N998AT

Part: IDG — FAULTED (RIGHT) · airframe 59,349 hrs · 42,860 cycles

SHIP 9547-MISC/DE- ON DESCENT THE CREW RECEIVED A "RT GEN OFF" MESSAGE WITH THE APU ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL RTS TESTS.(7586116)

Part: OIL SYSTEM — LEAKING (APU) · airframe 59,349 hrs · 42,860 cycles

SHIP 9547 OIL FUMES PRESAENT IN COCKPIT AND FORWARS GALLEY WITH APU RUNNING AND LEFT PACK IN AUTO. COCKPIT SMELLED OF FRESH OIL & GALLEY SMELLED OF BURNED POPCORN. CORRECTIVE ACTION: CLEAN AND BURN OUT THE PNEMATIC HIGH PRSSEURE DUCTING PER B717 AMM 21-51. OPERATE THE LEFT AND RIGHT AIR CONDITIONING SYSTEM WITH BOTH ENGINE OPERATING PER B717 AMM 21-00. OPS CK GOOD. (7586100)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 58,361 hrs · 41,984 cycles

FOUND EMERGENCY LIGHTS TO BE INOPERATIVE FOR THE TAILCONE HANDLE RELEASE AND WALKWAY. MAINTENANCE REPLACED B5-260 EMERGENCY LIGHTS BATTERY POWER SUPPLY AND BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7027929)

Part: PAN — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK ON UPPER PAN. ALSO FWD EDGE PAN ON BEAM #2 CRACKED AT LH FWD EMERGENCY EXIT. SUMMARY OF NRC-00781: UPPER PAN AND ALSO FWD EDGE PAN CRACKS ON BEAM #2 AT LH FWD EMERGENCY EXIT WERE REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE 1 REPAIR 1. (LP #0919966)

Part: SKIN — DAMAGED (ZONE 800) · airframe 58,258 hrs · 41,894 cycles

WORN AND BENT ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1. ALSO LOOSE RIVETS ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA). SUMMARY OF NRC 00238: REPAIR DOUBLER OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA) WAS FABRICATED AND REPLACED PER B717-200 SRM 52-10-01-2R-1, PROCEDURE 1, REPAIR 1, FIG 201. (LP #0919666)

Part: PAN — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACK ON INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00139: INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 623951-14 REV ORIGINAL. ASSOCIATED ER/A 14-623951 ADDED FOR AC 9547. (LP #0916072)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ALONG OF LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0255: CORROSION LEVEL 2. LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-40-04-0G, 51-41-01-0G, AND 51-41-05-0G.

Part: REPAIR — MISINSTALLED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

FASTENER DISCREPANT INSTALLATION ON PREVIOUS FUSELAGE SKIN REPAIR, ALSO THERE ARE LIGHTNING STRIKES AT TWO LOCATIONS ADJACENT TO REPAIR FASTENERS AT AFT LH ALTERNATE STATIC PORT AREA BTW STA Y=256-362 AND BTW LONG 26LH-27RH. SUMMARY OF NRC 00664: FASTENER DISCREPANT INSTALLATION ON PREVIOUS FUSELAGE SKIN REPAIR AND LIGHTNING STRIKES AT TWO LOCATIONS ADJACENT TO REPAIR FASTENERS AT AFT LH ALTERNATE STATIC PORT AREA BTW STA Y=256-362 AND BTW LONG 26LH-27RH WERE REPAIRED PER ER/A 590835-14 REV A, SECTION I PERMANENT REPAIR. TIME CONTROLLED ITEMS: SECTION DTE: REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 03-APR-2025. 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. MONITORING LOG PAGE #0902212. ASSOCIATED ER/A 14-590835 ADDED FOR AC 9547. (LP #0903399)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT. SUMMARY OF NRC 0256: CORROSION LEVEL 2. LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PARAGRAPH 8 AND 51-41-02-0G PARAGRAPH 4. (LP #0902246)

Part: SUPPORT — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACKED ON SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00740: SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 FIG 201. (LP #0895966)

Part: VANE — DENTED (ZONE 500) · airframe 58,258 hrs · 41,894 cycles

DENTS ON AFT MOVABLE VANE (LOWER SURFACE) AT LH WING. SUMMARY OF NRC 00468: AFT MOVABLE VANE (LOWER SURFACE) AT LH WING WAS REPAIRED PER ER/A 624886-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV 2. ASSOCIATED ER/A 14-624886 ADDED FOR AC 9547. (LP #0896103)

Part: RETAINER — CRACKED (SLIDING WINDOW) · airframe 58,258 hrs · 41,894 cycles

CRACK WAS FOUND ON RETAINER OF LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00878: CRACK ON RETAINER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ER/A 624944-14 REV ORIG SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624944 ADDED FOR AC 9547. (LP #0891407)

Part: REPAIR — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACKED PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH. SUMMARY OF NRC 00334: PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH, WERE REPLACED PER B717-200 SRM 53-10-14-2R PROCEDURE 2 PAR 5 FIG 201, 51-41-01-0G, 51-41-02-0G PAR 4, AND 51-41-05-0G PAR 8. PERFORM AN EXTERNAL GVI EVERY "C-CHECK" PER B717-200 SRM 53-10-14-2R PROCEDURE 2 PAR 6 TABLE 203. (LP #0884333)

Part: PAN — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACKED INNER PAN OVER BEAM #4 AFT EDGE, AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00171: INNER PAN OVER BEAM #4 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 623968-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623968-14 REV 2. ASSOCIATED ER/A 14-623968 ADDED FOR AC 9547. (LP #0883157)

Part: SKIN — DENTED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

PERFORM REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP. SUMMARY OF NRC 00637: SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP WAS REPAIRED PER ER/A 624583-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624583-14 REV 3. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 19-MAR-2025. 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. AMOC TO AD 2017-01-03, PSE# 53.30.02.13, IS REQUIRED TO BE INCORPORATED FOR CONTINUED SERVICE BEYOND 45,000 TOTAL FLIGHT CYCLES (3,106 CYC UNTIL 45,000 FLIGHT CYCLES) REF ER/A 624583-14AD REV ORIG SEC DTE & AMOC. FOLLOW UP UNDER LOGS 0876966 AND 0877012. ASSOCIATED ER/A 14-624583 ADDED FOR AC 9547. (LP #0881153)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00456: LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP #0878851)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF THE NRC 00284: CORROSION LEVEL 2. END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (UT) THICKNESS MEASURED WAS ACCOMPLISHED AFTER REWORKED AREA ON END-LONGERON BTW STA=994 LONGERON 27RH AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.063IN MINIMUM REMAINING THICKNESS IS 0.010IN THEREFORE AREAS IT IS OUT LIMITS PER B717-200 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 C (2) FIG 103 AND DC-MD/BOEING NDT SPM PART. 4,04 -00-06 PAR 4. FIG 9. PERFORM VISUAL INSPECTION ON NEXT SERVICE PER B717-200 SRM 53-00-00-1A PAR 5 TABLE 101. (LP #0874825)

Part: SUPPORT — CORRODED (ZONE 300) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING. SUMMARY OF NRC 00770: CORROSION LEVEL 2. AREA ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING WAS REPAIRED PER ER/A 619864-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-619864 ADDED FOR AC 9547. (LP #0873255)

Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON CONTACT AREA OF FUEL ACCESS PLATE 620QB. ALSO, CORROSION ON FASTENER HOLES OF PLATE 620JB AT RH WING. SUMMARY OF NRC 00604: CORROSION LEVEL 2. ACCESS PLATE 620JB WAS REPLACED AND VERIFIED FOR A NEW ACCESS PLATE PER B717-200 AIPC 57-23-01-01 ITEM 260J. FUEL ACCESS PLATE 620QB WAS REPAIR PER B717-200 SRM 57-10-01-2R-2. (LP #0870420)

Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PLATES 620GB, 620HB, 620CB, 620FT, 620DB, AND ARB0872-535 AT RH WING WAS FOUND. SUMMARY OF NRC 00602: CORROSION LEVEL 2. FUEL ACCESS DOORS 620FT AND 620DB WERE REPAIRED PER B717-200 SRM 57-10-01-2R PROCEDURE 2. FUEL ACCESS DOOR ARB0872-535 AT RH REPLACED AND VERIFIED PER B717-200 AIPC 57-22-01-01 ITEM 020. FUEL ACCESS DOOR 620HB WAS REPLACED PER B717-200 AIPC 57-23-01-01 ITEM 310J. FUEL ACCESS DOOR 620CB WAS REPLACED PER B717-200 AIPC 57-23-01-01 ITEM 465J. FUEL ACCESS DOOR 620GB WAS REPLACED AND VERIFIED PER B717-200 AIPC 57-23-01-01 ITEM 345J. (LP #0870414)

Part: BARREL NUT — CORRODED (ZONE 300) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON HORIZONTAL STAB BARREL NUTS RH SIDE #13 AND #27. SUMMARY OF NRC 00800: LEVEL CORROSION 2. BARREL NUTS HORIZONTAL STAB RH SIDE #13 AND 27 WERE REPAIRED PER PRI 624606-14 REV 1 & ER/A 624606-14 REV ORIG. SECTION I: PERMANENT REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (12MAR25). 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. PER ERA 624606-14 REV ORIGINAL, UNDER LOG PAGE #0863250. ASSOCIATED ER/A 14-624606 ADDED FOR AC 9547. (LP #0868438)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION ON FLOOR SUPPORTS BTW STA Y=210 TO STA Y=218 X=-11, Y=180 TO STA Y=190 X=-56, STA Y=190 TO STA Y=198 X=54, STA Y=197 X=22 TO X=42 AND STA Y=180 X=-22 TO X=-42, STA X=7RH BTW Y=148-200, IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4. C, FIG 103. SUMMARY OF NRC 00845: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=210 TO STA Y=218 X=-11, Y=180 TO STA Y=190 X=-56, STA Y=190 TO STA Y=198 X=54, STA Y=197 X=22 TO X=42 AND STA Y=180 X=-22 TO X=-42, STA X=7RH BTW Y=148-200 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #0865422)

Part: PAN — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK ON INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00532: INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0864707)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK ON CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00649: CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID CABIN PASSENGER WAS REPAIRED PER B-717-200 SRM 53-00-55-2R REP 4, PAR 5, FIG 212. (LP #0856963)

Part: FRAME — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACK AT FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00638: FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0853086)

Part: FRAME — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0851423)

Part: PAN — CRACKED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

CRACKS ON INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FWD EDGE) AT FWD CARGO DOOR WERE FOUND. SUMMARY OF NRC 00501: INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FWD EDGE) AT FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 7 REPAIR 7, 52-30-02-2R PROCEDURE 3 REPAIR 3, AND PRI 624394-14 REV 1, ERA 624394-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624394 ADDED FOR AC 9547. (LP #0851547)

Part: SKIN — DENTED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

DENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 202 SHEET 1. (LP #0852400)

Part: SKIN — DENTED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

DENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 202 SHEET 1. PERFORM AN EXTERNAL GENERAL VISUAL INSPECTION TO THE REPAIR PERFORMED EVERY 8,000 CYCLES PER B717 SRM 53-10-01-2R PROCEDURE 10 REPAIR 10 STEP 8.A TABLE 202. (LP #0852860)

Part: SKIN — CORRODED (ZONE 100) · airframe 58,258 hrs · 41,894 cycles

-AD- CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG W/W AREA. SUMMARY OF NRC 00670: CORROSION LEVEL 1. CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG WAS REPAIRED PER ER/A 624679-14AD REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 624679-14 REV 2. ASSOCIATED ER/A 14-624679 ADDED FOR AC 9547. (LP #0850795)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00652: CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201 AND (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERON STA 1022 5LH. NO CRACK S WERE FOUND PER DCMD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #0850685)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00794: CRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0847702)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=660-665, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR. 4. A. FIG 101. SUMMARY OF NRC 00831: CORROSION LEVEL 2. CORROSION ON CUSP WEB STA Y=660-665 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #084769)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=777-780, PER B717 SRM 51-10-02-0G PAR 8.F.(1). SUMMARY OF NRC 00832: CORROSION LEVEL 2. RH CUSP WEB STA Y=777-780 WAS REPAIRED PER B717-200 SRM 53-00-55-2R, PROCEDURE 4, REPAIR 4. (LP #0842953)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=389, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR. 4. A. FIG. 101. SUMMARY OF NRC 00830: CORROSION LEVEL 2. THE RH CUSP WEB STA Y=389 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 219. (LP #0841359)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,258 hrs · 41,894 cycles

CRACK ON CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00650: CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 221. (LP #0841317)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,258 hrs · 41,894 cycles

CORROSION OUT OF LIMITS, IN REF TO NRC 0642. CORROSION ON RH CUSP WEB STA Y=262-270, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4. A. FIG 101. SUMMARY OF NRC 00829: CORROSION LEVEL 2. THE RH CUSP WEB STA Y=262-270 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. FIG. 215. (LP #0841398)

Part: SKIN — DENTED (ZONE 800) · airframe 58,258 hrs · 41,894 cycles

PERFORM PERMANENT REPAIR DUE TO DENT ON EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE. SUMMARY OF NRC 00299: EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE WAS REPAIRED PER B717-200 SRM 52-00-01-02R PROCEDURE 8 REPAIR 8 FIGURE 204 PERMANENT REPAIR. PERFORM EXTERNAL VISUAL INSPECTION ON DENTED AREA AT AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE PER B717-200 SRM 52-00-01-02R PROCEDURE 8 REPAIR 8 FIGURE 204 PERMANENT REPAIR, STEP 6 A TABLE 203 AT EVERY C-CHECK. (LP #0813375)

Part: ACCESS DOOR — MISSING (ZONE 500) · airframe 58,258 hrs · 41,894 cycles

-PDA- THE LEFT ELEVATOR LEFT CENTER HINGE NUT ACCESS LOWER DOOR IS MISSING. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED. FWD TO CDL 55-25-01, PLACARD INSTALLED. SUMMARY NRC 00528: NUTS OF ELEVATOR HINGE ACCESS DOORS WERE INSTALLED PER B717 AMM 20-50-01. (LP #6423206)

Part: STRINGER SPLICE — DAMAGED · airframe 57,226 hrs · 41,000 cycles

STR 26L PRODUCTION SPLICE AREA, 1EA FASTENER SHOWS INDICATION WITH VISIBLE DAMAGE TO THE BACKSIDE OF THE STRINGER HOLE-LOCATED FIVE HOLES AFT OF PRODUCTION CUT LINE (MARKED) REF PRI 610260-14 REV 2 STEP 7. SUMMARY SEE NRC 004-0001:10-0653-8-7621/004 00009: COMPLED WITH ER/A 610260-14 REV B. PRI REV. "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 610260-14 REV B PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL FUSELAGE / EXTERNAL SKIN / BELLY / DENTS ER/A 6010268-14 REV B SECTION I: PERMANENT REPAIR INSTRUCTIONS. (LP #0447074)

Part: SKIN — DENTED · airframe 57,226 hrs · 41,000 cycles

C/W ER/A 610260-14 REV B FUSELAGE SKIN DENTS. SUMMARY SEE NRC 004-0001:10-0653-8-7621/002 00006: COMPLIED WITH ER/A 610260-14 REV B. PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 610260-14 REV B. PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL FUSELAGE / EXTERNAL SKIN / BELLY / DENTS ER/A 6010268-14 REV B. SECTION I: PERMANENT REPAIR INSTRUCTIONS.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,223 hrs · 40,996 cycles

THE FLIGHT COMPARTMENT EMERGENCY FLOOD LIGHT, L2-785, DOES NOT ILLUMINATE IN EMERGENCY LIGHT TEST. REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD.

Part: BULB — NO TEST (EMERGENCY LIGHT) · airframe 57,223 hrs · 40,996 cycles

AIRCRAFT 9547, TAIL CONE SLIDE EMER LIGHT L2-941 (MIDDLE BULB OF 3) DOES NOT ILLUM IN EMER LTS TEST. CORRECTIVE ACTION: FOUND EMER LIGHT L2-941 MIDDLE BULB HOLDER LOOSE AND CORRODED. SECURED AND CLEANED HOLDER REF B717 SWPM 20-10-10. (LP 5943933)

Part: SKIN — DAMAGED (BS 954-974) · airframe 57,064 hrs · 40,847 cycles

FUSELAGE SKIN DAMAGED BETWEEN STA 954 AND 974 LONGERON 20L AND 21L. COMPLIED WITH STEPS 1-3 PER RI 618607-14. PERFORMED HFEC PER RI 618607-14 STEP 4 W/ NO DEFECTS NOTED. COMPLIED WITH STEPS 5 & 6 PER RI 618607-14. ADDITIONAL INFORMATION: STEPS 1-3, 5-6 PERFORMED VISUAL INSPECTION, BLENDED DAMAGE PER B717 SRM 53-01-01-1A-1, VISUALLY INSPECTED WITH 10X NO DEFECTS, RESTORED SURFACE AND IDENTIFIED REPAIR PER RI 618607-14. (LP #0379412)

Part: BULB — INOPERATIVE (LANDING LIGHT) · airframe 56,747 hrs · 40,574 cycles

THE LEFT WING LANDING LIGHT WAS REPLACED IN ORD DUE TO BEING INOPERATIVE. UPON ARRIVAL IN MSP, THE LEFT WING LANDING LIGHT BULB (PARTIAL) AND RETAINER RING WAS DISCOVERED TO HAVE DEPARTED THE AIRCRAFT WHILE IN FLIGHT BETWEEN ORD AND MSP. MAINTENANCE IN MSP REPLACED THE LEFT LANDING LIGHT BULB AND RETAINER RING PER B717 AMM 33-41. OPERATIONAL CHECK WAS GOOD. (LP #5288604)

Part: PSEU — FAULTED (MLG) · airframe 56,218 hrs · 40,128 cycles

SHIP 9547 -MISC/DE- DURING THE DEPARTURE CLIMBOUT FROM QRO, THE MLG "UNSAFE" LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE UP POSITION. THE FLIGHT CREW COMPLIED WITH THE QRH, WHICH HAD THEM CYCLE THE LANDING GEAR. THE UP AND LOCKED GEAR POSITION INDICATIONS RETURNED TO NORMAL AFTER CYCLING. UPON ARRIVAL AT ATL, THE PILOT DECLARED AN EMERGENCY WITH ATC DUE TO THE EARLIER GEAR COMPLICATION. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT WAS INSPECTED BEFORE TAXI TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE GEAR PSEU. (LP #5076818)

Part: DOOR FRAME — CORRODED (UNKNOWN) · corrosion level 2 · airframe 56,169 hrs · 40,084 cycles

SEVERAL SPOTS OF CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00033: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R REP. 7. (LP #0155777)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,169 hrs · 40,084 cycles

ELONGATED HOLES AT EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00064: EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 614841-14 REV ORIG. SECTION I: TIME LIMITED REPAIR. ACCOMPLISH PERMANENT REPAIR AT NEXT H-CHECK OR 24 MONTHS WHICHEVER COMES FIRST PER SECTION II OF ERA 614841-14 REVISION ORIGINAL IN REFERENCE LOG PAGE 0154333. ASSOCIATED ER/A 14-614841 ADDED FOR AC 9547. (LP #0155713)

Part: SKIN — DAMAGED (UNKNOWN) · airframe 56,169 hrs · 40,084 cycles

FUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L-26R TO L-28R / ELONGATED HOLES & CORROSION TIME LIMITED. REPAIRED FUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L- 26R TO L-28R / ELONGATED HOLES & CORROSION PER ERA 614841-14 REV ORIGINAL SECTIONI TIME LIMITED REPAIR. TERMINATING ACTION IS REQUIRED AT NEXT H CHECK OR WITHIN 24 MONTHS WHICHEVER OCCURS FIRST. ASSOCIATED ER/A 00-614841 ADDED FOR AC 9547. ADDING DATE OF 12JAN25 TO MASK FOR 730 DAYS AFTER 13JAN23. (LP #0154333)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,139 hrs · 40,061 cycles

ON DOOR CLOSURE AT BLOCKOUT, GATE AGENT FOUND BOTTOM OF DOOR 01L BENT, BOTTOM RIGHT. MAINTENANCE INSPECTED 1L DOOR AND FOUND AFT LOWER EDGE FLANGE RADIUS BENT OUT. PERFORMED REPAIR 3 - DOOR EDGE FLANGE REPAIRS PER SRM 52-00-00-2R PROCEDURE 3. WAS ABLE TO WORK EDGE STRAIGHT. NO CRACKS OR PULLED RIVETS NOTED. NO OTHER DEFECTS PRESENT. (LP #5495776)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,752 hrs · 39,771 cycles

THE EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY PER B717 AMM 33-51. LIGHTS OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #4992178)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,723 hrs · 39,744 cycles

THE EMERGENCY EXIT SIGN ABOVE THE AFT F/A SEAT AND THE TAIL CONE EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 BATTERY FOR THE EMERGENCY LIGHT IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4992152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,669 hrs · 39,698 cycles

FOUND FORWARD DOOR L1 AND R1 DOOR LOWER EXIT SIGNS NOT ILLUMINATED. REPLACED BATTERY PACK AT B5-118 IAW B717 AMM 33-51. (LP #4992105)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,483 hrs · 39,530 cycles

MULTIPLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK, POSITION B5-259, PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4781079)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,375 hrs · 39,442 cycles

THE OVERHEAD EMERGENCY LIGHT ABOVE 29C IS MISSING THE LENS. FORWARD TO MEL 33-51-01A. PLACARD INSTALLED. OK FOR SERVICE. INSTALLED LENS COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #4781003)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,936 hrs · 39,042 cycles

OUTER WINDSHIELD PANE CRACKED AND ARCED IN CRUISE FLIGHT AT FL330. THE QRH WAS COMPLIED WITH AND C/B Z24 WAS PULLED. THE LANDING AT HPN WAS UNEVENTFUL. *** CONTRACT MAINTENANCE EVENT - OCM: 264588 *** RESET C/B Z24. DEFERRED AND PLACARD PER MEL 30-41-01B. 'M' PROCEDURES WERE COMPLIED WITH. MAINTENANCE REPLACED THE F/O WINDSHIELD PER B717 AMM 56-11. MCO AND PLACARD REMOVED. (LP #9963390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,910 hrs · 39,021 cycles

SHIP 9547 -ATB/GEAR/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL FOLLOWING A "RIGHT GEAR DOOR OPEN" INDICATION AND A "RIGHT GEAR UNSAFE" LIGHT ON CLIMB OUT. AN EMERGENCY WAS DECLARED BY THE CREW. THE GEAR POSITION SHOWED GOOD DOWN AND LOCKED INDICATIONS AND THE LANDING AND TAXI TO THE GATE WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED LOOSE AND MISSING HARDWARE ON THE RIGHT GEAR DOOR UP LOCK MECHANISM AND PERFORMED A SUCCESSFUL GEAR EXTENSION AND RETRACTION. (LP #9963368)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,891 hrs · 39,003 cycles

BOTH OVER-WING EMERGENCY EXIT LIGHTS ONLY ILLUMINATE FOR A FEW SECONDS BEFORE GOING OUT. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51-06-401. BOTH OVERWING EMERGENCY LIGHTS NOW WORK CORRECTLY. (LP #9963359)

Part: NONE — NONE · airframe 54,212 hrs · 38,416 cycles

**THIS LOG CREATED TO REPLACE CLOSED IN ERROR LOG #2152236.** EVIDENCE OF LIGHTNING STRIKE AT STA 428 STR 19. INSTALLED TEMPORARY REPAIR DOUBLER PER STEPS 5A, (3A) FIG. 202 (SHEET 19) B717 SRM 53-02-01-2R-1. OK TO CONT ON SRM WITH THE CONDITIONS LISTED ON B717 SRM 52-02-01-2R-1 TABLE 203. (LP #2567498)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,913 hrs · 38,141 cycles

MAINTENANCE FOUND THE EXTERNAL EMERGENCY LIGHTS TO BE INOPERATIVE. DETERMINED THAT THE EXTERNAL EMERGENCY LIGHTS BATTERY WAS INOPERATIVE. THE EXTERNAL EMERGENCY LIGHT BATTERY WAS REPLACED IAW AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 53,919 hrs · 38,147 cycles

THE FORWARD CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THAT THE CABIN EMERGENCY LIGHTS BATTERY AT B10 IS DEAD. THE CABIN EMERGENCY LIGHTS BATTERY AT B10 WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT HAS RETUERNED TO SERVICE.

Part: HINGE — MECHANIC ERROR (RT WING BUTTE) · airframe 56,172 hrs · 40,085 cycles

MSP MISDRILLED A HOLE ON THE RH WING TE OUTBOARD BUTE DOOR HINGE LANDING AT XTE 302.390 WHERE THE SUPPORT ATTACHES TO THE SPAR CAP. REPAIR TO RH WING TE OUTBD BUTE DOOR HINGE ATTACH AT SPAR CAP. SUMMARY: REAR SPAR LOWER CAP OUBOARD BUTE DOOR HINGE LE XTE 302.39 WAS REPAIRED PER PRI 596277-14 REV 2 AND ERA 596277-14 REV B, SECTION II, PERMANENT REPAIR. (LP #2533136)

Part: ANTI-ICE VALVE — FAULTED (NR 1 ENGINE) · airframe 53,616 hrs · 37,878 cycles

SHIP 9547 - ATB - THE CREW RETURNED THE AIRCRAFT TO DTW FOLLOWING A "#1 ENGINE ANTI-ICE" MESSAGE. AN EMERGENCY WAS DECLARED WITH ATC ON APPROACH FOR LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE ENGINE ANTI-ICE PRESSURE VALVE AND THE PRESSURE SWITCH. ALSO PERFORMED AN ENGINE PNEUMATIC HEALTH CHECK AND RETURNED TO SERVICE. (LP #9603400)

Part: NONE — NONE · airframe 53,057 hrs · 37,366 cycles

THE OVERWING EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8574665)

Part: NONE — NONE · airframe 53,050 hrs · 37,361 cycles

CAPT GRIMES LIGHT WIRE FRAYED. SPARKS COMING FROM CONNECTOR. MAINTENANCE REPLACD THE CAPT BRIEFCASE UTILITY SPOT AND FLOOD LIGHT ASSEMBLY. OPERATION IS NORMAL. (LP #8574660)

Part: NONE — NONE · corrosion level 2 · airframe 52,631 hrs · 36,971 cycles

CONTINUATION FROM LP #2271496. CORROSION REMOVAL COMPLIED WITH ON ERA 599949-14. RECEIVED FINAL ERA 599949-14 ORG NO CHANGES. (LP #2271502)

Part: TRUNNION — CORRODED · corrosion level 2 · airframe 52,631 hrs · 36,971 cycles

TRANSFERRED FROM LOG PAGE 8626448. LT MLG FIXED STRUT O/B ATTACH AT TRUNNION FITTING CORRODED ON FWD AND AFT SIDES OF LUG. *******REFER TO NR002 AND LP#8626448**** REMOVED LUG BUSHING AND MACHINED TO REMOVE CORROSION TO 1.475. WITHIN LIMITS PER OVERHAUL MANUAL 57-40-1. INSPT LT MLG FIXED STRUT O/B ATTACH IAW B717 OHM 57-40-1 ITEM 6.C F.P.I. NO ITEMS. (QC1315) FABRICATED OVERSIZE BUSHING, C/W M.P.I OF BUSHING, AND INSTALLED BUSHING PER B717 OHM 57-40-1. (LP #2271496)

Part: TRUNNION — CORRODED · corrosion level 2 · airframe 52,631 hrs · 36,971 cycles

RT MLG FIXED O/B ATTACH AT TRUNNION FITTING CORRODED ON FWD AND AFT SIDES OF LUG. REMOVED LUG BUSHING AND MACHINED TO REMOVE CORROSION TO 1.502. WITHIN LIMITS PER OVERHAUL MANUAL 57-40-1. INSP RT MLG FIXED STRUT O/B ATTACH IAW B717 OHM 57-40-01 ITEM 6-C F.P.I. NO ITEMS (QC1315), FABRICATED OVERSIZED BUSHING, C/W MPI OF BUSHING, AND INSTALLED NEW BUSHING PER B717 OHM 57-40-1. CORROSION WORKED ON ERA 599950-14. RECIEVED FINAL ERA 599950-14 REV ORG. NO CHANGES NOTED. (LP #2270913)

Part: TRUNNION — CORRODED · corrosion level 2 · airframe 52,631 hrs · 36,971 cycles

TRANSFERRED FROM LOG PAGE #8626448. LT MLG FIXED STRUT O/B ATTACH AT TRUNNION FITTING CORRODED ON FWD & AFT SIDES OF LUG. REMOVED LUG BUSHING AND MACHINED TO REMOVE CORROSION TO 1.475. WITHIN LIMITS PER OVERHAUL MANUAL 57-40-01. INSP LT MLG FIXED STRUT O/B ATTACH, FABRICATED OVERSIZED BUSHING, C/W MPI OF BUSHING, AND INSTALLED BUSHING PER B717 OHM 57- 40-01. CORROSION REMOVAL COMPLIED WITH ON ERA 599949-14. RECEIVED FINAL ERA 599949-14 ORG. NO CHANGES NOTED. (LP #2270999)

Part: NONE — NONE · airframe 52,369 hrs · 36,728 cycles

NOTED THE OVERWING EMERGENCY LIGHTS (EXTERIOR) ON BOTH THE LEFT AND RIGHT TO BE INOPERATIVE DURING THE WALKAROUND. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY PER B717 AMM 33-51. (LP #8743217)

Part: NONE — NONE · airframe 52,200 hrs · 36,585 cycles

EVIDENCE OF LIGHTNING STRIKE AT STA 428 STR 19. MAINTENANCE INSTALLED A TEMPORARY REPAIR DOUBLER PER STEPS 5A, (3A) FIG. 202 ( SHEET 19) B717 SRM 53-02-01-2R-1. OK TO CONTINUE ON SRM WITH THE CONDITIONS LISTED ON B717 SRM 52-02-01-2R-1 TABLE 203. (LP #2152236)

Part: NONE — NONE · airframe 51,861 hrs · 36,307 cycles

TAIL SLIDE IS INPROPERLY PACKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE SLIDE PER AMDS 5352-4002. (LP #2072354)

Part: NONE — NONE · airframe 51,861 hrs · 36,307 cycles

REF NRC 276 "WEAR MARKS ON OUTSIDE OF MATING SURFACE TO SLANT PANEL". SMOOTHED 3EA AREAS AND LOWEST READING WAS .092. ORIG MATL THICKNESS IS .125. REMOVED INBOARD SLANT PANEL BRACKET FOR FOM. ROUTED TO SHOP. COMPLIED WITH PRI 596194 -14 REV 0, REV,1, REV 2, REV 3, REV 4, REV 5, REV 6, AND FINAL ERA 596194-14 REV 0. ASSOCIATED ER/A 14-596194 ADDED FOR AC 9547. (LP #2070858)

Part: NONE — NONE · corrosion level 2 · airframe 51,861 hrs · 36,307 cycles

THE R1 DOOR FWD GIRT BAR FITTING IS CORRODED. THE AFT FITTING IS CORRODED AND BENT. SUMMARY SEE NRC 070-0023:5310-2005/003 00274: CLEANED AND CHECKED LIMITS. CORROSION LEVEL 2. REPLACED FLOOR FITTINGS REF BOEING DWG 9936534 AND B717 SRM 51-40-02. (LP #2068598)

Part: NONE — NONE · airframe 51,861 hrs · 36,307 cycles

(LOG 2066142) DURING INSPECTION FOUND FWD ELECTRONIC BAY, DRAIN MAST BASE SHOW SIGNS OF CORROSION. REPAIRED REF B717 SRM 53-01-01 AND B717 DRW # 9923686 .

Part: NONE — NONE · corrosion level 2 · airframe 51,861 hrs · 36,307 cycles

(LOG 2065059) DURING INSPECTION FOUND FWD CARGO DOOR JAMB HAS SEVERAL AREAS WITH SURFACE CORROSION. REPAIRED FWD CARGO DOOR JAMB PER B717 SRM 53-20-15-2R PROCEDURE 6.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,103 hrs · 35,606 cycles

THE EMERGENCY LIGHTS ABOVE THE FWD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235. TEST NORMAL PER B717-AMM 33-51-00 710-801. (LP #1895051)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,676 hrs · 35,236 cycles

EMERGENCY EXIT SIGN AFT OF R1 DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY AT ROW 2CD PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7344171)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,676 hrs · 35,236 cycles

THE EMERGENCY EXIT SIGN FORWARD OF L1 DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY AT ROW 2CD. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #7344170)

Part: BATTERY PACK — CORRODED (EMERGENCY LIGHTS) · airframe 50,447 hrs · 35,062 cycles

THE EMERGENCY LIGHTS WILL NOT TEST FROM THE F/A PANEL. MAINTENANCE REPLACED THE OVERWING EXIT EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. THE OPERATIONAL CHECK IS NOW NORMAL. (LP #7297057)

Part: NONE — NONE · airframe 50,194 hrs · 34,856 cycles

SUPPLEMENTAL INFORMATION - MAINTENANCE COMPLIED WITH ER/A 590042-14 REV ORIG, SEC 1. TIME LIMITED REPAIR. SHIP 9547 - WHILE TAXIING IN PIT AND TRANSITIONING FROM TAXIWAY TO RUNWAY, THE AIRCRAFT EXITED THE HARD SURFACE. THE NOSE GEAR IS OFF OF THE TAXIWAY AND DOWN AN EMBANKMENT. THERE IS FUSELAGE DAMAGE AND BELLY SKIN IS TOUCHING SNOW. NO CUSTOMER INJURIES. PASSENGERS & CREW EXITED THE AIRCRAFT THROUGH THE TAIL CONE ONTO AIRSTAIRS BROUGHT OUT TO THE AIRCRAFT. THE TAIL SLIDE WAS REMOVED BY MAINTENANCE TO ALLOW AIRSTAIR ACCESS. CORRECTIVE ACTION: MAINTENANCE COMPLIED WITH ER/A 590042-14 REV ORIG, SEC 1. TIME LIMITED REPAIR. (LP #1730326)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,750 hrs · 34,484 cycles

THE EMERGENCY EXIT SIGNS ARE INOPERATIVE AT LOCATION 606. MAINTENANCE FOUND THE POWER SUPPLY AND BATTERY AT LOCATION 606 TO BE BAD. REPLACED SAME, PER B717 AMM 33-51. OK FOR SERVICE.

Part: LANYARD — BROKEN (L1 GIRT BAR) · airframe 49,510 hrs · 34,255 cycles

THE 1L GIRT BAR LANYARD WAS DISCOVERED TO BE BROKEN. MAINTENANCE REPLACED THE LANYARD AT 1L DOOR, REF B717 AMM 52-11. NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,718 hrs · 33,521 cycles

THE EMERGENCY LIGHTING CEILING PANELS IN THE PASSENGER COMPARTMENT AT ROW 1 TO ROW 13 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK FOR ROWS 1 TO 13 PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #1534575)

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 48,109 hrs · 33,023 cycles

C-2 DOOR CUT-OUT JAMB AREAS HAVE LIGHT CORROSION ON PAN, SEAL DEPRESSORS, AND AROUND FASTENERS. AREAS MARKED. NRC 001-0306: 5231-2002/001 00169: REPLACED PAN SECTION REF B717 SRM 53-20-15-2R PROCED 7. (LP #1392441)

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 47,786 hrs · 32,787 cycles

FOUND L1 DOOR SLIDE BOTTLE PRESS LOW. REMOVED AND REPLACED LEFT ENTRY DOOR SLIDE PER JOB CARD# 2561- 9004 C/W RII INSP 614338 SLIDE, EVAC, FO OFF 97-2561-9-0003 03160 ON 97-2561-9-0003 02679. (LP5779762)

Part: BATTERY — FAILED (CABIN) · airframe 45,109 hrs · 30,967 cycles

ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT DOORS 1R AND 1L WERE INOPERATIVE. AFTER TROUBLESHOOTING PER FIM 35-50-00, THE BATTERY B5-118 WAS FOUND TO HAVE FAILED. THE BATTERY WAS REPLACED PER AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP 5199717)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,095 hrs · 30,264 cycles

MAINTENANCE FOUND THE AFT EMERGENCY EXIT, OVERWING SIGNS INOPERATIVE. THE POWER SUPPLY BATTERY PACK WAS REPLACED IAW AMM 33-51-03. OPS CHECKED SATISFACTORY.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,352 hrs · 29,737 cycles

CRACK INDICATION BELOW THE LEADING EDGE SKIN SPLICE AT ZFS=51.67, ZFS=50.17, ZFS=49.17 AND ZFS=48.17 OF THE LT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. REPAIRED IAW ETI-17-18-010, REV 1, DWG SG95550005 AND ER/A 566080-14AD, REV. ORIG.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 43,352 hrs · 29,737 cycles

CRACK INDICATION BELOW THE LEADING EDGE SKIN SPLICE AT ZFS=51.67, ZFS=50.17, ZFS=49.17, AND ZFS=48.17 ON THE LT VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE. REPAIRED IAW ETI-17-18-010, REV 1, DWG SG95550005 CONFIGURATION -7005 AND ER/A 566080-14AD REV. ORIG.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION TYPE EXFOLIATION AT CENTER WING TANK UPPER SKIN AT LT MLG WHEEL WELL AREA BELOW SLANT PRESSURE PANELS. THIS NRC WAS ATTENDED WITH ETI-17-18-009 REV 5 AND ER/A 565972-14 REV ORIG. ASSOCIATED ER/A 00-565972.

Part: FITTING — CRACKED (BS 661) · airframe 43,352 hrs · 29,737 cycles

CRACK ON FUSELAGE FITTING LONGERON 22R, BS 661. THE FITTING WAS REPAIRED ETI-17-18-004, REV 1, AND ER/A 565939-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1076) · airframe 43,352 hrs · 29,737 cycles

CRACK ON THE SKIN AT BS 1076 BETWEEN LONGERONS 13L AND 14L. THE SKIN WAS REPAIRED IAW ETI-17-18-002, REV 2 AND ER/A 565871-14, REV ORIGINAL. HFEC INSPECTION WAS PERFORMED THE CRACK WAS FOUND OF 0.110" OF LENGTH IAW NDT SPM 06-10-01.001.

Part: SKIN — CRACKED (BS 1037) · airframe 43,352 hrs · 29,737 cycles

CRACK ON THE FUSELAGE SKIN, BS 1037, LONGERONS 13R AND 14R. THE SKIN WAS REPAIRED IAW ETI-17-18-003, REV 4, AND ER/A 565867-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 696) · airframe 43,352 hrs · 29,737 cycles

CRACK OF 0.250 INCH IN LENGTH APROXIMATELY ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT BS 696 RT. THE FRAME WAS REPLACED IAW 5310-01436-03B.

Part: DOOR — CORRODED · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON LOWER INNER EDGE OF THE FWD AIR STAIRWELL DOOR. THE STAIRWELL DOOR WAS REPLACED IAW AMM 52-63-01.

Part: FRAME — CORRODED (BS 1037) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORRODED FRAME BS 1037, BETWEEN LONGERONS 28L AND 28R IN THE AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, FIG 201.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,352 hrs · 29,737 cycles

CRACKED FRAME ANGLE AT BS 1022, LONGERON 7L. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-008, REV 1, AND ER/A 565874-14, REV ORIGINAL.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,352 hrs · 29,737 cycles

CRACK ON THE FRAME ANGLE BS 1022, BETWEEN LONGERONS 16L TO 17L. CRACK WAS FOUND TO BE 0.750 INCH IN LENGTH. REPLACED THE FRAME ANGLE IAW DWG 9912243, REV JS, SRM 51-41-02, AND 51-41-05.

Part: GRILL — CORRODED · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON FRAME GRILL R1. THE FRAME GRILL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG.201.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,352 hrs · 29,737 cycles

CRACK FOUND ON THE ON THE FRAME ANGLE BS 1022 BETWEEN LONGERONS 13R TO 14R. THE CRACK IS 0.250" LONG. REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON THE ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.

Part: RUB STRIP — CORRODED (RT WING) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORRODED RUB STRIP ON THE RT WING. REPLACED THE RUB STRIP IAW SRM 57-10-01-2R, REP 3, PAR 6.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION POINTS ON FUEL ACCESS PANEL RUB STRIP, LT WING. REPLACED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON THE ACCESS PANEL. REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520DB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON THE ACCESS PANEL 520HB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: CUSP WEB — CRACKED (BS 665-684) · airframe 43,352 hrs · 29,737 cycles

CRACKED CUSP WEB, BS 665 TO 684, LBL 44 TO 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 222.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520FT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5,

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 620EB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 43,352 hrs · 29,737 cycles

DELAMINATED FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R-3.

Part: FORMER — CRACKED (BS 694) · airframe 43,352 hrs · 29,737 cycles

CRACKED EGDE FORMER BS 694 IN THE KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REP 1.

Part: PAN — CRACKED (BS 908) · airframe 43,352 hrs · 29,737 cycles

CRACK ON RING PAN AFT LOWER CORNER BS 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R-1, FIG 202.

Part: FORMER — CRACKED (BS 679) · airframe 43,352 hrs · 29,737 cycles

CRACKED RT EGDE FORMER BS 679 AT THE KEEL BEAM AREA REPAIRED IAW SRM 51-70-11, REP 1.

Part: PAN — CRACKED (BS 446) · airframe 43,352 hrs · 29,737 cycles

CRACK ON RING PAN FWD LOWER CORNER BS 446 . REPAIRED PER B717 SRM 56-20-02-2R-1 FIG 202 . LONG CRACK 0.100" INCH. (LP #0410120)

Part: FLOOR SUPPORT — CORRODED (BS 150-200) · airframe 43,352 hrs · 29,737 cycles

CORROSION ON FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 PAX CABIN IS OUT OF LIMITS (W1) (AMDS 5300-2010). NRC 00453: LEVEL CORROSION 2, FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 WERE REPLACED PER B717 SRM 51-41-02, SRM 51-41-05, AND SRM 51-41-08. (LP #0409155)

Part: FRAME — CRACKED (NLG WW) · airframe 43,352 hrs · 29,737 cycles

CRACKED NOSE LANDING GEAR WHEEL WELL FRAME. REPAIRED IAW SRM 53-10-14-2R, REP 2, FIGURE 201.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,352 hrs · 29,737 cycles

CRACKED PAN 5 BEAM POSITION, ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. PAN 5 BEAM POSITION ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02 FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,352 hrs · 29,737 cycles

CORROSION ON CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 AT CAB PAX (CPAX). CORROSION LEVEL 2. CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 WAS REPAIRED PER SRM 53-00-55-2R-4.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,352 hrs · 29,737 cycles

CRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. CRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 43,352 hrs · 29,737 cycles

PUNCTURE ON CUSP WEB STA Y=696 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2-4 FIG 203. (HFEC) WAS ACCOMPLISHED ON CUSP WEB AT CAB PAX, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10-01.001.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,352 hrs · 29,737 cycles

CRACK ON CUSP WEB BTW STA Y=655 TO Y=674 AND X=54 TO X=60 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206. HFEC INSPECTION WAS PERFORMED ON CUSP WEB AFT CUT OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 43,352 hrs · 29,737 cycles

CRACKED PAN 3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE (PTAS). CRACKED PAN #3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 43,352 hrs · 29,737 cycles

CRACK ON ANGLE AT BEAM 1 AND STA 197 APPROX AT FWD PASSENGER DOOR INT STRUCTURE. BEAM 1 AT FWD PASSENGER DOOR PAN WAS REPAIRED PER SRM 52-10-02-2R PROCEDURE 7 FIG 201.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,352 hrs · 29,737 cycles

CRACK ON CUSP WEB AT STA Y=256 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4- FIG 221. HFEC WAS ACCOMPLISHED ON CUSP WEB, TRIM OUT AREA WAS FOUND AT STA Y=256 AND X=-49 AT CAB PAX AND NO CRACK INDICATION WAS FOUND PER NDTSPM PART 6. 06-10-01.001.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,352 hrs · 29,737 cycles

CRACK ON INTERCOSTAL BTW BEAM 4/5 AND STA 185.0 APROX (L1). INTERCOSTAL WAS REPLACED PER SRM 51-41-02-0G AND DWG 9955763 REV L.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,881 hrs · 29,425 cycles

EMERGENCY EXIT SIGN L2-791 IS INOPERATIVE. TROUBLE SHOT PER WDM 33-51-12 AND FOUND BATTERY PACK AT B5-259 FOR THE EMERGENCY LIGHTS BAD. REPLACED THE SAME PER AMM 33-51. OPERATIONAL CHECK IS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,682 hrs · 29,301 cycles

WHILE PERFORMING SERVICE CHECK, FOUND BOTH EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. INSTALLED A NEW BATTERY IN THE POWER SUPPLY AND FUNCTIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,575 hrs · 26,997 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPS CHECK WAS GOOD.

Part: SKIN — DELAMINATED (SPOILER)

DURING NON ROUTINE MAINTENANCE, CHECK SPOILER FOUND DELAMINATED.

Part: SPAR CAP — NOT REPORTED (VERTICAL STAB) · airframe 38,616 hrs · 26,189 cycles

STABILIZER / VERTICAL / RT SPAR CAP FORWARD FLANGE,ZFS = 49-50 REPAIRED IAW ERA 543293-14.

Part: SLIDE — UNSERVICEABLE (TAILCONE) · airframe 38,626 hrs · 26,194 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. THE SLIDE BECAME UNRAVELED INSIDE THE COVER. AN OUT OF POSITION, MISRIGGED, POOR CONDITION, OR ILL-ARRANGED SLIDE ASSEMBLY COULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYSTEM AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAILCONE SLIDE WAS REPLACED.

Part: SKIN — CRACKED (BS 1133) · airframe 38,616 hrs · 26,189 cycles

AFT FUSELAGE SKIN IS CRACKED, 1.0" AT STA 1133 BETWEEN STR 2RT AND STR 3RT, HFEC -M-. SEE NR FOR ADDITIONAL INFORMATION 001-0219:0593-2005, 012 00102. REPAIRED BY CUTOUT AND INSTALLATION OF DOUBLER. STA LOCATION IAW ENGINEERING IS ACTUALLY BS 1152 NOT BS 1133 AND STATED ON FINAL ER/A 544220-14, REV ORIGINAL. ALL WORK RECORDED ON PRI 544220-14 REV 0 AND COMPLIES WITH FINAL ER/A 544220-14 REV ORIGINAL SECTION I. REPAIR IS CLASSIFIED PERMANENT, MAJOR, WITH RII AND SDR REQUIREMENTS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,365 hrs · 25,998 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,180 hrs · 25,011 cycles

DURING SERVICE CHECK, FOUND AFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (OVERWING LIGHT) · airframe 34,830 hrs · 23,068 cycles

WHILE PERFORMING JC 3351-2001, FOUND OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY INOPERATIVE. REPLACED IAW WC 3351-2001. OPS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,080 hrs · 22,372 cycles

FRAME CORRODED AT BS 889, BETWEEN LONGERON 29L TO LONGERON 19R. REPAIRED FRAME IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 34,079 hrs · 22,370 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 34,079 hrs · 22,370 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,079 hrs · 22,370 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 908, BETWEEN LONGERON 25L TO LONGERON 25R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,079 hrs · 22,370 cycles

FRAME BEAM CRACKED AT BS 715, LONGERON 18R. R & R FRAME IAW SB & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,079 hrs · 22,370 cycles

FRAME CORRODED AT BS 974, BETWEEN LONGERON 30L TO LONGERON 29R. REPAIRED FRAME IAW SRM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 33,837 hrs · 22,215 cycles

FWD FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FRAME BEAM CRACKED AT BS 715, LONGRON 18R. R & R FRAME IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FRAME CORRODED AT BS 908, LONGERON 30R. REPAIRED FRAME IAW SRM.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR BOARD 211AQF CRACKED. REPAIRED FLOOR BOARD IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FRAME CORRODED AT BS 889, BETWEEN LONGERON 29L TO LONGERON 29R. R & R FRAME IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

SEAT TRACK CORRODED BETWEEN BS 429 TO BS 431, LBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS 200 BETWEEN LBL 33 TO LBL 45. R & R CHANNEL IAW SRM & DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 200 BETWEEN RBL 6 TO LBL 6. R & R ANGLE IAW DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 200, RBL 46. R & R ANGLE IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

SUPPORT FRAME BRACKET CRACKED AT BS 636 LONGERON 19R. R & R BRACKET IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS 200, BETWEEN STRINGER 45L TO STRINGER 58L. R & R SUPPORT IAW SRM & DRAWING.

Part: FITTING — CORRODED (R1 DOOR) · airframe 33,837 hrs · 22,215 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. R & R FITTING IAW AMM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 33,837 hrs · 22,215 cycles

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

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR BOARD 222AMF DELAMINATED. R & R FLOOR BOARD IAW DRAWING & MM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR BOARD 222AVF DELAMINATED BETWEEN BS 889 TO BS 950, RBL 25. R & R FLOOR BOARD IAW AMM & DRAWING.

Part: HEAT SHIELD — CRACKED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

PNEUMATIC DUCT HEAT SHIELD CRACKED AT BS 1051 LBL 40. R & R SHIELD IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FLOOR BOARD SUPPORT CHANNEL CORRODED BETWEEN BS 1022 TO BS 1027, LBL 17. R & R CHANNEL IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 33,837 hrs · 22,215 cycles

AFT CARGO COMPARTMENT CARGO TRACK CORRODED AT BS 954, BETWEEN LONGERON 27R TO LONGERON 28R. R & R TRACK IAW SRM.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 33,837 hrs · 22,215 cycles

FWD CARGO DOOR INTERNAL STRUCTURE FOR AFT LOWER STOP PAD, AFT SIDE OF DOOR STUB FRAME, L ANGLE CRACKED. R & R L ANGLE IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 33,837 hrs · 22,215 cycles

FWD CARGO DOOR, FWD SIDE OF DOOR STUB FRAME ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW SRM & DRAWING.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FRAME GUSSET CORRODED AT BS 954, LONGERON 30R. R & R GUSSET IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 33,837 hrs · 22,215 cycles

FWD CARGO DOOR INTERNAL STRUCTURE FWD LOWER STOP PAD, AFT SIDE OF DOOR STUB FRAME ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

FRAME CORRODED AT BS 974, BETWEEN LONGERON 30R TO LONGERON 30L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,837 hrs · 22,215 cycles

SHEAR TIE CORRODED AT BS 908, BETWEEN LONGERON 30L TO LONGERON 29L. R & R SHEAR TIE IAW SRM.

Part: FAIRING — CRACKED (RT HORIZ STAB) · airframe 33,837 hrs · 22,215 cycles

RT HORIZONTAL STABILIZER LOWER BANANA FAIRING AFT FROM LE ON LOWER EDGE CRACKED. REPAIRED FAIRING IAW WO.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 33,021 hrs · 21,682 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MM.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 32,455 hrs · 21,332 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO PUT IN GIRT BAR HOLDER BECAUSE LANYARD IS GETTING STUCK ON GIRT BAR. REMOVED DEBRIS FROM GIRT BAR & LATCH PER AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 32,112 hrs · 21,132 cycles

R1 CATERING DOOR SLIDE PACK COVER IS LOOSE FROM THE DOOR. SECURED SLIDE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,336 hrs · 20,659 cycles

AFT F/A FLASHLIGHT DOES NOT TEST. REMOVED AND REPLACED AFT F/A FLASHLIGHT BATTERY REF AMM.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 30,820 hrs · 20,330 cycles

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

Part: ATTACH FITTING — OBSTRUCTED (GIRT BAR) · airframe 30,134 hrs · 19,871 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HARD TO ENGAGE. CLEANED GIRT BAR ATTACH FITTINGS PER MM.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 30,092 hrs · 19,846 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD FRAYED. REMOVED AND REPLACED LANYARD IAW AMM.

Part: RETAINER — DIRTY (GIRT BAR) · airframe 29,688 hrs · 19,563 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER FAULTY. CLEANED AND LUBED RETAINER PER MM.

Part: HOLDER — DIRTY (GIRT BAR) · airframe 29,616 hrs · 19,526 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO UNARM. CLEANED HOLDER PER MM.

Part: ANGLE — CRACKED (HORIZ STAB)

LEFT STAB LOWER BANANA FAIRING ANGLE, CRACKED. ACCOMPLISHED ANGLE REPLACEMENT PER B717 SRM 51-41-02, 51-20-03, 51-20-09 AND 51-10-04. SEE NR 24325.

Part: SIGN — UNSECURE (CABIN)

EXIT SIGN ON CEILING IN BUSINESS CLASS IS DANGLING BY WIRE (TEMP SECURED). OPEN DEFECT.

Part: GIRT BAR — LOOSE (R1 DOOR)

R1 EVACUATION SLIDE NOT ATTACHED GIRT BAR. RE-SECURED GIRT BAR AS REQUIRED AT R1 DOOR 25-61. (R1 OK FOR SERVICE)

Part: SIGN — BROKEN (CABIN)

EXIT SIGN BROKEN ON CEILING OVER BUSINESS CLASS. RE-SECURED, OK FOR SERVICE REF MM 33 28.

Part: SIGN — BROKEN (CABIN)

FWD EMERGENCY EXIT SIGN IS BROKEN. RE-SECURED SIGN REF MM 33-50, OPS CHECK NORMAL.

Part: LANYARD — UNKNOWN (EVAC SLIDE)

CHECK R1 EMERGENCY SLIDE INTEGRITY (PILOT REQUEST). REMOVED AND REPLACED R1 DOOR SLIDE GIRT BAR LANYARD REF AMM 25-61.

Part: LIGHT — DISCONNECTED (CABIN)

L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND L1 DOOR EMERGENCY EXIT LIGHT WAS DISCONNECTED, CHECKED GOOD IAW AMM 33-51.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SEAT TRACK, STA 200 TO 237, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 53-05 FIG 2F AND EA 17-53-024631R.

Part: DOOR FRAME — CORRODED (CARGO BAY)

FWD CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15.

Part: CUSP WEB — CORRODED (FUSELAGE)

MAIN CABIN SUBFLOOR CUSP LINE WEB, STA 200, RBL 44 TO RBL 22, CORROSION. ACCOMPLISHED SUBFLOOR CUSP LINE WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: STRUCTURE — CRACKED (RT PYLON)

RIGHT PYLON APRON NR 2 HINGE CUT OUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: STRUCTURE — CRACKED (NR 1 PYLON)

LEFT PYLON APRON NR 4 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 4 HINGE CUTOUT AREA, DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: FRAME — CRACKED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: RUB STRIP — CORRODED (FUSELAGE)

AFT FUSELAGE RT LOWER BODY FAIRING PANEL 160SR RUB STRIPS, CORROSION. ACCOMPLISHED RT LOWER BODY FAIRING PANEL 160SR RUB STRIPS REPLACEMENT PER B717 SRM 53-20-70 AND B717 AMM 20-60-20.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 196, LBL 14 TO LBL 28, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 237, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 157, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 24 TO RBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: RUB STRIP — CORRODED (FUSELAGE)

AFT FUSELAGE LOWER BODY FAIRING RUB STRIPS, STA 870 TO 889, CORROSION. ACCOMPLISHED LOWER BODY FAIRING RUB STRIPS REPLACEMENT PER B717 SRM 51-31-00 AND B717 SRM 53-20-70.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, LBL 7 TO RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: CUSP WEB — CORRODED (FUSELAGE)

MAIN CABIN SUBFLOOR CUSP LINE WEB, LBL 7 TO RBL 7, CORROSION. ACCOMPLISHED SUBFLOOR CUSP LINE WEB DOUBLER & FILLER REPAIR PER B717 51-70-10.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2987.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON EMERGENCY LIGHT TEST THE LIGHTS ON SIDE WALLS AT L1-DOOR, R1-DOOR AND THE TWO LIGHTS AT FLOOR ON RT GALLEY AND THE LIGHTS ON SEAT ROWS 1D, 2D, 3D, AND 10D ARE ALL INOPERATIVE. REMOVED & REPLACED BATTERY SUPPLY ASSY AND BATTERY REF AMM 33-51-03, OPS CHECKED GOOD.

Part: SUPPORT — CRACKED (RT VENT BOX)

RIGHT VENT BOX ANGLE SUPPORT IS CRACKED. INSTALLED DOUBLER REPAIR AT RIGHT VENT BOX IAW AIRTRAN T/C 17-5320-2023 FIG 1. MATERIAL USED 0.050 2424 T3 4" X 3".

Part: FRAME — CRACKED (FUSELAGE)

LEFT CANTED FRAME IS CRACKED, AFT FUSELAGE SECTION. INSTALLED REPAIR ON LEFT HAND CANTED FRAME AT STA 1178 BETWEEN LONG 16 AND L17, IAW B717 SRM 51-70-11L. MATERIAL USED FILLER 7075-T6-.071 X 1" DOUBLER 7075.0.080 9" X 1" X 1.25". HEAT TREATED TO 7075-T6.080 PER GPS 98PMS.247PS-01.