N994AT

Part: LIMITER — DAMAGED · airframe 57,986 hrs · 41,581 cycles

ON WAKEUP FOUND SPEED TAPE ON RH VORTILON. DAMAGE WITHIN LIMITER PER EAA 570743-14MA REV B APPLIED TEMP REPAIR. WILL NEED PERMINENT REPAIR WITHIN 100 FLIGHT HOURS.(7372557)

Part: PAN — CRACKED (ZONE 800) · airframe 56,170 hrs · 39,942 cycles

CRACK ON FWD INNER PAN BTW STA 954 BEAM 3 APPROX AT AFT CARGO DOOR. SUMMARY OF NRC 00086: AFT CARGO DOOR WAS REPLACED WITH A SERVICEABLE AFT CARGO DOOR AND PART NUMBER WAS VERIFIED PER B717-200 AIPC 52-33-01-01 ITEM 130J AND IS INSTALLED UNDER AMDS 5231-4004.

Part: PAN — CRACKED (ZONE 100) · airframe 56,170 hrs · 39,942 cycles

CRACK ON INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00325: INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 621747-14, REV ORIGINAL. ASSOCIATED ER/A 14-621747 ADDED FOR AC 9539. (LP #0671941)

Part: SKIN — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACK ON FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R. SUMMARY OF NRC 0053: FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R WAS REPAIRED PER ER/A 621624-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. MAINTENANCE REQUIREMENTS WERE VERIFIED AND THE FOLLOWING ACTIONS ARE NEEDED: REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 12NOV24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. UNDER LOG 0660286, PER ER/A 621624-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR ASSOCIATED ER/A 14-621624 ADDED FOR AC 9539. (LP #0661534)

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,170 hrs · 39,942 cycles

CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00076: CORROSION LEVEL 2. CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROC 7 REPAIR 7. (LP #0655665)

Part: VANE — DENTED (ZONE 600 FLAP) · airframe 56,170 hrs · 39,942 cycles

DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE FOUND OUT OF LIMITS BY DISTANCE BTWN OTHER DAMAGES. SUMMARY OF NRC 00628: DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE REPAIRED PERMANENTLY PER B717-200 SRM 51-70-02-0G AND 57-53-01-2R-1. (LP #0655190)

Part: ACCESS PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,170 hrs · 39,942 cycles

CORROSION ON ACCESS PANEL 5971074 -1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00616: CORROSION LEVEL 2. ACCESS PANEL 5971074-1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0653678)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,170 hrs · 39,942 cycles

CORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSION LEVEL 2. DOUBLER ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R WAS FABRICATED PER DWG 9923686 REV D AND REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0653581)

Part: VANE — DENTED (ZONE 500 FLAP) · airframe 56,170 hrs · 39,942 cycles

DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. SUMMARY OF NRC 00618: IN REFERENCE TO NRC 00501 DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. WERE REPAIRED PERMANENTLY PER B717-200 SRM 51-70-02-0G AND 57-53-01-2R-1. (LP #0652245)

Part: VANE — DENTED (ZONE 600 FLAP) · airframe 56,170 hrs · 39,942 cycles

DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE. DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING. SUMMARY OF NRC 00620: ON REF NRC 00503 DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING WAS REPAIRED PERMANENTLY PER B717-200 SRM 51-70-02-0G AND 57-53- 01-2R-1. (LP #0652243)

Part: SKIN — GOUGED (ZONE 100) · airframe 56,170 hrs · 39,942 cycles

GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A. FIG 202. PERFORM A VISUAL INSPECTION EVERY 8,000 CYCLES PER B717 SRM 53-03-01-2R-PROCEDURE 1 REPAIR 1 STEP 7 TABLE 201. (LP #0649505)

Part: HINGE — WORN (F/A SEAT) · airframe 56,170 hrs · 39,942 cycles

WEAR ON DOBLER AND FLIGHT ATTENDANT SEAT HINGES OF AFT CABIN BULKHEAD VENTRAL DOOR. AND WEAR ON UPPER / LWR SIDE FITTING (7 EA) 0F AFT CABIN BULKHEAD VENTRAL DOOR. SUMMARY OF NRC-00452: UPPER / LWR SIDE FITTINGS (7 EA) AND FLIGHT ATTENDANT SEAT HINGES WERE BLENDED OUT PER B717-200 SRM 51-10-02-0G. DOUBLER AT AFT CABIN BULKHEAD VENTRAL DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 16, OPTION 1. (LP #0643368)

Part: SKIN — GOUGED (ZONE 100) · airframe 56,170 hrs · 39,942 cycles

GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A, FIG 202. (LP #0642594)

Part: FRAME — CRACKED (ZONE 100) · airframe 56,170 hrs · 39,942 cycles

CRACK ON MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00433: MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0639803)

Part: WEB — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACK ON WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00380: WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. FIGURE 217. -PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30- 10-70 PAGE 14 PAR I. LOG PAGE DEFERRED TO DECAL CONDITION MONITOR PER TOPP 30-10-70 TO BE INSPECTED AT THE APPROPRIATE CHECK INTERVAL. (LP #0637205)

Part: LONGERON — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACK ON LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00434: LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0637160)

Part: PAN — CRACKED (ZONE 100) · airframe 56,170 hrs · 39,942 cycles

CRACK WAS FOUND ON INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00486: INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0636755)

Part: SKIN — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACK ON SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER). SUMMARY OF NRC 00355: SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER) WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIGURE 201. (LP #0636659)

Part: BEAM — CRACKED (ZONE 800) · airframe 56,170 hrs · 39,942 cycles

CRACK ON BEAM #1 AFT SECTION AT FWD PASSENGER DOOR. SUMMARY OF NRC 00266: BEAM #1 AFT SECTION AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0634844)

Part: WEB — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACKED WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00432: WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 204. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK PER B717-200 SRM 51-00-55-2R PROCEDURE 4, STEP 6 A, TABLE 201. SUMMARY OF NRC 00432: WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 204 PERFORM A GENERAL VISUAL INSPECTION EVERY C CHECK PER B717-200 SRM 53-00-55-2R PROCEDURE 4 STEP 6. A. TABLE 201. (LP #0635107)

Part: WEB — CRACKED (ZONE 200) · airframe 56,170 hrs · 39,942 cycles

CRACK ON WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00378: WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4, REPAIR 4, FIGURE 217. (LP #0627536)

Part: INTERCOSTAL — CRACKED (BS 1224) · airframe 54,828 hrs · 38,796 cycles

CRACK ON INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00078: INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESSORY COMPARMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. SPRING ON RUDDER STOP ASSEMBLY WAS INSTALLED PER B717 AMM 27-26-03 400-801 STEP E (1) (C). (LP #0235490)

Part: FRAME — CRACKED (BS 116 L15-16L) · airframe 54,813 hrs · 38,782 cycles

CRACK ON CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00084: CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 SRM 51- 41-05-0G. (LP #0230453)

Part: FRAME — CRACKED (BS 1116 L15-16R) · airframe 54,813 hrs · 38,782 cycles

CRACK ON CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00087: CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #0230455)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,404 hrs · 38,451 cycles

RAMP REPORTS DENT ON LOWER LEFT CORNER OF L1 DOOR OUTER SKIN. INSPECTED IAW B717 SRM 53-01-01-1A PROC 3, DENT MEASURES 2 X 0.125 X 0.342. DENT IS OUT OF LIMITS IAW SRM. PERFORMED PRESSUIZATION OF A/C PER B717 AMM 21-30, FOUND LEAK OUT OF DAMAGE LOCATION. INSPECTED DOOR MOUNTS PER B717 AMM 52-11, NO DEFECTS NOTED. DOOR OPENS AND CLOSES NORMALLY. ACCOMPLISED SECTION 1: FERRY FLIGHT PREPERATION IAW ER/A 614248 -14 REV ORIGINAL. C/W PERMANENET REPAIR PER ERA 614248-14 REV ORIG SEC II. REPAIRED DOOR SEAL PER SRM 52-00-17-2R. PERFORMED LEAK CHK, OPS NORMAL. (LP #4378564)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,756 hrs · 37,945 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT JUST AFT OF GALLEY. MAINTENANCE INSTALLED THE EMERGENCY EXIT SIGN COVER BETWEEN ROW 1 SEATS REF B717 AIPC 33-51-18-05. LIGHTS CHECK GOOD. (LP #2952421)

Part: NONE — NONE · airframe 52,435 hrs · 36,816 cycles

PDA. LH WING SKIN ASSY STA XFS 70.812-196.236 MISSING. FWD TO MON PER ER/A 604219-14 REV ORIGINAL. C/W SECTION 1. PERMANENT REPAIR TO BE ACCOMPLISHED IN 90 DAYS. C/W PERMANENT REPAIR ON ERA 604219-14 REV. ORIGINAL. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 17FEB23 AND LOG COMMENTS. (LP #9603288)

Part: NONE — NONE · airframe 50,209 hrs · 34,836 cycles

LH VERTICAL STAB LE, CRACK INDICATION IN 4TH HOLE UP FROM SLICE AT STA ZFS 52.267. FOUND DURING OPEN HOLE INSPECTION REF AMDS 5530-01048-02-ET STEP 8 AND AD 2018-10-08. -M-. SUMMARY SEE NRC 069-0001:5530-01048-02/002 00420: REPAIRED PER PRI 597048-14 REV 0 THRU REV 3 AND FINAL ERA 597048-14AD REV ORIGINAL. ASSOCIATED ER/A 00-597048 ADDED FOR AC 9539. (LP #2118706)

Part: NONE — NONE · airframe 50,209 hrs · 34,836 cycles

TAILCONE R/H SIDE LATCH LEVER REQUIRES RIG ADJUSTMENT TO TOP OF SLOT PER B717 AMM 53-52-01 830-802 STEP E.1.AG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/002 00461: CHECKED ADJUSTMENT AND RIGGED REF B717 AMM 53-52-01 830-802 STEP E.1.AG. (LP #2115935)

Part: NONE — NONE · airframe 50,209 hrs · 34,836 cycles

TAILCONE EMERGENCY RELEASE; LEFT LOWER LATCH LEVER CABLE IS FRAYED AT UPPER PULLY AREA. -M- SUMMARY SEE NRC 001-0317:5353-2001/001 00453: REPLACED, RIGGED, AND SAFETIED CABLE REF B717 AMM 53-52-01. OPERATIONALS CHECK WAS GOOD. (LP #2115930)

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,727 hrs · 32,831 cycles

AFT CARGO LOWER DOOR JAMB CORRODED (MARKED). NRC 001-0302:5231-2002/001 00013: REPAIRED REF SRM 53-20-15-2R PROC 7. (LP #1266353)

Part: TRANSCEIVER — MALFUNCTIONED (WINDSHEAR DETECT) · airframe 45,670 hrs · 31,380 cycles

SHIP 9539 - ATO - AT 105 KNOTS DUE TO PREDICTIVE WINDSHEAR WARNING AT 95-100KNOTS. SUSPECT A FALSE WARNING AS OTHER DEPARTURES AND ARRIVALS REPORTED GOOD FLIGHT CONDITIONS WITHOUT WINDSHEAR. CORRECTIVE ACTION: TROUBLESHOT PER FIM. REPLACED WEATHER RADAR TRANSCEIVER PER AMM. (LP0841059)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,623 hrs · 31,349 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND THE AFT LEFT LOWER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE AFT LEFT LOWER EMERGENCY EXIT SIGN PER B717 AMM 33-55. (LP #5088722)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN. CORROSION LEVEL 2. RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN WAS REPAIRED (PERMANENT REPAIR) PER ER/A 562367-14 REV ORIGINAL AND ETI-17-17-214 REV 3.

Part: LONGERON — CRACKED (BS 1022) · airframe 42,980 hrs · 29,505 cycles

CRACKED LONGERON 16L, BS 1022. THE LONGERON WAS REPAIRED IAW ER/A 562376-14, REV ORIGINAL, AND ETI-17-17-223, REV 3.

Part: PAN — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORRODED PAN OF THE CARGO DOOR FRAME. REPAIR SPLICES WERE FABRICATED AND INSTALLED AND THE PAN WAS REPAIRED IAW SRM 53-20-15-2R-7.

Part: FRAME ANGLE — CRACKED (BS 927) · airframe 42,980 hrs · 29,505 cycles

CRACKED FRAME ANGLE AT BS 927 BETWEEN STRINGERS 29L TO 30L IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-0I-3, DWG 5919707, REV BU, S124681 REV L. SRM 51-41-02-0G, AND 51-41-05-0G.

Part: STRUCTURE — DAMAGED (DOOR FRAME) · airframe 42,980 hrs · 29,505 cycles

ELONGATED FWD & AFT HINGE HOLES AT FWD CARGO DOOR. THE HINGES WERE REMOVED IAW AMM 52-31-02. THE HOLES WERE REWORKED, BUSHINGS WERE INSTALLED, AND WASHERS WERE REPLACED IAW ERA 559577-14MA, REV ORIGINAL.

Part: FITTING — CRACKED (BS 662 BULKHEAD) · airframe 42,980 hrs · 29,505 cycles

CRACK IN FITTING ON THE AFT BULKHEAD FWD FACE BS 662, LONGERON 24R. THE FITTING WAS REPLACED IAW SRM 51-40-08-0G, 51-41-02-0G, AND 51-41-05-0G.

Part: DOOR FRAME — CORRODED (BS 201) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON DOOR FRAME WEB AND STRAP BS 201, LBL 57. THE DOOR FRAME WEB WAS REPAIRED IAW ER/A 562371-14, REV ORIGINAL, ETI-17-17-219, REV 4 AND THE STRAP WAS REPLACED IAW SRM 51-41-05-0G.

Part: SKIN — CRACKED (BS 1022) · airframe 42,980 hrs · 29,505 cycles

CRACKED SKIN BS 1022, LONGERON 14L. PERMANENT REPAIR WAS ACCOMPLISHED IAW ETI-17-17-209 REV. 2 AND ER/A 521459-14 REV. A.

Part: SKIN — CRACKED (BS 1022) · airframe 42,980 hrs · 29,505 cycles

CRACK ON FUSELAGE SKIN AT BS 1022 AND LONGERON 14R. REPAIRED IAW ETI-17-17-210, REV 3, AND ER/A 562364-14, REV ORG.

Part: HOUSING — WORN (L1 DOOR) · airframe 42,980 hrs · 29,505 cycles

WEAR ON HOUSING OF THE HOOK AT THE L1 DOOR. A NEW HOUSING WAS FABRICATED IAW DWG 4955948, REV D, AND REPLACED IAW SRM 51-41-02.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 42,980 hrs · 29,505 cycles

CRACK ON INTERCOSTAL BS 617 TO 636, BL 0, Z=0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 51-40-08-0G.

Part: SKIN — CORRODED (BS 655-696) · airframe 42,980 hrs · 29,505 cycles

SEVERAL CORROSION POINTS ON THE SKIN BETWEEN BS 655 AND 696, LBL 44 AND LBL 60. REPAIRED IAW ER/A 562374-14 REV. ORIGINAL, AND ETI-17-17-210 REV 1.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 42,980 hrs · 29,505 cycles

CRACKED SHEAR TIE BS 1022 BETWEEN LONGERONS 12L TO 17L. THE SHEAR TIE WAS REPLACED IAW SRM 51-20-09-0G, 54-41-05-0G, AND DWG 9912243, REV J.

Part: BEAM — CRACKED (BS 46) · airframe 42,980 hrs · 29,505 cycles

CRACKED LEFT BEAM AT NLG DOOR FRAME BS 46. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R-2, FIG 201, SHEET 1.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 42,980 hrs · 29,505 cycles

CRACKED RT CUSP WEB BETWEEN BS 218 TO 237. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: WEB — CRACKED (NLG DOOR FRAME) · airframe 42,980 hrs · 29,505 cycles

CRACKED WEB AT NLG DOOR FRAME STATION 46, REPAIRED IAW SRM 53-10-14-2R-2, FIG 201, SHEET 1.

Part: FORMER — CRACKED (BS 694) · airframe 42,980 hrs · 29,505 cycles

CRACKED FORMER BS 694. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1, 51-41-02-0G, AND 51-41-05-0G.

Part: PAN — CRACKED (CARGO DOOR) · airframe 42,980 hrs · 29,505 cycles

CRACK ON INNER PAN AT FWD CARGO DOOR AFT EDGE BS BS 427 BETWEEN BEAMS NR 5 AND 4. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-1, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON FLOOR SUPPORT RBL 45, BS 160 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.

Part: SKIN — CRACKED · airframe 42,980 hrs · 29,505 cycles

CRACK ON THE FUSELAGE SKIN AROUND AFT THE HINGE OF THE NLG DOOR. THE SKIN WAS REPAIRED IAW SRM 53-10-01-2R-11, 51-41-02-0G, AND 51-41-05-0G.

Part: STOP FITTING — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON THE AFT CARGO DOOR STOP FITTING NR 3. THE STOP FITTING WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON FLOOR SUPPORT LBL 7 BETWEEN BS 148 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-01-0G, 51-41-08-0G, AND 51-10-04-0G, PAR 21, 15, 37.

Part: SHEAR TIE — CRACKED (BS 1087) · airframe 42,980 hrs · 29,505 cycles

CRACK ON SHEAR TIE BS 1087 BETWEEN LONGERONS 13 & 14R. THE SHEAR TIE WAS REPLACED IAW SRM 51-20-09-0G, 51-41-05-0G, AND DWG 9971140, REV F.

Part: FLOOR SUPPORT — CORRODED (BS 197-200) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON FLOOR SUPPORT BS 197 TO 200 LBL 57. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-20-09-0G, 51-41-05-0G, AND 51-41-02-0G.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

EXCESSIVE CORROSION ON DIAPHRAGM AT STA Y=200 BTW X=7 AND X=8 IN REF NRC 00328. LEVEL CORROSION 2. REPAIR WAS ACCOMPLISHED PER SRM 53-00-00-2R.

Part: WEB — CORRODED (BS 200) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON WEB AT BS 200 BETWEEN RBL 7 AND RBL 13. REPAIRED IAW SRM 51-70-10-2R.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,980 hrs · 29,505 cycles

CRACKED CUSP HOLES ON STA Y=661, Y=645 BTW X=-55 TO X=-60, AND Y=631 BTW X=-45 TO X=-55 (CPAX). PERMANENT REPAIRS WERE ACCOMPLISHED AT STA Y=661 BTW X=-55 TO X=-60 PER SRM 53-00-55-2R-4 FIG 206, AND THE OTHER TWO STA Y=645 AND Y=631 DAMAGE WAS REMOVED PER SRM 53-00-00-1A FIG 101 SHEET 1, AND WAS MEASURED.

Part: INTERCOSTAL — WORN (FUSELAGE) · airframe 42,980 hrs · 29,505 cycles

WORN INTERCOSTAL AT AFT CARGO DOOR BTW STA Y=970 AND Y=974 BTW LOWER EDGE AND BEAM 1. INTERCOSTALS WERE REPLACED PER DWG 9957666 REV U, SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 42,980 hrs · 29,505 cycles

CRACKED LONG 17 LT STA Y=1022 AT CABIN PAX (CPAX). LONGERON WAS REPAIRED PER SRM 53-00-05-2R FIG 201. IT IS AS PERMANENT REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION OUT OF LIMITS ON FLOOR SUPPORT LT SIDE BTW STA Y=1022 TO Y=1060 X=45. LEVEL CORROSION 2. FLOOR SUPPORT WAS REPLACED PER SRM 51-41-01-0G.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 42,980 hrs · 29,505 cycles

CRACKED LONGERON 8L ON STA Y=1022 AT AFT LAVATORY INTERNAL STRUCTURE AREA. LONGERON 8L ON STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATES 620CT AND 520CT. CORROSION LEVEL 2. FUEL ACCESS PLATES 520CT AND 620CT (P/N 3912757-503) WERE REPLACED BY NEW PER SRM 57-10-01 AND IPC 57-22-01 ITEM 065.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF (2EA) FUEL ACCESS PLATES ARB0872-535. CORROSION LEVEL 2. FUEL ACCESS PLATES (2EA) P/N ARB0872-535 WERE REPLACED BY NEW PER SRM 57-10-01 AND IPC 57-22-01 ITEM 020.

Part: PAN — CRACKED (FUSELAGE) · airframe 42,980 hrs · 29,505 cycles

CRACKS ON RT FWD UPPER CORNER OF RING PAN FROM STA Y=636 AND RT LOWER AFTER CORNER RING PAN FROM STA Y=908 IN REF AMDS 5331-2003 (CPAX). ON RT FWD UPPER CORNER OF RING PAN FROM STA Y=636 AND RT LOWER AFTER CORNER RING PAN FROM STA Y=908 NO CRACKS WERE FOUND AFTER TRIM OUT DAMAGE, EQUIPMENT. RT FWD UPPER CORNER OF RING PAN FROM STA Y=636 AND RT LOWER AFTER CORNER RING PAN FROM STA Y=908 WERE REPAIRED PER SRM 56-20-02-2R-1.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATES 620CT AND 520CT. CORROSION LEVEL 2. FUEL ACCESS PLATES 520CT AND 620CT (P/N 3912757-503) WERE REPLACED BY NEW PER SRM 57-10-01 AND IPC 57-22-01 ITEM 065.

Part: RETAINER — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 42,980 hrs · 29,505 cycles

CORROSION ON PRESSURE SEAL RETAINER AT THE R1 SERVICE DOOR. THE SEAL RETAINER WAS REPLACED IAW SRM 51-41-01-0G.

Part: DOUBLER — CRACKED (BS 1074) · airframe 42,282 hrs · 29,039 cycles

THRUST REVERSER HCU ACCESS DOOR INTERNAL DOUBLER CRACKED, BS 1074 LONGERON 22R, . NO WORK ACCOMPLISHED ON THIS NON-ROUTINE CARD. THIS NON-ROUTINE WRITTEN FOR SDR TRACKING ONLY. T/R HCU ACCESS DOOR CUT OUT INTERNAL DOUBLER STA 1074 LONGERON 22RT REPAIRED ON NR-00001 (CRACK DIM 2.0"). (LP #0118289)

Part: ACCESS DOOR — DAMAGED · airframe 42,282 hrs · 29,039 cycles

RT SIDE OF ACFT DAMAGED AROUND RIGHT THRUST REVERSER HCU ACCESS DOOR. REPAIRED THE DOOR IAW ER/A 556431-14, REV. ORIGINAL.

Part: LONGERON — CRACKED (BS 1074) · airframe 42,282 hrs · 29,039 cycles

LONGERON 22R AT BS 1074 IS CRACKED, REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 2.

Part: FORMER — CRACKED (BS 1074) · airframe 42,282 hrs · 29,039 cycles

FRAME BS 1074 RT FORMER CRACKED BETWEEN LONGERONS 21R TO 22R. REMOVED, FABRICATED, AND INSTALLED A NEW FORMER IAW SRM 51-40-08 AND DRW #9958239 REV AB, PART HEAT TREAT FROM "0" CONDITION TO T6" IAW AMS 27-70. (LP #0117308)

Part: FRAME — DENTED (BS 1076) · airframe 42,282 hrs · 29,039 cycles

BS 1076 FRAME AT LONGERON 22R IS DENTED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME BETWEEN LONGERONS 25R TO LONGERON 19R, USING 7075 "0." 050 DIM 44"X4" IAW B717 SRM 51-40-08 AND DRW #9958239 REV AB. PART HEAT TREATED FROM "0" CONDITION TO "T6" IAW AMS 27-70. (LP #0117314)

Part: FRAME — CRACKED (BS 1074) · airframe 42,282 hrs · 29,039 cycles

FRAME BS 1074 CRACKED BETWEEN LONGERONS 21R AND 22R. . REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-40-08, AND DWG 9958239, REV AB,

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 39,024 hrs · 26,569 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS LAVATORY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 38,292 hrs · 25,970 cycles

VERTICAL STABILIZER L/E, SKIN CRACKED AT BS 1152, BETWEEN LONGERON 1 AND 2L. REPAIRED IAW ER/A 541498-14, SECTION 1.

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 38,292 hrs · 25,970 cycles

AFT CARGO DOOR CUTOUT AFT SIDE MID DOOR AREA HAS DEFORMED METAL WITH SUSPECTED CRACK. REPAIRED IAW ER/A 541497-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,292 hrs · 25,970 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 1 TO ROW 14. REPLACED BATTERY PACK AT BS 398.

Part: SKIN — DENTED (BS 218) · airframe 35,902 hrs · 24,038 cycles

DURING INSPECTION, NOTED A DENT AFT OF L1 DOOR BS 218 STRINGER 18L. REPAIRED IAW SRM 53-10-01, FIGURE 202.

Part: LANYARD — DETACHED (TAIL SLIDE CABLE) · airframe 33,967 hrs · 22,301 cycles

DURING 121 COMPLIANCE INSPECTION, NOTED THE TAIL INTERIOR SLIDE CABLE STRAP WAS DETACHED. ATTACHED TAIL INTERIOR TAILSLIDE RELEASE LANYARD IAW AMM 53-52-01-430-008.

Part: CONTROL BOX — DENTED (TAILCONE RELEASE) · airframe 33,967 hrs · 22,301 cycles

DURING 121 COMPLIANCE INSPECTION, NOTED THE TAIL INTERIOR LT CONTROL BOX WAS DENTED. REPLACED TAILCONE LOCK CABLE IAW AMM 53-52-01-420-001 AND 53-52-01-430-001.

Part: LIGHT — LOOSE (CABIN) · airframe 33,958 hrs · 22,292 cycles

RT FWD EEPLS LOOSE. SECURED EEPLS IAW MM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

SEAT TRACK SPLICE CORRODED AT STATION 889, RBL 44. R & R SPLICE IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FLOOR PANEL 222SF CORRODED BETWEEN STATION 565 TO STATION 589 INBD SIDE FLOOR. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FLOOR PANEL 222SF CORRODED BETWEEN STATION 593 TO STATION 612 INBD SIDE. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FLOOR PANEL 222SF CORRODED BETWEEN STATION 541 TO STATION 560 INBD SIDE. REPAIRED PANEL IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 33,911 hrs · 22,257 cycles

TAIL CONE EMERGENCY EXIT SIGN AT RELEASE BOX CRACKED. R & R SIGN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FWD CARGO FLOOR SUPPORT CRACKED AT BS 370, BETWEEN 530 & 529R. R & R SUPPORT IAW SRM & DRAWING.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

CUSP WEB CRACKED BETWEEN STATION 650 TO STATION 655, RBL 54. REPAIRED CUSP WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

RT WW FWD VERTICAL DOOR CUT OUT CRACKED. REPAIRED DOUBLER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FLOOR PANEL SUPPORT CORRODED AT STATION 1034, RBL 18. R & R SUPPORT IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

LT SIDE WALL CENTER STRAP CRACKED AT STATION 237. REPAIRED STRAP IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

AFT CARGO COMP FWD PRESSURE BULKHEAD INNER SUPPORT CRACKED AT STATION 817- 2. R & R SUPPORTS IAW DRAWING.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

CUSP WEB CRACKED AT BS 655, RBL 54. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

RT CUSP WEB CORRODED BETWEEN BS 503 TO BS 522. R & R CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

VERTICAL FLOOR SUPPORT CRACKED AT BS 737, LBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

VERTICAL STIFFENER CRACKED AT BS 660, RBL 20. R & R STIFFER IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

VERTICAL FLOOR SUPPORT CRACKED AT BS 737, RBL 44. R & R SUPPORT IAW DRAWING.

Part: PANEL — CORRODED (RT WING) · airframe 33,911 hrs · 22,257 cycles

RT WING UPPER SIDE FUEL TANK CUTOUT PANEL 620AT RING CORRODED. R & R PANEL IAW SRM.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB) · airframe 33,911 hrs · 22,257 cycles

LT ELEVATOR GEAR TAB CENTER HINGE CUTOUT SKIN DELAMINATED. REPAIRED TAB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STATION 899 TO STATION 1022, RBL 44. R & R SEAT TRACK IAW SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

AFT ACCESSORY COMPARTMENT AT STATION 1087 RT SIDE AC SUPPLY DUCT ROD SUPPORT BRACKET CORRODED. R & R BRACKET IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

SEAT TRACK CORRODED BETWEEN STATION 256 TO STATION 589, RBL 22. R & R SEAT TRACK IAW DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

AFT ACCESSORY COMPARTMENT LT LOUVER UPPER WEB CRACKED AT AFT END. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB) · airframe 33,911 hrs · 22,257 cycles

LT ELEVATOR GEAR TAB OTBD HINGE CUTOUT SKIN DELAMINATED. REPAIRED TAB IAW SRM.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB) · airframe 33,911 hrs · 22,257 cycles

LT ELEVATOR GEAR TAB INBD HINGE CUTOUT DELAMINATED ON SKIN. REPAIRED TAB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

SEAT TRACK CORRODED BETWEEN STATION 589 TO STATION 646, LBL 44. R & R SEAT TRACK IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

SEAT TRACK CORRODED BETWEEN STATION 823 TO STATION 899, LBL 22. R & R SEAT TRACK IAW SRM & DRAWING.

Part: SKIN — CRACKED (RT ELEVATOR TAB) · airframe 33,911 hrs · 22,257 cycles

RT ELEVATOR GEAR TAB OTBD HINGE CUTOUT 1" SKIN CRACKED. REPAIRED TAB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STATION 256 TO STATION 589, RBL 54. R & R SEAT TRACK IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

AFT ACCESSORY COMPARTMENT RT LOUVER UPPER AFT END REPAIRED DOUBLER CRACKED AT WEB. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

SEAT TRACK CORRODED BETWEEN STATION 899 TO STATION 1022, LBL 22. R & R SEAT TRACK IAW DRAWING.

Part: STRAP — CRACKED (RT WING) · airframe 33,911 hrs · 22,257 cycles

RT WING LE MOST INBD AREA FAIRING PANEL INNER SIDE ATTACH STRAP LOWER AREA CRACKED. R & R STRAP IAW DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

RT SIDE MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT STATION 661, LONGERON 22R. R & R ANGLE IAW DRAWING & SRM.

Part: PANEL — CRACKED (RT WING) · airframe 33,911 hrs · 22,257 cycles

RT WING AT INBD PANEL FWD OF BUTTE DOOR CRACKED. REPAIRED PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STATION 256 TO STATION 589, LBL 44. R & R SEAT TRACK IAW SRM & DRAWING.

Part: PANEL — CRACKED (LT MLG WW) · airframe 33,911 hrs · 22,257 cycles

LT MLG WW AFT BULKHEAD SHIELD PANEL CRACKED. REPAIRED DOUBLER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

CLIP CRACKED AT BS 1152, LONGERON 2R. R & R CLIP IAW DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

LT UNDER WING BARREL KEEL BEAM FORMER CRACKED AT BS 715 OTBD END. R & R FORMER IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 33,911 hrs · 22,257 cycles

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

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 674, UNDER WING BARREL KEEL BEAM LT SIDE. R & R FORMER IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,911 hrs · 22,257 cycles

L1 DOOR AFT OF INTERIOR DOOR HANDLE CRACKED. R & R INTERCOSTAL IAW DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 1144, LONGERON 2L. R & R FORMER IAW DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 1022, BETWEEN LONGERON 13R TO LONGERON 14R. R & R FORMER IAW SRM & DRAWING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2L. REPAIRED LONGERON IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

CLIP CRACKED AT BS 1152, LONGERON 2L. R & R CLIP IAW DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 674, UNDER WING BARREL KEEL BEAM RT SIDE. R & R FORMER IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FUSELAGE SKIN CRACKED AT BS 1022, BETWEEN LONGERON 13L TO LONGERON 14L. REPAIRED SKIN IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 696, UNDER WING BARREL KEEL BEAM LT SIDE. R & R FORMER IAW DRAWING.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 33,911 hrs · 22,257 cycles

LT WING FUEL TANK ACCESS PANEL 520HB LANDING RING CORRODED. R & R PANEL IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

RT UNDER WING BARREL KEEL BEAM FORMER CRACKED AT BS 715 AT OTBD END. R & R FORMER IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

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

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 696, UNDER WING BARREL KEEL BEAM RT SIDE. R & R FORMER IAW DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FORMER CRACKED AT BS 1022, BETWEEN LONGERON 13L TO LONGERON 14L. REPAIRED FORMER IAW EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,911 hrs · 22,257 cycles

FWD CARGO DOOR, DOOR JAMB CORRODED BETWEEN BS 370 TO BS 380. REPAIRED JAMB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,966 hrs · 22,299 cycles

AFT ACCESSARY COMPARTMENT FORMER SHEAR CLIP CRACKED AT BS 1144 LONGERON 2L. R & R SHEAR CLIP IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 32,986 hrs · 21,666 cycles

RIGHT EEPLS BROKEN AT ROW 20. REMOVED AND REPLACED EEPLS PER AMM.

Part: ISOLATION VALVE — FAULTY (TAIL) · airframe 32,614 hrs · 21,440 cycles

DECLARED EMERGENCY - LEFT HYDRAULIC QNTY LOW ALERT. REMOVED AND REPLACED MANIFOLD ISOLATION VALVE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,570 hrs · 21,414 cycles

EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 31,574 hrs · 20,791 cycles

R-1 SLIDE INFLATION BOTTLE GAS PRESSURE LOW. REMOVED AND REPLACED R-1 DOOR SLIDE PER AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 31,493 hrs · 20,739 cycles

FORWARD SERVICE DOOR GIRT BAR CAUGHT IN DOOR. SECURED GIRT BAR PER MM.

Part: UNKNOWN — ODOR (CABIN & COCKPIT)

DETECTED CHLORINE ODOR IN CABIN & COCKPIT CREW MEMBERS EYES SENSED BURNING (A LITTLE) FA USED OXY MASK. PER DEFECT 1922990 ITM 1, INSP PERFORMED & SIGNED OFF ON 1922990-2 AND POB SERVICED ON 1922990-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 218, LONG 18R, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-70-52.

Part: SEAT TRACK — CORRODED (A DEAF WOMAN WHO)

MAIN CABIN SEAT TRACK, STA 218 TO 256, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR, STA 200 TO 203, RBL 41 TO RBL 48, CORROSION. ACCOMPLISHED FLOOR DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 13 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO TIE SHEAR, STA FS908, LONG 29L TO 30 CORROSION. ACCOMPLISHED TIE SHEAR DOUBLER REPAIR PER B717 SRM 53-00-06 FIG 20.

Part: PAN — CORRODED (FUSELAGE)

MAIN CABIN FLOOR PAN, STA 200, RBL 41 TO RBL 53, CORROSION. ACCOMPLISHED FLOOR PAN DOUBLER REPAIR PER B717 SRM 51-41-02 AND 51-70-10 REP 2, FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 141, RBL 31 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 258, LBL15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

FWD CABIN L1 DOOR CUTOUT - AFT JAMB INNER SKIN, STA 200, LONG S15L, CRACKED. ACCOMPLISHED L1 DOOR CUTOUT - AFT JAMB INNER SKIN DOUBLER & FILLER REPAIR PER B717 SRM 51-70-10 .

Part: FITTING — CORRODED (GIRT BAR)

FWD & AFT MAIN CABIN GALLEY DOOR GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 180, RBL 10 TO RBL 41, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, LBL 13 TO RBL 13, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 150 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 150 TO 200, RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 194, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 53-00-00, 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 218 TO 256, RBL 44, CORROSION. OPEN DEFECT

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG)

AFTER GEAR RETRACTION STILL HAD A LEFT GEAR UNSAFE LIGHT INDICATION. ADJUSTED LEFT MLG UP LATCH PROX SENSOR REF AMM 32-61-00 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

BULBS, COCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT, REF 33-00 MM.

Part: LIGHT — INOPERATIVE (COCKPIT)

FLT DECK EMERGENCY LIGHT ON OVERHEAD PANEL HAS ONE BULB BURNT OUT. RELAMPED BULB, OPS CHECK GOOD IAW AMM 33-51-11.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: ATTACH ANGLE — CRACKED (RT PYLON)

PYLON LOWER ATTACHMENT ANGLE AT RIGHT SIDE STA 1178.225 IS CRACKED. CUT OUT DAMAGED SECTION 2.125 INCHES X 1.0 INCH AND INSTALLED ANGLE REPAIR, REF EA 17-53-02186IR AND B717 SRM 51-70-11 FIG 201.

Part: SKIN — DENTED (FUSELAGE)

DENT BEHIND L-1 DOOR LOWER CORNER APPROX 18 INCHES AFT OF DOOR MEASURES 5 INCHES WIDE BY 8 INCHES LONG. MAX DEPTH DEPRESSION FWD OF FRAME IS .050 INCH AND AFT IS .085 INCH. CUT OUT DAMAGED SKIN AND INSTALLED SKIN DOUBLER REPAIR PER B717 SRM 53-00-01 REPAIR 6 FIG 201. REF NR 3765, 3822 AND 3828.

Part: SKIN — DENTED (FUSELAGE)

DENT BEHIND L-1 DOOR LOWER CORNER APPROX. 18 INCHES AFT OF DOOR MEASURES 5 INCHES WIDE BY 8 INCHES LONG. MAX DEPTH DEPRESSION FWD OF FRAME IS .050 INCH AND AFT IS .085 INCH. CUT OUT DAMAGED SKIN AND INSTALLED SKIN DOUBLER REPAIR PER SRM 53-00-01 REPAIR 6 FIG 201. REF NR 3765, 3822 AND 3828.

Part: THRESHOLD — CORRODED (FUSELAGE)

AFT CARGO DOOR THRESHOLD HAS CORROSION ALONG LOWER SECTION BEYOND LIMITS. REPAIRED LOWER SECTION AT AFT CARGO DOOR CUTOUT PAN AS PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: FRAME — CRACKED (FUSELAGE)

LEFT HAND CANTED FRAME IS CRACKED AT STA 1178, BETWEEN STR 16 AND 17. INSTALLED DOUBLER ANGLE REPAIR AT LEFT CANTED FRAME AT STA 1178 BETWEEN STR 16 TO STR 17 IAW SRM 51-70-11 FIG 201. MATERIAL USED 0.080 7075-0 12" X 1" X 1.25", HEAT TREATMENT TO T6 IAW B717 SRM 52-32-01.

Part: SUPPORT ANGLE — CRACKED (LT VENT BOX)

VENT BOX, LEFT UPPER SUPPORT ANGLE IS CRACKED. INSTALLED NEW UPPER SUPPORT ANGLE AT LEFT VENT BOX IAW B717 SRM 51-41-02. MATERIAL USED 2024-0.040 2" X 12". HEAT TREATED ANGLE TO 2024-T4 PER AVBORNE G-PS 98PMS.247PS-01.

Part: SUPPORT ANGLE — CRACKED (RT VENT BOX)

VENT BOX, RIGHT UPPER SUPPORT ANGLE IS CRACKED. INSTALLED NEW UPPER SUPPORT ANGLE AT LEFT VENT BOX IAW B717 SRM 51-41-02. MATERIAL USED 2024T3 .050 3" X 2.5".

Part: DOOR — BENT (L1 DOOR)

BEND FOUND IN BOTTOM EDGE OF MAIN CABIN DOOR PER RES 05-1513 HFEC AT EVERY C-CHECK. INSTALLED DOUBLER REPAIR AT BOTTOM EDGE OF MAIN CABIN DOOR IAW SRM 52-10-01 PAGE 202 FIG 201. MATERIAL USED 7075.T6.050 35 X 8 INCHES.

Part: RELAY — MALFUNCTIONED (PAX OXYGEN SYS)

PAX O2 ALT REL C/B NR L33 POPPED AFTER 1 RESET. REMOVED AND REPLACED RELAY R2-5152 AND C/B B1-870. PERFORMED O2 MASK DROP CHECK PER M/M 35-23, OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE)

A/C HAS DENT LOCATED AFT OF L-1 DOOR AT APPROX STA 235, 8 INCHES ABOVE CUSP LINE .5 L X .75 W X .018 DEEP. INSTALLED DOUBLER REPAIR AT AFT OF L-1 DOOR STA 235 AS PER B717 SRM 53-00-01. MATERIAL USED 2024 T3.032, 6.25 X 5.75 INCHES.

Part: OXYGEN MASK — DEPLOYED (CABIN)

IMMEDIATELY AFTER TAKEOFF ALL PASSENGER'S OXYGEN MASKS DEPLOYED. REPACKED PASSENGER'S OXYGEN MASKS AM 35-23 AND PERFORMED FUNCTIONAL TEST OF PASSENGER MASK RELEASE SYSTEM, OPS NORMAL AMM 35-22 AND FIM 35-20 TASK 804.