213: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 9 AND RBL 39 STA Y=193 WAS REPLACE AND INSTALLED PER DWG S2929169 REV B AND B717-200 SRM 51-41-05-0G. (LP #2821958)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT CPAX CABIN. SUMMARY OF NRC 00218: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT CPAX CABIN WAS REPLACED PER DWG S2932222 REV A AND B717-200 SRM 51-41-02-0G. (LP #2820357)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON GUSSET BELOW AFT ACCESSORY COMPARMENT DOOR RBL 15 STA Y=1072 AT CPAX CABIN. SUMMARY OF NRC 00378: CORROSION LEVEL 2. GUSSET BELOW AFT ACCESSORY COMPARMENT DOOR RBL 15 STA Y=1072 AT CPAX CABIN WAS REPLACED PER DWG 3925389 REV A AND B717-200 SRM 51-41-05-0G. (LP #2821155)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00567: CORROSION LEVEL 2. LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 219. (LP #2819734)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON LOWER SKIN AT CUSP WEB MEMBRANE STA 634. SUMMARY OF NRC 00149: LOWER SKIN AT CUSP WEB MEMBRANE STA 634 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG.221. (LP #2819538)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00566: CORROSION LEVEL 2. LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #2818952)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CORROSION ON UPPER SIDE AND LOWER SIDE OF CUSP WEB BTW STA Y=200 TO STA Y=220 AT PASSENGER CABIN. SUMMARY OF NRC 00203: CORROSION LEVEL 2. CUSP WEB BTW STA Y=200 TO STA Y=220 AT PASSENGER CABIN WAS REPLACED PER DWG #9936535 REV CS AND B717-200 SRM 51-41-02-0G. (LP #2816784)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1. SUMMARY CORROSION LEVEL 2. FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02-0G. (LP #2809951)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON SUPPORT ANGLES ON STA 271.5, 291, 305, 311, 539, 647, 847, 874, 883, AND 924 AT CUSP WEB LH. SUMMARY OF NRC 00143: CORROSION LEVEL 2. NEW CLIPS WERE INSTALLED PER B717-200 SRM 51-41-02-0G. (LP #2808532)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON INTERCOSTAL BTW STR 30 AND STR 29RH FROM STA Y=946 TO 954 AT AFT CARGO. SUMMARY OF NRC 00275: CORROSION LEVEL 2. NEW INTERCOSTAL WAS REPLACED PER B717 SRM 51-41-02-0G PAR 4. (LP #2804838)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON FRAME ANGLE BTW STA Y=1022 AND L-12RH TO L-14RH AT PASSENGER CABIN. SUMMARY OF NRC 592: FRAME ANGLE BTW STA Y=1022 AND L-12RH TO L-14RH WAS REPLACED PER DWG 9912243 REV JS. (LP #2800077)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,161 hrs · 38,713 cycles

CRACK ON FLOOR PANEL OF FWD CARGO COMPARTMENT. SUMMARY OF NRC 00499: FLOOR PANEL OF FWD CARGO COMPARTMENT WAS MANUFACTURED PER ER/A 591778-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. PANEL INSTALLED PER AMDS 2040-0006. ASSOCIATED ER/A 14-591778 ADDED FOR AC 9575. (LP #2799882)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON LH/RH CUPS WEB MEMBRANE AT STA Y=1045 AT CPAX CABIN. SUMMARY OF NRC 00369: CORROSION LEVEL 2. LH/RH CUPS WEB MEMBRANE AT STA Y=1045 AT CPAX CABIN WERE REPLACED PER DWG 9981474 REV L AND B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41 -05-0G. (LP #2797544)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,161 hrs · 38,713 cycles

CORROSION ON FLOOR SUPPORT RBL 54 STA Y=1050 AND Y=1054 AT CPAX CABIN. SUMMARY OF NRC 00374: CORROSION LEVEL 2. FLOOR SUPPORT RBL 54 STA Y=1050 AND Y=1054 AT CPAX CABIN WAS REPLACED PER DWG 9981474 REV L AND B717-200 SRM 51-41-05-0G. (LP #2793392)

Part: BUCKLE — DIRTY · airframe 53,346 hrs · 38,036 cycles

AFT FLIGHT ATTENDANT JUMPSEAT HARNESS BUCKLE WILL NOT RELEASE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED DEBRIS FROM THE HARNESS BUCKLE PER B717 AMM 25-23. (LP #9831886)

Part: SLIDE — DISPLACED · airframe 53,289 hrs · 37,985 cycles

WHILE PERFORMING OTHER MAINTENANCE, FOUND THE AFT EMERGENCY EXIT ESCAPE SLIDE NOT STOWED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REINSTALLED THE AFT EMERGENCY EXIT SLIDE PER AMDS WORK CARD 2561-9006. RII COMPLETE QC 5107. (LP #9831857)

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,028 hrs · 37,762 cycles

ON APPROACH, THE CREW REPORTED A LIGHTNING STRIKE AND A SIMULTANEOUS COMPRESSOR STALL (WITH EICAS MESSAGES) ON THE #1 ENGINE. ALL ENGINE PARAMETERS REMAINED NORMAL. THE CREW DID DECLARE AN EMERGENCY WITH ATC. MAINTENANCE PERFORMED AN AIRCRAFT LIGHTNING STRIKE INSPECTION AND FOUND THE RIGHT ELEVATOR STABILIZER OUTBOARD STATIC WICK TO BE DAMAGED AND REPLACED IT. PERFORMED A #1 ENGINE LIGHTNING INSPECTION AND NO WAS DAMAGE FOUND. THE P30 SENSOR WAS CLEANED THOUGH.

Part: WIRE — BROKEN · airframe 52,536 hrs · 37,341 cycles

SIDE WINDOW HEAT WIRES SPARKED AND DISCONNECTED. *** CONTRACT MAINTENANCE EVENT - OCM: 251010 *** FOUND 2 WIRES FOR CAPT CLEARVIEW WINDOW ANTI-FOG BROKEN. PERFORMED TIME LIMITED REPAIR PER ERA 601364-14 REV ORIGINAL. PERMANENT REPAIR IAW THIS ERA IS REQUIRED. DEFER ANTI-FOG SYSTEM TO MEL 30-41-01A . M PROCEDURES C/W. PERFORMED PERMANENT WIRING REPAIR IAW ERA 601364-14 SECTION II, REV ORIGINAL. OPERATIONAL CHECK WAS GOOD IAW B717 AMM 30-42. PLACARD REMOVED. MEL CLEARED. (LP #9234090)

Part: BATTERY PACK — INOPERATIVE · airframe 52,184 hrs · 37,021 cycles

THE TAIL COMPT EMERGENCY LIGHTS ARE INOPERATIVE. TO INCLUDE THE TAILCONE SLIDE AND PATHWAY CEILING LIGHTS. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-116, PER B717 AMM 33-51. (LP #8823894)

Part: NONE — NONE · airframe 51,801 hrs · 36,657 cycles

SHIP 9575 - THE TAKEOFF WAS SAFELY ABORTED AT 141 KNOTS DUE TO A LEFT ENGINE COMPRESSOR STALL. AN EMERGENCY WAS DECLARED WITH THE DTW TOWER, THUS ARFF MET AND INSPECTED THE AIRCRAFT AFTER IT CLEARED THE RUNWAY. THE ALL CLEAR WAS GIVEN AND THE AIRCRAFT TAXIED TO THE GATE UNDER IT'S OWN POWER. CORRECTIVE ACTION: MAINTENANCE PERFORMED A BORESCOPE AND FOUND MULTIPLE BLADES OUT OF LIMITS ON THE FIRST STAGE HPC. THE ENGINE WAS REPLACED. (LP #8793748)

Part: POWER SUPPLY — INOPERATIVE · airframe 51,720 hrs · 36,591 cycles

EMERGENCY WING LIGHTS REMAIN ON WITH SWITCH OFF AND POWER REMOVED FROM PLANE. EXTERIOR EMERGENCY ILLUMINATION SYSTEM FWD TO MEL 33-51-02A FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. EXT EMER LIGHTS INOP. DAYLIGHT ONLY OPS. TROUBLE SHOT PER B717 FIM 33-50-00 810-801 AND FOUND BAD BATTERY POWER SUPPLY B5-125. REPLACED BATTERY POWER SUPPLY B5-125 PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT OK FOR SERVICE. MCO/PLAC RMVD. (LP #8793712)

Part: LIGHT — INOPERATIVE · airframe 51,720 hrs · 36,591 cycles

THE OVERWING LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8793707)

Part: NONE — NONE · airframe 51,446 hrs · 36,340 cycles

BOTH OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK FOR THE OVERWING LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7860334)

Part: BATTERY PACK — FALSE INDICATION · airframe 51,156 hrs · 36,095 cycles

(8127554) AFT EMERGENCY LIGHTS ILLUMINATED. R/R AFT EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51.

Part: NONE — NONE · airframe 50,892 hrs · 35,855 cycles

ALL EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-125. THE EXTERIOR EMERGENCY LIGHTS NOW CHECK GOOD. (LP #7903688)

Part: NONE — NONE · airframe 50,612 hrs · 35,570 cycles

SHIP 9575 - THE NOSE LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED ON APPROACH. THE CREW COMPLIED WITH THE QRH AND PERFORMED THE ALTERNATE GEAR EXTENSION PROCEDURES. THE GREEN SAFE INDICATION DID ILLUMINATE WHILE ON FINAL APPROACH AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE ADJUSTED THE NOSE LANDING GEAR LOCK LINK ASSEMBLY. THE MAIN GEAR DOORS WERE REPLACED DUE TO CONTACT WITH THE RUNWAY ON LANDING. (LP #8070874)

Part: FRAME — CRACKED (BS 696) · airframe 50,140 hrs · 35,160 cycles

LEFT HAND F.S. 696.000 FRAME IS CRACKED CONDITION 3 (GREATER THAN 0.125"). REPLACED THE LEFT HAND OVERWING FRAME AT STA.696 PER AMDS CARD 5310-01436- 03A. (LP #1844974)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

LEFT WING HAS CORROSION ON UPPER SURFACE, FRONT SPAR. XRS 250, IN LINE WITH THE I/B END OF #3 SLAT. -MARKED-. REPAIR COMPLETE PER PRI 592003-14 REV. 0, 1, 2 AND 3, FINAL ER/A 592003-14 REV. 0 MATCHES PRI 592003-14 REV. 0,1,2 AND 3. (LP #1845263)

Part: INTERCOSTAL — CORRODED (BS 1028 S30) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

AFT CARGO INTERCOSTAL ABOVE STR 30 IS CORRODED AT FRAME 1028, AFT SIDE. NRC 247: SUMMERY - REPLACED INTERCOSTAL ABOVE STR 30 AT FRAME 1028 PER B717 SRM 53-20-04 PROCEDURE 3. (LP #1842038)

Part: FRAME — CORRODED (BS 908 L28R-29L) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

AFT CARGO COMPARTMENT HAS CORROSION ON FRAME AND FRAME CLIP STA 908 BETWEEN L29L & 28R. NRC 258 - SUMMARY: REPLACED FRAME CLIP PER DWG 9915524. (LP #1842039)

Part: LANYARD — FRAYED (TAIL CONE) · airframe 50,135 hrs · 35,155 cycles

THE KEVLAR DEPLOYMENT LANYARD FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE LANYARD PER B&!& AMM 53-52-01.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

FLOOR SUPPORT CORRODED AT L-1 DOORWAY APPROX. 11 IN INBD OF FLOOR PAN, FROM STA 160 TO STA 200. SUMMARY - NRC 001-0024:2040-0024/001 00358: REPLACED FLOOR SUPPORT PER BAC DWG 9936534. (LP #1841878)

Part: FRAME — CORRODED (BS 1028 S30) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

AFT CARGO FRAME 1028 (AFT BULKHEAD) IS CORRODED ON AFT SIDE ABOVE STR30. MARKED. NRC 041-0008:5331-2001/002 00246: REPAIRED CARGO FRAME 1028 PER B717 SRM 53-20-07 REPAIR 3. (LP #1841380)

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 50,135 hrs · 35,155 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE KEVLAR CABLE PER IPC 53-52-30-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001 TAILCONE SERVICE. FUNCTIONAL CHECK WAS SATISFACTORY. (LP #1840034)

Part: PAN — CORRODED (BS 1022) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

CORROSION FOUND AT STA 1022. NRC 002-0001:21-0553-8- 5566/004 00292: REPLACED LAV SERVICE PAN DOUBLER PER ER/A 568263-14 REV. A. (LP #1838628)

Part: LONGERON — CORRODED (BS 890-930 S29L) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

AFT CARGO COMPARTMENT HAS CORROSION ON LONGERON 29L FROM STA 890 TO 930. *MARKED*. NRC 041-0008:5331-2001/017 00265: REPLACED LONGERON PER B717 SRM 53-20-05-2R AND SRM 53-00-05-2R. CLOSING REQUIREMENTS RII: INSPECTOR 00670737. (LP #1838627)

Part: STRAP — CORRODED (BS 954 S28R) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

AREA OF CORROSION FOUND ON TOP SURFACE OF FLOOR STRUCTURE STRAP IN AFT CARGO JUST INSIDE OF DOOR AND JUST FORWARD OF STA. 954 AND ABOVE LONGERON 28R- MARKED. NRC 001-0369:0593-2006/004 00127: REPLACED STRAP PER B717 SRM 51-40-02. (LP #1835143)

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

THE WEB JUST ABOVE C2 DOOR THRESHOLD IS CORRODED, AT FWD END, NEAR FWD DOOR OPENING, APPROXIMATELY 14" FROM DOOR (MARKED). NRC 001-0369:0593-2006/011 00288: REPLACED WEB PER B717 SRM 51-40-02. (LP #1835144)

Part: THRESHOLD — CORRODED (FWD CARGO) · corrosion level 2 · airframe 50,135 hrs · 35,155 cycles

LIGHT CORROSION AT FORWARD CARGO THRESHOLD- MARKED. NRC 001-0281:0593-2007/003 00120: REPLACED FWD CARGO LOWER DOOR PAN REF B717 SRM 53-20-15-2R-6 . (LP #1833922)

Part: CABLE — CORRODED (TAILCONE DOOR) · airframe 50,135 hrs · 35,155 cycles

THE CABLE COMING FROM THE INTERIOR RELEASE HANDLE THAT GOES OUT TO A "Y" SPLIT CONNECTION HAS CORROSION ON IT. MARKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 001-0316:5353-2001/002 00183: CLEANED CABLES PER B717 AMM 20-00-02 AND RE-INSPECTED. (LP #1824223)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,578 hrs · 34,691 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THAT THE AFT EMERGENCY EXIT LIGHTS, LEFT AND RIGHT, ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,189 hrs · 34,396 cycles

DURING SVC, FOUND EMERGENCY LIGHT ABOVE L1 DOOR INOP. R/R BATTERY PACK (B5-123) ABOVE R1 SERVICE DOOR PER B717 AMM 33- 51. OPS CKS GOOD. (LP6066846)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,988 hrs · 32,800 cycles

THE EMERGENCY LIGHT BATTERY PACK, B5-259, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, B5-259, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5312310)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,338 hrs · 31,587 cycles

SEVERAL CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THEM ALL PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 45,289 hrs · 31,556 cycles

THE 1L DOOR EMERGENCY EXIT LIGHT WAS NOTED TO BE INOPERATIVE. MAINTENANCE FOUND THAT THE POWER SUPPLY FOR THE DOOR SIGN HAD FAILED AND THEY REPLACED PS B5-123 AND BATTERY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: PLATE — DAMAGED (CARGO DOOR) · airframe 42,383 hrs · 29,446 cycles

AFT CARGO DOOR SEAT PLATE PULLED AWAY FROM FUSELAGE. REPAIRED IAW ER/A (2) 555305-1, SECTION 1, STEPS 1-8.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 41,558 hrs · 28,871 cycles

THE PILOT REPORTED THAT THE CENTER ISLE EXIT SIGN AT THE OVERWING EXIT HATCH IS CRACKED AND HANGING DOWN. MAINTENANCE ADJUSTED THE CORNER OF THE EXIT SIGN AND RETURNED THE EMERGENCY LIGHTS TO SERVICEABLE CONDITION.

Part: WEDGE — DAMAGED (RT SPOILER)

DURING NON-ROUTINE LINE UNSCHEDULED INSPECTION OF RT SPOILER AFT WEDGE FOUND DAMAGED.

Part: SKIN — CORRODED · corrosion level 2 · airframe 40,418 hrs · 27,977 cycles

UPPER WING TO CENTER TANK PLANK ON FORWARD BULKHEAD CORRODED FROM BL0 TO RBL 58. REPAIRED UPPER CENTER TANK PLANK SKIN IAW ER/A 545622-14, REV A.

Part: SPRING — MISSING (TAILCONE RELEASE) · airframe 40,418 hrs · 27,977 cycles

DURING THE TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THE TAIL CONE FAILED TO DROP BECAUSE A SINGLE SPRING WAS MISSING FROM A RELEASE CABLE SYSTEM PIN. THE SPRING WAS INSTALLED AND THE SYSTEM WAS SUCCESSFULLY FUNCTIONALLY CHECKED IAW AMM 53-52-01 720-805.

Part: FORMER — CRACKED (BS 660) · airframe 40,418 hrs · 27,977 cycles

FORMER CRACKED BS 660. REPAIRED IAW ER/A 545665-14, REV 0 AND NDT SPM PORT 606-10-01.

Part: FORMER — CRACKED (BS 660) · airframe 40,418 hrs · 27,977 cycles

2 FORMERS CRACKED INTERNAL STRUCTURE OF THE CANTED KEEL, RT OTBD SIDE AT BS 660.0 AND 675.5. REMOVED R1 AND R2 WING TO BODY FRAMES, HYD LINES, AND FORMERS AT BS 660 AND 675.5 RT. FABRICATED REPAIR ANGLES AND FILLERS. HEAT TREATED REPAIR ANGLES AND FILLERS TO 7075-T6. TREATED AND PRIMED REPAIR ANGLES AND FILLERS. PERFORMED HFEC AT CUTOUTS AND HOLES COMMON TO REPAIR AREA WITH NO DEFECTS NOTED, TAG 6782. INSTALLED AND CIC REPAIR ANGLES AND FILLERS AT BS 66 AND BS 675.5, INSTALLED WING TO BODY FRAMES AND HYD LINES IDENTIFIED, REPAIRED AND COMPLIED WITH ER/A 545665-14, REV 0. LEAK CHECK PERFORMED, NO LEAKS IAW ER/A 545665-14, REV 0 AND AMM 29-00-00-200-802. ASSOCIATED ER/A 00-545665 ADDED FOR AC 9575.

Part: SKIN — CRACKED (BS 1076) · airframe 40,418 hrs · 27,977 cycles

EXTERNAL FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED CRACKED AREA WITH FILLER END DOUBLER RT PANEL DUCT REMOVED AND REINSTALLED LEAK CHECK COMPLETED IAW AMM 36-00-00-863-804 IAW PRI 545666-14, REV 2.

Part: CUSP WEB — CORRODED (BS 193) · airframe 40,418 hrs · 27,977 cycles

CORROSION FOUND ON CUSP WEB, BS 193, LBL56. REPAIRED CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 40,418 hrs · 27,977 cycles

LOWER BEAM CRACKED AT HINGE ATTACH POINT ON RIGHT GALLEY SERVICE DOOR. REMOVED R1 DOOR LOWER BEAM AND REPLACED IAW SRM 51-40-08, PAR 3, 51-41-02, PAR 4, 51-41-05, FIG 1, AND 51-41-01, FIG 2. TOOL TAG 6782.

Part: SEAL — DAMAGED (RT SPOILER)

DURING NON SCHEDULED ROUTINE CHECK FOUND DAMAGED RT INBD SPOILER T/E SEAL.

Part: SEAT TRACK — DAMAGED (BS 148-1022) · airframe 40,418 hrs · 27,977 cycles

LEFT CTR SEAT TRACK, BS 148-1022, BL44.5 HAS MULTIPLE DISCREPANCIES. BLENDED MULTIPLE DISCREPANCIES ON LT CTR SEAT TRACK FROM BS 148 TO 1022 REMOVED .004" FROM TOP REMAINING .136" REMOVED .011 IN CENTER OF TRACK REMAINING .099" FOUND TO BE WITHIN LIMITS AT STA 332-1022 IAW SRM 53-20-52 ALLOWABLE DAMAGE 1, PAR 4A, FIG 101, SEAT TRACK SPLICED FROM BS 148-332 OUT OF EXTRATION IAW SRM 53-20-52, REPAIR 5 ALODINED BLENDED AREAS IAW SRM 51-10-04, ITEM 4 PRIMED ALODINED AREAS IAW SRM 51-10-04, PG 16, PAR 12 A TOP COATED PRIMED AREAS IAW AMM 51-10-370-803.

Part: FRAME — CORRODED (BS 870) · airframe 40,418 hrs · 27,977 cycles

ALC FRAME BS 870 AT LONGERON CORRODED. CLEAN, EVALUATED, TREAT WORK WITH ORNRC 0100-0101. REPAIRED FRAME AT FS 870 BETWEEN 29L AND 29R. REMOVED FASTENER IAW SRM 51-41-01, BLENDED AREA IAW SRM 53-00-00, FIG 103, REMOVING OUT OF LIMITS AREA IAW SRM 53-20-07, REPAIR 3 AS MEASURED BY UT TOOL TAG 6785, ORIGINAL THICKNESS .063, REMOVED .033. INSTALLED DOUBLERS, CHANNEL, AND FILLER IAW SRM 53-20-07, REPAIR PARTS ALODINED IAW DPS-900-2-4-1, NR 2 AND PRIMED IAW DPS 900-3-6, NR 03. REMOVED PARTS AND FASTENERS INSTALLED IAW SRM 51-41-02 AND SRM 51-41-05. TOP COATED REPAIRED AREA IAW DPS 900-3-6 NR 03.

Part: FITTING — CORRODED (COCKPIT) · airframe 40,418 hrs · 27,977 cycles

CORROSION FOUND UNDER FLIGHT DECK FLOOR PANEL 211ANF F/O AFT OTBD SEAT TRACK FITTING. CHECK LIMITS, CLEAN, BLEND 53-00-00. BLENDED CORROSION ON SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105, FIG 103. REPLACED SEAT TRACK F/O AFT OTBD SEAT TRACK IAW SRM 51-11-01.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 40,418 hrs · 27,977 cycles

AFT CARGO SCUFF PLATE CRACKED AT FWD INBD END AND SAME END DOES NOT SET FLUSH WITH FLOOR PANELS. WELD REPAIR SCUFF PLATE. REF ORNRC 66531-0100-0005. AFT CARGO SCUFF PLATE FWD INBD REPAIR IAW STEPS 3 THRU 7 IAW ER/A 54149-14MA. W/O 66532-0012 FOR ALL MAINTENANCE PERFORMED.

Part: FRAME — CORRODED (BS 889) · airframe 40,418 hrs · 27,977 cycles

ALC FRAME BS 889 CORRODED BETWEEN LONGERON 29L-29R. REPAIRED FRAME AT FS 889 BETWEEN LONGERON 29L AND 29R BY BLENDING AREA IAW SRM 53-00-00, FIG 103, REMOVED SECTION THAT WAS OUT OF LIMITS IAW SRM 53-20-07, AND INSTALLED REPAIR FILLER, CHANNELS IAW SRM 53-20-07, ALODINED FILLER AND REPAIR CHANNELS IAW DPS 900-2-4-1 NO. 2 AND DPS 900-3-6 NR 03, AND TOPCOATED AREA IAW DPS 900-3-6 NR 3. REPAIR FILLERS AND CHANNELS WHERE HEAT TREATED. FASTENERS WHERE INSTALLED IAW SRM 51-41-01, 51-41-02, AND 51-41-05. L ANGLE ON FWD SIDE OF FRAME WAS REMOVED AND REINSTALLED IAW SRM 51-41-02 AND 51-41-05.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 40,418 hrs · 27,977 cycles

FWD CARGO DOOR JAMB CORRODED IN SEVERAL PLACES AT LOWER PART OF JAMB. MARKED. REPLACED FORWARD CARGO LOWER PAN SECTION IAW SRM 53-20-15, REPAIR 6. REPLACED 2 EA LOWER SEAL DEPRESSOR SPLICES IAW SRM 51-41-02. TAG 1553387.

Part: CUSP WEB — CRACKED (BS 672) · airframe 40,418 hrs · 27,977 cycles

UPPER CABIN FLOOR CUSP WEB BS 672, LBL 42 IS CRACKED REPLACE CUSP WEB. REF ORNRC 66531-0200-0102. REPLACED CUSP WEB IN UPPER CABIN AT BS 672, LBL42 IAW SRM 51-41-02, PG 1, PARA 4 AND 51-41-08, PG 9, PARA 7.

Part: FRAME — CORRODED (BS 140) · airframe 40,418 hrs · 27,977 cycles

LOWER FUSELAGE, ELECTRONIC EQUIPMENT COMPARTMENT, MAIN FRAME, BS 140-L30, CORROSION FWD OF ELECTRONIC EQUIPMENT OPENING, MARKED. BLENDED NOTED AREAS IAW SRM 51-10-04, SECTION 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 103. REPAIRED OUT OF LIMITS AREA IAW SRM 53-00-05, REPAIR 3.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 40,418 hrs · 27,977 cycles

AFT CARGO DOOR HAS CRACK IN INTERIOR SKIN AT LOWER FWD CORNER NEAR DOOR HOOK. REPAIRED CRACK IN INTERIOR SKIN AT LOWER FWD CORNER NEAR DOOR HOOK IAW SRM 52-30-02 REPAIR 4, FIG 201.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 40,418 hrs · 27,977 cycles

AFT CARGO DOOR JAMB HAS CORROSION AND A DENT TO FWD WEB. BLENDED CORROSION IAW SRM 53-00-00, ORIGINAL TC .050. REMOVED T .005 REMAINING R .045 USING TAG NR 3210, ALODINED, PRIMED, TOPCOATED IAW SRM 51-10-04 DENT MEASURES .045 X 2.00 USING TAG 3810.

Part: ANGLE — CORRODED (BS 220) · airframe 40,418 hrs · 27,977 cycles

UPPER CABIN FLOOR CUSP ANGLE AT BS 220, RBL 60 IS CORRODED AT UPPER SURFACE BLEND, CHECK LIMITS REF OR NRC 66531-0200-0115. BLENDED NOTED AREA IAW SRM 51-10-04, SECTION 26, FOUND TO BE IN LIMITS IAW SRM 53-00-00, FIG 103. REMOVED .013 FROM ORIGINAL .071 DEPTH GAUGE 3310. UPON REMOVAL OF CUSP WEB, FOUND TO BE CRACKED. REPLACED CUSP WEB IAW SRM 51-41-02, SECTION 4 AND 51-41-05, SECTION 3.

Part: CUSP WEB — CORRODED (BS 470) · corrosion level 2 · airframe 40,418 hrs · 27,977 cycles

UPPER CABIN FLOOR CUSP WEB, BS 470, RBL 56 HAS CORROSION ON UPPER SURFACE. BLEND AND CHECK LIMITS, REF OR NRC 66531-0200-0114. REPAIRED CORRODED CUSP WEB AT BS 470, RBL 56 IAW SRM 53-00-55, FIG 207.

Part: SKIN — DAMAGED (BS 1087) · airframe 39,566 hrs · 27,307 cycles

DURING LIGHTNING STRIKE INSPECTION FOUND RT SIDE FUSELAGE CRACKED AT BS 1087.060 L14R. PERMANENT REPAIR IAW ERA 541671-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,925 hrs · 26,797 cycles

DURING WALKAROUND CHECK, CREW NOTED THE CABIN EMERGENCY EXIT LIGHT AT THE TAILCONE EXIT WAS INTERMITTENTLY BLINKING AND WAS INOPERATIVE WHEN TURNED ON. MAINTENANCE REPLACED THE B5-260 POWER SUPPLY AND THE SYSTEM CHECKED NORMALLY.

Part: PIN — UNSECURE (R1 DOOR SLIDE) · airframe 36,189 hrs · 24,620 cycles

DURING LINE CHECK, NOTED THE R1 DOOR SLIDE PARACHUTE PINS WERE RELEASED. THE R1 DOOR SLIDE WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: TIE — LOOSE (EVAC SLIDE) · airframe 35,623 hrs · 24,191 cycles

TAIL CONE SLIDE TIE WRAP LOOSE. SECURED WRAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,623 hrs · 24,191 cycles

AFT RT OVERWING EMERGENCY EXIT LIGHT BULBS INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,623 hrs · 24,191 cycles

TAIL COMPARTMENT RT VENT BOX REPAIR CRACKED. R & R ANGLE IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,623 hrs · 24,191 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,623 hrs · 24,191 cycles

TAIL COMPARTMENT CATWALK EMERGENCY EXIT LIGHTS BULBS INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,623 hrs · 24,191 cycles

AFT EMERGENCY LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 35,623 hrs · 24,191 cycles

AFT LT EEPLS LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 35,623 hrs · 24,191 cycles

R1 DOOR EEPLS LENS CRACKED. R & R LENS IAW AMM.

Part: FITTING — DIRTY (L1 DOOR) · airframe 34,949 hrs · 23,758 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING DIRTY. CLEANED FITTING IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 34,949 hrs · 23,758 cycles

LEFT EMERGENCY LIGHT POWER SUPPLY FAILED OPERATIONS CHECK. R & R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 34,949 hrs · 23,758 cycles

RIGHT EMERGENCY LIGHT POWER SUPPLY FAILED OPERATIONS CHECK. R & R POWER SUPPLY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 34,949 hrs · 23,758 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: PLATE — CORRODED (R1 DOOR) · airframe 34,949 hrs · 23,758 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNT PLATE CORRODED. REPAIRED PLATE IAW SRM.

Part: PLATE — CORRODED (R1 DOOR) · airframe 34,949 hrs · 23,758 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT PLATE CORRODED. REPAIRED PLATE IAW SRM.

Part: TRIM PANEL — CRACKED (COCKPIT) · airframe 34,949 hrs · 23,758 cycles

AIRCRAFT FLIGHT COMPARTMENT LT CAPTAIN WINDSHIELDS INTERNAL FRAME TOP TRIM COVER CRACKED. REMOVED & REPAIRED WINDSHIELD TRIM COVER IAW AMM.

Part: TRIM PANEL — CRACKED (COCKPIT) · airframe 34,949 hrs · 23,758 cycles

AIRCRAFT FLIGHT COMPARTMENT RT FIRST OFFICERS WINDSHIELDS INTERNAL FRAME TOP TRIM COVER CRACKED. REMOVED & REPAIRED WINDSHIELD TRIM COVER IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 34,949 hrs · 23,758 cycles

RIGHT WING FIXED LE SKIN CRACKED AT NR 4 LE SLAT ACTUATOR CUT OUT. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,732 hrs · 24,261 cycles

RT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 14. RELAMPED LIGHT IAW SIP.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 35,524 hrs · 24,129 cycles

RT PYLON AFT UPPER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DRAWING.

Part: ENGINE — FAILED (RIGHT) · airframe 35,544 hrs · 24,142 cycles

INFLIGHT SHUTDOWN RT ENG SPOOLED DOWN ON APPROACH. R & R NR 2 ENG IAW TC.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 35,429 hrs · 24,067 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIRTY. CLEANED GIRT BAR IAW AMM.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 33,746 hrs · 23,022 cycles

RT PYLON AFT UPPER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DWG.

Part: LENS — MISSING (CABIN) · airframe 33,841 hrs · 23,087 cycles

RIGHT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 3. INSTALLED LENS IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 33,764 hrs · 23,035 cycles

LENS COVER MISSING FOR EXIT SIGN OVER ROW 1. INSTALLED LENS IAW MM.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 32,842 hrs · 22,476 cycles

RT PYLON AFT UPPER ATTACH ANGLE CRACKED. TRIMMED DAMAGED AREA PER BOEING DRAWING SG95530003.

Part: LENS — LOOSE (EXIT SIGN) · airframe 32,771 hrs · 22,429 cycles

EXIT SIGN AT ROW 2 FELL OFF. REPLACED EXIT SIGN LENS, REF AMM

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,742 hrs · 22,413 cycles

LOWER FWD F/A FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED FLASHLIGHT AND BATTERY REF 717 AMM PLACARDS REMOVED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

RIGHT MAIN CABIN CUSP WEB CORRODED BETWEEN BS 674 TO BS 703. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

RIGHT MAIN CABIN CUSP WEB CRACKED AT STA 664. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 389 TO BS 408. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

RIGHT MAIN CABIN CUSP WEB CORRODED AT BS 519. REPAIRED CUSP WEB IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

STRINGER CRACKED AT BS 1133, STR 2L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,142 hrs · 21,383 cycles

AFT CARGO DOOR CUTOUT LOWER SILL CORRODED. REPAIRED SILL IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,807 hrs · 21,153 cycles

FWD CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,807 hrs · 21,153 cycles

MID CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LOCK — LACK OF LUBE (GIRT BAR) · airframe 30,807 hrs · 21,153 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LOCK INOP. LUBED AND CLEANED LOCK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,807 hrs · 21,153 cycles

EEPLS INOP BETWEEN ROW 20 TO ROW 24. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,807 hrs · 21,153 cycles

FWD CEILING EMERGENCY EXIT LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — BROKEN (TAILCONE) · airframe 30,807 hrs · 21,153 cycles

TAIL CONE EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,807 hrs · 21,153 cycles

MID CABIN EMERGENCY EXIT LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — FAULTY (MAIN BATTERY)

BATTERY CHARGING ALERT. REMOVED AND REPLACED BATTERY CHARGER REF B717 AMM 24-34 , OPS CHECKED GOOD. NOTE: SUBMITTED AT THE REQUEST OF DQA.

Part: DOOR FRAME — CRACKED (RT MLG)

RIGHT MLG DOOR, BELOW UP LOCK ROLLER FRAME CUTOUT, CRACKED. ACCOMPLISHED FRAME CUTOUT ANGLE REPAIR PER B717 SRM 53-20-2.

Part: STRUCTURE — CRACKED (RT PYLON)

RIGHT PYLON APRON LOWER NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 45, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: ANGLE — CRACKED (LT MLG DOOR)

LEFT MLG DOOR, BELOW UPLOCK ROLLER LOWER PAN "Z" ANGLE, CRACKED. ACCOMPLISHED LOWER PAN "Z" ANGLE DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, RBL48, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 22 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR PANEL — CORRODED (CABIN)

CABIN FLOOR PANEL, STA 160 TO 200, RBL 48, CORROSION. ACCOMPLISHED FLOOR PANEL REPLACEMENT PER B717 SRM 51-41-02 AND BOEING DRAWING PL9957828.

Part: TRACK — CORRODED (FUSELAGE)

MAIN CABIN FLOOR TRACK HAS SPOT OF CORROSION AT STA 144 LBL 8. REMOVED AND REPLACED FLOOR TRACK ON MAIN CABIN PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT STA 237 BL 0. REPLACED FLOOR SUPPORT AT STA 237 BL 0 PER B717 SRM 51-41-02.

Part: LENS — MISSING (CABIN)

E-PATH LIGHT MISSING COVER ON SEAT 14D. INSTALLED E-PATH LIGHTING LENS AT 14D AS REQUIRED.

Part: ANGLE — CRACKED (FUSELAGE)

RT VENT BOX ANGLE CRACKED AT STA 1174. REPLACED ANGLE PER SRM 51-41-07.

Part: FRAME — CRACKED (FUSELAGE)

ROLLED Z-FRAME CRACKED AT FUSELAGE STA 1098 RT BETWEEN L 11 & 13. CUT OUT DAMAGED AREA, REPAIRED PER B717 SRM 53-00-07 FIG 201.

Part: REPAIR — CRACKED (FUSELAGE)

STA 1144 REPAIR ANGLE CRACKED AFT OF VENT BOX RT SIDE. REPLACED ANGLE PER B717 SRM 51-41-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEATS 25 THRU 31 EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT BATTERY & PWR SUPPLY REF AMM 33-51. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS OUT AT SEAT 1-3 AND 20-24. EMERGENCY LIGHT BATTERY PACK ASSEMBLIES WERE REMOVED AND REPLACED AS PER 33-51. OPS CHECK NORMAL.

Part: FITTING — MISSING (EVAC SLIDE)

L1 DOOR SLIDE PACK MISSING A CLIP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY REF AM/M 25-61.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT FAILURE AT SEATS 1D, 2D, 3D, AND 11D WHILE PERFORMING EMERGENCY LIGHT TEST ON A RON SERVICE CHECK. REPLACED POWER SUPPLY B5-118, ALSO REPLACED BAD LAMP SOCKET AT SEAT 11D REF AMM 33-51, OPS CHECK GOOD.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

AFTER SEVERAL MOMENTARY (FIRE DETECTION RIGHT FAIL) INDICATIONS AS WE APPROACHED MYR HAD BELL AND LIGHTS RIGHT FIRE HANDLE. SECURED RIGHT ENGINE AND INDICATIONS STOPPED FOR SEVERAL MINUTES. LIGHT AND BELL RETURNED SO WE PULLED THE FIRE HANDLE WHICH AGAIN STOPPED INDICATIONS LANDING COMPLETED WITH FIRE DEPARTMENT RESPONSE. REMOVED AND REPLACED TE UPPER FIRE LOOP SPLITTER.

Part: ENGINE — FAILED (LEFT)

NR 1 ENGINE FAILURE, ENGINE AUTO SHUTDOWN, TGT NOT EXCEEDED, ENGINE RELIGHT ATTEMPTED, ENGINE SURGING, MANUAL ENGINE SHUTDOWN. ENGINE NOT SHUTDOWN FOR MORE THAN 30 MINUTES. REMOVED AND REPLACED NR 1 ENGINE.

Part: TERMINAL BLOCK — BURNED (WINDOW HEAT)

AT 9000 FEET STRONG BURNING ODOR AND SMOKE (LIGHT) COMING FROM CAPTAIN'S WINDSHIELD. WHEN WINDSHIELD HEAT WAS SELECTED OFF, SMOKE DISSIPATED. ATL MAINTENANCE DISPATCHED, REMOVED AND REPLACED THE CAPTAIN'S LEFT WINDSHIELD, WINDOW HEAT CONTROL TERMINAL BLOCK, AND WINDOW HEAT CONTROLLER.