N929AT

Part: SKIN — CORRODED (ZONE 100) · airframe 60,540 hrs · 44,839 cycles

CORROSION ON FUSELAGE SKIN( AREA UNDER FILLET PANELS) Y=590 BTW LONG 24RH, Y=615 BTW LONG 23RH-25RH, Y=901 BTW LONG 25LH-26LH , Y=586-590 LONG 24 RH , Y=588 TO Y=598 LONG 22RH-23RH. CORROSION WAS REMOVED PER BOEING 717 SRM 51- 10-04. (1378734)

Part: SKIN — CORRODED (ZONE 200) · airframe 60,540 hrs · 44,839 cycles

CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)

Part: WIRE SPLICE — DAMAGED (ZONE 200) · airframe 59,498 hrs · 43,909 cycles

EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP AT 12C AND 27C CEILING. INSP AND FOUND DAMAGED SPLICES R5-6720 @ LIGHT L2-746 & R5-6722 @ LIGHT L2-771. REPLACED SPLICES PER B717 SWPM 20-10 & WDM 33-51 -12. MEL AND PLACARD REMOVED.

Part: DOOR — UNSECURE (ZONE 100) · airframe 59,026 hrs · 43,465 cycles

SHIP 9570 -ATB/DE- AIRCRAFT HAD AN UNCOMMANDED HEAVY ROLL IN FLIGHT DURING CLIMB AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED THE AIRCRAFT BACK TO ATL, LANDING UNEVENTFULLY. CORRECTIVE ACTION: UPON ARRIVAL, MAINTENANCE FOUND THAT THE RIGHT BUTE DOOR WAS NOT SECURED. (LP #0913910)

Part: LIGHT — INOPERATIVE (ROWS 24-27) · airframe 58,214 hrs · 42,730 cycles

EMERGENCY LIGHTS ABOVE ROWS 24-27 ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY (B5-231) AND OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51. (LP #6585094)

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 58,001 hrs · 42,564 cycles

THE EMERGENCY LIGHTS AT LOCATION SEAT ROW 20 ARE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK AT LOCATION B5-230 WAS BAD. THE BATTERY AT LOCATION B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6658874)

Part: CONNECTOR — NOT SEATED (ZONE 200) · airframe 57,787 hrs · 42,383 cycles

THE AFT EMERGENCY CEILING LIGHT REMAINED ON IN THE ARM POSITION. MAINTENANCE RESEATED THE CANNON PLUG ON THE AFT CABIN EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. ALL LIGHTS OPERATE NORMALLY. OK FOR SERVICE. (LP #4065840)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,140 hrs · 41,803 cycles

DURING SVC CHK FOUND R FWD AND L FWD OVERWING EXIT IDENTIFIER INOPERATIVE. T/S PER B717 WD 33-51-14, FOUND BATTERY PACK B5-118 INOPERATIVE. REPLACED BATTERY PACK PER B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #5958700)

Part: HEATER — INOPERATIVE (LT WINDSHIELD) · airframe 56,904 hrs · 41,595 cycles

LT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,259 hrs · 41,035 cycles

CRACK ON WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00095: WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX) WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4 AND 51-41-05-0G PAR 8. AFT CABIN BULKHEAD DOOR WAS REMOVED AND INSTALLED PER B717-200 AMM 52-12-03. (LP #0091418)

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 56,453 hrs · 41,199 cycles

CORROSION WAS FOUND ON BOLTS HOUSING AT FLAP HINGE FITTING #3 AND #2. (AI). SUMMARY OF NRC 00366: LH CENTER WING FLAP HINGE FITTING WAS REPLACED PER B717-200 AMM 57-55-25 AND LH INBD WING FLAP HINGE FITTING WAS REPLACED PER B 717-200 AMM 57-55-25 AND OUTBOARD HINGE FLAP "WING FLAP OUTBOARD CYLINDER WAS REPLACED UNDER LP #0059036. (LP #0091108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK WAS FOUND ON OUTER AND INNER PAN IN LOWER AREA STA Y=974 AT AFT CARGO DOOR. SUMMARY OF NRC 00469 AFT CARGO DOOR WAS REMOVED PER B717-200 AMM 52-31-01 AND SERVICEABLE AFT DOOR WAS INSTALLED UNDER AMDS 5231-4004. (LP #0088352)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,048 hrs · 40,866 cycles

CORROSION ON RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX. SUMMARY OF NRC 00308: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX WAS REPAIRED PER ER/A 613282-14 REV ORGINAL, SECTION 1 PERMANENT REPAIR. (LP #0084908)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,048 hrs · 40,866 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00053: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0085760)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1). SUMMARY OF NRC 00507: WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2, REPAIR 2 AND SRM 51-41-08-0G PAR 7 A. (LP #0081861)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,048 hrs · 40,866 cycles

CORROSION WAS FOUND ON SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX. SUMMARY OF NRC 00483: CORROSION LEVEL 2. SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5, AND 51-41-01-0G. (LP #0081151)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,048 hrs · 40,866 cycles

CORROSION ON PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX WAS REPLACED PER B717 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0078664)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON L2L STA 1144 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00192: LONGERON ON L2 STA 1144 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R, PROCEDURE 2. (LP #0077910)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00188: FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-02-0G; TOGETHER WITH THE AMDS 5310-01436-03B AND AMDS 5310-01436-01D. ASSOCIATED AA 5310-01436 ADDED FOR AC 9570. (LP #0076534)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00189: FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G; TOGETHER WITH THE AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9570. (LP #0075811)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE. SUMMARY OF NRC 00252: FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE WAS REPAIRED PER ERA 613218-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0074650)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACKS (2 EA) ON EXTERNAL FUSELAGE SKIN ON PREVIOUS REPAIR AREA, BTW STA 503-522 AND BTW LONG 27RH AND 29RH. SUMMARY OF NRC 00505: EXTERNAL FUSELAGE SKIN BTW STA 503-522 AND BTW LONG 27RH AND 29RH WAS REPAIRED PER B717-200 SRM 53-03-01-2R FIGURE 205 SHEET 1, 51-41-02-0G, AND 51-41-05-0G. THE REPAIR IS CLASSIFIED AS CLASS I AND SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 8,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 8,000 CYCLES, PER B717 SRM 53-03-01-2R-1, PAR 7A. (LP #0073387)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT. SUMMARY OF NRC 00290: FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT WAS REPAIRED PER B717 SRM 53-00-00-2R PROCEDURE 1. (LP #0073479)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK WAS FOUND ON THE CONTRAFRAME STRUCTURE OF THE AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00362: COUNTERFRAME STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1. (LP #0068675)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACKS ON PAN AFT UPPER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00130: PAN AFT UPPER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACK ON FRAME STA 1037 L17L AT PAX CABIN. SUMMARY OF NRC 00201: FRAME STA 1037 L17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-41-05-0G PAR 8 AND 53-20-07-2R PROCEDURE 4. (LP #0054034)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 40,866 cycles

CRACKS WERE GENERATED AROUND FASTENER HOLES OF REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APPROX, DURING REMOVAL OF FASTENERS. SUMMARY OF NRC 00372: REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APPROX WAS REPAIRED PER B717-200 SRM 55-00-00-2R PROCEDURE 2, 51-41-08-0G PAR 7, AND 51-41-05-0G PAR 8. (LP #0052408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,000 hrs · 40,001 cycles

SHIP 9570 -ATO- THE PILOT ABORTED THE TAKEOFF AT 100 KTS DUE TO THE AIRCRAFT DRIFTING LEFT OF CENTER LINE. CORRECTIVE ACTION: MAINTENANCE PERFORMED A HIGH ENERGY STOP INSPECTION AND ACCOMPLISHED CHECKS OF ALL OF THE FLIGHT CONTROLS. NO DEFECTS WERE FOUND. (LP #4703424)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,890 hrs · 39,899 cycles

FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #4773170)

Part: NONE — NONE · airframe 54,479 hrs · 39,536 cycles

FOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PRI 606111-14 REV'S "0","1","2","3" AND ALL REPAIR INSTRUCTIONAL STEPS ARE COMPLETED, ENSURED FINAL ER/A 606111-14 -14 REV. ORIG. SECTION I PERMANENT REPAIR INSTRUCTIONS FOR FUSELAGE / AFT CARGO AREA / L-25R / SKIN REPAIR AND MATCHED WITH INSTRUCTIONAL STEPS COMPLETED ON ER/A PRI 606111-14 REV'S "0","1","2","3". (LP #2641238)

Part: NONE — NONE · airframe 54,428 hrs · 39,493 cycles

LONGERON TEMPORARY REPAIR INSTALLED AT 25R BETWEEN STA 1022 AND STA 1042. COMPLIED WITH LONGERON SPLICE REPAIR PER B717 SRM 53-00-05-2R REPAIR 2 LONGERON REPAIR. A/C WAS DAMAGED BY BELTLOADER ON 13FEB22, REF LOG PAGE 9046786. (LP #2633018)

Part: NONE — NONE · airframe 54,428 hrs · 39,493 cycles

AIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOCIATED ER/A 14-605962 ADDED FOR AC 9570. (LP #9046786)

Part: UNKNOWN — FAULTED (EMERGENCY LIGHTS) · airframe 53,863 hrs · 38,987 cycles

UPON LANDING GEAR EXTENSION, ALL OF THE EMERGENCY EXIT LIGHTS EXTINGUISHED (WENT INOPERATIVE). MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS. ALL LIGHTS CHECKED GOOD. (LP #9580236)

Part: NONE — NONE · airframe 53,320 hrs · 38,490 cycles

---SUPPLEMENTAL INFORMATION: ATL 10AUG22 INSTALLED LEFT LOGO LIGHT PER B717 AMM 33-41. OPS CHECK GOOD. THIS CLEARS CDL. PLACARDS REMOVED. M PROCEDURES REVERSED. --- THE LEFT LOGO LIGHT IS MISSING FROM THE AIRCRAFT. *** CONTRACT MAINTENANCE EVENT - OCM: 250470 *** FORWARD LEFT LOGO LIGHT TO CDL AND PLACARD PER CDL 33-44-01. THE MISSING LIGHT WIRES WERE STOWED AND THE CIRCUIT BREAKER K-17 WAS SECURED OPEN. THE AIRCRAFT IS OK FOR SERVICE. MAINTENANCE WILL REQUIRE THE COMPLETE LOGO LIGHT ASSEMBLY, STK# 92-3300-3-0102, WHICH IS NOT IN STOCK AT THIS STATION. CONTINUE ON CDL. (LP #9051624)

Part: NONE — NONE · airframe 52,371 hrs · 37,616 cycles

THE AFT EMERGENCY OVERWING DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51-04. OPERATIONAL CHECKS IS NOW GOOD. (LP #8542605)

Part: NONE — NONE · corrosion level 2 · airframe 51,726 hrs · 37,049 cycles

CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA). SUMMARY NRC #00213: CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA) WAS TREATED. THE AREA REWORKED IS OUT OF LIMITS PER B717 SRM 57-00-00-1A. THE AILERON WAS REMOVED PER B717 AMM 27-10-01 AND A SERVICEABLE AILERON ASSEMBLY WAS INSTALLED, ADJUSTED, AND TESTED PER B717 AMM 27-10-01. (LP #1995792)

Part: NONE — NONE · corrosion level 2 · airframe 51,672 hrs · 36,998 cycles

CORROSION ON LOWER DOOR JAMB PAN BTW STA 954 -994 AT AFT CARGO COMPARMTENT. SUMMARY OF NRC 00067: CORROSION LEVEL 2, LOWER DOOR JAMB PAN BTW STA 954-994 AT AFT CARGO COMPARMTENT WAS REPAIRED PER B717 SRM 53-20-15-2R. PROCEDURE 7. REPAIR 7. (LP #1995219)

Part: NONE — NONE · corrosion level 2 · airframe 51,672 hrs · 36,998 cycles

CORROSION ON FRAME AT STA Y=927 AND L-30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00222: CORROSION LEVEL 2, FRAME AT STA Y=927 AND L-30 WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/ A 594977-14 REV. ORIGINAL. ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 24999 FLIGHT CYCLES AFTER 23OCT21 AND REPEAT WITHIN EVERY 6500 FLIGHT CYCLES THEREAFTER. UNDER LOG PAGE 1993520. ASSOCIATED ER/A 00-594977 ADDED FOR AC 9570. (LP #1995154)

Part: NONE — NONE · corrosion level 2 · airframe 51,672 hrs · 36,998 cycles

CORROSION ON FRAME AT STA Y=908 AND L-29L TO L-29R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2 FRAME AT STA Y=908 AND L-29L TO L-29R WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/A 594972-14 REV. ORIGINAL. ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 24999 FLIGHT CYCLES AFTER 23OCT21 AND REPEAT WITHIN EVERY 6500 FLIGHT CYCLES THEREAFTER. UNDER LOG PAGE 1993492. ASSOCIATED ER/A 00-594972 ADDED FOR AC 9570. (LP #1995151)

Part: NONE — NONE · airframe 51,672 hrs · 36,998 cycles

CARGO DOOR JAMB WEB WAS FOUND CRACKED ON FRAME AT STA Y=954 AND BETWEEN L-29R TO L-27R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: FRAME AT STA Y=954 AND BETWEEN L-29R TO L- 27R, AFT CARGO COMPARTMENT WAS REPAIRED PER ETI-17-21-026 REV. ORIGINAL AND ERA 594963-14 REV. ORIG. SECTION 1 TIME LIMITED REPAIR. ACCOMPLISH SECTION II: PERMANENT REPAIR OF ERA 594963-14 WITHIN 24 MONTHS FROM 19OCT21. UNDER LOG 1992743. ASSOCIATED ER/A 14-594963 ADDED FOR AC 9570. (LP #1993931)

Part: NONE — NONE · airframe 51,672 hrs · 36,998 cycles

LOOSE FASTENER ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00249: PERMANENT REPAIR WAS PERFORMED ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT PER ETI-17-21- 017 REV. 2 AND ER/A 594962-14 REV. ORIGINAL, SECTION I. ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS: INITIAL INSPECTION WITHIN 2999 FLIGHT CYCLES AFTER 23OCT21 AND REPEAT WITHIN EVERY 3000 FLIGHT CYCLES THEREAFTER UNDER LOG #1993733. (LP #1993937)

Part: NONE — NONE · airframe 51,672 hrs · 36,998 cycles

CARGO DOOR JAMB WEB WAS FOUND CRACKED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00221: REPAIR WAS PERFOMED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. PER B717 SRM 51-70-11-2R FIG. 201 SECTION A-A. (LP #1993787)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,057 hrs · 40,873 cycles

FUSELAGE FRAMES STA 954.0 BETWEEN L- 28R & L-29R IS CRACKED. REPAIR PER SECTION I IS TIME LIMITED AND REQUIRES REPLACEMENT WITH SECTION II PERMANENT REPAIR. ACCOMPLISH ER/A 594963-14, SECTION II PERMANENT REPAIR WITHIN 24 MONTHS FROM 19OCT21. ASSOCIATED ER/A 00-594963 ADDED FOR AC 9570. ASSOCIATED ER/A CHANGED FROM 00-594963 TO 14-594963 FOR AC 9570. SUMMARY OF NRC 0017: FRAME STA Y=954 BTW L-28R TO L29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER ERA 594963-14 REV A, SECTION II, PERMANENT REPAIR. (LP #1992743)

Part: NONE — NONE · corrosion level 2 · airframe 51,670 hrs · 36,997 cycles

CORROSION ON LONGERON L-29L AT STA Y=946 AND Y=954, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00244: CORROSION LEVEL 2, LONGERON L-29L AT STA Y=946 AND Y=954 AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #1986109)

Part: NONE — NONE · corrosion level 2 · airframe 51,670 hrs · 36,997 cycles

CORROSION ON LOWER SPLICE OF AFT PRESSURE BULKHEAD ON STA Y=1053 AND L-30, AFT CARGO COMPARTMENT. SUMMARY, CORROSION LEVEL 2: LOWER SPLICE OF AFT PRESSURE BULKHEAD ON STA Y=1053 AND L-30 AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-08-0I, PROCEDURE 2 FIGURE 1 ITEM 13 AND 51-41-05 0G. (LP #1985726)

Part: NONE — NONE · corrosion level 2 · airframe 51,670 hrs · 36,997 cycles

CORROSION ON LONGERON 30 AND BTW STA Y=954 TO Y=964 UNDER REPAIR SPLICE, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00180: LONGERON 30 OF STA 935 TO 1010 WAS REPAIRED PER B717 SRM 53-20-05-2R. (LP #1981483)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,961 hrs · 39,967 cycles

SOME DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING (AD). ADDL TIME RLTD MON 1972923 ADDED. SUMMARY OF NRC 00161: 57 DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING WERE MEASURED WITH A LARGER DIMENSION: DEPTH: 0.015 IN, DIAMETER: 0.599 IN, DIAMETER/DEPTH: 0.599 IN/0.015 IN=39.93 AND A SMALLER DIMENSION: DIAMETER 0.100 IN, DEPTH: 0.0010 IN, DIAMETER/DEPTH=100. (UT) (TAP-TEST) WAS ACCOMPLISHED AND NO DISBONDS WERE FOUND AT DENTED AREAS. THEREFORE IT IS WITHIN LIMITS PER B717 SRM 57-53-01-1A-1 PAR 3. A. AND 57-53- 01-1A-1 PAR 2. B & DC-MD/BOEING NDTSPM PART 5, 05-10-02.001. PERFORM A DETAILED VISUAL INSPECTION (DVI) AND TAP TEST FOR POSSIBLE DISBOND AT EVERY C-CHECK OR 3,000 CYCLES. OR REPAIR PER AN APPLICABLE SRM 57-53-01-1A-1 PAR 2.B REPAIR. UPDATE DETAILS: FOR TAP TEST INSPECTION SEE LP 1972923. DUPLICATE DAMAGE TO MONITOR LOG 1274668. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 10MAY23 AND LOG COMMENTS. (LP #1972880)

Part: TAB — DELAMINATED (RT WING AILERON)

TAB WAS DELAMINATED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,341 hrs · 35,015 cycles

THE ENTRY DOOR EMERGENCY LIGHTS WERE NOTICED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IAW B717 AMM 33-51-03. (LP #6964715)

Part: CABLE — OUT OF POSITION (TAILCONE) · airframe 48,892 hrs · 34,610 cycles

MAINTENANCE FOUND THE TAILCONE DEPLOYMENT KEVLAR CABLE TO BE INSTALLED/ROUTED INCORRECTLY. THE CABLE WAS RE-INSTALLED AND ROUTED CORRECTLY IN ACCORDANCE WITH B717 AMM 53-52. THE REQUIRED INSPECTION IS COMPLETE. (LP #6898954)

Part: PAN — UNKNOWN (BS 954-994) · airframe 56,351 hrs · 41,113 cycles

SRM REPAIR INSPECTION AFT CARGO DOOR JAMB LOWER PAN SPLICE STA 954-994, L-27R LOG-PAGE UPDATED AT 15JAN14. REMOVED AND INSTALLED AFT CARGO DOOR JAMB LOWER PAN THRESHOLD PER B717 SRM 53-20-15-2R PROC 7 PER NRC 107 ON 19FEB19. OK FOR SERVICE. AFT CARGO DOOR JAMB LOWER PAN WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #1272841)

Part: TAB — DELAMINATED (RT WING)

NON-ROUTINE CHECK UNSCHED

Part: SKIN — DAMAGED (BS 256) · airframe 47,381 hrs · 33,435 cycles

FUSELAGE SKIN DAMAGE AT STA 256, 2 INCHES BELOW L17LT. NRC 011-0001:0514-2001/001 00001: COMPLIED WITH ER/A 580474-14 REV O. ASSOCIATED ER/A 14-580474 ADDED FOR AC 9570. NRC 16: COMPLIED WITH ER/A 580474-14 REV ORIG. PRI 580474-14 REV 0 MATCHES ER/A 580474-14 REV ORIG CLOSING REQUIREMENTS. (LP #1225382)

Part: PANEL — DELAMINATED (RT SPOILER)

RIGHT INBOARD SPOILER PANEL IS DELAMINATED ON THE LOWER INBOARD PORTION OF THE PANEL.

Part: SEAT TRACK — CORRODED (GALLEY) · airframe 46,112 hrs · 32,548 cycles

FORWARD GALLEY FLOOR - RIGHT INBOARD SEAT TRACK HAS CORROSION. NRC 001-0213:2561-1001/001 00245: REPLACED PER B717 SRM 53-20-52-2R-5 FIG 201. (LP #0952566)

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 46,112 hrs · 32,548 cycles

CORROSION FOUND AT AFT CARGO DOOR THRESHOLD. REPLACED AFT CARGO DOOR JAMB REF SRM 53-20-15-2R PROC 7.

Part: GUARD — BROKEN (TOGGLE SWITCH) · airframe 42,227 hrs · 29,801 cycles

FOUND EMERGENCY LIGHT GUARD SWITCH BROKEN. REPLACED TOGGLE SWITCH GUARD. LP# 3434126

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

AFT CARGO COMPARTMENT HAS CORROSION ON RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022. RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022 WAS REPLACED PER SRM 51-41-01 0G.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FRAME Y=1022 BTW LONG 28L AND 27R AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER SRM 53-20-07 2R-3. HFEC INSPECTION WAS PERFORMED PER NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND ALONG TRIM LINE.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

MLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA 755 Z=-9 FROM X=O TO X=-53. AS VIEWED FROM RT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI 17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

MLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA STA 755 Z=-9 FROM X=O TO X=-53. AS VIEW FROM LT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI-17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.

Part: RUB STRIP — CORRODED (BS 579-813) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON LEFT UPPER RUBTRIPS BETWEEN BS 775 TO 813 AND BETWEEN BS 579 TO 696. THE RUB STRIPS WERE REPLACED IAW SRM 51-20-05 0G.

Part: SKIN — CORRODED (BS 760-800) · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.

Part: SEAT TRACK — CORRODED (BS 110-140) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON INBD & OTBD F.O. SEAT TRACK , ALSO ON FLOOR SUPPORT RBL 54 BTW BS 140 TO 110. REPAIRED IAW ETI-17-17-034 REV. 1 AND ER/A 555629-14 REV.ORIGINAL.

Part: ANGLE — CRACKED (BS 674) · airframe 41,170 hrs · 29,008 cycles

ANGLE CRACKED ON REPAIR ON FWD CARGO BAY BULKHEAD BS 674, LONGERON 24L. REPLACED IAW SRM 51-41-05 AND SRM 51-40-08 0G.

Part: SKIN — CORRODED (FUEL TANK) · airframe 41,170 hrs · 29,008 cycles

TO ACCOMPLISH REMOVAL OF CORROSION ON CENTER TANK UPPER SKIN, CUT/REPAIR WEB/ANGLE AS REQUIRED FROM STA Y=727, 737, AND X=0. AREA WAS REPAIRED ON CENTER TANK UPPER SKIN (WEB/ANGLE) FROM STA Y=726, 755, AND X=0 PER 51-70-11 2R, 51-40-02, AND 51-40-05.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FLOOR PANELS 222XF AND 222AQF (SM). DUE TO EXCESSIVE DAMAGE FLOOR PANELS WERE REPLACED PER SRM 51-40-08 06 AND DWG 9952521 REV BB.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

CRACK IN WEB OF THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB AT 2 HRS POSITION (CPAX). REPAIR WAS ACCOMPLISHED PER INSTRUCTIONS OF ETI 17-17-023 REV 3 AND ER/A 554168-14 REV ORIGINAL.

Part: ANGLE — CORRODED (BS 465-470) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON CUSP ANGLE FROM BS 465 - 470, LONGERON 18R. THE CUSP ANGLE WAS REPAIRED IAW ETI-17-17-028 REV.2, AND ER/A 555636-14 REV. ORIGINAL.

Part: BEAM — CRACKED (R1 DOOR) · airframe 41,170 hrs · 29,008 cycles

FWD R1 DOOR AREA HAS A CRACKED NR 4 BEAM AT FWD EDGE. A NEW BEAM WAS FABRICATED AND REPLACED IAW SRM 51-41-02, 51-41-05,AND DWG 911582 REV T.

Part: BEAM — CRACKED (NLG WW) · airframe 41,170 hrs · 29,008 cycles

CRACKED LATERAL BEAM LBL 60- 18 AND RBL 18 IN THE NOSE LANDING GEAR WHEEL WELL. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 53-10-14-2R PROCEDURE 2.

Part: SEAL DEPRESSOR — CRACKED (BS 994) · airframe 41,170 hrs · 29,008 cycles

CRACK ON AFT CARGO DOOR FRAME SEAL DEPRESSOR BS 994 BETWEEN LONGERONS 24 AND 25R. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15 2R.

Part: FLOOR SUPPORT — CRACKED (BS 715) · airframe 41,170 hrs · 29,008 cycles

CRACKED FITTING BS 715 LBL 44 FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05 0G.

Part: CHANNEL — CRACKED (CABIN) · airframe 41,170 hrs · 29,008 cycles

CRACK ON FLOOR PANEL CHANNEL. REPAIRED IAW SRM 53-20-50 2R-5.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 41,170 hrs · 29,008 cycles

CRACKED FLOORBEAM, BS 737 RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-01 0G , SRM 51-41-02 0G, AND SRM 51-41-05 0G.

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON ACCESS PANEL CUT OUT RUB STRIPS ON THE LT WING THE RUB STRIPS WERE REPLACED IAW SRM 57-10-01 2R PROCEDURE 3.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON THE SETTLEMENT AREA OF THE UPPER FUEL ACCESS PANEL OF THE LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 AND SRM 51-22-2A COND. III.

Part: FRAME — CRACKED (BS 715) · airframe 41,170 hrs · 29,008 cycles

CRACKED FRAME ANGLE BS 715. THE FRAME WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 41,170 hrs · 29,008 cycles

AFT CARGO DOOR HAD A CRACKED INTERCOSTAL AT AFT CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05 AND DWG 9957665 REV. R.

Part: PAN — CRACKED (CARGO DOOR) · airframe 41,170 hrs · 29,008 cycles

CRACKED OTBD PAN IN BEAM NR 5 AT AFT CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02, REPAIR 6, FIG. 201.

Part: FRAME — CRACKED (BS 696) · airframe 41,170 hrs · 29,008 cycles

CRACKED FRAME ANGLE BS 696. THE FRAME ANGLE WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 41,170 hrs · 29,008 cycles

FWD CARGO BAY HAD A CRACKED INTERCOSTAL BS 636 - 617, BL 0. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00 2, FIGURE 201, AND INSTALLED IAW SRM 51-41-05.

Part: FRAME — CRACKED (BS 674) · airframe 41,170 hrs · 29,008 cycles

CRACKED FRAME ANGLE BS 674. THE FRAME ANGLE WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR. 1.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 41,170 hrs · 29,008 cycles

CRACKED ON SIDES FLOOR PANELS OF COCKPIT (CAB PILOT). FLOOR PANEL WAS REPAIRED PER SRM 53-00-00 2R-1.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 41,170 hrs · 29,008 cycles

CRACK ON COCKPIT FLOOR PANEL 211EF. FLOOR PANEL WAS REPAIRED PER SRM 53-00-00 2R-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON ANGLE AT LWR FWD EDGE. ANGLE WAS REPLACED PER SRM 51-41-02, 51-41-05, AND DWG 9911578 REV H.

Part: FLOORBEAM — CRACKED (BS 715) · airframe 41,170 hrs · 29,008 cycles

CRACK ON FLOORBEAM BS 715 BETWEEN LBL 22 TO RBL 22. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

CRACKED ON LOWER CENTER INTERCOSTALS OF AFT CARGO DOOR. LOWER CENTER INTERCOSTALS WERE REPLACED PER SRM 51-41-02 0G AND 51-41-05 0G.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FLOOR SUPPORT BS 160 - 200 BETWEEN LBL 44 AND 54. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, AND 51-30-07-0G FIG 9.J. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08 0G AND SRM 51-30-07 0G FIG. 9(J) AND 19.

Part: FLOORBEAM — OUT OF LIMITS (BS 180) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

FLOORBEAM BS 180, RBL 7 - 44 WAS FOUND OUT LIMITS. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-07 0G, FIG 9.J, 51-40-08 OG, 51-10-04 0G PAR 21 AND 15, 51-41-02 0G, AND 51-41-05 0G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

CRACKED CLIP ON DOOR JAMB STA Y=208 BTW LONGERON 12 AND 11 LT. CLIP WAS REPAIRED PER SRM 53-10-15 2R-1 REPAIR 1 FIG 201.

Part: BEAM — CRACKED (L1 DOOR) · airframe 41,170 hrs · 29,008 cycles

FWD ENTRANCE DOOR (L1): CRACKED BEAM 7 AT FWD EDGE. BEAM WAS REPAIRED PER SRM 52-10-02 FIG 202 REPAIR 13.

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

CRACK ON STRAP STA 172.156 BTW BEAM 5 AND 6 AT LH1 FWD PASSENGER DOOR OPENING. DAMAGE STRAP WAS REPLACED PER SRM 51-41-02 AND 51-41-05, DWG 9955750 REV U.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

CRACK ON CHANNEL (MID SECTION) AND CRACK ON UPPER SKIN FLOOR PANEL 222NF. FLOOR PANEL 222NF WAS REPAIR ON CHANNEL FLOOR PANEL AND UPPER SKIN PER SRM 53-20-50 2R-5 AND 53-00-00 2R-1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,170 hrs · 29,008 cycles

DELAMINATED FLOOR PANEL. REPLACED IAW SRM 53-20-50 2R.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 41,170 hrs · 29,008 cycles

FLOOR PANEL CRACKED. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R.

Part: FLOOR SUPPORT — OUT OF LIMITS (BS 160-200) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

FLOOR SUPPORT BS 160 TO 200, RBL 44 , FOUND OUT OF LIMITS. REPLACED IAW SRM 51-30-07-0G FIG 9.J.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,170 hrs · 29,008 cycles

DENT ON EXTERNAL FUSELAGE SKIN BTW LONG 28R AND 29R STA Y=510). FUSELAGE SKIN WAS REPAIRED PER SRM 53-02-01 2R-1 FIG 202 SHEET 13. MAINTENANCE REQUIREMENTS PERFORM GENERAL VISUAL INSPECTION, INITIAL 8,000 CYCLES AND REPETITIVE 8,000 CYCLES PER SRM 53-02-01-2R-1 STEP 6 (A).

Part: CUSP WEB — CORRODED (BS 794-813) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON LT CUSP WEB BETWEEN LBL 44 AND 60, BS 794 - 813. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 2R-4, FIG 215.

Part: CUSP WEB — CORRODED (BS 525-527) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 525 - 527 AND LBL 55 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 2R-4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON THE FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-07 0G, FIG.18, SHEET 3 AND 51-41-02.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FUEL TANK ACCESS PANEL 141AR. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.

Part: FLOORBEAM — CORRODED (BS 212) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON FLOORBEAM BETWEEN LONGERONS 28R AND 28L BS 212. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-01 0G, 51-41-02 0G, AND 51-41-03 0G.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON ACCESS PANEL COUNTERSINK AND SETTLEMENT AREAS. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01 2R-2 PAR 5 B,

Part: FLOOR PANEL — DELAMINATED · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

FLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.

Part: CUSP WEB — CORRODED (BS 455-490) · corrosion level 2 · airframe 41,170 hrs · 29,008 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 455-459, 488-490, RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4, FIG. 215.

Part: FLOOR PANEL — BROKEN (LAVATORY) · airframe 41,170 hrs · 29,008 cycles

BROKEN LAVATORY FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.

Part: PAN — CRACKED (BS 636-927) · airframe 41,170 hrs · 29,008 cycles

CRACK ON LEFT RING PAN, FWD LOWER CORNER BS 636 - 927. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R FIG 202 TYPE B, 51-41-02 0G, AND 51-41-05 0G.

Part: BEAM — CRACKED (L1 DOOR) · airframe 41,170 hrs · 29,008 cycles

L1 DOOR HAD A CRACKED BEAM NR 1 AT FWD EDGE. REPAIRED IAW SRM 52-10-02, FIGURE 202, REPAIR 7.

Part: PAN — CRACKED · airframe 41,170 hrs · 29,008 cycles

CRACK ON LT RING PAN, AFT UPPER CORNER BS 813 - 832, 832 - 851, 851 - 870. LEFT RING PAN, REPAIRED IAW SRM 56-20-02-2R FIG 202 TYPE B, 51-41-02 0G, AND 51-41-05 0G.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 40,960 hrs · 28,859 cycles

AFT CARGO, LOWER ENTRY JAMB CORRODED. REMOVED CORROSION PER SRM 53-00-15 FIG. 101. FABRICATED AND INSTALLED NEW SPLICE PLATES PER DWG 5910158. REINSTALLED THRESHOLD AND SEALED PER 51-41-01.

Part: SKIN — DEBONDED (FUSELAGE) · corrosion level 2 · airframe 38,456 hrs · 26,949 cycles

LEFT ALTERNATE STATIC PORT INTERNAL DOUBLER DISBONDED FROM SKIN. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412.

Part: DOOR FRAME — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 38,456 hrs · 26,949 cycles

FWD CARGO, LOWER ENTRY JAMB CORRODED. REPLACED FWD CARGO LOWER ENTRY DOOR JAM IAW SRM 53-20-15, REPAIR NR 6, ACCESS RESTORED.

Part: LONGERON — CORRODED (BS 954) · airframe 38,456 hrs · 26,949 cycles

AFT CARGO LONGERON 30 CORRODED AT BS 954. BLENDED CORROSION ON LONGERON 30 AT BS 954 ORIGINAL MATERIAL THICKNESS .125, .063 REMAINING AT DEEPEST POINT. INSTALLED REPAIR IAW SRM 53-00-05, REPAIR 3. WIP: BLENDED CORROSION ON LONGERON 30 AT BS 954 ORIGINAL MATERIAL THICKNESS 125, .063 REMAINING AT DEEPEST POINT. INSTALLED REPAIR IAW SRM 53-00-05, REPAIR 3. CORROSION LEVEL 1 CLOSING REQUIREMENTS RII: INSPECTOR 229865.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,456 hrs · 26,949 cycles

FUSELAGE SKIN BS 1087 AND L-14R. CRACK REPAIR.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 36,953 hrs · 25,766 cycles

DURING LINE CHECK IN MSP, DETERMINED FORWARD F/A PANEL EMERGENCY LIGHT SWITCH WOULD NOT TOGGLE FROM ARM TO ON POSITION. REPLACED SWITCH AND PERFORMED OPS TEST IAW AMM 33-51-00-710-801. LP 1950780 & 1950789.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,617 hrs · 24,666 cycles

FWD EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-03. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,246 hrs · 24,357 cycles

DURING LINE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY FOR THE FIRST CLASS EMERGENCY LIGHTS IAW AMM 33-51 AND OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 33,952 hrs · 23,221 cycles

LT AFT OVERWING EMERGENCY EXIT DOOR INOPERATIVE. R & R CHARGER IAW AMM.

Part: CHARGER — FAILED (CABIN) · airframe 33,618 hrs · 23,008 cycles

EMERGENCY EXIT LIGHT BATTERY CHARGER FAILED OPERATION TEST AT BS 119. R & R CHARGER IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN FLOOR PANEL 221KF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN FLOOR PANEL 221EF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

MAIN FLOOR PANEL 211ATF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN FLOOR PANEL 221FF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN FLOOR PANEL 221CF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN FLOOR PANEL 221AF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN SEAT TRACK, RBL 22 IS CORRODED AT STATION 898. R & R SEAT TRACK SECTION IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

MAIN CABIN SEAT TRACK, RBL 56 IS CORRODED AT STATION 870 TO STATION 898. R & R SEAT TRACK SECTION IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

RT CUSP WEB BETWEEN STATION 656 TO STATION 674 CRACKED. REPAIRED CUSP WEB IAW SRM.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 33,618 hrs · 23,008 cycles

L1 DOOR UPPER AFT BEAM DOUBLER CRACKED. REPAIRED DOUBLER IAW SRM.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 33,618 hrs · 23,008 cycles

LT WING NR 3 SLAT CTR TRACK ATTACH FITTING CRACKED. R & R NR 3 SLAT IAW MM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,618 hrs · 23,008 cycles

L1 DOOR INTERCOSTAL CRACKED IN DOOR HANDLE BOX. R & R INTERCOSTAL IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 33,618 hrs · 23,008 cycles

L1 DOOR NR 2 BEAM CRACKED. R & R DOOR BEAM IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

AFT CARGO DOOR CUT OUT LOWER WEB CORROSION AT FWD OTBD CORNER. R & R WEB IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

AFT CARGO DOOR JAMB WEB CORRODED. R & R JAMB WEB IAW SRM.

Part: HINGE — CRACKED (FUSELAGE) · airframe 33,618 hrs · 23,008 cycles

GND CONDITIONED AIR DOOR FUSELAGE SIDE HINGE CRACKED AT THE LOBES. R & R HINGE IAW SRM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 33,399 hrs · 22,875 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: COVER — MISSING (CABIN) · airframe 30,602 hrs · 21,116 cycles

EEPLS COVERS MISSING. INSTALLED COVERS IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 30,602 hrs · 21,116 cycles

EEPLS LAMP MISSING. RELAMPED IAW AMM.

Part: DOOR — LOOSE (TAILCONE) · airframe 30,427 hrs · 20,986 cycles

TAIL CONE DOOR HANDLE IN AFT ACCESSORY COMPARTMENT LOOSE. SECURED DOOR IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,734 hrs · 20,532 cycles

EMERGENCY LIGHTS INOP AT L2-761 & L2-765. REMOVED AND REPLACED BATTERY & CHARGER PER MM.

Part: CHECK VALVE — FAULTY (FUEL SYSTEM) · airframe 29,725 hrs · 20,525 cycles

DIVERSION / DECLARED EMERGENCY. WHILE AT CRUISE FUEL BEGAN TO TRANSFER TO CENTR TANK. REMOVED AND REPLACED CENTER CHECK VALVE ASSY AND CENTER TANK FLOAT PER MM.

Part: COVER — CRACKED (EXIT SIGN) · airframe 29,611 hrs · 20,445 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,611 hrs · 20,445 cycles

EMERGENCY BATTERY ASSY INOP AT ROW 24. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

SKIN CRACKED BETWEEN BS 844 TO BS 851, BETWEEN STR 27L TO STR 28R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,611 hrs · 20,445 cycles

FWD EMERGENCY FLASHLIGHT LED INDICATOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 29,611 hrs · 20,445 cycles

FWD CARGO DOOR SKIN CRACKED AT BS 425, STR 25R. REMOVED AND REPLACED FWD CARGO DOOR ASSY PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 29,611 hrs · 20,445 cycles

RIGHT WING I/B SPOILER DELAMINATED AT BOTH SIDES OF ACTUATOR HINGE PLATE. REMOVED AND REPLACED SPOILER PER MM.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

L1 DOOR FRAME CREASED AT BS 237, BETWEEN STR 17L TO STR 18L. REPAIRED FRAME PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

MAIN CUSP WEB CORRODED AT BS 229, RBL 54. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

L1 DOOR FRAME CREASED AT BS 237, BETWEEN STR 16L TO STR 17L. REPAIRED FRAME PER SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

FRAME CREASED AT BS 908, BETWEEN STR 27R TO STR 30R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

RT CABIN FLOOR CREASE WEB CORRODED AT FS 170. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

FRAME PUNCTURED AT BS 851, STRL 29L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

STRINGER CORRODED AT BS 754, STR 30R. REPAIRED STRINGER IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

SKIN CORRODED AT BS 851, BETWEEN STR 24L TO STR 30L. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN FS 198 TO FS 210. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

MAIN CABIN CUSP MEMBRANE CRACKED AT BS 637, LBL 54.5 SEAT TRACK. REMOVED AND REPLACED DOUBLER IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 29,611 hrs · 20,445 cycles

RIGHT EMERGENCY EXIT LIGHT LENS MISSING BETWEEN ROW 20 TO ROW 24. INSTALLED LENS PER MM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,611 hrs · 20,445 cycles

MAIN CABIN CUSP MEMBRANE CRACKED BETWEEN BS 579 TO BS 598, LBL 54.5. REMOVED AND REPLACED MEMBRANE IAW SRM.

Part: SLIDE — LOW PRESSURE (TAILCONE) · airframe 29,611 hrs · 20,445 cycles

AFT TAIL CONE EMERGENCY EXIT SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MM.

Part: COVER — MISSING (CABIN)

TRANSFER ED FROM CDR 20D EMERGENCY PATH LIGHT COVER IS NOT THERE. INSTALLED EMERGENCY ESCAPE PATH LIGHT AT 20D REF AMM 33-51.

Part: LANYARD — UNKNOWN (EVAC SLIDE)

INSPECT L-1 SLIDE. INSTALLED L-1 DOOR LANYARD REF B717 MM 25-61.

Part: LANYARD — FRAYED (R1 DOOR)

R1 DOOR LANYARD FRAYED. REMOVED AND REPLACED LANYARD.

Part: LIGHT — INOPERATIVE (CABIN)

BOTH BULBS INOP IN ONE OF THE TWO EMERGENCY ESCAPE PATH LIGHT ASSY ON AISLE SIDE OF SEAT 2D. RELAMPED, OPS CHECK GOOD REF MM 33-50.

Part: LENS — MISSING (CABIN)

ONE OF THE TWO EMERGENCY ESCAPE PATH LIGHT ASSY ON AILSE SIDE OF SEAT 3D IS MISSING ITS LENS COVER. RE-INSTALLED LENS COVER REF MM 33-50.

Part: SHROUD — LOOSE (CABIN)

EMERGENCY TRACK LIGHTING LOOSE ON SEAT 10D. REMOVED AND REPLACED SHROUD ASSY PER 25-23.

Part: LENS — MISSING (CABIN)

MISSING RED LENS, EMERGENCY LIGHT, ROW 21D. INSTALLED NEW LENS AS REQUIRED, LIGHT OPS CHECK OK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, LBL 20, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 199, LBL 7, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 AND B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 24, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 199, RBL 5 TO RBL 36, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOP AT ROWS 25-31. REPLACED BATTERY PACK IAW MM 33-51. OPS NORMAL.

Part: LENS — MISSING (CABIN)

EPL LIGHT LENS MISSING AT SEAT 21D (WHITE LENS, AFT POSITION). REPLACED MISSING EPL LENS AT SEAT 21D, AFT POSITION, WHITE.

Part: WIRE — PULLED (CABIN)

SEAT ROW 30 E-PATH LIGHT QUICK DISCONNECT WIRING PULLED OUT OF CONNECTOR. RE-TERMINATED QUICK DISCONNECT AT SEAT/WALL INTERFACE IAW SWPM 20-31-13, OPS CHECK NORMAL IAW AMM 33-51-00.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB CORRODED BEYOND LIMITS. CUT OUT CORRODED PAN & REPLACED PER B717 SRM 23-20-15.

Part: BATTERY — DISCHARGED (CABIN)

EPL LIGHTS OUT ON SEATS 25-31. REMOVED AND REPLACED BATTERY ASSY B5-119.

Part: CONNECTOR — BROKEN (CABIN)

EMERGENCY LIGHTS AT ROWS 25-31 DEF INOPERATIVE. REPAIRED BROKEN CONNECTOR AT ROW 30 IAW WDM. SWAPPED BATTERY PACKS 123 & 119 IAW 33-51-03. OP CHECKS GOOD.

Part: PAN — CORRODED (FUSELAGE)

CORROSION ON FWD CARGO DOOR CUTOUT LOWER JAMB AREA, OUT OF AMM LIMITS. INSTALLED FWD CARGO DOOR LOWER JAMB PAN CORROSION SPLICE REPAIR PER SRM 53-20-15 FIG 201.

Part: SLIDE — UNSERVICEABLE (TAIL CONE)

DURING ROUTINE MAINTENANCE SERVICE CHECK FOUND TAIL CONE EMERGENCY ESCAPE SLIDE PRESSURE LOW. REMOVED AND REPLACED TAIL CONE EMERGENCY ESCAPE SLIDE ASSY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FOUND DURING SERVICE CHECK BUSINESS CLASS SEAT ROWS 1, 2 AND 3 EMERGENCY PATH LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY B5-118 IAW AMM 33-51-03, OPS CHECK GOOD. BLOWN FUSE INTERNAL.