N895AT

Part: SLIDE — OUT OF POSITION (TAIL CONE) · airframe 47,213 hrs · 33,209 cycles

ON WAKE-UP CHECK FOUND THE AFT TAIL CONE SLIDE PACK HAD ROTATED OUT OF SECURED POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED THE TAIL SLIDE PACK REF W/C 2561-9006 AND B717 AMM 285-61. INSTALLED NEW SLIDE REF W/C 2561-9006 & B717 AMM 25-61. (LP #6586012)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,796 hrs · 32,840 cycles

FOUND THE LEFT FORWARD ENTRY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6464450)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,046 hrs · 31,357 cycles

DURING SERVICE CHECK FOUND R1 EMERGENCY SLIDE BOTTLE PRESSURE UNSERVICEABLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED R1 SLIDE PER AMDS CARD 2561-9005. RII COMPLETE BY QC. (LP #5590708)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON SKIN STA Y=214 BTW STR 28R AND STR 29R AT (E/E). SUMMARY OF NRC 00458: CORROSION LEVEL 2. SKIN STA Y=214 BTW STR 28R AND STR 29R WAS REPAIRED PER ER/A 608703-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR TIME CONTROLLED ITEMS, ACCOMPLISH SECTION II WITHIN EVERY 8000 FLIGHT CYCLES FROM 30,163 TOTAL AIRCRAFT FLIGHT CYCLES AS OF 22 MAY 23 UNDER LOG PAGE# 2779457. (LP #2779924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. FWD PASSENGER ENTRANCE SERVICEABLE DOOR REMOVED. SUMMARY OF NRC 00682: PASSENGER FORWARD ENTRANCE DOOR WAS REPLACED PER B717-200 AMM 52-11-01. THIS LOG PAGE SHOULD HAVE BEEN A YES FOR RII AND WORK THAT REQUIRED AND RII INS PECTOR WAS CHECKED BY AN RII INSPECTOR ON THE NRC. (LP #2779305)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

SHEARED OUT AND ELONGATED HOLE ON SKIN, CLOSE TO HINGE #1 OH CONTROL TAB AT RH ELEVATOR STA XE=17 HVS. SUMMARY OF NRC 00339: SKIN, CLOSE TO HINGE #1 OH CONTROL TAB AT RH ELEVATOR STA XE=17 HVS WAS REPAIRED PER ER/A 607692-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS REPAIR APPROVAL IS LIMITED TO 12 MONTHS FROM 20MAY23. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A) REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT UNDER LOG 2775481. ASSOCIATED ER/A 00-607692 ADDED FOR AC 9555. (LP #2775543)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. SUMMARY OF NRC 00090: PASSENGER ENTRANCE DOOR WAS REPLACED FOR SERVICIABLE PASSENGER ENTRANCE DOOR PER B717-200 AMM 52-11-01. (LP #2775388)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON FWD STOP FITTING AT AFT CARGO COMPARTMENT DOOR, (PTAS). SUMMARY OF NRC 00205: AFT CARGO DOOR WAS REPLACED FOR SERVICEABLE AFT CARGO DOOR. (LP #2773786)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH (FUS). SUMMARY OF NRC 00512: EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH WAS REPAIRED PER ER/A 607682-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 12MAY23. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE ANALYSIS (DTA) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. UNDER LOG #2770336. ASSOCIATED ER/A 14-607682 ADDED FOR AC 9555. (LP #2770560)

Part: SKIN — NO DISCREPANCY (ZONE 200) · airframe 47,210 hrs · 33,204 cycles

REPAIR TO FUSELAGE SKIN & DOUBLER AT STA Y=1037 B/W L-13L & L-14L IS PENDING DTE STAGE II & III APPROVAL WITHIN 24 MONTHS OF 12MAY23. DISCONTINUE REVENUE SERVICE ON OR BEFORE 12MAY25 PENDING STAGE II & III APPROVAL. ASSOCIATED ER/A 00-607682 ADDED FOR AC 9555. ER/A 607682-14 REV A, DTE STAGE 2 AND 3 ACCOMPLISHED. ER/A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED AND ARE TRACKED ON NEW LOG PAGE 0670940. TERMINATED LOG PER ENGINEERING COMMENTS. (LP #2770336)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

WEAR ON FWD SEAL RETAINER AREA AFT CARGO DOOR (PTAS). SUMMARY OF NRC 00081: REPAIR ANGLE AT SEAL RETAINER AREA WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LP #2766108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

DURING ATENTION OF NRC 00192, AFTER REMOVE CORROSION, LONGERON 30 FROM STA Y=908 TO Y=927 WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00550: CORROSION LEVEL 2. LONGERON 30 STA Y=900 TO Y=936 WAS REPAIRED PER B717-200 SRM 53-20-05-2R REPAIR 1. (LP #2762922)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON LOWER SURFACE BTW STA Y=370-427 AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00202: CORROSION LEVEL 2. DOOR LOWER JAMB PAN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #2759022)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

WEAR ON ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT STOWAGE AREA AT AFT CABIN BULKHEAD DOOR (PTAS). SUMMARY OF NRC 00184: ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT AT AFT CABIN BULKHEAD DOOR WERE EVALUATED AND REPAIRED AS FOLLOWS: LH HAND SIDE ANGLE WAS BLENDED OUT AND EVALUATED: WITH AN EDGE MARGIN OF 0.631" AND A REMAINING EDGE MARGIN OF 0.581" THEREFORE IT'S WITHIN OF LIMITS. THE RH HAND SIDE ANGLE WAS REPAIRED PER B717-200 SRM 52-10-02-2R AND SRM 52-00-00-1A. (LP #2756166)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON FRAME STA 1021 LONG 7 LH PAX CABIN (CPAX). SUMMARY OF NRC 00312: FRAME STA 1021 LONG 7 LH WAS REPAIRED PER ER/A 607808-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2753465)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR PANEL STRAP AND FITTINGS AT R1 ENTRY CPAX. SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR PANEL STRAP AND FITTINGS WERE REPLACED PER DGW 995782 REV AB & DWG 3936190 REV. (LP #2753530)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA (SM). SUMMARY OF NRC 00296: FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2753031)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA (SM). SUMMARY OF NRC 00295: FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2753140)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACKED LONGERON 2 RH/LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00417: LONGERON 2 RH/LH ON STA Y=1133 WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE, REPAIR 2. (LP #2752081)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH SIDE AT PASSENGER CABIN. SUMMARY OF NRC 00415: CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2751970)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 AT PAX CABIN. SUMMARY OF NRC 00623: CORROSION LEVEL 2. RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #2750646)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND Y=952-953 AND CUSP WEB STA Y=952-953 AND 975-976 RH SIDE AT PAX CABIN IN REF NRC S/N 403. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND CUSP WEB STA Y=952-953 AND 975-976 RH SIDE AT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2748414)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON RH CUSP WEB SPLICE LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59. SUMMARY OF NRC 00408: CORROSION LEVEL 2. RH CUSP WEB SPLICE UPPER AND LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59 WAS REPLACED PER B717-200 SRM 51-41-05-0G & DWG 9910151 REV CH. (LP #2747166)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON LH CUSP WEB ON LIGHTENING HOLE UPPER SIDE ALSO LOWER SIDE STA Y=633, STA Y=670, AND STA Y=810 AT CABIN PAX FLOOR SRTUCTURE. FUS. IN REF NRC 0402. SUMMARY OF NRC 00616: CORROSION LEVEL 2. LH CUSP WEB ON LIGHTENING HOLE UPPER SIDE ALSO LOWER SIDE STA Y=633, STA Y=810 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 & LH CUSP WEB ON STA Y=670 MUST BE REPAIRED UNDER NRC 00415. (LP #2748226)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACK ON INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX (CPAX). SUMMARY OF NRC 00592: INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #2742787)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FORWARD STAIRWELL DOOR INTERNAL SKIN AND RUSTED HARDWARE WERE FOUND IN REFERENCE TO NRC 00256. SUMMARY OF NRC 00577: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B717-200 AMM 52-63-01 420-801. (LP #2741310)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON SETLEMENT ON INBD SEAT TRACK STA 196 TO 200 RBL 20 AT PAX CABIN. W1. SUMMARY OF NRC 00503: CORROSION LEVEL 2. SECTION SEAT TRACK STA 196 TO 265 RBL 20 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR. 5 (LP #2740710)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON LH CUSP WEB UPPER SIDE STA Y=421 ALSO STA Y=468 TO Y=471 IN REF NRC 00401. SUMMARY OF NRC 00614: CORROSION LEVEL 2. LH CUSP WEB STA Y=421 ALSO STA Y=468 TO Y=471 WERE REPAIRED PER B717-200 SRM 53-00-55- 2R FIG 215 AND 216. (LP #2740723)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 AT PAX CABIN. (W1). SUMMARY OF NRC 00526: CORROSION LEVEL 2. FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2737864)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR. LOG PAGE WAS GENERATED BY ERROR PLEASE CLOSE THIS LOG LOGPAGE. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 25APR23 AND LOG COMMENTS. (LP #2736860)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #2736926)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR SUPPORTS STA Y=198 LBL 57 AT PAX CABIN FLOOR SUPPORT. CPAX. SUMMARY OF NRC 00596: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=198 LBL 57 AT PAX CABIN FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP #2735528)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

CRACKED FRAME STA Y=1037 LONG 17 LH AT PAX CABIN (W2). SUMMARY OF NRC 00553: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM. 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #2735918)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN FLOOR STRUCTURE. W1. SUMMARY OF NRC 597: CORROSION LEVEL 2. GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2735690)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200, LBL 7, RBL 7, RBL 44, & RBL 53 AT PAX CABIN (W1). SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORTS (4EA) FROM STA Y=157 TO Y=200, LBL 7, RBL 7, RBL 44, & RBL 53 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #2732863)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

DURING REMOVED FLOOR SUPPORT FROM STA Y=157 TO STA Y=200 & LBL 54 AT PAX CABIN (2EAS) CORROSION ON WEB WAS FOUND IN REFERENCE TO NRC 00526. SUMMARY OF NRC 00580: CORROSION LEVEL 2. WEB BTW STA 160 TO 200 AND X=54 TO X=60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PAR 4 A. (LP #2729498)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON LONGERON SPLICES 29L AND 29RH, INTERNAL STRUCTURE AFT FUSELAGE STA 1110 TO 1120 APROX. SUMMARY OF NRC 00327: CORROSION LEVEL 2. LONGERON SPLICES 29LH AND 29RH, INTERNAL STRUCTURE AFT FUSELAGE STA 1110 TO 1120 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2729290)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR SUPPORTS AT STA Y=177 FROM RBL 10 TO RBL 43 AND STA Y=200 FROM RBL 10 TO RBL 43 IN REF NRC 0522. SUMMARY OF NRC 00595: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 FROM RBL 10 TO RBL 43 AND STA Y=200 FROM RBL 10 TO RBL 43 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2728072)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,641 hrs · 30,163 cycles

CORROSION ON FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 AT PAX CABIN. SUMMARY OF NRC 00507: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 WAS REPLACED PER B717-200 SRM 51-41- 01-0G. (LP #2724884)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,704 hrs · 29,313 cycles

THE EMERGENCY LIGHTS AT WING EXIT DOORS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IN REFERENCE TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7080575)

Part: PRESSURE BLKHD — DAMAGED · airframe 41,695 hrs · 28,446 cycles

HOLE IN PRESSURE DOME BELOW THE NOSE LANDING GEAR ACTUATOR. NRC 001-0270:5300-2001/001 00014: COMPLIED WITH ER/A 582891-14 REV O. (LP #1361132)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,641 hrs · 30,163 cycles

FUSELAGE BULKHEAD STA 110 LBL 14 WEB DAMAGE. REPAIR APPROVAL IS LIMITED TO THE NEXT C-CHECK (NOT TO EXCEED 24 MONTHS) SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 00-582891 ADDED FOR AC 9555. THE REPAIR ON THE 110 BULKHEAD AND SURROUNDING AREAS HAS BEEN INSPECTED AS GVI AND FOUND NO DAMAGE, NO CORROSION, NOR ANY DEFECT AND FOUND TO BE SAFE FOR FERRY FLIGHT FROM SBD TO QRO WHERE PERMANENT REPAIR WILL BE COMPLETED. SUMMARY: PERMANENT REPAIR ON STA 110 LBL 14 BULKHEAD WEB WAS PERFORMED PER ER/A 582891-14 REV. A SECTION II: PERMANENT REPAIR. IN REFERENCE NRC 00281, PLEASE CLOSE THIS LOG PAGE. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 04MAY23 AND LOG COMMENTS. (LP #1358939)

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 41,691 hrs · 28,443 cycles

FOUND CORROSION IN C-2 THRESHOLD AREA. NRC 001-0262:5300-2016/001 00011: CORROSION LEVEL 1, MAINTENANCE REPLACED THE DOOR JAMB PAN REF B717 SRM 53-20-15-2R PROC 7. (LP #1351022)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,398 hrs · 28,237 cycles

THE OVERWING EMERGENCY ESCAPE LIGHTS WILL TURN ON WHEN THE SWITCH IS TURNED OFF. MAINTENANCE REPLACED THE OVERWING EMERGENCY ESCAPE LIGHTING BATTERY PACK IAW AMM 33-51. LIGHTS NOW OPERATE NORMALLY. (LP #6025180)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,444 hrs · 27,530 cycles

THE AFT ACCESSORY COMPARTMENT AND TAIL CONE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT POSITION B5-116 PER AMM 33-51-03. LIGHTS NOW OPERATE NORMALLY. (LP #5692881)

Part: BATTERY PACK — INOPERATIVE (B5-118) · airframe 40,315 hrs · 27,441 cycles

THE EMERGENCY LIGHTS IN CEILING PANELS 8 & 9 AND ADJACENT TO THE PASSENGER DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS B5-118 AND B5-120 PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #5164593)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,589 hrs · 26,928 cycles

MAINTENANCE FOUND MULTIPLE OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE IN THE FORWARD CABIN. MAINTENANCE REPLACED A BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #3717838)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,360 hrs · 26,777 cycles

THE L1-DOOR EXIT SIGN ABOVE FLIGHT ATTENDENT SEAT IS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK B5-235 PER B717 AMM 33-53. OPERATIONAL CHECK WAS GOOD. (LP #4592427)

Part: CRADLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,634 hrs · 26,336 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND THE AFT TAILCONE EMERGENCY LIGHTS TO BE INOPERATIVE. THE EMERGENCY CRADLE ASSEMBLY WAS REPLACED IAW AMM 33-51. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (AC BAY) · airframe 37,921 hrs · 25,823 cycles

THE TAIL SECTION WALKWAY, LOWER EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THAT THE B5-200 POWER SUPPLY AND BATTERY PACK ARE BAD. REPLACED THE B5-200 POWER SUPPLY AND BATTERY PACK REF AMM 33-51. LIGHT OPERATION NOW CHECKS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,207 hrs · 25,306 cycles

UPPER RADIUS OF FRAME TAB AT STA 715.0 FOUND CRACKED REF STEP 13 OF WC 5310-01436-04B 95771310. C/W CARD 5310-01436-02A.

Part: INTERCOSTAL — DAMAGED (BS 696-715) · airframe 37,207 hrs · 25,307 cycles

HOLES DAMAGED IN THE INTERCOSTAL, LONGERON 12L, BS 696 TO 715. REPLACED THE INTERCOASTAL IAW SRM 51-41-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,558 hrs · 24,884 cycles

THE EMERGENCY LIGHTS BETWEEN AFT LAVATORYS ARE INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED GOOD.

Part: LINE — FAILED (HYD SYSTEM) · airframe 35,216 hrs · 23,947 cycles

THE CREW REPORTED THAT WHILE IN CRUISE AT FL 330, THE RT HYD QTY LOW MESSAGE CAME ON. COMPLIED WITH THE QRH AND LANDED NORMALLY AT THE SCHEDULED DESTINATION. MAINTENANCE FOUND THE NR 4 TIRE TREAD SEPARATED, A DAMAGED OTBD SPOILER HYDRAULIC RETURN LINE, AND DAMAGE TO THE RIGHT FLAP LOWER SKIN. A TEMPORARY LINE WAS INSTALLED, THE RIGHT MAIN SPRAY DEFLECTOR, AND ALL OF THE MAIN LANDING GEAR WHEEL AND BRAKE ASSEMBLIES WERE REPLACED. THE RIGHT FLAP ASSEMBLY IS IN WORK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,037 hrs · 23,064 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,338 hrs · 22,573 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER AND THE OPS CHECK WAS GOOD.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 4,503 hrs

DURING NON-ROUTINE LINE UNSCHEDULED CHEK, RT INBD SPOILER FOUND DELAMINATED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,226 hrs · 21,659 cycles

R1 SERVICE DOOR EXIT LIGHT INOPERATIVE. FOUND INLINE WIRE CONNECTOR TO R1 EXIT SIGN, FROM EMERGENCY BATTERY PACK DISCONNECTED. RECONNECTED INLINE WIRE CONNECTOR TO R1 EMERGENCY EXIT SIGN AMM 33-51-00.

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 32,226 hrs · 21,659 cycles

WHILE ACCOMPLISHED RIVET INSPECTION AND OK TO REINSTALL LOWER SCUFF PLATE, FOUND CORROSION AT FWD LOWER CORNER OF C2 DOOR CUTOUT. EWO REQUIRED CHECK LIMITS/REPAIR AS REQUIRED REF ORNRC 63853-0100-0134. REPAIRED C2 DOOR CUTOUT IAW SRM 53-20-15, FIG 201 AND DWG SR09530117, USING 2024T3 .063, 2024-T3 .071, 2024-T3 .080, 2024-T3 .090.

Part: ATTACH FITTING — CRACKED (BS 737) · airframe 32,226 hrs · 21,659 cycles

LT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY LBL 45, FS 737 IS CRACKED IN 2 PLACES AT BOTTOM END. REPLACED ATTACH FITTING IAW SRM 51-41-02, PAGE 40 AND 51-41-05 PAGE 1.

Part: FRAME — DAMAGED (R1 DOOR) · airframe 32,226 hrs · 21,659 cycles

R1 INSIDE DOOR AT BOTTOM OF DOOR AT 2ND BAY FOUND DAMAGE ON THE MIDDLE OF FRAME. SUMMARY OF 63853-0800-0035: SRM 51-41-00, P1 ITEM 2. REPAIRED DAMAGED AREA IAW SRM 51-70-11 REPAIR 201. REINSTALLED LOWER SILL LINKAGE ROD IAW AMM 20-50-01-911-801.

Part: FLOOR SUPPORT — CORRODED (BS 170-190) · airframe 32,226 hrs · 21,659 cycles

FORWARD GALLEY SERVICE DOOR FLOOR SUPPORT HAS CORROSION IN SEVERAL AREAS BETWEEN BS 170-190. MARKED. BLENDED FLOOR SUPPORT IAW SRM 53-00-00, PG 5, FIG 103. REMOVED AND REPLACED THE FLOOR SUPPORT IAW AMM 51-10-00-370-803 SUB TASK 380-001, AMM 51-10-00-370-805, 51-10-00-370-805, SRM 51-41-05, PG 3 FIG 2, SRM 51-20-05, PG 12, FIG 3, AND SRM 51-10-04, STEP 37.

Part: SUPPORT BRACKET — CRACKED (BS 737) · airframe 32,226 hrs · 21,659 cycles

TOP OF CENTER TANK FUSELAGE BS 737, RBL45, SEAT TRACK SUPPORT BRACKET CRACKED FWD AND AFT MOUNTING FASTENERS AT LOWER END. MARKED. REPLACED BS RBL 45, SEAT TRACK SUPPORT BRACKET IAW SRM 51-41-05, PG 1.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,609 hrs · 21,203 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT PATHWAY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: FRAME — CRACKED (BS 696) · airframe 29,893 hrs · 19,855 cycles

BS 696, FRAME CRACKED THROUGH FLANGE JUST BELOW FLOOR REF POINT AT LBL 56. REPLACED THE FRAME IAW 95530013, REV A.

Part: FRAME — CRACKED (BS 674) · airframe 29,893 hrs · 19,855 cycles

UPPER RADIUS OF THE RT OVERWING FRAME BS 674, IS CRACKED. REPLACED THE FRAME IAW DWG SR95530013, REV A.

Part: FRAME — CRACKED (BS 715) · airframe 29,893 hrs · 19,855 cycles

BS 715 FRAME CRACKED THROUGH FLANGE JUST BELOW FLOOR, RBL 56. REPLACED THE FRAME IAW DWG SR 95530013, REV A.

Part: INTERCOSTAL — DAMAGED (BS 674) · airframe 29,893 hrs · 19,855 cycles

FOUND INTERCOSTAL LOWER TEE DAMAGED. REPLACED THE INTERCOSTAL IAW DWG 9919669, REV J.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,365 hrs · 19,455 cycles

DURING SERVICE CHECK, FOUND EXIT SIGN ABOVE FWD LT & RT OVERWING EXITS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY & POWER SUPPLY R5-121, REF AMM 33-51.

Part: PIN — WORN (TAILCONE) · airframe 28,698 hrs · 18,906 cycles

DURING SCHEDULED INSPECTION, IT WAS NOTED THE UPPER LEFT LOCK PIN FOR THE TAILCONE WAS WORN. THE LOCK PIN WAS REPLACED AND THE REQUIRED INSPECTION COMPLETED.

Part: LIGHT — LOOSE (CABIN) · airframe 27,724 hrs · 18,023 cycles

TAIL CONE CEILING PANEL CTR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,724 hrs · 18,023 cycles

FWD EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 27,417 hrs · 17,832 cycles

AFT LT LAVATORY EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 27,417 hrs · 17,832 cycles

LOWER FWD RT OVERWING EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 27,417 hrs · 17,832 cycles

RT WING FIXED LE REFUELING PANEL HOLD OPEN ROD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,417 hrs · 17,832 cycles

RT WW BELOW TRAPEZOIDAL ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: PANEL — CRACKED (RT MLG WW) · airframe 27,417 hrs · 17,832 cycles

RT WW BELOW RESERVOIR AFT BULKHEAD PANEL CRACKED. R & R PANEL IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,417 hrs · 17,832 cycles

RT WW FWD RT BULKHEAD HYD LINE SUPPORT CLIP CRACKED. R & R CLIP IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 26,894 hrs · 17,484 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT. REINSTALLED SLIDE IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,009 hrs · 16,947 cycles

FORWARD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: HOUSING — CORRODED (NLG WW) · airframe 16,773 hrs · 16,773 cycles

NLG HOUSING UPPER BEARING BORE CHAMFER AND LOWER BEARING FACE CORRODED. REPAIRED NLG HOUSING ASSY PER EA.

Part: LANYARD — LOOSE (L1 DOOR) · airframe 24,723 hrs · 16,170 cycles

L1 SLIDE PACK COVER LOOSE. RE-ATTACHED ESCAPE SLIDE LANYARD PER AMM 25-61-01.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 24,170 hrs · 15,803 cycles

WEB PUNCTURED AT BS 148, LBL 44. REPAIRED WEB IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 24,170 hrs · 15,803 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BOTH LATCH ATTCH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,170 hrs · 15,803 cycles

FRAME CORRODED AT BS 974, BETWEEN STR 29R TO STR 29L. REPAIRED FRAME IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,170 hrs · 15,803 cycles

AFT CARGO BILGE CORRODED BETWEEN BS 927 TO BS 960, LBL 29. REPAIRED SKIN IAW SRM.

Part: FITTING — BROKEN (GIRT BAR) · airframe 23,077 hrs · 15,098 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM.

Part: COVER — MISSING (EXIT SIGN)

EMERGENCY EXIT SIGN COVER AT MID CABIN IS MISSING. REPLACED SIGN COVER REF M/M 33-50, OPS CK NORMAL.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: STRUCTURE — CRACKED (LT PYLON)

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

Part: STRUCTURE — CRACKED (LT PYLON)

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

Part: SUPPORT — CRACKED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SUPPORT, STA 1178, LONG L16R TO L17R, CRACKED. ACCOMPLISHED LONGERON SUPPORT REPLACEMENT PER B717 SRM 51-41-05 AND BOEING DWG SR95530005.

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 B717 SRM 54-50-02 FIG 203 REP 1.

Part: ANGLE — CRACKED (THRUST REVERSER)

NR 1 ENGINE, O/B AFT LIGHTENING HOLE, TR DEFLECTOR DOOR ANGLE, CRACKED. ACCOMPLISHED TR DEFLECTOR DOOR ANGLE REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

THE SECURE PIN ON THE GALLEY SERVICE DOOR LOOSE. REMOVED AND REPLACED R1 DOOR SLIDE.

Part: COFFEEMAKER — ODOR (GALLEY)

DURING DESCENT F/A ADVISED OF SMOKE IN THE CABIN. IN FLIGHT EMERGENCY WAS DECLARED. ALL CIRCUIT BREAKERS SET & GALLEY POWER SWITCH THEN BEING TURNED OFF. OPERATED ALL NORMAL OPERATIONS WITHIN THE GALLEY FOUND NR 3 COFFEEMAKER TO BE EMITTING A FOUL ODOR. REMOVED AND REPLACED NR 3 COFFEEMAKER BREWED NUMEROUS TIMES, NO DEFECTS NOTED REF AMM 25-00.

Part: SKIN — DAMAGED (FUSELAGE)

AIRCRAFT STRUCK BY BAG CART, DAMAGED 2 FEET AFT OF TAIL SKID. INSTALLED DOUBLER REPAIR AT LT AND RT VERTICAL SUPPORT CHANNELS AS PER B717 SRM 51-70-11. MATERIAL USED 7075-T6.050. LEFT 4.15" X 2.5" AND RIGHT 4.0" X 2.5". FABRICATED NEW SKIN AS PER B717 SRM 53-30-01 FIG 1. MATERIAL USED 7075-T6. 040" X 59.5" X 27.5" AS PER B717 SRM 51-30-08. MATERIAL SUBSITUTION TABLE A. INSTALLED NEW SKIN AT AFT OF TAIL SKID IAW B717 SRM 57-41-02 AND 51-41-05.