N954AT

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 65,738 hrs · 48,184 cycles

EXTERIOR OVERWING EMERGENCY LIGHT WON'T EXTINGUISH. T/S OVERWING EMERGENCY LIGHTS PER B717 FIM 33-50-00-810-801. R & R EMERGENCY LIGHT POWER SUPPLY AT LOC B5-125 PER AMM 33-51. OPS CKD GOOD. (7844834).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,639 hrs · 44,462 cycles

SHIP 9513 -MISC/DE- THE CREW DECLARED AN EMERGENCY WHILE IN ICING CONDITIONS IN ORDER TO RAPIDLY DESCEND OUT OF ICING CONDITIONS AFTER RECEIVING A "WING MANIFOLD FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PODS PROCESSOR, REPAIRED A BLOWN DUCT, AND XXX. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #9375946)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,233 hrs · 44,095 cycles

THE CREW DISCOVERED THAT THE 1L GIRT BAR CABLE WAS DETACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. CONTRACT MAINTENANCE REATTACHED THE GIRT BAR LANYARD PER B717 AMM 25-61. THE AIRCRAFT IS OK TO CONTINUE IN SERVICE. (LP #4274224)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,888 hrs · 43,771 cycles

THE PILOT NOTICED THE 1L DOOR GIRT BAR TETHER STRAP WAS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE STRAP BUCKLE. OPERATIONAL CHECK WAS GOOD. (LP #4498172)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,687 hrs · 43,597 cycles

THE MAIN CABIN DOOR GIRT BAR STRAP NOT ATTACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE GIRT BAR STRAP AS PER B717 AMM 25-61. (LP #4951546)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,542 hrs · 43,469 cycles

AFTER PARKING AT GATE IT WAS DISCOVERED THAT METAL LANYARD AND BRACKET WAS DISCONNECTED FROM FWD MAIN CABIN DOOR SLIDE. THIS WOULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REINSTALLED 1L DOOR SLIDE LANYARD AS REQUIRED PER B717 AMM 25-61. AIRCRAFT IS OK FOR SERVICE. (LP #4798136)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

IN REFERANCE TO AMDS 5352-4002: DURING INSTALLATION OF TAILCONE SLIDE, THE RESTRAINT STRAPS WERE FOUND MISSING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF THE NRC 712: STRAP (2 EAS) WERE INSTALLED PER B-717 SRM 51-41-01-0G. (LP #2714901)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

CRACK ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR. (C2) SUMMARY OF NRC 00639: FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR (C2) WAS REPAIRED PER ER/A 606786-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 606786-14 REV 2. (LP #2708762)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

CORROSION ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1). SUMMARY OF NRC 00408: CORROSION LEVEL 2. REPAIR ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1) WAS PERFORMED PER PRI ER/A606769-14 REV. 0 AND ER/A 606769-14 REV. ORIGINAL SECTION I, PERMANENT REPAIR. ASSOCIATED ER/A 14-606769 ADDED FOR AC 9513. (LP #2708586)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

CRACKED FRAME BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR. LOCATED JUST ON HANDLE HOUSING AREA. SUMMARY OF NRC 00075: FRAME (INTERCOSTAL) BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR ON HANDLE HOUSING AREA WAS FABRICATED AND REPLACED PER DWG 9955763 REV K AND B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2707268)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

CRACKED BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR. SUMMARY OF NRC 00077: BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2706615)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

CORROSION ON CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND. SUMMARY OF NRC 00553: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND WAS REPAIRED PER PRI 606633-14 REV.2 AND ER/A 606633-14 REV. ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2705924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, AFTER TAILCONE SLIDE REMOVAL, IT WAS FOUND UNPACKED. CORRECTIVE ACTION: TAILCONE SLIDE WAS REMOVED P/N: D29984-213 S/N: 1539 PER AMM 25-61-02-000-801 AND SERVICEABLE TAILCONE SLIDE P/N: D29984-213 S/N: 1561RP WAS REPLACED. (LP 2695495)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CRACK ON OVERWING FRAME STA Y=674 LH SIDE AT WING BOX AREA. CORRECTIVE ACTION: OVERWING FRAME STA Y=674 LH WAS REPLACED PER CARD 5310-01436-03A. (LP 2691308)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CORROSION ON INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 51-41-05-0G. AND PER DRAWING 9971095 ITEM 51 REV AP. (LP 2692447)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION: CUSP ANGLE AT STA Y-200 ON STRINGER L18 WAS REPAIRED PER B717-200 SRM 53-00-55-2 REPAIR 3 PAR. 5. (LP 2689728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH AT EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH WERE REPAIRED PER PRI 606376-14 REV. 1 AND ER/A 606376-14 REV. ORIGINAL SECTION: I, PERMANENT REPAIR. (LP 2691207)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AT CUSP ANGLE LOWER SURFACE ON STA=560 TO STA =579 ON FWD CARGO COMPARTMENT RH SIDE. CORRECTIVE ACTION: CUSP ANGLE LOWER SURFACE ON STA =560 TO STA=579 ON FWD CARGO COMPARTMENT RH SIDE WAS REPAIRED PER B717 200 SRM 53-00-55-2R. (LP 2689818)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54. CORRECTIVE ACTION: FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54 WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP 2686942)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 200 TO STA 210. CORRECTIVE ACTION: ANGLE SUPPORT WAS REPLACED PER DRAWING 5910085 ITEM 15 REV. DJ. (LP 2685489)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON CUSP WEB TO BTW STA 218 TO STA 237 RH. CORRECTIVE ACTION: CUSP WEB TO BTW STA 218 TO STA 237 RH WAS FABRCATED AND REPAIRED PER B 717-200 SRM 53-00-55-2R-4 FIG 226, DWG 9930538-109 REV. CC AND WAS REMOVED AND INSTALLED PER NRC 00553. (LP 2685543)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-9 TO X=-42. CORRECTIVE ACTION: FLOOR SUPPORTS WERE REPLACED PER DWG 9936534 REV. BW AND PER B717-200 SRM-51-41-02-0G PAR. 4. (LP 2685485)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CORROSION ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E/E COMPARTMENT. CORRECTIVE ACTION: REPAIR ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E / E COMPARTMENT WAS PERFORMED PER B-717-200 SRM 51-70-10 REPAIR 2 PAR. 4 FIG. 201. (LP 2685554)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON RH CUSP WEB STA. Y= 198 TO Y=202 (R1) RBL50 AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=200 TO Y=218 (R1) RBL50 AT PASSENGER CABIN WAS FABRICATED AND REPLACED PER DWG 9936535 REV. CS ITEM: -95 AND B717-200 SRM 51-41-02-0G PAR. 4 AND B717-200 SRM 51-41-08-0G PAR. 7. (LP 2686094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CLIP ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-40-02-0G. AND SRM 51-41-05-0G. (LP 2686715)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 137 TO STA 160. CORRECTIVE ACTION: ANGLE WAS FABRICATED PER DWG 5910085 REV DE. (LP 2685491)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CRACKS (2EAS) AND ELONGATED HOLES ON LH CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4, SRM 51-41-02-0G AND DWG 9910151-163 REV. CH. (LP 2684487)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX. CORRECTIVE ACTION: FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. PAR.8. (LP 2681442)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FRAME BTW STA=1037 BTW LONGERON 17RH AND LONGERON #18RH OF PAX CABIN. CORRECTIVE ACTION: REPAIR WAS PERFORMED PER B717-200 SRM 53- 20-07-2R PROCEDURE 4 REPAIR 4. (LP2680687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, CRACK ON FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FOUND. CORRECTIVE ACTION: FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-01-0G, SRM 51-41-05-0G AND DWG: 3914025 REV. D. (LP 2681651)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: UPPER PAN ON STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1 PAR. (LP2680219)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR. CORRECTIVE ACTION: INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1. (LP 2675859)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AND CRACK ON LH CUSP WEB (UPPER-LOWER SURFACE) STA. Y= 636 TO Y=655 AT PASSENGER CABIN. CORRECTIVE ACTION: LH CUSP WEB ON STA. Y=636 TO Y=655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 210 AND B717-200 SRM 51-41-02-0G. (LP 2676120)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 427 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: CLIP ON LOWER PAN SECTION STA Y 427 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2674408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. WAS REPAIRED PER B717-200 SRM 53-00-55-2R. REP. 4. (LP2674411)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: CLIP OF LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2675114)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LUGS (FLOOR SUPPORT) STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT. CORRECTIVE ACTION: FLOOR SUPPORT ON STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT FABRICATED PER DWG 9936533-89 REV. CM AND WAS REPLACED PER B717-200 SRM 51-41-02-0G. PAR 4. (LP 2675436)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON BEAM NBR 1, (FWD EDGE) OF L1 PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 2675276)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2675117)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FITTING ATTACH UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: UPPER FITTING STA Y 389 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2673904)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN. CORRECTIVE ACTION: CUSP WEB RH (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. CONFIGURATION 7003 CUSP FIG. 204. (LP 2673159)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

IN REF NRC 00485 CORROSION ON RH CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 216. (LP #2671432)

Part: UNKNOWN — UNKNOWN · airframe 60,176 hrs · 43,173 cycles

CRACK ON INTERNAL ANGLE ON AFT PAN MIDDLE SECTION AT LH FWD OVERWING EMERGENCY EXIT DOOR. (PTAS) SUMMARY OF NRC 00073: INTERNAL ANGLE AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS FABRICATED AND REPLACED PER DWG 9957735 REV G, B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2668940)

Part: UNKNOWN — UNKNOWN · airframe 60,176 hrs · 43,173 cycles

CRACKED ON FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00655: FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R. (LP #2667352)

Part: NONE — NONE · corrosion level 2 · airframe 60,176 hrs · 43,173 cycles

CRACKED RH CUSP WEB BTW STA Y=918-925 AND Y=935-942 AT PASSENGER CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP WEB RH BTW STA Y=918-925 AND Y=935-942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 PAR 5 B FIG 216. (LP #2661740)

Part: PSEU — FAILED · airframe 59,817 hrs · 42,879 cycles

SHIP 9513- MISC/DE - WHILE ON APPROACH FOR LANDING THE CREW NOTED THE MASTER CAUTION WITH EICAS MESSAGE OF "PSEU FAIL". WHICH REQUIRED A NO SLAT / NO FLAP LANDING BE ACCOMPLISHED. THE CREW DID DECLARE AN EMERGENCY WITH ATC AND COMPLIED WITH THE QRH. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND REPLACED THE #2 VIA (WHICH CORRECTED A TRIPPED VIA CIRCUIT BREAKER). ENGINE RUNS AND AUTO-LAND TESTS WERE ALL GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9502752)

Part: NONE — NONE · airframe 58,088 hrs · 41,269 cycles

DURING CHECK THE OPERATION OF THE EMERGENCY LIGHTING SYSTEM, LEFT AND RIGHT OVER-WING EMERGENCY EXTERIOR LIGHTS DON'T ILLUMINATE IN REFERENCE CARD 0514-2001 STEP 8. SUMMARY OF NRC 00110: OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717-200 AMM 33-51-06. TEST OK. (LP #2157914)

Part: NONE — NONE · airframe 58,088 hrs · 41,269 cycles

LIGHTNING STRIKE ON CUT OUT OUTER PANE OF PASSENGER WINDOW NBR 17 LH SIDE (SM). SUMMARY OF NRC 00032: LIGHTNING STRIKE ON CUT OUT OUTER PANEL OF PASSENGER WINDOW NBR 17 LH SIDE WAS REPAIRED PER ER/A 597798-14 REV.ORIG. PRI REV.0 SECTION I TEMPORARY REPAIR. ACCOMPLISH SECTION II: REPETITIVE HFEC INSPECTIONS WITHIN EVERY 24 MONTHS OF 07MAR22 UNTIL PERMANENT REPAIR PER SECTION III HAS BEEN COMPLETED. LOG PAGE 2156719. ACCOMPLISH THE SECTION III: PERMANENT REPAIR PRIOR TO 54,000 TOTAL FLIGHT CYCLES. LOG PAGE 2156719. (LP #2156987)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,176 hrs · 43,173 cycles

ER/A 597798-14, FUSELAGE / SKIN / LH WINDOW BELT PANEL / Y=522-541 / LIGHTNING STRIKE. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTION AND PERMANENT REPAIR. ACCOMPLISH ER/A 597798-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS OF SECTION I ACCOMPLISHMENT ON 07MAR22 UNTIL SECTION III PERMANENT REPAIR IS COMPLETED. ACCOMPLISH SECTION III PERMANENT REPAIR WITHIN 54,000 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 14-597798 ADDED FOR AC 9513. PERMANENT REPAIR WAS PERFORMED PER PRI 597798-14 REV 0 AND ER/A 597798-14AD REV A SECTION III: PERMANENT REPAIR. (LP #2156719)

Part: NONE — NONE · airframe 58,085 hrs · 41,267 cycles

THE AFT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY PER B717 AMM 33-51. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8541981)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,915 hrs · 40,212 cycles

THE EMERGENCY EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE B5-235 BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7926603)

Part: CONNECTOR — MISSING (EMERGENCY LIGHTS) · airframe 56,818 hrs · 40,131 cycles

CEILING PANEL 27CDE MISSING CONNECTOR ON EMERGENCY LIGHT WIRES. RESCURED CONNECTOR 27CDE PER B717 AMM 20-30. OPERATIONAL CHECK IS GOOD. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (LP #7963852)

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 56,703 hrs · 40,035 cycles

MAINTENANCE FOUND THAT THE AFT EMERGENCY EXIT IDENTIFIER FLASHES WHEN ARMED AND BACK TO "ON" POSITION. THE BATTERY CHARGER WAS REPLACED IAW B717 AMM 33-51-03. AIRCRAFT IS OK FOR SERVICE. (LP #7340781 )

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 56,663 hrs · 40,003 cycles

THE FLIGHT ATTENDANT INFORMED MAINTENANCE THAT THE OVER EMERGENCY LIGHT COVERS WERE MISSING. MAINTENANCE REPLACED THE LIGHT COVERS. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #1849420)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHTS) · airframe 56,618 hrs · 39,967 cycles

THE EMERGENCY EXIT SIGN OVER THE AFT CABIN BULKHEAD DOOR AND THE TAIL COMPARTMENT PATHWAY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-260, PER B717 AMM 33-51. (LP #7340722)

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,473 hrs · 38,161 cycles

SEVERAL EMERGENCY LIGHTS IN THE CEILING ARE INOPERATIVE. MAINTENANCE REPLACED THE APPLICABLE EMERGENCY LIGHT POWER SUPPLY BATTERY. THE EMERGENCY AND STANDBY LIGHTS ALL CHECK GOOD NOW IAW AMM 33-55.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,281 hrs · 37,993 cycles

CORROSION ON FWD SIDE OF FRAME 974 AT L30. FOUND TO BE OUT OF LIMITS REF B717 SRM 53-00-00-01A. REPLACED FWD FRAME SECTION OF 974 L30 WITH A NEW FABRICATED FRAME SECTION REF B717 SRM 53-20-07-2R PROCED 3. (LP #1519051)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,281 hrs · 37,993 cycles

CORROSION ON FWD SIDE OF FRAME 974 AT L-30. NRC 054-0008:5331-2001/002 00265: REPAIRED REF B717 SRM 53-20-07-2R PROCED 3. (LP #1518684)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,281 hrs · 37,993 cycles

CORROSION LONGERON 26LT, FORWARD AND AFT SIDE STA 1002. NRC 054-0008:5331-2001/060 00367: REPAIR COMPLIED WITH REF B717 SRM 53-00-05-2R PROCED 2 AND ER/A 585769- 14 REV O. (LP #1517266)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,281 hrs · 37,993 cycles

CORROSION ON FRAME AT STA 1037 BETWEEN L21LT AND L22LT FWD AND AFT SIDE. NRC 054-0008:5331-2001/067 00375: REPAIRED REF B717 SRM 53-20-07-2R. (LP #1517598)

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,281 hrs · 37,993 cycles

CORROSION ON AFT SIDE OF FRAME 851 ABOVE L-30. NRC 054-0008:5331-2001/017 00280: REPAIRED REF B717 SRM 53-20-07-2R PROCED 3. (LP #1515028)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,281 hrs · 37,993 cycles

L30 CORRODED IN MULTIPLE AREAS FROM STA 898.5 TO STA 1012. NRC 054-0008:5331-2001/046 00331: SPLICED IN NEW SECTION OF LONGERON B717 SRM 53-20-05-2R PROCED 1. (LP #1509159)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,493 hrs · 37,398 cycles

EMERGENCY LIGHTS IN AFT TAIL INOP. REMOVED AND REPLACED OVER HEAD BATTERY PACK FOR REAR AFT TAIL. OPS CHECK GOOD. IAW B717-AMM 33-55. (LP6356548)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,155 hrs · 36,413 cycles

THE LT AND RT AFT OVERWING EXIT IDENTIFIERS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5668218)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,593 hrs · 33,336 cycles

NO POWER SUPPLY TO FWD CEILING EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT BATTERY PACK B5 227 IAW AMM 33-51-03. OPS CHECKED GOOD. EMERGENCY LIGHTS ON CEILING OPS OK FOR SERVICE.

Part: POWER SUPPLY — OVERHEATED (CABIN) · airframe 46,039 hrs · 32,204 cycles

THE F/A REPORTED A LOUD BANG FOLLOWED BY WHITE SMOKE WITH AN ELECTRICAL ODOR NEAR EXIT ROW 19. MAINTENANCE FOUND THAT THE UPPER BEACON POWER SUPPLY HAD OVERHEATED AND THAT THE WIRE HARNESS GOING TO THE BEACON WAS DISCOLORED. THE POWER SUPPLY, WIRE HARNESS, AND UPPER BEACON WERE ALL REPLACED PER AMM. COMPLIED WITH NO GO ODI PREVENTION PROGRAM. ALL CHECKS OKAY.

Part: LENS — LOOSE (EXIT SIGN) · airframe 45,805 hrs · 32,025 cycles

THE PILOT DISCOVERED THAT THE MAIN CABIN DOOR EMERGENCY EXIT SIGN HAD A LOOSE LENS/COVER. MAINTENANCE RE-ATTACHED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: DOUBLER — DENTED (L1 DOOR) · airframe 44,616 hrs · 31,101 cycles

DENTS ON PREVIOUS REPAIR ON LOWER SKIN AT L1 DOOR. REPLACED IAW SRM VOL 1 52-10-01, FIG 4 AND 51-30-02, VOL II.

Part: LONGERON — CORRODED (BS 974-1003) · airframe 44,299 hrs · 30,813 cycles

LONGERON 30, FROM BS 974 TO 1003 CORRODED ALSO ADDITIONAL AREAS OF CORROSION FOUND ON LONGERON 30, FROM BS 927 TO 974. CLEANED, INSPECTED, AND BLENDED ALL AREAS OF CORROSION IAW SRM 53-00-00. NOMINAL THICKNESS FOUND WAS .125 FOUND WAS .074 ALL AREAS WERE BLENDED TO WITHIN LIMITS IAW SRM 53-00-05, REPAIR 3 EXCEPT FOR BS 998 WAS OUT OF LIMITS. BS REPAIRED IAW SRM 53-00-05, REPAIR 3. ALL AREAS WERE THEN ALODINED, PRIMED, AND TOPCOATED IAW DPSM 900-2-4-1, NR 2, 900-3-6, NR 1 AND 900-3-6, NR 3. VT TOOL TAG NR WAS 6783. ADDED RII & MAJOR REPAIR. RII WAS COMPLETED BY INSP 288005 ON NR 161, 100.

Part: STRUCTURE — NOT REPORTED (BS 157-1022) · airframe 44,299 hrs · 30,813 cycles

PERFORMED DETAIL VISUAL INSPECTION OF LT AND RT CUSP WEB TO TOP OF SKIN ATTACH ANGLE FROM FS 157 TO 1022. REPLACED AT CUSP WEB FS 655 TO FS 737 IAW SRM 51-41-02, REPAIR RT CUSP WEB IN SEVERAL LOCATIONS IAW SRM 53-00-85, REPAIR NR 4.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 44,299 hrs · 30,813 cycles

FORWARD CARGO DOOR FRAME IS CORRODED AT LOWER MIDDLE SURFACE. REPLACED FWD CARGO DOOR FRAME IAW SRM 51-41-02, 51-41-05, 51-41-08, 53-20-15 REPAIR 6, WITH NEW SECTION.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 45,695 hrs · 31,943 cycles

WEB IS CORRODED AFT OF CARGO DOOR CUTOUT. REMOVED AND REPAIRED DAMAGE IAW ER/A 544348-14 REV ORG. ASSOCIATED ER/A 00-544348 ADDED FOR AC 9513.

Part: CUSP WEB — CORRODED · airframe 44,299 hrs · 30,813 cycles

CUSP WEB AT LOWER AFT CORNER OF R-1 DOOR CORRODED. REMOVE DOOR AND RE-EVALUATE. REMOVED CORRODED CUSP WEB, FABRICATED REPLACEMENT WEB IAW B DWG NR 5930540. INSTALLED REPLACEMENT WEB IAW SRM 51-41-02 AND 53-00-55, FIG 201, REPAIR 1.

Part: BULKHEAD — CRACKED (BS 1022) · airframe 44,299 hrs · 30,813 cycles

BS 1022, RT PYLON SUPPORT BULKHEAD, STRINGER 6R CRACKED. BULKHEAD REPAIRED IAW SRM 53-00-05, REP 2.

Part: SKIN — CORRODED (BS 1005) · airframe 44,299 hrs · 30,813 cycles

SKIN CORRODED AT BS 1005 ABOVE LONGERON 27R AND ON LONGERON 25R AT BS 1003 AFT OF LOWER CARGO DOOR CUTOUT. BLENDED CORROSION, AND FOUND WITHIN LIMITS IAW SRM 53-00-00, FIG 103.

Part: STRINGER — CRACKED (BS 1022) · airframe 44,299 hrs · 30,813 cycles

BS 1022, LT PYLON SUPPORT BULKHEAD, STRINGER 6L CRACKED. VERIFY CRACK, SUBMIT EWO, SRM 53-00-05 REP 2. REPAIRED S6L AS MARKED IAW SRM 53-00-05, REPAIR 2.

Part: GUSSET — CRACKED (BS 1022) · airframe 44,299 hrs · 30,813 cycles

LT PYLON BULKHEAD UPPER GUSSET IS CRACKED AT BS 1022, LONGERON 7L. REPAIRED IAW SRM 51-70-11, REPAIR 1.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 42,218 hrs · 29,164 cycles

DURING SCHEDULED CHECK, MAINTENANCE NOTED DOOR 1R SERVICE DOOR SLIDE PRESSURE GAUGE IN THE NO-GO RED BAND. REPLACED DOOR 1R SERVICE DOOR SLIDE IAW AMDS CARD 2561-9005. REQUIRED INSPECTIONS PERFORMED.

Part: OVEN — SMOKE · airframe 41,775 hrs · 28,799 cycles

DURING CLIMB OUT, F/A NOTIFIED COCKPIT CREW THAT SMOKES WAS COMING FROM THE GALLEY OVEN. THE OVEN WAS TURNED OFF AND THE SMOKE STOPPED AND CLEARED. CREW TURNED OFF GALLEY POWER IAW SMOKE, FIRE, FUMES CHECK LIST. THE FORWARD GALLEY OVEN WAS DEFERRED IAW NEF 25-34-02 AND WAS LATER REPLACED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,702 hrs · 28,749 cycles

DURING LINE CHECK, NOTED RT OVERWING EMERGENCY LIGHT LAMP WAS NOT ILLUMINATING. REPLACED LAMP IAW AMM 33-51.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,725 hrs · 27,024 cycles

L1 DOOR EMERGENCY EXIT SIGN FWD OF DOOR BULB INOPERATIVE. R & R BULB IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 39,725 hrs · 27,024 cycles

EMERGENCY EXIT LIGHT LENS CRACKED AFT OF R1 DOOR. R & R LIGHT LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 39,725 hrs · 27,024 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: LANYARD — CORRODED (EVAC SLIDE) · airframe 39,275 hrs · 26,741 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD CORRODED. R & R LANYARD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,275 hrs · 26,741 cycles

FWD LAVATORY EMERGENCY EXIT LIGHT BULB DROP DOWN PANEL INOPERATIVE. R & R BULB IAW AMM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 39,725 hrs · 27,024 cycles

FORMER CRACKED AT BS 1152, LONGERON 2L. R & R FORMER IAW SRM.

Part: SKIN PANEL — CRACKED (RUDDER) · airframe 39,725 hrs · 27,024 cycles

LOWER LT HAND RUDDER SKIN DOUBLER PANEL CRACKED. REPAIRED DOUBLER IAW EA.

Part: CABLE — FRAYED (L1 DOOR) · airframe 39,275 hrs · 26,741 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RELEASE CABLE FRAYED. R & R CABLE IAW AMM.

Part: SKIN PANEL — CRACKED (RUDDER) · airframe 39,275 hrs · 26,741 cycles

LOWER LT RUDDER SKIN PANEL CRACKED. REPAIRED SKIN IAW SWA EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

FORMER CRACKED AT BS 1152, LONGERON 2L. R & R FORMER IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

AFT DOOR FRAME WEB, LT SIDE LOOKING AFT, VENTRAL STAIRWAY BULKHEAD DOOR JAM CRACKED. REPAIRED JAMB IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 200 TO BS 218, LBL 16. R & R SUPPORT IAW SRM & DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

FWD GALLEY DOOR SURROUND, GALLEY FLOOR AFT SPLASH ANGLE CORRODED OTBD SIDE. R & R ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

CUSP WEB CRACKED AT BS 655, RBL 55. REPAIRED CUSP WEB IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,275 hrs · 26,741 cycles

FLOOR SUPPORT ANGLE CORRODED AT BS 192, LBL 55. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (RUDDER) · airframe 39,275 hrs · 26,741 cycles

EMPENNAGE RUDDER PANEL 370AR LOWER FWD CORNER ANGLE CRACKED AT RADIUS BEND. REPAIRED ANGLE IAW SRM & DRAWING.

Part: LIGHT — LOOSE (CABIN) · airframe 38,038 hrs · 25,949 cycles

RIGHT EMERGENCY EXIT LIGHT LOOSE AT ROW 24. R & R EEPLS IAW MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 37,615 hrs · 25,688 cycles

L1 DOOR EMERGENCY EVAC SLIDE CABLE DISCONNECTED. REMOVED AND REPLACED SLIDE ASSY PER AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 37,313 hrs · 25,508 cycles

EMERGENCY LIGHTS INOP BETWEEN ROW 5 TO ROW 12. SECURED CONNECTOR PER M/M.

Part: LIGHT — WEAK (COCKPIT) · airframe 36,500 hrs · 25,000 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT EXTREMELY DIM. RELAMPED COCKPIT OVERHEAD EMERGENCY LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,066 hrs · 24,726 cycles

FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 35,690 hrs · 24,464 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED CABLE IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 35,361 hrs · 24,246 cycles

FORWARD EMERGENCY BATTERY POWER SUPPLY FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

STRINGER CRACKED BETWEEN BS 1136 TO BS 1123, STR 2L. REPAIRED STRINGER PER SRM.

Part: DIODE — FAILED (CABIN) · airframe 35,361 hrs · 24,246 cycles

FWD EEPLS DIODE FAILED OPERATION CHECK. REMOVED AND REPLACED DIODE IAW WDM.

Part: FITTING — CRACKED (R1 DOOR) · airframe 35,361 hrs · 24,246 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER DOOR CLIP CRACKED. REMOVED AND REPLACED CLIP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

SKIN CORRODED BETWEEN BS 851 TO BS 870, BETWEEN STR 26R TO STR 26L. REPAIRED SKIN PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

LEFT CUSP WEB CORRODED AT BS 518. REPAIRED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 541 TO BS 560. REPAIRED WEB PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT SKIN CORRODED BETWEEN BS 446 TO BS 465. REPAIRED SKIN PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT CUSP WEB CORRODED AT BS 550. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

STRINGER CORRODED BETWEEN BS 832 TO BS 851, BETWEEN STR 29R TO STR 29L. REPAIRED STRINGER PER SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT SKIN CORRODED BETWEEN BS 465 TO BS 484. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT SKIN CORRODED BETWEEN BS 541 TO BS 560. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 35,361 hrs · 24,246 cycles

L1 DOOR INTERNAL STRUCTURE WEB CRACKED AT DOOR OPERATING MECHANISM. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

FWD CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 370 TO BS 362, STR 28R. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

T-ANGLE CORRODED BETWEEN BS 813 TO BS 832, STR 30R. REMOVED AND REPLACED T-ANGLE SUPPORT IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 465 TO BS 484. REPAIRED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 440 TO BS 446. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

STRINGER CORRODED AT BS 832, STR 27R. REPAIRED STRINGER PER SRM AND DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 446 TO BS 450. REPAIRED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

LEFT CUSP WEB CORRODED AT BS 507. REPAIRED WEB PER SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 35,361 hrs · 24,246 cycles

L1 DOOR UPPER BEAM AFT SIDE CRACKED. REPAIRED BEAM PER SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 35,361 hrs · 24,246 cycles

STRAP CORRODED AT BS 994, BETWEEN STR 29R TO STR 28R. REPAIRED STRAP PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 3,531 hrs · 24,246 cycles

LEFT KEEL BEAM ANGLE CRACKED AT STA 752. REPAIRED KEEL BEAM IAW SRM.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 35,331 hrs · 24,224 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD FRAYED. REMOVED AND REPLACED LANYARD IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS ON LT/RT SIDE OF AIRCRAFT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IN AFT CARGO PIT IAW B717 AMM CHAPTER 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EXTERIOR EMERGENCY LIGHTS FAILED TO EXTINGUISH WHEN SWITCHED OFF - (EXT WHEN IN ARM). REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY IAW AMM 33-51-06 OPS CHECK NORMAL IAW AMM 33-51-00.

Part: LIGHT — MALFUNCTIONED (CABIN)

OVERWING EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WHEN EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. PERFORM OPERATIONAL CHECK OF THE EMERGENCY LIGHTS SEVERAL TIMES, POWER A/C DOWN WITH EMERGENCY LIGHT ON & OFF, COULD NOT DUPLICATE AT THIS TIME, REF 33-51, CLEARED MEL.

Part: NUT — MISSING (EXTERIOR LIGHT)

RIGHT EXTERIOR EMERGENCY LIGHT, 2 MISSING ANCHOR NUTS. UNABLE TO SECURE LENS. SECTION NR 1 OF EA 17-33-02830IR COMPLIED WITH. LENS IS SECURED. RE-SECURED RT EMER LT ANCHOR NUTS CHECKS GOOD REF MM 33-51. MDDR CLEARED.

Part: LIGHT — INOPERATIVE (AC BAY)

EMER LIGHT AT AFT ACCESSORY L/CATWALK (AFT) HAS 1 BULB INOP.

Part: LIGHT — MISSING (CABIN)

SEAT 1DF (FWD) E-PATH LIGHTS & LENS MISSING. INSTALLED MISSING LAMP AND LENS IAW AMM 33-51-01-420-002. =/003. OPS CHECK NORMAL IAW AMM 33-51-00.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2979.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2987.

Part: STRUCTURE — CRACKED (NACELLE)

RIGHT FIXED COWL APRON HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER AND FILLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237 TO 246, RBL24, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F.

Part: STRAP — CORRODED (FUSELAGE)

FILLER STRAP BETWEEN SAT 160-200 I/B OF GALLEY DOOR SCUFF PLATE CORROSION. REMOVED AND REPLACED FILLER STRAP BETWEEN STA 160-200 I/B OF SCUFF PLATE PER B717 SRM 51-41-01, AND DRAWING PL 9957828.

Part: WEB — CORRODED (FUSELAGE)

CORROSION AT FLOOR WEB BETWEEN LBL 7 AND RBL 7 FROM STA 160-200. CUT OUT DAMAGED SECTION FROM STA 160-200 LBL 6 TO LBL 7 AND INSTALL DOUBLER REPAIR 7075-T6-.25 & .02 FILLER SIZE 19.5" X 39.75" PER REF SRM 51-70-10 REP 2 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CORROSION AT FLOOR SUPPORT RBL 7 FROM STA 148 TO 200. REMOVED AND REPLACED FROM STA 148 TO 200 RBL 7 PER REF B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORROSION FROM RBL 7 TO RBL 46 AT STA 200. INSTALLED FLOOR SUPPORT AT MAIN CABIN RBL 7 TO RBL 46 STA 200 REF 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, LBL 6 TO RBL 6 AT FS 160, CORROSION. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-42-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORROSION FROM RBL 16 TO LBL 16 AT STA 237. INSTALLED NEW FLOOR SUPPORT RBL 16 TO LBL 16 STA 237 REF B-717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, LBL 9 AT STA 200, CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-41-02.

Part: WEB — CRACKED (FUSELAGE)

CRACK WEB AT STRINGER 15 LEFT AND LONG 209. INSTALLED DOUBLER REPAIR 7075T6.050 ON LONG 15 AND STA 200 PER REF B717 SRM 51-70-10 REPAIR 2.

Part: ENGINE — UNSERVICEABLE (NR 2)

NR 2 ENGINE SHUT DOWN IN FLIGHT; TGT REACHED 150 DEGREES CELSIUS. REMOVED AND REPLACED NR 2 ENGINE IAW TASK CARD 603; MM 71-00.

Part: THRESHOLD — CORRODED (CARGO BAY)

FWD CARGO DOOR THRESHOLD CORRODED BEYOND LIMITS. REPAIRED PER B717 SRM 53-20-15, INSTALLED NEW PAN.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT ROW 21 ABOVE OVERWING EXITS LT & RT INOP. REMOVED AND REPLACED E-BATTERY AT STA 715-737R (B5-230) IAW-AMM-33-51-10, OP CHECKS GOOD.

Part: SHROUD — BROKEN (AFT CABIN)

EXIT SIGN SHROUD AT AFT FLIGHT ATTENDANTS HANDSET BROKEN. REPLACED LIGHT ASSY, OPS CHECK GOOD REF MM 33-28.

Part: COMPRESSOR — STALLED (NR 2 ENGNE)

COMPRESSOR STALL NR 2 AFTER T/O. HAD ROLLBACK TO IDLE. FOR VIBRATION FOR 3 TO 5 MIN RAN CHECK LIST- ENGINE CAME BACK WE RETURNED FOR LANDING. NO TGT EXCEEDED. REPLACED NR 2 ENG A/C OK FOR SERVICE

Part: STRUCTURE — DENTED (FUSELAGE)

DENT OUTSIDE F/O'S WINDOW AND SLIGHTLY FWD, DENT AT STA 83 MEASURES 3.5" X 5.0" X .110" AND DENT AT STA 76 MEASURES 3.5" X 3.5" X .050". CUT OUT DAMAGE AS PER B717 SRM 53-00-01, INSTALLED FINGER DOUBLER REPAIR AS PER B717 SRM 53-00-01.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS)

AIRCRAFT A/P DISCONNECTED AT 13,000 FEET DURING DESCENT. AT THAT POINT HAD NO ROLL CONTROL. BOTH YOKES HELD FIRMLY BY ?. AFS OVERRIDE OFF, STILL NO ROLL CONTROL. AFTER 3-4 MINS CONTROLS RELEASED. AIRCRAFT OPERATED W/O A/P TO LANDING. FOUND -AILERON SERVO/AILERON CMD RESPONSE- FAULT MESSAGE ON FCC-2 IN FAULT HISTORY, LAST LEG. ACCOMPLISHED FIM 22-12 TASK 808. ALL CHECKS NORMAL. REPLACED DUAL AILERON SERVO AS PER AMM 22-12-01. INSPECTED AILERON CONTROL CABLES & ALL ASSOCIATED LINKAGE FOR OPERATION & CONDITION. NO DEFECTS NOTED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 DOOR EVACUATION SLIDE PRESSURE INDICATES JUST OUT OF GREEN ARC. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER B717 AMM 25-61-01.

Part: ODOR — DETECTED (CABIN)

RIGHT AFTER TAKEOFF A STRONG BURNING SMELL WAS FELT THROUGHOUT CABIN BEING THE STRONGEST IN THE BACK ALL THE WAY TO THE COCKPIT. AIR TURNBACK, LANDING WITH A WEIGHT OF 105100 AT TOUCHDOWN, SMOOTH LANDING. RAN APU, RT AND LT PACKS WITH VARIOUS TEMPERATURES ADJUSTMENTS AND PACKS OP'D TOGETHER, RAN ENGINES AT HIGH POWER FOR 30 MINUTES. PACK TEMPS AND PRESSURES NORMAL. NORMAL SMELL THROUGHOUT THE CABIN, NO ABNORMAL SMELL NOTED. REF 36-10.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

DURING SERVICE CHECK FOUND EMERGENCY EXTERIOR LIGHTS INTERMITTENT OPERATION (OVERWING LIGHTING). REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY, IAW B717 33-51-06, OPS NORMAL.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

TEMPORARY REPAIR OF FORWARD CARGO PIT FLOORBOARD STA 218 TO 331, REQUIRES FAB OF NEW FLOORBOARD. INSTALLED NEW FLOOR BOARD IAW 17-2558-A1529 REV IR AND RES NR 02-0824.

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

FORWARD CARGO PIT, FLOORBOARD STA 465 TO 541 HAS SEVERAL PUNCTURES. INSTALLED NEW FLOOR BOARD AT FORWARD CARGO PIT IAW B-717 SRM 25-58-01, AND AS PER EA NR 17-2558-A1521 REV IR AND RES NR 02-0824.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

TEMPORARY REPAIR OF FORWARD CARGO PIT FLOORBOARD STA 369 TO 426, FLOORBOARD REQUIRES FAB OF NEW BOARD. INSTALLED NEW FLOOR BOARD IAW EO 17-2558-A1530, REV IR AND RES 02-0824.

Part: SLIDE — DEFECTIVE (R1 DOOR)

R1 DOOR SLIDE GIRTH BAR WAS NOT SECURED AFTER FLIGHT AND SLIDE WAS DEPLOYED BY CLEANERS WHEN R1 DOOR OPENED. SLIDE WAS REPLACED 2ND TIME DUE TO FIRST SLIDE FACE PLATE ROTATED AND BAD FROM STOCK. REMOVED AND REPLACED SLIDE.

Part: ODOR — DETECTED (CABIN)

SMOKE SMELL IN AFT CABIN. PERFORMED GVI AND SYSTEM CHECKS, AIRCRAFT SHOWS NO SIGN OF ORIGIN OF ODOR.

Part: PLATE — BROKEN (CABIN)

FOUND EMERGENCY PATH LIGHT BACKING PLATE BROKEN AT ROW 21. REPLACED BACKING PLATE.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND NACELLE LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK IAW B717 MM 33-51.