N892AT

Part: BOLT — MISSING (ZONE 300) · airframe 49,179 hrs · 35,031 cycles

MISSING AND SUNKEN BOLTS ALONG DOUBLER SPLICE APPROX BTW STA ZFS=49 AND ZFS=76 AT VERTICAL STABILIZER LEADING EDGE. REPAIRED PER ER/A 630634-14. (1338826)

Part: SKIN — CRACKED (ZONE 200) · airframe 49,151 hrs · 34,999 cycles

TWO CRACKS ON FUSELAGE SKIN PANEL APPROX ON BS 1076 & 1095, L14R. DAMAGED AREA WERE REPAIRED IAW ER/A 630576-14. (1335394)

Part: OIL CAP — UNSECURE (APU OIL SYS) · airframe 49,134 hrs · 34,985 cycles

NOTICED UNPLEASANT ODOR ON TAXI IN AFTER APU START AND OBSERVED LEAKING DARK FLUID UNDERNEATH APU COMPARTMENT ON SUBSEQUENT WALK AROUND. APU OIL CAP NOT PROPERLY SEATED AND APU AND COMPARTMENT AND AFT FUSELAGE COVERED WITH OIL. THE APU OIL CAP WAS PROPERLY SEVURED AND APU AND EXTERNAL AFT FUSELAGE WAS CLEANED. R/R COALESCER BAGS PER B717 AMM 21-54. CLEANED OUT AND BURNED OUT PNEUMATIC DUCTING. (7978044)

Part: RELAY — FAULTED (GENERATOR) · airframe 48,353 hrs · 34,280 cycles

SHIP 9552-DIV- FLIGHT DIVERSION TO CLE DUE TO LOSS OF LEFT GEN AND LEFT AC BUS CROSS TIE LOCKOUT. / CORRECTIVE ACTION: RESET LEFT PCDU & RESET LEFT BUS TIE SWITCH. AS PRECAUTIONARY REPLACED EPCU, PCDU, L GENERATOR RELAY AND L BUS TIE RELAY. OPS NORMAL AND RETURNED TO SERVICE. (LP 7556390)

Part: TAB — DAMAGED (RT AILERON) · airframe 48,004 hrs · 33,957 cycles

SHIP 9552 RT AILERON CONTROL TAB HAS DAMAGE. CORRECTIVE ACTION: RMEOVED RT AILERON CONTROL TAB PER B717 AMM 27-10 WIP 374716. (0967220)

Part: DUCT — DISCONNECTED (ACM) · airframe 46,142 hrs · 32,291 cycles

SHIP 9552 -DIV/PRESS/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO MEM FOLLOWING THE RAPID LOSS OF CABIN PRESSURIZATION. CREW DONNED O2 MASKS, DECLARED AN EMERGENCY, AND INITIATED AN EMERGENCY DESCENT TO 10K FEET. CABIN MASKS AUTOMATICALLY DEPLOYED. LANDED SAFELY WITH BOTH CABIN PRESSURE CONTROLLERS FAILED. CORRECTIVE ACTION: MAINTENANCE FOUND THE AIR CONDITIONING GROUND AIR SUPPLY DUCT DISCONNECTED AND THE RIGHT WATER SEPARATOR DUCT DAMAGED. DISCONNECT WAS DUE TO A DAMAGED BRACKET WITH MISSING HARDWARE AND THE RIGHT CONDITIONED AIR CHECK VALVE DAMAGED. REPLACED ALL AND PERFORMED PACK CONFIDENCE CHECK AND PACK LEAK CHECK. REPLACED ALL USED O2 GENERATORS IN THE CABIN. (LP #5879904)

Part: OXYGEN MASK — INOPERATIVE (SEATS 11C-29A) · airframe 46,142 hrs · 32,291 cycles

SHIP 9552 -MISC- REFERENCE LOG PAGE #5879904 ABOUT A RAPID DECOMPRESSION EVENT. MASKS AT SEAT ROWS 11C, 18A, 19C, 21C, 24C, 25A, 29A, & AFT F/A SEAT DID NOT DROP DURING THE ODI EVENT. MAINTENANCE FORWARDED THE O2 SYSTEM TO MEL 35-21-01A. "M" PROCEDURES COMPLIED WITH. PLACARD INSTALLED. OK FOR SERVICE. (LP #5879911)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,788 hrs · 31,979 cycles

THE FORWARD DOOR LEVER EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-61. OPERATIONAL TEST WAS GOOD. (LP #5920917)

Part: NONE — NONE (NONE) · airframe 45,380 hrs · 31,641 cycles

THE EMERGENCY EXIT SIGNS WERE DISCOVERED TO BE INOPERATIVE AT LOCATIONS: 600, 601, 604, AND 605. THE EXIT SIGNS WERE NOT ILLUMINATED WHEN THE CABIN LIGHTING WAS OFF AS DESIGNED. MAINTENANCE CHECKED AND DETERMINED THAT ALL EMERGENCY EXIT SIGNS OPERATED NORMALLY. THE AIRCRAFT IS OK FOR SERVICE. (LP #0261302)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,839 hrs · 31,176 cycles

ON WALK AROUND FOUND RIGHT REAR EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY REF B717 AMM 33-51. (LP #5049081)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00273: CRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT ACCESSORY COMPARTMENT WERE REPAIRED PER B717-200 SRM 51-41-05-0G, 51-41-01-0G, 51-41-02-0G, 53-00-05-2, AND B717-200 AMM 21-54-20 000-801 AND 21-54-01 400-801. (LP #0111511)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACK ON BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR. SUMMARY OF THE NRC 00081: BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #0111304)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

SKIN DELAMINATION ON LOWER SURFACE OF VANE. SUMMARY OF NRC 00495: SKIN ON LOWER SURFACE OF VANE WAS REPAIRED PER ERA 613937-14 REV ORIG. SECCTION I: PERMANENT REPAIR. SEC II: ACCOMPLISH WITHIN EVERY 24 MONTHS OR 3,000 CYCLES, WHICHEVER OCCURS FIRTS UNDER LOGPAGE 0106855. ASSOCIATED ER/A 14-613937 ADDED FOR AC 9552. (LP #0108785)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON PREVIOUS REPAIR ON FRAME STA 927 BTW LONGERONS 29L-28L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. PREVIOUS REPAIR ANGLE ON FRAME STA 927 BTW LONGERONS 29L-28L AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, 51-41-02-0G, AND 51-41-05-0G. (LP #0099495)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACK ON UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT IN REF NRC 00408. SUMMARY OF NRC 00487: UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER PRI 614087-14 REV 2 AND ER/A 614087-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614087 ADDED FOR AC 9552. (LP #0100062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON DOOR JAMB LOWER AT AFT CARGO DOOR. SUMMARY OF NRC 00067: CORROSION LEVEL 2. DOOR JAMB LOWER AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 53-20-15-2R REP 7. (LP #0088493)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACK ON OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR. SUMMARY OF NRC 00059: OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1. (LP #0089031)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN SEAT TRACK X=-44.5, BTW Y =200/256. SUMMARY OF NRC 00226: CORROSION LEVEL 2. SEAT TRACK X=-44.5, BTW Y=200/256 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5 FIG 201 SHEET 1,2,9,10,11. (LP #0081182)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

A CRACK ON FLOOR WEB, STA Y=196 TO 200 X-30 TO X-35 APROX WAS FOUND AT PASSENGER CABIN IN REF NRC #00226. SUMMARY OF NRC 00490: REPAIR WAS PERFORMED PER B717 SRM 51-70-10-2R PAR 4 FIG 201. (LP #0075520)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACK ON REAR SPAR RUDDER ACCESS PANEL 1. SUMMARY OF NRC 00312: REAR SPAR RUDDER ACCESS PANEL 1 WAS REPAIRED PER B717-200 SRM 55-00-00-2R PROCEDURE 2, REPAIR 2, PARAGRAPH A, FIGURE 201. (LP #0074053)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORT, STA X=-7, BTW Y=148/200. SUMMARY OF NRC 00211: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=-7, BTW Y=148/200 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0071998)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORT, STA X=7, BTW Y=148/200. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=7, BTW Y=148/200 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0072026)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,704 hrs · 31,070 cycles

CRACK INTERCOSTAL BTW BEAM NO 4 TO BEAM NO 5 AND STA Y=185.5 AT FWD PASSENGER DOOR INTERNAL EXTRUCTURE. SUMMARY OF NRC 00368: INTERCOSTAL BTW BEAM NO 4 TO BEAM NO 5 AND STA Y=185.5 AT FWD PASSENGER DOOR INTERNAL EXTRUCTURE WAS FABRICATED AND REPLACED PER DOUGLAS AIRCRAFT COMPANY DWG 9955763 REV L, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #0071567)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORTS (2 EA) STA Y=200, BTW X=7/-7, AND BTW X=-45.5/-56.5 (OUT OF LIMITS). SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) STA Y=200, BTW X=7/-7, AND BTW X=-45.5/-56.5 WERE FABRICATED PER B717 DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0071557)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORT, STA X=44.5, BTW Y=160/196. SUMMARY OF NRC 00215: CORROSION LEVEL 2. FLOOR SUPPORT, STA X= 44.5, BTW Y=160/196 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0065622)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORT, STA X=-44.5, BTW Y=160/200. SUMMARY OF NRC 00212: CORROSION LEVEL 2. CABIN FLOOR SUPPORT STA X=-44.5 BTW Y=160/200 WAS REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-02-0G. (LP #0063456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORTS (2 EA), STA Y=180, BTW X=13/38 AND BTW X=-7/-44.5. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR SUPPORT (2 EA), STA Y=180, BTW X=13/38 AND BTW X=-7/-44.5, WERE FABRICATED AND REPLACED PER DWG 9936534 REV BW AND B717-200 SRM 51-41-02- 0G. (LP #0057167)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON FLOOR WEB, STA Y=196 TO 200 X-50 TO X-55 AND Y=201 AT X- 44 TO X-48 AT PASSENGER CABIN (OUT OF LIMIT). PER NRC 0411: CORROSION LEVEL 2. FLOOR WEB STA Y= 196 TO 200 X-50 TO X-55 AND Y=201 AT X-44 TO X-48 AT PASSENGER CABIN WAS REPAIRED PER B-717-200 SRM 51-70-10-2R REP. 1 FIG. 201. (LP #0056058)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 44,704 hrs · 31,070 cycles

CORROSION ON CABIN FLOOR SUPPORT, STA Y=196, BTW X=22/44.5. SUMMARY OF NRC 00221: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=196, BTW X=22/44.5 WAS REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-02-0G PAR 4. (LP #0055761)

Part: LENS — MISSING (EXIT SIGN) · airframe 39,808 hrs · 27,314 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING AT LOCATIONS: 600. EMERGENCY EXIT COVER IS MISSING AND BARE WIRES ARE EXPOSED. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN EQUIPMENT L2-832 AT DOOR R1 PER WDM 33-51-14. OPERATIONAL CHECK IS GOOD. (LP 0791755)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 39,244 hrs · 26,938 cycles

EMERGENCY EXIT LIGHT LENS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 39,244 hrs · 26,938 cycles

EMERGENCY EXIT LENS WAS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.

Part: COVER — LOOSE (EXIT SIGN) · airframe 39,141 hrs · 26,867 cycles

THE FWD CENTER AISLE CEILING EMERGENCY EXIT SIGN COVER IS LOOSE. MAINTENANCE REATTACHED THE EXIT SIGN. OPERATIONAL CHECK IS GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 39,073 hrs · 26,814 cycles

THE FORWARD MOST EMERGENCY EXIT LIGHT IS NOT SECURELY FASTENED TO THE CEILING AS DESIGNED. MAINTENANCE SECURED THE LIGHT ASSEMBLY AS REQUIRED. OK FOR SERVICE.

Part: BRACKET — BROKEN · airframe 38,293 hrs · 26,298 cycles

LOUD BUZZING NOISE AND VIBERATION UNDER THE FLOOR AT ROW 19A. FOUND EIGHT RUBBER NUTS AT THE LT OVERWING FILLET PANEL. RAN HYD PUMPS AND FUEL PUMPS, ALL SOUND OK. INSPECTED THE UPPER LT WING FILLET AREA AND FOUND MIDDLE SUPPORT BRACKET FOR FWD OVERWING FILLET PANEL BROKEN. REPLACED BRACKET IAW DWG 59171068. OK FOR SERVICE.

Part: SKIN — CRACKED (TE FLAP VANE) · airframe 38,159 hrs · 26,202 cycles

CRACKED LOWER SKIN AT RT UPPER MOVABLE VANE. RT UPPER MOVABLE VANE WAS REPAIRED PER SRM 57-53-01-2R-1 PARAGRAPH 4 FIG 201.

Part: DOOR FRAME — CRACKED (AFT CARGO BAY) · airframe 38,012 hrs · 26,106 cycles

A CRACK WAS FOUND ON THE AFT CARGO DOOR FRAME AFT EDGE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-20-15-2R, PROCEDURE 12, PARAGRAPH 6 A.

Part: DOOR FRAME — CRACKED (LT NLG DOOR) · airframe 38,012 hrs · 26,106 cycles

CRACK FOUND ON THE LT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.

Part: DOOR FRAME — CRACKED (RT NLG DOOR) · airframe 38,012 hrs · 26,106 cycles

CRACK ON THE RT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,980 hrs · 26,086 cycles

DURING A SERVICE CHECK, FOUND THE TAIL CONE EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW AMM 33-51. CLEANED AND REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: PYLON — CRACKED (NR 1) · airframe 34,572 hrs · 23,670 cycles

NUMBER 1 PYLON UPPER AND LOWER AFT COWL ATTACH POINTS HAVE CRACKS IN CUTOUTS ON SKIRT FAIRING. REMOVED BRACKETS, FITTINGS, GUSSETS, AND SHIMS. BLENDED OUT CRACKS IN RADIUS. PERFORMED PENETRANT INSPECTION OF CUTOUT LOCATIONS IAW ER/A 552108-14 REV. A SECTION 1 STEP 2C. NO CRACK NOTED. FIT, DRILLED, TREATED, AND PAINTED REPAIR IAW ER/A 552108-14 REV. A SECTION 1. COMPLETED THE REPAIR IAW ER/A 552108-14 REV. A SECTION 1.

Part: PYLON — CRACKED (LT NACELLE) · airframe 34,572 hrs · 23,670 cycles

LEFT ENGINE PYLON APRON FOUND TO BE CRACKED IN FOUR LOCATIONS. REPAIRED IAW ER/A 552108-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,445 hrs · 23,570 cycles

REV ORIG, PERFORMED CUT OUT OF DAMAGE AS SHOWN FIG 1. C/W HFEC AND BHEC PER PRI 551316-14 REV ORIG NR ITEMS 2034. FABRICATED REPAIR PARTS AS SHOWN FIG 1 REF PRI 551316-14 REV ORIG. COMPLETED REPAIR PER PRI 551316-14 REV ORIG COMPLETING ER/A 551316-14 REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,415 hrs · 22,780 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING BETWEEN ROWS 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: CUSP WEB — CORRODED (BS 488) · corrosion level 2 · airframe 34,595 hrs · 23,689 cycles

LEFT OUTER CUSP WEB CORRODED AT BS 488. CORRISION BLENDED AND FOUND BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4.

Part: FUEL TANK — CORRODED (LT MLG WW) · airframe 32,949 hrs · 22,416 cycles

LEFT WHEEL WELL TO RT WHEEL WELL FUEL TANK SKIN PLANK PANEL T/E CORRODED AT SEVERAL LOCATIONS. CLEAN/ EVAL, TREAT & PAINT REF OR NRC 62937-0100-0065. BLENDED OUT CORROSION ON RT WHEEL WELL FUEL TANK SKIN PLANK PANEL. MEASURED THICKNESS LOSS OF .015 TAG 3310 COMPLIED WITH ER/A 542367-14 AND REINSTALLED PANEL, CABLES, AND FASTERS IN TANK AS REQ. DID OPS CHECKS ON BREAKS IAW DAL-B717-32-44-00-720-804. ASSOCIATED ER/A 00-542367 ADDED FOR AC 9552.

Part: CUSP WEB — CORRODED (BS 427-446) · airframe 32,949 hrs · 22,416 cycles

RIGHT CUSP WEB CORRODED AT CUSP TEE BS 427-446 BOTTOM SIDE. REMOVED CORROSION IAW SRM 55-00-55, PG 101, ITEM 4 FOUND TO BE OUT OF LIMITS. INSTALLED NEW CUSP WEB AT BS 389 TO 503, RBL 45 TO RBL 54 IAW SRM 51-40-08 AND 51-40-02. REINSTALLED SEAT TRACKS AT RBL 45 & RBL 54, 389 TO 503 IAW SRM 51-40-02. FOR ALL OTHER WORK SEE AMES CONTINUATION FORMS 1 & 2.

Part: SEAT TRACK — CORRODED (BS 148-1022) · corrosion level 2 · airframe 34,587 hrs · 23,683 cycles

CENTER SEAT TRACK HAS MULTIPLE DEFECTS FROM BS 148 TO 1022. CLEANED RH CENTER SEAT TRACK AS MARKED, STA 148-STA 1032 AND FOUND ALL DEFECTS TO BE NEGLIGIBLE IAW SRM 51-10-02 PG. 65 PAR. F(1). REPLACED THE SEAT TRACK IAW SRM 51-41-05 PG. 32 ITEM 10, 51-40-02 PAR. 4 FIG 3, 51-40-03 PAR.3 AND 51-40-01 FIG. 1 PG.2. ALL B

Part: CUSP WEB — CRACKED (BS 674) · airframe 32,949 hrs · 22,416 cycles

RT CUSP WEB IS CRACKED AT APPROXIMATELY RBL 47 UNDER SEAT TRACK BS 674. REMOVED OLD CUSP WEB FROM BS 656 TO 715 INSTALLED NEW CUSP WEB IAW SRM 51-41-05 & 51-41-02 AND REINSTALLED. REMOVED SEAT TRACKS RBL 45 & RBL 54, BS 598-715 IAW SRM 51-41-01, PG 3, FIG 1. NEW CUSP WEB. REMOVED EWIS PROTECTION IAW TOPPS MANUAL 40-20-50. FOR ALL WORK, SEE CONTINUATIONS 1 & 2 FOR JOB COMPLETE.

Part: CUSP WEB — CORRODED (BS 522) · airframe 32,949 hrs · 22,416 cycles

RIGHT CUSP WEB HAS CORROSION AROUND FWD LIGHTING HOLE AFT OF BS 522. BLENDED AREA IAW 53-00-00, PG 105, FIG 103. REMOVING .006", FOUND TO BE OUT OF LIMITS, DRILLED & LOCATED NEAR CUSP WEB IAW SRM 51-40-08, PG 2, TABLE 6 AND 51-40-08, PG 7, FIG 1, INSTALLED NEW CUSP WEB IAW SRM 51-41-01 AND 51-41-02.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 32,949 hrs · 22,416 cycles

VERTICAL STABILIZER L/E WRAP AROUND SKIN PANEL JUST BELOW REMOVABLE PANELS 370DL 370GR HAS SEVERAL LOOSE SMOKING FASTENERS PULLING THROUGH SKIN. INSTALLED FABRICATED REPAIR DOUBLER AT VERTICAL STABILIZER WRAP AROUND SKIN PANEL IAW SRM 53-30-01, REPAIR (7) AND DWG SG95550001.

Part: SKIN — CRACKED (BS 1155) · airframe 32,949 hrs · 22,416 cycles

RIGHT AFT FUSELAGE SKIN IS CRACKED AROUND FASTENER, BS 1155 JUST ABOVE LONGERON 2R NEAR VERTICAL STABILIZER REPAIRED RT AFT FUSELAGE SKIN CRACK BS 1155 ABOVE L2R AS MARKED IAW ER/A 542364-14, REV ORIGINAL. ASSOCIATED ER/A 54-236514 ADDED FOR AC 9552.

Part: SHEAR TIE — CRACKED (BS 1152) · airframe 32,949 hrs · 22,416 cycles

CRACKED SHEAR TIE W/W SRM 53-30-08, REPAIR 8. REMOVED VERTICAL STIFFENER AT BS 1152, S2R FOR ACCESS IAW SRM 51-40-02, PG 1, PER 1 A. REPLACED SHEAR TIE AT BS 1152 S2R IAW SRM 51-40-02, PG 1, PAR 1 A, 51-40-08, PAR 3 AND 51-40-05, FIG 1 AND FIG 2. RE-INSTALLED VERTICAL STIFFENER AT BS 1252 S2R IAW SRM 51-40-02, FIG 1.

Part: ANGLE — CORRODED (BS 579) · corrosion level 2 · airframe 34,587 hrs · 23,683 cycles

ANGLE CORRODED S18R, BS 579. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, 53-00-55 REPAIR 1 AND DWG 82912047.

Part: ATTACH FITTING — CRACKED (BS 737) · airframe 32,949 hrs · 22,416 cycles

LEFT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY LBL 45, FS 737, IS CRACKED IN 2 PLACES AT BOTTOM END. REMOVED ATTACH FITTING FOR REPLACEMENT IAW SRM 51-41-02, PAGE 40. INSTALLED NEW FITTING ON 3925812-1 IAW SRM 5141-05, PAGE 1.

Part: FITTING — CORRODED (GIRT BAR) · airframe 32,949 hrs · 22,416 cycles

CORROSION ON GIRT BAR FITTING BS 157, 18R. REPLACED GIRT BAR FITTINGIAW SRM 51-41-01, PG 17.

Part: FRAME — CRACKED (BS 696) · airframe 32,949 hrs · 22,416 cycles

CRACK ON OTBD END OF FORMER IN RT SIDE CANTED KEEL AREA AT BS 696, ASSOCIATED HI-LOCS MARKED ON EXTERIOR SURFACE, CRACK CHECKED BY EDDY CURENT, M62937-0100-0091. REPLACED FORMER IN THE RT CANTED KEEL AREA AT BS 696 IAW SRM 51-41-02, PG 1, PARA 4 AND 51-41-05, PG 17, PARA 8.

Part: CUSP WEB — CORRODED (BS 550) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

BS 545, RBL 57, CUSP WEB UPPER & LOWER SURFACE CORRODED & BS 550 LWR SURFACE CORRODED. REF ORNRC 62937-0200-0125. REMOVED CORROSION IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS .020" MATERIAL REMOVED .014" MATERIAL REMAINING .006". GAUGE TAG NR 10371. OUT OF LIMITS IAW SRM 53-00-55, PG. 101, PAR 4, A. CUSP WEB PN 9930538-82 WILL BE REPLACED ON ORNC 62937-0200-0090, BS 503-BS 579.

Part: CUSP WEB — CORRODED (BS 526) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

BS 526, RBL 57, CUSP WEB UPPER & LOWER SURFACE CORRODED. REF ORNRC 62937-0200-0126 REMOVED CORROSION IAW SRM 53-00-00 PG 105, FIG 103. ORIGINAL THICKNESS .020" MATERIAL REMOVED .005" MATERIAL REMAINING, .015" GAUGE TAG 10371. DAMAGE OUT OF LIMITS IAW SRM 53-00-55, PG 101 PAR 4 A. CUSP WEB WILL BE REPLACED ON ORNRC 62937-0200-0090, BS 503, BS 579.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 32,949 hrs · 22,416 cycles

L1 DOOR SKIN LOWER EDGE IS WAVY AND CHAFED ALONG THE BOTTOM IN SEVERAL PLACES. TRIM/BLEND AND CHECK LIMITS. INSPECTED AND FOUND SKIN TO BE OIL CANNED AT LWR AFT CORNER OUT OF LIMITS IAW SRM 53-01-01, ALLOWABLE DAMAGE 1. FABRICATED REPAIR DOUBLER AND FILTER IAW SRM 52-10-01, REPAIR 2, FIG 201, PGS 201-203. ALLODINED REPAIR PARTS IAW AMM 51-10-00-370-803 SUBTASK 380-001. PRIMED REPAIR PARTS IAW AMM 51-10-00-370-803 SUBTASK 370-001. INSTALLED REPAIR PARTS IAW SRM 52-10-01, REPAIR 2, PAGES 201-203. RESTORED TOP COAT TO EXTERIOR IAW AMM 51-10-00/370.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 32,949 hrs · 22,416 cycles

RIGHT CUSP WEB HAS CORROSION AROUND FWD LIGHTING HOLE BETWEEN BS 446-465. BLENDED AREA IAW SRM 53-00-55, PG 101. FOUND TO BE OUT OF LIMITS. CUSP WEB REPLACED.

Part: CUSP WEB — CORRODED (BS 408-427) · airframe 32,949 hrs · 22,416 cycles

RT CUSP WEB HAS CORROSION AROUND SEVERAL FASTENERS BETWEEN BS 408-427. BLENDED AREA IAW SRM 53-00-55, PG 101, PAR 4A. FOUND TO BE OUT OF LIMITS. CUSP WEB REPLACED.

Part: FRAME — CRACKED (NOT REPORTED) · airframe 32,949 hrs · 22,416 cycles

FRAME CRACKED, REPAIRED THE FRAME SECTION IAW SRM 51-41-02, PG 1, STEP 4.

Part: ATTACH FITTING — CRACKED (BS 713) · airframe 32,949 hrs · 22,416 cycles

RIGHT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY RBL 45, FS 713 IS CRACKED WITH FASTENER HEADS SHEARED OFF AND RIGHT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY RBL 45, FS 737 IS CRACKED IN 2 PLACES AT BOTTOM END. BOTH FITTINGS MARKED. REF 62937-0100-0085: REPLACE FITTING AS RBL FS 713, PN 3925812-2 IAW SRM 51-41-05. REPLACED TILLING AT FS 737, RBL 45 IAW SRM 51-41-05, PAGE 17.

Part: CUSP WEB — CORRODED (BS 674) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

RIGHT CUSP WEB LOWER SURFACE IS CORRODED AROUND A FASTENER AT APPROXIMATELY RBL 62 AT FRAME BS 674. CLEAN, BLEND CHECK LIMITS 53-00-55. REMOVED 6 FASTNERS IAW SRM 51-40-02, PG 1, PARA 1A FOR ACCESS. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105 FIG 103 ORIGINAL THICKNESS =.020", MATERIAL REMOVED =.004" OUT OF LIMITS, IAW SRM 53-00-55, PG 101, PAR 4A, CUSP WEB, PN 9910151-164 WILL BE REPLACED ON NR 0111.

Part: CUSP WEB — CORRODED (BS 692) · airframe 32,949 hrs · 22,416 cycles

BS 692, RBL 58, CUSP WEB LOWER SURFACE CORRODED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS =.020" MATERIAL REMOVED =.004" OUT OF LIMITS IAW SRM 53-00-55, PG 101, PAR 4, A, CUSP WEB WILL BE REPLACED ON NR 0111. GUAGE TAG NR 6887.

Part: CUSP WEB — CORRODED (BS 700) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

BS 700, RBL 58 CUSP WEB LWR SURFACE CORRODED. CLEAN, BLEND CHECK LIMITS 53-00-55. REMOVED 3 FASTENERS IAW SRM 51-40-02, PG 1, PAR 1, A FOR ACCESS. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS=.020". MATERIAL REMOVED = .004". OUT OF LIMITS IAW SRM 53-00-55, PG 101, PAR 4. CUSP WEB, PN 9910151-164 WILL BE REPLACED ON NR 0111.

Part: CUSP WEB — CORRODED (BS 713) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

RIGHT CUSP WEB LOWER SURFACE HAS CORROSION AROUND 2 FASTENERS JUST FWD OF MAIN FRAME AT FS 713 APPROXIMATELY, RBL 62, MARKED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS=.020", MATERIAL REMOVED=.004". OUT OF LIMITS IAW SRM 53-00-55, PG 101, PAR 4, A CUSP WEB REPLACED.

Part: CUSP WEB — CORRODED (BS 670) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

BS 670, RBL 58 CUSP WEB LOWER SURFACE CORRODED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG. 105, FIG 103 ORIGINAL THICKNESS =.020" MATERIAL REMOVED = .004" OUT OF LIMITS, IAW SRM 53-00-55, PG 101, PAR 4, A CUSP WEB WILL BE REPLACED ON NR 0111. GUAGE TAG 6887.

Part: PAN — CORRODED (DOOR) · corrosion level 2 · airframe 32,949 hrs · 22,416 cycles

PAN AT LOWER ALC DOOR CUTOUT CORRODED. REPLACE PAN. REPLACED, AND INSTALLED LOWER AFT CARGO DOOR PAN AT DOOR CUTOUT. ALL WORK DONE IAW SRM 53-20-15, REPAIR NR 7, 51-41-02, 51-41-05, AND AMM 20-20-23-911-801, AND AMM 25-58-01-400-804.

Part: ANGLE — CORRODED (BS 900) · airframe 32,949 hrs · 22,416 cycles

RT SIDEWALL FUSELAGE BS 900, S18R CORRODED AT FLOOR SUPPORT ANGLE TO FUSELAGE SKIN. REPLACED SPLICE PLATE AT BS 900, STR 18R IAW SRM 51-41-05.

Part: LONGERON — CRACKED (BS 225) · airframe 32,233 hrs · 21,879 cycles

BS 225, LONGERON 17L CRACKED . REPLACED THE LONGERON IAW SRM 51-00-07.

Part: FRAME — CRACKED (BS 715) · airframe 31,384 hrs · 21,167 cycles

DURING SPECIAL VISIT FOR THE OVERWING FRAME INSPECTION, GVI AND HFEC CONFIRMED CRACK IN THE LT FRAME AT FS 715. FRAME WAS REPLACED IAW AMDS WC 5310-01436-03A. LP 1926584.

Part: ATTACH ANGLE — CRACKED (BS 715) · airframe 31,384 hrs · 21,167 cycles

DURING OVERWING FRAME INSPECTION, NOTED WEB ATTACH ANGLE AT FS 715 BELOW LT CENTER SEAT TRACK CRACKED. REPLACED WEB ATTACH ANGLE IAW SRM 51-40-02. LP 1926102.

Part: CUSP WEB — CRACKED (BS 674) · airframe 31,384 hrs · 21,167 cycles

DURING OVERWING FRAME INSPECTION VISIT, NOTED CUSP WEB MEMBRANE IS CRACKED AT FS 674 UNDER MID SEAT TRACK. REPLACED CUSP WEB MEMBRANE IAW SRM 51-40-02. LP 1925089.

Part: CUSP WEB — CRACKED (BS 655) · airframe 30,735 hrs · 20,664 cycles

PASSENGER CABIN BS 655, RBL 54 CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, REPAIR 4, FIG 203.

Part: CUSP WEB — CRACKED (BS 655) · airframe 30,735 hrs · 20,664 cycles

PASSENGER CABIN BS 655, LBL 54, CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, FIG 203.

Part: SIGN — CRACKED (CABIN) · airframe 28,565 hrs · 18,755 cycles

FWD CEILING EMERGENCY EXIT SIGN LIGHT CRACKED. R & R SIGN IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 28,441 hrs · 18,674 cycles

CEILING PANEL 222JC EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED WIRE IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,313 hrs · 17,393 cycles

FWD CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FORWARD CABIN LOWER EMERGENCY FLASHLIGHT BATTERY IAW AM/M . THIS CLEARS MDDR 238669.

Part: SEAL — MISSING (EMERGENCY EXIT) · airframe 26,306 hrs · 17,389 cycles

AFT EMERGENCY EXIT DOOR HANDLE MISSING SILVER SEALS. REPLACED SEAL AT REQUIED IAW AMM.

Part: HOLDER — BROKEN (GIRT BAR) · airframe 25,958 hrs · 17,171 cycles

R1 GIRT BAR HOLDER BROKEN. REMOVED AND REPLACED R1 DOOR GIRT BAR HOLDER PER MM.

Part: HOLDER — BROKEN (GIRT BAR) · airframe 25,961 hrs · 17,172 cycles

R1 GIRT BAR HOLDER BROKEN. REMOVED AND REPLACED R1 DOOR GIRT BAR HOLDER PER M/M.

Part: COVER — MISSING (CABIN) · airframe 25,293 hrs · 16,720 cycles

AFT OVERHEAD EMERGENCY EXIT COVER MISSING. INSTALLED COVER PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 25,425 hrs · 16,808 cycles

EMERGENCY EXIT SIGN LOOSE NEAR ROW 1. SECURED SIGN PER AMM.

Part: LANYARD — FRAYED (L1 DOOR) · airframe 24,449 hrs · 16,155 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD FRAYED. REMOVED AND REPLACED LANYARD PER MM.

Part: COVER — BROKEN (CABIN) · airframe 24,388 hrs · 16,112 cycles

AFT EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,230 hrs · 16,075 cycles

FWD EEPLS SECTION INOP. RELAMPED EEPLS PER MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 218, LBL 45. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FRAME CORRODED AT BS 954, RBL 2. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 220, BETWEEN BL 0 TO LBL 6. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR WEB CORRODED BETWEEN BS 220 TO BS 209, BL 0. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

STRINGER CORRODED AT BS 954, STR 29L. REPAIRED STRINGER PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 34 TO LBL 26. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 198 TO BS 220, RBL 45. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 178, LBL 5. REPAIRED SUPPORT PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

SUPPORT ANGLE CORRODED AT BS 220, RBL 60. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 29L TO STR 29R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FRAME CORRODED AT BS 908, BETWEEN STR 29L TO STR 29R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 30R TO STR 29R. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 220, BETWEEN RBL 9 TO RBL 38. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,318 hrs · 16,067 cycles

FLOOR SUPPORT CORRODED AT BS 220, BETWEEN LBL 29 TO LBL 17. REPAIRED SUPPORT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

THE 1D ESCAPE PATH LIGHT INOPERATIVE WILL NOT ILLUMINATE. REMOVED & REPLACED LIGHT ASSY AT 1D REF CH 33-51-04 OF THE B717 MM.

Part: CABLE — DETACHED (GIRT BAR)

CABLE ASSY THAT ATTACHS FROM L1 GIRT BAR TO THE SLIDE DOOR IS NO LONGER ATTACHED ON PAX ENTRY DOOR (REQUIRES AWI). INSPECTED GIRT BAR AND LANYARD ASSY AS PER AMM 25-61 NO DEFECTS FOUND.

Part: SIGN — UNSECURE (CABIN)

EXIT ROW SIGN OVER ROW 21 NOT SECURED. SECURED SIGN AS REQUIRED.

Part: FRAME — CRACKED (BS 1178)

AFT FUSELAGE INT TAIL AREA FOUND CRACK AT CANTED FRAME RT AREA STA 1178.225 BETWEEN STA 16R AND 17R. INSTALLED FORMER ANGLE REPAIR PER SRM 51-70-11 FIG 201.

Part: SKIN — DENTED (FUSELAGE)

DENTED FUSELAGE AT STA 245 AND L STR 16 TO L STR 18. INSTALLED FLUSH REPAIR LT FUSELAGE BETWEEN STA 229 TO STA 263.55 AND LONGERON 16 TO 18 LEFT HAND, IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED DOUBLER 2024T3.025 SIZES 50" X 6", 2024T3.050 SIZE 34.25" X 14.125", 2024T3.063 SIZE 34.75" X 4".

Part: VENT — CRACKED (RIGHT)

CRACK ON VENT BOX RIGHT HAND SECTION AFT CORNER. INSTALLED REPAIR OF AFT FUSELAGE RIGHT SIDE VENT BOX DRAIN PAN IAW T/C 17-5320-2023 FIG 1.

Part: FRAME — DENTED (BS 1178)

AFT FUSELAGE LT CANTED FRAME IS CRACK IN TWO PLACES AT STA 1178.225 BETWEEN L-16L TO 18L. INSTALLED DOUBLER REPAIR AT LEFT CANTED FRAME AT STA 1178.225 BETWEEN L-16L TO 18L IAW B717 SRM 51-70-01 FIG 201. MATERIAL USED 7075-080; HEAT TREATED TO T6 IAW AVBORNE G-PS 98PMS.247PS-01 AND 7075T6 SIZE OF REPAIR 15 X 4 INCHES.