N966AT

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,984 hrs · 44,510 cycles

AFTER REMOVAL OF INBOARD RT SEAT TRACK, SUB FLOOR SKIN IS CORRODED. REPAIRED SUB FLOOR MEMBRANE IAW SRM 53-00-55 (1375171)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,742 hrs · 42,493 cycles

THE EMERGENCY LIGHTS POWERED BY BATTERIES B5-235 AND B5-118 ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS B5-235 AND B5-118 PER B717 AMM 33-51. OK FOR SERVICE. (LP #6519628)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,795 hrs · 40,802 cycles

FOUND THE FORWARD ENTRANCE EXIT PATHWAY SIGN GOING INTO COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. LIGHT OPERATION NOW CHECKS GOOD IAW B717 AMM 33-51-18. (LP #5448489)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,165 hrs · 40,297 cycles

THE EMERGENCY LIGHTS DON'T OPERATE CORRECTLY DURING SERVICE CHECKS. SUMMARY OF NRC 00700: DURING CONTINUITY AND VOLTAGE CHECK TERMINAL 10, 11, AND 12 ON S3-559 WERE FOUND WITH CONTINUITY BETWEEN THEM. TERMINAL 10, 11, AND 12 ON S3-559 WERE INSTALLED CORRECTLY PER B717 WDM 33-51-11. EMERGENCY LIGHT BATTERY ASSEMBLY WAS REPLACED PER B717 AMM 33-51-04. OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM WAS PERFORMED PER B717 AMM 33-51-00 710-801. TEST OK. (LP #0017539)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,165 hrs · 40,297 cycles

IMPROPERLY INSTALLED TAIL-CONE KEVLAR LANYARD (CAT). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00703: TAIL-CONE KEVLAR LANYARD WAS INSTALLED CORRECTLY PER B717 AMM 53-52-01 400-801 STEP E(3). (LP #0016261)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

ELONGATED HOLES (2 EA) ON FAIRING PANEL 360AT. SUMMARY OF NRC 00511: ANGLE WAS FABRICATED AND REPLACED PER DWG 5912175 REV BR AND B717-200 SRM 51-41-02-0G AND FAIRING WAS REPAIRED PER ERA 612574-14 REV ORIGINAL, AND PRI 612574-14 REV 1. ASSOCIATED ER/A 14-612574 ADDED FOR AC 9525. (LP #0013280)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO. SUMMARY OF NRC 00366: CORROSION LEVEL 2. SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO WAS REPAIRED PER ERA 612306-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612306 ADDED FOR AC 9525. (LP #0000189)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00649: FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIG 201 SHEET 1. (LP #0000432)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA. SUMMARY OF NRC 00163: CORROSION LEVEL 2. CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA WAS REPAIRED PER PRI 611928-14 REV 3 AND ER/A 611928-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-611928 ADDED FOR AC 9525. (LP #0001688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT. (CCT) SUMMARY OF NRC 00622: CORROSION LEVEL 2. STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0000131)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON BRACKET AND SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR. SUMMARY OF NRC 00099: SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1, AND BRACKET (FITTING) INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-02-0G. (LP #2999912)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00336: CORROSION LEVEL 2. SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #2999010)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00230: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R-2 REPAIR 2 & 53-20-06-2R-2 REPAIR 2. (LP #2997973)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00203: CORROSION LEVEL 2. INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2996865)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00197: CORROSION LEVEL 2. FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2. CORROSION ON FRAME WAS ATTENDED UNDER NRC 00673. (LP #2996824)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00349: CORROSION LEVEL 2. FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND DWG 9912243 REV JS. (LP #2995243)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION EXCESSIVE ON STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00643: CORROSION LEVEL 2. STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PER DWG 3936440 REV D, DWG 5936021 REV EH, B717 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2995206)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116 WAS REPAIRED PER B717 SRM 53-00-05-2R REPAIR 2 FIG 201 SHEET 2. (LP #2992175)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 0345: CORROSION LEVEL 2. FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 9958215 REV AM. (LP #2992309)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

FITING AT STA 620 TO STA 636 L-30 HAD CORROSION FOUND ON SAME FITTING. CORROSION LEVEL 2. FITTING AT STA 620 TO STA 636 L-30 WAS FABRICATED PER DWG 5971577 REV D. FITTING OF STA 620 TO STA 636 L-30 WAS REPLACED PER DWG 5971577 REV D B717 SRM 51-41-05-0G AND 51-41-01-0G. (LP #2992173)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FLOOR FITTING STA 200 TO 218 RBL=11 WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C, ORIGINAL THICKNESS IS 0.975IN AND MINIMUM REMAINING THICKNESS IS 0.850IN THEREFORE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 (C) FIG 103. SUMMARY OF NRC 00614: CORROSION LEVEL 2. FLOOR FITTING STA 200 TO 218 RBL=11 WAS REPLACED PER DWG 5968021 AND B717 SRM 51 -41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #2993364)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON INTERCOSTAL STA Y=916 OVER STRG 28R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00328: CORROSION LEVEL 2. INTERCOSTAL ON STA Y=908 TO Y=927 STGR 28 RH WAS REPLACED PER DWG 9957704 REV M, B717 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2991968)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00139: CORROSION LEVEL 2. WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (LP #2990111)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00603: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2988599)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CABIN FLOOR WEB DOUBLER BTW STA=641 TO 646 X=-58. CORROSION ON WEB DOUBLER BTW STA=476 TO STA=498 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00542: CORROSION LEVEL 1. CORROSION ON CABIN FLOOR WEB DOUBLER (SPLICE ANGLE) BTW STA=641 TO 646 X=-58 WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C, (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ORIGINAL THICKNESS=0.080", REMAINING THICKNESS=0.075", PERCENTAGE REMOVAL THICKNESS=6.5 %. THEREFORE, IT IS WITHIN LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PAR 4 C (2), FIG 103 AND DCMD/BOEING NDTSPM PART 4, 04-00-06 PAR 4. CORROSION LEVEL 2. CUSP WEB BTW STA=476 TO 487 RH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 207. (LP #2988443)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS ON CUSP WEB RBL=57 AND STA 266, 331, 926, 935, AND 944. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND REMAINING THICKNESS OF 0.007 INCHES, THE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, PAR 4 C, FIG 101 AND BOEING NDT SPM PART 4, 04-00-06 PAR 4 FIG 9. SUMMARY OF NRC 00610: CORROSION LEVEL 2. REPAIR ON CUSP WEBS (RBL=57 AND STA, 266, 331, 926, 935, AND 944) WAS PERFORMED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIGURE 211 AND 216. (LP #2985216)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CUSP WEB STA Y=680 X=-50, AT CABIN PAX. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB BTW STA 655 TO STA 684 X=-50 AT CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 4 AND 5 FIGURE 223. (LP #2983819)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CABIN FLOOR CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO X=-54, STA=636 TO 655 FROM X=-55 TO X=-46, AND BTW STA=655 TO STA=674 FROM X=-55 TO X=-46 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00549: CORROSION LEVEL 2. CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO X=-54, STA=636 TO 655 FROM X=-55 TO X =-46 WERE REPAIRED AND REPLACED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIGURE 216 AND DWG 9910151 REV CH, BTW STA=655 TO STA=674 FROM X=-55 TO X=-46 WAS REPAIRED WITH NRC 00619. (LP #2983810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00093: WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PER DRAWING 9929480-49 REV BW, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G PAR 8. (LP #2982829)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CUSP WEB STA FROM Y=860 TO Y=870 X=- 58, AT CABIN PAX. SUMMARY OF NRC 00621: CORROSION LEVEL 2. CUSP WEB STA FROM Y=860 TO Y=870 X=- 58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 216. (LP #2982286)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

AFTER INNER SKIN REMOVAL, A CRACK WAS FOUND ON BEAM #1 AFT SECTION OF L1 DOOR. SUMMARY OF NRC 00647: BEAM #1 AFT SECTION OF L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2981121)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CUSP WEB STA Y=256 X=-58. SUMMARY OF NRC 00618: CORROSION LEVEL 2. CUSP WEB STA 256 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 220. (LP #2978269)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS ON CABIN FLOOR CUSP WEB STA=377, STA=390, STA=417, AND STA=636 BTW -X=46 TO -X=59 RH SIDE AT PAX CABIN. ORIGINAL THICKNESS IS 0.020IN REMAINING THICKNESS IS 0.014IN THEREFORE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4 C, FIG 101. SUMMARY OF NRC 00613: CORROSION LEVEL 2. CUSP WEB STA=377, STA=390, AND STA=417 BTW -X=46 TO -X=59 RH SIDE WAS REPAIRED PER B717 SRM 53-00-55-2R-4. CUSP WEB ON STA=636 AREA OUT OF LIMITS WAS REPAIRED WITH NRC 00549. (LP #2978057)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS ON CUSP WEB X=+57 STA 444, 517, 523, 544 TO 557, 608, 646 TO 660, AND 804 AT CPAX. WITH AN ORIGINAL THICKNESS=0.020 INCHES AND REMAINING THICKNESS=0.014 INCHES THEREFORE AREAS ARE OUT LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, PAR 4 C, FIG 101 AND DC-MD/BOEING NDT SPM PART 4, 04-00-06 PAR 4 FIG 9. SUMMARY OF NRC 00611: COROSION LEVEL 2. CUSP WEB X=+57 STA 444, 517, 523, 544 TO 557, 608, AND 804 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 215 AND FIG 216 AND BTW STA 646 TO 660 WAS REPLACED WITH NRC 00400. (LP #2977775)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL. SUMMARY OF NRC 00381: FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976623)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB. SUMMARY OF NRC 00628: CORROSION LEVEL 2. CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB WERE REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, FIG 215. (LP #2975964)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION WAS FOUND AT FLOOR SUPPORT ON STA 200.0 LBL 12. SUMMARY OF NRC 00634: CORROSION LEVEL 2. FLOOR SUPPORT ON STA 200.0 LBL 12 WAS REPLACED PER B717 SRM 51-40-08-0G AND WITH NRC 00615. (LP #2976011)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA 200 AND LBL=5-10 AT FWD CPAX. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND MINIMUM REMAINING THICKNESS OF 0.013, THE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 C AND FIG 103. SUMMARY OF NRC 00615: CORROSION LEVEL 2. DIAPHRAGM BTW STA 200 AND LBL=5-10 AT FWD CPAX WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #2975860)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX. SUMMARY OF NRC 00301: CORROSION LEVEL 2. FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX WERE REPLACED PER B717 SRM 51-41-01-0G. (LP #2976176)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00389: FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2975043)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00388: FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976018)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS WAS FOUND ON THE CUSP WEB STA 696 AND 715 X=-58, AT CABIN PAX. SUMMARY OF NRC 00620: CORROSION LEVEL 2. CUSP WEB STA 696 AND 715 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2974760)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON ANGLE OF LOWER BEAM APPROX STA 185 AT L1 DOOR. SUMMARY: CORROSION LEVEL 2. ANGLE OF LOWER BEAM APPROX STA 185 AT L1 DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-04-0G. (LP #2974532)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FLOOR FITTING BWT STA 148 TO STA 200 AND LBL/RBL=7 (2 EA), STA 148 AND LBL=10 (1 EA), ALSO STA 198 AND LBL=44 (1 EA) AT FWD CPAX. SUMMARY OF NRC 00302: CORROSION LEVEL 2. FLOOR FITTING ON STA 198 LBL=44 WAS REPLACED PER B717 SRM 51-41-05-0G & FLOOR FITTING BWT STA 148 LBL=10 WAS CLEANED PER PS 900-1-2-2 NO. 02 & GVI PER B717 AMM 05-21-02 210-801 WAS PERFORMED AND NO CORROSION WAS FOUND. (LP #2970264)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON CUSP WEB STA 717-723 AND RBL=44 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA 717-723 AND RBL=44 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 4 AND 5, FIGURE 221. (LP #2970302)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION OUT OF LIMITS. CORROSION ON FLOOR FITTINGS STA 200 RBL=9 TO 44 AND STA 196 LBL=9 TO 44. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.035IN AREA, THUS IT IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 (C) FIG 103. SUMMARY OF NRC 00612: CORROSION LEVEL 2. FLOOR FITTINGS STA 200 RBL=9 TO 44 AND STA 196 LBL=9 TO 44 WERE REPLACED PER B717 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2970273)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,164 hrs · 40,296 cycles

CRACK ON CUSP WEB STA 717-723 AND RBL=44 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA 717-723 AND RBL=44 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR. 4 AND 5, FIGURE 221. (LP #2970366)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON FERRULES OF FLOOR PANELS 9936601- 351, 121VF, AND 121RF. SUMMARY OF NRC 00539: FLOORS PANELS 9936601-351, 121VF, AND 121RF WERE FABRICATED PER B717-200 AMM 25-58-01 350-801C2 PAR A AND ER/A 591778-14TR REV ORIGINAL SECTION I: PERMANENT REPAIR. FLOOR PANELS WERE INSTALLED PER B717 AMM 25-58-01-350-801C2. ASSOCIATED ER/A 14-591778 ADDED FOR AC 9525. (LP #2968548)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,164 hrs · 40,296 cycles

CORROSION ON SPLICE BTW STA Y=895 TO STA Y=901 L18R (BELOW THE CABIN FLOOR) AT CABIN PAX. SUMMARY OF NRC 00273: CORROSION LEVEL 2. SPLICE ON BTW STA Y=895 TO STA Y=901 L18R WAS REPLACED PER DWG 9930612 REV CB AND B717 SRM 51-41-05-0G. (LP #2964582)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,821 hrs · 40,004 cycles

THE PILOT NOTICED A LOOSE PART NEAR 1R DOOR GIRT BAR. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED 1R DOOR SLIDE DEPLOY MECHANISM. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #4399428)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,120 hrs · 39,394 cycles

AIRCRAFT 9525, ROWS 1-13 EMERGENCY LTS INOP. CORRECTIVE ACTION: REPLACED 2 EMERGENCY BATTERY PACK AT LOCATION 342R, AND 398R. (LP 4112094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,186 hrs · 39,454 cycles

A TRAY TABLE WAS DISCOVERED TO BE INSTALLED IN THE EMERGENCY EXIT ROW ON SEAT 21B. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED TRAY TABLE ASSEMBLY FROM THE SEAT BACK. THE AIRCRAFT IS OK FOR SERVICE. (LP #4112060)

Part: STEERING SYS — OUT OF ALIGNMENT (NLG) · airframe 55,714 hrs · 39,033 cycles

DURING THE TAKEOFF ROLL, FROM 80 KNOTS TO V1, THE AIRCRAFT YAWED LEFT. YAW ENOUGH TO REQUIRE HALF RUDDER TO MAINTAIN CENTERLINE. AIRCRAFT ALSO MOVED, YAW LT ON LANDING, AGAIN ENOUGH TO REQUIRE HALF RUDDER CORRECTION. MX IAW FIM 32-50-00 810-801, FOUND LT NLG TIRE PRESSURE 10 PSI LOW & REPLACED BOTH NLG TIRES IAW 32-42-01. MAIN TIRES WERE SPUN & PRESSURE CHECKED. SHIMMY DAMPERS, STEERING CONTROL VALVE, & LOAD SPRING CHECKED. EACH RESULTED IN NO ISSUES. CHECKED NLG WHEEL CENTERING USING WHEEL RIGGING FIXTURE & FOUND STEERING OFF 1 DEGREE TO LT. ADJUSTED STEERING CABLES 123D & 124D. SAFETIED BOTH M & P TURNBUCKLES IAW AMM 32-51-01. PERFORMED TAXI CHECK AND AIRCRAFT TRACKED NORMAL. OK FOR CONTINUED SERVICE.

Part: ACTUATOR — FAILED (RT MLG) · airframe 55,614 hrs · 38,953 cycles

THE FLIGHT CREW REPORTED AN IMMEDIATE LOSS OF RIGHT HYDRAULIC QUANTITY UPON GEAR EXTENSION DURING APPROACH FOR LANDING. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES. THAT LANDING WAS UNEVENTFUL, BUT THE MAIN GEAR DOORS DID CONTACT THE RUNWAY. CORRECTIVE ACTION: MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR HAD FAILED AND WAS THE SOURCE OF THE FLUID LOSS. THE RIGHT MLG RETRACT ACTUATOR, ALL OF THE RIGHT SYSTEM HYDRAULIC FILTERS, THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP, AND ALSO THE ELECTRIC HYDRAULIC PUMP WERE REPLACED DUE TO COMPLETE SYSTEM FLUID LOSS & PROBABLE CAVITATION.

Part: ACTUATOR — FAILED (RT MLG) · airframe 55,614 hrs · 38,953 cycles

THE FLIGHT CREW REPORTED AN IMMEDIATE LOSS OF RIGHT HYDRAULIC QUANTITY UPON GEAR EXTENSION DURING APPROACH FOR LANDING. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES. THE LANDING WAS UNEVENTFUL, BUT THE MAIN GEAR DOORS DID CONTACT THE RUNWAY. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR HAD FAILED AND WAS THE SOURCE OF THE FLUID LOSS. THE RIGHT MLG RETRACT ACTUATOR, ALL OF THE RIGHT SYSTEM HYDRAULIC FILTERS, THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP, AND ALSO THE ELECTRIC HYDRAULIC PUMP WERE REPLACED DUE TO COMPLETE SYSTEM FLUID LOSS & PROBABLE CAVITATION. (LP #9483660)

Part: LANYARD — BROKEN (L1 DOOR) · airframe 55,378 hrs · 38,738 cycles

THE FLIGHT CREW DICOVERED THAT THE METAL CABLE FROM 1L DOOR SLIDE TO GIRT BAR WAS BROKEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. *** CONTRACT MAINTENANCE REPLACED THE L1 DOOR SLIDE RELEASE LANYARD PER B717 AMM 25-61-01. AIRCRAFT IS OK FOR SERVICE. (LP #9580716)

Part: NONE — NONE · airframe 55,219 hrs · 38,586 cycles

TAIL COMPARTMENT EMERGENCY CEILING LIGHTS AND TAIL CONE SLIDE EMERGENCY LIGHTS INOP LOG-PAGE UPDATED @ 27OCT22 0620 UTC 02 CORR BY HOLDEN 00466094 CLT 27OCT22 ATA 3352 RII: N ENTR 00466094 W R/R EMERGENCY LIGHT BATTERY ASSY PER B717 AMM 33-51. P/N OFF 803949-1, P/N ON AD-803949-1. BATTERY PACK# B5-116. OP TEST OF EMERG LIGHTING CKS GOOD. (LP #9346330)

Part: COVER — LOOSE · airframe 54,331 hrs · 37,792 cycles

THE AFT SIDE COVER IS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE SECURED THE SLIDE COVER AND REPLACED THE TAIL CONE SLIDE PER JIC B717 CARD 2561-7006. INSPECTED PER B717 CARD 2561-9001 ALL RII COMPLIED WITH OK FOR SERVICE (QC 5199). (LP #8805410)

Part: CIRCUIT BREAKER — TRIPPED · airframe 53,796 hrs · 37,298 cycles

SHIP 9525 - THE CREW DIVERTED THE AIRCRAFT TO CLT AFTER THE LOSS OF THE RT DC BUSS AT CRUISING ALTITUDE. THE #4 AND #5 SCREENS WENT BLANK AND AP DISENGAGED. THE QRH WAS COMPLIED WITH AND THEN DUE TO WEATHER AT THE SCHEDULED DESTINATION THE DECISION WAS MADE TO DIVERT TO CLT BASED ON BETTER CONDITIONS. AN EMERGENCY WAS DECLARED BECAUSE THE CREW WAS NOT SURE WHAT THE FINAL LANDING CONFIGURATION WOULD BE BASED ON EICAS STATUS MESSAGES. A NORMAL UNEVENTFUL APPROACH AND LANDING INTO CLT WAS ACCOMPLISHED AND THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. CORRECTIVE ACTION: FOUND RT PCDU BREAKER CB3 TRIPPED. REPLACED RIGHT PCDU. OPS CHECKS GOOD. (LP #8251994)

Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON UPPER CENTER TANK SKIN AT STA. 745, RBL 23- RBL33. SUMMARY NRC 001-0284:5310-2003/012 00412: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863517)

Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON UPPER CENTER TANK SKIN AT STA. 705 RBL 53. SUMMARY NRC 001-0284:5310-2003/014 00414: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863519)

Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON UPPER CENTER TANK SKIN AT PULLEY SUPPORT ANGLE AT STA. 745 LBL 25-34. BLENDED AND REMOVED ALL CORROSION REF B717 SRM 57-10-01-1A. UT THICKNESS INSPECTED AND MAPPED ON 1/2" GRID PER NDTSPM PART 04-00-00 TO 04-00-09. ORIGINAL THICKNESS IS .252. LOWEST BLENDED AREA MEASURES .190. FOUND TO BE OUT OF LIMITS PER B717 SRM 57-10-01-1A. REPAIRED PER ERA 592454-14 REV. ORIG. (LP #1863538)

Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON UPPER CENTER TANK SKIN AT PULLEY SUPPORT ANGLE AT STA. 745 RBL 48-53. SUMMARY NRC 001-0284:5310-2003/015 00415: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863524)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

ON OK TO CIC R1 SUBFLOOR AREA: CORROSION WAS FOUND ON SUBFLOOR AND FLOOR PANEL SUPPORT. ALSO AREAS OF BARE METAL. (MARKED). SUMMARY NRC 001-0024:2040-0024/002 00454: REMOVED CORROSION AND CHECKED LIMITS REF B717 SRM 53-00-00-1A. REPLACED FLOOR SUPPORTS AS REQUIRED REF BAC DWG #9936534. AREAS OF BARE METAL, TREATED AND PAINTED REF DELTA P.S. 900-3-6- NO. 34. (LP #1861216)

Part: SKIN SPLICE — CORRODED (BS 900 S29-30L) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

AFT CARGO INTERNAL SKIN SPLICE CORRODED AT STA 900 BETWEEN STR 30 AND 29LT. SUMMARY SEE NRC 061-0008:5331-2001/005 00304: REPAIRED PER ER/A 592326-14 REV A ASSOCIATED ER/A 00-592326 ADDED FOR AC 9525. (LP #1860302)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 52,135 hrs · 35,830 cycles

LT WING UPPER SURFACE HAS CORROSION AT FASTENERS AFT EDGE OF UPPER SURFACE FWD OF INBOARD CORNER OF OUTBOARD SPOILER (MKD). COMPLIED WITH PRI 592282-14 REV. 0 AND 1. FINAL ERA AND PRI MATCH. REMOVED CORROSION AT STATION XRS267 AT STRINGER 1 AND CHECKED LIMITS REF B717 SRM 57-10-01. IT WAS FOUND TO BE OUT OF LIMITS. ORIGINAL THINCKNESS IS .138 REMAINING THICKNESS .100. RECEIVED ERA 592282-14 REV. ORIG AND FOUND TO MATCH PRI 592282-14 REV 1 REPAIRED PER ERA 592282-14 REV ORIG. (LP #1855339)

Part: RELEASE MECH — FAILED (TAIL CONE) · airframe 52,134 hrs · 35,828 cycles

TAIL-CONE RELEASE SYSTEM. FAILED STEP 2.G.(5). CLAMP (ITEM 28) TO CONDUIT (ITEM 29) CLEARANCE WAS BELOW 0.5 IN. WITH LATCH LEVERS IN FULL OPEN POSITION. TASK CARD 5352-2001, FIG. 5, SHEET 4. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED LOCK CABLE CLAMP TO BE WITHIN CLEARANCE LIMIT OF THE CONDUIT AS PER B717 AMM 53-52-01 STEP E(1)(J) FIG 504. (LP #1855352)

Part: STRINGER — CORRODED (BS 908 S30) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

IN THE AFT CARGO, STRINGER 30 IS CORRODED AT FS 908. MARKED. REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1.

Part: FRAME — CORRODED (BS 954) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON FRAME ATTACH POINT FRAME STATION 954 AFT SIDE. REPLACED ATTACH POINT PER LONG BEACH DRAWING #9958214. (LP #1852991)

Part: FRAME — CORRODED (BS 974 S27-28L) · corrosion level 2 · airframe 52,134 hrs · 35,828 cycles

CORROSION ON FRAME ATTACH AT STA 974 BETWEEN STRINGER 27 AND 28L. REPLACED ATTACH CLIP PER LONG BEACH DRAWING #9958215. (LP #1853038)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,209 hrs · 34,418 cycles

THE LEFT ENTRY DOOR EMERGENCY LIGHT WENT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,517 hrs · 32,526 cycles

CRACK IN FRAME AT STATION 737 RT IN RADIUS AT FLOOR LEVEL. CRACK GREATER THAN 125", CONDITION 3, REF AA5310-01439-01D. NRC 075-0004:5310-01439-01D/001 00172 FRAME REPLACED ON ROUTINE CARD 083-0002:5310-01439-02B.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,517 hrs · 32,526 cycles

FOUND DENT 13 INCHES AFT OF L1 DOOR UPPER RIGHT HAND CORNER. CUT OUT DAMAGE SKIN UPPER AFT SIDE OF L1 DOOR REF SRM 53-02-01 REPAIR 1. FABRICATED FINGER DOUBLER REF SRM 53-02-01 REPAIR 1. TREATED AND PRIMED FINGER DOUBLER AND FILLERS REF SRM 53-02-01 REPAIR 1. INSTALLED FINGER DOUBLER AND FILLERS REF SRM 53-02-01.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 45,755 hrs · 31,352 cycles

EMERGENCY EXIT SIGN LENS FELL OFF. REINSTALLED THE LENS ON THE EMERGENCY EXIT SIGN AT ROW 20. OPS NORMAL IAW AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,674 hrs · 31,303 cycles

ON SERVICE CHECK MAINTENANCE FOUND THAT THE EXIT SIGN OVER BOTH LT AND RT AFT OVERWING EXITS DO NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUPPLY B5-230 PER AMM 33-51. THE OPERATIONAL CHECK WAS GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 45,495 hrs · 31,182 cycles

EMERGENCY EXT SIGN HAS BEEN KNOCKED OFF. MAINTENANCE REINSTALLED THE SIGN AND OPERATIONAL CHECKS ARE GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,394 hrs · 31,106 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING. REINSTALLED THE SIGN COVER. OK FOR SERVICE.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 45,330 hrs · 31,053 cycles

MID CENTER EXIT SIGN. BACKSIDE COVER HAS FALLEN OFF. INSTALLED THE COVER.

Part: COVER — LOOSE (EXIT SIGN) · airframe 44,853 hrs · 30,715 cycles

EMERGENCY EXIT SIGN COVER LOOSE, LOCATION 604. ADJUSTED EXIT SIGN, OK FOR SVC.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,777 hrs · 30,677 cycles

EMERGENCY EXIT SIGN LENS MISSING OVER R1 DOOR. INSTALLED A NEW LENS, OPS CHECKED GOOD.

Part: DOOR — DENTED (APU) · airframe 44,540 hrs · 30,488 cycles

APU DOOR HAS DENTS INCURRENCE PER TOPP 40-60-05, PARAGRAPH XBZ THAT THIS CONDITION IS ACCEPTABLE FOR A SINGLE NON-REVENUE FERRY FLIGHT FROM SLC TO VQQ PROVIDED LEFT HAND APU DOOR IS CLOSED. REPLACED LEFT APU ACCESS DOOR IAW SRM 51-41-01 AND DRAWING 5915081 REV AU.

Part: FRAME — CORRODED (BS 1095) · corrosion level 3 · airframe 44,540 hrs · 30,488 cycles

CORROSION TO THE LOWER FRAME TEE CAP AT BS 1095.87 NEAR LONGERON 28R. FOUND OUT OF LIMITS IAW SRM 53-00-00 AND DRAWING S4923323 REV -. REPAIRED AREA IAW ER/A 553860-14 REV. ORIGINAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,438 hrs · 29,719 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 42,756 hrs · 29,144 cycles

VERTICAL STABILIZER L/E HAS A 3" CRACK & FASTENERS PULLED INTO THE SKIN & ELONGATED HOLES BY LWR VOR ACCESS PANELS, REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS USING 7075-0 HEAT TREATED TO 7075-T6 2090. INSTALLED REPAIR PARTS IAW ER/A 545681-14AD REPETITIVE INSPECTION EVERY 3300 FLIGHT CYCLES.

Part: LONGERON — CORRODED (BS 927-946) · corrosion level 2 · airframe 42,756 hrs · 29,144 cycles

LONGERON 30 AND SPLICE CORRODED FROM BS 927-946. BLENDED CORROSION ON L30 SPLICE AT BS 927 TO BS 946 ORIGINAL THICKNESS .250 REMAINING .245 FOUND TO BE WITHIN LIMITS IAW 53-00-00 AND 53-00-05, REPAIR 2, FIG 201, TAG 1768. BLENDED L30 BETWEEN BS 927 AND BS 946 FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS .125, REMAINING .087. REPLACED L30 BETWEEN BS 890 AND BS 946 IAW SRM 51-41-02. REPLACED ANTENNA MOUNT BOX IAW SRM 51-41-02. ALSO INSTALLED NEW ANTENNA. OPS CHECK GOOD IAW AMM 23-12-00-710-801.

Part: SUPPORT — CRACKED (BS 606) · airframe 42,755 hrs · 29,143 cycles

LOWER FUSELAGE, UNDER WING BARREL KEELBEAM BS 606 CRACKED KEELBEAM SUPPORT, MARKED. REMOVED DAMAGED FORMER LT KEEL BS 606. REPAIRED FORMER IAW ER/A 545683-14MA. REINSTALLED FORMER IAW ER/A 545683-14MA, STEPS 1 THRU 10.

Part: DOOR FRAME — CORRODED (R1) · airframe 42,756 hrs · 29,144 cycles

R1 DOOR JAMB HAS CORROSION VISIBLE IN FWD AND AFT LOWER CORNER POCKETS OF JAMB AND IN LOWER POCKET OF AFT DOOR FRAME MARKED WITH ARROW. REMOVED CORROSION FROM LWR AND AFT LWER POCKETS AT R1 DOOR JAMB AREA AND LOWER POCKET OF AFT DOOR FRAME. INSTALLED REPLACEMENT WEBS AND FLOOR SUPPORTS IAW SRM 51-11-02, PG 14 AND ER/A 545682-14, REV 0. ASSOCIATED ER/A 54-568214, ADDED FOR AC 9525.

Part: SKIN — CRACKED (BS 1095) · airframe 42,755 hrs · 29,143 cycles

RIGHT FUSELAGE BS 1095 SKIN CRACKED FROM FASTENER HOLE APPROXIMATELY .75" JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE BS 1095 CRACKED SKIN FROM FASTENER HOLE JUST ABOVE LONGERON 14-R IAW ER/A 545684-14, REV. OR. ASSOCIATED ER/A 00-545684 ADDED FOR AC 9525.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 42,755 hrs · 29,143 cycles

CRACK ON LT SIDE OF VERITCAL STABILIZER AT MATING SURFACE OF EMPENNAGE AT BS 116. REPAIRED CRACK ON LT SIDE OF VERTICAL STABILIZER AT MATING SURFACE OF EMPENNAGE BS 1116 IAW SRM 55-30-01, FIG 201, REPAIR 5.

Part: STOP FITTING — CRACKED · airframe 42,755 hrs · 29,143 cycles

BS 1053, VENTRAL DOOR UPPER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED, REPLACED DOOR STOP FITTING IAW SRM 51-41-02, PAR 4.

Part: STOP FITTING — CRACKED (BS 1053) · airframe 42,755 hrs · 29,143 cycles

BS 1053 VENTRAL DOOR LOWER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED. REPLACED DOOR STOP IAW SRM 51-41-02, PAR. 4.

Part: SUPPORT — CRACKED (BS 680) · airframe 42,755 hrs · 29,143 cycles

RIGHT WING, KEEL BEAM, BS 680, CRACKED LONGERON SUPPORT INSIDE BOX. REPLACED CRACKED LONGERON SUPPORT ON RT WING KEEL BEAM BS-680 REPAIR DOUBLER ON FORMER IAW ER/A 545683-14MA-O, STEP 8. WORK COMPLETE ASSOCIATED ER/A 00-545683 ADDED FOR AC 9525.

Part: STIFFENER — CRACKED (BS 1200) · airframe 42,755 hrs · 29,143 cycles

AFT ACCY CANTED FRAME BS 1200 INSIDE LT VENT BOX, VERTICAL STIFFENER CRACKED. REPLACED IAW DWG ORNRC 67775-0300-0036. FABRICATED NEW VERTICAL STIFFENER, INSTALLED IAW SRM 51-41-02, PARA 4.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 42,755 hrs · 29,143 cycles

VERTICAL STAB L/E FWD OF RAM AIR SCOOP COMMON TO PANEL 370AL LOWER LT SIDE SKIN IS CRACKED AND UPPER AREA IS HEAVILY ERODED. REPLACED DOUBLER, PN 5910242-121, SKIN, ON VERT SLAB DORSAL FIN FWD OF RAM AIR SCOOP COMMON TO PANEL 370 AL IAW SRM 51-41-02, PG 1 PARA 4 AND 51-41-05, PARA 8, PG 17.

Part: CUSP WEB — CORRODED (BS 148-331) · corrosion level 2 · airframe 42,755 hrs · 29,143 cycles

CORRODED CRACKS, AND MISSING FASTENERS AT FLOOR SUPPORT ON LT CUSP WEB BETWEEN BS 148-331. REPLACED CORRODED FLOOR SUPPORT AND SUB FLOOR IAW SRM 51-41-02. INSTALLED MISSING FASTNERS IAW SRM 51-41-02. REPAIRED LT CRACKED CUSP WEB IAW SRM 53-00-55, REPAIR 4.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 42,755 hrs · 29,143 cycles

AT THE LEFT HORIZONTAL STABILIZER AFT SPAR, BOTH ELEVATOR CONTROL TAB FITTING CLOSEOUTS ARE CRACKED, MARKED CA016 AND CA017. REPLACED LT OTBD AND INBD ELEVATOR CONTROL TAB FITTING CLOSEOUTS IAW SRM 51-45-05, PARA 10.

Part: SUPPORT — CRACKED (BS 674) · airframe 42,755 hrs · 29,143 cycles

LOWER FUSELAGE UNDER WING KEEL BEAM LT BS 674 CRACKED KEEL BEAM SUPPORT. REPAIRED KEEL BEAM SUPPORT IAW ER/A 545683-14MA.

Part: STIFFENER — DAMAGED (HORIZONTAL STAB) · airframe 42,755 hrs · 29,143 cycles

LEFT HORIZONTAL STABILIZER AFT SPAR STIFFENERS DAMAGED, TWO DENTED AND ONE TORN CORNER, REMOVED THE STIFFENERS IAW SRM 51-40-08.

Part: STRINGER — CRACKED · airframe 42,755 hrs · 29,143 cycles

WHILE REMOVING THE RUDDER ACTUATOR FOUND STR FOR RUDDER BRACE AT OTBD END CRACKED. ALSO 3 MOUNTING SCREWS LOOSE AND 1 MISSING FOR BRACE. REPLACED INTERCOASTAL AND SCREWS IAW SRM 51-41-02.

Part: ATTACH ANGLE — CRACKED (BS 1022) · airframe 42,755 hrs · 29,143 cycles

AFT SIDE, BS 1022 AT LONGERON 7R ATTACH ANGLE CRACKED FROM FASTENER INTO RADIOUS. REMOVED DAMAGE ON AFT SIDE, BS 1022 LONGERON 7R ATTACH ANGLE. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 51-70-11, 51-41-02, 51-41-05.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 42,755 hrs · 29,143 cycles

AFT CARGO DOOR AND SEAL RETAINER DAMAGED ON LOWER/ AFT CORNER, 2 AREAS, MARKED. REPAIRED DAMAGE TO AFT LOWER CARGO DOOR AFT LOWER CORNER BY BLENDING OUT DAMAGE AND INSTALLING DOUBLER IAW B717 SRM 52-30-02 REPAIR 8 FIG 201. REMOVED AND REPLACED AFT LOWER CORNER SEAL RETAINER WITH NEW SEAL RETAINER.

Part: INTERCOSTAL — CRACKED (BS 636) · airframe 42,755 hrs · 29,143 cycles

INTERCOSTAL CRACKED ON FWD SIDE OF BS 636, FLOORBEAM BL0. REPAIRED CRACK IN INTERCOSTAL IAW SRM 53-00-00, REPAIR 1, FIG 201 AND SRM 51-41-05, PARA 10.

Part: STIFFENER — CRACKED (BS 737) · airframe 39,719 hrs · 26,807 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN BS 737, LBL 44 VERTICAL STIFFENER CRACKED. INSTALLED A NEW STIFFENER IAW SRM 51-41-02 AND SRM 51-41-05.

Part: STIFFENER — CRACKED (BS 737) · airframe 39,719 hrs · 26,807 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN BS 737, RBL 44 VERTICAL STIFFENER CRACKED. REPLACED THE STIFFENER IAW DWG 9923417 AND SRM 51-41-02, 51-41-03, 51-40-08, 51-40-03, AND 51-41-05.

Part: LIGHT — DIRTY (CABIN) · airframe 37,813 hrs · 25,240 cycles

LEFT EMERGENCY EXITS LIGHT DIRTY. CLEANED LIGHT IAW AMM.

Part: LATCH — MISSING (DOOR) · airframe 37,813 hrs · 25,240 cycles

TAIL COMPARTMENT DOOR LOWER LATCH FOR SLIDE ARMING PANEL MISSING. INSTALLED LATCH IAW SRM & AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 37,813 hrs · 25,240 cycles

L1 DOOR EMERGENCY LIGHT BULB LOOSE. SECURED BULB IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 37,813 hrs · 25,240 cycles

TAIL COMPARTMENT OVERHEAD EMERGENCY EXIT LIGHT WIRING LOOSE. SECURED LIGHT IAW SWPM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

CUSP WEB CRACKED BETWEEN BS 508 TO BS 513, RBL 55. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT — CRACKED (RT AILERON) · airframe 37,313 hrs · 24,915 cycles

RIGHT WING AILERON MOST OTBD HINGE SUPPORTS CRACKED. R & R SUPPORTS IAW SRM & DWG.

Part: SUPPORT — CRACKED (LT AILERON) · airframe 37,313 hrs · 24,915 cycles

LEFT WING AILERON MOST OTBD HINGE SUPPORTS CRACKED. R & R SUPPORTS IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 900 LT SIDE. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BL 0. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO BS 200, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 10 TO RBL 41. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 190, LBL 50. R & R FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO RBL 42. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

MAIN CABIN LT SIDE LAVATORY FLOOR SUPPORT CORRODED BETWEEN BS 100 TO BS 1053. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

FLOOR SUPPORT CORRODED AT BS 200, LBL 30. REPAIRED SUPPORT IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

AFT CARGO PIT ON AFT CLOSE OUT WEB C2 DOOR CUT OUT CORRODED BETWEEN BS 292 TO BS 1002, BETWEEN STRINGER 26L TO STRINGER 25L. R & R WEB IAW SRM & DWG.

Part: DOUBLER — CRACKED (LT WING) · airframe 37,313 hrs · 24,915 cycles

LEFT WING FIXED LE OTBD SIDE OF SLAT TRACK NR 6 STATION XRS 267 DOUBLER CRACKED. R & R DOUBLER IAW SRM & DWG.

Part: ANGLE — CORRODED (LT WING) · airframe 37,313 hrs · 24,915 cycles

LEFT WING FIXED LE BETWEEN SLAT TRACK NR 3 & NR 4 STATION XRS 164 INTERNAL ANGLE CORRODED. R & R ANGLE IAW SRM & DWG.

Part: DOUBLER — CORRODED (LT WING) · airframe 37,313 hrs · 24,915 cycles

LEFT WING FIXED LE BETWEEN SLAT TRACK NR 3 & NR 4 STATION XRS 164, INTERNAL DOUBLER CORRODED. R & R DOUBLER IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 37,313 hrs · 24,915 cycles

LEFT WING TO BODY INBD SIDE OF INBD FLAP CARRIAGE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 37,313 hrs · 24,915 cycles

RIGHT WING FLAP CTR HINGE AFT FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: STIFFENER — CRACKED (LT SPOILER) · airframe 37,313 hrs · 24,915 cycles

LEFT WING OTBD SPOILER INBD END STIFFENER Z ANGLE CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 38,020 hrs · 25,377 cycles

RIGHT WING INBD BUTE DOOR UPPER SURFACE CRACKED OTBD SKIN SIDE APPROXIMATELY STATION 170. REPAIRED SKIN IAW EA.

Part: PAN — CORRODED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

C2 DOOR JAMB PAN CORRODED. REPAIRED JAMB PAN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 37,313 hrs · 24,915 cycles

RIGHT WING INBD BUTE DOOR UPPER SURFACE OTBD SIDE CRACKED. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 37,313 hrs · 24,915 cycles

LEFT WING FLAP CTR HINGE FWD FAIRING ATTACH FUEL PANEL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT MLG DOOR) · airframe 37,313 hrs · 24,915 cycles

LEFT WW DOOR INSIDE PANEL 722 AZ LOWER ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

LEFT WW FWD DOOR CUT OUT INBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 37,313 hrs · 24,915 cycles

RIGHT WW FWD DOOR CUT OUT INBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FAIRING — CRACKED (RT HORIZ STAB) · airframe 36,917 hrs · 24,667 cycles

LOWER RT HORIZONTAL STABILIZER FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: FAIRING — CRACKED (RT HORIZ STAB) · airframe 36,423 hrs · 24,324 cycles

LOWER RT SIDE HORIZONTAL STABILIZER BANANA FAIRING CRACKED. REPAIRED FAIRING IAW TRA.

Part: RETAINING RING — OUT OF POSITION (EVAC SLIDE) · airframe 36,638 hrs · 24,476 cycles

L1 DOOR EMERGENCY EVAC SLIDE RETAINING PIN OUT OF POSITION. R & R SLIDE IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 36,126 hrs · 24,149 cycles

FWD OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED LIGHT ASSEMBLY IAW MM.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 35,352 hrs · 23,678 cycles

INFLIGHT SHUTDOWN/AIR TURNBACK. AFTER TAKEOFF ENGINE VIBE HIGH VIBE LEVEL 1 ALERT FOLLOWED BY INCREASE OF TGT. APPROX 1 MIN LATER EGT ROSE TO 1149 MAX ALONG WITH ENGINE LEFT BEARING OVERHEAT AND LEFT ENGINE AUTO SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: RETAINER — DIRTY (GIRT BAR) · airframe 34,708 hrs · 23,280 cycles

DIFFICULT TO INSERT AND REMOVE SLIDE GIRT BAR AT THE L1 DOOR. CLEANED AND LUBED GIRT BAR RETAINERS AT L1 DOOR, OPS CHECK GOOD.

Part: RECEPTACLE — DIRTY (GIRT BAR) · airframe 344,600 hrs · 23,120 cycles

FWD L1 ENTRY DOOR SLIDE GIRT BAR HARD TO INSERT AND RELEASE. CLEARED DEBRIS FROM GRIT BAR RECEPTACLES ON FLOOR OPERATIONAL CHECKS GOOD PER MM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

CUSP WEB CRACKED AT BS 589, LBL 55. REMOVED AND REPLACED WEB IAW SRM.

Part: SUPPORT — CORRODED (R1 DOOR) · airframe 33,161 hrs · 22,276 cycles

R-1 DOOR GIRT BAR AFT SUPPORT PLATE HAS CORROSION. REMOVED & REPLACED NEW GIRT BAR SUPPORT IAW B717 SRM 51-40-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

CUSP WEB CRACKED AT BS 674, LBL 55. REMOVED ANAD REPLACED CUSP WEB IAW SRM AND AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

CUSP WEB CORRODED BETWEEN BS 488 TO BS 500, RBL 55. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

CUSP WEB CRACKED AT BS 674, RBL 55. REMOVED AND REPLACED WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

CUSP WEB CORRODED BETWEEN BS 508 TO BS 513, RBL 55. REMOVED AND REPLACED WEB IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

RIGHT WHEEL WELL, FWD VERTICAL DOOR CUTOUT ON AC SIDE CRACKED AT RADIOUS. REPAIRED CUTOUT PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 365 TO BS 589, RBL 44. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: STRIP — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

RIGHT WTB LANDING STRIP ON FUSELAGE CORRODED STA 845-898 LONG 26R-30 42-24. REMOVED AND REPLACED RIGHT WTB LANDING STRIP AT STA 845-898 LONG 26R-30 IAW B717 SRM 51-20-05, 51-40-08 & 51-10-04.

Part: SUPPORT — CRACKED (RT WING) · airframe 33,161 hrs · 22,276 cycles

RIGHT WING TO FUSELAGE ANGLE SUPPORT ARM CRACKED. REMOVED ANGLE SUPPORT ARM IAW B717 SRM 51-41-02 AT RIGHT WING FABRICATED NEW PARTS FROM 6061-0-.063" PO 2208633 DIM 9" APPROX IAW B717 DRW PL5919110 AND INSTALLED NEW PART IAW B717 SRM 51-41-05.

Part: SUPPORT — CRACKED (LT WING) · airframe 33,161 hrs · 22,276 cycles

LEFT WING TO FUSELAGE ANGLE SUPPORT CRACKED. REMOVED ANGLE SUPPORT ARM IAW B717 SRM 51-41-02 LEFT WING. FABRICATED NEW PART FROM 6061-0-.063" PO 2208633 DIM 4.5" APPROX IAW B717 DRW PL5919110 AND INSTALLED NEW PART IAW B717 SRM 51-41-05.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

LONGERON CORRODED BETWEEN BS 936 TO BS 1012, LONGERON 30. REMOVED AND REPLACED LONGERON IAW SRM.

Part: DOOR — CRACKED (NLG) · airframe 33,161 hrs · 22,276 cycles

RIGHT AFT CUTOUT ON NLG STRUT DOOR HAS CRACK NDT VERIFIED & END OF CRACK MARKED. REPAIRED DOUBLER IAW B717 SRM 53-10-01 R6, 51-10-04, 51-00-07.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 33,161 hrs · 22,276 cycles

FORWARD SERVICE DOOR SLIDE LANYARD ASS'Y FRAYED. REMOVED AND REPLACED FORWARD SERVICE DOOR SLIDE LANYARD ASSY IAW B717 AMM 25-61-03.

Part: PAN — CORRODED (FUSELAGE) · airframe 33,161 hrs · 22,276 cycles

C-1 DOOR PAN LOWER SECTION CORRODED. REMOVED AND REPLACED HAT IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 33,340 hrs · 22,391 cycles

EEPLS COVERS MISSING BETWEEN ROW 1 TO ROW 3. RELAMPED COVER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,340 hrs · 22,391 cycles

EEPLS LIGHTS INOP BETWEEN ROW 1 TO ROW 3. RELAMPED BULBS PER AMM.

Part: FITTING — OBSTRUCTED (GIRT BAR) · airframe 33,118 hrs · 22,248 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTINGS DIFFICULT TO ARM/DISARM. CLEANED DEBRIS FROM FITTINGS PER MM.

Part: FITTING — OBSTRUCTED (GIRT BAR) · airframe 33,118 hrs · 22,248 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTINGS DIFFICULT TO ARM/DISARM. CLEANED DEBRIS FROM FITTINGS PER MM.

Part: SEAL — BROKEN (EVAC SLIDE) · airframe 33,090 hrs · 22,229 cycles

TAIL CONE SLIDE AFT ATTACH CLIP SLIDE LANYARD RETAINER SEAL BROKEN. REMOVED AND REPLACED SEALS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 2D ESCAPE PATH LIGHTING OUT AND COVER OFF. REPLACED LIGHT BULBS AND LENS, OPS CHECK OK REF MM 33-51.

Part: DOUBLER — CRACKED (NR 2 PYLON)

NR 2 ENG AFT PYLON UPPER SURFACE FASTENER ROW DOUBLER REPAIR, CRACKED. ACCOMPLISHED FASTENER ROW DOUBLER REPAIR ANGLE AND STRAP REPAIR PER EA 17-53-03506IR.

Part: DOUBLER — CRACKED (NR 1 PYLON)

NR 1 ENG AFT PYLON UPPER SURFACE FASTENER ROW DOUBLER REPAIR, CRACKED. ACCOMPLISHED FASTENER ROW DOUBLER REPAIR ANGLE AND STRAP REPAIR PER EA 17-53-03506IR.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 200 TO 216, RBL 57, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-05.

Part: FASTENER — SHEARED (FUSELAGE)

AFT ACCESSORY BULKHEAD FRAME CLIP HI-LOKS, SHEARED. ACCOMPLISHED FRAME CLIP HI-LOKS REPLACEMENT PER EA 17-53-03015A.

Part: LONGERON — CRACKED (LT PYLON)

FWD OF YOKE MOUNT, LEFT PYLON APRON LOWER LONGERON, CRACKED. ACCOMPLISHED LONGERON DOUBLER REPAIR PER EA 17-54-02261IR.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD AIRSTAIR HANDLE BASE FLOOR SUPPORT, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON LOWER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON LOWER NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 166, LBL 6, CRACKED. ACCOMPLISHED FLOOR SUPPORT DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: LONGERON — CRACKED (LT PYLON)

FWD OF AFT MOUNT, LEFT PYLON APRON UPPER AND LOWER LONGERON, CRACKED. ACCOMPLISHED LONGERON DOUBLER REPAIR PER EA17-54-02261IR.

Part: PANEL — CORRODED (CABIN)

GALLEY ENTRANCE DOOR JAMB GAP PANEL, STA 160 TO 200, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: WEB — PUNCTURED (FUSELAGE)

CABIN FLOOR WEB, STA 199, RBL 15, PUNCTURED. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: PAN — CRACKED (CARGO DOOR)

FWD CARGO DOOR PAN LOCK AREA, CRACKED. ACCOMPLISHED PAN LOCK AREA DOUBLER REPAIR PER B717 SRM 52-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: CHANNEL — CORRODED (FUSELAGE)

CABIN FLOOR HAT, STA 160 TO 200, BL 0, CORROSION. ACCOMPLISHED FLOOR HAT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 171, RBL 8 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 8 TO RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOORBOARD — DAMAGED (CABIN)

TEMP REPAIR DONE TO FWD GALLEY FLOOR DUE TO SPONGY FLOORBOARD REF EA 17-25-00724IR. (RESOLVED ON W/O: 163526 TASKCARD: N/R-00003 ) N/R-00003 COMPLIED WITH ON AAR W/O 2000052 NR 5155 AND 5192 PER EA 17-25-00724 SECTION 2. FABRICATED FLOOR PANEL.

Part: FRAME — DAMAGED (FUSELAGE)

REPAIR OF FUSELAGE CANTED FRAME CAP STA 1178.225 ACFT LT SIDE. ACCOMPLISHED T/C 17-5310-2973 REV IR STEPS 3-20 LT SIDE.

Part: FRAME — DAMAGED (FUSELAGE)

REPAIR OF FUSELAGE CANTED FRAME CAP STA 1178.225 ACFT RT SIDE. ACCOMPLISHED T/C 17-5310-2989 REV IR STEPS 3-20 RT SIDE.

Part: PAN — CORRODED (AFT CARGO BAY)

AFT CARGO COMPARTMENT LOWER CARGO DOOR JAMB CORRODED. INSTALLED AFT CARGO DOOR JAMB PAN SPLICE REPAIR PER SRM 53-20-15 P 201.

Part: FRAME — CRACKED (BS 1178)

AFT FUSELAGE COMPARTMENT LT STA 1178 CANTED FRAME CRACKED JUST BELOW L-7.L. CUT OUT DAMAGED SECTION 3.0" BY 1.0" AND INSTALLED FILLER .071" 70-75-T6 PO 021267 AND REPAIR ANGLE DOUBLER .080" 7075-0 PO NR 04721. HEAT TREATED TO T-6 PER B717 SRM 51-32-01 AND INSTALLED IAW B717 SRM 51-70-11.

Part: STRUCTURE — CRACKED (VENT BOX)

RT AFT FUSELAGE COMPARTMENT VENT BOX AFT CORNER CRACKED. STOP DRILLED CRACK PER B717 SRM 51-00-07. FABRICATED AND INSTALLED REPAIR PER TASK CARD 5320-2023.

Part: SEALANT — IMPROPER (WINDSHIELD)

ON CLIMBOUT OF RSW AT 17000. CRACKING NOISE STARTED FROM FO'S WINDSHIELD. WINDSHIELD WAS VIBRATING AS WELL. DIVERTED, OVERWEIGHT LANDING AT 106.2. VISUALLY INSPECTED WINDOW IAW MM. NO CRACKS FOUND. CHECKED TORQUE IAW MM 56-11. TORQUE CHECKED GOOD. PRESSURIZED AC TO 6 PSI DIFF. NO LEAKS FOUND. FOUND AERO DYNAMIC FILLET SEALANT UNCURED AND COMING OUT OF FILLET SLAPPING FUSELAGE ABOVE F/O WINDOW CAUSING VIBRATION. CLEANED AND REMOVED SEAL.

Part: SKIN — DENTED (BS 329 - 342)

ON POST FLIGHT FOUND SMALL DENT ON RIGHT SIDE OF A/C FWD OF FWD CARGO PIT. INSTALLED PERMANENT REPAIR ON RIGHT FUSELAGE AT STA 329 TO 342.5 BETWEEN L-19R TO 21R PER B717 SRM 53-00-01.