N926AT

Part: DOOR — OUT OF ALIGNMENT (NLG) · airframe 59,404 hrs · 43,333 cycles

DIVERTED TO STL DUE TO INTERMITTENT AIRFRAME VIBRATION ABOVE 270KTS, SLOWED TO 250KTS AND VIBRATION STOPPED. FOUND RIGHT NOSE GEAR DOOR GAP MUCH LARGER THAN LEFT NOSE GEAR DOOR GAP, ADJUSTED GAP ON RIGHT DOOR AND PERFORMED PRELOAD CHECK AND FINAL ADJUSTMENT.(7842924)

Part: DOUBLER — CRACKED (ZONE 100) · airframe 58,591 hrs · 42,600 cycles

DOUBLER CRACKED. AFT LOWER CORNER OF AFT CARGO DOOR. MARKED NRC 455. REMOVED EXISTING REPAIR & REPLACED DOUBLER REF B717 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12. AFT CARGO DOOR JAMB EDGE SKIN REP- AIR. (LP #0940824)

Part: WIRE — DAMAGED (ZONE 200) · airframe 58,591 hrs · 42,600 cycles

SEAT EMERGENCY PATH LIGHTS ARE INOPERATIVE. SUMMARY SEE NRC 087-0001:3351-2001/001 00359: REPAIRED WIRE E9405-7-16N REF B717 SWPM 20-10-03. REPLACED POWER SUPPLY AND BATTERY PACK REF B717 AMM 33-51-03 AND CHECKED OPERATION. (LP #0927540)

Part: PUMP — LEAKING (ZONE 100) · airframe 58,508 hrs · 42,517 cycles

SHIP 9573 -ATB- ON ROTATION, THE CREW RECEIVED A "HYD R LO PRESS" MESSAGE AND THE INABILITY TO RETRACT THE GEAR. THEY MOVED THE GEAR SELECTION LEVER DOWN AND RECEIVED THREE GREEN "GEAR SAFE" INDICATIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT, OTHER THAN THE MAIN GEAR DOORS TOUCHING ON ROLL-OUT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP, DAMAGED RIGHT SYSTEM PRESSURE LINES, THE MAIN GEAR ACTUATOR "UP" HYDRAULIC LINE, AND A DAMAGED RIGHT RESERVOIR. AS A PRECAUTION THE PTU, ELECTRIC PUMP, AND ALL ASSOCIATED FILTERS WERE ALSO REPLACED. CYCLED GEAR AND ALL RTS TEST WERE NORMAL. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #6722742)

Part: RESERVOIR — LEAKING (ZONE 100) · airframe 57,940 hrs · 42,047 cycles

SHIP 9573 -MISC- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LOSS AFTER GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE RIGHT HYDRAULIC RESERVOIR WAS LEAKING. THE RESERVOIR WAS REPLACED PER B717 AMM. OPERATION AND LEAK CHECK WAS GOOD. QUANTITY AND PRESSURE ARE NOW NORMAL. (LP #6919675)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,583 hrs · 39,972 cycles

DOOR 1L WILL NOT OPEN FROM INSIDE OR OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SOMETHING IS CATCHING ON THE UPPER SKIN DOOR SEAL AREA. THE UPPER COSETIC PANEL WAS REMOVED TO INSPECTED UPPER SEAL AND ARM ASSIST. THE UPPER GATE SEEMED OUT OF ADJUSTMENT. LUBRICATED DOOR SEAL. CHECKED FORCE NEEDED TO OPEN WITH FORCE GUAGE, MEASURED 38 FTLB ON THE OUTSIDE AND 20 FTLB ON THE INSIDE. BOTH ARE WELL WITHIN LIMITS PER B717 FRMFIM 52-10-00 810-801. A/C IS OK FOR SERVICE. (LP #4418140)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,583 hrs · 39,972 cycles

THE 1L DOOR WOULD NOT OPEN FROM THE OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE LUBRICATED AND ADJUSTED DOOR 1L IAW B717 FRM/FIM 52-10-00 810-801. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR CONTINUED SERVICE. (LP #4418138)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON INTERNAL REPAIR DOUBLERS BTW STA 966/1000 AND BTW STR 28L/25L APROX AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00158: CORROSION LEVEL 2. REPAIR WAS PERFORMED PER PRI 525610-14 REV 2 AND ERA 525610-14 REV A. SECTION II PERMANENT REPAIR. ACCOMPLISH SECTION III WITHIN 24 MONTHS FROM 02JUN23 (726 DAYS 06JUN23) AND REPEAT WITHIN EVERY 24 MONTHS (730 DAYS) THEREAFTER. UNDER LP #2803036. ASSOCIATED ER/A 14-525610 ADDED FOR AC 9573. (LP #2813119)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

AFTER P DOME STIFFENER REMOVAL, 4 HOLE LOCATIONS WERE NOTED TO BE MISSDRILED. IN REF TO NRC 00209. SUMMARY OF NRC 00566: HOLES (4 LOCATIONS) WERE REPAIRED PER PRI 608965-14 REV. 1 AND ER/A 608965-14AD REV. ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2802136)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON CHORD ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00208: CORROSION LEVEL 2. ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH WERE REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #2797307)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH AT CPAX (CPAX). SUMMARY OF NRC 00215: FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-608496 ADDED FOR AC 9573. (LP #2794147)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH AT CPAX (CPAX). SUMMARY OF NRC 00210: FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2794144)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG 1 SHEET 2 ITEM 32. (LP #2794167)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

SEVERE CORROSION ON GALLEY SERVICE DOOR CUSP ANGLE STA 168 TO 201 X=-44 TO X=-60. SUMMARY OF NRC 374: CORROSION LEVEL 2. CUSP ANGLE OF GALLEY SERVICE DOOR STA 168 TO 201 X=-44 TO X=-60 WAS REPAIRED PER PRI 608340-14 REV 1 AND ER/A 608340-14 REV ORIGINAL. (LP #2794160)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00207: CORROSION LEVEL 2. REPAIR ON AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2); WAS PERFORMED PER B717-200 SRM 53-20-08-2R PROCEDURE 7 PAR 5. (A) FIG. 201. (LP #2791807)

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,553 hrs · 39,123 cycles

CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH. (FUS). SUMMARY OF NRC 00300: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH WAS REPAIRED PER PRI 608247-14 REV 1 AND ER/A 608247-14 REV. ORIGINAL. ACCOMPLISH SECTION II: REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR IAW ER/A 608247-14 REV ORIG UNDER LP 2786137. (LP #2786331)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60. SUMMARY OF NRC 00454: CORROSION LEVEL 2. MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2, 51-41-02-0G, AND 51-41-08-0G. (LP #2783928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG.1 SHEET 2 ITEM 32. (LP #2776332)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

REMOVAL CABIN FLOOR SUPORT AT STA Y=148 BTW X=- 44 TO X=- 60, REVEALED CORROSION ON IT, IN REF TO NRC 00454. SUMMARY OF NRC 00565: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=148 BTW X=- 44 TO X=- 60 WAS REPLACED PER B717-200 SRM 53-10-51-01 PROC. 2. (LP #2773853)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148 WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2774007)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

AFTER REMOVAL OF SUPPORT, CORROSION WAS FOUND ON FLOOR SUPORT STA Y=160 BTW RBL 44 TO RBL 54 CABIN PAX (CPAX). SUMMARY OF NRC 00548: CORROSION LEVEL 2. FLOOR SUPPORTS LH STA 201 X=-8 TO X=8 WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2. (LP #2773618)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION WAS FOUND ON FLOOR SUPORT STA Y=180 BTW RBL 44 TO RBL 10 CABIN PAX (CPAX) AFTER REMOVAL OF SUPPORT. SUMMARY OF NRC 00547: CORROSION LEVEL 2. FLOOR SUPORT STA Y=180 BTW RBL 44 TO RBL 10 WAS REPLACED PER B717-200 SRM 53-10-51- 01 PROC 2 AND MUST BE INSTALLED BY NRC 00454. (LP #2770847)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

SEVERE CORROSION ON MAIN ENTRANCE DOOR JAMB WEB STA 200. SUMMARY OF NRC 00372: CORROSION LEVEL 2. DOOR JAMB WEB WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4. (LP #2771772)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON CUSP WEB STA=389 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00424: CORROSION LEVEL 2. CUSP WEB STA=389 RH WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #2768693)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON CUSP WEB STA=370 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00423: CUSP WEB STA=370 RH SIDE AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-41-02-0G PAR 4 AND SRM 53-00-55-2R PAR 5 B (23) FIG 225 REPAIR 4. (LP #2762882)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON CUSP WEB RH STA=650 TO STA=660 PROX. SUMMARY OF NRC 00439: CUSP WEB RH STA=650 TO STA=660 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2762620)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON BEAM #1, STA Y=195 FWD PASSENGER DOOR (L1). SUMMARY OF NRC-00101: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, FIG. 201. AND MEETS REPAIR REQUIREMENTS. MAINTENANCE REQUIREMENTS: PERFORM VISUAL INSPECTION EVERY "C" CHECK PER B717-200 SRM 52-10-02-2R-7 STEP 7 TABLE 202. (LP #2760012)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK ON BEAM #1, STA Y=160 FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00100: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, FIG. 202. AND MEETS REPAIR REQUIREMENTS. MAINTENANCE REQUIREMENTS: PERFORM VISUAL INSPECTION EVERY "C" CHECK PER B717-200 SRM 52-10-02-2R-7 STEP 7 TABLE 202. (LP #2760008)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 620PB RH WING. SUMMARY OF NRC 470: FUEL ACCESS PLATE 620PB DUE TO REPAIR OF WAS NOT POSSIBLE AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR. 5 B. CONDITION II AND WAS REPLACED PER B717 AIPC 57-23-01-01-130J. (LP #2756814)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 520MB LH WING. SUMMARY OF NRC 459: FUEL ACCESS PLATE 520MB WAS NOT POSSIBLE REPAIR AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR 5 B. CONDITION II, AND WAS REPLACED PER B717 AIPC 57-23-01- 01-165J, AND WAS INSTALLED MAGNETIC DRIPLESS FUEL MEASURING STICK HOUSING PER B717 AMM 28-42-01 400-802. (LP #2756866)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

WEAR ON AFT INNER EDGE NEAR OF DOOR LATCH AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00059: INNER PAN AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #2756404)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,553 hrs · 39,123 cycles

CRACK EVIDENCE ON FWD LWR CORNER OF LH WINDOW BELT STA S 851 AND 908 AT PAX CAB. SUMMARY OF NRC 00408: REPAIR WAS PERFORMED PER B717-200 SRM 56-20-02-2R PROCEDURE 1. (LP #2750268)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 54,553 hrs · 39,123 cycles

CORROSION ON FLOOR SUPPORTS X=-8 TO X=8 STA 201. SUMMARY OF NRC 00451: CORROSION LEVEL 2. FLOOR SUPPORT LH STA 201 X=-8 TO X=8 WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2. (LP #2748476)

Part: UNKNOWN — UNKNOWN · airframe 54,378 hrs · 38,976 cycles

THE R1 EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENACE REPLACED THE BATTERY B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4072112)

Part: NONE — NONE · airframe 53,374 hrs · 38,086 cycles

THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-55. (LP #7679774)

Part: NONE — NONE · airframe 53,306 hrs · 38,029 cycles

UPON SERVICE CHECK, THE FIRST CLASS EMERENGCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EMERENGCY LIGHTS BATTERY AT B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OKAY FOR SERVICE. (LP #7679730)

Part: NONE — NONE · airframe 53,089 hrs · 37,839 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT SEAT ROW 20. MAINTENANCE SECURED EXIT ROW SIGN COVER. (LP #2365299)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,271 hrs · 35,356 cycles

THE CEILING EMERGENCY LIGHTS IS OUT AT 16,17,18. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT 17CDE, O/H BIN, PER B717 AMM 33-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY. CHECK WAS GOOD. (LP #7584468)

Part: SIGN — DISLODGED (ROW 19) · airframe 49,980 hrs · 35,130 cycles

THE EXIT SIGN AT RO 19 IS DISLODGED. MAINTENANCE SECURED THE EXIT SIGN. (LP #7446516)

Part: BATTERY PACK — INOPERATIVE (WING LIGHTS) · airframe 49,347 hrs · 34,627 cycles

THE LEFT AND RIGHT FORWARD OVER WING EXIT IDENTIFIER LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY FOR POWER SUPPLY B5-118 BAD AND REPLACED IT, IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,126 hrs · 34,425 cycles

THE EMERGENCY EXIT SIGN AT ROW 1 IS INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY AT B5-259. OPERATIONAL CHECK IS NORMAL, PER B717 AMM 33-54.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,955 hrs · 34,258 cycles

DURING SERVICE CHECK, FOUND 5 EACH EMERGENCY CEILING LIGHTS IN THE AFT SECTION INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-231, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,820 hrs · 34,131 cycles

BOTH FORWARD OVERWING EXIT SIGN LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS GOOD REF B717 AMM 33-55

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 48,279 hrs · 33,642 cycles

CORROSION FOUND AT AFT CARGO DOOR THRESHOLD - MARKED. RCN 067-0008:5331-2001/009 00165: REPAIRED REF B717 SRM 53-20-15-2R PROCED 7. CLOSING REQUIREMENTS RII: INSPECTOR 00664880. (LP #1539185)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,279 hrs · 33,642 cycles

FLOOR SUPPORT IS CORRODED AT STA 196 LBL 52. NRC 068-0011:2531-4006/001 00280: REPLACED SUPPORT REF BOEING DWG #9936534. (LP #1538491)

Part: ENGINE — SURGES (NR 2) · airframe 42,650 hrs · 29,719 cycles

SHIP 9573 - THE CREW EXPERIENCED AN ENGINE SURGE AND HIGH EXHAUST TEMPERATURES WITH THE #2 ENGINE SO THE FLIGHT DIVERTED TO CAE. THE PILOT DID REDUCE POWER ON THE PROBLEM ENGINE SINCE THAT ENGINE DID NOT RECOVER FROM THE SURGE. THE QRH DIRECTED TO SHUTDOWN THE #2 ENGINE. THE FLIGHT DESCENDED TO FL200 AND DECLARED AN EMERGENCY WITH ATC FOR THE DIVERSION. UPON ARRIVAL, MAINTENANCE FOUND METAL IN THE TAILPIPE. CORRECTIVE ACTION: THE #2 ENGINE WAS REPLACED. (LP #3823804)

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 41,848 hrs · 29,151 cycles

EMERGENCY EXIT SIGN COVER LOOSE. SECURED THE SIGN, CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 41,033 hrs · 28,569 cycles

R1 DOOR EXIT LIGHT LENS MISSING. REINSTALLED THE LENS.

Part: SKIN — DAMAGED (RUDDER) · airframe 38,631 hrs · 26,820 cycles

DURING RUDDER INSTALL LOWER LT SKIN WAS CRACKED AND BENT. LOWER LT SKIN WAS REPAIRED IAW SRM 51-70-13, REPAIR 1.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620AT. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION OUT OF LIMITS IN COUNTERSINK, 3 HOLES NON ADJACENT AT FUEL ACCESS DOOR 620JB. FUEL ACCESS DOOR WAS REPAIRED IAW SRM 57-10-01, CONDITION II.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. FUEL ACCESS DOOR REPLACED IAW IPC 57-23-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 520CB. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.

Part: WEB — PUNCTURED · airframe 38,631 hrs · 26,820 cycles

PUNCTURE AT FLOOR WEB, UNDER FLOOR PANEL. WEB WAS REPAIRED IAW 53-00-00, FIG 102.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON UPPER WING SKIN AFT EDGE FROM BS XCW=16 TO XCW=50 AT RT MLG WHEEL WELL. DAMAGE WAS REPAIRED IAW ER/A 545128-14, REV ORIGINAL, AND ETI 17-16-013, REV 2. RII COMPLETED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620DT. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 620DT WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 4 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPAIRED IAW SRM 51-10-01 AND TREATED IAW SRM 51-10-04.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620MB. CORROSION WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 3 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS WAS REPAIRED IAW SRM 51-10-01 AND TREATED IAW SRM 51-10-04.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,631 hrs · 26,820 cycles

CRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14 REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 816-889) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LT CARGO TRACK FROM BS 816 TO 889. CARGO TRACK WAS REPLACED IAW SRM 51-40-08, 51-41-01, 51-10-4.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 38,631 hrs · 26,820 cycles

CRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV. ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 994-1022) · corrosion level 2 · airframe 39,792 hrs · 27,718 cycles

CORROSION ON CARGO TRACK FROM BS 994 - 1022, BETWEEN LONGERONS 27 TO 28R. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-40-08, AND 51-10-04 PAR 15 AND 21.

Part: CARGO TRACK — CORRODED (BS 816-889) · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT CARGO TRACK FROM BS 816 TO 889. RT CARGO TRACK WAS REPLACED IAW SRM 51-41-01.

Part: CARGO TRACK — CORRODED (BS 900-954) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT CARGO TRACK FROM BS 900 TO 954. CARGO TRACK WAS REPLACED IAW SRM 51-41-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620GB. DUE TO EXCESSIVE CORROSION FUEL ACCESS PLATE NR 620GB WAS REPLACED IAW SRM 57-10-01 CONDITION III.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,631 hrs · 26,820 cycles

CRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV ORIGINAL SECTION I.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. OUT OF LIMITS FUEL ACCESS PLATE WAS REPLACED IAW SRM 57-10-01.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 38,631 hrs · 26,820 cycles

CRACKED ZEE ON LOWER LT CORNER AT AFT CABIN BULKHEAD DOOR. DAMAGE ZEE WAS REPLACED FOR NEW 1 IAW SRM 51-41-02.

Part: SKIN — CORRODED (LT WING) · airframe 38,631 hrs · 26,820 cycles

CORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW 10 TO XCW=50 AT LT MLG WHEEL WELL FWD BULKHEAD, SM, CARD 3, ZONE 140. CORROSION WAS REMOVED, MEASURE NDT SPM 04.00.07 PAR 5, FIG 3, SH 1-2, ORIGINAL THICKNESS 0.177" REMAINING THICKNESS 0.157" WITHIN LIMITS IAW SRM 51-10-04, PAR 15, 21, 26 AND SRM 57-10-01 ALLOWABLE 1. FOR GAIN ACCESS WEB AND ANGLE WERE REPAIRED IAW SRM 51-70-11, REPAIR 1 AND REPAIR SRM 51-70-10, REPAIR 1. OLYMPUS NDT 35DL SONOPEN V260SM, 08-DEC-16.

Part: DOUBLER — CORRODED (BS 969) · airframe 38,631 hrs · 26,820 cycles

CORROSION AT PRODUCTION DOUBLER UNDER LONGERON 30, BS 969. REPAIRED IAW ER/A 5451-04-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION OUT OF LIMITS ON FUEL ACCESS PANEL 520CT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 AND IPC 57-22-01-01.

Part: LONGERON — CORRODED (BS 927-1000) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LONGERON 30 BETWEEN BS 927 - 1000 ON AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.

Part: LONGERON — CORRODED (BS 889-927) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LONGERON 30 FROM BS 889 TO 927 AT AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 38,631 hrs · 26,820 cycles

CRACKED UPPER PAN AT RT, FWD OVERWING EMERGENCY EXIT DOOR JAMB. CRACK WAS STOPPED IAW 53-20-15, FIG 201, REP 8. NEW DOUBLER WAS DRILLED IAW 51-40-08. NEW DOUBLER WAS INSTALLED IAW 51-40-02. LENGTH CRACK .265".

Part: SKIN — CRACKED (BS 1086) · airframe 38,631 hrs · 26,820 cycles

CRACK ON FUSELAGE SKIN BS 1086.5, LONGERON 14L. SKIN WAS REPAIRED IAW ETI-17-16-002, REV 2 AND ER/A 545090-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 679) · airframe 38,631 hrs · 26,820 cycles

CRACKED FRAME BS 679, LONGERONSS 25 AND 26R AT KEEL BEAM AREA. FRAME REPAIRED IAW SRM 51-70-11, REP 1.

Part: FRAME — CORRODED (BS 1022) · airframe 38,631 hrs · 26,820 cycles

CORROSION ON FRAME BS 1022 BETWEEN LONGERON 20 RT TO 26 RT AT AFT CARGO COMPARTMENT, C2,SM, CARD 10, ZONE 180. CORROSION WAS REMOVED, REWORKED AREA WAS MEASURED, TREATED, AND PAINTED IAW SRM 51-10-04, PAR 26, 21 AND 5. ORIGINAL THICKNESS: 0.063", REMAINING THICKNESS: 0.056". THEREFORE ITS WITHIN LIMITS IAW SRM 53-00-00, FIG 103. PREVIOUS STRAP ON FRAME WAS REPLACED IAW SRM 53-20-07, FIG 201 AND 51-41-02. EQUIPMENT: OLYMPUS NDT 35DL SONOPEN V-260 SM EXP DATE: 08-DEC-16. RII COMPLETED.

Part: RUB STRIP — BROKEN (FLOOR PANEL) · airframe 38,631 hrs · 26,820 cycles

BROKEN RUBSTRIP ON FLOOR PANEL NR 223. NEW SECTIONS OF RUB STRIPS WERE INSTALLED IAW SRM 51-20-05, 51-10-04 PAR 15 DWG NR 9956320, REV G AND SRM 51-40-08.

Part: LONGERON — CORRODED (BS 889-908) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LONGERON 30 BETWEEN BS 889-908. DAMAGE WAS REPAIRED IAW SRM 53.00.05, REPAIR 3, 2.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON AFTER CARGO DOOR FRAME LOWER AREA. DOOR JAMB WAS REPAIRED IAW SRM 53-20-15, REP 7.

Part: CUSP WEB — CORRODED (BS 851-870) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LT CUSP WEB BS 851 TO BS 870 BETWEEN X=44 AND X=60 AT CPAX IN REF CARD 22, ZONE 000, CARD 87, ZONE 200. CORROSION ON CUSP WEB WAS ATTENDED IAW SRM 51-41-02, 51-41-03, 51-41-05, 5141-01, 51-10-04 PAR 15, 21 AND 37, AND 53-00-55, FIG 215, SHEET 1 OF 9.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 38,631 hrs · 26,820 cycles

DISBONDED AND CRACKED CHANNEL ON FLOOR PANEL NR 222AJF7. CHANNEL ON FLOOR PANEL REPAIRED AND BONDED IAW SRM 53-20-50 FIG 202, 51-20-09, 51-30-08, AND 51-10-4 PAR 15/21.

Part: SEAT TRACK — CORRODED (BS 1022-1065) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON SEAT TRACK X -54.5 BETWEEN BS 1022 AND 1065,. SEAT TRACK WAS REPLACED IAW SRM 51-41-05.

Part: SEAT TRACK — CORRODED (BS 256-340) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT SEAT TRACK X=54 FROM BS 256 TO BS 340 IN REF CARD 14, ZONE 200. CARD 88 ZONE 200. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201, REPAIR 5 CONFIGURATION -7005.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 38,631 hrs · 26,820 cycles

CRACKED FWD INNER FITTINGS ON BEAM NR 1 AT AFT CARGO DOOR. FITTING WAS REPLACED IAW SRM 51-41-05, 51-40-08, 51-10-04, PAR 15/21.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 38,631 hrs · 26,820 cycles

CRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW SRM 53-20-50.

Part: FRAME — CRACKED (BS 679) · airframe 38,631 hrs · 26,820 cycles

CRACKED FRAME BS 679, LONGERON 25 LT AT KEEL BEAM AREA. FRAME WAS REPAIRED IAW 51-70-11, FIG 201. CRACK LENGTH 0.500".

Part: FRAME — CRACKED (BS 694) · airframe 38,631 hrs · 26,820 cycles

CRACKED FRAME BS 694, LONGERON 26 LT AT KEELBEAM AREA. SM, CARD 24, ZONE 140. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02 AND 51-41-05 CRACK LENGTH 0.650".

Part: SEAT TRACK — CORRODED (BS 218) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON SPLICE OF SEAT TRACK X=-56, BS 218. SEAT TRACK SPLICE, X=-56, BS 218 WAS REPLACED IAW SRM 51-40-08 AND DWG 5953059, REV H, SRM 51-40-01.

Part: SEAT TRACK — CORRODED (BS 952-988) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT SEAT TRACK BS 952-988, SEAT TRACK WAS REPLACED IAW SRM 53-20-52, FIG 201, REPAIR 5 AND 51-41-01.

Part: BEAM — CORRODED (BS 427) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER IN BEAM BS 427 BETWEEN LONGERONS 26-27R IN FWD CARGO COMPARTMENT. NEW REPAIR DOUBLERS WERE REPLACED IAW SRM 53-20-15, REA 6, 51-41-02, 51-10-04 PAR 15 AND 21, AND 51-20-09.

Part: CUSP WEB — DAMAGED (BS 551-) · airframe 38,631 hrs · 26,820 cycles

DAMAGE OUT OF LIMITS CUSP WEB, BS 551 X=56 - 60 AT LT AREA OF CABIN PAX. DAMAGE WAS REMOVED IAW IAW SRM 53-00-55, FIG 125. REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 125.

Part: BEAM — CRACKED (L1 DOOR) · airframe 38,631 hrs · 26,820 cycles

CRACK ON BEAM AFT EDGE AND FWD EDGE AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND 202, 51-40-02, 51-40-05, AND 51-10-04. PAR 15 AND 21.

Part: SEAT TRACK — CORRODED (BS 1022-1065) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON SEAT TRACK X=44.5 BETWEEN BS 1022 AND BS 1065. SEAT TRACK WAS REPLACED IAW SRM 53-20-50, FIG 1, 51-41-05, 51-40-08, AND 51-10-04, PAR 15/21.

Part: SEAT TRACK — NOT REPORTED (BS 578) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

SEAT TRACK X=56 AND BS 578 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.

Part: SEAT TRACK — NOT REPORTED (BS 817-870) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

LT SEAT TRACK X=56 FROM BS 817 TO 818 AND 868 TO 870 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,631 hrs · 26,820 cycles

MAINTENANCE DISCOVERED THAT THE RT FORWARD EMERGENCY ESCAPE DOOR HAD A CRACKED CLIP BEHIND THE DOOR STOP. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR CLIP WAS REPLACED IAW SRM 51-41-05 AND DWG 5916159, REV CD.

Part: LONGERON — CRACKED (BS 1133) · airframe 38,631 hrs · 26,820 cycles

CRACK LONGERON 2 LT AND BS 1133 AT AFT ACCESSORY COMPARTMENT. SM, CARD 12, ZONE 310. CRACK LONGERON 2 LT WAS REPAIRED IAW SRM 53-00-05, R2, FIG 201, 51-10-04, PAR 21 AND 14, 51-41-05. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT CUSP WEB X=-57 TO 61 BS 446-465 LOWER SURFACE AT FLOOR STRUCTURE. CFS, SM, CARD 31, ZONE 200. CUSP WEB WAS REPAIRED X=-57 TO 61 BS 446-465 IAW SRM 51-10-4, PAR 26, 53-00-55, FIG 209, AND 51-41-02.

Part: CUSP WEB — CRACKED (BS 665) · airframe 38,631 hrs · 26,820 cycles

CRACK ON LT CUSP WEB BS 665, BETWEEN X=44 AND X=56 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 226, 51-41-02, 51-10-4 PAR 15, 21 AND 37.

Part: LONGERON — CRACKED (BS 1133) · airframe 38,631 hrs · 26,820 cycles

CRACK LONGERON 2 RT AND BS 1133 AT AFT ACCESORY COMAPRTMENT. SM, CARD 13, ZONE 310. CRACK LONG 2 RT WAS REPAIR IAW SRM 53-00-05, FIG 201, R2, 51-10-04, PAR 21 AND 15, 51-41-05. RII COMPLETED.

Part: PAN — CRACKED (BS 237-256) · airframe 38,631 hrs · 26,820 cycles

CRACKED RING PAN BETWEEN BS 237 - 256 AT UPPER, FWD CORNER AREA. RING PAN BETWEEN BS 237-256 WAS REPAIRED IAW SRM 56-20-02, FIG 202.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTED) · airframe 38,631 hrs · 26,820 cycles

PUNCTURED ON FLOOR PANEL NR 222HF. DAMAGE WAS REPAIRED IAW SRM 53-00-00, FIG 102.

Part: PAN — CRACKED (BS 636-655) · airframe 38,631 hrs · 26,820 cycles

CRACKED RING PAN BETWEEN BS 636-655 AT LWR/FWD CORNER AREA. CFS, SM, CARD 23, ZONE 201. RING PAN BETWEEN BS 636-655 WAS REPAIRED IAW SRM 56-20-02, FIG 202.

Part: CUSP WEB — CRACKED (BS 256) · airframe 38,631 hrs · 26,820 cycles

CRACK ON RT CUSP WEB BS 256, X=-49 AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, 51-41-02, FIG 203, REPAIR 4.

Part: WEB — CORRODED (BS 187) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION AT FLOOR WEB BETWEEN BS 194, BS 187 X=53.5, SM, W1, CARD 73, ZONE 200. FLOOR WEB WAS REPAIRED IAW SRM 53-00-00, REPAIR 1, FIG 201, 51-41-02, AND 51-10-04, PAR 37.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT CUSP WEB X=-56 TO 61 BS 465-484 LOWER SURFACE AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 101, 51-41-02, AND 51-10-04, PAR 37. EQUIPMENT PANAMETRICS NDT 35, DATE 25-AUG-16 TRANSDUCER SONOPEN V260SM.

Part: CUSP WEB — PUNCTURED (BS 728) · airframe 38,631 hrs · 26,820 cycles

PUNCTURED LT CUSP WEB BS 728 X=56 AT C PASSENGER STRUCTURE. LEFT CUSP WEB BS 728 X=56 AT CABIN PAX WAS REPAIRED IAW SRM 53-00-00, FIG 102.

Part: WEB — CRACKED (BS 218) · airframe 38,631 hrs · 26,820 cycles

CRACKED WEB BS 218 X=19 AT PAX CABIN IN REF CARD 55, A/C ZONE 200. CARD 82, ZONE 200. WEB WAS REPAIRED IAW SRM 51-70-10, FIG 201, 51-41-05, AND 51-10-4, LENGTH CRACK .125".

Part: CUSP WEB — CORRODED (BS 916-930) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON RT CUSP WEB X=-57 TO 61 FROM BS 916 TO BS 930 AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 51-41-02, 53-00-55, FIG 216, AND 51-10-04, PAR 21, 15 AND 37.

Part: SEAT TRACK — NOT REPORTED (BS 256) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

OUT OF LIMITS, SEAT TRACK X=-44, BS 256. AREA WAS ATTENDED IAW SRM 53-20-52, FIG 201 51-10-04, 51-41-01.

Part: CUSP WEB — CRACKED (BS 674) · airframe 38,631 hrs · 26,820 cycles

CRACK ON RT CUSP WEB X=-44 TO 50, BS 674. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R4 CRACK LENGTH .125.

Part: LONGERON — CORRODED (BS 907-964) · corrosion level 2 · airframe 38,631 hrs · 26,820 cycles

CORROSION ON LONGERON 29L FROM BS 907 TO 964 AT AFT CARGO COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-20-05, 51-40-08, 51-40-08, 51-41-02, 51-41-05, AND 51-10-4 PAR 15, 21.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 37,093 hrs · 25,699 cycles

WHILE PERFORMING OVERWING FRAME INSPECTION AT BS 737. FOUND FLOORBEAM CRACKED THRU UPPER RADIUS. REPLACED FLOORBEAM IAW DWG 5940863-18599. REQUIRED INSPECTION COMPLETED.

Part: PIN — MIGRATED (L1 DOOR SLIDE) · airframe 35,953 hrs · 24,809 cycles

DURING SERVICE CHECK, FOUND L1 DOOR SLIDE PARACHUTE PINS MIGRATED OUT OF POSITION. REPLACED L1 DOOR SLIDE ASSY IAW WC 2561-9004, SB873231. COMPLIED WITH RII INSPECTION IAW TOPP 40-30-05 AND TOPP 40-10-20, RS238849 RII, LP 6620958.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,367 hrs · 24,316 cycles

DURING EMERGENCY LIGHT TEST, FOUND FWD EXIT IDENTIFIER LIGHT WILL NOT STAY ILLUMINATED. REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,209 hrs · 24,186 cycles

DURING SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS FROM ROW 1-12 INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,103 hrs · 24,097 cycles

CREW REPORTED SMOKE IN THE COCKPIT AFTER DEPARTING, ENROUTE. AN EMERGENCY WAS DECLARED AND DIVERTED. EMERGENCY EQUIPMENT MET THE FLIGHT. SMOKE DISSIPATED. MAINTENANCE PERFORMED SMOKE/FUMES INSPECTION IAW AMM 05-52-04 AND FIM 21-22, TASK 809 WITH NO DEFECTS NOTED. A DUCT BURNOUT WAS PERFORMED REF AMM 21-54-00, ALL CHECKED NORMAL. MAINTENANCE REPLACED A FWD GALLEY OVEN DUE TO A STRANGE ODOR WHEN USED.

Part: COVER — LOOSE (TAIL CONE) · airframe 33,849 hrs · 23,085 cycles

TAIL CONE SLIDE PACK COVER LOOSE. INSTALLED COVER IAW CMM.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 33,849 hrs · 23,085 cycles

RIGHT MLG WW DOOR FWD FRAME CRACKED AT UPPER SUPPORT CUT OUT. REPAIRED CUT OUT IAW SRM.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 33,849 hrs · 23,085 cycles

TAIL CONE SLIDE PACK COVER LANYARD LOOSE. SECURED COVER IAW CMM.

Part: FLASHLIGHT — DIRTY (CABIN) · airframe 33,849 hrs · 23,085 cycles

RIGHT AFT LAVATORY AISLE WALL EMERGENCY FLASHLIGHT WELL DIRTY. CLEANED FLASHLIGHT ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,159 hrs · 22,644 cycles

L1 LOWER EMERGENCY EXIT SIGNS INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,159 hrs · 22,644 cycles

R1 LOWER EMERGENCY EXIT SIGNS INOPERATIVE. R & R BATTERY IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,008 hrs · 23,189 cycles

FRAME LOWER FLANGE CORRODED AT BS 1037, BETWEEN LONGERON 30L TO LONGERON 29L. REPAIRED FLANGE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,008 hrs · 23,189 cycles

FRAME CORRODED AT BS 1022, BETWEEN LONGERON 29R TO LONGERON 29L. REPAIRED FRAME IAW SRM.

Part: PANEL — DELAMINATED (R1 DOOR) · airframe 33,159 hrs · 22,644 cycles

R1 DOOR EMERGENCY EVAC SLIDE PANEL DELAMINATED. REPAIRED PANEL IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

FRAME LOWER FLANGE CORRODED AT BS 1022, BETWEEN LONGERON 29R TO LONGERON 29L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

FRAME LOWER FLANGE CORRODED AT BS 1037, BETWEEN LONGERON 30L TO LONGERON 29L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

AFT EMPENNAGE COMPARTMENT CANT FRAME 1178.225, UPPER RT SIDE ANGLE BRACKET CRACKED. REPAIRED ANGLE IAW SRM.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

FORWARD FLOOR STRUCTURE GALLEY MOUNT CORRODED AT BS 218, RBL 11. R & R MOUNT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

CABIN FLOOR SUPPORT STRUCTURE CORRODED AT STATION 200, RBL 10 TO RBL 45. R & R SUPPORT IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT AILERON) · airframe 33,159 hrs · 22,644 cycles

LT WING AILERON HINGE CUTOUT UPPER PANEL SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 33,159 hrs · 22,644 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. R & R FITTINGS IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

AFT EMPENNAGE COMPARTMENT SUPPORT ROD ATTACH FITTINGS CORRODED BETWEEN BS 1145 TO BS 1178, BETWEEN STRINGER 25L TO STRINGER 28L. R & R FITTING IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 33,159 hrs · 22,644 cycles

RIGHT AFT OVERWING EMERGENCY EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 33,159 hrs · 22,644 cycles

RIGHT FWD OVERWING EMERGENCY EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 33,159 hrs · 22,644 cycles

R1 DOOR EMERGENCY EXIT LOWER SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

FORWARD ENTRY DOOR SURROUND FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 160 TO BS 198, LBL 60. R & R SUPPORT IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 33,159 hrs · 22,644 cycles

R1 DOOR UPPER EMERGENCY EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

AFT EMPENNAGE COMPARTMENT SUPPORT ROD ATTACH FITTINGS CORRODED BETWEEN BS 1145 TO BS 1178, BETWEEN STRINGER 21L TO STRINGER 24L. R & R FITTINGS IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 33,159 hrs · 22,644 cycles

L1 DOOR UPPER EXIT SIGN LENS CRACKED. R & R LENS IAW MM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

R1 DOOR SURROUND LOWER CORNER CLOSEOUT STRAP CORRODED AT STATION 200, RBL60. R & R STRAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,159 hrs · 22,644 cycles

AFT EMPENNAGE COMPARTMENT CANT FRAME 1200 RT SIDE, FWD OF ELEC MECHANICAL ACTUATOR VENT BOX ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 33,898 hrs · 23,118 cycles

FAINT ELECTRICAL ODOR WAS COMING FROM FWD COFFEE POTS. PULLED CB`S & ODOR WENT AWAY. CLEANED RESIDUE UNDER COFFEE MAKER & HOT PLATE IAW MM.

Part: LATCH — LOOSE (R1 DOOR) · airframe 32,066 hrs · 21,940 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,446 hrs · 20,288 cycles

FRAME CORRODED AT BS 889, STR 30. REPAIRED FRAME IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,446 hrs · 20,288 cycles

LEFT FUSELAGE SKIN CORRODED BETWEEN BS 851 TO BS 870. REPAIRED SKIN IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 29,446 hrs · 20,288 cycles

C-2 DOOR THRESHOLD PAN, MULTIPLE AREAS CORRODED. REMOVED AND REPLACED THRESHOLD PAN IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 29,446 hrs · 20,288 cycles

C-1 DOOR THRESHOLD PAN, MULTIPLE AREAS CORRODED. REMOVED AND REPLACED THRESHOLD PAN IAW SRM.

Part: COVER — CRACKED (CABIN) · airframe 29,774 hrs · 20,504 cycles

RIGHT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,774 hrs · 20,504 cycles

LEFT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 29,686 hrs · 20,449 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER M/M.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 29,053 hrs · 20,031 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: COVER — MISSING (CABIN)

SEAT 30D EMERGENCY LIGHT COVER MISSING. INSTALLED EMERGENCY LIGHT COVER AT SEAT 30D IAW B717 AMM 33-51. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (APU)

POSSIBLE APU FIRE / BOTH BOTTLES DISCHARGED (APU START AND 250A CB'S IN E&E BAY AND APU CONTROL, Z-39 CB PULLED AND COLLARED) REF: / ITEM 2 OF LOGPAGE 1803139 FOR FIRE BOTTLE REPLACEMENT. PENDING RESOLUTION.

Part: LENS — MISSING (CABIN)

SEAT 10DEF EMERGENCY EXIT LIGHT LENS COVER MISSING ON FWD END OF SEAT, CLEAR LENS. INSTALLED MISSING EMERGENCY EXIT LIGHT LENS COVER ON FWD END OF SEAT 10 DEF IAW B717 AMM 33-51.

Part: PIN — UNSECURE (EVAC SLIDE)

ON PREFLIGHT F/A REPORTED THERE IS NO PIN SHOWING ON THE L1 DOOR WINDOW WHERE THE GAUGE IS AND IF NEEDED THE SLIDE WOULD NOT DEPLOY. REMOVED L1 DOOR SLIDE SECURED PINS AND RE-INSTALLED SLIDE IAW AMM 25-61-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 46 TO RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

CABIN FLOOR PANEL, STA 193 TO 200, RBL 34 TO RBL 35, CORROSION. ACCOMPLISHED FLOOR PANEL DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

CABIN FLOOR PANEL, STA 200, RBL 22 TO RBL 25, CORROSION. ACCOMPLISHED FLOOR PANEL DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, RBL 44.5, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

CABIN FLOOR PANEL, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR PANEL DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 234, LBL 17, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: HINGE — BROKEN (SLIDE COVER)

SLIDE PACK DOOR IS NOT SECURED TO R1 DOOR. HINGE IS BROKEN. REMOVED AND REPLACED R1 SLIDE COVER ASSY REF MM 25-61-02.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT ROWS 1, 2, 3, 10, AND L1/R1 DOOR IDENTIFIERS INOP. REPLACED B5-118 AND OPS GOOD PER AMM 33-51.

Part: SLIDE — UNKNOWN (R1 DOOR)

REMOVED AND REPLACED R-1 DOOR SLIDE. INSTALLED SLIDE DOES NOT HAVE EO 17-2561-294 C/W. REMOVED AND REPLACED R-1 DOOR SLIDE.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB CUTOUT AREA HAS CORROSION STA FROM 954 TO 994. INSTALLED AFT CARGO COMPARTMENT DOOR JAMB LOWER SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIGURE 201. SEE NR 3797, 3829 AND 2382.

Part: DOOR FRAME — CORRODED (BS 370-427)

FWD CARGO DOOR JAMB AREA HAS CORROSION FROM STA 370-427. CUT OUT DAMAGED LOWER SECTION AND INSTALLED NEW LOWER SECTION AND SPLICES, REPAIR PER REF B717 SRM 53-20-15 REPAIR 6.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW TASK CARD 17-5310-2980.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2989.

Part: BATTERY — DEFECTIVE (CABIN)

OVERWING EMERGENCY LIGHTS ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN ARM. REMOVED AND REPLACED EMERGENCY BATTERY SUPPLY FOR EMERGENCY OVERWING LIGHTS. REF 717 AMM 33-51-06. OPS CHECKED GOOD.

Part: PCDU — UNSERVICEABLE (LEFT)

ON TAKEOFF, RECEIVED LT GEN OFF, LOST LT SIDE OF AIRCRAFT NR 3 DU, RESET GEN, WILL NOT RESET. LOST LT DC BUSS. WENT TO EMERGENCY PWR. REMOVED AND REPLACED LEFT PCDU.

Part: BATTERY — FAILED (EMERGENCY LIGHTS)

RIGHT ROW 1 THRU 10 EMERGENCY LIGHTS ON SEATS INOP G2 GALLERY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK/POWER SUPPLY B5-118 IAW AMM 33-51-03 REF WDM 33-51-14, EMERGENCY LIGHTS OPS CHECK GOOD PER 33-51-00.