N928AT

Part: SKIN — CRACKED (ZONE 200) · airframe 60,406 hrs · 43,921 cycles

CRACK EVIDENCE ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L. SUMMARY OF NRC 0180: AREA WAS REPAIRED ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L PER PRI 624765-14 REV 2 AND PER ER/A 624765-14 REV ORIG SECTION I. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (07MAR25) REF LP 0849461. ASSOCIATED ER/A 14-624765 ADDED FOR AC 9571. (LP #0849867)

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 60,406 hrs · 43,921 cycles

THE EMERGENCY LIGHT DOES NOT TURN ON IN THE AFT ACCESSORY VENTRAL WALKWAY. SUMMARY OF NRC 00219: CONNECTOR P1-260 OF BATTERY PACK B5-250 AND CONNECTOR P1-116 OF BATTERY PACK B5-116 WAS CONNECTED CORRECTLY PER B717 WDM 33-51-11 AND PERFORMED TEST PER B717 AMM 33-51-00. OPERATIONAL TEST SATISFACTORY. (LP #0847895)

Part: FRAME — CRACKED (ZONE 100) · airframe 60,406 hrs · 43,921 cycles

CRACK ON FRAME STA Y=1037 LONG 17 LH. SUMMARY OF NRC 00189: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0845545)

Part: SKIN — WORN (ZONE 800) · airframe 60,406 hrs · 43,921 cycles

WEAR ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1. SUMMARY OF NRC 00036: DAMAGE ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1 WAS REPAIRED PER ER/A 624489-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624489-14 REV 1. ASSOCIATED ER/A 14-624489 ADDED FOR AC 9571. (LP #0838935)

Part: PAN — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,406 hrs · 43,921 cycles

CORROSION ON AFT CARGO DOOR JAMB PAN BTW LONG 24RH TO LONG 27RH (NEW SECTION AND PRODUCTION SECTION OF PAN). SUMMARY OF NRC 00118: CORROSION LEVEL 2. CARGO DOOR JAMB PAN STA 954 LONG 28 LH AND STA 986 BTW LONG 28 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R REPAIR 7. (LP #0835949)

Part: FASTENER — LOOSE (ZONE 300) · airframe 60,406 hrs · 43,921 cycles

-AD- LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE FOUND IN REFERENCE TO AMDS 5530-01048-02 STEP 3 "AA 5530-01048" AND "AD 2018-10-08". SUMMARY OF NRC 00058: FASTENERS (5 EA) OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE REPLACED AND FASTENERS HOLES AND COUNTER SINKS WERE CHECKED AND FOUND OK PER AMDS 5530-01048-02. ASSOCIATED AA 5530-01048 ADDED FOR AC 9571. (LP #0819455)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,015 hrs · 42,728 cycles

ON SERVICE CHECK FOUND OVERWING EMERGENCY EVACUATION LIGHTS NOT ILLUMINATING. REPLACED OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LIGHTS NOW ILLUMINATE CORRECTLY. (LP #6026764)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,483 hrs · 42,273 cycles

THE CABIN CREW NOTED THAT THE AFT TAIL COMPT EMERGENCY EXIT LIGHT LENS IS MISSING. MAINTENANCE INSTALLED THE MISSING LIGHT COVER AT AFT TAIL OF AIRCRAFT. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #5829167)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,113 hrs · 40,232 cycles

PARTS DEPARTED AICRAFT. GROUND CREW FOUND AIRCRAFT PANEL ACCESS DOOR MISSING. MAINTENANCE REPLACED THE GROUND AIR PANEL ACCESS DOOR. TOP/3998-23 (LP #4027955)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,106 hrs · 40,226 cycles

ARCING LIGHT WITH ASSOCIATED SMELL AND NOISE FROM BEHIND TRIM FORWARD OF F/O CLEARVIEW WINDOW. CBZ24 PULLED R/H WINDSHIELD ANTI-ICE FOR TROUBLESHOOTING NA 2375451. REMOVED R1 WINDSHIELD IAW B717 56-11-02. PERFORMED TERMINAL BLOCK REPLACEMENT PER ERA 608256-14 UP TO STEP 4 OF SECTION 1 TIME LIMITED REPAIR INSTRUCTIONS. INSTALLED R1 WINDSHIELD PER B717 AMM 56-11-02. OPS CHECK GOOD. C/W ERA 608256-14. (LP #4027944)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,979 hrs · 40,113 cycles

AIRCRAFT 9571, INITIAL INSPECTION: BROKEN BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING. CORRECTIVE ACTION: BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING WERE REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2694546)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,979 hrs · 40,113 cycles

AIRCRAFT 9571, INITIAL INSPECTION: CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-04-0G, B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G. AND B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP 2694036)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,979 hrs · 40,113 cycles

AIRCRAFT 9571, CORROSION AT SLIDE SUPPORTS LOCATED AT RBL 53 BETWEEN STA-163 AND STA-186. CORRECTIVE ACTION: NEW SUPPORTS (2EAS) WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6. (LP 2686865)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,979 hrs · 40,113 cycles

AIRCRAFT 9571, DURING OK TO TREAT RH WING BOX AREA WITH CIC, CRACKED CUSP MEMBRANE WEB WAS FOUND ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: CUSP MEMBRANE WEB ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP 2686385)

Part: NONE — NONE · airframe 55,946 hrs · 40,085 cycles

SHIP 9571 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY INTO ATL DUE TO THE "RIGHT HYDRAULIC LOW-PRESSURE" MESSAGE. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT HYDRAULIC SYSTEM RESERVOIR. (LP #4127322)

Part: LIGHT — MISWIRED (CABIN) · airframe 55,635 hrs · 39,819 cycles

FOUND EMERGENCY LIGHT FLOOD LIGHT AT R1 DOOR INOPERATIVE. FOUND POWER WIRE FOR EMERGENCY LIGHT IN WRONG TERMINAL. RE-CONFIGURED PER WDM 33-51-12. ALSO FOUND POWER SUPLY BAD AND REPLACED IT PER B717 AMM 33-51. (B5-235) EMERGENCY LIGHT OPERATION IS NOW NORMAL. (LP #8952931)

Part: HUB CAP — MISSING · airframe 54,386 hrs · 38,671 cycles

ON LANDING IN KGRR, GOT "ANTI-SKID L FAIL" MESSAGE. ON SD BRAKES WERE NOT APPLIED UNTIL ABOUT 75 KNOTS ON LANDING ROLL. *** CONTRACT MAINTENANCE EVENT - OCM: 248846 *** FOUND LT INBD HUBCAP MISSING. INSTALLED NEW HUBCAP ASSY REF B717 AMM 32-41. C/W RTS CK OF ANTI-SKID SYS PER B717 AMM 32-45. ALL CHECK OK. NO CURRENT FAULTS. AIRCRAFT OK FOR SERVICE. (LP #8576544)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,629 hrs · 34,577 cycles

THE EMERGENCY EXIT SIGN IS INOPERATIVE AT 602. EXIT PLACARD IS MISSING ON CEILING EXIT SIGN AT WINDOW EXITS. MAINTENANCE FOUND THE MISSING EXIT SIGN AND REINSTALLED IT IN SERVICEABLE CONDITION. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #1494469)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,629 hrs · 34,577 cycles

THE EMERGENCY EXIT SIGN IS INOPERATIVE AT 603. EXIT PLACARD MISSING ON CEILING EXIT SIGN AT WINDOW EXITS. MAINTENANCE FOUND THE MISSING EXIT SIGN LENS AND REINSTALLED IT IN SERVICEABLE CONDITION. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS NOW OK FOR SERVICE. (LP #1494470)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,028 hrs · 34,095 cycles

THE TAIL COMPARTMENT EMERGENCY FLOOD LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, B5-260, IAW B717 AMM 33-51 AND WDM 33-51-11. LIGHTS NOW CHECK GOOD. (LP #6532443)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,207 hrs · 33,498 cycles

OVERHEAD EMERGENCY LIGHT FORWARD OF ROW 1 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-57-03. OPERATIONAL CHECK OF THE LIGHTS IS NOW GOOD. (LP #5967728)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,007 hrs · 33,371 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THE CEILING PANEL EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN THE OVER WING EXITS TO THE AFT LAVATORIES. THE BATTERY PACK B5-231 WAS FOUND TO BE BAD AND WAS REPLACED. OPERATIONAL CHECK IS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #5954816)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,789 hrs · 33,219 cycles

BOTH AFT OVERWING EXIT DOOR SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-230. OPERATIONAL CHECK IS GOOD REF B717 AMM 33-51. OK FOR SERVICE. (LP #5813918)

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

SHEAR TIE CLIP STA 1152 LONG 2-3L WAS FOUND CRACKED (CAT). NRC 00608: SHEAR TIE CLIP STA 1152 LONG 2-3L WAS REPLACED PER ER/A 534014-14 REV. A SECTION II AND ETI-17-19-042 REV. 1. ASSOCIATED ER/A 14-534014 ADDED FOR AC 9571. (LP #0992033)

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON LAVATORY SERVICE PAN (FUS). NRC 00016: CORROSION LEVEL 2, CORROSION IS OUT OF LIMITS SO LAVATORY SERVICE PAN WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G TOOL USED P/N TE25AC S/N C1048 D/D 21AUG19. (LP #0990264)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON DOOR JAMB INTERNAL ESTRUCTURE (AFT AREA) AT FWD ACCESORY COMPARTMENT DOOR. (CDA). NRC 00474: CRACK ON DOOR JAMB INTERNAL ESTRUCTURE AT FWD ACCESORY COMPARTMENT DOOR WAS REPAIRED PER ETI-17-19-044 REV 2 AND ER/A 576425-14 REV ORIG. SECTION I. ASSOCIATED ER/A 00-576425 ADDED FOR AC 9571. (LP #0989843)

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON CUTOUT SURROUND ALSO ON FUSELAGE SKIN AT FWD LOWER CORNER OF LAVATORY SERVICE ACCESS (FUS). NRC 00015: CRACK ON CUTOUT SURROUND ALSO ON FUSELAGE SKIN AT FWD LOWER CORNER OF LAVATORY SERVICE ACCESS WAS REPAIRED PER ETI-17-19-028 REV 4 AND ER/A 576379-14 REV ORIGINAL SEC I. ASSOCIATED ER/A 14-576379 ADDED FOR AC 9571. (LP #0988981)

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON FLAP FITTING AND LOWER EXTERNAL PIN AT FLAP HINGE STA 251.6. RT WING. (AD). NRC 00381: CORROSION LEVEL 2, CENTER WING FLAP LOWER EXTERNAL PIN WAS REPLACED PER AMM 57-55-25-401. HINGE FITTING RT WAS REPLACED FOR SERVICEABLE HINGE FITTING PER AMM 57-55-25-400-802. (LP #0987830)

Part: RETAINER — CRACKED (WINDOW) · airframe 47,348 hrs · 32,882 cycles

CRACK ON UPPER AFT CORNER OF LT CLEAR VIEW WINDOW RETAINER. (CPIL). NRC 00356: CRACK ON UPPER AFT CORNER OF LT CLEAR VIEW WINDOW WAS REPAIRED PER SRM 56-10-02-2R-1. (LP #0987009)

Part: HINGE FITTING — CRACKED (LT ELEVATOR) · airframe 47,348 hrs · 32,882 cycles

LT ELEVATOR HINGE FITTING STA XE103 WAS FOUND CRACKED (EHV). NRC 00368: LT ELEVATOR HINGE FITTING STA XE103 WAS REPAIRED PER ETI-17-19-024 REV. 6 AND ER/A 576382-14 REV. ORIGINAL SECTION I. ASSOCIATED ER/A 00-576382 ADDED FOR AC 9571. (LP #0986322)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON INTERCOSTAL INTERNAL SKIN AROUND ANNTENA CONNECTOR AT STA 917 APROX BTW LONG 30 AND 29L AT AFT CARGO (C2). NRC 00260: CORRROSION LEVEL 2, CORROSION IS OUT OF LIMITS AND INTERCOSTAL INTERNAL SKIN AROUND ANNTENA CONNECTOR WAS REPLACED PER SRM 51-41-02-0G. (LP #0984979)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON LONG 30 FROM STA 1028 TO 889 AFT CARGO COMPT (C2). CORROSION LEVEL 2, CORROSION WAS REMOVED PER SRM 51-10-04-OG PAR 26. (UT) WAS ACCOMPLISHED PER NDT/SPM 04-00-07, PAR. 5, FIG. 3, SHEET. 1-2. ON LONG 30 FROM STA 1028 TO 889 AFT CARGO COMPT ORIGINAL THICKNESS IS 0.125" AND MINIMUM REMAINING THICKNESS FOUND IS 0.082"; THEREFORE AREA IS OUT OF LIMITS PER SRM 53-00-00-1A. SECTION DAMAGE ON LONGERON WAS REPLACED PER SRM 53-20-05-01 FIG1. (LP #0984941)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 47,348 hrs · 32,882 cycles

TWO CRACKS ON VERTICAL STAB LEADING EDGE STA Y=1095.868 AND Y=1133 LT/RT SIDE. (EHB). NRC 00050: CRACKS (2EA) ON VERTICAL STAB LEADING EDGE STA Y=1095.868 AND Y=1133 LT/RT SIDE WERE REPAIRED PER SRM 55-30-01-2R-5 FIG 201 AND 202 REPAIR 5, 51-41-02-0G, AND 51-41-05-0G. (LP #0985245)

Part: FORMER — WORN (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

WORN FORMER ON STA Y=800 UNDER LWR MARKER BEACON LIGHT ACCESS PANEL (FUS). NRC 00346: FORMER ON STA Y=800 WAS REPLACED PER SRM 53-20-02-0I, 51-20-09-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0984244)

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,352 hrs · 32,886 cycles

2 (EA) CRACKS ON FUSELAGE SKIN STA. 102 LONGERONS 27L AND 27R. ON NLG AFT DOORS. CRACKS (2EA) ON FUSELAGE SKIN STA. 102 LONGERONS 27L AND 27R. ON NLG AFT DOORS WERE REPAIRED PER SRM 53-10-01-2R-11 REPAIR 11 PERFORM DECAL CONDITION INSPECTION EVERY "C" CHECK PER TOPP MANUAL 30-10-70 PAR.I PAGE 14. (LP0985015)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT (5231-2002). (CCT). NRC 00191: CORROSION LEVEL 2, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-15-2R-7 FIG 201 REPAIR 7. (LP #0983196)

Part: SKIN — DENTED (TE FLAP) · airframe 47,348 hrs · 32,882 cycles

DENT ON FLAP LOWER SKIN 73'' FROM INBD EDGE AND 18'' FROM T/E APROX AT LT WING. (AI). NRC 00642: DENT OUT OF LIMITS ON FLAP LOWER SKIN AT LT WING WAS REPAIRED PER SRM 57-00-00-2R-2 PAR. 4. A FIG. 201. (LP #0983336)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON AFT CARGO COMPARTMENT FRAME AND CHANNEL STA Y=1023 BTW LONGS 29L AND 29R (5331-2001)(C2). NRC 00313: CORROSION LEVEL 2, FRAME AND CHANNEL STA Y=1023 BTW LONGS 29L AND 29R WERE REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #0981974)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACKED LONGERON 2L AT AFT ACCESSORIES COMPARTMENT STA Y=1133 (CAT). NR 00423: LONGERON 2L AT AFT ACCESSORIES COMPARTMENT STA Y=1133 WAS REPAIRED PER SRM 53-00-05-2R FIGURE 201 REPAIR 2 AND 51-41-05-0G. (LP #0978743)

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 47,348 hrs · 32,882 cycles

CORROSION AT FWD BASE AREA ON FO INBOARD SEAT TRACK (CPIL). NRC 00468: CORROSION LEVEL 1, FWD BASE AREA ON FO INBOARD SEAT TRACK WAS REPAIRED PER ER/A 576216-14 REV. ORG. SECTION I AND ETI-17-19-043 REV. 1. ASSOCIATED ER/A 00-576216 ADDED FOR AC 9571. (LP #0979396)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

IN REF NRC 00452 AFTER ANGLE REMOVAL, CORROSION WAS FOUND ON WEB FROM STA 200 TO 207 X=53 APPROX AT FWD WET AREA (W1). NRC 0575: CORROSION LEVEL 2, WEB FROM STA 200 TO 207 X=53 APPROX AT FWD WET AREA WAS REPAIRED PER ETI-17-19-029 REV. 1 AND ER/A 576187-17 REV. ORIG. SECTION I. ASSOCIATED ER/A 00-576187 ADDED FOR AC 9571. (LP #0977223)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON SEAT TRACK 56 LT ON STA Y=774 TO STA Y=776, STA Y=806 TO STA Y=806, AND STA Y=835 TO Y=838 AT CABIN PASSENGER (CPAX). NRC 00633: CORROSION LEVEL 2, SEAT TRACK 56 LT ON STA Y=747 TO Y=862 WAS REPLACED PER SRM 53-20-52-2R-5 AND 51-41-01-0G. (LP #0975383)

Part: CUSP WEB — CUT (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CUT ON RT CUSP ANGLE AND FINGER DOUBLER AT STA Y=486. (CPAX). NRC 00563: RT CUSP ANGLE AND FINGER DOUBLER AT STA Y=486 WAS REPAIRED PER SRM 53-00-55-2R-4 AND DGW #S2777976 REV. B. (LP #0975105)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON CUSP MEMBRANE WEB FROM STA Y=200 TO Y=218 RT SIDE AT PAX CABIN (AMDS 5300-2020). (CPAX). NRC 00188: CORROSION LEVEL 2, CORROSION ON CUSP MEMBRANE WEB FROM STA Y=200 TO Y=218 RT SIDE AT PAX CABIN WAS OUT OF LIMITS AND WAS REPLACED PER DWG #9936535 REV. "CS", SRM 51-41-02-0G, AND 51-41-08-0G. (LP #0974983)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON CUSP MEMBRANE WEB FROM STA Y=218 TO Y=237 RT SIDE AT PAX CABIN (5300-2020) (CPAX). NRC 00187: CORROSION LEVEL 2, REPLACED CUSP WEB PER SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0975731)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION OUT OF LIMITS ON SEAT TRACK 56R BTW STA Y=446 TO Y=481 AT PAX CABIN IN REF NRC S/N 00075. NRC 00641: CORROSION LEVEL 2, SEAT TRACK 56R BTW STA Y=446 TO Y=481 AT PAX CABIN WAS REPAIRED PER SRM 53-20-52-2R-5 AND 51-41-01-0G. (LP #0975559)

Part: FRAME — CRACKED (NLG WW) · airframe 47,348 hrs · 32,882 cycles

CRACK ON NLG FRAME WHEEL WELL STA 45.5 LT SIDE. (FYT). NRC 00610: NLG FRAME WHEEL WELL STA 45.5 LT SIDE WAS REPAIRED PER SRM 53-10-14-2R-2, 51-40-02-0G, AND 51-40-05-0G. (LP #0974887)

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON METALIC FLOOR PANEL BTW R1 DOOR SCUFF PLATE AND FLOOR PANEL 221EF. (CPAX). NRC 00612: CORROSION LEVEL 2, METALIC FLOOR PANEL BTW R1 DOOR SCUFF PLATE AND FLOOR PANEL 221EF WAS REPLACED PER DGW #9957828 REV.: AB. (LP #0973822)

Part: HINGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON LT APU DOOR HINGE AFT SIDE (FUS). NRC 00433: CORROSION LEVEL 2, LT APU DOOR HINGE AFT SIDE WAS REPLACED PER AMM 52-45-01 000-801 PAR. B. (1). (B) AND AMM 52-45-01 400-801 PAR. B. (1).(B). (LP #0974491)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON SEAT TRACK 56R BTW STA Y=898 TO Y=1022 AT PAX CABIN. NRC 00079: CORROSION LEVEL 2, CORROSION ON SEAT TRACK 56R BTW STA Y=898 TO Y=1022 AT PAX CABIN WAS OUT OF LIMITS AND WAS REPAIRED PER SRM 53-20-52-2R REPAIR 5 FIG 201. (LP #0974805)

Part: FRAME ANGLE — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACKED FRAME CLIPS ON RIGHT ENGINE PYLON SUPPORT BULKHEAD STA Y=1022 BTW LONGS 13L-14L AND LONGS 16L-17L AT PAX CABIN (CPAX). NRC 00499: FRAME CLIPS (2EAS) ON RIGHT ENGINE PYLON SUPPORT BULKHEAD STA Y=1022 BTW LONGS 16L-17L WERE REPLACED PER SRM 51-41-02-0G, 51-41-05-0G, AND DWG #9912243 REV:JS AND (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FRAME CLIP STA Y=1022 BTW LONGS 13R-14R AND NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001 EQUIPMENT: N/C 1601 EXP 15MAR19. (LP #0972563)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON ANGLE CUSP ON R1 LOWER DOOR JAMB FROM Y=160 TO Y=200 AT CABIN PAX (5300-2010). (W1). NRC 0318: CORROSION LEVEL 2, ANGLE CUSP ON R1 LOWER DOOR JAMB FROM Y=160 TO Y=200 AT CABIN PAX WAS REPAIRED PER REPAIR PER ETI-17-19-020 REV.1. AND SRM 51-41-02-0G, 51-41-05-0G, AND ER/A 575992-14 REV. ORIG. ASSOCIATED ER/A 00-575992 ADDED FOR AC 9571. (LP #0972583)

Part: FRAME ANGLE — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACKED FRAME CLIPS ON LEFT ENGINE PYLON SUPPORT BULKHEAD STA Y 1022 BTW LONGS 13L-14L AND LONGS 16L-17L AT PAX CABIN (CPAX). NRC 00498: FRAME CLIPS (2 EAS) ON LEFT ENGINE PYLON SUPPORT BULKHEAD STA Y=1022 BTW LONGS 16 AND 17 WERE REPLACED PER SRM 51-41-02-0G AND SRM 51-41-05.-0G AND DWG #9912243 REV: JS AND (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FRAME CLIP AT SUPPORT BULKHEAD STA Y=1022 BTW LONGS 13L-14L AND NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001. EQUIPMENT: N/C 1601 EXP 15MAR19. (LP #0971897)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,348 hrs · 32,882 cycles

DELAMINATION ON FLOOR PANELS #222KF, 211ANF, AND 222ATF AT PAX CABIN. (CPAX). NRC 00576: FLOOR PANELS #222KF, 211ANF, AND 222ATF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0970049)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,348 hrs · 32,882 cycles

DELAMINATION ON FLOOR PANELS #221QF, 211ALF, AND 223GF AT PAX CAB. (CPAX). NRC 00582: FLOOR PANELS #221QF, 211ALF, AND 223GF AT PAX CABIN WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0968165)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK ON FUEL ACCESS PANEL #520CT AT LT WING (AI). NRC 00585: CORROSION LEVEL 2, FUEL ACCESS PANEL #520CT AT LT WING CORROSION WAS FOUND OUT OF LIMITS PER SRM 57-10-01-2R PROCEDURE 2 PARAGRAPH 5 CONDITION II AND III. THEREFORE FUEL ACCESS PANEL #520CT AT LT WING WAS REPLACED AND APPLICABILITY WAS VERIFIED PER IPC 57-22-01-01 ITEM 65. (LP #0968155)

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK ON FUEL ACCESS PANEL #620CT AT RT WING (AD). NRC 00584: CORROSION LEVEL 2, FUEL ACCESS PANEL #620CT AT RT WING CORROSION WAS FOUND OUT OF LIMITS PER SRM 57-10-01-2R PROCEDURE 2 PARAGRAPH 5 CONDITION II AND III. THEREFORE FUEL ACCESS PANEL #620CT AT RT WING WAS REPLACED AND APPLICABILITY WAS VERIFIED PER IPC 57-22-01-01 ITEM 65. (LP #0967963)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION OUT OF LIMITS ON SEAT TRACK 56R FROM STA Y=379 TO STA Y=381 AND FROM STA Y=395 TO STA Y=397 AT PAX CABIN IN REF NRC 00074. (CPAX). NRC 00625: CORROSION LEVEL 2, SEAT TRACK 56R FROM STA Y=379 TO STA Y=381 AND FROM STA Y=395 TO STA Y=397 AT PAX CABIN WAS REPAIRED PER SRM 53-20-52-2R-1 PAR. 4 FIG. 201. (LP #0968370)

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 47,348 hrs · 32,882 cycles

PUNCTURE ON FLOOR PANEL #222ARF AT PAX CAB. (CPAX). NRC 00579: FLOOR PANEL #222ARF AT PAX CABIN WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0967983)

Part: FORMER — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON FORMERS STA Y=674, 696, & 715 ON LT SIDE AT UNDERWING KEELBEAM AREA (FUS). NRC 0599: FORMERS STA Y=674, 696, & 715 ON LT SIDE AT UNDERWING KEELBEAM AREA WERE REPAIRED PER SRM 51-70-11-2R-1 FIG. 201, 51-41-02-0G, AND 51-41-05-0G. (LP #0967068)

Part: FORMER — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON FORMERS STA Y=674, 696, & 715 ON RT SIDE AT UNDERWING KEELBEAM AREA (FUS). NRC 0600: FORMERS STA Y= 674, 696, & 715 ON RT SIDE AT UNDERWING KEELBEAM AREA WERE REPAIRED PER SRM 51-70-11-2R-1 FIG. 201, 51-41-02-0G, AND 51-41-05-0G. (LP #0967076)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACKED AFT SUPPORT BTW BEAM 3 AND PAN AT AFT CARGO COMPARTMENT DOOR. (PTAS). NRC 196: NEW AFT SUPPORT "FITTING" BTW BEAM 3 AND PAN AT AFT CARGO COMPARTMENT DOOR WAS REPLACED PER SRM 51-41-01-0G, 51-41-05-0G, AND DWG #3914025 REV. C. (LP #0965754)

Part: PAN — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK AT INNER PAN FWD EDGE BELOW OF STOP FITTING NR 3 FWD CARGO COMPARTMENT DOOR. (PTAS) IN REFERENCE NRC 00217. NRC 00623: INNER PAN FWD EDGE BELOW OF STOP FITTING NR 3 FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER SRM 52-30-02-2R REPAIR 3 FIG 201. (LP #0965992)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON CUSP MEMBRANE WEB FROM STA Y=636 TO Y=655 LT SIDE AT PAX CABIN. (CPAX). NRC 00619: CUSP MEMBRANE WEB FROM STA Y=636 TO Y=655 LT SIDE WAS REPAIRED PER SRM 53-00-55-2R-4- FIG 220 REPAIR 4. (LP #0963874)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 47,348 hrs · 32,882 cycles

CRACK ON FLOOR SUPPORT BELOW SEAT TRACK X=44 STA Y=737 AND ALSO CRACK ON FLOOR SUPPORT BELOW SEAT TRACK X=-44 STA Y=737. (WB). NRC 00324: FLOOR SUPPORTS BELOW SEAT TRACK X=44 STA Y=737 AND FLOOR SUPPORT BELOW SEAT TRACK X=-44 STA Y=737 WERE REPLACED PER SRM 51-41-05-0G AND 51-41-02-0G. (LP #0964465)

Part: SUPPORT — CRACKED (CARGO DOOR AREA) · airframe 47,348 hrs · 32,882 cycles

CRACKED FWD SUPPORT BTW BEAM 5 AND PAN AT AFT CARGO COMPARTMENT DOOR. NRC 00195: FWD SUPPORT BTW BEAM 5 AND PAN AT AFT CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0962888)

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 47,348 hrs · 32,882 cycles

CRACK ON CUSP MEMBRANE WEB FROM STA Y=655 TO Y=715 LH SIDE AT PAX CABIN. NRC 00141: CUSP MEMBRANE WEB FROM STA Y=655 TO Y=715 LH SIDE AT PAX CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 FIG 225 SHEET 5 AND 51-41-02-0G. (LP #0961393)

Part: CUSP WEB — CRACKED (BS 813-832) · airframe 47,348 hrs · 32,882 cycles

CRACK ON CUSP MEMBRANE WEB FROM STA Y=813 TO Y=832 RH SIDE AT PAX CABIN. (CPAX). NRC 0177: CUSP MEMBRANE WEB FROM STA Y=813 TO Y=832 RH SIDE AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 226 (SHEET1), SRM 51-41-02-0G, AND SRM 51-41-05-0G. (LP #0961395)

Part: SUPPORT — WORN (DOOR HINGE) · airframe 47,348 hrs · 32,882 cycles

WORN SUPPORT ON CABIN PRESSURE BULKHEAD DOOR LOWER HINGE AREA (PTAS). NRC 00506: SUPPORT ON CABIN PRESSURE BULKHEAD DOOR LOWER HINGE AREA WAS REPAIRED PER B717-200 SRM 52-10-02-2R REP. 16, PAR 4, A, OPTION 1. (LP #0958537)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION OUT OF LIMITS ON CUSP MEMBRANE WEB FROM STA Y=411 TO Y=414 RT SIDE AT PAX CABIN IN REF NRC S/N 00184. (5300-2020). (CPAX). NRC 0590: CORROSION LEVEL 2, CUSP MEMBRANE WEB FROM STA Y=411 TO Y=414 RT SIDE AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 215. AND SRM 51-41-05-0G. (LP #0958731)

Part: CUSP WEB — CORRODED (BS 908-954) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON CUSP MEMBRANE WEB FROM STA Y=908 TO Y=954 RH SIDE AT PAX CABIN (AMDS 5300-2020). (CPAX). NRC 00173: CORROSION LEVEL 2, CUSP MEMBRANE WEB FROM STA Y=908 TO Y=954 RH SIDE AT PAX CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 FIG 225 SHEET 5, SRM 51-41-02-0G, AND SRM 51-41-05. (LP #0958656)

Part: CUSP WEB — CORRODED (BS 855) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION OUT OF LIMITS ON CUSP MEMBRANE (WEB) ON STA Y=855 RH SIDE AT PAX CABIN IN REF NRC 00170 (AMDS 5300-2020). NRC 0588: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) ON STA Y= 855 RH SIDE AT PAX CABIN WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIGURE 216 AND SRM 51-41-02-0G. (LP #0958732)

Part: ACCESS PANEL — DAMAGED (WING) · airframe 47,348 hrs · 32,882 cycles

ELONGATED HOLES ON FUEL ACCESS PANELS 620LB AND 620MB (AD). NRC 00617: FUEL ACCESS PLATE #620MB WAS REPAIRED PER B-717 200 SRM 57-10-01-2R PAR. 5 B. CONDITION II. TOOL USED: DIGITAL CALIPER P/N: 500-171-30 S/N: A1720947 DUE DATE: 20MAR19 AND ACCESS PLATE #620LB WAS REPLACED, THE APPLICABILITY WAS VERIFIED ACCORDING PER B717 IPC 57-23-01-01, ITEM 220J. (LP #0958655)

Part: ANGLE — CRACKED · airframe 47,348 hrs · 32,882 cycles

CRACKED ANGLE ON FWD BULKHEAD OF CENTER TANK THROUGH FWD CARGO COMPARTMENT LONG 24RH (CCD). NRC 0556: ANGLE ON FWD BULKHEAD OF CENTER TANK THROUGH FWD CARGO COMPARTMENT LONG 24RH WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0956228)

Part: SEAT TRACK — CORRODED (BS 200-218) · corrosion level 2 · airframe 47,348 hrs · 32,882 cycles

CORROSION ON SEAT TRACK X=-22 FROM STA 200-218 AT FWD WET AREA (W1). NRC 00535: CORROSION LEVEL 2, SEAT TRACK X=-22 FROM STA Y=200 TO Y=301 WAS REPAIRED PER B717-200 SRM 53-20-52-2R FIGURE 201 (SHEET 1) REP. 5 AND 51-41-01-0G. (LP #0953284)

Part: RELAY — MALFUNCTIONED (GENERATOR) · airframe 42,620 hrs · 29,521 cycles

DURING APPROACH, EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS IN CEILING CAME ON WHEN LANDING GEAR WAS PUT DOWN. ALSO CAME ON ONCE DURING TAXI . BOTH TIMES WERE ONLY ON FOR ABOUT 1 SECOND. SUSPECT APCDU IS FAULTING. R & R THE APCDU & GENERATOR RELAY IAW AMM 24-21. NO FAULTS NOTED THIS TIME.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 42,610 hrs · 29,515 cycles

DURING LANDING, FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHTS CAME ON BRIEFLY, TWICE. MAINTENANCE PERFORMED AN OPS CHECK IAW FIM 33-50-00 810-801. IAW THE FIM IT WAS AN INTERMITTENT FAULT. NO PREVIOUS HISTORY, OK FOR SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 42,317 hrs · 29,292 cycles

AFT CARGO BAY LOWER DOOR FRAME CORRODED. REPAIRED IAW SRM 53-20-15, FIG 201, REPAIR 7.

Part: SKIN — CRACKED (BS 1087) · airframe 42,317 hrs · 29,292 cycles

SKIN HAS 3/16 INCH LONG CRACK FROM RIVET HOLE AT BS 1087, APPROXIMATELY ONE INCH ABOVE LONGERON 14L. REPAIRED IAW PRI 556129-14, REVISION 0, AND COMPLIED WITH ER/A 556129-14, REVISION ORIGINAL.

Part: SKIN — CRACKED (BS 1087) · airframe 42,317 hrs · 29,292 cycles

SKIN HAS A .50 INCH LONG WYE SHAPED CRACK AT BS 1087, APPROXIMATELY ONE INCH ABOVE LONGERON 14R. REPAIRED IAW PRI 556130-14, REVISION 0, AND COMPLIED WITH ER/A 556130-14, REVISION ORIGINAL.

Part: SKIN — CRACKED (BS 1076) · airframe 42,317 hrs · 29,292 cycles

SKIN HAS A ONE INCH LONG CRACK AT BS 1076, APPROXIMATEY ONE INCH ABOVE LONGERON 14R. REPAIRED IAW PRI 556130-14, REVISION 0, AND COMPLIED WITH ER/A 556130-14, REVISION ORIGINAL.

Part: FRAME — CRACKED (BS 1076) · airframe 42,317 hrs · 29,292 cycles

FRAME CRACKED RT SIDE BS 1076 AFT FLANGE IN RADIUS. REPAIRED IAW PRI 556132-14, REVISION O, AND COMPLIED WITH ER/A 556132-14 REVISION ORIGINAL.

Part: SENSOR — FAULTY (RT MLG) · airframe 36,744 hrs · 25,058 cycles

RIGHT MAIN GEAR INDICATES UNSAFE AFTER TAKEOFF. CYCLED GEAR IAW QRH. R & R RT MLG POSITION SENSOR IAW MM.

Part: CYLINDER — FAULTY (RT MLG) · airframe 36,742 hrs · 25,056 cycles

RIGHT MAIN GEAR SHOWED UNSAFE AFTER TAKEOFF. CYCLED GEAR IAW QUICK REFERENCE. R & R CYLINDER IAW AMM.

Part: GUARD — BENT (RT MLG) · airframe 36,701 hrs · 25,029 cycles

AIR TURN BACK RT MAIN GEAR UNSAFE LIGHT. CYCLED LG, GEAR STILL UNSAFE INDICATION DISPLAYED. R & R RT MLG LATCH GUARD IAW MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 36,463 hrs · 24,866 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,731 hrs · 24,387 cycles

FWD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 35,644 hrs · 24,336 cycles

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

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 35,090 hrs · 23,976 cycles

L1 FLASH LIGHT BRACKET BROKEN. R & R FLASHLIGHT HOLDER IAW MM.

Part: CABLE — MISROUTED (L1 DOOR) · airframe 33,641 hrs · 23,045 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE CONNECTOR MISROUTED. REROUTED CABLE IAW MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 33,469 hrs · 22,944 cycles

FORWARD F/A EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,461 hrs · 22,939 cycles

FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,912 hrs · 22,586 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: ECU — FAILED (SPOILER) · airframe 30,803 hrs · 21,218 cycles

SPOILER OUTBOARD FAILED. REMOVED AND REPLACED SPOILER ELECTRONIC CONTROL UNTIL PER MM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,433 hrs · 20,979 cycles

SEAT TRACK CORRODED AT BS 256, RBL 47. REPAIRED TRACK PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,433 hrs · 20,979 cycles

SKIN CREASED AT BS 218, BETWEEN STR 17L TO STR 18L. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,431 hrs · 20,978 cycles

WEBBED FLOOR SUPPORT CORRODED AT BS 218, BL 56R. REMOVED AND REPLACED WEB IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,433 hrs · 20,979 cycles

SKIN CREASED AT BS 237, BETWEEN STR 17L TO STR 18L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,433 hrs · 20,979 cycles

SHEAR TIE CORRODED AT BS 974, BETWEEN STR 29R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,433 hrs · 20,979 cycles

SEAT TRACK CORRODED AT BS 237, RBL 47. REMOVED AND REPLACED TRACK PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,740 hrs · 21,179 cycles

FUSELAGE SKIN CREASED AT BS 218 BETWEEN, STR 17L TO STR 19L. REPAIRED SKIN IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,431 hrs · 20,978 cycles

CUSP WEB CRACKED AT BS 655, RBL 56. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,431 hrs · 20,978 cycles

SKIN CRACKED BETWEEN BS 846 TO BS 853, BETWEEN LBL 6 TO RBL 6. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (MAIN)

EMER PWR TST FAIL DISPLAYED. RESET BATTERY CHARGER CIRCUIT BREAKER BATTERIES WERE VERY LOW. GIVEN TIME TO CHARGE FULLY. PERFORMED EMERGENCY POWER TEST, TEST PASSED OK ALL INDICATIONS NORMAL. OK FOR SERVICE REF MM 24-30.

Part: LENS — MISSING (CABIN)

E-PATH LIGHT LENSES AT ROWS 12, 18 AND 22 MISSING. INSTALLED MISSING E-PATH LENSES IAW AMM 33-51-04-420-003. OPS CHECK OF EMERGENCY LIGHT SYSTEM NORMAL IAW AMM 33-51-00.

Part: GIRT BAR — UNSECURE (EVAC SLIDE)

FOUND R1 EMERGENCY SLIDE PACKAGE LOOSE AND GIRT BAR DANGLING IN THE WIND. RE-SECURED GIRT BAR ON R1 DOOR SLIDE REF B717 AMM 25-61-03. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LENS — MISSING (CABIN)

EPL LENS MISSING 16D, 21D, 25D. RELAMPED MISSING EP LENS IAW AMM 33-51.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 190 TO 200, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 REPAIR 2 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 148 TO 157, LBL 157, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER BOEING DWG PL9936534.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR PANEL, CORROSION. ACCOMPLISHED FLOOR PANEL REPLACEMENT PER BOEING DWG PL99577828.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 189, RBL 46 TO RBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 148 TO 170, RBL 7, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 189, RBL 8 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

PASSENGER ENTRANCE AREA DOOR JAMB, STA 200, LONG 15, CRACKED. ACCOMPLISHED DOOR JAMB DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 7 TO RBL 7, 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: SKIN — DENTED (FUSELAGE)

RIGHT FWD FUSELAGE BELOW CATERING DOOR, STA 185, DENTED. ACCOMPLISHED DOUBLER AND FINGER REPAIR PER B717 SRM 53-00-01 FIG 201 REPAIR 1.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 15 & 16 EMERGENCY PATH LIGHT INOPERATIVE. RELAMPED ROW 15 & 16 EMERGENCY LIGHT IAW MM 33-20.

Part: COVER — MISSING (CABIN)

ROW 2 EMERGENCY PATH LIGHT MISSING CLEAR COVER. INSTALLED EMERGENCY PATH LIGHT COVER IAW MM 33-20.

Part: LANYARD — BROKEN (EVAC SLIDE)

R1 SLIDE LANYARD BROKEN. REMOVED AND REPLACED SLIDE LANYARD MM 25-61.

Part: LENS — IMPROPER PART (CABIN)

EMERGENCY PATH LIGHTING SEAT 21D, AFT LIGHT WHITE, SHOULD BE RED. REMOVED AND REPLACED EPL LENS AFT AT SEAT 21D FROM CLEAR TO RED REF 33-51. OK FOR SERVICE AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ROWS 1-3 INOPERATIVE ON MAINTENANCE CHECK. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY IAW 33-51. OPS CHECK GOOD.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2979.

Part: FRAME — DAMAGED (FUSLEAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2986.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY PATH LIGHTING AT ROWS 1-10 ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY AND BATTERY IAW B717 MM 33-51. OPS CHECK NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN)

FIRST CLASS EMERGENCY LIGHT PATH LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHT ARE INOP FROM ROW 10 AND ALL OF BUSINESS CLASS, LIGHTS AT FLOOR 2 EA NR 3 GALLEY SIDE WALL AND WALL LIGHTS AT L1-DOOR AND R1 DOOR, THERE'S ONE BULB OUT IN WALL ALL FWD RT OVERWING EXIT. REMOVED AND REPLACED 2 EA EMERGENCY LIGHT BATTERY PACKS LOCATED AT STA 398 & 803. OPS CHECK GOOD, ALL WORK PERFORMED IAW B717 AMM 33-51.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

FOUND EMERGENCY LIGHT INOPERATIVE ROW 1 - 10. REMOVED AND REPLACED BATTERY POWER SUPPLY.