N921AT

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,776 hrs · 42,624 cycles

SHIP 9577 DURING SVC CHECK FOUND EMERGENCY LIGHT ABOVE R1 WOULD COME ON THEN IMMEDIATELY EXTINGUISH. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY ASSY B5-259. REF B717 AMM 33-51-04. OPS CHECK GOOD (7321200)

Part: SEAL — ELONGATED (ZONE 500 SLAT) · airframe 58,523 hrs · 42,407 cycles

AIRCRAFT 9577, AFTER REMOVAL OF LH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOUND ON SLAT 1 TO 5. CORRECTIVE ACTION: ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS ON SLAT 1 TO 5 WERE REPAIRED PER PRI 626359-14 REV.3 AND ER/A 626359-14 REV.ORIGINAL SECTION I: PERMANENT REPAIR. (LP 1015063)

Part: STRUCTURE — DAMAGED (ZONE 600 SLAT) · airframe 58,523 hrs · 42,407 cycles

AIRCRAFT 9577, AFTER REMOVAL OF RH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOUND ON SLAT 1 AND 5. CORRECTIVE ACTION: RH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOUND ON SLAT 1 AND 5 WAS REPAIRED PER PRI 626407-14 REV.3 AND PER ER/A 626407-14 REV.ORIG SECTION I: PERMANENT REPAIR. (LP 1015351).

Part: SKIN — DAMAGED (ZONE 300) · airframe 58,523 hrs · 42,407 cycles

AIRCRAFT 9577, VERT STAB LEADING EDGE SKIN, B717 - REPAIR, RII IN REF PER AMDS 5530-01048-03. CORRECTIVE ACTION: VERT STAB LEADING EDGE SKIN, B717 - REPAIR, RII WAS ACCOMPLISHED PER AMDS 5530-01048-03. (LP 1014363)

Part: FASTENER — LOOSE (ZONE 300) · airframe 58,523 hrs · 42,407 cycles

ARCRAFT 9577, LOOSE FASTENERS ON RH/LH LEADING EDGE SPLICE (MOVABLE), STA ZFS=52.267 AT VERTICAL STABILIZER. VERTICAL LEADING EDGE (MOVABLE) ON STA ZFS = 52.267 AT VERTICAL STABILIZER WAS REPAIRED PER SERVICE GENERAL DRAWING SG95550001 REV. B IN ACORDANCE TO AMDS 5530-01048-02 AND AMDS 5530-01048-03. (LP 1010804)

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

AIRCRAFT 9577, CRACK ON ANGLE ATTACHET WING BOX TO UPPER SKIN PANEL BTW STA Y=710 TO STA Y=720 -X=44. CORRECTIVE ACTION: ANGLE ATTACHET WING BOX TO UPPER SKIN PANEL BTW STA Y=710 TO STA Y=720 -X=44 WAS REPAIRED PER ER/A 625883-14AD REV ORIG, SECTION I: PERMANENT REPAIR. (LP 1007095)

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 58,523 hrs · 42,407 cycles

AIRCRAFT 9577, AFTER REMOVED METALLIC SEAL ALONG UPPER EDGES OF APRON HINGE AT LH PYLON, CRACK ON FWD UPPER CORNER SKIN OF APRON WAS FOUND. CORRECTIVE ACTION: FWD UPPER CORNER SKIN OF APRON LH PYLON WAS REPAIRED PER B717-200 SRM 54-50-01-2R REPAIR 2. (LP 1003939)

Part: SKIN — DENTED (ZONE 100) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 INITIAL INSPECTION: DENT ON EXTERNAL FUSELAGE SKIN ON STA Y=213 BTW LONG= 18L AND LONG=19L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 625868-14 REV ORIGINAL (0996949)

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE NRC S/N:00617: CORROSION OUT OF LIMITS ON FUEL ACCESS PLATE COUNTERSINK 620DT PER B717-200 SRM 57-10-01-2R PROCEDURE 2. DOOR CAN NOT BE REPAIRED UNDER CONDITION I OR II. CORRECTIVE ACTION: REPAIRED PER B717 AMM 57-11-02- 300-801 (0998316)

Part: TAB — DELAMINATED (ZONE 300 ELEVATR) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE TO NRC 00033: AFTER REMOVAL PAINT ON ELEVATOR CONTROL TAB (LH) AREAS WERE FOUND DELAMINATED. CORRECTIVE ACTION: REPAIRED PER 625939. (0994012)

Part: SUPPORT FITTING — WORN (ZONE 100) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 WEAR ON SUPPORT FITTING AND BUSHING ALSO RUSTED HARDWERE OF SPRING RELEASE MECHANISM AT TAILCONE. REPAIRED PER B717-200 SRM 51-41-01-0G (0988292)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE NRC 269: CORROSION OUT OF LIMITS (ORIGINAL THICKNESS 0.060 IN AND REMAINING THICKNESS 0.005 IN IN FLANGE AREA) OF AFT CARGO TIE TRACK LOCATED BETWEEN Y= 813 AND Y= 1022; L-27L L-28L. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-05-0G, PER B717 SRM 51-41-01 (0983137)

Part: FRAME — CRACKED (ZONE 100) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE TO NRC 00291; CRACK ON FRAME CANT "CAP" STA Y=1178 AND PROJECTION OF LONGERON 17R AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B-717-200 SRM 53-00-00-2R REP.1 (0983728)

Part: FITTING — CORRODED (ZONE 300 ELEV) · corrosion level 2 · airframe 59,228 hrs · 43,056 cycles

CORROSION ON COUNTERWEIGHT FITTING OF ELEVATOR LH. COUNTERWEIGHT FITTING OF ELEVATOR LT WAS REPAIRED PER ERA 592404-14TR REV ORIGINAL SECTION I. (0977129)

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 CRACKED LOWER RH AND LH JAMB REPAIR REINFORCEMENTS AT NLG WHEEL WELL. CORRECTIVE ACTION: LOWER RH AND LH JAMB REPAIR REINFORCEMENTS AT NLG WHEEL WELL PER ER/A 495600-14MA (0973673)

Part: FASTENER — LOOSE (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 AFTER INSPECTION ON PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN STA Y= 1037 BTW LONG 13 RH TO LONG 14RH WERE FOUND LOOSE FASTENERS ON REPAIR DOUBLER AND NEAR TO REAPOIR DOUBLER. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 14-568647 (0975044)

Part: HINGE FITTING — CORRODED (ZONE 600 FLAP) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 AFTER SEALANT REMOVAL CORROSION WAS FOUND ON ( OTBD LOWER ATTACHING BOLT ) MID FLAP HINGE FITTING STA XW= 251.6 AT RH WING. CORRECTIVE ACTION: STUDS WERE REPLACED AND CENTER WING FLAP HINGE WAS REPLACED BY SERVICEABLE CENTER WING FLAP HINGE PER B717 AMM 57-55-25 (0974785)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 AFTER REMOVED CORROSION, GALLEY FLOOR SUPPORT FITTING STA Y=218 - 200 AND STA X= -11 WAS MEASURED AND EVALUATED AND WAS FOUND OUT OF LIMITS. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER CORROSION LEVEL 2, SUPPORT FITTING ON STA Y=218 - 200 STA X= -11 WAS REPLACED PER B717-200 SRM 51-41-01-0G . (0973445)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 CORROSION OUT OF LIMITS PASSENGER CABIN SEAT TRACK (X=- 44; Y= 200 - 256). CROWN WITH ORIGINAL THICKNESS IS 0.115IN. REMAINING THICKNESS IS 0.070IN. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B-717-200 SRM 53-20-52 (0969326)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE TO NRC 00217: OUT OF LIMITS AFTER BLENDED OUT FRAME STA Y=889 BTWEN L29L TO L29R. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. (0969661)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 CRACKS 3 EA AROUND FASTENER HOLE OF THE LH COCKPIT WINDOW RETAINER STA Y=148. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 626178 -14 REV ORIGINAL (0968634)

Part: HINGE FITTING — WORN (ZONE 600 FLAP) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 ELONGATED BORE OF INB LUG AND WEAR ON BUSHINGS AND HARDWARE OF OUTBD FLAP HINGE FITTING STA XRS 383 AT RH WING. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 625998-14 REV ORIGINAL AND PRI 625998-14 REV 2. (0969698)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

SHIP 9577 IN REFERENCE TO NRC 385 WIP 4 CORROSION ON SEAT TRACK X=-22 BTW STA Y=200 TO STA Y=200 TO STA Y=256 ,STA Y=275, AT PASSENGER CABIN, ORIGINAL THICKNESS ON CROWN IS 0.115IN AND THE MINIMUN REMAINING THICKNESS IS 0.046IN; AND WITH ORIGINAL THICKNESS ON BOTTOM IS 0.100IN AND MINIMUM REMAINING THICKNESS OF 0.032IN, THEREFORE AREA IT'S OUT LIMITS. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER SEAT TRACK X=-22 BTW STA Y=200 TO STA Y=300 WAS REPLACED PER B-717-200 SRM 53-20-52- 2R REP. 5 PAR. 4 FIG. 201 AND SRM 51-41-01-0G AND SRM 51-41-05 (0968408)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

CUSP WEB LOCATED BETWEEN Y=237 AND Y=256; X=-44 AND X=-58 WAS FOUND CRACKED. SUMMARY OF NRC 00817: CUSP WEB LOCATED BETWEEN Y=237 AND Y=256; X=-44 AND X=-58 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 215. (LP #0966489)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

CUSP WEB LOCATED BETWEEN Y=218 AND Y=237; X=-44 AND X=-58 WAS FOUND CRACKED. SUMMARY OF NRC 00816: CUSP WEB BETWEEN STA Y=218 AND Y=237; STA X=-44 AND X=-58, WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIGURE 21. (LP #0963051)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION OUT OF LIMIT ON LONGERON 26L BTW STA Y=962/967 AND BTW STA Y=974/988 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00792: CORROSION LEVEL 2. LONGERON 26L BTW STA Y= 962/967 AND BTW STA Y=974/988 WAS REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 3 PAR 4 A (1). (LP #0963162)

Part: STRUCTURE — CORRODED (ZONE 300) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

-AD- CORROSION WAS FOUND ON BORES 31, 33, ALSO ON HOLE #10 (VERTICAL AND TRANSVERSAL). SUMMARY OF NRC 667: CORROSION LEVEL 2. BORES 10, 31, AND 33 OF HORIZONTAL STABILIZER BARREL NUTS WERE REPAIRED PER PRI 625941-14 REV 1 & ER/A 625941-14AD REV ORIG. SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS: DTE COTROLLED WITH LP 0962474 AND AMOC 0962535. ASSOCIATED ER/A 14-625941 ADDED FOR AC 9577. (LP #0964124)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON SEAT TRACK X=22 Y=200 TO Y= 210 (ON SEAT TRACK LOWER FLANGES). ORIGINAL THICKNESS BOTTOM IS 0.100 IN AND MINIMUM REMAINING THICKNESS IS 0.030 IN THEREFORE AREA IS OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 1 PAR 4 FIG 101. AND DC-MD/BOEING NDT SPM PAR 4, 04-00-06 PAR 4 FIG 9. SUMMARY OF NRC 00677: SECTION SEAT TRACK X=22 Y=200 TO Y=238 WAS REPLACED DUE CORROSION LEVEL 2 PER B717-200 SRM 53-20-52-2R PROC 5, REPAIR 5 FIG 201; 51-41-01-0G, AND 51-41-05-0G. (LP #0964136)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION OUT LIMITS ON PASSENGER CABIN CUSP WEB LOCATED Y=427 - 446; X=-56. SUMMARY OF NRC 00769: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB LOCATED Y=427 - 446; X=-56 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP 4 FIG 211 CONFIG. 7017. (LP #0962260)

Part: HINGE FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

FRETTING CORROSION (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED PLATE RH OUTBD ON VERTICAL STABILIZER SPAR HINGE. FITTINGS WITH ORIGINAL THICKNESS =0.250" AND MINIMUM REMAINING THICKNESS IS 0.212" THEREFORE IT IS OUT LIMITS. SUMMARY OF NRC 00820: CORROSION LEVEL 2. PLATE RH OUTBD ON VERTICAL STABILIZER SPAR HINGE FITTINGS (2 EA) WERE REPLACED PER B717-200 SRM 51-41-05 PAR 8. (LP #0958134)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

CRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 00025: FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE WAS REPAIRED PER ER/A 625728-14 REV ORIG SECTION I: PERMANENT REPAIR AND PER PRI 625728-14 REV 3. TIME CONTROLLED ITEMS (SECTION II) MONITORED WITH LP 0956079. ASSOCIATED ER/A 14-625728 ADDED FOR AC 9577. (LP #0957684)

Part: CABLE — WORN (ZONE 100) · airframe 58,523 hrs · 42,407 cycles

TAILCONE EMERGENCY RELEASE HANDLE CABLE ASSEMBLY WAS FOUND WORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00623: RELEASE HANDLE CABLE ASSEMBLY WAS REPLACED PER B717 AMM 20-00-02 960-801 AND MUST BE ADJUSTED UNDER AMDS 5352-2001. (LP #0954695)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=541 - 580; X=-56. SUMMARY OF NRC 00768: CORROSION LEVEL 2. PREVIOUS REPAIR LOCATED ON PASSENGER CABIN CUSP WEB STA Y=541 - 580; X=-56, WAS REPLACED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5, FIG 207. (LP #0952836)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION OUT LIMITS ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=256; X=-56. SUMMARY OF NRC 00770: PREVIOUS REPAIR ON CUSP WEB LOCATED Y=256; X=-56 AT PASSENGER CABIN WAS REPLACED DUE CORROSION LEVEL 2 PER B717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5, FIG 207. (LP #0952290)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN FLOOR SUPPORTS (2 EA) BETWEEN Y=148 - 200, X=7 AND X=-7. SUMMARY OF NRC 00637: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) BETWEEN Y=148 - 200, X=7 AND X=-7, WERE FABRICATED PER DWG 9936534 REV BW, AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0950671)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON TIE TRACK STA 898.5-954 L27R TO L28R IN AFT CARGO COMPARTMENT. ORIGINAL THICKNESS 0.060IN AND MINIMUM REMAINING THICKNESS 0.05IN; FLANGE AREA IS OUT OF LIMITS. SUMMARY OF NRC 00771: CORROSION LEVEL 2. AFT CARGO COMPARTMENT TIE TRACK STA 898.5-954 L27R TO L28R WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05 PAR 8. (LP #0946171)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=503 - 522; X=-56. SUMMARY OF NRC 00767: CORROSION LEVEL 2. PREVIOUS REPAIR LOCATED Y=503 - 522; X=-56 ON PASSENGER CABIN CUSP WAS REPLACED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0945857)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION PER (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED PER DC/MD/BOEING NDT SPM, PART 4 04- 00-07, PAR 4 FIG 9, FLOORS SUPPORT AT LAVATORIES ZONES: [1 EA; BETWEEN Y=1053 - 1022, X=-44]. WITH ORIGINAL THICKNESS =0.125" AND MINIMUM REMAINING THICKNESS =0.062", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PROCEDURE 1 ALLOWABLE DAMAGE 1, PAR 4 (C), FIG 103. SUMMARY OF NRC 00775: CORROSION LEVEL 2. FLOOR SUPPORT AT LAVATORY ZONE BETWEEN Y=1053 TO 1022, X=-44 WAS FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0945864)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=446 - 465; X=-56. SUMMARY OF NRC 00764: CORROSION LEVEL 2. CABIN CUSP WEB (PREVIOUS REPAIR) LOCATED Y=446 - 465; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0940714)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=465 - 484; X=-56. SUMMARY OF NRC 00765: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=465 - 484; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R, REPAIR 4. (LP #0940877)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=484 - 503; X=-56. SUMMARY OF NRC 00766: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=484 - 503; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R, REPAIR 4. (LP #0940885)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION IN REFERENCE TO (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON CUSP MEMBRANE WEB X=58, STA Y=340, STA Y=868 C PAX (LH). ORIGINAL THICKNESS IS 0.020IN AND MINIMUM REMAINING THICKNESS IS 0.012IN., THEREFORE IT IS OUT LIMITS PER B717-200 SRM 53-00-55-1A ALLOWABLE DAMAGE 1 PAR 4 FIG 101 AND DC-MD/BOEING NDTSPM 4,04-00-06, PAR 4 FIG 9. SUMMARY OF NRC 00709: CORROSION LEVEL 2. CUSP MEMBRANE WEB X=58, STA Y=340, STA Y=868 C PAX (LH) WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 207. PERFORM GVI EVERY "C" CHECK PER B717-200 SRM 53-00-55-2R REPAIR 4 PAR 6 A TABLE 201. (LP #0941528)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

CRACKED LONGERONS 6R, 4L, AND 8R LOCATED AT RH LAVATORY ZONE Y=1022. SUMMARY OF NRC 00417: LONGERON 6R AND 8R STA Y=1022 AT RH AFT LAVATORY ZONE WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. NO CRACKS WERE FOUND ON LONGERON 4L PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. PERFORM A GENERAL VISUAL INSPECTION AT EVERY "C" CHECK PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2, PAR 7A, TABLE 202. DEFERRED LOG TO QC, ESTABLISH MONITOR INSPECTION 21-0553-8-1857 S/N 09577 REPETITIVE. (LP #0930554)

Part: HINGE FITTING — CORRODED (ZONE 500 FLAP) · corrosion level 2 · airframe 59,228 hrs · 43,056 cycles

CORROSION ON FLAP FWD HINGE FITTING XRS=267 OF REAR SPAR AREA AT LH WING. REPLACED PER SERVICEABLE LT CENTER WING FLAP HINGE FITTING (0931308)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,523 hrs · 42,407 cycles

CRACK ON CUSP WEB RH BTW STA Y=715 AT PASSENGER CABIN. CUSP WEB RH BTW STA Y=715 AT PASSENGER CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 203.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,523 hrs · 42,407 cycles

CORROSION ON INTERNAL DOUBLER AND ON INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=1022 AND STA Y=1037 BTW LONG 23L AND LONG 25L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00232: CORROSION LEVEL 2. INTERNAL DOUBLER AT INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=1022 AND STA Y=1037 BTW LONG 23L AND LONG 25L AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0926272)

Part: COMPRESSOR WHEEL — DAMAGED (NR 1 ENGINE) · airframe 57,476 hrs · 41,499 cycles

SHIP 9577 -FUME/DE- ON CLIMB OUT THROUGH FL200, AN ODOR SIMILAR TO MELTING PLASTIC WAS BRIEFLY NOTED. ABOUT ONE MINUTE LATER THE CREW EXPERIENCED SOME ENGINE VIBRATION ON THE LEFT SIDE AND AT THE SAME TIME, THE "ENG COMP L STALL" MESSAGE ILLUMINATED. SHORTLY THE ODOR WENT AWAY, AND ALL ENGINE INDICATIONS WERE NORMAL. DISPATCH AND MAINTENANCE OPERATIONS AGREED TO CONTINUE TO SCHEDULED DESTINATION. WHILE ON APPROACH FOR LANDING, THE SAME ODOR RETURNED AND THE CREW DONNED OXYGEN MASKS. AND THEN THERE WAS ANOTHER ENGINE COMPRESSOR STALL ON THE #1 ENGINE, ACCOMPANIED BY THE SAME "ENG COMP L STALL" MESSAGE. AN EMERGENCY WAS DECLARED WITH ATC ALONG WITH A REQUEST FOR ARFF TO MEET THE AIRCRAFT. CORRECTIVE ACTION: MAINTENANCE ACCOMPLISHED A BORESCOPE OF THE #1 ENGINE AND FOUND THE HPC STAGE 1-4 DAMAGED OUT OF LIMITS. ENGINE CHANGE REQUIRED. (LP #6004584)

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 56,536 hrs · 40,662 cycles

BIRD STRIKE DAMAGE TO RT HORIZONTAL STAB AT XFS 169.50. OVERALL DENT LENGHTH IS 12 IN LONG BY 7 IN WIDE. SECONDARY DENT IS 2.75 IN LONG BY 2.0 IN WIDE 0.125 DEPTH. THIRD DENT IS 4 IN LONG BY 3 IN WIDE 0.030 IN DEPTH. PERFORMED DAMAGE CONTAINMENT HFEC IAW TOPP 30-10-70 AND MDC93K0393 NDTSPM PART 06 10-01.001. NO DAMAGE INDICATIONS FOUND QC5223 518316. COMPLETED SECTION 1 OF ERA 616472-14 REV ORG PERMENANT REPAIR AFTER 1 CYCLE. INSTALLED PERMANENT REPAIR RT HORIZONTAL STABILIZER LEADING EDGE IAW B717 AMM 55-12-01 PER ER/A 6164472-14 REV ORIG. THIS COMPLETES TERMINATING ACTION. PLEASE CLOSE LOG. CLOSED LOG AND REMOVED MONITOR INSP. (LP #5334026)

Part: DISPLAY — INOPERATIVE (NAVIGATION) · airframe 55,992 hrs · 40,229 cycles

SHIP 9577 -MISC/DE- THE FLIGHT CREW REPORTED ELECTRICAL ISSUES, VIA FAILURE, FCP BLANKING, NAV DISPLAY BLANKING, FLIGHT DIRECTORS NOT WORKING, AND ALL ARE CAUSING UNRELIABLE PRIMARY NAVIGATION. THE QRH WAS COMPLIED WITH AND THE SITUATION STABILIZED ONCE THE EMERGENCY POWER SWITCH WAS SELECTED ON. AN EMERGENCY WAS DECLARED BY ATC. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE FCC-1 AND GCP HAD BOTH FAILED. THE FCC-1, GLARESHIELD CONTROL PANEL, DATA CONCENTRATOR UNIT, AND THE POWER CONVERSION DISTRIBUTION UNIT WERE ALL REPLACED. AIRCRAFT IS NOW OK FOR SERVICE. (LP #5730728)

Part: SIGN — DAMAGED (FWD CABIN) · airframe 55,952 hrs · 40,202 cycles

THE FORWARD EMERGENCY EXIT SIGN IS DAMAGED. MAINTENANCE REINSTALLED AND SECURED THE FORWARD EMERGENCY EXIT SIGN. OK FOR SERVICE. (LP #0191155)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,012 hrs · 39,402 cycles

THE EMERGENCY WINDOW, EXIT ROW, EMER EXIT COVER DIFFFUSER LENS FELL OFF. MAINTENANCE RESECURED COVER. (LP #2978024)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,646 hrs · 39,086 cycles

CREW TURNED ON WINDOW ANTI-FOG AND IMMEDIATELY NOTICED SMOKE FROM NEAR WINDOW FIN, ACCOMPANIED WITH AN ELECTRICAL BURN SMELL. CONTRACT MAINTENANCE INSPECTED F/O WINDOW AND CONFIRMED THE SMOKE AND ODOR WHEN THE SWITCH IS TURNED ON. NO EVIDENCE OF SMOKE OR ODOR WHEN SYSTEM IS OFF. DEFERRED THE SYSTEM TO MEL 30-41-01A. 'M' PROCEDURES WERE COMPLIED WITH AND A PLACARD WAS INSTALLED. MAINTENANCE REPLACED THE RIGHT HAND WINDSHIELD IAW B717 AMM 56-11-00. OPERATION AND LEAK CHECKS WERE GOOD. THE MEL AND PLACARD WERE REMOVED. THE AIRCRAFT IS OK FOR SERVICE. (LP #4734082)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,835 hrs · 38,365 cycles

AIRCRAFT 9577, TAIL COMPT FRAME CRACKED STA 1133 AT STR 2R-MARKED. CORRECTIVE ACTION: COMPLIED WITH ER/A 607133-14 REV. ORIG. PRI REV. "0" ALL INSTRUCTIONAL STEPS. I ALL INSTRUCTIONAL STEPS ON ER/A 607133-14 REV. ORIG. PRI REV. "0" MATCH FINALE ER/A 607133-14 REV. ORIG. (LP 2686115)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, TAIL COMPT STR 2L CRACKED AT STA 1133. CORRECTIVE ACTION: REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2. (LP 2675309)

Part: NONE — NONE · airframe 53,791 hrs · 38,330 cycles

FLOOR NEAR 1ST CLASS COAT CLOSET SEEMS SOFT. REMOVED AND FABRICATED FLOOR PANEL PER B717 AMM 53-21 AND SRM 53-20-50 PG 2. FIG 3. FOUND SUPPORT ANGLE BROKEN AT STA 237. REMOVED, FABRICATED, DRILLED UP, PRIMED, AND PAINTED A NEW SUPPORT ANGLE. INSTALLED FLOOR SUPPORT ANGLE PER BOING DRAWING #9971184. INSTALLED FLOOR PANEL PER B717 AMM 53-21. (LP #4025076)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,954 hrs · 37,565 cycles

AIRCRAFT 9577, ROW 20 EMERGENCY EXIT LOWER LIGHTS INOP. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY ROW 19 RT AND EMERGENCY PWR SUPPLY ROW 23 RIGHT. LP 9383357

Part: DOUBLER — DAMAGED · airframe 51,714 hrs · 36,428 cycles

AFT ATG ANTENNA AND DOUBLER DAMAGED REF 0514-2001, NRC 11. COMPLIED WITH REPAIR AT ATG ANTENNA PER ER/A 598111-14, PRI REV 0,1,2,3. FINAL REV A. ASSOCIATED ER/A 14-598111 ADDED FOR AC 9577. (LP #2176117)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,845 hrs · 38,377 cycles

AIRCRAFT 9577, 7 EXPERIENCED A TAILSTRIKE UPON ARRIVAL INTO ATL. SKIN PANEL 5919707-521 AND THE EXTERNAL DOUBLER (PN P28538) ASSOCIATED WITH THE AFT ATG4 ANTENNA INSTALLATION (ASSY P19112-2005) WERE FOUND DAMAGED BETWEEN STA 974 TO STA 994 AND LONGERON 29L TO 30. CORRECTIVE ACTION: FABRICATED A REPLACEMENT EXTERNAL ATG4 MOD DOUBLER (FIG. 1, ITEM 50), AND REPLACEMENT INTERNAL ATG4 MOD DOUBLER (FIG. 1, ITEM 100) FROM 0.071 THICK 2024-T3 CLAD SHEET, ENLARGED TO FIT THE FASTENER PATTERN SHOWN IN FIGURE 4. FABRICATED A REPLACEMENT SKIN CUTOUT FILLER (FIG. 1, ITEM 90) FROM 0.063 THICK 2024-T3 CLAD SHEET ENLARGED TO FIT THE DAMAGE CUTOUT. (LP 2172254)

Part: NONE — NONE · airframe 51,186 hrs · 35,961 cycles

THE AFT FLIGHT ATTENDANT JUMPSEAT SEAT BELT BUCKLE DISCONNECTED FROM THE BELT. THIS COULD PREVENT PROPER RETENTION OF THE OCCUPANT IN THE SEAT RESULTING IN PERSONAL INJURY AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE BELT DISCREPANCY WAS FORWARDED TO MEL 25-23-01C. MCC NOTIFIED AND A PLACARD WAS INSTALLED. THE AFT RIGHT FLIGHT ATTENDANT LAPBELT WAS REPLACED PER B717 AMM 25-23. THIS CLEARS MEL 25- 23-01C AND THE PLACARD WAS REMOVED. (LP #8185520)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,272 hrs · 35,159 cycles

THE THE FLIGHT ATTENDANT FOUND THAT THE OVERWING FWD SIDE EMERGENCY EXIT SIGN COVER DIFFUSER LENS IS MISSING. DFRD BY WEISS 00389354 HSV 21JUL21 RII: N ENTR 00389354 P MCC FCP DEFERRAL, FLIGHT CREW PLACARD REQUIRES VALIDATION FLIGHT CREW PLACARD INSTALLED. FOUND AND REINSTALLED O/H EMERGENCY EXIT SIGN AT THE OVERWING EXITS. NO NEF OR MEL ISSUED. (LP #1882918)

Part: SKIN — CORRODED (LT NR 5 SLAT) · corrosion level 2 · airframe 50,042 hrs · 34,951 cycles

LT WING UPPER SURFACE CORRODED. AFT OF #5 SLAT, APROX 6 FEET INBD FROM WING-TIP. MARKED. REPAIRED PER ER/A 591833-14 REV. ORIGINAL (PRI AND ER/A MATCHES). (LP# 1838785)

Part: CARGO TRACK — CORRODED · corrosion level 2 · airframe 50,042 hrs · 34,951 cycles

CORROSION FOUND ON BOTTOM SIDE OF AFT CARGO TRACK SECTION. MARKED. REPLACED TRACK, REF. BAC DWG 5956331. (LP #1836707)

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 50,042 hrs · 34,951 cycles

FWD CARGO DOOR SURROUND HAS CORROSION IN MULTIPLE LOCATIONS (MARKED). FABRICATED AND INSTALLED 2 SPLICES REF B717 SRM 53-20-15-2R. (LP #1836365)

Part: DOOR FRAME — CORRODED (FWD CARGO) · airframe 50,087 hrs · 34,994 cycles

FWD CARGO DOOR SURROUND HAS CORROSION IN MULTIPLE LOCATIONS (MARKED). SUMMARY NRC 133-0009:5300-2007/006 00257: FABRICATED AND INSTALLED 2 SPLICES REF B717 SRM 53-20-15-2R. SUMMARY NRC 133-0009:5300-2007/006 00257: FABRICATED AND INSTALLED 2 SPLICES REF B717 SRM 53-20-15-2R. (LP #1836367)

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,042 hrs · 34,951 cycles

LOWER DOOR SILL IS CORRODED AT LOC C-2 DOOR CUT OUT. REPAIRED PER B717 SRM 53-20-15-2R. (LP #1826803)

Part: CAM — OUT OF ADJUST (TAILCONE RELEASE) · airframe 50,042 hrs · 34,951 cycles

THE TAILCONE RELEASE CAM IS OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 102-0001:5352-2001/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF. B717 AMM 53 -52-03. (LP #1822703)

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 58,129 hrs · 42,065 cycles

R1 DOOR CUTOUT SURROUND WAS DAMAGED BY GROUND EQUIPMENT. PERFORM A DAILY INSPECTION OF THE R1 DOOR REWORK AREA REF ER/A 584985-14 REV ORIGINAL, SECTION 2. ACCOMPLISHED DURING LAYOVER IN MSP 31JAN20. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II EVERY DAY AFTER SECTION I UNTIL SECTION III ACCOMPLISHMENT. SECTION I ACCOMPLISHMENT IF LIMITED TO 01MAY2020. SECTION III TRACKS THIS REQUIREMENT. ASSOCIATED ER/A 95-584985 ADDED FOR AC 9577. 08JUN21 PERMANENT REPAIR IS ACCOMPLISHED IN ATL DURING C-CHECK PER ER/A 584985-14 REVISION A. THIS LOGPAGE RESTRICTION IS NO LONGER REQUIRED AND OK TO BE CLOSED. TERMINATED PER ENGINEERING COMMENTS. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 08JUN21 AND LOG COMMENTS. (LP #1470155)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,201 hrs · 34,269 cycles

THE FLOOR LEVEL EXIT SIGNS FOR THE LEFT AND RIGHT AFT OVERWING EXITS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 22 PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #6108599)

Part: LENS — MISSING (CABIN) · airframe 48,962 hrs · 34,078 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT COVER. (LP #1279759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 503 AND LONGERON 19. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP 1113706)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 313 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP 1113694)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP 1113705)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 446 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP 1113699)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP1113702)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 332 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP 1113697)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,831 hrs · 38,360 cycles

AIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 256 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANENT REPAIR REQUIRED AT 8000 CYCLES PER TABLE 203. RESTORED FINISH. (LP1113690)

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 45,555 hrs · 31,656 cycles

PUNCTURED AFT MOVABLE FLAP VANE LOWER SKIN, LT WING. THE FLAP VANE LOWER SKIN WAS REPAIRED IAW SRM 57-53-01-2R.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE 620EB ON THE RT WING. FOUND TO BE OUT OF LIMITS AND WAS REPLACED.

Part: FRAME — CRACKED (BS 1133) · airframe 45,555 hrs · 31,656 cycles

CRACKED FRAME BELOW LONGERON 2R BS 1133. THE FRAME WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AND DWG 5913595, REV AP.

Part: FRAME — CRACKED (BS 715) · airframe 45,555 hrs · 31,656 cycles

CRACKED FORMER BS 715 LT SIDE AT CANTED KEEL INTERNAL STRUCTURE. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REPAIR 2.

Part: FORMER — CRACKED (BS 679) · airframe 45,555 hrs · 31,656 cycles

CRACKED FORMER AT BS 679, RT SIDE AT CANTED KEEL BEAM INTERNAL STRUCTURE. REPAIRED IAW SRM 51-70-11-2R, 51-41-02-0G, AND 51-41-05-0G.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

FUEL ACCESS PANEL 520DB CORRODED OUT OF LIMITS IAW SRM 57-10-01-2R, PAR 5. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01-2R, PAR 5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,555 hrs · 31,656 cycles

CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13R-14R. PERMANENT REPAIR WAS ACCOMPLISHED PER ETI-17-18-078 R5 AND ER/A 568647-14 REV ORIGINAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,555 hrs · 31,656 cycles

CRACK ON LONGERONS 16R AND 17R STA Y=1022 AT PAX CABIN. LONGERONS 16 AND 17 RT WERE REPAIRED PER SRM 53-00-05-2R-2 FIG 201 AND ER/A 568581-14 REV ORG AND ETI-17-18-093 REV 1.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION STRAP UNDER LONGERON 26L BTW STA Y=946 TO Y=1002 AT AFT CARGO COMPARTMENT. NEW REPAIR PART WAS INSTALLED PER SRM 51-41-02-0G.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620CT ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0012.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520EB ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0010.

Part: FRAME ANGLE — CRACKED (BS 1087) · airframe 45,555 hrs · 31,656 cycles

CRACKED FRAME ANGLE BS 1087, BETWEEN LONGERONS 14 AND 15. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05-0G, & DWG 9971140, REV F.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520CT ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0010.

Part: ANGLE — CORRODED (BS 164-200) · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE R1 CUSP ANGLE BETWEEN BS 164 - 200. THE ANGLE WAS REPAIRED IAW ER/A 568469-14, REV ORG, AND ETI -17-18-085, REV ORIG.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SEVERAL POINTS ON EXTERNAL SKIN AT FUSELAGE EXTERNAL DOUBLER FROM STA Y=851 TO STA Y=870 BTW LONG 27L AND 27R. CORROSION LEVEL 2, DOUBLERS WERE REPLACED PER SRM 53-20-70-2R REPAIR 1.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 45,555 hrs · 31,656 cycles

PUNCTURE FOUND ON THE AFT MOVABLE LT WING FLAP VANE LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R.

Part: LONGERON — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REAPIRED IAW SRM 53-00-05-2R-2.

Part: SEAT TRACK — CORRODED (BS 200-205) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE RT SEAT TRACK, X-44, BS 200 - 205. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G.

Part: SKIN — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACK FOUND ON THE EXTERNAL SKIN BS 1022 BETWEEN LONGERONS 13L - 14L. REPAIRED IAW ER/A 568451-14, REV ORIGINAL, AND ETI-17-18-083, REV 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,555 hrs · 31,656 cycles

CRACK ON FRAME STA Y=1039 AND LONGER 17R AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1039 AND LONGER 17R WAS REPAIRED PER SRM 53-20-07 FIG. 201 REPAIR 4.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 45,555 hrs · 31,656 cycles

DELAMINATION FOUND ON FLOOR PANEL 222UF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50-2R.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 45,555 hrs · 31,656 cycles

CRACKED FLOOR PANEL 222DF. THE FLOOR PANEL WAS REPLACED SRM 53-20-50-2R.

Part: GUSSET — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED GUSSET AT BS 1022, LONGERON 7R. REPAIRED IAW ER/A 568440-14, REV ORIG, AND ETI-17-18-080, REV 1.

Part: GUSSET — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED GUSSET AT BS 1022, LONGERON 7L. REPAIRED IAW ER/A 568440-14, REV ORIG. AND ETI-17-18-080, REV 1.

Part: CUSP WEB — CORRODED (BS 427-430) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE RT CUSP WEB BETWEEN BS 427 TO 430, X-44 TO X-60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 211.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 520JB, LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: CUSP WEB — CORRODED (BS 385-391) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORRODED RT CUSP WEB BETWEEN BS 385 & 391, X-44 TO X-60. REPAIRED IAW SRM 53-00-55 2R, FIG 217.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED FRAME ANGLE AT BS 1022 BETWEEN LONGERONS 16 - 16R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 45,555 hrs · 31,656 cycles

CRACKED ACCESS PANEL 370AL ON THE VERTICAL STABILIZER. REPAIRED IAW SRM 55-00-00-2R-2, & SRM 51-41-02-0G.

Part: FAIRING — CRACKED (LT ELEVATOR) · airframe 45,555 hrs · 31,656 cycles

CRACKED FIXED FAIRING OF GEARED TAB INBOARD PUSH ROD ON THE LT ELEVATOR. REPAIRED IAW SRM 55-00-00-2R-1-.

Part: FLOOR SUPPORT — CRACKED (BS 737) · airframe 45,555 hrs · 31,656 cycles

FLOOR SUPPORT BS 737, X-56 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: CUSP WEB — CRACKED (BS 651-655) · airframe 45,555 hrs · 31,656 cycles

CRACKED RT CUSP WEB, BS 651 AND 655, X-54 TO X-60. REPAIRED IAW SRM 53-00-55-2R, FIG 221.

Part: ACCESS PANEL — CORRODED (CENTER TANK) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON THE COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 141AL, AT THE CENTER TANK. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: CUSP WEB — CRACKED (BS 665) · airframe 45,555 hrs · 31,656 cycles

CRACKED LT CUSP WEB BS 665, X 44 TO X 54. REPAIRED IAW SRM 53-00-55-2R-4, FIG 221.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

THE FUEL ACCESS PANEL 141AL WAS FOUND DAMAGED OUT OF LIMITS IAW SRM 57-10-01-2R, PAR 5. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 520QB, LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: FLOOR SUPPORT — CORRODED (BS 160-198) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON THE FLOOR SUPPORT AT X 44 BETWEEN BS 160 - 198. THE CORROSION WAS REMOVED IAW SRM 51-10-04-0G, PAR. 26. FOUND TO BE OUT LIMITS IAW SRM 53-00-00-1A, FIG 103, SHEET 1. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08.

Part: WEB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE DOOR FRAME WEB BS 200, X=56. REPAIRED IAW SRM 53-00-00-2R, FIG 201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620GB ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620DB ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: SCUFF PLATE — CRACKED (R1 DOOR) · airframe 45,555 hrs · 31,656 cycles

CRACKED SCUFF PLATE ON THE FWD R1 SERVICE DOOR. THE SCUFF PLATE WAS WELDED IAW ETI 17-18-089, REV ORIGINAL, AND ER/A 568360-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: CUSP WEB — CRACKED (BS 218-232) · airframe 45,555 hrs · 31,656 cycles

CRACKED CUSP WEB BETWEEN BS 218 TO 232. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9930538 RE. CC.

Part: DOUBLER — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON THE PRODUCTION DOUBLER. THE DOUBLER WAS REPLACED IAW DWG 9936534, ITEM 179, REV BW, AND SRM 51-41-02.

Part: CUSP WEB — CORRODED (BS 427-430) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION FOUND ON THE RT CUSP WEB BETWEEN BS 427 TO 430, X-44 TO X-60. REPAIRED IAW SRM 53-00-55-2R, FIG 211.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON THE FLOORBEAM BS 180, X-10 TO X-43. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON FLOOR SUPPORT, X=7, BS 200 CABIN. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620FT, RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: CUSP WEB — CRACKED (BS 647-665) · airframe 45,555 hrs · 31,656 cycles

CRACKED LT CUSP WEB BS 647 AND 665, X 44 TO X 54. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9910151, REV CH.

Part: CUSP WEB — CRACKED (BS 660-665) · airframe 45,555 hrs · 31,656 cycles

CRACKED LT CUSP WEB BETWEEN BS 660 AND 665, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 203, AND 51-41-02-0G.

Part: CUSP WEB — CRACKED (BS 670) · airframe 45,555 hrs · 31,656 cycles

CRACKED RT CUSP WEB, BS 670, X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 223.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 13 - 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 16 - 17L. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.

Part: LONGERON — CRACKED (BS 1022) · airframe 45,555 hrs · 31,656 cycles

CRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2, FIG 201.

Part: CUSP WEB — CRACKED (BS 908-912) · airframe 45,555 hrs · 31,656 cycles

CRACK ON THE LT CUSP WEB, BETWEEN BS 908 AND 912, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: PLATE — CORRODED (BS 1037-1053) · corrosion level 2 · airframe 45,555 hrs · 31,656 cycles

CORROSION ON THE RT PLATE BETWEEN BS 1037 - 1053, X-57 TO X-60. THE PLATE WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9981474, REV L.

Part: DOUBLER — WORN · airframe 45,555 hrs · 31,656 cycles

WORN RT PRODUCTION DOUBLER Z=11 IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. THE DOUBLER WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 16, REPAIR 16.

Part: DOUBLER — WORN (BS 370-416) · airframe 45,555 hrs · 31,656 cycles

WEAR ON PRODUCTION DOUBLER LOWER SURFACE FROM BS 370 TO 416, THE FWD CARGO DOOR. THE DOUBLER WAS REPLACED IAW DWG 5910141, REV FE, AND SRM 51-41-02-0G.

Part: PAN — CRACKED (BS 832-908) · airframe 45,555 hrs · 31,656 cycles

CRACKED LT WINDOW RING PAN FWD LOWER CORNER BS 832, 851, 889, AND 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1 FIG.202.

Part: PAN — CRACKED (BS 351) · airframe 45,555 hrs · 31,656 cycles

RT WINDOW RING PAN CRACKED, FWD UPPER CORNER, BS 351. REPAIRED IAW SRM 56-20-02-2R1 FIG. 202.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,471 hrs · 31,601 cycles

THE LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LAMP IAW AMM 33-51. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,413 hrs · 30,963 cycles

EMERGENCY EXIT DIFFUSER LENS MISSING ABOVE ROW 29.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,167 hrs · 30,115 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. LENS COVER IS MISSING. INSTALLED SIGN. OPERATIONAL CHECKED NORMAL.

Part: LENS — UNKNOWN (EXIT SIGN) · airframe 41,813 hrs · 29,176 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT THE OVERWING EXIT PATH AT 29C EMERGENCY EXIT SIGN HAD A DAMAGED OR MISSING LENS/COVER. MAINTENANCE INSTALLED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: CAM — DISLODGED (TAILCONE RELEASE) · airframe 40,301 hrs · 27,965 cycles

DURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THE CAM ASSY FOR THE TAILCONE LATCH WAS DISLODGED. MAINTENANCE REINSTALLED THE CAM ASSY. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII COMPLETED FOLLOWING MAINTENANCE.

Part: LONGERON — CORRODED (BS 1008) · corrosion level 2 · airframe 40,294 hrs · 27,958 cycles

AFT CARGO BAY- L23R CORRODED AT BS 1008. REPAIRED IAW SRM 53-00-05, REPAIR 2.

Part: FRAME — CORRODED (BS 1028) · corrosion level 2 · airframe 40,294 hrs · 27,958 cycles

AFT CARGO BAY- FRAME AT BS 1028 IS CORRODED FROM L28L TO L28R. REPAIRED FRAME SECTION IAW SRM 53-20-07, REPAIR 3.

Part: SUPPORT — CORRODED (BS 1028 BULKHEAD) · corrosion level 2 · airframe 41,566 hrs · 29,002 cycles

VERTICAL SUPPORT AT BS 1028 AFT BULKHEAD IN AFT CARGO BAY CORRODED. REPLACED THE SUPPORT IAW DRAWING 5965788-15A.

Part: LONGERON — CORRODED (BS 1038) · corrosion level 2 · airframe 40,294 hrs · 27,958 cycles

L30 CORRODED AT STA 1038. REPAIRED IAW SRM 53-20-07, REPAIR 3, DWG 9912243.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,557 hrs · 31,658 cycles

FOUND AISLE FLOORBOARD SOFT AT SEAT ROW 17. REPAIRED THE FLOORBOARD IAW SRM 53-00-50, REPAIR 2. TAP TEST WAS PERFORMED AND DELAMINATION WAS FOUND IAW SRM 53-00-50 REPAIR 2. A NEW FLOORBOARD WAS FABRICATED AND REPLACED IAW SRM 53-20-50-2R, AND CARD 2040-0024.

Part: NUT PLATE — WORN (VERTICAL STAB) · airframe 40,283 hrs · 27,950 cycles

VERTICAL STABILIZER MID SPAN PANEL HORSE COLLAR NUTPLATES WORN. REPAIRED OVERSIZE FASTENER HOLE IAW PRI 545887-14, REV 0, ER/A 545887-14, REV. O AND REPLACED NUTPLATES IAW SRM 51-41-01. REF LOG NR 2453267 FOR CORRECT MAJOR REPAIR ANNOTATION.

Part: SKIN — CORRODED (BS 898) · corrosion level 2 · airframe 40,283 hrs · 27,950 cycles

AFT CARGO, SKIN SPLICE AT BS 898 IS CORRODED AT BL 0, REF NR 00199. REPAIRED SKIN SPLICE REF ER/A 545889-14, REV ORIGINAL ASSOCIATED ER/A 14-545889 ADDED FOR AC 9577.

Part: SKIN — CORRODED (BS 898) · corrosion level 2 · airframe 40,283 hrs · 27,950 cycles

AFT CARGO, SKIN SPLICE AT BS 898 IS CORRODED AT BL 0. ACCOMPLISHED REPAIR REF ER/A 545889-14, REV ORIGINAL REF LP 2454063 FOR SDR.

Part: PAN — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 41,550 hrs · 28,988 cycles

AFT CARGO DOOR LOWER FRAME PAN HAS CORROSION. BLENDED CORROSION AND FOUND OUT OF LIMITS, REPLACED THE PAN IAW SRM 53-00-00 FIG. 103.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 40,283 hrs · 27,950 cycles

VERTICAL STABILIZER MID SPAN PANEL FRAME LOWER FASTENER HOLES ELONGATED. REPAIRED IAW REPAIR DWG SG95550001 AND SRM 55-30-01, REPAIR 7.

Part: BEAM — CRACKED (L1 DOOR) · airframe 40,283 hrs · 27,950 cycles

L1 DOOR NR 1 BEAM CRACKED AT FWD END IN RADIUS. L1 INT NR 1 BEAM AT FWD END REPAIRED IAW SRM 52-10-02, REPAIR 7.

Part: BEAM — CRACKED (L1 DOOR) · airframe 40,283 hrs · 27,950 cycles

L1 DOOR NR 1 BEAM CRACKED AT AFT END IN RADIUS. L1 INT NR 1 BEAM AT AFT END REPAIRED IAW SRM 52-10-02, REPAIR 7.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 41,550 hrs · 28,988 cycles

RANDOM CORROSION ALONG EDGE OF FLOOR PANEL & UNDER PLASTIC FLOOR WRAP. CLEANED AND EVALUATED CORROSION IAW SRM 53-00-00 FIG 1. REPLACED IAW DRAWING 9957828.

Part: SHEAR TIE — CORRODED (BS 954) · corrosion level 2 · airframe 41,550 hrs · 28,988 cycles

AFT CARGO BAY SHEAR TIE AT BS 954 IS CORRODED BETWEEN LONERONS 29 AND 30L. REPAIRED IAW SRM 53-00-06 REPAIR 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,903 hrs · 27,652 cycles

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

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,655 hrs · 26,035 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,041 hrs · 25,547 cycles

DURING SERVICE CHECK, FOUND FWD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FWD OVERWING EMERGENCY EXIT BATTERY PACK REF AMM 33-51-03.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,372 hrs · 25,001 cycles

LEFT EXTERIOR OVERWING EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS & OPS CHECKED GOOD IAW AMM 33-51.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 35,728 hrs · 24,423 cycles

DURING LINE CHECK, NOTED THE L1 DOOR SLIDE LACING PINS WERE NOT SECURE AND THE LACING WAS BECOMING DETACHED. THE L1 DOOR WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,369 hrs · 24,128 cycles

LEFT RAIL IN TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 35,369 hrs · 24,128 cycles

EE BAY DOOR JUNCTION BOX SURROUND DOUBLER CRACKED AT BS 160 LOWER AFT CORNER. REPAIRED DOUBLER IAW SRM.

Part: WIRE — LOOSE (CABIN) · airframe 35,369 hrs · 24,128 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT WIRING IAW SWPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,369 hrs · 24,128 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

FORMER CORRODED AT BS 927, LONGERON 30R. REPAIRED FORMER IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

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

Part: FITTING — CORRODED (CABIN) · airframe 34,674 hrs · 23,698 cycles

R1 DOOR SLIDE AFT GIRT BAR FITTING SUPPORT CORRODED. R & R FITTING ASSEMBLY IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

CUSP WEB CRACKED AT STATION 221, RBL 45. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 221JF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 221DF DELAMINATED. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 222 ATF DAMAGED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 222 AGF DAMAGED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 222 AEF DAMAGED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 34,674 hrs · 23,698 cycles

MAIN CABIN FLOOR PANEL 221FF DAMAGED. R & R FLOOR PANEL IAW SRM.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

AFT CARGO COMPARTMENT LONGERON SPLICE CORRODED BETWEEN BS 899 TO BS 1012, LONGERON 30R. REPAIRED LONGERON IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

AFT ACCESSORY COMPARTMENT LT SIDE LOUVER SHROUD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ANGLE — BROKEN (LT SPOILER) · airframe 34,674 hrs · 23,698 cycles

LEFT WING OTBD SPOILER OTBD END T ANGLE BROKEN. R & R T ANGLE IAW SRM & DWG.

Part: DOOR — CRACKED (LT WING) · airframe 34,674 hrs · 23,698 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

LEFT WW FWD DOOR CUT OUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FITTING — CRACKED (RT MLG WW) · airframe 34,674 hrs · 23,698 cycles

RIGHT MLG WW FWD DOOR CUT OUT CLIP CRACKED. R & R CLIP IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

RIGHT WW FWD DOOR CUT OUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: PANEL — CRACKED (RT WING) · airframe 34,674 hrs · 23,698 cycles

RIGHT WING INBD BUTTE DOOR FWD PANEL AT WING SIDE CRACKED. R & R PANEL IAW SRM & DWG.

Part: DOOR — CORRODED (RT WING) · airframe 34,674 hrs · 23,698 cycles

RIGHT WING CTR BUTTE DOOR AT BOTH SURFACES CORRODED. R & R BUTTE DOOR ASSEMBLY IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,674 hrs · 23,698 cycles

FORWARD CARGO DOOR LOWER JAMB PAN CORRODED. R & R PAN IAW SRM.

Part: COVER — MISSING (EXIT SIGN) · airframe 35,418 hrs · 24,158 cycles

EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: LANYARD — LOOSE (L1 DOOR) · airframe 35,316 hrs · 24,094 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED LANYARD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 34,095 hrs · 23,334 cycles

EMERGENCY LIGHT BATTERY PACK FOR BUSINESS CLASS SECTION INOPERATIVE AT STATION 341. R&R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,913 hrs · 23,215 cycles

CEILING EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 1 THROUGH ROW. R&R BATTERY IAW AMM.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 33,528 hrs · 22,983 cycles

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

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

MAIN CABIN FLOOR MEMBRANE CORRODED AT BS 155, RBL 9. REPAIRED DOUBLER IAW SRM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 30,932 hrs · 21,297 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 446 TO BS 674. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 256 TO BS 927. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 256 TO BS 927. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 30,932 hrs · 21,297 cycles

FWD ENTRY DOOR - L1 DOOR INTERNAL STRUCTURE, INTERCOSTAL CRACKED, AFT SIDE OF DOOR HANDLE MECHANISM. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

SKIN CORRODED BETWEEN BS 851 TO BS 870, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 30,932 hrs · 21,297 cycles

RIGHT WING AT I/B SIDE XW 58.500 FRONT SPAR, BONDING STRAP, CRACK. REMOVED AND REPLACED BONDING STRAP 5919110U97, PO 790191208 IAW B717 SRM 51-40-08 AND 51-41-05.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 30,932 hrs · 21,297 cycles

LEFT WING I/B SIDE AT XCW 58.500 FRONT SPAR, BONDING STRAP CRACK AT BOTTOM SIDE. REMOVED AND REPLACED 5919110U97 BONDING STRAP, PO 790191208 IAW B717 SRM 51-40-08 AND 51-41-05.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 30,932 hrs · 21,297 cycles

RIGHT NLG STRUT DOOR CUTOUT CRACKED AT CORNER AFT SIDE. REPAIRED DOUBLER IAW SRM & AMM.

Part: GUSSET — CRACKED (NR 1 NACELLE) · airframe 30,932 hrs · 21,297 cycles

LTW MDDR 221578T- NR 1 APRON CRACKED AT UPPER COWL ATTACH PAINT. REMOVED AND REPLACED GUSSET IAW SRM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 30,653 hrs · 21,104 cycles

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

Part: SLIDE — LOOSE (R1 DOOR) · airframe 30,447 hrs · 20,974 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.

Part: WIRE — BROKEN (CABIN)

ROW 15 DEF EMERGENCY PATH LIGHTING INOPERATIVE. REPAIRED BROKEN WIRES IAW SWPM 20-20. OPS CHECKED NORMAL IAW AMM 33-51-00.

Part: LIGHT — MISSING (CABIN)

EPL BULBS AND LENSES MISSING AT ROWS 14, 15, AND 21. RELAMPED AND INSTALLED NEW LENS COVERS. RED LENS INSTALLED AT ROW 21. OPS OK FOR ALL.

Part: PIN — UNSECURE (L1 DOOR SLIDE)

L1 GIRT DOOR ATTACH CABLE POPPED OFF WHEN DOOR OPENED. RE-INSTALLED LANYARD PIN AS OUTLINED IN 717 MM 25-61.

Part: STRAP — DETACHED (GIRT BAR)

L1 DOOR GIRT BAR STRAP NOT ATTACHED. RE-INSTALLED GIRT BAR STRAP.

Part: LENS — MISSING (CABIN)

THE 21D MISSING RED EMERGENCY LIGHT COVER. REPLACED LIGHT LENS 21D.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FIRST CLASS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FIRST CLASS EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW B717 AMM 33-51, OPS CHECK GOOD.

Part: PRINTER — MALFUNCTIONED (ACARS)

SMOKE COMING OUT OF ACARS PRINTER IN COCKPIT NO C/B'S POPPED. REMOVED AND REPLACED ACARS PRINTER REF AMM 31-32-01.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 1022, LONG L26L TO L26R, CORROSION. ACCOMPLISHED FRAME SPLICE REPAIR PER B717 SRM 53-00-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD AIRSTAIR HANDLE BASE FLOOR SUPPORT, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: PANEL — CORRODED (CABIN)

CABIN GRILL PANEL, STA 237 TO 256, RBL 57, CORROSION. ACCOMPLISHED GRILL PANEL SPLICE REPAIR PER B717 SRM 51-70-11 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 256, LBL15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 246, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 8 TO LBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 8 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SKIN — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR LOWER FWD CORNER SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: RIB — GOUGED (LT NACELLE)

LEFT LOWER ENGINE COWLING RIB, GOUGED. ACCOMPLISHED ENGINE COWLING RIB ANGLE AND FILLER REPAIR PER B717 SRM 54-20-05 FIG 201 REPAIR 3.

Part: SKIN — CRACKED (FUSELAGE)

LEFT FUSELAGE SKIN, STA 208, LONG L15L, CRACKED. ACCOMPLISHED FUSELAGE SKIN FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1.

Part: SKIN — CRACKED (FUSELAGE)

LEFT FUSELAGE SKIN, STA 208, LONG L11L, CRACKED. ACCOMPLISHED FUSELAGE SKIN FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 20 1 REPAIR 1.

Part: LIGHT — MISSING (CABIN)

ROW 21 RIGHT SIDE, BOTH ESCAPE LENSES MISSING. BULBS WERE FOUND MISSING FROM THE FRONT AND AFT POSITIONS. REPLACED MISSING BULBS AND LENSES (RED), AND OPS CHECK PER AMM 33-51.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 22D EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. RELAMPED EPL AT SEAT 22D. OPS CHECK OK, REF 33-00.

Part: SKIN — DENTED (FUSELAGE)

MDDR 141071T - LT FUS STA 240 DENTED - PREVIOUSLY REPAIRED. CUT OUT DAMAGED AREA, INSTALLED FLUSH REPAIR PER B717 SRM 53-00-01 REPAIR 6 FIG 201.

Part: CONNECTOR — LOOSE (CABIN)

E PATH LIGHT AT ROW 24 INOP. REMOVED AND REPLACED LAMPS, RESECURED LOOSE CONNECTOR IAW B717 MM 33-51.

Part: SKIN — DAMAGED (FUSELAGE)

DAMAGE TO RIGHT FUSELAGE JUST AFT OF RIGHT AOA VANE. CUT OUT DAMAGED SECTION AT RIGHT HAND FUSELAGE, FABRICATED DOUBLER REPAIR AND REPAIRED SKIN PER AIRTRAN EA17-53-01150IR.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

TEST OF EMERGENCY LIGHTS FOR SERVICE CHECK, TC601 STEP 34, REVEALED LIGHT INOPERATIVE AT SEAT 23D. REPAIRED BROKEN WIRE AT SEAT 23D IAW GMM 12-00-00, SYS CHECKS GOOD.