N964AT

Part: TRANSCEIVER — FAULTED (RADIO ALTIMETER) · airframe 61,992 hrs · 44,012 cycles

SHIP 9523-ATO- ABORTED TAKE-OFF DUE TO RECEIVING A STICK PUSHER FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH RADIO ALTIMETER TRANSCEIVERS AND PERFORMED ALL APPLICABLE RETURN TO SERVICE TESTS. (LP 7808224)

Part: NONE — NONE (NONE) · airframe 60,683 hrs · 42,903 cycles

-AD- OVERWEIGHT LANDING. LW - 110.1. MAX 110.0. VERTICAL SPEED AT TOUCHDOWN ~ 50 FT/MN. WT EXITING RUNWAY INDICATED 109.8. PERFORMED B717 AMM 05-51-04 210-801 A-1 CHECK INSP FOR HARD OR OVERWEIGHT LANDING. FLOW CHART FIGURE 602 USED FOR OVERWEIGHT LANDING ONLY. C/W A-1 CHECK. NO DAMAGE FOUND. C/W B717 W/C 5312- 01194-03 FOR AD MANDATED INSP OF THE CANTED BULKHEAD STATION 1178.225. NO DAMAGE FOUND. OK FOR CONTINUED SVC. (LP #6731692)

Part: WARNING MESSAGE — FALSE INDICATION (PSEU) · airframe 58,939 hrs · 41,406 cycles

SHIP 9523 -MISC/DE- ON CLIMB OUT, AT APPROXIMATELY 5,000 FEET, THE "PSEU FAIL" MESSAGE ILLUMINATED. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED WITH ATC DUE TO THE PSEU FAILURE. THE PSEU RETURNED TO NORMAL ON DESCENT AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE OPERATIONAL CHECK WAS GOOD. (LP #5455052)

Part: SPAR — CRACKED (LT WING) · airframe 58,618 hrs · 41,125 cycles

CRACK ON REAR SPAR LOWER SECTION LH WING AT XRS=214.000. SUMMARY OF NRC 00651: REAR SPAR LOWER SECTION LH WING AT XRS=214.000 WAS REPAIRED PER ERA 615443-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615443 ADDED FOR AC 9523. (LP #0188635)

Part: PAN — CRACKED (DOOR FRAME) · airframe 58,618 hrs · 41,125 cycles

CRACKED PAN AND FITTING ON BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00156: FITTING REPLACED PER B717-200 SRM 51-41-03-0G, 51-41-01-0G, AND 51-41-05-0G. PAN BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REV 6 AND ERA 614439-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0185710)

Part: PAN — CRACKED (AFT CARGO) · airframe 58,618 hrs · 41,125 cycles

CRACKED PAN AND FITTING ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00154: FITTING WAS FABRICATED PER DWG 3914025 REV C AND PAN ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REV 6 AND ERA 614439-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-614439 ADDED FOR AC 9523. SUMMARY OF NRC 00154: FITTING WAS FABRICATED PER DWG 3914025 REV C AND REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-03-0G, AND PAN ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REV 6 AND ERA 614439-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614439 ADDED FOR AC 9523. (LP #0184279)

Part: ANGLE — CORRODED (BS 200-226) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION WAS FOUND ON LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN. SUMMARY OF NRC 00571: CORROSION LEVEL 2. LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3. (LP #0181235)

Part: FRAME — CRACKED (BS 1133) · airframe 58,618 hrs · 41,125 cycles

CRACK ON FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00146: FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1 EXAMPLE A. (LP #0181239)

Part: ANGLE — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP #0179772)

Part: WEB — CRACKED (BS 1053) · airframe 58,618 hrs · 41,125 cycles

CRACKS ON INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR. SUMMARY OF NRC 00255: INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G PROCEDURE GENERAL, 51-41-05-0G, AND 51-41-03-0G.

Part: CARGO TRACK — CORRODED (BS 889) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR TRACK LH STA Y=889, AFT CARGO WAS REMOVED AND REMAINDER TRACK IS OUT OF LIMITS. SUMMARY OF NRC 00648: CORROSION LEVEL 2. FLOOR TRACK LH STA Y=889, AFT CARGO WAS REPAIRED B717-200 SRM 53-20-52-2R PROCEDURE 4 FIG 201. (LP #0178275)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 58,618 hrs · 41,125 cycles

CRACK ON INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR. SUMMARY OF NRC 00239: INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR WERE REPAIRED PER PRI 614520-14 REV 5 AND ERA 614520-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614520 ADDED FOR AC 9523. (LP #0177479)

Part: LONGERON SPLICE — CORRODED (BS 889-908 L24L) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON LONGERON SPLICE 24L BTW STA Y=889 AND STA Y=908 IN REFERENCE TO NRC 00644. SUMMARY OF NRC 00650: CORROSION LEVEL 2. SPLICE ON LONGERON 24L BTW STA Y=889 AND STA Y=908 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0176297)

Part: CUSP WEB — CORRODED (BS 200-294) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB. SUMMARY OF NRC 00361: CORROSION LEVEL 2. LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB WAS FABRICATED AND REPLACED PER DWG 9936535-3 REV CR AND PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08- 0G. REFER TO NRC 00571 AND REFER TO NRC 00619. (LP #0174840)

Part: FLOOR SUPPORT — CORRODED (BS 186-195) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SUPPORT (1 EA) (UPPER/ LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00408: CORROSION LEVEL 2. FLOOR SUPPORT (1 EA) (UPPER/LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-02-05-0G AND DWG 9936534 REV I. (LP #0174571)

Part: DOUBLER — CORRODED (BS 844-859) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN. SUMMARY OF NRC 00395: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN WAS REPLACED PER B717 SRM 53-20-70-2R PROCEDURE 1 REPAIR 1. (LP #0173843)

Part: STRINGER SPLICE — CORRODED (BS 908 L26-27L) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON PREVIOUS REPAIR SPLICE AT STA Y=908 BTW LONG 26L AND LONG 27L IN AFT CARGO COMPARTMENT. SUMMARY OF NRC 00647: CORORSION LEVEL 2. SPLICE OF STA Y=908 BTW LONG 26L AND LONG 27L WAS REPLACED PER B717-200 DGW 9971183 REV 'J'. (LP #0174281)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 407: CORROSION LEVEL 2. FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717 SRM 51-41-02-0G PAR 4, 51-10-05-0G PAR 8, AND DWGS 9936534-11 AND 9936534-7 REV BW. (LP #0174332)

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00413: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G PAR 8. (LP #0173671)

Part: WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND REPLACED PER B717 DWG 9936534-5 REV BN AND B717-200 SRM 51-41-02-0G AND 51-41-02-05-0G. (LP #0174758)

Part: ANGLE — CORRODED (BS 180) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION WAS FOUND ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH, PAX CABIN. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CUSP ANGLE ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH WAS REPAIRED PER B717 SRM 53-00-55-2R-3. (LP #0173416)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 58,618 hrs · 41,125 cycles

FASTENER HOLES AND COUNTERSINKS ARE ELONGATED OUT OF LIMITS ON 1/4 FASTENERS ROW AT VERT STAB FIX LE. ALSO, ON VERT STAB REMOVABLE LE STA ZFS=52.267 REF SERVICE GENERAL DRAWING SG95550001. SUMMARY OF NRC 00538: FASTENER HOLES AND COUNTERSINKS AT VERT STAB FIX LE AND ALSO ON VERT STAB REMOVABLE LE STA ZFS=52.267 WERE REPAIRED PER DRAWING SG95550001 REV B. ASSOCIATED AA 5530-01048 ADDED FOR AC 9523. (LP #0171014)

Part: SEAT TRACK — CORRODED (BS 200-219) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON SEAT TRACK X=-44.5 BTW STA 200-219 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00403: SEAT TRACK SECTION X=-44.5 BTW STA 200-246 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED OFF PER B717-200 SRM 53-20-52-2R PROCEDURE 5. (LP #0169174)

Part: SKIN — DAMAGED (BS 256 S17-18L) · airframe 58,618 hrs · 41,125 cycles

CREASES WERE FOUND ON REPAIR SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH PER B717 SRM 53-00-01-02 REPAIR 6 PAR. 7. SUMMARY OF NRC 00270: SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH WAS REPAIRED PER B717-200 SRM 53-00-01-2R REP 6. SPECIFIC MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 8,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 8,000 CYCLES, PER B717 SRM 53-00-01-2R-6, PAR 7A. (LP #0168990)

Part: SKIN — GOUGED (BS 237 L18-19L) · airframe 58,618 hrs · 41,125 cycles

GOUGE AND DENT ON FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L. SUMMARY OF NRC 00615: FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L WAS PERMANENT REPAIRED PER B717-200 SRM 53-02-01-2R-1 FIG 202. THE PERMANENT REPAIR SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 8,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 8,000 CYCLES, PER B717 SRM 53-02-01-2R-1, PAR 6A. (LP #0167362)

Part: WEB — PUNCTURED (BS 160-200) · airframe 58,618 hrs · 41,125 cycles

PUNCTURES (2 EA) ON WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00415: WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R. (LP #0163433)

Part: WEB — CRACKED (BS 1200) · airframe 58,618 hrs · 41,125 cycles

WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION. SUMMARY OF NRC 00599: WEB FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION II. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #0162948)

Part: WEB — CRACKED (BS 1200) · airframe 58,618 hrs · 41,125 cycles

WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION. SUMMARY OF NRC 00598: WEB FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #0162944)

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 58,618 hrs · 41,125 cycles

CRACK ON RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00397: RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0161271)

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORT (UPPER/ LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-01-0G AND DWG 9936534 REV BW. (LP #0162152)

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SUPPORTS AT W1 AREA STA 200 BTW X=7 AND X=-44 IN REF TO NRC 00401. SUMMARY OF NRC 00539: CORROSION LEVEL 2. FLOOR SUPPORTS WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0160759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK ON LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB. SUMMARY: LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0154369)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK OF 0.125 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00205: OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B) WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND AMDS 5310-01436-03A. ASSOCIATED AA 5310-01436 ADDED FOR AC 9523. (LP #0154349)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK ON FRAME STA 1037 LONG 17 RH AT PAX CABIN. SUMMARY OF NRC 00289: FRAME STA 1037 LONG 17 RH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0144771)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON CABIN FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT CPAX. SUMMARYOF NRC 00600: CORROSION LEVEL II. FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND DWG 9981477-15 REV L. (LP #0145572)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,618 hrs · 41,125 cycles

CORROSION ON FLOOR SKIN LOWER SURFACE BTW STA 389 AND X=-58 AT FWD CARGO DOOR JAMB AREA. SUMMARY OF NRC 00203: CORROSION LEVEL 2. FLOOR SKIN LOWER SURFACE BTW STA 389 AND X=-58 AT FWD CARGO DOOR JAMB AREA WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0144064)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK ON RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00445: RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROC 2 PAR 4. (LP #0144067)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK ON RH CUSP MEMBRANE ON STA Y=813 AND X =-44 AT PAX CABIN. SUMMARY OF NRC 00446: RH CUSP MEMBRANE ON STA Y=813 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0138861)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

TOOL MARK ON CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PAX CABIN. SUMMARY OF NRC 00448: CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 208. (LP #0132552)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,618 hrs · 41,125 cycles

CRACK ON INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOOR. SUMMARY OF NRC 00136: INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0122246)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,116 hrs · 40,720 cycles

SHIP 9523 -HYD/DE- THE CREW RECEIVED A "HYD R QTY LOW" MESSAGE AT TOP OF CLIMB. THEY WERE UNABLE TO REPRESSURIZE THE SYSTEM. THE QRH WAS COMPLIED WITH AND PERFORMED THE ALTERNATE GEAR EXTENSION (DUE TO A RIGHT HYDRAULIC SYSTEM LOW QUANTITY). AN EMERGENCY WAS DECLARED WITH ATC AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE ELECTRIC AUXILIARY HYDRAULIC PUMP AND THE RIGHT MAIN LANDING GEAR DOOR (DUE TO RUNWAY CONTACT ON LANDING). THE SHIP HAS RETURNED TO SERVICE. (LP #4580142)

Part: POWER SUPPLY — INOPERATIVE · airframe 56,330 hrs · 39,145 cycles

THE EXTERIOR EMERGENCY LIGHTS IN THE AFT FUSELAGE WILL NOT EXTINGUISH. MAINTENANCE REPLACED THE AFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #9017959)

Part: NONE — NONE · airframe 55,857 hrs · 38,718 cycles

THE LOWER AFT OVERWING EXIT DOOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW GOOD. (LP #8954064)

Part: DIFFUSER — MISSING · airframe 54,988 hrs · 37,917 cycles

EMERGENCY EXIT COVER DIFFUSER MISSING. MAINTENANCE RE-INSTALLED 1L DOOR EXIT SIGN COVER. (LP #8625158)

Part: NONE — NONE · airframe 54,149 hrs · 37,167 cycles

MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS, FROM ROW 15-19, WERE INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AT STA 645 WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8121299)

Part: NONE — NONE · airframe 53,918 hrs · 36,970 cycles

FOUND FORWARD CARGO DOOR SKIN LEAKING AT LOWER EDGE APPROXIMATELY STA Y 408. - M - SUMMARY SEE NRC 001-0050:5230-2004/003 00364: REPLACED FWD CARGO DOOR REF B717 AMM 52-31-01. (LP #2041378)

Part: NONE — NONE · airframe 53,918 hrs · 36,970 cycles

THE TAIL CONE RELEASE CABLE TURNBUCKLE IS BENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/001 00349: REPLACED BENT TURNBUCKLE REF B717 AMM 53-52- 01. (LP #2036500)

Part: NONE — NONE · airframe 53,918 hrs · 36,970 cycles

LEFT HAND AFT EMERGENCY DOOR JAMB HAS DAMAGE AT BOTTOM. POSSIBLE CRACK. REFER TO NRC 98: W/O P324720220210922, COMPLIED WITH ER/A 595511-14 TO REPAIR DAMAGE IN DOOR JAMB. (LP #2036011)

Part: NONE — NONE · corrosion level 2 · airframe 53,918 hrs · 36,970 cycles

FWD CARGO DOOR JAMB: 6 AREAS OF CORROSION LOCATED ON DOOR JAMB. -M- SUMMARY SEE NRC 001-0371:5230-2001/011 00187: CORROSION LEVEL 2, BLENDED AND CHECKED LIMITS REF B717 SRM 51-10-06. INSTALLED A NEW FWD CARGO LOWER DOOR JAM PAN, LOWER SCUFF PLATE, FWD AND AFT SPLICE, AND TWO FITTINGS PER B717 SRM 53-20-15-2R-6 REPAIR 6. (LP #2029430)

Part: NONE — NONE · corrosion level 2 · airframe 53,918 hrs · 36,970 cycles

1R DOOR AFT GIRT BAR FITTING HAS CORROSION. SUMMARY SEE NRC 042-0023:5310-2005/006 00274: 1R DOOR AFT GIRT BAR FITTING CORROSION FOUND TO BE BEYOND LIMITS PER B717 SRM 53-00-00-1A FIG 103. 1R DOOR AFT GIRT BAR FITTING WAS REPLACED WITH NEW PART REF BOEING DWG 9936534. (LP #2022214)

Part: NONE — NONE · airframe 53,918 hrs · 36,970 cycles

ERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 3000 FC THEREAFTER. ACCOMPLISH SECTION II CONCURRENTLY WITH EM 5530-01048-02. ASSOCIATED ER/A 95-590337 ADDED FOR AC 9523. (LP #2018828)

Part: NONE — NONE · airframe 53,918 hrs · 36,970 cycles

ERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. ACCOMPLISH SECTION III WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 2400 FC THEREAFTER. ASSOCIATED ER/A 95-590337 ADDED FOR AC 9523. (LP #2018832)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 53,573 hrs · 36,632 cycles

THE EXIT SIGN COVER FELL OFF. MAINTENANCE REINSTALLED THE EXIT LIGHT SIGN IAW B717 AMM 33-51. (LP #7366767)

Part: HYDRAULIC SYSTEM — LEAKING (LEFT) · airframe 53,490 hrs · 36,550 cycles

SHIP 9514 - THE FLIGHT CREW DECLARED AN EMERGENCY WHILE ON APPROACH DUE TO THE LEFT HYDRAULIC SYSTEM LOSS OF PRESSURE FROM EITHER THE LT ENGINE DRIVEN PUMP OR THE TRANSFER PUMP. CORRECTIVE ACTION: MAINTENANCE BLED THE LT HYDRAULIC SYSTEM AND ALSO REPLACED BOTH THE LT ENGINE DRIVEN HYDRAULIC PUMP AND THE LT SYSTEM RESERVOIR. (LP #7366708)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,412 hrs · 36,475 cycles

THE L&R AFT OVERWING EXIT UPPER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-230 AND BATTERY PER B717 AMM 33-51. TESTS GOOD. (LP #7807523)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,269 hrs · 36,339 cycles

BOTH OF THE OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCR REPLACED THE AFT CARGO EMERGENCY BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7336449)

Part: SWITCH — NO TEST (EMERGENCY LIGHTS) · airframe 52,949 hrs · 36,060 cycles

DURING SERVICE CHECK, FOUND F/A EMERGENCY LIGHT SWITCH NOT TESTING. MAINTENANCE REPLACED THE F/A PANEL SWITCH, NO HELP REF B717 WDM 33-51. REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK 5-125 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7408876)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,531 hrs · 35,733 cycles

THE EMERGENCY LIGHTS WOULD NOT TEST FROM F/A SWITCH. MAINTENANCE FOUND THE OVERWING BATTERY PACK LOW AND REPLACED IT. THE EMERGENCY LIGHTS NOW CHECK GOOD FROM BOTH THE F/A AND COCKPIT POSITIONS. (LP #7577565)

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR LIGHTS) · airframe 52,508 hrs · 35,709 cycles

BOTH LEFT & RIGHT EXTERIOR EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMEGRENCY EVACUATION LIGHT BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7577552)

Part: SKIN — CRACKED (RH VERT STAB) · airframe 52,437 hrs · 35,648 cycles

CRACK DETECTED ON OPEN HOLE BY HFEC ROUTINE CARD 5530-01048-02, STEP 14, VERT STAB L/E SKIN AND FRONT SPAR CAP. CRACK INDICATION IS FIRST HOLE GOING UP R/H SIDE SKIN SPLICE L/E ZFS 52.267. MAINTENANCE REMOVED VOR #1 RH / LH AND VOR #2 RH / LH PER B717 AMM 34-32. REMOVED L/E VERT STAB PER B717 AMM 34-32. INDICATION OF DEFECT/CRACK NOTED PER B717 NDT SPM PART 6-10-01.003. C/W PRI 590337-14AD REV O DATED 26FEB21 AT 1330E STEPS 1 THRU 5. PERFORMED NDT OPEN HOLE HFEC PER PRI 590337-14AD, REV O DATED 26FEB21 1330E, STEPS 1-5. NO CRACK INDICATION AT RH SPAR CAP L/E STA ZFS 52.267. C/W PRI 590337-14AD REV 1 STEP 6. RECONNECTED RUDDER LIMITER PITOT TUBE AND VOR COAXIAL CABLE AT LWR AND UPPER CONNECTORS PER B AMM 55- 32. REINSTALLED L/H AND R/H LWR VOR ANT PER B717 AMM 34 -32 THRU STEP F(1)(F).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,411 hrs · 35,627 cycles

THE OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHTS BATTERY PER B717 AMM 33-51. THE OPERATIONAL CHECK IS NOW GOOD. (LP #7543697)

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,379 hrs · 35,603 cycles

THE EMERGENCY LIGHT SWITCH AT THE ATTENDANT PANEL IS INOPERATIVE. LIGHTS WILL NOT TURN ON WHEN SWITCHED TO ARM (ON). TROUBLE SHOT PER B717 SDS 33-51-00-003 & WDM 33-51-11 AND SUSPECT B5-125 BATTERY PACK. REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY PACK PER B717 AMM 33-51 AND NOW THE OPERATIONAL CHECK IS GOOD.

Part: SLIDE — DETACHED (TAILCONE) · airframe 51,981 hrs · 35,281 cycles

MAINTENANCE FOUND THAT THE AFT TAIL COMPARTMENT EMERGENCY ESCAPE SLIDE WAS DETACHED FROM THE AIRCRAFT. THE TAIL CONE SLIDE WAS REPLACED, PER AMDS WORKCARD 2561-9006. RII INSPECTION OF TAILCONE SLIDE INSTALL WAS COMPLIED WITH (QC 5158) 598514. AIRCRAFT IS OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 237 S19-20L) · airframe 58,618 hrs · 41,125 cycles

FUSELAGE GOUGE AND DENT AT STA 237 BETWEEN STRINGERS 19L AND 20L AT 8 O CLOCK POSITION STRAIGHT BELOW L/E OF SECOND WINDOW PLUG. BLENDED GOUGE. DENT DAMAGE WITHIN LIMITS PER B717 SRM 53-01-01 CONDITION 1B. ACTUAL DENT LOCATION IS BETWEEN L18L AND L19L. INTERNAL STRUCTURE DVI MUST BE ACCOMPLISHED WITHIN 30 DAYS. AFTER INITIAL DVI ACCOMPLISHED CHANGE REPETITIVE DVI TO 24 MONTH INCREMENT. ADDED INI & CORRECTED MASK PER SRM 53-01-01 AD3. AREA OF DAMAGE IS ALLOWABLE DAMAGE PER B717 SRM 53-01-01. A/C OK FOR SVC FOR ANOTHER 24 MONTHS. ON 23JAN24 FUSELAGE SKIN AT STA 237 BTWN LONG 18L-19L WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-02-01-2R-1 FIG 202. (LP #2503537)

Part: MODULE — INOPERATIVE (CABIN) · airframe 51,902 hrs · 35,205 cycles

DURING EMERGENCY LIGHT BATTERY PACK REPLACEMENT, FOUND BATTERY POWER SUPPLY MODULE FOR SEATS 10-12 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY MODULE PER B717 AMM REF 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7161872)

Part: INTERCOSTAL — CORRODED (BS 994-1022) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

INTERCOSTAL AT STRINGER 26L AND LOCATED BETWEEN FS994 AND FS 1022 IS CORRODED. REPLACED INTERCOSTAL PER B717 SRM 51-40. RII COMPLETED QC 1988. (LP #1467731)

Part: SHEAR TIE — CORRODED (BS 946) · airframe 51,607 hrs · 34,966 cycles

FRAME Y946 BETWEEN 23-24L FRAME FORMER FOOT CORRODED. BHEC INSPECTION OF AREA SHOWED NO DEFECT NOTED PER B717 NDT SPM PART 06-10- 01.003 DETLA QC 1991. INSTALLED FABRICATED FRAME FORMER FOOT IAW SRM 53-20 -06-2R. SKIN FASTENERS IN FORMER FOOT INSTALLED.

Part: STRINGER SPLICE — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 28L HAS TWO CORRODED SPLICE FITTINGS LOCATED BETWEEN F.S. 898 AND F.S. 1053. AND LONGERON 28L FROM F.S. 898 TO F.S. 1053 NEEDS REPLACED. REPLACED STRINGER 28L QC2037 REPLACED 28L LONGERON AND SPLICE FITTINGS FROM F.S. 898-1053 IAW B717 SRM 51-40.

Part: DOUBLER — CORRODED (PRESS BULKHEAD) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

REMOVED DOUBLER ON LOWER INBD OF PRESSURE BULK HEAD DUE TO CORROSION. REQUIRES OPEN HOLE INSP BHEC. NO CRACKS NOTED QC1988. REPLACED WITH NEW DOUBLER TO AFT PRESSURE BULKHEAD PER SRM 51-40.

Part: STRINGER — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 24L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS 1053. REPLACED FWD PART OF LONGERON SPLICE PER SRM 51-41. REPLACED AFT SHOVEL FITTING AT FS 1053 AND LONGERON. REPLACED LONGERON 24L FS 1022 TO FS 898 PER SRM 51-41.

Part: STRINGER — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 27L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS1053. REPLACED STRINGER 27L BETWEEN FS 898-1053 IAW B717 SRM 51-40.

Part: TEE FITTING — CORRODED (BS 1053 BULKHEAD) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

AFT PRESSURE BULKHEAD T-CORD HAS CORROSION Y1053 R29-L27. BHEC REQUIRED. NO CRACKS NOTED QC 1988. REPLACED THE AFT PRESSURE BULKHEAD T-CORD PER B717 SRM 51-40. RII COMPLETE ON T-CORD INSTALL QC 5137. (LP #1467725)

Part: LONGERON — CORRODED (BS 898-946) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

LONGERON L28RT FROM FS 946 TO FS 898 NEEDS REPLACED DUE TO CORROSION. INSTALLED 28RT LONGERON PER B717 SRM 51-41. INSTALL COMPLETE. (LP #1467794)

Part: STRINGER — CORRODED (BS 1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 28L END FITTING AT F.S. 1053 IS CORRODED. FITTINGS INSTALLED PER B717 SRM 51-40. RII COMPLETED QC1988. (LP #1467826)

Part: DOUBLER — CORRODED (BS 946-975) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

AT STRINGERS 29R TO 30R BETWEEN BS 946 TO 974, THERE IS CORROSION ON THE INTERNAL DOUBLER. REPAIRED PER ER/A 584183-14 REV O.

Part: SKIN — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FUSELAGE SKIN HAS MULTIPLE AREAS OF CORROSION AND FASTENERS PULLING THROUGH FRAME Y898-Y1053 R29-L26. REPLACED SKIN PANEL IAW SRM 51-40. RII COMPLETED.

Part: LONGERON — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

LONGERON 26L HAS MULTIPLE AREAS OF CORROSION BETWEEN BS 898 AND 1053. REPLACED THE LONGERON IAW SRM 53-00-05-02-R2 AND ER/A 584398-14, REV ORG.

Part: LONGERON — CORRODED (BS 898-1053) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

LONGERON 25L HAD MULTIPLE AREAS OF CORROSION BETWEEN BS. 898 AND 1053. REPLACED THE LONGERON SPLICE IAW SRM 53-00-05-02 R2, AND ER/A 584398-14, REV ORG.

Part: FRAME ANGLE — DAMAGED (BS 1002) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

AT BS 1002 BETWEEN STRINGER 29 AND 30L, THERE IS A FRAME SPLICE ANGLE WITH DAMAGE BEYOND LIMITS. REPLACED FRAME ANGLE IAW SRM 51-41.

Part: INTERCOSTAL — CORRODED (BS 1022-1037) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

INTERCOSTAL HAS CORROSION ON FRAMES 1022-1037 AT L25. REPLACED THE INTERCOSTAL IAW SRM 51-41.

Part: FORMER — CORRODED (BS 1002) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FORMER AT FRAME 1002 AND FRAME 1002 CUT AND REMOVED DUE TO CORROSION. REPLACED FRAME 1002 BETEEN STRINGER L21-30 AND SPLICE AT L21 IAW B717 SRM 53-20-07-2R-3. RII COMPLETED BY QC2037. (LP #1455181)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FRAME FORMER Y927 R29-L23 IS CORRODED. ALSO FRAME 927 IS CORRODED. REMOVED FRAME FORMER AND FRAME AT SPLICE. APPLIED TREAT / SURFACE PROTECTION IAW SRM 51-10. COMPLETED FRAME FORMER & FRAME / SPLICE WAS INSTALLED IAW SRM 53-20-07 & 51-41-05. RII COMPLETED. OK FOR SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FRAME FORMER CORRODED Y946 R29-L26. REPLACED FRAME FORMER AT Y946 R29-L26 PER SRM 51-41-05. RII COMPLETED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FRAME FORMER Y974 CORRODED. REPLACED 2 EA FORMERS FROM FRAME AT Y974 FROM L23R-L29L PER SRM 51-41. RII BYBACK C/W.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FRAME FORMER Y954 R29-L24 CORRODED. REMOVED FRAME FORMER AT Y954 R29-L24. CORROSION LEVEL 2, INSTALLED FRAME FORMERS PER SRM 51-41. RII COMPLETED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 30 HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER #30 IAW SRM 51-40. RII COMPLETE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,607 hrs · 34,966 cycles

STRINGER 30 HAS THREE STRINGER FITTING WITH CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER 30 BUT ONLY ONE SPLICE REQUIRED. INSTALLED STRINGER SPLICE FITTING BETWEEN FS 898-FS1053 IAW SRM 51-40. RII COMPLETE.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER "LONGERON" 29L IS CORRODED FROM STA 1002 TO 898. REPLACED LONGERON 29L PER SRM 51-41. INSTALLATION FROM FS 898 TO FS 1053 COMPLETE. RII COMPLETE.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

STRINGER 29L HAS TWO CORRODED SPLICE FITTINGS LOCATED BETWEEN FS898 AND FS1053. REPLACED SPLICE FITTINGS PER SRM 51-41. INSTALLATION COMPLETE. RII COMPLETE.

Part: FORMER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

FRAME FORMER Y994 L29-L23 CORRODED. REMOVED FORMER FROM Y994 L20-25, DRILLED, TREATED, AND FITTED FORMER Y994 L20-L25. OK TO INSTALL FORMER. INSTALLED FRAME FORMER ON Y994 FROM L20-L25 PER SRM B717 51-41. RII COMPLETE. (LP #1436253)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,607 hrs · 34,966 cycles

FLOOR SUPPORT AT FR908 FROM L-L27 THRU L-L23 IS CRACKED. BHEC REQUIRED PRIOR TO INSTALLING NEW PART. NO CRACK NOTED BUT INSTALLED NEW FLOOR SUPPORT PER SRM 51-41. OK FOR SVC. (LP #1427718)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,607 hrs · 34,966 cycles

INTERNAL SKIN DOUBLER LOCATED BETWEEN STRINGER 22L AND STRINGER 26L AND BETWEEN FS 994 AND FS 1053 HAS MULTIPLE AREAS OF CORROSION ON DOUBLER. REMOVED CORROSION, COMPLIED WITH PRI ER/A 584182-14 REV O STEP 7. C/W STEPS 8 AND 9 OF ER/A 584182-14 REV O. RII COMPLETED BY QC1988. ASSOCIATED ER/A 14-584182 ADDED FOR AC 9523. (LP #1427736)

Part: BOLT — FROZEN (RT WING TE FLAP) · airframe 49,830 hrs · 33,711 cycles

RT WING, OUTBD FLAP HINGE PIVOT BOLT FROZEN, SEALER BROKEN INDICATING FROZEN RUSTED BOLT. REMOVED MIDDLE AND OUTBOARD HINGE BOLTS REF B717 AMM 27-50-01. REMOVED SEALER AND FOUND I/B FITTING LEG BOLT HOLE ELONGATED REF B717 AMM 27-50-01. MACHINED O/B LUG OUTER FACE AND I/B LUG BORE AND INNER FACE BEYOND REPAIR LIMITS PER OHM 27-50-5. COMPLIED WITH PRI 576897-14 REV. O & 1, FINAL ER/A 576897-14 REV. O MATCHES PRI 576897-14 REV. O & REV. 1. REF NRC 140 C-CK. REPLACED BUSHING IAW PRI 576897-14 #2. INSTALLED O/B WING FLAP HINGE BOLT, CENTER WING FLAP HINGE BOLT, AND O/B ACTUATOR CYLINDER BOLT IAW B717 AMM 27-50-01. RESEALED BOTH SIDE OF BOLT REF B717 AMM 27-50 01. (LP #1017937)

Part: SKIN — CORRODED (LT WING) · airframe 49,830 hrs · 33,711 cycles

LT WING UPPER SKIN CORROSION AT REAR SPAR. FWD OF O/B SPOILER I/B END. REPAIRED COMPLIED WITH PER ER/A 575477-14 REV. O.

Part: BUSHING — DAMAGED (RT WING TE FLAP) · airframe 51,965 hrs · 35,267 cycles

THE BEARING HOLE WAS FOUND ELONGATED ON THE OUTBOARD IDLER HINGE FITTING OF THE TRAILING EDGE FLAP ON THE RT WING. THIS DAMAGE WAS REPAIRED, PER ERA 576897-14 REV ORIGINAL. THIS REPAIR IS TIME-LIMITED TO 24 MONTHS OF SERVICE. THIS LOG PAGE CAN NOW BE CLOSED PER ER/A 576897-14 REVISION A. STAGE II APPROVAL GIVEN VIA 8100-9 FORM FOR REPAIR ACCOMPLISHED IN SECTION I OF ERA 576897-14. REPAIR IS NOW TRACKING STAGE II APPROVAL VIA LOG PAGE #1642865.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,762 hrs · 33,670 cycles

LT AND RT OVER WING THRESHOLD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT LOCATION B6-121 PER AMM 33-55. OPERATIONAL CHECK WAS GOOD. A/C OK FOR SERVICE. (LP #4992365)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,756 hrs · 30,246 cycles

RIGHT OUTBOARD CUSP HAS CORROSION AROUND LOWER SURFACE OF LIGHTENING HOLES AT STA 484 TO 503. REPAIRED O/B CUSP WEB STA 484-503 IAW SRM 53-00-55-2R-4. FABRICATED REPAIR DOUBLER IAW SRM 53-00-55-2R-4. HEAT TREATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-55-2R-4 AD 51-41-02-0G PG 1 PARA 4.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 44,756 hrs · 30,246 cycles

AFT CARGO DOOR JAMB HAS CORROSION ALONG LOWER SURFACE. AREAS MARKED. REPLACED AFT CARGO DOOR JAMB SURROUND WEB IAW B717 51-41-02. (LP #2989957)

Part: SKIN — CRACKED (BS 1022) · airframe 44,756 hrs · 30,246 cycles

STA 1022 BELOW L7R FUSELAGE SKIN CRACKED AT FORMER UPPER FASTENER. HFEC VERIFIED IAW BOEING NDT SPM ETHF 06-10-01.001 PROCEDURE 1, TAG #6742. (2 EA CRACKS WERE IDENTIFIED AND REPAIRED USING SAME DOUBLERS) TRIMMED / CUT OUT BOTH FASTENER HOLE CRACKS-ONE @ LAP SEAM ONE @ STA 1022 FRAME JUST BELOW L7R. THIS REQUIRING PRI-555600-14 TO BE INITIATED. FABRICATED AND INSTALLED DOUBLER AND FILLERS PER ER/A 555600-14. ACCOMPLISHED ALL REQUIRED PRE / POST INSPECTIONS IAW ER/A 555600-14 SEALED, TREATED, PRIMED, AND TOP COAT REPAIR PER ER/A 555600-14 AND B717 SRM 57-10-04 PARA 15/21 AMM 51-10-00-370-805. ASSOCIATED ER/A 00-555600 ADDED FOR AC 9523. (LP #2989993)

Part: SKIN — CORRODED (BS 851) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

LOWER EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND FASTENER STA 851 LONGERON 30. BLENDED CORROSION FROM SKIN IAW B717 SRM 51-01-01-14-1 AT L28L STA 861-865 .150" ORIG THICK NESS .021" REMOVED .129" RMAINING AT STA 877-883 L27L ORIG THIC .130", .005" REMOVED .128 REMAINING BOTH WITHIN ALLOWABLE LIMITS IAW B717 SRM 53-20-70-2R-1 FIG 201 AND DRAWING #5924876 AT STA 851 L30 AND L29L ORIG THICKNESS .160" REMOVED .042" 118 REMAINING OUT OF ALLOWABLE LIMITS IAW SRM 53-20-70-2R-1 FIG 201 REPAIRED OUT OF LIMITS DAMAGE WITH FILLER AND DOUBLER IAW B717 SRM 53-20-70-2R-1 APPLIED ALODINE PRIMER AND TOPCOAT IAW B717 SRM 51-22-01 AS REQUIRED. (LP #2989947)

Part: CARGO TRACK — CORRODED (BS 946) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

AFT LWR CARGO, BILGE BS 946 LBL 28, CARGO TRACK CORRODED . REMOVED THE CARGO TRACK, A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-10-04-06, 51-10-04-06, AND 51-41-01.

Part: CUSP WEB — CORRODED (BS 406) · airframe 44,756 hrs · 30,246 cycles

RIGHT OTBD CUSP WEB HAS CORROSION AT BS 406. BLENDED CORROSION IAW SRM 53-00-00, FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 103. RPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4, FIG 212.

Part: LONGERON — CORRODED (BS 908-965) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

AFT LOWER CARGO BILGE BS 908 - 965, LONGERON 29L HAD MULTIPLE SECTIONS OF LONGERON CORRODED. BLENDED THE CORROSION WITH 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-05-2R. REPLACED THE LONGERON IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 946-954) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

AFT LWR CARGO, BILGE BS 946 TO 954, RBL 29. CORRODED CARGO TRACK. REPLACED THE CARGO TRACK IAW SRM 51-41-02, 51-41-05, AND DRAWING 9915578.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

LONGERON 30 IN AFT LOWER CARGO HAS CORROSION FROM FS 1027 TO 1032. FOUND CORROSION TO BE IN EXCESS OF 100% MATERIAL THICKNESS. REPLACED SECTION OF LONGERON 30 IN AFT LOWER CARGO FROM STA 1012 TO 1053 IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 500016.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

SHEAR TIE CORRODED BEYOND LIMITS. REPLACED WITH NEW IAW DEG 5913537, AND. SRM 51-40-01.

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

UPPER CABIN FLOOR SUPPORT IS CORRODED AT BS 200, LBL 56 UNDER FWD LEFT LAVATORY OTBD FLOOR PANEL. BLENDED THE FLOOR SUPPORT IAW SRM 53-00-00-1A. FABRICATED A NEW FLOOR SUPPORT IAW DWG 9910078, AND INSTALLED IAW SRM 51-41-05-0G.

Part: CUSP WEB — CORRODED (BS 965-986) · airframe 44,756 hrs · 30,246 cycles

RIGHT CUSP WEB IS CORRODED BETWEEN BS 965-986. REMOVED DAMAGE AND FABRICATED A DOUBLER AND FILLER, INSTALLED THE DOUBLER & FILLER IAW SRM 53-00-55-2R4.

Part: CUSP WEB — CORRODED (BS 508) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT OTBD CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE BS 508. REPLACED THE CUSP WEB IAW SRM 53-00-55-2R, REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 456-556) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

UPPER FUSELAGE, LEFT CTR SEAT TRACK, BS 456 TO 556, LBL 22 GOUGED AND CORRODED. BLENDED THE SEAT TRACK AND FOUND TO BE OUT OF LIMITS. INSTALLED A 3 LUG REPAIR IAW SRM 53-20-52-2A.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT OUTBOARD CUSP WEB CORRODED ON LOWER SURFACE UNDER DOUBLER (UNDER FLOOR) AROUND LIGHTENING HOLE AT STA 579 TO 598. BLENDED CORROSION ON LOWER SURFACE OF RIGHT OUTBOARD CUSP WEB AROUND LIGHTENING HOLE REMOVED .002" OF MATERIAL FROM A NOMINAL THICKNESS OF .020" FOUND TO BE WITHIN LIMITS WITH A REMAINING THICKNESS OF .018" REF B717 SRM 53-00-55 GUAGE TOOL TAG #2932 FOUND LWR SPLICE TO BE CORRODED OUT OF LIMITS REPLACED LWR SPLICE REF B717 SRM 51-41-05. (LP #2966762)

Part: CUSP WEB — CORRODED (BS 440) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT SIDE OTBD CUSP WEB HAS CORROSION ON LOWER SURFACE BS 440. BLENDED AND CUT OUT DAMAGE, FABRICATED, AND INSTALLED A DOUBLER IAW SRM 53-00-55-2R-4.

Part: RUB STRIP — CORRODED · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

AREAS OF SURFACE CORROSION ON THE LOWER AFT RUB STRIP FOR FILLET PANEL 150SL STA 898.5-920. L-24L-26L. BLENDED CORROSION IAW SRM 53-00-00 FIG 103 FOUND TO BE OUT OF LIMITS. INSTALLED A NEW RUBSTRIP IAW AMM 20-60-01 914-801.

Part: CUSP WEB — CORRODED (BS 560-579) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT OTBD CUSP WEB CORRODED BS 560 - 579. BLENDED CORROSION, CUT OUT AREA OF DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER & RING DOUBLER IAW SRM 53-00-55-2R-4.

Part: SEAT TRACK — DAMAGED (BS 400) · airframe 44,756 hrs · 30,246 cycles

SEAT TRACK RBL 44.5 IS CORRODED, GOUGED, AND NEEDS PAINT IN SEVERAL AREAS BS 356 - 456. BLENDED AND FOUND TO BE OUT OF LIMITS AT BS 400. CUT OUT DAMAGE AREA. INSTALLED A REPAIR IAW SRM 53-20-52-2A.

Part: CUSP WEB — CORRODED (BS 446-459) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT SIDE OTBD CUSP WEB HAS CORROSION BS 446 TO 459. REMOVED CORROSION IAW SRM 53-00-55. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. REPAIRED THE DAMAGE IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CORRODED (BS 237-256) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

LEFT SIDE OTBD CUSP WEB HAS CORROSION FROM BS 237 -- 256. BLENDED THE DAMAGE IAW SRM 53-00-00-1A. FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM 53-0055-2R-4.

Part: SEAT TRACK — CORRODED (BS 759) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT CENTER SEAT TRACK BS 759 CORRODED BEYOND LIMITS. CUTOUT DAMAGED AREA AND INSTALLED A REPAIR IAW SRM 53-20-52-2R.

Part: SEAT TRACK — CORRODED (BS 777-779) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT CENTER SEAT TRACK CORRODED BEYOND LIMITS AT BS 777 - 779. CUT OUT DAMAGED AREA AND INSTALLED A THREE LUG REPAIR IAW SRM 53-20-52-2A.

Part: CUSP WEB — CORRODED (BS 834) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

LEFT OTBD CUSP WEB HAS A SMALL SPOT OF CORROSION AT BS 834. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: CUSP WEB — CRACKED (BS 256) · airframe 44,756 hrs · 30,246 cycles

RIGHT, INBOARD CUSP WEB CRACKED AT BS 256 BETWEEN SEAT TRACKS. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: SEAT TRACK — CORRODED (BS 808-810) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT CENTER SEAT TRACK BS 808 - 810 CORRODED BEYOND LIMITS. CUT OUT DAMAGE AND INSTALLED A REPAIR IAW SRM 53-20-52-2R.

Part: CUSP WEB — CORRODED (BS 522-541) · corrosion level 2 · airframe 44,756 hrs · 30,246 cycles

RIGHT OTBD CUSP WEB CORRODED AROUND UPPER AND LOWER SURFACES BS 522 - 541. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 44,247 hrs · 29,892 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 3C IN THE CABIN WAS DAMAGED. MAINTENANCE SECURED THE COVER.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 44,247 hrs · 29,892 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 2C IN THE CABIN WAS DAMAGED. MAINTENANCE REPLACED THE COVER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,880 hrs · 28,130 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT THE FIRST CLASS LAVATORY HAD FAILED. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: FRAME — CRACKED (BS 696) · airframe 40,470 hrs · 27,099 cycles

DURING FRAME INSPECTION, SPECIAL VISIT, FOUND FRAME BS 696 CRACKED. REPLACED IAW EO 5310-01439, ER/A 537346-14AD & 538052-14AD.

Part: FRAME — CRACKED (RT MLG WW) · airframe 39,791 hrs · 26,605 cycles

RIGHT MLG WW FWD FRAME CRACKED AT UPPER OTBD END. REPAIRED FRAME IAW SRM & DWG.

Part: FLASHLIGHT — OUT OF ADJUST (CABIN) · airframe 39,791 hrs · 26,605 cycles

AFT EMER FLASHLIGHT INOPERATIVE. ADJUSTED FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,791 hrs · 26,605 cycles

LEFT AFT OVERWING EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: FLASHLIGHT — OUT OF ADJUST (CABIN) · airframe 39,791 hrs · 26,605 cycles

FORWARD LOWER EMER FLASHLIGHT INOPERATIVE. ADJUSTED FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (TAIL) · airframe 39,791 hrs · 26,605 cycles

TAIL COMPARTMENT CATWALK 3RD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

L2 DOOR EMER EXIT SIGN INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

L1 DOOR EMER EXIT SIGN INOPERATIVE. R & R BATTERY PER AMM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

RIGHT CUSP MEMBRANE CORRODED BETWEEN BS 200 - 220. R & R MEMBRANE IAW SRM & DWG.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 38,544 hrs · 25,750 cycles

LEFT MLG DOOR INNER SKIN FWD OTBD CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: HINGE BRACKET — CRACKED (RT AILERON) · airframe 38,544 hrs · 25,750 cycles

RIGHT AILERON, NR 4 HINGE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 39,962 hrs · 26,720 cycles

LEFT MLG DOOR INNER SKIN FWD OTBD CORNER CRACKED. REPAIRED DOOR IAW FAS EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

CUSP ANGLE CORRODED BS 200, RBL 56. R & R CUSP ANGLE IAW EA & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

MEMBRANE CORRODED BETWEEN BS 160 - 180, BETWEEN RBL 43 - 54. R & R MEMBRANE IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN WET AREA MEMBRANE CORRODED AT BS 200, RBL 54. REPAIRED MEMBRANE IAW SRM.

Part: HINGE BRACKET — CRACKED (LT AILERON) · airframe 38,544 hrs · 25,750 cycles

LEFT AILERON, NR 4 HINGE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 38,544 hrs · 25,750 cycles

L1 DOOR EMER EXIT IDENTIFIER ASSEMBLY CRACKED. R & R IDENTIFIER ASSEMBLY IAW AMM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN FLOORBOARD 222 DF DAMAGED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN FLOORBOARD 222 WF DAMAGED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN FLOORBOARD 222 YF DAMAGED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN FLOORBOARD 222 EF DAMAGED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 38,544 hrs · 25,750 cycles

MAIN CABIN FLOORBOARD 222 AHF DAMAGED. R & R FLOORBOARD IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

CABIN L1 DOOR JAMB LOWER FLOOR ATTACH SUPPORT CORRODED BETWEEN BS 160 - 200, LBL 55. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CRACKED (LT MLG DOOR) · airframe 38,544 hrs · 25,750 cycles

LEFT MLG WW DOOR LOWER FWD CORNER CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

AFT CARGO COMPARTMENT DOOR CUT OUT FWD JAMB DOUBLER CORRODED. REPAIRED DOUBLER IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

SERVICE DOOR JAMB CORRODED BETWEEN BS 170 - 200, RBL 55. R & R PANEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 38,544 hrs · 25,750 cycles

LEFT WW OTBD AFT WING TO BODY CRACKED ATTACH ANGLE ABOVE NR 4 FLAP TRACK. R & R ANGLE IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 38,544 hrs · 25,750 cycles

LEFT WING BUTTE DOOR 530GB CRACKED FROM INBD END. REPAIRED DOUBLER IAW EA.

Part: FASTENER — BROKEN (TE FLAP) · airframe 38,544 hrs · 25,750 cycles

RIGHT WING FIXED TE BEHIND NR 1 FLAP HINGE FASTENER BROKEN. R & R FASTENER IAW EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

E & E COMPARTMENT DOOR JAMB AFT LIP CORRODED. REPAIRED DOOR JAM IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,544 hrs · 25,750 cycles

CUSP WEB CRACKED AT BS 218, RBL 58. R & R CUSP WEB IAW DWG & SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 38,544 hrs · 25,750 cycles

R1 DOOR EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 38,544 hrs · 25,750 cycles

R1 DOOR EMER EXIT IDENTIFIER LENS & HOUSING CRACKED. R & R IDENTIFIER ASSEMBLY IAW AMM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 38,274 hrs · 25,578 cycles

BUSINESS CLASS CABIN EMERGENCY EXIT SIGN LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY IAW SIP.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 37,781 hrs · 25,269 cycles

DIVERSION RT HYD DECREASE DURING FLIGHT. R & R NR 2 ENG EDP IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 37,662 hrs · 25,195 cycles

FWD FLIGHT ATTENDANT`S AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW MM.

Part: LATCH — LOOSE (GIRT BAR) · airframe 36,292 hrs · 24,329 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED LATCH IAW SIP.

Part: SCREW — LOOSE (L1 DOOR) · airframe 36,198 hrs · 24,272 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR SCREW LOOSE. SECURED SCREW IAW SIP.

Part: BONDING STRAP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

WING TO BODY BONDING STRAPS CRACKED. R & R STRAPS IAW SRM AND DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT SIDE CABIN CUSP WEB CRACKED AT STA 671, RBL 45. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT CUSP WEB CRACKED AT BS 237, LBL 45. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

AFT CABIN FLOOR PANEL 223FF DELAMINATED. R & R PANEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FRAME CORRODED AT BS 908, LONG 29L TO LONG 30L. REPAIRED FRAME IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LONGERON CORRODED BETWEEN BS 922 TO BS 925, LONG 30. R & R LONGERON IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

AFT CARGO COMP FRAME CORRODED AT BS 927, BETWEEN LONGERON 30L TO LONGERON 29R. R & R FRAME IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LONGERON CORRODED BETWEEN BS 907 TO BS 954, LONG 29L. R & R LONGERON IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FRAME CORRODED AT BS 889, BETWEEN LONG 28L TO LONG 30L. REPAIRED FRAME IAW SRM.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FLOORBOARD WEB CRACKED AT STA 655, LBL 54. REMOVED AND REPLACED WEB IAW SRM.

Part: LONGERON — CRACKED (NR 1 PYLON) · airframe 35,288 hrs · 23,725 cycles

NR 1 ENG PYLON/APRON CRACKED ON UPPER LONGERON AT AFT HINGE CUT OUT. REPAIRED PYLON IAW T/R.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FLOOR SUPPORT CRACKED AT STA 655. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FLOORBOARD WEB CRACKED AT STA 672, LBL 46. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,063 hrs · 24,185 cycles

FRAME CORRODED AT STA 889, BETWEEN LONG 28L TO LONG 30L. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,063 hrs · 24,185 cycles

AFT CARGO COMP FRAME CORRODED AT STA 908, BETWEEN LONG 29L TO LONG 30L. R & R FRAME SECTION IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FLOOR SUPPORT FITTING CRACKED AT STA 737, LBL 44. REMOVED & REPLACED FITTING IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,063 hrs · 24,185 cycles

AFT CARGO COMP FRAME CORRODED AT STA 927, BETWEEN LONGERON 30R TO LONGERON 29R. R & R FRAME IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RUB STRIP CRACKED AT LEFT FUSELAGE UNDER FILLET FAIRING 150 CL STA 645. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT CUSP WEB CORRODED BETWEEN STA 522 TO STA 503. REMOVED AND REPLACED WEB IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT RUB STRIP UPPER CRACKED AT STA 560 UNDER THE FILLET FAIRING 150AL. REMOVED AND REPLACED RUB STRIP IAW AMM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT RUB STRIP CRACKED AT STA 560. REMOVED AND REPLACED RUB STRIP IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RT CUSP WEB CORRODED BETWEEN STA 598 TO STA 617. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 655 TO STA 674. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FUSELAGE WING TO BODY FAIRING LOWER SIDE RIGHT RUB STRIP CRACKED AT STA 696. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT MAIN CABIN CORRODED ON CUSP WEB BETWEEN STA 560 TO STA 541. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT CUSP WEB CORRODED BETWEEN STA 696 TO STA 715. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FWD CARGO FRAME CORRODED. R & R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 541 TO STA 560. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

LEFT MAIN CABIN DELAMINATED FLOOR PANEL 222AFF. REPAIRED PANEL IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RUB STRIP CRACKED AT LEFT FUSELAGE UNDER FILLET FAIRING 150DL STA 636. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

MAIN CABIN WINDOW FRAME CRACKED AT STA 579 LOWER END. REPAIRED DOUBLER IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 223 DF DELAMINATED. R & R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 522 TO STA 541. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

R & R FRAME CRACKED AT BS 674. R & R FRAME IAW SRM AND DWG.

Part: PAN — CORRODED (CARGO DOOR) · airframe 35,288 hrs · 23,725 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222AMF DELAMINATED. R & R PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

SEAT TRACK CORRODED BETWEEN STA 256 TO STA 579, LBL 44. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222LF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222AAF DELAMINATED. R & R PANEL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RT WING TO BODY AT STA 665, LONG 22R SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222AVF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222AGF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: PANEL — CRACKED (RT MLG WW) · airframe 35,288 hrs · 23,725 cycles

RT WHEEL WELL BELOW HYD RESERVOIR PANEL CRACKED. REPAIRED DOUBLER IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222ACF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 446 TO STA 465. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FWD CARGO COMPT AFT BULKHEAD RT SIDE 8 O'CLOCK POSITION FITTING CRACKED AT FS 655, 27R. R & R FITTING IAW SRM AND DWG.

Part: BONDING STRAP — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

WING TO BODY BONDING STRAPS CRACKED. R & R STRAPS IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222APF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

FLOORBOARD 221 UF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222ABF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222 WF DELAMINATED. R & R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 465 TO STA 484. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222RF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 484 TO STA 503. REPAIRED WEB IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222AEF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222PF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222JF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LEFT SIDE ATTACHED ANGLE TO FRAME 1520, CRACKED. R & R ANGLE IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,288 hrs · 23,725 cycles

CABIN FLOORBOARD 222ATF DELAMINATED. R & R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 503 TO STA 522 RIGHT SIDE. REMOVED AND REPLACED WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LONGERON CRACKED AT BS 1144, LONG 2R. REPAIRED LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,288 hrs · 23,725 cycles

LONGERON CRACKED AT BS 1144, LONG 2L. R & R LONGERON IAW SRM.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 35,288 hrs · 23,725 cycles

NR 1 ENGINE PYLON /APRON SMALL CRACKED ON UPPER LONGERON AT AFT HINGE CUTOUT. REPAIR DOUBLER IAW SRM.

Part: DOUBLER — CRACKED (LT NLG DOOR) · airframe 35,288 hrs · 23,725 cycles

LEFT NLG STRUT DOOR AFT HINGE CUT OUT CRACKED. REPAIRED DOUBLER IAW SRM.

Part: DOUBLER — CRACKED (RT NLG DOOR) · airframe 35,288 hrs · 23,725 cycles

RIGHT NLG STRUT DOOR AFT HINGE CUT OUT CRACKED. REPAIRED DOUBLER IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 35,058 hrs · 23,585 cycles

ONE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT 2D HAS A MISSING LENS COVER. INSTALLED LENS COVER PER AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 34,568 hrs · 23,287 cycles

NR 1 ENGINE PYLON/APPRON HAS SMALL CRACK .75" LONG ON UPPER LONGERON AT AFT HINGE CUTOUT-- C/W SECTION 1 OF TRA 17-54-TR00192. REPAIRED PER SRM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 34,135 hrs · 22,998 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS ABOVE ROW 15AC OUT. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-51. OP CHECK GOOD.

Part: SKIN — DAMAGED (FUSELAGE)

EXTERIOR FUSELAGE SKIN, STA 220, LONG L20R, DAMAGED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER B717-53-03336A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT, STA 180, LBL 15 TO LBL 36, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 8 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, LBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02. \

Part: WEB — CRACKED (FUSELAGE)

CABIN FLOOR WEB, STA 218, RBL46, CRACKED. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 45 TO RBL 50, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT ANGLE, STA 200, LBL 15 TO LBL 25, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22R, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN L-1 DOOR LOWER SILL FLOOR SUPPORT ANGLE, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: STRUCTURE — CORRODED (GALLEY)

GALLEY COFFEEMAKER COMPARTMENTS 101, 102 AND 103 LOWER SURFACE, CORROSION. ACCOMPLISHED LOWER SURFACE REPLACEMENT PER EA 17-25-03226IR.

Part: PANEL — CRACKED (FUSELAGE)

PASSENGER ENTRANCE DOOR JAMB AFT STRAP PANEL, LONG L15L, CRACKED. ACCOMPLISHED STRAP PANEL DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 6 TO BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WIRE — DAMAGED (CABIN)

SEAT ROW 24DEF EMERGENCY EXIT PATH LIGHTING INOP. REPAIRED WIRING PER WDM 33-51, OPS CHECK GOOD.

Part: GASKET — DAMAGED (SLAT PANEL)

ON DESCENT AIRCRAFT ATTEMPTED TO LEVEL OFF AT 11000 FEET. THE AUTOPILOT KICKED OFF, AT THAT POINT WE HAD NO MANUAL CONTROL OF THE AIRCRAFT EXCEPT LONGITUDINAL. FLIGHT CONTROLS BROKE FREE AFTER FLT CREW WORKED CONTROLS. REGAINED AIRCRAFT CONTROLS UPON HAND FLYING AIRCRAFT. CONTROLS FELT HEAVY. REMOVED AND REPLACED BOTH LEFT AND RIGHT SLANT PANEL GASKETS, LEAK CHECK GOOD IAW MM 53-32-02 REF NRWC N156660 AND N156662.

Part: ENGINE — DAMAGED (LEFT)

LEFT ENGINE SEVERE DAMAGE. REMOVED AND REPLACED NR 1 ENGINE PER W/O 232308 AND TASK CARD 603, AUTOLAND ACCOMPLISHED ON TASK CARD 625 ALL OPS & LEAK CHECK GOOD.

Part: CONTACTOR — OUT OF POSITION (EMERGENCY LIGHT)

FOUND ON SERVICE CHECK, L1 DOOR OVERHEAD EMERGENCY LIGHTS INOP. FOUND CENTER CONTACTOR OF FWD BULB SHORTED TO GROUND. REPOSITIONED CENTER CONTACTOR, REF WD 33-51-12. ALSO REPLACED 5A FUSE IN BATTERY PACK B5-235 REF CMM 33-50-02 AND AMM 33-51-03. ALL OPS CHECKS GOOD.

Part: SLIDE — DEPLOYED (L1 DOOR)

L-1 DOOR SLIDE DEPLOYED. REMOVE AND REPLACED L-1 DOOR SLIDE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR LOWER JAM CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED PAN AND SPLICES PER B717 SRM 53-20-15 R17.

Part: NUT — LOOSE (RT MLG DOOR)

ON DESCENT, THE RIGHT MAIN GEAR UNSAFE (RED) ILLUMINATED WITH THE GEAR LEVER UP. FOUND RIGHT MLG DOOR LATCH ROLLER LOOSE. REMOVED AND REPLACED ALL 4 NUTS ON ROLLER AND TIGHTENED AS REQ'D REF M/M 32-34. RETRACTED GEAR, ALL OPS NORMAL REF M/M 32-33.

Part: STRUCTURE — GROUND DAMAGE (FUSELAGE)

PUSHBACK STRUCK BAGGAGE CART WHICH STRUCK AIRPLANE FUSELAGE LOCATED BELOW AND AFT OF GALLEY DOOR. REPAIRED FUSELAGE PER RES 06-0789 AND B717 SRM 53-00-01 CLASS III REPAIR. REQUIRES REPETITIVE INSP AT 3000 CYCLES AND REPLACEMENT AT 8000 CYCLES.