N607AT

Part: FUEL SYS — LEAKING (ZONE 500) · airframe 52,580 hrs · 45,204 cycles

FUEL LEAK FOUND DURING INSPECTION OF THE LT WING AFT LOWER SKIN AT XRS=164. REPAIRED PER ERA 629418-14AD (1375656)

Part: STRINGER — CORRODED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

CORROSION ON S-30, BS 936-984. CORRODED LONGERON REPLACED ON NR 450 IAW SRM 53-20-05 (1371383)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,580 hrs · 45,204 cycles

CORROSION AT AFT CARGO KEEL SPLICE STA 974 L28L TO L28R. REPAIRED FRAME SECTION PER B717 SRM 53-20-07-2R-3 AND REPAIRED SKIN FORMER SECTION PER B717 SRM 53-00-06-2R (1370207)

Part: SUPPORT CHANNEL — CORRODED (ZONE 200) · airframe 52,580 hrs · 45,204 cycles

FOUND CORROSION AROUND HOLE FOR VHF ANTENNA AT BS 916, LONGERON 3. REPLACED ANTENNA SUPPORT CHANNEL REF BAC DWG 5936434. (1367333)

Part: DOUBLER — DAMAGED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

AFT CARGO DOOR AND FRAME: DOOR CUTOUT DOUBLER AT AFT FRAME DAMAGED. REPLACED REPAIR AT AFT CARGO DOOR JAMB EDGE IAW SRM 53 -20-15-2R (1363827)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,580 hrs · 45,204 cycles

FOUND CORROSION ON SKIN CLIP AT FRAME 927 BETWEEN STRINGER 29L AND 30. REMOVED AND REPLACED DAMAGED FORMER PN 9915524-33 PER BOEING DWG 9915524 (1362226)

Part: DOOR FRAME — GOUGED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

AFT CARGO DOOR AND FRAME: UNIDENTIFIED BLEND OUT AT DOOR FWD FRAME CUTOUT HAS GOUGE AND DAMAGE. REPAIRED PER B717-200 SRM 53-20-15-2R. (1359038).

Part: PAN — CORRODED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

SHIP 9569 AFT CARGO DOOR AND FRAME: CORROSION AT DOOR PAN AREA AROUND FASTENERS. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-20- 15-2R (1355626)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,580 hrs · 45,204 cycles

CORROSION ON STRINGER 30 STA 997. REMOVED AND REPLACED DISCREPENT LONGERON 30 IAW SRM 53-20-05 (1354315)

Part: LONGERON — CORRODED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

AFT CARGO LONGERON 30 AT APROX STATION 1005 AND FWD CORRODED. REPAIRED ON NR 450 IAW SRM 53-20-05-2R PRO. 1, & BAC DWG 5919707. (1354309)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,580 hrs · 45,204 cycles

FOUND CORROSION ON LONGERON 30, BS 900 TO 936. REMOVED AND REPLACED DISCREPENT LONGERON 30 FROM IAW SRM 53-20-05 (1354312)

Part: PAN — CORRODED (ZONE 100) · airframe 52,580 hrs · 45,204 cycles

AFT CARGO BS 1022 - 1053, CORROSION AT LAV TANK DUMP CHUTE AT LAV PAN. REMOVED CORROSION FROM PAN IAW SRM 51-40-02 (1333475)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 52,518 hrs · 45,137 cycles

CEILING EMERGENCY LIGHTS INOP BETWEEN ROWS 24 TO 29. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY AT B5-231 PER B717 AMM 33-51. CHECKS GOOD. (7957044)

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 52,457 hrs · 45,090 cycles

FUEL LEAK FOUND DURING INSPECTION OF THE LT WING AFT LOWER SKIN DOUBLER XRS=164. : COMPLIED WITH PRI 629418-14AD (1268439).

Part: FUEL CELL — LEAKING (ZONE 600) · airframe 52,457 hrs · 45,090 cycles

FUEL LEAK FOUND DURING INSPECTION OF RT WING AFT LOWER SKIN XRS=164. RT WING AFT LOWER SKIN DOUBLER XRS=164, & RT WING REAR SPAR LOWER CAP. COMPLIED WITH PRI 629419-14AD (1268436).

Part: RIB — DAMAGED (ZONE 000) · airframe 52,417 hrs · 45,051 cycles

HOUR GLASS PANEL LOWER WING RIB, UPPER ROW, FWD FASTENER HOLE DAMAGED. REPAIRED PER PRI 630032-14 REV. 0, 1 AND 2 AND ER/A 630032-14 REV ORIGINAL. (1267567)

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 52,297 hrs · 44,937 cycles

ATB TO ORD DUE TO LT ENGINE COMPRESSOR STALL. REPLACED LEFT ENGINE. (7851686)

Part: HYDRAULIC LINE — LEAKING (ZONE 700) · airframe 52,154 hrs · 44,823 cycles

RETURNED TO ATL DUE TO A RIGHT SYSTEM HYDRAULIC FLUID AND PRESSURE LOSS REQUIRING A MANUAL GEAR EXTENSION. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR BUNGEE CYLINDER LINE AND UNION.

Part: SKIN — DAMAGED (ZONE 200) · airframe 51,723 hrs · 44,432 cycles

SHIP 9569 FUSELAGE SCRAPE AND GOUGE JUST BELOW L1 DOOR AREA. CORRECTIVE ACTION: REPAIRED PER ERA 6264451-14. (0967283)

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 51,278 hrs · 44,038 cycles

THE AFT EMERGENCY EXIT LIGHT IS FLICKERING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 1050. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #7236550)

Part: RELAY — FAILED (ANTI-SKID SYS) · airframe 49,591 hrs · 42,537 cycles

SHIP 9569 -MISC/DE- THE "ANTI-SKID FAIL" ALERT POSTED WHEN THE LANDING GEAR WAS SELECTED DOWN. A GO-AROUND WAS PERFORMED. DUE TO WET RUNWAYS, THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFETY WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED RELAY R2-5037 AND THE BCU PER B717 AMM 32-45 REF WDM 32-45-00. PERFORMED SUCCESSFUL ANTI-SKID RTS TESTS. NO FAULTS. BEFORE THE BCU CHANGE THERE WERE NO LAST LEG FAULTS. LEG 2 "ANTI-SKID POWER 2" FAULTS. (LP #5892380)

Part: SEAL — CUT (MAIN DOOR) · airframe 49,287 hrs · 42,290 cycles

SHIP 9569 -ATB- CABIN CREW STATED THAT THERE WAS A SLOW DEPRESSURIZATION OCCURRING DURING THE CLIMB OUT AFTER TAKEOFF. THE LEAD F/A PASSED OUT (REGAINED CONSCIOUSNESS LATER) AND ANOTHER FELT LIGHTHEADED. THE OXYGEN MASKS AT ROW 24DEF DID AUTOMATICALLY DEPLOY BUT WERE NOT ACTIVATED BY PASSENGERS. NEITHER F/A WERE ABLE TO CONTINUE THEIR DUTIES SO THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: MAINTENANCE FOUND A CUT IN THE DOOR SEAL LOWER CORNER ON THE 1L DOOR. THE DAMAGED SEAL WAS REPAIRED PER B717 SRM 52-10-17-2R PROC 1. (LP #0317194)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,937 hrs · 41,998 cycles

FOUND DAMAGE TO FWD SIDE OF AFT CARGO DOOR CUTOUT SKIN. ACCOMPLISHED REPAIR PER B717 SRM 53-20-15-2R PROCEDURE 10, PARA 4E. .187 MATERIAL REMOVED. NO REPETITIVE OR PERMANENT REPAIR REQUIRED. REPAIR ID INSTALLED. (LP #5828020)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,840 hrs · 41,916 cycles

THE FWD OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5424766)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,048 hrs · 41,272 cycles

EXFOLIATION CORROSION ON FRAME CLIP STA Y=655 LONGERON 29R AND 29L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00213: CORROSION LEVEL 2. FRAME CLIP ON STA Y=655 LONGERON 29R AND 29L AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #0001174)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION WAS FOUND ON PRODUCCION DOUBLER ON CHANNEL AFT CARGO COMPARTMENT AT STA Y=974 TO STA Y=994. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORROSION ON PRODUCCION DOUBLER STA Y=974 TO STA Y=994 WAS REPAIRED PER ERA 611975-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 611975-14 REV 3. ACCOMPLISH SECTION II REPETITIVE INSPECTION WITHIN 8000 FLIGHT CYCLES (8000 FROM 41,269 TOTAL AIRCRAFT CYCLES AS OF 3OCT23) AND REPEAT WITHIN EVERY 8000 FLIGHT CYCLES THEREAFTER. ASSOCIATED ER/A 14-611975 ADDED FOR AC 9569. (LP #2999891)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACK ON INTERNAL STRUCTURE LOWER (PAN) AT FWD CARGO DOOR. SUMMARY OF NRC 00194: INTERNAL STRUCTURE LOWER (PAN) AT FWD CARGO DOOR WAS REPAIRED PER PRI 611939-14 REV 1 & ER/A 611939-14 REV ORIG. SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-611939 ADDED FOR AC 9569. (LP #0000040)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

WEAR ON DOOR EXTERNAL SKIN FWD LOWER EDGE AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00145: EXTERNAL SKIN ON FWD LOWER EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 611900-14 REV ORIGINAL SECTION I. PERMANENT REPAIR AND PRI 611900-14 REV 3. ASSOCIATED ER/A 14-611900 ADDED FOR AC 9569. (LP #2998342)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACK ON LONGER 17LH AND STA 1022 AT PAX CABIN IN REF NRC 00588. SUMMARY OF NRC 00603: LONGER 17LH AND STA 1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 PAR 5 A FIG 201 (SHEET 1). (LP #2996649)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACK ON INTERNAL STRUCTURE (WEB) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: AREA INTERNAL STRUCTURE (WEB) AT FWD CARGO DOOR WAS REPAIRED PER ER/A 611845-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 611845-14 REV 0. ASSOCIATED ER/A 14-611845 ADDED FOR AC 9569. (LP #2995474)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON EXTERNAL SKIN BTW STA Y=1037 TO Y=1022, L-29R TO L-28R AT LOWER FUSELAGE. SUMMARY OF NRC 00085: CORROSION LEVEL 2. EXTERNAL SKIN BTW STA Y=1037 TO Y=1022, L-29R TO L-28R AT LOWER FUSELAGE WAS REPAIRED PER ERA 612001-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612001-14 REV. 0. (LP #2984358)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00148: CORROSION LEVEL 2. PAN JAMB LOWER WAS REPLACED PER B-717-200 SRM 53-20-15 PROCEDURE 7 REPAIR 7, 51-41-02-0G PAR 4 B, AND 51-41-05-0G PAR 8. (LP #2984182)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON LONGERON 30 BTW STA 909 TO STA 912, STA 921 TO STA 922, STA 962 TO STA 968, STA 998 TO STA 1000, LONGERON 29L STA 910 TO STA 912, STA 940 TO STA 950, STA 952 TO STA 955, AND LONGERON 29R STA 924 TO STA 928, STA 1005 TO STA 1006 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00202: CORROSION LEVEL 2. LONGERON 30 AND LONGERON 29 LH WERE REPLACED PER B717-200 SRM 51-41-02-0G PAR 4 B AND 51-41-05-0G. (LP #2982579 )

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

SCRATCHES ON DOUBLER OF AFT CARGO DOOR CUTOUT (AFT EDGE) BTW LONG PROJECT 24R AND LONG PROJECT 26R AT AFT FUSELAGE. SUMMARY OF NRC 00147: DOUBLER REPAIR OF AFT CARGO DOOR CUTOUT (AFT EDGE) BTW LONG PROJECT 24RH AND LONG PROJECT 26RH WAS REPLACED PER B717-200 SRM 53-20-15-2R PROC 10 REP 10. (LP #2976729)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON LH TIE TRACK BTW STA 813 TO STA 1022 BTW L-28L TO L-27L OF AFT CARGO. SUMMARY OF NRC 00412: CORROSION LEVEL 2. TIE TRACK BTW STA 813 TO STA 1022 BTW L-28L TO L-27L OF AFT CARGO WAS FABRICATED AND REPLACED PER DWG 5936663 AND B717 SRM 51-41-01-0G. (LP #2975853)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON FILLET FAIRING FORMER LH SIDE STA Y=832. SUMMARY OF NRC 00603: CORROSION LEVEL 2. FILLET FAIRING FORMER LH SIDE STA Y=832 WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4. (LP #2969510)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00555: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2965323)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON SUPPORT SETTLEMENT (ELECTRIC CONECTORS) STA Y=746 BTW L-20 AT LH MLG WHEEL WELL (FYT). SUMMARY OF NRC 00166: CORROSION LEVEL 2. SUPPORT WAS FABRICATED AND REPLACED PER DWG 7971426 AND B-717-200 SRM 51-41-01-0G PAR 6. (LP #2963170)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON FLOOR SUPPORT STA Y=370, Y=427, Y=465, Y=636 BTW LONGERON 28L AND 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=370, Y=427, Y=465, Y=636 BTW LONGERON 28L AND 28R AT FWD CARGO COMPARTMENT WERE FABRICATED PER DWG 5936597 REV AC, REV AE AND REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND 51-41-02-0G PAR 4. (LP #2962853)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

AD. CRACK OF 2.900IN LENGTH APPROX AROUND UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH IN REF CARD 5310-01436-04B JOB #154-0002. STEP 7. SUMMARY OF NRC 00287: OVERWING FRAME STA 674 LH SIDE WAS REPLACED PER A.A. AMDS 5310-01436-03A. ASSOCIATED AA 5310-01436 ADDED FOR AC 9569. (LP #2963108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON LONGERON 27LH BTW STA Y=813-832 AT UNDER OF FILLET FAIRING AREA. SUMMARY OF NRC 00304: CORROSION LEVEL 2. SECTION OF LONGERON 27LH BTW STA Y=813-832 WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8. (LP #2960017)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00142: CORROSION LEVEL 2. DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R WAS REPAIRED PER B717-200 SRM 53-20-15-2R REPAIR 6. (LP #2959873)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACK OF 0.100 IN AT UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=696.00 RH (REF CARD 5310-01436-04D). SUMMARY OF NRC 00326: OVERWING SECTION FRAME STA Y=696 RH WAS REPLACED PER CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9569. (LP #2954617)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

CRACK OF 0.720IN LENGTH APPROX ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 LH IN REF CARD 5310-01436-04B JOB #154-0002 STEP 10. SUMMARY OF NRC 00288: OVERWING FRAME AT STA Y=696.000 LH WAS REPLACED PER AMDS 5310-01436-03A ASSOCIATED AA 5310-01436 ADDED FOR AC 9569. (LP #2954914)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

SEVERAL CRACKS ON CUSP WEP BTW STA Y=655 TO STA Y=696, X=44 TO X=60 AT LH CABIN PAX. SUMMARY OF NRC 00324: CUSP WEB STA Y=655 TO Y=715 X=44 TO X=60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 226 AND DWG 9910151 REV "CH". (LP #2951562)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,043 hrs · 41,269 cycles

ELONGATED SEVERAL HOLES ON RH CUSP WEB STA 674, 693-696, AND 715 AT PAX CABIN. SUMMARY OF NRC 00342: CUSP WEB STA Y=655 TO Y=715, X=-44 TO X=-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 226 AND DWG 9910151 REV "CH". (LP #2948161)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION OUT OF LIMITS AT CUSP WEB RH STA 451-452, STA 458-459, AND STA 864-866 WAS FOUND. CABIN PAX. SUMMARY OF NRC 00515: CORROSION LEVEL 2. CUSP WEB RH STA 451-452, STA 458-459, AND STA 864-866 WERE REPAIRED PER B717-200 SRM 53-00-55-2R. (LP #2944575)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION ON FLOOR SUPPORTS (2 EA) FROM STA=1022 TO STA=1053 & X=20 ALSO X=-20 CABIN PAX W2. SUMMARY OF NRC 00317: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) FROM STA=1022 TO STA=1053 & X=20 ALSO X=-20 CABIN PAX W2 WERE REPLACED PER DWG 9936656 REV AM AND PER B-717-200 SRM 51-41-01-0G. (LP #2941264)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 48,043 hrs · 41,269 cycles

CORROSION OUT OF LIMITS AT CUSP WEB STA X=60 BTW STA Y=375 TO STA Y=380 AND STA Y=797 TO STA Y=802 LH SIDE PAX CABIN IN REFERENCE NRC 0323. SUMMARY OF NRC 00439: CORROSION LEVEL 2. WEB STA X=60 BTW STA Y=375 TO STA Y=380 AND STA Y=797 TO STA Y=802 LH WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIG. 203 AND FIG. 207. (LP #2937062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,305 hrs · 40,608 cycles

SHIP 9569 -GEAR/DE- THE CREW NOTED THE "GEAR DOOR OPEN" MESSAGE AFTER THE LANDING GEAR WAS EXTENDED ON APPROACH INTO CLT. THEY UTILIZED THE ALTERNATE GEAR EXTENSION METHOD AND DECLARED AN EMERGENCY WITH ATC. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDING GEAR DOORS REMAINING IN THE DOWN POSITION AND TOUCHING UPON LANDING. THE AIRCRAFT WAS TOWED TO THE GATE. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR DOOR ACTUATING CYLINDER WAS BYPASSING INTERNALLY. THE CYLINDER WAS REPLACED AND RIGGED. ALSO, THE GEAR DOOR BUMPERS WERE REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #9514404)

Part: LIGHT — INOPERATIVE · airframe 45,160 hrs · 38,693 cycles

THE TAIL COMPARTMENT EMERGENCY LIGHTS, THE TAILCONE SLIDE LIGHTS, AND THE AFT CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-116 PER B717 AMM 33- 51. (LP #8544127)

Part: NONE — NONE · airframe 44,636 hrs · 38,241 cycles

THE EMERGENCY EXIT EVACUATION LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EXIT EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8125023)

Part: COVER — MISSING · airframe 44,416 hrs · 38,055 cycles

(LOG 8380514) DURING INSPECTION FOUND CEILING LIGHT COVER OVER ROW 1DEF MISSING. REPLACED LIGHT COVER PER B717 AMM 33-51.

Part: NONE — NONE · airframe 44,224 hrs · 37,876 cycles

THE EMERGENCY CEILING LIGHT AT ROW 15-19 IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY AT LOCATION B5-120 & B5-121 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8084079)

Part: NONE — NONE · airframe 44,046 hrs · 37,714 cycles

THE AFT STAIRWAY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY REF B717 AMM 33- 51. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #8022371)

Part: FLOOR SUPPORT — CORRODED (BS 148) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON FLOOR SUPPORT LOCATED 36RBL AT STA 148. SUMMARY SEE NRC 147-0023:5310-2005/024 00331: REPLACED FLOOR SUPPORT PER DOUGLAS DWG #9936534. (LP #1892060)

Part: FLOOR SUPPORT — CORRODED (BS 180) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION FLOOR SUPPORT LOCATED 36RBL AT STA 180. SUMMARY SEE NRC 147-0023:5310-2005/029 00336: REPLACED FLOOR SUPPORT PER DOUGLAS DWG #9923667. (LP #1892099)

Part: SEAT TRACK — CORRODED (BS 200) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SEAT TRACK 22RBL AT STA 200. SUMMARY SEE NRC 147-0023:5310-2005/035 00354: REPLACED SEAT TRACK PER DWG #5930547. (LP #1892185)

Part: STRUCTURE — CORRODED (BS 150) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SUB FLOOR LOCATED 48RBL AT STA 150. SUMMARY SEE NRC 147-0023:5310-2005/022 00329: REPAIRED PER B717 SRM 51-70-10-2R. (LP #1892059)

Part: STRUCTURE — CORRODED (BS 150) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SUB FLOOR LOCATED 60RBL AT STA 150. REPAIRED PER B717 SRM 51-70-10-2R. (LP #1892177)

Part: DOOR FRAME — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

L-1 DOOR FRAME AREA HAS CORROSION ON SHORT AFT FLOOR SUPPORT (MKD). SUMMARY SEE NRC 147-0023:5310-2005/010 00262: REPLACED FLOOR SUPPORT REF BAC DWG #9936534. (LP #1892098)

Part: STRUCTURE — CORRODED (BS 163) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SUB FLOOR LOCATED 48RBL AT STA 163. REPAIRED PER B717 SRM 51-70-10-2R. (LP #1892175)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,597 hrs · 37,294 cycles

CRACK INDICATION FOUND LEFT SIDE OF VERTICAL, FIFTH HOLE DOWN FROM SPLICE (MARKED). CRACK COMMON TO SKIN OVERSIZED AND BUSHED AS PER PRI 592770-14AD REV. O AND 1. FINAL ERA 592770-14AD REV. O MATCHES PRI 5922770-14AD REV. O AND 1. (LP #1892249)

Part: STRUCTURE — CORRODED (BS 160) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SUB FLOOR LOCATED 49RBL AT STA 160. SUMMARY SEE NRC 147-0023:5310-2005/027 00334: REPAIRED PER B717 SRM 51-70-10-2R. (LP #1892067)

Part: DOOR FRAME — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

L-1 DOOR FRAME AREA HAS CORROSION ON SHORT AFT FLOOR SUPPORT. REPLACED FLOOR SUPPORT REF BAC DWG #9936534. (LP #1891886)

Part: STRUCTURE — CORRODED (BS 200-218) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON SUBFLOOR STA 200 TO 218 RBL 48. SUMMARY SEE NRC 147-0023:5310-2005/037 00404: REPLACED SUB FLOOR PER DOUGLAS DWG #9936534. (LP #1892168)

Part: DOOR FRAME — CORRODED (BS 200) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

CORROSION ON AFT SIDE OF R1 DOOR JAMB AT STA 200 AT FLOOR LEVEL (MARKED WITH TAPE). SUMMARY SEE NRC 147-0023:5310-2005/004 00251: REPLACE CUSP ANGLE PER ER/A 592855-14 REV ORIGINAL. INSTALL FRAME FEET PER BOEING LONGBEACH DRAWING #9911520. ASSOCIATED ER/A 00-592855 ADDED FOR AC 9569. (LP #1891010)

Part: PAN — CORRODED (AFT CARGO) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

AFT CARGO DOOR PAN IS CORRODED IN NUMEROUS LOCATIONS. MARKED IN RED. SUMMARY SEE NRC 001-0372:5231-2002/001 00026: REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #1886649)

Part: DOUBLER — CORRODED (AFT PRESS BLKHD) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

AFT PRESSURE BULKHEAD TRIANGULAR SUPPORT DOUBLER CORRODED AFT OF STA 1053 A/C CENTERLINE. SUMMARY SEE NRC 147-0022:5310-2014/002 00244: REPLACED DOUBLER PER BOEING DWG #5930760. (LP #1887873 )

Part: LONGERON — CORRODED (BS 950-972 L30) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

AFT CARGO BILGE AREA: LONGERON 30 CORRODED FROM STA 950 TO STA 972. "MARKED". SUMMARY SEE NRC 163-0008:5331-2001/002 00228: REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1884015)

Part: SKIN — GOUGED (AFT CARGO) · airframe 43,597 hrs · 37,294 cycles

AFT CARGO DOOR CUTOUT: SKIN HEAVILY GOUGED JUST ABOVE AFT SIDE OF SCUFF PLATE. MARKED. SUMMARY SEE NRC 001-0371:5230-2002/008 00043: REPAIRED PER B717 SRM 53-20-15-2R REPAIR 12. (LP #1879543)

Part: SEAL DEPRESSOR — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

FOUND SEAL DEPRESSOR SPLICE PLATES CORRODED (MKD). SUMMARY SEE NRC 001-0214:5300-1001/001 00362: REPLACED SEAL DEPRESSOR SPLICE PLATES REF B-717 SRM 53-20-15-2R PROCEDURE 4. (LP #1877517)

Part: STRINGER — CORRODED (BS 930-935 S30) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

AFT CARGO BILGE AREA SHOWS EVIDENCE OF CORROSION ON STR 30 AT APROX STATION 930-935. SUMMARY SEE NRC 163-0008:5331-2001/005 00290: REMOVED AND REPLACED PER B717 SRM 51-40-02. (LP #1875177)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 43,597 hrs · 37,294 cycles

L-1 DOOR FRAME AREA HAS CORROSION ON O/B FLOOR SUPPORT (MKD). SUMMARY SEE NRC 147-0023:5310-2005/008 00260: REPLACED FLOOR SUPPORT, REF BAC DWG 9936534. (LP #1872600)

Part: BLADE — BROKEN (WINDSHIELD WIPER) · airframe 41,857 hrs · 35,892 cycles

CAPTAIN WINDSHIELD WIPER BLADE BROKE OFF IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE FROM DEPARTED WIPER ARM. NO DAMAGE FOUND. INSTALLED NEW WIPER ARM AND BLADE ASSY IAW B717 AMM 30-43-03/04. OPERATIONAL TEST WAS GOOD. (LP #6393514)

Part: LONGERON — UNKNOWN (BS 668) · airframe 39,200 hrs · 33,968 cycles

CUT LONGERON 11RT AT APPROX. STA 668 FOR FRAME REMOVAL. NRC 149-0002:5310-01436-03B/001 00144. REPAIRED REF ER/A 530437-14MA REV O. (LP #0831001)

Part: WINDOW — CRACKED (OVERWING EXIT) · airframe 37,994 hrs · 33,170 cycles

LEFT AFT OVERWING EXIT DOOR HAS CRACKED WINDOW. REPLACED WINDOW IN LEFT AFT OVERWING EXIT DOOR PER AMM 56-20.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,847 hrs · 33,050 cycles

THE OVERHEAD EMERGENCY LIGHT LENS AT ROW 17ABC WAS MISSING. MAINTENANCE REPLACED THE LENS. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,135 hrs · 32,567 cycles

DURING WALK AROUND, PILOT FOUND THE EMERGENCY LIGHTS L2-793 AND L2-794 TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-121 BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD AND THE AIRCRAFT WAS OK FOR SERVICE.

Part: DIAL — WORN (TE FLAP) · airframe 35,048 hrs · 31,128 cycles

THE FLIGHT CREW SAFELY ABORTED THE TAKEOFF AT 125 KNOTS DUE TO THE A FLAP CONFIGURATION WARNING ILLUMINATING. MAINTENANCE SUSPECTS THE 4 DIAL-A-FLAP DETENT IS WORN AND THAT ALLOWED THE WARNING MESSAGE TO ILLUMINATE. ALL FOUR MAIN LANDING GEAR TIRES AND BRAKE ASSEMBLIES HAVE BEEN REPLACED.

Part: CARGO TRACK — CORRODED (BS 900-1022) · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

AFT CQRGO COMPARTMENT, CORROSION CARGO TRACK BS 900 TO 1022. THE CARGO TRACK WAS REPAIRED IAW SRM 53-20-52 FIG 201 REPAIR 4. REF. NRC #537.

Part: ANGLE — CRACKED (BS 1144) · airframe 34,221 hrs · 30,544 cycles

AFT ACCESSORY COMPARTMENT HAS A CRACKED FRAME ANGLE AT BS 1144 BETWEEN LONGERONS 2 AND 3R. REPLACED PER ETI-17-16-182 REV 2 AND ER/A 552860-14 REV. ORIG.

Part: CARGO TRACK — CORRODED (BS 370-427) · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

CORROSION ON LT CARGO TRACK FROM BS 370-427. THE CARGO TRACK WAS REPAIRED IAW SRM 53-20-52 FIG 201 REPAIR 4.

Part: STRUCTURE — DAMAGED (WING) · airframe 34,221 hrs · 30,544 cycles

ELONGATED HOLES ON CUTOUTS OF ACCESS PANEL. ACCESS PANEL LANDING WAS REPAIRED IAW ETI 17-16-179 REV3 AND ER/A 552854-14 REV. ORIG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED BEAM NR 4 FWD END AT FWD SERVICE DOOR. BEAM NR 4 WAS REPLACED BUT WAS REPAIRED BEFORE OF HOLES MISALIGNED PER SRM 51-41-02, 51-41-05, ETI-17-16-181 REV 2, AND ER/A 552859-14 REV ORIG.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

CORROSION ON FUEL ACCESS PANEL 620CT SETTLEMENT AREA AND COUNTERSINK. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 STEP 5 C(1) CONDITION III.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACK ON UPPER FWD CORNER SKIN PAN AT PASSENGER DOOR L1. REPAIRED IAW ER/A 552841-14 REV: ORIGINAL AND ETI-17-16-174 REV.

Part: SKIN — BENT (RUDDER) · airframe 34,221 hrs · 30,544 cycles

BENT RUDDER LT SKIN LOWER & MID SECTION. THE RUDDER SKIN WAS REPAIRED IAW ETI- 17-16-176 REV 2 AND ER/A 552853-14 REV ORIGINAL.

Part: FRAME — CRACKED (BS 674) · airframe 34,221 hrs · 30,544 cycles

CRACKED FRAME BS 674. REPAIRED IAW SRM 51-70-11 REPAIR 1.

Part: FLOOR PANEL — CRACKED · airframe 34,221 hrs · 30,544 cycles

CRACKED FLOOR PANEL 222AJF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50 REPAIR 5.

Part: FLOOR SUPPORT — CRACKED · airframe 34,221 hrs · 30,544 cycles

CRACK ON FLOOR SUPPORT. REPAIRED IAW SRM 53-20-50 REPAIR 5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED FITTINGS (4EA) ON AFT VENTRAL DOOR JAMB STA Y=1076. FITTINGS WERE REMOVED (4EA). NEW FITTINGS DRILLED, TREATED, PAINTED, AND INSTALLED PER SRM 51-41-01, 51-41-02, 51-10-04, PAR 15 & 24, AND 51-40-08.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED FRAME AT STA Y=1133 AND LONGERON 2R IN THE AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED PER SRM 51-41-02 AND DRAWING 5913595 REV AP.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 34,221 hrs · 30,544 cycles

DELAMINATED FLOOR PANEL 222JF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.

Part: PAN — CRACKED (CARGO DOOR) · airframe 34,221 hrs · 30,544 cycles

CRACKED FWD CARGO DOOR PAN BETWEEN STOP FITTINGS 1 & 2. HFEC INSPECTION WAS ACCOMPLISHED AND THE CRACKS WERE CONFIRMED IN FWD SECTION OF 1.625", AND AFT SECTION OF 1.5" IAW NDTSPM 06-10-01.001. STOP DRILLED IAW SRM 52-30-02 FIGURE 201 SHEET 3 OF 3, HFEC INSPECTION WAS ACCOMPLISHED , AND NO CRACKS WERE FOUND IAW NDTSPM 06-10-01.001. REPAIRED IAW SRM 52-30-02 REPAIR 4 FIGURE 201.

Part: DOOR FRAME — CRACKED (NLG) · airframe 34,221 hrs · 30,544 cycles

NOSE LANDING GEAR WHEEL WELL DOOR FRAME BEAM CRACKED. THE BEAM WAS REPAIRED IAW SRM 53-10-14 FIGURE 201 REPAIR 2.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 34,221 hrs · 30,544 cycles

CRACKED INTERNAL ANGLE ON LT FWD EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.

Part: DOOR FRAME — CRACKED (NLG) · airframe 34,221 hrs · 30,544 cycles

NOSE LANDING GEAR WHEEL WELL DOOR FRAME BEAM CRACKED . REPAIRED IAW SRM 53-10-14 FIGURE 201 REPAIR 2.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 34,221 hrs · 30,544 cycles

CRACKED FWD CARGO DOOR PAN UPPER EDGE BS 389 - 408. THE DOOR PAN WAS REPAIRED IAW SRM 52-30-02 FIG. 201 REP 1.

Part: SKIN — WORN (TE FLAP VANE) · airframe 34,221 hrs · 30,544 cycles

WEAR ON RT FLAP AFT MOVEABLE VANE UPPER SURFACE OUTBOARD EDGE NEAR TO STA XRS 111. RT MOVEABLE VANE WAS REPAIRED PER SRM 57-53-01 REPAIR 1. PARAGRAPH 4.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED BEAM NR 1 AT AFT END, ALSO BEAM CLIP SAME AREA, AT FWD SERVICE DOOR. BEAM NR 1 AND CLIP AFT EDGE WERE REPLACED PER SRM 51-41-02, 51-41-05.

Part: CUSP WEB — CRACKED (BS 672) · airframe 34,221 hrs · 30,544 cycles

CRACK ON THE LEFT CUSP WEB BS 672 BETWEEN LBL 60 AND 54. THE DAMAGE WAS REMOVED IAW SRM 53-00-55 REPAIR 4, HFEC WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. A REPAIR WAS FABRICATED IAW SRM 53-00-55 REPAIR 4 FIG 215, AND INSTALLED IAW SRM 53-00-55, FIG 215. AND SRM 51-41-02.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 34,221 hrs · 30,544 cycles

PUNCTURED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 20-60-10 340-801.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 34,221 hrs · 30,544 cycles

CRACK ON AFT EDGE ANGLE BETWEEB BEAM NR 5 AND 6. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND DWG 5914121 REV: AV.

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

CORROSION ON PRODUCTION DOUBLER OF FWD E/E BAY MAST DRAIN. THE DOUBLER WAS REPLACED IAW SRM 51-41-02.

Part: CUSP WEB — CORRODED · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

CORROSION OUT LIMITS ON LH CUSP WEB UPPER AND LWR SURFACE BTW X:60 AND X:44 STAY:544-551 IN REF NRC. S/N. 00329 (CPAX) (NRC 00499). SEAT TRACK ON STA 541 TO 588 LH WAS REMOVED PER B-717 SRM 51-41-01 AREA OUT LIMITS WAS CUT OUT ON STA. 544 TO 556, X=60 AND X=44 L/H PER B-717 SRM 53-00-55 FIG. 208 HFEC INSPECTION WAS ACCOMPLISHED ON LH CUSP WEB UPPER AN LWR SURFACE STA Y544-551, NO CRACKS WERE FOUND AFTER CUT OUT PER DC/MD NDTSPM 06-10-01.- 001. EQUIPMENT. PHASEC 2D N/C 925 DUE DATE 08APR17. PARTS REPAIR WERE FABRICATED PER B717 SRM 53-00-55 REPAIR 4 FIG. 208. REPAIR PARTS WERE INSTALLED PER B-717 SRM 53-00-55, FIG 208 AND SRM 51-41-02. SEAT TRACK WERE INSTALLED ON STA 464 TO STA 579 PER, B-717, SRM 51-41-01. SEAT TRACK WERE INSTALLED ON STA 579 TO STA 588 PER, B-717, SRM 51-41-01. (LP #2794129)

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 34,221 hrs · 30,544 cycles

CRACK ON COCKPIT FLOOR PANEL P/N 9957824-3 (CPIL) (NRC 00465). HFEC WAS ACCOMPLISHED ON COCKPIT FLOOR PANEL P/N 9957824-3 (CPIL) NO CRACKS WERE FOUND AFTER STOP DRILL PER MD-DC/BOEING NDT SPM 06-10-01.001 EQUIPMENT: MENTOR C/N 1205 EXP DATE: 24AGO17 FLOOR PANEL WAS REPAIR PER 53-00-00 FIG 201 SHT 2. (LP #2794149)

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 34,221 hrs · 30,544 cycles

CRACK ON RT CUSP WEB BS 655 - 715 AND RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 223 REPAIR 4.

Part: SKIN — DAMAGED (MLG DOOR) · airframe 34,221 hrs · 30,544 cycles

CRACK ON INNER SKIN BESIDE LATCH LINK ON LT MLG DOOR. INNER SKIN BESIDE LATCH LINK ON LH MLG DOOR X=55 APROXIMATELY WAS REPAIRED PER B-717 SRM 52-82-01 FIG 201 REPAIR 3, 51-41-08, AND 51-41-05. REQUIRED VISUAL INSPECTION EVERY 3000 CYCLES PER SRM B717 REPAIR 3 PAR 6. (LP #2793355)

Part: LONGERON — CRACKED · airframe 34,221 hrs · 30,544 cycles

AFT ACCESSORY COMPARTMENT: CRACKED LONGERONS 2LH AND 2RH AT STA Y=1133 (AMDS 5300-2004) (NRC 00343). LONGERONS 2 LH AND 2 RH AT STA Y=1133 WERE REPAIRED PER B-717 SRM 53-00-05 REPAIR 2. (LP #2793607)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED RT CUSP WEB STA Y=218 BELOW SEAT TRACK X.-44. DAMAGE WAS TRIMMED OUT PER SRM 53-00-55 REPAIR 4 FIG 210. HFEC INSP WAS ACCOMPLISHED ON RT CUSP WEB STA Y=218 BELOW SEAT TRACK X.-44. NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. REPAIR PARTS WERE FABRICATED PER SRM 53-00-55 REPAIR 4 FIG 210. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02. FASTENERS FROM STA Y=218 BTW X=-54 TO X=-44 AND SEAT TRACK FROM Y=200 TO Y=246 X=-44 WERE INSTALLED PER SRM 51-41-02, 51-41-05, AND 51-41-01.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 34,221 hrs · 30,544 cycles

CRACKED INTERNAL CLIP ON RT FWD EMERGENCY EXIT DOOR. CLIP WAS REPLACED PER SRM 51-41-02 AND 51-41-05 DWG 9957735 REV G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED LT FRAME CLIP STA Y1022 BTW LONG 14-13L. FRAME CLIP WAS REPLACED PER SRM 51-41-02, 51-41-05 AND DWG 9912243-197 REV JS.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED LT RING PAN LOWER/AFT CORNER STA Y=636 INTERNAL STRUCTURE (FUS). RING PAN WAS REPAIR PER B717 SRM 56-20-02 FIG 202.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,221 hrs · 30,544 cycles

CRACKED RT RING PAN LOWER/FWD CORNER STA Y=927 INTERNAL STRUCTURE (FUS). DAMAGE AREA WAS REPAIRED PER SRM 56-20-02, REPAIR 1, FIG 202.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,221 hrs · 30,544 cycles

CORROSION ON RT SEAT TRACK X=54 FROM STA Y=984 TO Y=986 AT CABIN FLOOR STRUCTURE. DAMAGE AREA WAS REPAIRED PER B717 SRM 53-20-52 FIG 201 REPAIR 1.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 34,061 hrs · 30,447 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CATWALK EMERGENCY EXIT LIGHT LOST IT`S LENS. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

NR13 FRAME AT STA 1022, BETWEEN STR 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP OF FRAME. NR13 REPAIRED FRAME PER SRM 53-20-07 REPAIR 3, AND LONG BEACH DWG 9912243.

Part: FRAME — CORRODED (BS 1022) · airframe 33,983 hrs · 30,390 cycles

FRAME AT BS 1022, BETWEEN STRINGERS 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP. REPAIRED THE FRAME IAW SRM 53-20-07 REPAIR 3, AND DWG 9912243.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

LONGERON SPLICE BETWEEN STA 954-974 IS CORRODED. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER SRM 53-00-05 REPAIR 2.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

LONGERON 30 SPLICE BETWEEN STA 927 AND 946 IS CORRODED. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER SRM 53-00-05 REPAIR 2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

FRAME AT STA 1022, BETWEEN STR 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP OF FRAME. REPAIRED FRAME PER SRM 53-20-07, AND DWG 9912243.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

FOUND FRAME CORRODED ON LOWER SURFACE AT FS 974 LONGERON 30. SEE NR FOR ADDITIONAL INFORMATION 001-0002:2000-2002/014 00014. REPAIR FRAME PER SRM 53-20-07 REPAIR 3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,307 hrs · 30,605 cycles

CORROSION ON STR30 AT STA 974, 994, AND 1005. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER B717 SRM 53-00-05 REPAIR 2.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,121 hrs · 28,843 cycles

DURING AN OVERNIGHT CHECK, MAINTENANCE FOUND LT AND RT OVERWING EMERGENCY EXIT MARKERS INOPERATIVE. THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY B5-121WERE REPLACED FOR THE EMERGENCY OVERWING LIGHTS. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,663 hrs · 28,488 cycles

DURING LINE CHECK, NOTED SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED SEVERAL BULBS AND POWER SUPPLY ABOVE SEAT 6A. OPERATION CHECKS GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

FUSELAGE TO WING SUPPORT TEE CRACKED AT BS 715 RBL 42.125. R & R SUPPORT TEE IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

FUSELAGE TO WING BEAM SUPPORT CRACKED AT BS 737 RBL 42.128. R & R SUPPORT IAW DWG.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

AFT PIT FWD BULKHEAD LOWER LATERAL PANEL SUPPORT STRAP CRACKED AT BS 817 BETWEEN LBL 0 TO LBL 37. R & R STRAP IAW SRM & DWG.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

AFT PIT FWD BULKHEAD UPPER LATERAL PANEL SUPPORT STRAP CRACKED AT BS 817, BETWEEN RBL 0 TO RBL 37. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

AFT PIT FWD BULKHEAD LOWER LATERAL PANEL SUPPORT STRAP CRACKED AT BS 817 BETWEEN RBL 0 TO RBL 37. R & R STRAP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 28,693 hrs · 26,244 cycles

AFT PIT FWD BULKHEAD UPPER LATERAL PANEL SUPPORT STRAP CRACKED AT BS 817 BETWEEN LBL 0 TO LBL 37. R & R STRAP IAW DWG & SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 28,693 hrs · 26,244 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTING CORRODED AT AFT BS 170. R & R FITTING IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 28,693 hrs · 26,244 cycles

R1 DOOR GIRT BAR FITTING CORRODED AT AFT BS 200. R & R FITTING IAW SRM & DWG.

Part: FITTING — LACK OF LUBE (L1 DOOR) · airframe 29,145 hrs · 26,535 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTING WAS STICKING. LUBRICATED FITTINGS IAW SIP.

Part: CONNECTOR — DISCONNECTED (COCKPIT) · airframe 26,791 hrs · 25,004 cycles

FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. CONNECTED CONNECTOR IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,937 hrs · 24,465 cycles

EMERGENCY LIGHTS AT BASE OF PASSENGER SEATS INOP. REMOVED AND REPLACED BATTERY SUPPLY ASSY PER AMM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 24,736 hrs · 23,716 cycles

AFT CARGO COMPARTMENT LONGERON 30 HAS CORROSION BETWEEN STA 954 TO STA 974. REMOVED AND REPLACED LONGERON IAW B717 SRM.

Part: RIB — CRACKED (L1 DOOR) · airframe 24,736 hrs · 23,716 cycles

L-1 DOOR UPPER FWD RIB CRACKED IN CORNER LOWER SIDE. REMOVED AND REPLACED RIB IAW B717 DWG & SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 24,736 hrs · 23,716 cycles

C2 DOOR JAMB LOWER PAN HAS CORROSION. REPAIRED PAN IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 24,736 hrs · 23,716 cycles

L-1 DOOR INNER HANDLE INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW B717 SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 24,736 hrs · 23,716 cycles

CORROSION - C-1 DOOR LOWER PAN STA 375-425 EXTERIOR SURFACE, BELOW UPPER WEB. REMOVED AND REPLACED PAN IAW SRM.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 23,748 hrs · 23,048 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HARD TO GET IN TRACK. CLEANED GIRT BAR LOCKS PER AMM.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 23,748 hrs · 23,048 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HARD TO GET IN TRACK. CLEANED GIRT BAR LOCKS PER AMM.

Part: LATCH — LACK OF LUBE (L1 DOOR) · airframe 236,110 hrs · 22,956 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR SLIDE LATCHES STICKS. LUBRICATED AND CLEANED LATCHES PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,586 hrs · 22,941 cycles

OVERWING EMERGENCY EXIT LIGHTS INOP AT ROW 22. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,309 hrs · 22,747 cycles

AFT OVERWING EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,165 hrs · 22,651 cycles

BUSINESS CLASS EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,165 hrs · 22,651 cycles

OVERWING EMERGENCY EXIT LIGHT INOP BETWEEN ROW 20 TO ROW 24. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — CRACKED (CABIN) · airframe 23,042 hrs · 22,568 cycles

RT AFT OVERWING DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 23,006 hrs · 22,542 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER FITTING LOOSE. SECURED RETAINER PER MM.

Part: RETAINER — BROKEN (L1 DOOR GIRT BAR) · airframe 22,985 hrs · 22,531 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET BROKEN. REMOVED AND REPLACED RETAINER PER MM.

Part: PIN — LOOSE (EVAC SLIDE)

UPPER SLIDE PIN ON L1 DOOR HAS COME LOOSE. REMOVED AND REPLACED DOOR SLIDE REF MM 25-61.

Part: LANYARD — DISCONNECTED (GIRT BAR)

FOUND R1 GIRT BAR NOT ATTACHED TO SLIDE. RE-INSTALLED GIRT BAR LANYARD ASSEMBLY IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT ASSY INOP ON SEAT 1B. RELAMPED EMRGENCY PATH LIGHT BULB, OPS CHECK GOOD REF AMM 33-00.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY CEILING LIGHTS INOP ROW 15 AND FWD. REMOVED AND REPLACED EMERGENCY BATTERY ASSY AT ROW 10 OVERHEAD BIN IAW B717 MM 33-61, OPS CHECK GOOD.

Part: COVER — MISSING (CABIN)

ESCAPE PATH LIGHTING COVER AT 1D MISSING. INSTALLED COVER REF GMM8103.

Part: CHARGER — DEFECTIVE (MAIN BATTERY)

SHORTLY AFTER APU START-THE CABIN FILLED UP WITH SMELL OF ELECTRICAL SMOKE & THE PASSENGERS WERE DEPLANED-WITH THE RESULTANT / ""BATTERY CHARGER FAIL"" ALERT. REMOVED & REPLACED BATTERY CHARGER PER B717 AMM 24-34-03 AND REPLACED ALL THREE BATTERIES PER B717 / AMM 24-34-01. ALL RTS PASSED & CHECKS NORMAL. ALSO APU STARTS NORMAL NO DEFECTS NOTED AT THIIS TIME.

Part: COVER — MISSING (CABIN)

TRANSFERRED FROM CDR EMERGENCY LIGHT COVER AT 1 D IS MISSING. INSTALLED NEW LENS AT EMERGENCY ROW LIGHT AT SEAT 1 D, OK FOR SVC. REF MM 33-50.

Part: COVER — OUT OF POSITION (CABIN)

EMERGENCY LIGHT COVER ON 1D OFF. INSTALLED EMERGENCY LIGHT COVER AT SEAT 1D AS REQUIRED.