N951AT

Part: WARNING MESSAGE — ILLUMINATED (SLAT SYS) · airframe 63,857 hrs · 45,946 cycles

SHIP 9510 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 110 KTS DUE TO RECEIVING AN AURAL "SLAT CONFIGURATION" MESSAGE. CORRECTIVE ACTION: MAINTENANCE (LP #7507750)

Part: BARREL NUT — CORRODED (ZONE 300) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH), AND 29 (LOWER RH) AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00544: CORROSION LEVEL 2. BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH) CLEANED PER DAL P.S. 900-1-2-1 NO 01 AND NEW SELLANT WAS APPLIED PER B717-200 SRM-51-20-05-0G. AND 29 (LOWER RH) AT HORIZONTAL STABILIZER CENTER BOX WAS REPAIRED PER PRI 620137-14 REV 1 & ER/A 620137-14 REV ORIG, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-620137 ADDED FOR AC 9510. LINE 04 REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 28AUG24 PER ER/A 620137-14 REV ORIG SECTION TIME CONTROLLED ITEM. (LP #0589497)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

-AD- CORROSION ON UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL. SUMMARY OF NRC 00216: CORROSION LEVEL 2. UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL WAS REPAIRED PER PRI 620162-14 REV 8 AND ER/A 620162-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR ASSOCIATED ER/A 00-620162 ADDED FOR AC 9510. (LP #0580212)

Part: SKIN — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

-AD- CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH (FUS). SUMMARY OF NRC 00348: CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH WAS REPAIRED PER ER/A 619986-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 23-SEP-24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. LOG PAGE # 0577714 AMOC APPROVAL TO AD 2017-01-03 IS REQUIRED FOR SERVICE BEYOND 60,000 TOTAL FLIGHT CYCLES (NO MORE THAT 15,039 CYCLES REMAINING). LOG PAGE # 0577739 ASSOCIATED ER/A 14-619986 ADDED FOR AC 9510. (LP #0579490)

Part: SKIN — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R. SUMMARY OF NRC 00047: CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R WAS REPAIRED PER ERA 619868-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER 11-SEP-2024 UNDER LOG PAGE #0559602. ASSOCIATED ER/A 14-619868 ADDED FOR AC 9510. (LP #0561770)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00135: CORROSION LEVEL 2. FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT WAS REPLACED PER DWG 5971111 REV F AND PER B717-200 SRM 51-41-01-0G AND 51-41-02-0G.

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON JAMB PAN (BTW LONG 25RH-29RH) LOWER EDGE AND AFT EDGE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2. JAMB PAN (BTW LONG 25RH-29RH) FWD CARGO DOOR COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #0537653)

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00804: CORROSION LEVEL 2. INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT WAS REPLACED PER DRAWING 9923686 REV D AND NRC 00285. (LP #0535463)

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

CORROSION ON LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN. SUMMARY OF NRC 00753: CORROSION LEVEL 2. LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0530948)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON DOUBLER PRODUCTION OF MASTER DRAIN BTW STA Y=199 AND Y=218, L28R, AND L29R. ALSO STA Y=163, Y= 183 BTW L29L AND L30 AT E/E COMPARTMENT. SUMMARY OF NRC 00295: CORROSION LEVEL 2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R WAS FABRICATED PER DRAWING 9923686 REV D, AND PRODUCTION DOUBLER AT STA Y=163 TO Y=183 BTW L29L AND L30 WAS FABRICATED PER DRAWING 5971208 REV A. AND PRODUCTION DOUBLERS WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0530402)

Part: BEAM — CRACKED (ZONE 100) · airframe 62,710 hrs · 44,961 cycles

CRACK BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00225: BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 51-70-11-2R. PROCEDURE 2 REPAIR 2, FIG 201. (LP #0527465)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW. SUMMARY OF NRC 00693: FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0526479)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CORROSION OUT OF LIMITS WAS FOUND ON PASSENGER CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2- CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4. FIG. 216. (LP 0525041)

Part: LONGERON — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CRACK ON LONGERON END (2EAS) FROM STA 1133 BTW LONG 2 LH TO LONG 2RH OF AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: LONGERON END FROM STA 1133 LONG 2RH OF AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B-717-200 SRM 53-00-05-2R PROCEDURE 2 FIG.201, AND LONGERON 2LH NO CRACKS WERE FOUND. PER DC-MD/BOEING NDTSM PART 6, 06-10-01.001 (EQUIPMENT. - MENTOR C/N.- 1137 EXP.- 25-SEP-24). (LP 0523706)

Part: WEB — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CRACK UNDER, INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX. CORRECTIVE ACTION: INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0525055)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CORROSIONS ON CUSP MEMBRANE (WEB) RH ON SEVERAL LOCATIONS FROM STA Y=560 TO STA Y=579 AND STA Y=503 TO STA Y=522 AND STA Y=484 TO STA Y=503 AND STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH ON LOCATIONS FROM STA Y=560 TO STA Y=579, STA Y=503 TO STA Y=522, STA Y=484 TO STA Y=503 AND STA Y=446 TO STA Y=465 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.209, FIG. 210 AND FIG. 211. (LP 0523322)

Part: WINDOW FRAME — CRACKED (ZONE 100) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, HIDDEN DISCPRECANCY; AFTER BRACKET WAS REMOVED, CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW. CORRECTIVE ACTION: FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP 0523178)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, INITIAL INSPECTION: CRACK ON CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R FIGURE 223. (LP 0523259)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, AFTER BLEND OUT CRACKS WERE FOUND AT LH CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. WAS REPAIRED PER B717-200 SRM-53-00-55-2R-4. (LP 0523187)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0518607)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX. CORRECTIVE ACTION: CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP 0516683)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, CORROSION ON FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 AT PAX CABIN STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2, FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 WERE FABRICATED PER DWG 9936534 REV:BW AND REPLACED PER B717-200 SRM 51-41-02-0G. (LP 0514615)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

AIRCRAFT 9510, INITIAL INSPECTION: CORROSION ON LH REPAIR DOUBLER OF CUSP WEB STA Y=841, Y=866 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2-LH CUSP WEB STA Y=866 AT PAX CABIN WAS REPAIR PER B717-200 SRM-53-00-55-2R-4 FIG. 214, LH CUSP WEB STA Y=841 WAS ATTENDED WITH NRC 00754. (LP 0513035)

Part: SKIN — GOUGED (ZONE 800) · airframe 62,710 hrs · 44,961 cycles

GOUGE ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00704: EXTERNAL SKIN ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8 PAR 5 FIGURE 204. (LP #0506180)

Part: BEAM — CRACKED (ZONE 800) · airframe 62,710 hrs · 44,961 cycles

CRACK ON BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR. SUMMARY OF NRC 00357: BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL SECTION I PERMANENT. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9510. (LP #0505999)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 62,710 hrs · 44,961 cycles

CRACK ON INBD CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX. SUMMARY OF NRC 00389: CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIGURE 201. MAINTENANCE REQUIREMENTS VISUAL INITIAL NORMAL MAINTENANCE / REPETITIVE NORMAL MAINTENANCE 51-70-10-2R PROCEDURE 2 PAR 4 FIGURE 201 PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30- 10-70 PAGE 14 PAR I. (LP #0502953)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,710 hrs · 44,961 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2). SUMMARY OF NRC 00670: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2) FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP #0501026)

Part: APU — FIRE (ZONE 200) · airframe 62,590 hrs · 44,846 cycles

SHIP 9510 -FIRE- WORKING APU MEL FOR NO START, TECHNICIANS REPLACED FCU AND START FUEL PURGE VALVE. APU WAS RUNNING FOR 15 MINUTES FOR LEAK AND OPS CHECKED WHEN FIRE WARNING ANNUNCIATION SOUNDED. FIRE WAS CONFIRMED, FIRE HANDLE PULLED, BOTTLE DISCHARGED. DUE TO APU ACCESS DOORS OPEN FOR LEAK CHECK, REQUIRED USE OF RAMP FIRE EXTINGUISHER TO PUT OUT FIRE. CORRECTIVE ACTION: REPLACED APU, FIRE DETECTION ASSEMBLY, FIRE BOTTLES, AND FCU. (LP 0395848)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,907 hrs · 44,242 cycles

THE OVERWING EMERGENCY LIGHTS STAY ON. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY REF B717 AMM 33-51. BATTERY WAS CHARGED UP. OPERATIONAL CHECK IS GOOD. (LP #5478322)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,301 hrs · 43,714 cycles

BOTH THE LH & RH FWD OVERWING EXIT FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY AT STA 342R PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5070246)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,356 hrs · 42,894 cycles

WORKING AMDS AA CARD 5310-01436-03B. REPLACED RT SIDE FRAME AT STA 674 ON AMDS AA CARD 5310-01436-03B. (LP #4669550)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,356 hrs · 42,894 cycles

CRACK INDICATION AT OVERWING FRAME TAB STA 674 RT SIDE, MARKED (FLOOR LEVEL). SUMMARY SEE NRC 073-0004:5310-01436-01D/002 00055: REPLACED DAMAGED FRAME ON WC 5310-01436-03B. (LP #2804708)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,356 hrs · 42,894 cycles

LONGERON AT 11R FWD OF FRAME STA 674" REQUIRES REMOVAL FOR ACCESS TO MAKE FRAME REPLACEMENT AT STA. 674". SUMMARY SEE NRC 129-0002:5310-01436-03B/003 00293: COMPLIED WITH ERA 530437-14MA REV ORIG FOR REPAIR OF LONGERON AT 11R FWD OF FRAME STA 674". (LP #2801817)

Part: NONE — NONE · airframe 59,868 hrs · 42,482 cycles

THE AISLE OVERHEAD EMERGENCY LIGHT COVER IS MISSING AT ROW 3. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE. (LP #9677521)

Part: ACCESS PANEL — MISSING (LT WING TE FLAP) · airframe 59,330 hrs · 42,003 cycles

THE LEFT WING INBOARD FLAP IS MISSING THE INSPECTION COVER. MAINTENANCE INSTALLED AN ACCESS COVER.

Part: BATTERY — MISLOCATED · airframe 59,064 hrs · 41,752 cycles

DURING THE SERVICE CHECK, THE EMERGENCY LIGHTS AND CELING EXIT SIGN BETWEEN ROWS 105-19 WERE FOUND TO BE INOPERATIVE. TROUBLE SHOOTING SYSTEM PER B717 FIM 35-50-00 810-801, NARROWED DOWN TO BATTERY PACK B5-120 LOCATED UNDER PNL 222LR AT STA 645R PANEL; NOT LOCATED AT THAT STATION DUE TO WRONG (SUSPECTED) OVHD BIN INSTALLED AT THAT LOCATION. REPLACED THE EMERGENCY LIGHT BATTERY AT SEAT 17 PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #9086068)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 56,096 hrs · 39,045 cycles

AFT CARGO DOOR JAMB HAS HEAVY CORROSION. SUMMARY - NRC 060-0008:5331-2001/019 00359: REPLACED LOWER DOOR PAN REF B717 SRM 53-20-15-2R-7. (LP #1814089)

Part: STRINGER — CORRODED (BS 810-1010 S30) · corrosion level 2 · airframe 55,934 hrs · 38,917 cycles

AFT CARGO BIN STRINGER 30 CORRODED FROM STA 810 TO 1010. NRC 060-0008:5331-2001/002 00221: REPAIRED PER B717 SRM 53-20-05-2R. (LP #1811629)

Part: LONGERON — CORRODED (BS 908-994 L30) · corrosion level 2 · airframe 55,934 hrs · 38,917 cycles

LONGERON 30 CORRODED FROM STA 908 TO STA 994 (MARKED). NRC 060-0008:5331-2001/005 00333: REPAIRED PER B717 SRM 53-20-05 -2R. (LP #1811619)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,771 hrs · 37,941 cycles

THE EMERGENCY LIGHTS LOWER FLOOR SECOND ROW OVERWING ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PACK, PER B717 AMM 33-55. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,291 hrs · 37,500 cycles

THE EMERGENCY EXIT SIGN AT ROW 1 IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, B5-259, PER B717 AMM 33-51. (LP #6521132)

Part: CABLE — MISINSTALLED (TAILCONE) · airframe 53,616 hrs · 36,966 cycles

MAINTENANCE FOUND THE TAILCONE KEVLAR CABLE AND LOOP TO BE INSTALLED INCORRECTLY. THE CABLE WAS RE-INSTALLED IN ACCORDANCE WITH B717 AMM 53-52-03. THE REQUIRED INSPECTION IS COMPLETE. (QC2019). (LP #3465610)

Part: WEB — CORRODED (BS 946-949) · corrosion level 2 · airframe 62,405 hrs · 44,692 cycles

CORROSION ON WEB AT L26 RH TO L25 RH BTW STA Y=946 TO Y=949 APROX (C2). SUMMARY: OF NRC 00664: WEB WAS REPAIRED PER B717 SRM 51-70-10-2R-1 FIG 201. (LP #0136346)

Part: SPOILER — DELAMINATED (LT WING)

DELAMINATED, DENTS AND O/B SPOILER T/E HAS CRACKED RUBBER STRIPS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,571 hrs · 35,546 cycles

THE OVER WING EXIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY AT STA 726 PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 54,236 hrs · 37,446 cycles

SUBJECT AIRCRAFT WAS IN FOR SCHEDULED INSPECTIONS. WHILE ACCOMPLISHING WORKCARD 5530-01048-02, MAINTENANCE REPORTED A QUANTY OF 8 CRACK INDICATIONS AT HOLE LOCATIONS ON THE RH FRONT SPAR FORWARD FLANGE, IMMEDIATELY BELOW ZFS=52.267. ER/A 571576-14AD, ASSOCIATED WITH THIS LOG PAGE, PROVIDES THE AUTHORITY TO ACCOMPLISH REPAIR. DAMAGE TOLERANCE EVALUATION IS REQUIRED PER 8100-9. ASSOCIATED AA 5530-01048 AND ASSOCIATED ER/A 00-571576 WERE ADDED FOR AC 9510. ER/A 571576-14AD REV A IS NOW CURRENT. LOG PAGE #1545629 IS CREATED TO PROVIDE ALL REQUIRED FOLLOW ON ACTION, THIS LP MAY BE CLOSED. (LP #0759153)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,227 hrs · 33,939 cycles

FOUND THE EMERGENCY EXIT SIGN ABOVE THE L1 FLIGHT ATTENDANT SEAT INOPERATIVE. TROUBLESHOT IAW ASM 33-51-0. REPLACED THE CHARGER AND BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (RT SPOILER)

DURING UNSCHEDULED NON ROUTINE CHECK FOUND DELAMINATION ON LOWER SURFACE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,972 hrs · 33,092 cycles

R1 DOOR EMERGENCY LIGHT MISSING THE LENS. REPLACED THE LENS, CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 47,768 hrs · 32,952 cycles

EMERGENCY LIGHT LENS AT THE L1 DOOR HAS FALLEN DOWN. SNAPPED THE LENS INTO THE LIGHT ASSEMBLY.

Part: FRAME — CRACKED (BS 1037) · airframe 47,699 hrs · 32,895 cycles

CRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW ERA 559550.

Part: FRAME — CRACKED (BS 1037) · airframe 47,699 hrs · 32,895 cycles

CRACKED FRAME BS 1037, LONGERON 17L. THE FRAME WAS REPAIRED IAW ERA 559550.

Part: FRAME — CRACKED (BS 1022) · airframe 47,699 hrs · 32,895 cycles

CRACKED FRAME BS 1022, LONGERON 7L. THE FRAME WAS REPAIRED IAW ER/A 559530.

Part: SKIN — CRACKED (BS 1073-1076) · airframe 47,699 hrs · 32,895 cycles

CRACK ON FUSELAGE SKIN BS 1073 TO 1076, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 559529.

Part: SLAT TRACK — CRACKED (NR 5) · airframe 47,699 hrs · 32,895 cycles

CRACKED RT SLAT PANEL NR 2 LOWER SKIN BESIDE SLAT TRACK FITTING NR 5. THE SLAT TRACK FITTING WAS REPAIRED IAW SRM 57-00-00-2R-1.

Part: DOOR FRAME — CRACKED (BS 427) · airframe 47,699 hrs · 32,895 cycles

TWO CRACKS ON THE FWD CARGO DOOR FRAME WEB, LONGERON 27R, BS 427. THE DOOR FRAME WEB WAS REPAIRED IAW SRM 53-00-00-2R-2, FIG 201.

Part: LONGERON — CRACKED (BS 1133) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 2L, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: LONGERON — CRACKED (BS 1133) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 2R, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: LONGERON — CRACKED (BS 1022) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 4 L AT BS 1022. DAMAGED SECTION OF LONGERON WAS REPAIR IAW SRM 53-00-05-2R-2, FIG 201.

Part: LONGERON — CRACKED (BS 1022) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 5L AT BS 1022. DAMAGED SECTION OF LONGERON WAS REPAIR IAW SRM.

Part: ACCESS DOOR — CRACKED (COCKPIT FLOOR) · airframe 47,699 hrs · 32,895 cycles

CRACKED FLOOR PANEL ACCESS 211JF AND 211EF AT COCKPIT. FLOOR PANEL ACCESS WAS REPAIRED PER B717-200 SRM. LP# 0132355

Part: LONGERON — CRACKED (BS 1022) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 6L AT BS 1022. THE LONGERON WAS REPAIRED IAW SRM.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 47,699 hrs · 32,895 cycles

CRACKED STOP FITTING AND WEB ON RT SIDE OF VENTRAL DOOR FRAME. THE STOP FITTING WAS REPLACED IAW SRM.

Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 47,699 hrs · 32,895 cycles

CRACKED NLG DOOR FRAME AT BS 47 LONGERON 27L AND 27R. NLG DOOR FRAME WAS REPAIRED IAW SRM.

Part: SKIN — CRACKED (NLG DOOR AREA) · airframe 47,699 hrs · 32,895 cycles

CRACK ON FUSELAGE SKIN NEAR TO AFT HINGE OF LT AFT NLG DOOR. SKIN WAS REPAIRED IAW SRM.

Part: FORMER — CRACKED (BS 715) · airframe 47,699 hrs · 32,895 cycles

CRACKED RT FORMER ON BS 715 KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM.

Part: SUPPORT — CORRODED (BS 148-218) · airframe 47,699 hrs · 32,895 cycles

CORROSION ON SUPPORTS OF R1 EMERGENCY SLIDE BETWEEN BS 148 TO 218 AT PAX CABIN. THE SUPPORTS WERE REPLACED IAW SRM.

Part: FORMER — CRACKED (BS 679) · airframe 47,699 hrs · 32,895 cycles

CRACKED LT AND RT FORMERS ON BS 679 KEEL BEAM AREA. THE FORMERS WERE REPAIRED IAW SRM.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 47,699 hrs · 32,895 cycles

CRACKED BEAM NR 4 ON FWD EDGE AT FWD SERVICE DOOR R1. THE BEAM WAS REPLACED IAW SRM.

Part: FORMER — CRACKED (BS 694) · airframe 47,699 hrs · 32,895 cycles

CRACKED LT AND RT FORMERS BS 694 KEEL BEAM AREA. THE FORMERS WERE REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 472) · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT CUSP WEB BS 472 BETWEEN RBL 54 TO 60. RT CUSP WEB WAS REPAIRED.

Part: CUSP WEB — CORRODED (BS 387) · airframe 47,699 hrs · 32,895 cycles

CORROSION ON THE RT CUSP WEB BS 387 BETWEEN RBL 54 TO 60. REPAIRED.

Part: CUSP WEB — CORRODED (BS 419) · airframe 47,699 hrs · 32,895 cycles

CORROSION ON THE RT CUSP WEB BS 419 BETWEEN RBL 54 TO 60. RT CUSP WEB WAS REPAIRED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT CUSP WEB STA Y=488 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 216.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT CUSP WEB STA Y=348 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. CUSP WEB WAS REPAIRED PER SRM 53-00-55-23R-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT CUSP WEB STA Y=430 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. RT CUSP WEB STA Y=430 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 219.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON LH CUSP WEB MEMBRANE UPPER/LOWER SURFACE STA Y=865 BTW X=54 TO X=60. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R FIG 215.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT CUSP WEB STA Y=401 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. DAMAGE ON RT CUSP WEB STA Y=401 BETWEEN X=-54 TO X=-60 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 219 AND SRM 51-41-02-OG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON RT GRILL CLIPS ABOVE CUSP WEB MEMBRANE BTW STA Y=484 TO Y=503 (2E/A), Y=517 TO Y=527 (2E/A), Y=572 (1E/A), Y=660 TO Y=679 (2E/A), AND Y=920 (1E/A) X=60 IN REF 5300-2020 (CPAX). CLIPS WERE REPLACED PER SRM 51-41-02-0G AND DWG 5913698 REV "K".

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON LT CUSP WEB MEMBRANE UPPER/LOWER SURFACE STA Y=842 BTW X=54 TO X=60. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R FIG 216.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON LT GRILL CLIPS ABOVE CUSP WEB MEMBRANE BTW STA Y=313 TO Y=503 (4E/A), Y=541 TO Y=560 (2E/A), Y=589 TO Y=617 (2E/A), Y=636 TO Y=674 (3E/A), AND Y=908 TO Y=927 (2/EA) X=60 IN REF 5300-2020. CLIPS WERE REPLACED PER SRM 51-41-05-0G, 51-41-02-0G, AND DWG 5913698 REV K.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON COUNTERSINK ON FUEL TANK ACCESS PLATE 620DT. DUE TO EXCESSIVE DAMAGE BY CORROSION, ACCESS PLATES 620DT IS OUT OF LIMITS. NOT ALLOWED MORE THAN 2 ADJACENTS REPAIRS BUSHINGS AND MAXIMUM 6 PER ACCESS AND FUEL ACCESS PLATE 620DT WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCESS PLATES 520CT AND 520FT. ACCESS PLATE 520CT AND 520FT ARE OUT OF LIMITS AND WERE REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCES PLATE 620CT. ACCESS PLATE 620CT WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR. 5.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,699 hrs · 32,895 cycles

CRACKED WEB ON L1 DOOR OM LONG L11. WEB ON LT DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1 FIGURE 201.

Part: STRUCTURE — WORN (EMERGENCY EXIT) · airframe 47,699 hrs · 32,895 cycles

WORN ON LOWER INTERNAL STRUCTURE RT CORNER AT AFT CABIN EMERGENCY EXIT VENTRAL DOOR. WORN ON LOWER INTERNAL STRUCTURE RT CORNER AT AFT CABIN EMERGENCY EXIT VENTRAL DOOR WAS REPAIRED PER SRM 52-10-02-2R REP 16 OPTION 3.

Part: PAN — CRACKED (L1 DOOR) · airframe 47,699 hrs · 32,895 cycles

CRACKED PAN ON UPPER FWD. PASSENGER ENTRANCE DOOR L1. PAN ON UPPER FWD WAS REPAIRED PER SRM 52-10-02 REPAIR 3 FIG 201.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 47,699 hrs · 32,895 cycles

CORROSION ON FLOORBEAM BS 200, RBL 5 AND BTW RBL 46 TO RBL 56. REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: FITTING — CRACKED (CARGO BAY) · airframe 47,699 hrs · 32,895 cycles

CRACKED LOWER FITTING IN THE AFT CARGO COMPARTMENT. THE FITTING WAS REPLACED IAW DWG 5910157, REV CW, SRM 51-41-01, 51-41-02, AND 51-41-05.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,699 hrs · 32,895 cycles

DAMAGE FLOOR PANELS 211ANF, 211ASF, 211ATF, 211GF, AND 211MF. FLOOR PANEL 211 ANF WAS FABRICATED AND FLOOR PANEL 211 ASF AND 211 ATF WERE REPAIRED PER SRM 53-20-50. FLOOR PANELS 211ANF, 211ASF, 211ATF WERE INSTALLED ON 2040-0057 AND THE COVERS ON COCKPIT FLOOR PANELS WERE REPAIRED ON NRC 517.

Part: WEB — CRACKED (BS 176) · airframe 47,699 hrs · 32,895 cycles

CRACKED WEB LOWER SURFACE BETWEEN BS 176 AND RBL 57 IN THE E & E BAY. REPAIRED IAW SRM 53-00-00-2R, 51-41-02-0G, AND 51-41-05-0G.

Part: ANGLE — CRACKED (BS 986) · airframe 47,699 hrs · 32,895 cycles

CRACKED ANGLE ON AFT/LOWER CORNER OF RT WINDOW RING PAN BS 986. THE ANGLE WAS REPLACED IAW SRM 56-20-02-2R-1, AND DWG 3914137, REV C.

Part: LONGERON — CRACKED (BS 794-813) · airframe 47,699 hrs · 32,895 cycles

CRACKED LONGERON 2R BETWEEN BS 794 AND 813. LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2, 51-41-02-0G, AND 51-41-05-0G.

Part: PAN — CRACKED (BS 636) · airframe 47,699 hrs · 32,895 cycles

CRACKED FWD/LOWER CORNER OF RH WINDOW RING PAN BS 636. REPAIRED IAW SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 737) · airframe 47,699 hrs · 32,895 cycles

CRACKED FWD/UPPER CORNER OF RH WINDOW RING PAN BS 737. REPAIRED IAW SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 832-927) · airframe 47,699 hrs · 32,895 cycles

CRACKED AFT/UPPER CORNER OF THE LT WINDOW RING PAN ON BS 927, 870, 851, AND 832. REPAIRED IAW SRM 56-20-02-2R-1.

Part: ANGLE — CRACKED (OVERWING EXIT) · airframe 47,699 hrs · 32,895 cycles

CRACKED ANGLES ON UPPER BEAM FWD & AFT ENDS, AT THE AFT LT OVERWING EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735, REV G.

Part: ANGLE — CRACKED (DOOR BEAM) · airframe 47,699 hrs · 32,895 cycles

CRACKED ANGLE ON THE UPPER BEAM AFT END AT THE FWD RT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-05, 51-41-02, AND DWG 9957735, REV G.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,212 hrs · 32,522 cycles

SECTION OF EMERGENCY LIGHTS IN CEILING INOP AT STA 650. REPLACED BATTERY PACK B5-120 REF B717 AMM 33-51. OPS CHECK GOOD.

Part: LENS — LOOSE (EXIT SIGN) · airframe 46,639 hrs · 32,095 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT THE GALLEY DOOR EMERGENCY EXIT SIGN COVER WAS LOOSE. MAINTENANCE SECURED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,566 hrs · 30,562 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 15-18 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,356 hrs · 30,400 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHTING AT ROW 19 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,144 hrs · 29,496 cycles

DURING LINE CHECK, NOTED COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED BATTERY IN EMERGENCY LIGHT PACK, B5-123 AND TEST OK.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 43,144 hrs · 29,496 cycles

EMERGENCY LIGHT LT SIDE OF CEILING PANEL 1, INOPERATIVE DURING LINE CHECK TEST. REPAIRED CONNECTOR P1-6718 IAW SWPM 20-31-01 AND EMERGENCY LIGHTS TEST OK.

Part: WIRE — DAMAGED · airframe 42,961 hrs · 29,341 cycles

DIVERTED DUE TO MULTIPLE FLIGHT CONTROL WARNINGS; A CONSTANT AUDIBLE "STABILIZER MOTION" WARNING ACCOMPANIED WITH A STICK SHAKER WERE THE KEY INDICATIONS FOLLOWED BY NUMEROUS OTHER FLIGHT CONTROL WARNINGS/MESSAGES. THE FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED SAFELY WITH NO ACFT CONTROL ISSUES. MAINTENANCE FOUND CIRCUIT BREAKER B1-275 FAULTY AND 3 WIRES DAMAGED AT THE LOWER EPCU. WIRES, N1201-16-8C, N1201-13-8C & N1201-10-8C WERE REPLACED AS WELL AS BREAKERS B1-275 & B1-743. ALL FUNCTIONAL CHECK OUTS WERE SATISFACTORY.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,837 hrs · 29,224 cycles

LEFT WW FWD CUT OUT FRAME INBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,837 hrs · 29,224 cycles

TAIL COMPARTMENT AFT LT EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 42,837 hrs · 29,224 cycles

AFT EXIT DOOR UPPER EMER EXIT SIGN LOOSE. SECURED SIGN IAW SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,248 hrs · 28,114 cycles

LEFT OVERWING EMER EXIT LIGHT DAMAGED. R & R LIGHT IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

AFT CARGO COMPARTMENT INTERNAL SKIN CORRODED BETWEEN BS 900 - 908, LONGERON 26R. REPAIRED SKIN IAW SRM & EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

CUSP WEB CRACKED BETWEEN BS 636 - 655, RBL 55. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

LEFT CUSP WEB CRACKED AT STATION 637 - 674. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN CUSP WEB CRACKED BETWEEN BS 812 - 832, BETWEEN RBL 44 - 55. R & R CUSP WEB IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

SKIN CRACKED AT BS 226, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

SEAT TRACK CORRODED AT BS 237, RBL 44. REPAIRED SEAT TRACK IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 157, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, LBL 15. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 157 TO 200, LBL 55. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, LBL 12. R & R SUPPORT IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN MEMBRANE CORRODED AT BS 216, LBL 55. REPAIRED MEMBRANE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 216 TO 242, LBL 17. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

FLOOR SUPPORT CORRODED AT BS 216, BL 0. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 180 TO 200, LBL 7. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, LBL 17. R & R SUPPORT IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 210, RBL 12. R & R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 197) · airframe 41,248 hrs · 28,114 cycles

FOUND THE FLOORBEAM CORRODED AT BS 197, RBL 10 - 55. REPAIRED THE FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 - 44. R & R SUPPORT IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 41,248 hrs · 28,114 cycles

FOUND THE FLOORBEAM CORRODED AT BS 180, RBL 10 - 44. REPAIRED THE FLOORBEAM IAW SRM.

Part: FITTING — CORRODED (BS 177 FLOORBEAM) · airframe 41,248 hrs · 28,114 cycles

FOUND THE FLOORBEAM FITTING CORRODED AT BS 177, RBL 10 - 55. REPAIRED THE FLOORBEAM FITTING IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR CORRODED BETWEEN BS 157 TO 200, RBL 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (BS 157-210) · airframe 41,248 hrs · 28,114 cycles

FOUND THE FLOOR SUPPORT CORRODED BS 157 - 210. REPAIRED THE FLOOR SUPPORT SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 180, RBL 7. R & R SUPPORT IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

RIGHT CUSP WEB CRACKED AT STATION 696. REPAIRED WEB IAW SRM.

Part: CONNECTOR — CORRODED (TAILCONE RELEASE) · airframe 41,248 hrs · 28,114 cycles

AFT ACCESSORY COMPARTMENT TAIL CONE EMER RELEASE HANDLE TRANSMITTER CONNECTOR CORRODED. R & R CONNECTOR IAW SWPM & AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

RIGHT CUSP WEB CORRODED AT STATION 940. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

CUSP WEB CORRODED BETWEEN BS 598 - 617, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

RIGHT CUSP WEB CORRODED AT STATION 440. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

CUSP WEB CORRODED AT BS 674, RBL 45. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

RIGHT CUSP WEB CORRODED AT STATION 598 - 617. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,248 hrs · 28,114 cycles

RIGHT CUSP WEB CORRODED AT STATION 541 - 560. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 41,248 hrs · 28,114 cycles

RIGHT WING INBD SIDE OF INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: DOUBLER — CRACKED (LT WING) · airframe 41,248 hrs · 28,114 cycles

LEFT WING LE INTERIOR DOUBLER CRACKED AROUND NR 2 SLAT INBD TRACK. R & R DOUBLER IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,840 hrs · 29,225 cycles

MAIN CABIN FRAME CRACKED AT BS 696, LONGERON 18R. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,840 hrs · 29,225 cycles

MAIN CABIN FRAME CRACKED AT BS 715, LONGERON 18L. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (BS 696) · airframe 41,248 hrs · 28,114 cycles

A FUSELAGE FRAME WAS FOUND CRACKED AT BS 696, LONGERON 18L. REPAIRED THE FRAME IAW SRM.

Part: FRAME — CRACKED (BS 715) · airframe 41,248 hrs · 28,114 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 715, LONGERON 18L. REPAIRED THE FRAME IAW SRM.

Part: DOUBLER — CRACKED (LT WING) · airframe 41,248 hrs · 28,114 cycles

LEFT WING LE INTERIOR SKIN DOUBLER CRACKED AT NR 3 SLAT. R & R SKIN IAW SRM & DWG.

Part: FRAME — CRACKED (BS 696) · airframe 41,248 hrs · 28,114 cycles

A FUSELAGE FRAME WAS FOUND CRACKED AT BS 696, LONGERON 18R. REPAIRED THE FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,840 hrs · 29,225 cycles

MAIN CABIN FRAME CRACKED AT BS 696, LONGERON 18L. R & R FRAME IAW DWG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,892 hrs · 28,554 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 1 TO 4. R & R BATTERY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 41,269 hrs · 28,128 cycles

RIGHT EEPLS LENS COVER MISSING AT ROW 3. INSTALLED COVER IAW SIP.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 40,222 hrs · 27,456 cycles

FWD EEPLS BATTERY PACK LOOSE. R & R BATTERY PACK IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,222 hrs · 27,456 cycles

LT LOUVER CLIP CRACKED ON CANTED FRAME LOWER INBD. R & R CLIP IAW SRM & DRAWING.

Part: SIGN — CRACKED (CABIN) · airframe 40,222 hrs · 27,456 cycles

LT OVERWING LOWER EMERGENCY EXIT SIGN CRACKED. R & R SIGN IAW AMM.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,222 hrs · 27,456 cycles

L1 DOOR INTERNAL STRUCTURE UPPER BEAM DOUBLER CRACKED AT FWD CORNER. REPAIRED DOUBLER IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 40,222 hrs · 27,456 cycles

L1 DOOR INTERNAL STRUCTURE HANDLE MECHANISM INTERCOSTAL APPEARS TO BE CRACKED. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,222 hrs · 27,456 cycles

L1 DOOR INTERNAL STRUCTURE UPPER BEAM DOUBLER CRACKED AT AFT CORNER. REPAIRED DOUBLER IAW SRM.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,222 hrs · 27,456 cycles

L1 DOOR INTERNAL STRUCTURE DOUBLER 2ND FROM TOP BEAM CRACKED AT AFT CORNER. REMOVED DOUBLER IAW SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,670 hrs · 25,881 cycles

AFT F/A FLASHLIGHT INOP. REMOVED AND REPLACED AFT F/A FLASHLIGHT. OPS CHECK OK REF MM 25-60.

Part: DOOR — CRACKED (CARGO BAY)

AFT CARGO COMPARTMENT C-2 DOOR, CRACKED. ACCOMPLISHED COMPARTMENT C-2 DOOR DOUBLER REPAIR PER B717 SRM 52-30-02, 53-20-02 AND 51-10-02.

Part: PRECOOLER — FAILED (RT ENGINE)

SMOKE AND FUMES IN COCKPIT AND CABIN. REPLACED RT ENGINE PRECOOLER, CHECKED GOOD REF AMM 36-13 (FOUND A PLASTIC RESIDUE ON INLET OF PRECOOLER). AFTER INSPECTION, FOUND BAD PRECOOLER. CHECKED GOOD AFTER PRECOOLER CHANGE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

AT FL330 APPROX 80 MI SW OF CLT WHEN CABIN BEGAN TO DEPRESSURIZE AND NUMEROUS ALERTS APPEARED ON STATUS PAGE. ALERTS AS / FOLLOWS: VIA FAIL, DCU FAIL, NR 1 FAIL, ILS NR 1 FAIL, GPS NR 1 FAIL, VOR NR 1 FAIL, CABIN PRESS MAN, CABIN TEMP MAN, CKPT TEMP MAN, FUEL QTY FAIL, GPWS FAIL, CABIN ATT / ALERT DESCENDING THROUGH 11,500 FT. MASKS DID NOT DEPLOY. FOUND CPC NR 2 FAIL. REPLACED NR 2 CPC IAW B717 AMM 21-31. RTS PASSED. REPLACED LEFT PCDU DUE TO POWER INTERRUPTION IAW B717 AMM 24-21. REPLACED BOTH MAIN POWER RELAYS ON LEFT PCDU IAW B717 AMM 24-21. ALL RTS TESTS PASSED.

Part: LANYARD — FRAYED (EVAC SLIDE)

L1 DOOR EMERGENCY SLIDE LANYARD FRAYED. REMOVED AND REPLACED L1 DOOR EMERGENCY SLIDE LANYARD REF AMM 25-61.

Part: PIN — BACKED OUT (CABIN)

LEFT CEILING EMERGENCY LIGHT BETWEEN ROWS 29 & 30 INOPERATIVE. RESECURED PUSHED PIN AT L2-722 QUICK DISCONNECT IAW SWPM 20-31-17. OPS/FUNCTIONAL CHECK NORMAL IAW AMM 33-51-00.

Part: RUB STRIP — CORRODED (RT WING)

RIGHT WING UPPER ACCESS PANEL 620CT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 620CT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200 TO 218, RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 237, LBL 20 TO RBL 20, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 160 TO 200, RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

GALLEY ENTRANCE GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02267IR.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 870, LONG L29L TO L29R, CORROSION. ACCOMPLISHED LONGERON SECTION DOUBLER AND FILLER REPAIR PER B717 SRM 51-41-01 AND B717 SRM 51-41-05.

Part: STRAP — CORRODED (FUSELAGE)

RIGHT AFT WING TO BODY SUPPORT STRAP, STA 851, CORROSION. ACCOMPLISHED WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 246, LONG LBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02267IR.

Part: FITTING — CORRODED (CABIN)

RIGHT CABIN CUSP GRILL CLIP, STA 530, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR WEB AND SUPPORT ANGLE, STA 160 TO 200, LBL 8 TO RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02 AND FLOOR WEB DOUBLER REPAIR STA 160 TO 200, LBL 11 TO RBL 17 PER B717 SRM 51-70-10 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PASSENGER ENTRANCE AREA FLOOR SUPPORT ANGLE, STA 157, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

RIGHT FLOOR WEB AND BRACKET, STA 550, LONG L18R, CORROSION. ACCOMPLISHED BRACKET REPLACEMENT AND WEB DOUBLER REPAIR PER BOEING DWG SG09530003 AND B717 SRM 51-41-02.

Part: SEAL DEPRESSOR — CORRODED (CARGO BAY)

AFT CARGO DOOR SEAL DEPRESSOR SPLICES, CORROSION. ACCOMPLISHED SEAL DEPRESSOR SPLICES REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

RIGHT FLOOR WEB AND BRACKET STA 515, LONG L18R, CORROSION. ACCOMPLISHED BRACKET REPLACEMENT AND WEB DOUBLER REPAIR PER B717 SRM 51-40-02.

Part: SCUFF PLATE — CORRODED (FUSELAGE)

PASSENGER ENTRANCE AREA SCUFF PLATE METAL STRIP, CORROSION. ACCOMPLISHED SCUFF PLATE METAL STRIP REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 146 TO 200, RBL 56, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-01.

Part: BRACKET — CORRODED (FUSELAGE)

RIGHT FLOOR WEB BRACKET, STA 585, LONG L18R, CORROSION. ACCOMPLISHED FLOOR WEB BRACKET REPLACEMENT PER B717 SRM 51-41-02.

Part: BRACKET — CORRODED (FUSELAGE)

RIGHT FLOOR WEB BRACKET, STA 530, LONG L18R, CORROSION. ACCOMPLISHED FLOOR WEB BRACKET REPLACEMENT PER B717 SRM 51-41-02.

Part: BRACKET — CORRODED (FUSELAGE)

RIGHT FLOOR WEB BRACKET, STA 565, LONG L18R, CORROSION. ACCOMPLISHED FLOOR WEB BRACKET REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 1022 TO 1053, RBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM BLENDING WITHIN LIMITS PER B717 SRM 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 1022 TO 1053, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM BLENDING WITHIN LIMITS PER B717 SRM 51-10-04.

Part: SPLICE — UNKNOWN (CARGO DOOR)

FWD CARGO DOOR SEAL DEPRESSOR SPLICES. ACCOMPLISHED SEAL DEPRESSOR SPLICES REPLACEMENT PER B717 SRM 51-41-01.

Part: VENT — CRACKED (FUSELAGE)

AFT FUSELAGE RIGHT HAND VENT BOX REPAIR IS CRACKED. INSTALLED REPAIR OF AFT FUSELAGE RIGHT SIDE VENT BOX DRAIN PAN IAW T/C 17-5320-0223 FIG 1.

Part: SILL — CORRODED (FUSELAGE)

FWD CARGO PIT DOOR SILL AREA, HAS AREA'S OF SURFACE CORROSION AND CHIPPED/CRACKED PAINT. INSTALLED FWD CARGO DOOR CUTOUT LOWER JAMB PAN REPAIR IAW B717 SRM 53-20-15 REPAIR 6.

Part: FRAME — CRACKED (BS 1178)

AFT FUSELAGE CANTED FRAME AT F/A 1178 CRACKED AT LONGERON 16 LEFT. INSTALLED DOUBLER REPAIR AT LEFT HAND CANTED FRAME AT STA 1178 LONGERON 18L IAW B717 SRM 51-70311 FIG 201 PAGE 203. MATERIAL USED 0.080" 7075-0, 13 X 2.5 INCHES. HEAT TREATED TO T6 IAW AVBORNE G-PS 98PMS.247PS-01 AND SRM 51-32-01.

Part: SKIN — DAMAGED (BS 248 L18L)

FS 248 AT L18L HAS SMOOTH DENT WITH NO INTERNAL DAMAGE, NO LOOSE OR PULLED FASTENERS. MEASURES 2.5 X 2.5 X .048 INCH. CONDITION 2 WITH D/X 52.08. DENT IS ON L18L, PER RES 05-1279 REQUIRES HFEC OR DYE PENATRENT EVERY 500 HRS. INSTALLED DOUBLER REPAIR AT FS 248 AT L18L IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED DOUBLER 2024T3.025 SIZE 23.75 X 17 INCHES, 2024T3.050 SIZE 18 X 14 INCHES, 2024T3.063 SIZE 25 X 4 INCHES.

Part: EEC — FAILED (RT ENGINE)

IN CRUISE AT FL330 .771 M RIGHT ENGINE WENT TO IDLE - ENG R SYS FAIL ILLUMINATED, SELECT FADEC ALT DISPLAY, SELECTED NO CHANGE SHUT ENGINE DOWN. ALL OTHER INDICATIONS NORMAL. EPR INDICATION DISPLAYED A -X-. DIVERTED TO SAV. REMOVED AND REPLACED NR 2 ENGINE ELECTRONIC CONTROL FOR EEC BOX FAULT. PERFORMED RETURN TO SERVICE. OK FOR SERVICE.