N978AT

Part: PUMP — FAULTED (HYD SYSTEM) · airframe 61,929 hrs · 44,625 cycles

THE CREW REPORTED LT HYDRAULIC QTY LOW MESSAGE, FOLLOWED QRH AND LANDED WITH SYSTEM PRESSURE AND QUANTITY. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT RESERVOIR.(7954928)

Part: CONTROL MODULE — FAULTED (TE FLAPS) · airframe 60,123 hrs · 42,983 cycles

SHIP 9543 -FCNT/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE TRAILING EDGE FLAPS BEIN INOPERATIVE ON APPROACH. A NORMAL LANDING WAS ACCOMPLISHED AND NO ISSUES WITH BREAKING DURING ROLLOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FLAP/SLAT CONTROL MODULE. OPERATIONAL CHECK WAS GOOD. (LP #7236704)

Part: PAN — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH. SUMMARY OF NRC 00644: CORROSION LEVEL 2. CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH WAS REPAIRED PER ER/A 623018-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623018-14 REV 1 WITHIN EVERY 3000 FLIGHT CYCLES FROM 42,725 TOTAL AIRCRAFT FLIGHT CYCLES AS OF 24DEC24, PERFORM SECTION II: REPETITIVE INSPECTION PER ER/A 623018-14, REV ORIGINAL, REFER TO LP #0726751. ASSOCIATED ER/A 14-623018 ADDED FOR AC 9543. (LP #0726961)

Part: SUPPORT — CRACKED (ZONE 100) · airframe 59,823 hrs · 42,725 cycles

CRACK ON LH TRACK SUPPORT STA Y=918-915, STA Y=879-876, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00252: LH TRACK SUPPORT STA Y=876 TO 1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R- PROCEDURE 4 REPAIR 4. (LP #0721119)

Part: BEARING — WORN (ZONE 500 FLAP) · airframe 59,823 hrs · 42,725 cycles

WORN BEARING OF FLAP AND ELONGATED HOLES ON OUTB HINGE OF LH FLAP WERE FOUND. SUMMARY OF NRC 00684: OUTB HINGE OF LH FLAP WAS REPAIRED PER ER/A 622136-14 REV ORIG, SECTION I: PERMANENT REPAIR. "DTE" TIME CONTROLLED ITEM WITH LOG PAGE #0701683. ASSOCIATED ER/A 14-622136 ADDED FOR AC 9543. (LP #0717560)

Part: STRUCTURE — CORRODED (ZONE 300) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX WERE REPAIRED PER ER/A 622186-14 REV ORIGINAL & ER/A 622170-14 REV ORIGINAL TIME CONTROLLED ITEMS: DTE CONTROLLED WITH LP 0671037. ASSOCIATED ER/A 14-622170 ADDED FOR AC 9543. (LP #0718929)

Part: STRUCTURE — CORRODED (ZONE 300) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORRODED BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX WERE REPAIRED PER ER/A 622186-14 REV ORIGINAL & ER/A 622170-14 REV ORIGINAL. TIME CONTROLLED ITEMS: DTE CONTROLLED WITH LP #0689020. ASSOCIATED ER/A 14-622186 ADDED FOR AC 9543. (LP #0718927)

Part: STRUCTURE — WORN (ZONE 300) · airframe 59,823 hrs · 42,725 cycles

FOUND WEAR ON BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER. SUMMARY OF NRC 00754: BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER WAS REPAIRED PER ER/A 622465-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 29NOV24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE ANALYSIS (STAGE II AND II) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FACC AC 120-93 REF ER/A 622465-14 REV ORIG DTE SEC. FOLLOW UP UNDER LOG #0691570. ASSOCIATED ER/A 14-622465 ADDED FOR AC 9543. (LP #0718915)

Part: SKIN — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACKS ON EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE. SUMMARY OF NRC 00050: EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE WAS REPAIRED PER ER/A 621926-14 REV ORIG SECTION I PERMANENT REPAIR. TIME CONTROLLED ITEMS: SEC II: ACCOMPLISHED WITHIN EVERY 24 MONTHS AFTER SECTION I REPAIR UNDER LOG PAGE #0706642 PER ER/A 621926-14 REV ORIGINAL.

Part: SKIN — DAMAGED (ZONE 300) · airframe 59,823 hrs · 42,725 cycles

-AD- WEAR AND ELONGATED COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE. SUMMARY OF NRC 00053: COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE WERE REPAIRED PER ERA 621994-14AD REV ORIGINAL. ASSOCIATED ER/A 14-621994 ADDED FOR AC 9543. (LP #0714374)

Part: RETAINER — CRACKED (C/P WINDOW FRAME) · airframe 59,823 hrs · 42,725 cycles

CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00663: CRACK ON INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0707286)

Part: FRAME — WORN (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

WEAR AT FRAME OF STA Y=598 LH SIDE WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00716: FRAME OF STA Y=598 LH SIDE WAS REPAIRED PER ER/A 622297-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622297-14 REV 4. ASSOCIATED ER/A 14-622297 ADDED FOR AC 9543. (LP #0706882)

Part: SKIN — CRACKED (ZONE 300) · airframe 59,823 hrs · 42,725 cycles

ELONGATED HOLES AND CRACKS ON COUNTERSINK OF PANEL 370CR. SUMMARY OF NRC 00658: PANEL 370CR WAS REPAIRED PER ERA 622046-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622046-14 REV 1. ASSOCIATED ER/A 14-622046.

Part: SKIN — CRACKED (ZONE 100) · airframe 59,823 hrs · 42,725 cycles

CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00774: CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, PROCEDURE 12, REPAIR 12, FIG 201. THE REPAIR'S SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 8,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 8,000 CYCLES, PER B717 SRM 53-20-15-2R-12, PAR 7A. (LP #0704180)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON CUSP ANGLE OF FWD SERVICE DOOR JAMB AT FOUR POINTS; THE FIRST ONE, FORWARD OF STA Y=167; THE SECOND ONE, UNDER THE PAN AFT OF STA Y=167; THE THIRD ONE, ALSO UNDER THE PAN FORWARD OF STA Y=200; AND THE FOURTH ONE, AFT OF STA Y=200. SUMMARY OF NRC 00393: CORROSION LEVEL 2. CUSP ANGLE OF FWD SERVICE DOOR JAMB WAS REPAIRED PER PRI 622039-14 REV 2 AND ER/A 622039-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #0695519)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON FLOOR SUPPORTS (8 EA) X=-53.5, BTW STA Y=160 TO Y=200; STA X=44.5, BTW STA Y=160 TO Y=196; STA X=56, BTW STA Y=160 TO Y=196; STA Y=180.5, BTW STA X=13 TO X=38.25; STA Y=196, BTW STA X=15.5 TO X=44.5; STA Y=200, BTW STA X=-7 TO X=-44.5; STA Y=200, BTW STA X=-7 TO X=7; STA Y=200, BTW STA X=7 TO X=14.5, AT FWD PASSENGER CABIN (W1). SUMMARY OF NRC 00764: CORROSION LEVEL 2. FLOOR SUPPORTS (8 EA) X=-53.5, BTW STA Y=160 TO Y=200; STA X=44.5, BTW STA Y=160 TO Y=196; STA X=56, BTW STA Y=160 TO Y=196; STA Y=180.5, BTW STA X=13 TO X=38.25; STA Y=196, BTW STA X=15.5 TO X=44.5; STA Y=200, BTW STA X=-7 TO X=-44.5; STA Y=200, BTW STA X=-7 TO X=7; STA Y=200, BTW STA X=7 TO X=14.5 AT FWD PASSENGER CABIN WERE FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0693866)

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON SEVERAL POINTS OF FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT. SUMMARY OF NRC 00224: CORROSION LEVEL 2. FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, REPAIR 6. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK PER B717-200 SRM 53-20-15-2R-6 REPAIR 6 STEP 7. A. TABLE 203. (LP #0694463)

Part: CUSP WEB — CORRODED (STA Y=200-207) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION WAS FOUND ON LH CUSP ANGLE BTW STA Y=200-207 AT PASSENGER CABIN. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LH CUSP ANGLE BTW STA Y=200-207 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 3. (LP #0690306)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00660: CORROSION LEVEL 2. LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0691470)

Part: FUEL TANK — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

-AD- CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL WELL AREA). SUMMARY OF NRC 00678: CORROSION LEVEL 2. CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL WELL AREA) WAS REPAIRED PER ER/A 622294-14AD REV 0RIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622294-14 REV 2. ASSOCIATED ER/A 14-622294 ADDED FOR AC 9543. (LP #0691465)

Part: WEB — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACK WAS FOUND ON WEB IN STA Y=247 AND X-44.5 APPROX IN AREA OF X-44.5 (MEDIUM) AT STA Y=200 TO STA Y=266 RH SIDE. SUMMARY OF NRC 00671: CRACK ON WEB IN STA Y=247 AND X-44.5 APPROX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 215. (LP #0691502)

Part: CUSP WEB — CRACKED (Y=266, STA X=-44) · airframe 59,823 hrs · 42,725 cycles

CRACKED IN FIVE PLACES OF THE CUSP WEB MEMBRANE AT STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y= 663, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56. SUMMARY OF NRC 00472: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ONLY ON STA Y=663, STA X=-44.5, NO CRACKS WERE FOUND PER DC-MD/ BOEING NDTSPM PART 6, 06-10-01.001 // FOUR PLACES OF THE CUSP WEB MEMBRANE; STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0690164)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX. SUMMARY OF NRC 00738: CORROSION LEVEL 2. CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2, REPAIR 2. (LP #0691024)

Part: CUSP WEB — CORRODED (X=-56 TO X=-60) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX. SUMMARY OF NRC 00739: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR PARAGRAPH 5 B (14) FIG 216. (LP #0689566)

Part: SEAT TRACK — CORRODED (X=44) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON LH SEAT TRACK X=44 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00661: CORROSION LEVEL 2. LH SEAT TRACK X=44 STA Y=200 TO Y=304 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0685816)

Part: CUSP WEB — CRACKED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CUSP WEB LOCATED BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FOUND CRACKED. SUMMARY OF NRC 00647: DUE TO CRACKS, NEW CUSP WEB LOCATED AT BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 226 UNDER NRC 00709. **********FOR INSTALLATION, REFER TO NRC 00393***********. (LP #0685069)

Part: DOOR FRAME — CORRODED (PAX CABIN (L1)) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN (L1). SUMMARY OF NRC 00386: CORROSION LEVEL 2. ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0685066)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON RH SEAT TRACK X=22 BTW STA Y=200-256 IN PASSENGER CABIN. SUMMARY OF NRC 00662: CORROSION LEVEL 2. SEAT TRACK RH X=22 STA Y=200 TO Y=266 WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5, 51-41-01-0G, AND 51-41-05-0G PAR 8. (LP #0679793)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX. SUMMARY OF NRC 0486: CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0678029)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

FOUND RACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00737: CRACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0678225)

Part: SKIN — DENTED (ZONE 100) · airframe 59,823 hrs · 42,725 cycles

DENTS AND NICKS WERE FOUND ON THE EXTERNAL SKIN FLUSH REPAIR STA Y 237 AND BTW LONGERON 17L/18L. ALSO WRONG INSTALLED FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE. SUMMARY OF NRC 00343: PREVIOUS REPAIR ON STA Y 237 AND BTW LONGERON 17L/18L AND WRONG FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE WERE REPLACED PER B717-200 SRM 53-00-01-2R REP 6, 51-41-02-0G, AND 51-41-05-0G. PERFORM VISUAL INSPECTION, INITIAL 8000 CYCLES/LANDINGS AND REPETITIVE EVERY 8000 CYCLES/LANDINGS PER B717 SRM 53-00-01-2R, REPAIR 6, PAR 7, A, TABLE 202. (LP #0674444)

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 59,823 hrs · 42,725 cycles

SEVERAL DENTS ON SKIN OF AFT MOVABLE FLAP VANE GUIDE AT RH WING. SUMMARY OF NRC 00196: AFT RH FLAP VANE WAS REPLACED PER AMDS 2750-4008. (LP #0670862)

Part: FRAME — DENTED (ZONE 100) · airframe 59,823 hrs · 42,725 cycles

DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 634: DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 2, REPAIR 2, FIG. 201. (LP #0670995)

Part: HINGE FITTING — CRACKED (ZONE 600) · airframe 59,823 hrs · 42,725 cycles

CRACKED OUTBOARD LOWER BORE OF FLAP HINGE FITTING #3 AT RH WING. RH OUTBOARD WING FLAP HINGE FITTING WAS REMOVED PER B717-200 AMM 57-55-25 000-803 STEP A TO STEP E (2). RH OUTBOARD WING FLAP HINGE FITTING WAS REPLACED & INSTALLED PER B717-200 AMM 57-55-25 400-803 STEP A TO F 1 (I). (LP #0669690)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX. SUMMARY OF NRC 00406: CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0666517)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX. SUMMARY OF NRC 00405: CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. PERFORM GVI EVERY C-CHECK PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 6. (LP #0662057)

Part: RETAINER — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACK WAS FOUND ON LH CLEARVIEW WINDOW REATINER. SUMMARY OF NRC 00667: UPPER AFT LH CORNER ON LH CLEARVIEW WINDOW RETAINER WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0659031)

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON FLOOR PANELS 221GF & 222MF. SUMMARY OF NRC 00320: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL 221GF & 222MF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED WITHIN LIMITS FOR FLOOR PANEL 221GF. BUT FLOOR PANEL 222MF WAS REPAIRED PER DRAWING TOLERANCES PER B717-200 SRM 51-10-02-0G PAR 8 F, DOUGLAS AIRCRFT COMPANY DWG 9952521 REV BB AND PER B717 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #0659107)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON LH SEAT TRACK STA X=56 AND BTW STA Y=545-548 AT PAX CABIN. SUMMARY OF NRC 00686: CORROSION LEVEL 2. SEAT TRACK ON LH STA X=56 AND BTW STA Y=545 TO 548 AT PAX CABIN WAS REPAIR PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #0660518)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACKS ON UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX. SUMMARY OF NRC 00487: UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX WAS REPAIRED PER ER/A 622035-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 622035-14 REV 1. ASSOCIATED ER/A 14-622035 ADDED FOR AC 9543. (LP #0658954)

Part: VANE — DENTED (ZONE 500 FLAP) · airframe 59,823 hrs · 42,725 cycles

DENT ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS FOUND OUT OF LIMITS DUE TO DISTANCE. SUMMARY OF NRC 00674: AREA BTW XF 85 TO XF 95 ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE TO B717-200 SRM 57-53-01-2R REPAIR 1 PAR 4. (LP #0655649)

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON FLOOR PANEL STRAP AND WEB (LINES BOTTOM FLOOR PANELS) AT LOWER SILL. SUMMARY OF NRC 00456: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL STRAP AND WEB WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED. PANEL STRAP IS WITHIN OF LIMITS BUT WEB IS OUT LIMITS. WEB WAS FABRICATED AND REPLACED PER B717-200 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE, DWG 9957828 REV AB. (LP #0655708)

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CRACK AND CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF. SUMMARY OF NRC 00168: CORROSION LEVEL 2. CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND PANELS EVALUATED. FOUND WITHIN OF LIMITS ON FLOOR PANELS 211PF & 211LF. CRACKS WERE REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1, BUT ON FLOOR PANEL 211AJF IT IS OUT OF LIMITS PER B717-200 SRM 51-10-02-0G, DWG 9957805 REV Y AND DWG 9957802 REV AL. THEREFORE, SKIN OF FLOOR PANEL 211AJF WAS FABRICATED AND REPLACED PER DWG 9957805 REV Y, AND B717 SRM 51-41-02-0G. (LP #0655702)

Part: DOOR — CORRODED (ZONE 800) · corrosion level 2 · airframe 59,823 hrs · 42,725 cycles

CORROSION ON STAIRWELL DOOR. ALSO RUSTED HINGE. SUMMARY OF NRC 00071: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B717 AMM 52-63-01. (LP #0653912)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00381: CRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R, PROCEDURE 4, REPAIR 4. (LP #0650804)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,823 hrs · 42,725 cycles

CRACKS ON LONGERONS 17R, 13R, 12L, AND 13L STA Y 1037 AT C. PAX. SUMMARY OF NRC 00485: (ET) HFEC INSPECTION WAS PERFORMED. CRACK WAS FOUND ON LONG 13R, THE REST NO CRACKS WERE FOUND PER B717 DC/MD NDT SPM PART 6, 06-10-01.001. LONGERON 13R STA Y 1037 AT C. PAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0650305)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,410 hrs · 42,341 cycles

ER/A 610692-14 SECTION II INSPECTIONS. ER/A 610692-14, REV A AT OR PRIOR TO 46,893 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000 FLIGHT CYCLES THEREAFTER ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. AT THE TIME OF THIS LP CREATION, /FOR IAI SHOWS AIRPLANE HAS 42,289 TOTAL FLIGHT CYCLES. THEREFORE INI IS SET TO BE 4,604 FC FROM TODAY'S LP CREATION. ER/A 610692-14, REV A. THIS LP IS TERMINATED. THE LP WAS CREATED DURING THE ER/A REVISION DRAFT AND WAS DETERMINED TO BE INCORRECT DURING ER/A REVISION CHECK AND APROVAL. LP 0486004 WAS CREATED WHICH REPLACES THIS LP 0476508. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 06AUG24 AND LOG COMMENTS. (LP #0476508)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,120 hrs · 40,393 cycles

DAMAGE T: DURING JACK REACTION AND CENTER OF GRAVITY FOR NOSE LANDING GEAR STRUT SEAL REPLACEMENT, CRACK WAS FOUND FROM STA Y=371 TO Y=375 BTW LONG 30 TO LONG 29 RH AT EXTERNAL FUSELAGE SKIN IN REF AMDS 3221-4002. SUMMARY OF NRC 00084: EXTERNAL FUSELAGE SKIN FROM STA Y=371 TO Y=375 BTW LONG 30 TO LONG 29 RH WAS REPAIRED PER PRI 610692-14 REV 3 AND ER/A 610692-14 REV ORIGINAL SECTION I, PERMANET REPAIR. REPAIR APPROVAL IS LIMITED TO 12 MONTHS ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT UNDER LP 2899516. (LP #2901218)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,410 hrs · 42,341 cycles

DTE REQUIRED WITHIN 12 MONTHS OF ER/A 610692-14 ACCOMPLISHMENT ASSOCIATED ER/A 00-610692 ADDED FOR AC 9543. ER/A 610692-14, REV IR. DTE RESTRICTION IS FOR 12 MONTHS OF SERVICE. RTS DATE AT TIME OF REPAIR ACCOMPLISHMENT WAS 10AUG23. THEREFORE, THIS LP IS UPDATED TO EXPIRE ON 09AUG23. ER/A 610692-14, REV A. THIS LP IS TERMINATED PER REVISION A. NEW LP 0486004 IS CREATED TO TRACK STAGE III DTA LIMITS. LOG TERMINATED PER LINE 05 COMMENTS. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 06AUG24 AND LOG COMMENTS. (LP #2899516)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,120 hrs · 40,393 cycles

DENT ON INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING. SUMMARY OF NRC 00104: INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING, WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1 REPAIR 1. (LP #2897695)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,120 hrs · 40,393 cycles

CORROSION ON DOOR JAMB AFT CARGO (C2) STA=954 TO STA=980 APROX. SUMMARY OF NRC 00031: CORROSION LEVEL 2. DOOR JAMB AFT CARGO C2 STA=954 TO STA=980 APROX WAS REPLACED PER B717 SRM 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #2896570)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,841 hrs · 40,141 cycles

SHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIE RELAYS, AND THE RIGHT GENERATOR RELAY. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #4680524)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,832 hrs · 40,134 cycles

SHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIE RELAYS, AND THE RIGHT GENERATOR RELAY. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #4680524)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,590 hrs · 39,906 cycles

12TH HOLE ABOVE ZFS=52.267 HAS CRACK INDICATION ON VERT STAB R /H SIDE REF ERA 560946-14AD REV O AND LOG 0252731. REMOVED VERTICAL STAB L/E PER B717 AMM TASK CARD 55-32-01 00-802. CLEANED AND REINSPECTED 12TH HOLE ABOVE ZFS=52.267 PER ERA 560946-14AD ORIG. NO DEFECTS FOUND. REINSTALLED VERTICLE STAB L/E PER B717 AMM 55-32. LEAK CHECK GOOD FOR RUDDER LIMITER PITOT LINE PER B717 AMM 34-11. HEAT CHECK GOOD PER B717 AMM 30-31. (LP #2727849)

Part: NONE — NONE · airframe 56,298 hrs · 39,664 cycles

ONE CATWALK CEILING EMERGENCY LIGHT IN THE TAIL COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE PSU ASSEMBLY ABOVE THE AFT RIGHT LAVATORY. OPERATIONAL CHECK WAS GOOD. (LP #4026860)

Part: SLIDE — FAILED INSP · airframe 54,771 hrs · 38,309 cycles

THE SERVICE DOOR SLIDE FAILED THE DEPLOYMENT TEST PER FORECAST #95-0525-8-0121 MAINTENANCE REMOVED AND INSTALLED THE FORWARD SERVICE DOOR SLIDE REF WORK CARD 2561- 9005. (LP #9240753)

Part: SKIN — CORRODED · corrosion level 2 · airframe 52,771 hrs · 36,513 cycles

CORROSION ON AFT CARGO SKIN. SUMMARY SEE NRC 105-0008:5331-2001/012 00365: BLENDED AND CHECKED LIMITS IN SKIN PER B717 SRM 53-00-00- 1A. REPLACED SKIN CLIP PER DWG #9912243 AND B717 SRM 51-40-02. (LP #1915089)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,827 hrs · 34,858 cycles

THE EXIT SIGN ABOVE THE FORWARD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT B-5-235, PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,809 hrs · 34,842 cycles

MULTIPLE EMERGENCY LIGHTS OUT IN CABIN ON WALK AROUND. MAINTENANCE REPLACED 2 EMERGEGENCY BATTERY PACKS PER B717 AMM 33-53. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CRACKED (BS 1037 L14L) · airframe 59,050 hrs · 42,021 cycles

CRACKS WERE FOUND AFFECTING SKIN 5936436-101. AND FINGER DOUBLER 5936436-39 (M/F 0.025 7075-T6 CLAD SHEET) AT STA 1037 & L14L. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 560947-14. PERFORMED GVI OF DECAL AND AREA. DECAL IS IN GOOD CONDITION AND NO FURTHER DAMAGE SEEN IN AREA. OK TO CONTINUE ON MONITOR. ERA 560947-14 REV ORIG. (LP #0244171)

Part: TAB — DELAMINATED (LT WING AILERON) · airframe 9,316 hrs · 7,539 cycles

DURING INSPECTION, FOUND DELAMINATION ON UPPER AND LOWER SKIN SURFACE OF THE LT AILERON TAB.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 44,122 hrs · 29,916 cycles

EXIT SIGN LENS ABOVE THE L1 DOOR DETACHES. SECURED THE SIGN LENS. ACFT OK FOR SERVICE.

Part: SIGN — MISSING (CABIN) · airframe 44,011 hrs · 29,842 cycles

DOOR 1L EXIT SIGN IS MISSING. MAINTENANCE INSTALLED THE EXIT SIGN AS PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.

Part: SIGN — UNSECURE (CABIN) · airframe 44,000 hrs · 29,837 cycles

EMERGENCY EXIT SIGN COVER LOOSE AT LOCATION 601. EXIT SIGN FALLS OFF WHILE CLOSING INTERIOR DOOR. RE-SECURED EXIT SIGN AS REQUIRED.

Part: ACCESS PANEL — CRACKED (NOT REPORTED) · airframe 43,923 hrs · 29,793 cycles

FUEL ACCESS PANEL CRACKED. REPLACED THE ACCESS PANEL.

Part: WIRE — BROKEN (SLIDE LANYARD) · airframe 43,923 hrs · 29,793 cycles

BROKEN WIRES ON THE L1 DOOR SLIDE LANYARD. THE LANYARD WAS REPLACED IAW AMM 25-61-01-400-801.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION COUNTERSINK ON FUEL ACCESS PANEL 141AL. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2.

Part: CLAMP — WORN (TAILCONE RELEASE) · airframe 43,923 hrs · 29,793 cycles

WORN RT CABLE CLAMP OF TAIL CONE RELEASE SYSTEM ALSO RUSTED HARDWARE ON PULLEY AT 11 HRS POSITION. THE CABLE CLAMP WAS REPLACED IAW AMM 53-52-01 AND HARDWARE ON PULLEY WAS REPLACED IAW AMM 20-00-02.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 43,923 hrs · 29,793 cycles

CRACK INDICATION ON OPEN HOLE OF SPAR CAP AFT FLANGE AT ZFS=52.767 ON THE RIGHT SIDE VERTICAL STABILIZER. REPAIRED IAW ER/A 56094-14AD, REV ORG. AND ETI-17-17-175, REV 3. SECTION II.

Part: INTERCOSTAL — CORRODED (BS 1037-1053) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON AFT CARGO BAY INTERCOSTAL BS 1037 - 1053, LONGERONS 21 - 22L. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 5911423, REV CD.

Part: BEAM — CORRODED (BS 954-994) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON AFT CARGO BAY LOWER DOOR FRAME BEAM BETWEEN BS 954 TO 994. THE BEAM BTW WAS REPAIRED IAW SRM 53-20-15-2R-7.

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION OUT OF LIMITS ON FRAME BS 1022, BETWEEN LONGERONS 29 - 30L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW SRM 53-00-00-2R, PROCEDURE 2.

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR FRAME) · airframe 43,923 hrs · 29,793 cycles

AFT CARGO COMPARTMENT SEAL DEPRESSOR CRACKED AND WORN, ON THE AFT EDGE BETWEEN LONGERONS 24R TO 25R AND BS 994. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15-2R-4.

Part: SEAL DEPRESSOR — CRACKED (DOOR FRAME) · airframe 43,923 hrs · 29,793 cycles

CRACK ON THE LOWER CARGO DOOR FRAME SEAL DEPRESSOR BETWEEN BS 980 TO 985. THE LOWER SEAL DEPRESSOR WAS REPLACED IAW SRM SRM 53-20-15-0I-2, FIG. 1.

Part: FRAME ANGLE — CRACKED (BS 1053) · airframe 43,923 hrs · 29,793 cycles

CRACKED FRAME ANGLE ON AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR FRAME, BETWEEN BS 1053 AND 12 O'CLOCK POSITION. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND 51-41-02-0G.

Part: ANGLE — CRACKED (BS 1152) · airframe 43,923 hrs · 29,793 cycles

CRACKED ANGLE AT 1152 BETWEEN LONGERONS 2 & 3L . THE ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND DWG 9911840, REV CR.

Part: FRAME — CRACKED (BS 1022) · airframe 43,923 hrs · 29,793 cycles

CRACKED FRAME CAP BS 1022, LONGERON 7L. THE DAMAGE FRAME CAP WAS REPAIRED IAW ER/A 560900-14, REV ORIGINAL AND ETI-17-17-176, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1022) · airframe 43,923 hrs · 29,793 cycles

CRACKED SKIN AT BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIGINAL, AND ETI-17-17-172, REV 2.

Part: SKIN — CRACKED (BS 1037) · airframe 43,923 hrs · 29,793 cycles

CRACKED FUSELAGE SKIN AT BS 1037 LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIG, AND ETI-17-17-178, REV 2.

Part: WEB — CRACKED (BS 715) · airframe 43,923 hrs · 29,793 cycles

CRACKED WEB BS 715, BETWEEN LONGERONS 11 - 15R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 51-40-08-0G.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 43,923 hrs · 29,793 cycles

CABIN FLOOR PANEL 222ZF WAS FOUND CRACKED ON THE MID SECTION. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,923 hrs · 29,793 cycles

CRACKED LEFT DOOR FRAME AT BS 47, LONGERON 27L OF NLG. THE LT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,923 hrs · 29,793 cycles

CRACKED RT NLG DOOR FRAME AT BS 47, LONGERON 27R. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: SKIN — DENTED (RUDDER) · airframe 43,923 hrs · 29,793 cycles

DENT ON THE LT SIDE NEAR THE T/E OF THE RUDDER. THE RUDDER WAS REPAIRED IAW SRM 51-70-13-2R-1 PAR 4B.

Part: STOP FITTING — CRACKED (EMERGENCY EXIT) · airframe 43,923 hrs · 29,793 cycles

CRACKED STOP FITTINGS, LT LOWER AND MID POSITION, RT SIDE MID POSITION AT AFT EMERGENCY EXIT DOOR FRAME AREA BS 1053. HFEC INSPECTION WAS ACCOMPLISHED ON THE FITTING RT SIDE MID POSITION AND NO CRACKS WERE FOUND IAW NDT SPM, PART 6, 06-10-01.001. STOP FITTINGS LT LOWER AND MID WERE REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 3917624, REV C.

Part: LONGERON — CRACKED (BS 1133) · airframe 43,923 hrs · 29,793 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON FLOOR SUPPORTS STA Y=180 X=38 TO X=13 AND X=-9 TO -43 (2EA). CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=180 X=38 TO X=13 AND X=-9 TO -43 WERE REPLACED PER SRM 51-40-08-0G AND 51-41-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON LOWER EPC SUPPORT STA Y=-160X=14 TO X=54. CORROSION LEVEL 2 LOWER EPC SUPPORT STA Y=-160 X=14 TO X=54. WAS REPLACED PER SRM 51-41-02-0G AND 51-41-01-0G AND DWG 9955780 REV LA.

Part: SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON SLIDE LATCH SUPPORTS BS 160 TO 200, RBL 54 AT R1 FLOOR PANEL. THE LATCH SUPPORTS WERE REPLACED IAW SRM 51-40-08-0G, PAR 3.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 43,923 hrs · 29,793 cycles

CRACKED SHEAR TIE BS 1022, LONGERONS 6R TO 7R. THE SHEAR TIE WAS REPLACED SRM 51-41-02-0G, SRM 51-20-09-0G, SRM 51-41-05-0G, AND DWG 9912243, REV HF.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 43,923 hrs · 29,793 cycles

CRACKED SHEAR TIE BS 1022, LONGERONS 13 TO 14L AND RT. THE SHEAR TIE WAS REPLACED IAW DWG 9912243, REV JB, SRM 51-20-09-0G, 51-41-02-0G, AND 51-41-05-0G.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 43,923 hrs · 29,793 cycles

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

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,923 hrs · 29,793 cycles

CRACKED CUSP WEB ON STA Y=662 AND X=-54 AT PAX CABIN REF NRC 00349 (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206 AND SRM 51-41-02-0G AND 51-41-05-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON FLOOR SUPPORTS STA Y=195-200 X=54, X=14 (2EA) 5300-2010)(W1). LEVEL CORROSION 2. SUPPORT WAS REPLACED PER SRM 51-40-08-0G.

Part: FLOOR SUPPORT — CORRODED (BS 147-200) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON FLOOR SUPPORT BTW BS 147 - 200, RBL 7. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, 51 41-01, AND 51-10-04-0G. PAR 26, 15, AND 21.

Part: TAB — SCRATCHED (RUDDER) · airframe 43,923 hrs · 29,793 cycles

SCRATCHES ON RUDDER CONTROL TAB RT SIDE. RUDDER CONTROL TAB WAS REPAIRED PER SRM 51-70-02-2R PROCEDURE 1 AND CARD 2000-8149-01.

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON FLOOR SUPPORT BS BS 200 LBL 14. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, AND 53-10-51-0I-2, FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON RT SEAT TRACK X=-44.5 FROM STA Y=200 TO Y=237 REF NRC S/N 130 (W1). LEVEL CORROSION 2, SEAT TRACK WAS REPAIRED PER SRM 53-20-52-2R-5 FIG 201.

Part: FORMER — CRACKED (BS 715) · airframe 43,923 hrs · 29,793 cycles

CRACKED FORMER ON BS 715 AT KEELBEAM. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1- AND 51-41-02.

Part: FORMER — CRACKED (BS 737) · airframe 43,923 hrs · 29,793 cycles

CRACKED FORMER BS 737 AT THE KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1, AND 51-41-02.

Part: FORMER — CRACKED (BS 694) · airframe 43,923 hrs · 29,793 cycles

CRACKED FORMER AT BS 694 KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1, AND 51-41-02.

Part: BEAM — CRACKED (NR 4) · airframe 43,923 hrs · 29,793 cycles

CRACKED NR 4 BEAM ON FWD RIGHT GALLEY DOOR. THE BEAM WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-41-05.

Part: CUSP WEB — CRACKED (BS 440-601) · airframe 43,923 hrs · 29,793 cycles

CRACKED CUSP WEB, BS 440 - 601, BETWEEN RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: WEB — CORRODED (BS 198-202) · airframe 43,923 hrs · 29,793 cycles

CORROSION ON WEB LOWER SURFACE FROM BS 198 TO 202, BL 0 AND RBL 26, AND RBL 44 IN THE E & E BAY. THE WEB WAS REPAIRED IAW SRM 51-70-10-2R-2, 51-41-02-0G, AND 51-41-08-0G.

Part: FITTING — CRACKED (CARGO DOOR FRAME) · airframe 43,923 hrs · 29,793 cycles

CRACK IN UPPER PAN FITTING NEAR BS 974 AT THE AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-04, AND 51-41-05, PARAGRAPH 10.

Part: CUSP WEB — CORRODED (BS 923) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION ON THE RT CUSP WEB BS 923, BETWEEN LBL 54 TO 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4, FIG 215.

Part: WEB — CORRODED (BS 190-200) · corrosion level 2 · airframe 43,923 hrs · 29,793 cycles

CORROSION DIAPHRAGM FROM BS 190 TO 200, LBL 53 - 55. THE DIAPHRAGM WAS REPAIRED IAW SRM 51-70-10-2R-2, AND SRM 53-10-51-OI-2.

Part: PAN — CRACKED (BS 832-870) · airframe 43,923 hrs · 29,793 cycles

CRACK ON THE LT UPPER, AFT CORNER OF WINDOW RING PAN BS 832 AND 870. REPAIRED IAW 56-20-02-2R.

Part: LONGERON — CRACKED (BS 908) · airframe 43,923 hrs · 29,793 cycles

CRACKED LONGERON 10R, BS 908. REPAIRED THE LONGERON IAW SRM 53-00-05-2R-2, FIG 201.

Part: STRUCTURE — WORN (EMERGENCY EXIT) · airframe 43,923 hrs · 29,793 cycles

WORN ON LOWER RT CORNER INTERNAL STRUCTURE AT THE AFT EMERGENCY EXIT BULKHEAD DOOR. DAMAGED AREA WAS REPAIRED IAW SRM 52-10-02-2R, 16, FIG 201.

Part: SKIN — CRACKED · airframe 43,923 hrs · 29,793 cycles

CRACK ON FUSELAGE SKIN AROUND AFT HINGE OF THE LT AFT NLG DOOR. THE SKIN WAS REPAIRED IAW SRM 53-10-01-2R-11.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 43,923 hrs · 29,793 cycles

CRACKED ANGLE BELOW THE NR 1 BEAM AFT EDGE ON FWD SERVICE DOOR. REPLACED IAW SRM 51-41-05, AND DRAWING 9911579, REV L.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,923 hrs · 29,793 cycles

CRACKED NR 1 BEAM, AFT EDGE ON THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 43,100 hrs · 29,169 cycles

DURING TAXI IN, BOTH FWD COFFEEMAKERS STARTED SMOKING, ELECTRICAL ODOR, SHUT OFF GALLEY POWER THE SMOKE STOPPED. REPLACED THE COFFEEMAKERS IAW AMM 25-33. INSPECTED COFFEEMAKER COMPARTMENT AND WIRING, NO DEFECTS FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,334 hrs · 27,916 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,911 hrs · 25,126 cycles

DURING LINE CHECK, FOUND CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. FOUND BAD BATTERY PACK AT STA 398 ABOVE SEAT ROW 10 CD. REPLACED BATTERY PACK AND SYSTEM CHECKS GOOD. LP 7039143.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 35,423 hrs · 22,983 cycles

DURING LINE CHECK, MAINTENANCE NOTED THE L1 DOOR SLIDE PARACHUTE PINS WERE NOT ENGAGED. THE L1 DOOR SLIDE WAS REPLACED IAW WC 2561-9004 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,101 hrs · 22,679 cycles

PILOT REPORTED THE EMERGENCY LIGHTS AT ROW 25 INOPERATIVE. MAINTENANCE REPLACED LAMP AND OPS NORMAL.

Part: LIGHT — DIRTY (CABIN) · airframe 34,610 hrs · 22,258 cycles

RT EMERGENCY ESCAPE LIGHTING DIRTY AT ROW 29. CLEANED EEPLS IAW MM.

Part: LIGHT — DIRTY (CABIN) · airframe 34,610 hrs · 22,258 cycles

LT EMERGENCY ESCAPE LIGHTING DIRTY AT ROW 18. CLEANED EEPLS IAW MM.

Part: CHARGER — FAILED (CABIN) · airframe 34,311 hrs · 22,079 cycles

EMERGENCY LIGHT BATTERY CHARGER FAILED AT BS 259. R & R CHARGER IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,311 hrs · 22,079 cycles

OVERWING EMERGENCY EXIT LIGHTS FAILED TEST. R & R BATTERY PACK IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 34,311 hrs · 22,079 cycles

AFT ACCESSORY COMPARTMENT EMERGENCY EXIT LIGHT LENS CRACKED AT AFT UPPER LIGHT NEAR BS 1240. R & R LENS IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 JF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED. R &R FLOOR PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 221UF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

FLOOR PANEL 222 AHF DELAMINATED. R &R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222FF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 AVF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 AEF DELAMINATED. R &R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED. R & R FLOOR PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 ATF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 AGF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 223 DF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222BF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 PF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED. R & R FLOOR PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222LF DELAMINATED. R & R IAW FLOOR PANEL MM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANEL 222 AMF DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: LATCH — DIRTY (L1 DOOR) · airframe 34,311 hrs · 22,079 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCHES DIRTY. CLEANED LATCHES IAW MM & SRM.

Part: LATCH — DIRTY (R1 DOOR) · airframe 34,311 hrs · 22,079 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCHES DIRTY. CLEANED LATCHES IAW MM & SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

LONGERON CORRODED AT STATION 1028, LONGERON 26R. R&R LONGERON IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 34,311 hrs · 22,079 cycles

MID CABIN EMERGENCY EXIT WIRES BROKEN. REPAIRED WIRE IAW AMM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

LONGERON CRACKED BETWEEN STATION 1133 TO STATION 212. R&R LONGERON IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD RT UPPER HORIZONTAL STRAP CRACKED. R & R INTERCOSTAL IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

SHEAR TIE FORMED CRACKED AT STATION 115,2 STRINGER 2L. R&R FORMER CLIP IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,311 hrs · 22,079 cycles

AFT CARGO COMPARTMENT CARGO TIE DOWN TRACK CORRODED AT BS 954 RBL 14. R & R TIE DOWN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD RT LOWER HORIZONTAL STRAP CRACKED. R & R INTERCOSTAL IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

AFT CARGO COMPARTMENT FORMER CORRODED AT BS 908, BETWEEN LONGERON 30L TO LONGERON 29L. REPAIRED FORMER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,607 hrs · 22,254 cycles

AFT CARGO FRAME CORRODED AT STATION 1028, BETWEEN LONGERON 29L TO LONGERON 30. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

FRAME CORRODED AT STATION 1028, BETWEEN LONGERON 30L TO LONGERON 29. R&R FRAME IAW SRM & DRAWING.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 34,311 hrs · 22,079 cycles

FWD CARGO DOOR INNER SKIN CRACKED AT AFT LATCH. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

LT MAIN WINDOW AT FRAME STATION 636L, WINDOW FRAME LOWER FWD END CRACKED. REPAIRED FRAME IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

CUSP WEB CORRODED BETWEEN STATION 468 TO STATION 475, RBL 56. R&R CUSP WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

LT CABIN WINDOW AT FRAME STATION 889L, WINDOW FRAME LOWER AFT END CRACKED. REPAIRED FRAME IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

RT SIDE CABIN WINDOW BRACKET AFT OF STATION 889-R CRACKED IN UPPER & LOWER FWD. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 34,311 hrs · 22,079 cycles

AFT CARGO DOOR INNER SKIN CRACKED. R & R DOOR ASSEMBLY IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

SEAT TRACK CORRODED BETWEEN STATION 285 TO STATION 582, RBL 44. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

SEAT TRACK CORRODED BETWEEN STATION 267 TO STATION 580, RBL 22. R & R SEAT TRACK IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

RT CABIN WINDOW BRACKET FWD OF STATION 832-R CRACKED IN AFT LOWER CORNER. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

CUSP WEB CRACKED AT STATION 650R. REPAIRED CUSP WEB IAW SRM & AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

CUSP WEB CORRODED BETWEEN STATION 389 TO STATION 408, LBL 56. REPAIRED CUSP WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

SKIN CORRODED AT BS 822 BETWEEN LONGERON 27R TO LONGERON 26R. REPAIRED SKIN IAW SRM & DRAWING.

Part: RAMP — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

LT WW DOOR AFT SUPPORT BRACING UPPER ANGLE CRACKED. R&R RAMP ASSEMBLY IAW SRM.

Part: FITTING — CRACKED (LT MLG WW) · airframe 34,311 hrs · 22,079 cycles

LT WW FWD DOOR CUTOUT INBD FITTING CRACKED. R&R FITTINGS IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

CUSP WEB CORRODED AT STATION 898 LBL 56. R&R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,080 cycles

RT WING TO FS BODY FAIRING SUPPORT CORRODED AT STATION 832, BETWEEN STRINGER 30R TO STRINGER 24R. REPAIRED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

FLOOR SUPPORT CRACKED AT STATION 737, LBL 44. R&R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

FLOOR SUPPORT CRACKED AT STATION 737, RBL 44. R&R SUPPORT IAW SRM.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 34,311 hrs · 22,079 cycles

LT ELEVATOR GEARED TAB DELAMINATED AT OTBD HINGE FITTING CUTOUT. REPAIRED TAB IAW SRM.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 34,311 hrs · 22,079 cycles

LT ELEVATOR GEARED TAB DELAMINATED AT CENTER HINGE FITTING CUTOUT. REPAIRED TAB IAW SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 34,311 hrs · 22,079 cycles

LT ELEVATOR GEARED TAB DELAMINATED AT TE. REPAIRED TAB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,080 cycles

LT WING TO FS AFT BODY FAIRING SUPPORT CORRODED AT STATION 832, BETWEEN STRINGER 30L TO STRINGER 24L. REPAIRED SUPPORT IAW SRM.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 34,311 hrs · 22,079 cycles

LT ELEVATOR GEARED TAB DELAMINATED AT INBD HINGE FITTING CUTOUT. REPAIRED TAB IAW SRM.

Part: STRAP — CRACKED (RT WING) · airframe 34,311 hrs · 22,079 cycles

RT WING FIXED LE FAIRING PANEL AT MOST INBD AREA INTERIOR STRAY ATTACHED TO BODY FAIRING PANEL FRAME CRACKED AT UP & LOWER ATTACHED AREAS. R&R STRAPS IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN CUSP WEB CRACKED AT STATION 655, RBL 44. R&R CUSP WEB IAW SRM.

Part: PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN PANELS 222ACF, 222AEF, 222AGF, 222AHF, & 223DF AREA DELAMINATED. R & R PANEL IAW MM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANELS 221PF, 221UF, 222BF, 222JF, 222PF, 222AMF & 222ATF AREA DELAMINATED. R & R FLOOR BOARD IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,311 hrs · 22,079 cycles

MAIN CABIN FLOOR PANELS 221WF, 222LF, 222RF, 222ABF, 222APF, 222AVF & 222FF AREA DELAMINATED. R & R FLOOR PANEL IAW MM & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

RT OVERWING FRAME 715 CRACKED. R & R FRAME SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

RT OVERWING FRAME 696 CRACKED. R & R FRAME IAW SRM & DRAWING.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,311 hrs · 22,079 cycles

FWD CARGO COMPARTMENT LOWER DOOR PAN SECTION CORRODED. R&R PAN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,467 hrs · 21,585 cycles

LOWER FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY REF AMM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 30,403 hrs · 19,630 cycles

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

Part: SKIN — DENTED (FUSELAGE)

LEFT SIDE FUSELAGE EXTERIOR SKIN, STA 37 TO 56, LONG 17L TO 19L, DENTED. ACCOMPLISHED FUSELAGE EXTERIOR SKIN INTERNAL DOUBLER REPAIR PER B717 SRM 53-02-01 FIG 202, REPAIR 1.

Part: COVER — OUT OF POSITION (EXIT SIGN)

EXIT SIGN COVER ROW 1 FELL OFF. REPLACED EXIT SIGN COVER M/M 33-60.

Part: LIGHT — INOPERATIVE (EXIT SIGN)

BULBS IN EXIT SIGN OVER ROW 1 OUT. EXIT SIGNS BULBS OK FOR SERVICE MM 33-60.

Part: SKIN — DENTED (TE FLAP VANE)

RT AFT MOVEABLE FLAP VANE UPPER SURFACE SKIN, DENTED. ACCOMPLISHED UPPER SURFACE SKIN REPAIR PER B717 MM 27-50-03 AND B717 SRM 51-70-02.

Part: ANGLE — CRACKED (LT PYLON)

LEFT PYLON NUMBER 2 COWL LATCH APRON ANGLE, CRACKED. ACCOMPLISHED APRON ANGLE REPAIR PER B717 SRM 54-50-02.

Part: FITTING — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT CIRCUMFERENTIAL FRAME SHEAR CLIPS, STA 927, LONG S29L TO S29R, CORROSION. ACCOMPLISHED CIRCUMFERENTIAL FRAME SHEAR CLIPS REPLACEMENT PER B717 SRM 53-00-00, 53-00-06 AND 53-20-06.

Part: SKIN — DENTED (TE FLAP VANE)

RT AFT MOVEABLE FLAP VANE LOWER SURFACE SKIN, DENTED. ACCOMPLISHED LOWER SURFACE SKIN REPAIR PER B717 MM 27-50-03 AND B717 SRM 51-70-02.

Part: STRUCTURE — CRACKED (NR 2 PYLON)

NR 2 ENGINE LOWER COWLING NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA REPAIR PER B717 SRM 54-50-02.

Part: STRUCTURE — CRACKED (NR 2 COWLING)

NR 2 ENGINE UPPER COWLING NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA REPAIR PER B717 MM 71-12-02, SRM 54-50-02 AND 51-10-04.

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

LOWER FORWARD GALLEY DOOR CUT OUT ATTACHED ANGLE BRACKET, STA 160, CORROSION. ACCOMPLISHED ATTACHED ANGLE BRACKET REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-20-09 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 196, LBL 44. ACCOMPLISHED FLOOR SUPPORT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: SUPPORT — CRACKED (FUSELAGE)

FORWARD PASSENGER DOOR SUPPORT SKIN, STA 218, LONG 15, CRACKED. ACCOMPLISHED DOOR SUPPORT SKIN DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

CABIN FORWARD GALLEY DOOR WAY GIRT BAR ATTACH FITTINGS, STA 160 TO 200, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 7 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 258, LBL15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 7 TO RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-05.

Part: CAM — OUT OF ADJUST (TAILCONE)

DURING TAIL CONE FUNCTIONAL CHECK, RELEASE CAM FAILED TO OPERATE PROPERLY. ACCOMPLISHED ADJUSTMENT OF TAIL CONE RELEASE MECHANISM CAM. REF B-717 MM 53-52-03. OPS CHECKS NORMAL.

Part: GIRT BAR — DETACHED (EVAC SLIDE)

R1 GIRT BAR DETACHED FROM SLIDE ****AWI*** RE-ATTACHED AS REQUIRED REF B717 AMM 25-61 ****AWI***

Part: GIRT BAR — OUT OF POSITION (R1 DOOR)

GIRT BAR ON OUTSIDE OF A/C AT R1 DOOR. CABLE LANYARD CUT. REMOVED AND REPLACED DOOR SLIDE AND GIRT BAR LANYARD AT R1 DOOR PER AMM TASK 25-61. OPS CHECK OK.

Part: LOCK — OBSTRUCTED (GIRT BAR)

L1 DOOR GIRT BAR WILL NOT LOCK. REMOVED DEBRIS FROM THE GIRT BAR LOCK REF GMM 8103.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LEFT EMERGENCY EGRESS LIGHT REMAINS ON AFTER RESET. REMOVED AND REPLACED OVERWING POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD.

Part: COVER — SEPARATED (EVAC SLIDE)

R1 DOOR SLIDE COVER SEPARATED FROM HINGE. REPAIRED R1 DOOR SLIDE COVER PER EA 17-52-02402 IR.

Part: SIGN — OUT OF POSITION (CABIN)

EXIT SIGN BETWEEN ROW 1 & 2 FELL DOWN. RESECURED EXIT SIGN. OK FOR SERVICE. REF M/M 33-00.

Part: SKIN — DENTED (BS 237 L17-18L)

DENT IN FUSELAGE BS 237 BETWEEN LONG L17 AND L18. CUT OUT DAMAGED AREA, FABRICATED DOUBLERS, PER SRM 53-00-01. INSTALLED REPAIR DOUBLERS, PER 717 SRM 53-00-01 REPAIR 6.

Part: APU — ODOR (APU BAY)

AFTER APU START, INTRODUCED APU AIR, SMELLED ACRID PLACTIC SMELL AND CABIN STARTED FILLING WITH SMOKE. RAMP CREW REPORTED SEEING SMOKE AROUND TAIL AND HEARD A LOUD POP. REMOVED AND REPLACED APU.

Part: WIRE HARNESS — DAMAGED (LT ENGINE)

AFTER TAKEOFF ON 26L ATL, LOST NR 6 DU AND LT GENERATOR FAIL ALERT, SMELLED ELECTRICAL SMOKE. EMERGENCY LANDING ON 9R AT APPROX 114,000 LBS FIRM LANDING. EMERGENCY EVACUATION CONDUCTED. ACCOMPLISHED REPLACEMENT OF THE LT ENGINE WIRING AND ALL CONNECTORS FROM THE LEFT ENGINE SENSOR TO THE LEFT PCDU AND OPS CHECK WAS SATISFACTORY. PERFORMED AC POWER GENERATION AND CONTROL ADJ AND TEST IAW B717 MM 24-21-00 WAS SATISFACTORY.