N982AT

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 59,445 hrs · 42,191 cycles

AFT BULKHEAD DOOR CAUTION MESSAGE ON TAXI OUT FOR TAKEOFF. T/S PER FIM 52-70-00-810-809 CHECK PSEU SENSOR. CLEAN AND ADJUST PROX SENSOR PER B717 AMM 52-70 (7521980)

Part: PROXIMITY SENSOR — FAULTED (ZONE 100) · airframe 58,895 hrs · 41,715 cycles

ABORTED TAKEOFF APPROX. 35KTS DUE TO AFT CABIN BULKHEAD DOOR INDICATION. REPLACED BULKHEAD DOOR PROX SENSOR. OK FOR SERVICE.(1140292)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,645 hrs · 41,489 cycles

AIRCRAFT 9549, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. CORRECTIVE ACTION: REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER B717 AMM 33-51. OPS CHECK GOOD. (LP 7315329)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,691 hrs · 38,963 cycles

DURING CHECK OF THE EXTERIOR LIGHTS, LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258403)

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,691 hrs · 38,963 cycles

CRACKS ON SKIN WERE FOUND AFTER REMOVAL STOP FITTING ON AFT EDGE BEAM 2 APROX. SUMMARY OF NRC 00531: SKIN ON AFT EDGE BEAM 2 APROX WAS REPAIRED PER PRI 615938-14 REV 1 AND ERA 615938-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615938 ADDED FOR AC 9549. (LP #0257132)

Part: SKIN — CRACKED (BS 1154 L3L-R) · airframe 55,691 hrs · 38,963 cycles

CRACKS ON FUSELAGE SKIN (2 EA) ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) AT FUSELAGE. SUMMARY OF NRC 00072: FUSELAGE SKIN ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) WAS REPAIRED PER ERA 615858-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPETITIVE INSPECTIONS: ACCOMPLISH SECTION II WITHIN 24 MONTHS AFTER SECTION I WAS PERFORMED AND REPETITIVELY EVERY 24 MONTHS THEREAFTER. LP #0251086. (LP #0255820)

Part: SKIN — WORN (BS 994 L25-26R) · airframe 55,691 hrs · 38,963 cycles

WEAR ON EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R. SUMMARY OF NRC 00018: EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R WAS REPAIRED PER ERA 577681-14 REV B SECTION II: PERMANENT REPAIR AND PRI 577681-14 REV 1 PART C. REPAIR APPROVAL IS LIMITED TO 58,000 TOTAL AIRCRAFT CYCLES. ADDITIONAL ENGINEERING AUTHORIZATION (ERA 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 PAGE #0252688. ASSOCIATED ERA 14-577681.

Part: FITTING — WORN (SPOILER) · airframe 55,691 hrs · 38,963 cycles

WEAR ON TRACK FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 AND OTBD SPOILER XTE 341. SUMMARY OF NRC 00134: FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G AND TRACK FITTING SUPPORT OF SETTLEMENT AREA OTBD SPOILER XTE 341 WAS BLENDED OUT AND (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED WITH ORIGINAL THICKNESS OF 0.085IN AND REMAINING THICKNESS ON AREA REWORKED IS 0.076IN. THEREFORE, AREA REWORKED IT IS WITHIN LIMITS PER B717-200 SRM 57-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 2 B. (LP #0246947)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 55,691 hrs · 38,963 cycles

CORROSION ON FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -X=43, Y= 200 BTW -X=46 TO -X=50 AND Y=200 BTW X=5 TO -X=5 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00681: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -X=43, Y=200 BTW -X=46 TO -X=50 AND Y=200 BTW X=5 TO -X=5 AT PASSENGER CABIN STRUCTURE WERE FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-01-0G, AND 51-41-05-0G. (LP #0240010)

Part: PAN — CRACKED (L1 DOOR AREA) · airframe 55,691 hrs · 38,963 cycles

CRACK ON L1 DOOR PANE FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168. SUMMARY OF NRC 00704: L1 DOOR PAN FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0234210)

Part: FRAME — CRACKED (BS 908 L28L/R) · corrosion level 2 · airframe 55,691 hrs · 38,963 cycles

CORROSION ON FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0230532)

Part: VANE — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 59,370 hrs · 42,128 cycles

CORROSION ON LOWER SKIN OF OUTBD FLAP VANE AT RT WING. OTBD FLAP VANE AT RT WING WAS REPLACED BY ONE SERVICEABLE OTBD FLAP VANE (0228760).

Part: SKIN — DAMAGED (BS 446-465) · airframe 55,691 hrs · 38,963 cycles

FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER HAS A LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER PER ERA 596251-14AD REV A SECTION III TIME LIMITED REPAIR. REPETITIVELY INSPECT THE SUBJECT REPAIR EVERY 24 MONTHS (730 DAYS) PER ASSOCIATED ERA 596251-14AD REV A SECTION IV FROM DATE OF ACCOMPLISHMENT OF SECTION III REPAIR. ASSOCIATED ERA 00-596251 ADDED FOR AC 9549. (LP #0223851)

Part: DOUBLER — CRACKED (BS 396) · airframe 55,691 hrs · 38,963 cycles

CRACK ON HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC: 00120. HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 52-30-01-2R PROCEDURE 1 REPAIR 1. (LP #0222418)

Part: STRIP — CORRODED (BS 332-370) · corrosion level 2 · airframe 55,691 hrs · 38,963 cycles

CORROSION ON STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 FWD CARGO COMPARTMENT. SUMMARY OF NRC 00625: CORROSION LEVEL 2. STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-08-0G. (LP #0221234)

Part: CUSP WEB — CRACKED (BS 218) · airframe 55,691 hrs · 38,963 cycles

CRACK WAS FOUND AT CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00678: CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIG.215. (LP #0206279)

Part: CUSP WEB — CRACKED (BS 672) · airframe 55,691 hrs · 38,963 cycles

CRACK ON RH CUSP WEB (LOWER SURFACE) STA Y=672 X=- 57 AT PASSENGER CABIN. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=672 X=- 57 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND AFTER TRIM-OUT PER B717 DC/MD NDTSPM PART 6. 06-10-01.001. (LP #0203725)

Part: DOUBLER — CORRODED (BS 541-464) · corrosion level 2 · airframe 55,691 hrs · 38,963 cycles

CORROSION ON RH PREVIOUS REPAIR DOUBLERS STA Y=451-464 AND Y=479 (LOWER SURFACE) X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00524: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER STA Y=451-464 AND Y=479 (LOWER SURFACE) X=- 60 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-00-55-2R-4 REPAIR 4. (LP #0203708)

Part: CUSP WEB — CRACKED (BS 245) · airframe 55,691 hrs · 38,963 cycles

CRACK ON RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00518: RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ALONG THE CUT OUT EDGES, NO CRACKS WERE FOUND PER DC-MD/BOEING NDTSPM PART 6. 06-10-01.001. (LP #0203722)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 53,477 hrs · 37,031 cycles

THE EMERGENCY LIGHTS AT THE LOWER AFT, LT AND RT OVERWING EMERGENCY DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4138625)

Part: BULKHEAD — DAMAGED · airframe 52,366 hrs · 36,035 cycles

DURING EXTENSION AND RETRACTION OF NLG RETRACT ACTUATOR PER STEP 22 FOLLOWING GEAR MAINTENANCE, THE ACTUATOR CONTACTED THE REAR WHEELWELL BULKHEAD CAUSING DAMAGE. NRC 005-0003:3221-4001/013 00035; REPAIRED IAW ER/A 601048-14 REV. ORIG AND PER PRI 601048-14 REV 01. CLOSING REQUIREMENTS RII: INSPECTOR 00746460. (LP #2339754)

Part: NONE — NONE · corrosion level 2 · airframe 52,335 hrs · 36,005 cycles

L/H O/B FIXED STRUT MOUNT HAS CORROSION ON OUTBOARD/FWD MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/002 00023 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331304)

Part: NONE — NONE · corrosion level 2 · airframe 52,335 hrs · 36,005 cycles

L/H O/B FIXED STRUT MOUNT HAS CORROSION AND TOOLING MARKS ON OUTBOARD/AFT MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/001 00022 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331305)

Part: NONE — NONE · corrosion level 2 · airframe 52,335 hrs · 36,005 cycles

RIGHT MLG ATTACH FITTING CHAFED AND CORRODED WHERE FIXED STRUT MOUNTS. -M- SUMMARY SEE NRC 008-0003: 3211-4004/001 00018 PRI 600916-14 REV. 0 PRI 600916-14 REV. 1 AND FINAL ER/A 600916-14 REV. ORIGINAL HAVE BEEN COMPLIED WITH. (LP #2330440)

Part: CABLE ASSY — BROKEN · airframe 51,909 hrs · 35,614 cycles

TAIL CONE SLIDE PACK CABLE RETAINER BROKEN. THIS ITEM IS RII PER TOPP 40-30-05 QC5146. REPLACED CABLE RETAINER PER SAFRAN CMM 25-66-20 QC 5270. (LP #8745178)

Part: NONE — NONE · airframe 51,473 hrs · 35,227 cycles

THE AFT LEFT & RIGHT EMERGENCY EXIT OVERWING THRESHOLD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230 PER B717 AMM 33-51-04. THE EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. (LP #8262534)

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 51,125 hrs · 34,911 cycles

MAIN CABIN FLOOR SUPPORT UNDER FLOOR PANEL 221AF FOUND CORRODED. MAINTENANCE REPLACED SUPPORT PER BOEING DWG 9936534, AND B717 SRM 51-40-02. (LP #2076902)

Part: NONE — NONE · airframe 51,125 hrs · 34,911 cycles

THE RIGHT HAND GALLEY CABIN EMERGENCY EXIT SIGN LIGHT HAS BROKEN WIRES. -M- SUMMARY SEE NRC 001-0010:2500-2647/113 00431: REPAIRED WIRES PER REF B717 SWPM 20-10-03. OPERATIONAL CHECK WAS GOOD. (LP #2076170)

Part: NONE — NONE · corrosion level 2 · airframe 51,125 hrs · 34,911 cycles

AFT CARGO. FLOOR BOARD SUPPORT/FORMER CORRODED AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER. (M) FLOOR BOARD SUPPORT/FORMER AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER FOUND CRACK, FOUND TO BE 100% OUT OF LIMITS PER B717 SRM 53-00-00-1A 3. REPAIRED AFT CARGO. FLOOR BOARD SUPPORT ANGLE AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER PER B717 SRM 51-70-05-2R 5. OK CIC 8. APPLIED CIC ON REPAIR AREA PER PS 900-2 NO. 09 9. CORROSION LEVEL: 2. (LP #2074161)

Part: NONE — NONE · airframe 51,125 hrs · 34,911 cycles

FLOOR BEAM CRACKED AT STATION Y=737 RH OVERWING FRAME ATTACH POINT. REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072760)

Part: NONE — NONE · airframe 51,125 hrs · 34,911 cycles

FLOOR BEAM CRACKED AT STATION Y=737 LH OVERWING FRAME ATTACH POINT. MAINTENANCE REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072758)

Part: SKIN — DAMAGED (BS 446-465) · airframe 55,691 hrs · 38,963 cycles

RH FUSELAGE WINDOW BELT WINDOW #12 AT STA 446-465 HAD A LIGHTNING STRIKE. FOLLOW ON ACTION REQUIRED. ERA 596251-14 ISSUED. FOLLOW ON ACTION REQUIRED SECT I TBA DURING C-CHK VISIT IN MSP DEC2021. SECT II HFEC INSPECTIONS TBA AT EVERY 24 MONTH INTERVALS AFTER SECT I. SECT III PERM REPAIR NOT TO EXCEED 10,000 FC AFTER SECT I. ASSOCIATED ERA 00-596251 ADDED FOR AC 9549. CORRECTION TO PREVIOUS ENTRY. PERFORM SECTION III PRIOR TO AIRCRAFT ACCUMULATING 45000 TOTAL FLIGHT CYCLES OR 10089 FC FROM 30DEC 21. HFEC INSPECTON WAS PERFORMED, NO CRACKS WERE FOUND ON BLENDED AREA PER ERA 596251-14 REV ORIGINAL, SECTION II REPETITIVE INSPECTIONS, STEP 1. SUMMARY OF NRC 00356: RH SIDE WINDOW BELT PANEL AT WINDOW #12 WAS REPAIRED PER ERA 596251-14AD REV B SECTION III: PERMANENT REPAIR. REPETITIVE INSPECTIONS: TO BE ACCOMPLISHED EVERY 24 MONTH INTERVALS AFTER SECTION III WAS PERFORMED UNDER LP #0223851 REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL FLIGHT CYCLES (21,037 FLIGHT CYCLES FROM 38,963 TOTAL FLIGHT CYCLES AS OF 28 FEB 24). CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 06MAR24 AND LOG COMMENTS. (LP #2067714)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 50,424 hrs · 34,247 cycles

THE EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN SWITCHED ON. MAINTENANCE REPLACED THE BATTERY PACK REF B717 AMM 35-31-03. OPERATIONAL CHECK WAS GOOD. (LP #7374989 )

Part: THERMOSWITCH — FAILED (ANTIFOG) · airframe 48,520 hrs · 32,637 cycles

ON TAXI-IN, WHEN ATTEMPTING TO OPEN A FOGGED-UP WINDOW WITH WINDSHIELD ANTI-FOG SELECTED ON, THE WINDOW JAMMED ON THE CAPT HEADSET CAUSING A SHORT. THE RESULT WAS A LOUD BUZZ AND A FIREBALL THAT QUICKLY EXTINGUISHED. THE CB Z-26 ALSO TRIPPED. MAINTENANCE PULLED C/B Z26 AND Z25 AND DISCONNECT WIRE FROM CAPT CLEARVIEW WINDOW. THE CAPT SLIDING WINDOW THERMOSWITCH HARNESS WAS REPLACED PER B717 AMM 30-42. TERMINATED HARNESS ENDS REF B717 WDM 3-42-01. OPERATIONAL CHECK WAS GOOD. BREAKERS STAYED IN. WIRING ON A/C SIDE CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 46,833 hrs · 31,204 cycles

THE CABIN EMERGENCY LIGHTS FLICKER WHILE IN ARMED POSITION VERY OCCASSIONALY. MAINTENANCE REPLACED THE RELAY R2-5133 PER B717 WDM 24-51-01. OPERATIONAL CHECK WAS GOOD. NOTED NO DEFECTS.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 44,104 hrs · 29,220 cycles

MAINTENANCE FOUND THAT THE FWD EMERGENCY LIGHTS FAILED DURING A SERVICE CHECK TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51. OPS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,051 hrs · 29,188 cycles

THE R1 DOOR EXIT SIGN LENS WAS MISSING. MAINTENANCE INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 43,539 hrs · 28,827 cycles

ONE EMERGENCY LIGHT WAS OUT IN THE TAIL COMPARTMENT. MAINTENANCE FOUND A DISCONNECTED WIRE AND CONNECTED IT. OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1022) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 41,118 hrs · 27,093 cycles

0.5 INCH CRACK WAS FOUND ON VERTICAL STAB. FRONT SPAR CAP RT SIDE. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1022) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME BS 1022 ON LONGERON 7L AT PASSENGER CABIN AREA. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 41,118 hrs · 27,093 cycles

ELONGATED HOLES AT THE LT & RT SIDES OF VERTICAL STABILIZER L.E. FRONT SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.

Part: FAIRING — DAMAGED (LEFT) · airframe 41,118 hrs · 27,093 cycles

DURING INSPECTION, AN ELONGATED HOLE ON THE LE REMOVABLE FAIRNG LT SIDE WAS FOUND. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.

Part: SPAR CAP — DISTRESSED (VERTICAL STAB) · airframe 41,118 hrs · 27,093 cycles

DISTRESS AT LT & RT SIDES OF VERTICAL STABILIZER LE SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.

Part: DOOR FRAME — CORRODED (BS 200) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON THE LT WEB DOOR FRAME BS 200, LONGERONS 17 AND 18L REPAIRED IAW ETI-17-17-093, REV. 2 AND ER/A 559514-14 REV. ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 895-1022) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON THE RT CARGO TRACK BETWEEN BS 895 & 954, BS 994 & 1022 IN THE AFT CARGO BAY. THE SECTION OF CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-40-08.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON CENTRAL FUEL TANK SKIN BELOW SLANT PANEL STA Y=742 BTW X=18 TO X=25 LT WHEEL WELL AMDS 0593-2002. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON CTR FUEL TANK SKIN STA Y=742 BTW X=-20 TO X=-60 AT RT WHEELWELL SLANT PANEL AREA AMDS 5300-2003. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN FROM Y=737 TO Y=756, X=22 TO X=60, ALSO Y=705-710, X=-56 TO X=-60 AT CABIN PAX WING BOX AREA AMDS 5300-2008. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.

Part: COWLING — CRACKED (ENGINE) · airframe 41,118 hrs · 27,093 cycles

CRACK ON FIXED COWL APRON HINGE, LATCH ASSEMBLY AFT OF LOWER FAN COWL DOOR ENGINE LT. CRACK ON FIXED COWL WAS REPAIRED PER SRM 54-00-00 REP 1 HINGE, GUSSET, AND CLIP WERE REMOVED AND REINSTALLED PER SRM 51-41-02-0G AND 51-41-05-0G.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME ANGLE BS 1022 BELOW OF LONGERON 14L IN THE PAX CABIN. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05, AND DWG 9912243, REV JS.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME ANGLE BS 1022, LONGERON 14L. FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9912243, REV JB.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 41,118 hrs · 27,093 cycles

HOLES ELONGATED AT FUEL ACCESS PANEL 520GB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, PAR 5, REPAIR 2, CONDITION II.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 41,118 hrs · 27,093 cycles

CRACKED STRAP ON FRONT OF DOOR FRAME WEB BS 200 LONGERON 18L. THE STRAP WAS REPLACED IAW SRM 51-41-08, AND SRM 51-41-05.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 41,118 hrs · 27,093 cycles

ELONGATE HOLES ON THE FUEL ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.

Part: SKIN — CRACKED (BS 1076) · airframe 41,118 hrs · 27,093 cycles

CRACK ON FUSELAGE SKIN BS 1076 BETWEEN LONGERONS 15 - 13L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.

Part: SKIN — CRACKED (BS 1087) · airframe 41,118 hrs · 27,093 cycles

CRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 15L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.

Part: LONGERON — CRACKED (BS 1133) · airframe 41,118 hrs · 27,093 cycles

CRACKED LONGERON 2R, BS 1133 IN THE AFT ACCESSORIES BAU AREA. A REPAIR SPLICE WAS INSTALLED SRM 53-00-05-2R.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 41,118 hrs · 27,093 cycles

CRACK ON INTERCOSTAL IN THE CEILING AREA BETWEEN BS 617 - 636, BL 0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1.

Part: FRAME — CRACKED (BS 1022) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME ANGLE BS 1022, LONGERON 14R. THE DAMAGE WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-00-06-2R, AND DWG 9912243, REV JB.

Part: SKIN — CRACKED (BS 1076-1087) · airframe 51,125 hrs · 34,911 cycles

TWO CRACKS WERE NOTED ON THE FUSELAGE SKIN, BETWEEN 1076 AND 1087, L-14L. ER/A 559501-14 SECTION I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION FOR SECTION II IS REQUIRED. ACCOMPLISH ER/A 559501-14 SECTION II INSPECTION AT C-CHECK INTERVALS FROM SECTION I, NOT TO EXCEED 24 MONTH INTERVALS. FOLLOW ON ACTION IS REQUIRED. ASSOCIATED ER/A 95-559501 ADDED FOR AC 9549. **REDEFERRED LOG TO QC, ESTAB MON INSP **20-0553-8-6826 S/N 09549 REP. C/W DECAL CONDITIONAL INSPECTION, FOUND GOOD. NO FURTHER DEFFECT NOTED. ITEM 5 SHOULD STATE REF ERA 559501-14 REV ORIG SECT 2. C/W ER/A 559501-14 SECTION II INSPECTION . C/W DECAL CONDITIONAL INSPECTION, FOUND GOOD. NO FURTHER DEFECT NOTED. (LP #0104508)

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 41,118 hrs · 27,093 cycles

DISBONDED AREAS AT DENTS 6, 7, AND 18 ON RT WING AFT MOVABLE FLAP VAN. REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND OPN 1031 CARD 2000-8149-02.

Part: FRAME — CRACKED (BS 1168) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME ANGLE, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.

Part: PAN — CRACKED (BS 408) · airframe 41,118 hrs · 27,093 cycles

CRACKED PAN LOWER AREA INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02-2R PROCEDURE 1, REPAIR 1, FIG 201.

Part: SEAT TRACK — CORRODED (BS 822-937) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON RT SEAT TRACK RBL 22 BTW BS 822 & 937. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R, REPAIR 5.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 41,118 hrs · 27,093 cycles

DELAMINATION WAS FOUND BELOW DENTS NR 3 & 12 OF RT WING FLAP FORWARD MOVEABLE VANE LOWER SURFACE. REPAIRED SRM 57-53-01, FIG 201, REP 1.

Part: FRAME — CRACKED (BS 1168) · airframe 41,118 hrs · 27,093 cycles

CRACKED FRAME ANGLE BETWEEN LONGERONS 3R &3L, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.

Part: FITTING — CRACKED (BS 408) · airframe 41,118 hrs · 27,093 cycles

CRACKED LOWER FITTING INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPLACED IAW SRM 51-41-01, AND 51-41-05.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,118 hrs · 27,093 cycles

CRACKED INTERCOSTAL BETWEEN BEAMS 4 AND 5, BS 181, FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9955763, REV M.

Part: FRAME — CRACKED (BS 694) · airframe 41,118 hrs · 27,093 cycles

CRACK ON LT FORMER BS 694, LONGERON 26L. THE FRAME WAS REPAIRED IAW SRM 51-70-11, REP 1.

Part: RUB STRIP — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON RUBSTRIP OF FUEL ACCESS DOOR 520JB I. NEW RUB STRIP 520JB WAS REPLACED PER B717-200 SRM 57-10-01-2R REP 3 PAR 6. (LP #0098256)

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACK ON RT RING PAN (FWD UPPER CORNER) STA Y=756 AT PAX CABIN (CPAX). RING PAN WAS REPAIRED PER SRM 56-20-02-2R-1 REPAIR 1.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 41,118 hrs · 27,093 cycles

WEAR AND NICKS ON PREVIOUS REPAIR DOUBLERS STA 907 LT/LWR ALSO STA 909 LT/UPPER AT PASSENGER CABIN RING PANS AREA. REPAIR DOUBLERS WERE REPLACED PER SRM 56-20-02 REPAIR 1 FIGURE 202.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,118 hrs · 27,093 cycles

CRACKED LONGERON 6 LT ON STA 1022 AT PASSENGER CABIN AREA. LONGERON WAS REPAIRED PER SRM 53-00-05-2R-2, FIG 201.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,118 hrs · 27,093 cycles

CRACKED LONG 6 RT ON STA 1022. AT PASSENGER CABIN AREA. LONG 6 RT ON STA 1022. WAS REPAIRED PER SRM 53-00-05-2R-2-, FIG 201.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 520FT. FUEL TANK ACCESS 520FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WAS REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON SETTLEMENT AREA ON FUEL TANK ACCESS 520CT AND 520DT. FUEL TANK ACCESS 520CT AND 520DT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 41,118 hrs · 27,093 cycles

ELONGATE HOLES ON FUEL TANK ACCESS PANEL 620DB. THE ACCESS PANEL WAS OUT OF LIMITS FOR EXCESSIVE DAMAGES IAW SRM 57-10-01 AND WAS REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,118 hrs · 27,093 cycles

CRACK ON RT FORMERS Y=715 , Y= 694 AT UNDERWING CANTED KEEL , INTERNAL STRUCTURE. FRAMES WERE REPAIRED PER SRM 51-70-11-2R. HFEC INSPECTION WAS PERFORMED AND 01 CRACK OF 0.4" ON RT FORMER Y=694 AT UNDERWING CANTED KEEL, INTERNAL STRUCTURE AND 01 CRACK OF 0.5" ON RT FORMER Y=715 WERE FOUND PER NDT SPM 06-10-01.001.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 620CT AND 620FT. FUEL TANK ACCESS 620CT AND 620FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 41,118 hrs · 27,093 cycles

CRACKED SKIN BTW BEAM NR 1-2 AT HOUSING AREA FWD CARGO COMPARTMENT DOOR (C1). SKIN WAS REPAIRED PER SRM 52-30-01-2R-1, FIG 201.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA. LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA. LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,118 hrs · 27,093 cycles

CRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA. LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR1 FIG 201.

Part: PAN — CRACKED (CABIN) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 140) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON FLOOR SUPPORT BS 140 AND RBL 50. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.

Part: PAN — CRACKED (BS 618) · airframe 41,118 hrs · 27,093 cycles

CRACKED LT LOWER RING PAN BS 618. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 201.

Part: BEAM — CRACKED (PAX DOORWAY) · airframe 41,118 hrs · 27,093 cycles

CRACKED NR 1 BEAM FWD EDGE AT FWD PASSENGER DOORWAY. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 202.

Part: BEAM — CRACKED (PAX DOOR) · airframe 41,118 hrs · 27,093 cycles

CRACKED NR 1 BEAM, AFT EDGE AT FWD PASSENGER DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 201.

Part: CUSP WEB — CORRODED (BS 549-553) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON RT CUSP WEB BS 549 TO 553 BETWEEN RBL 54 TO 60 IN THE PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 41,118 hrs · 27,093 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO 200, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: FLOOR PANEL — BROKEN (COCKPIT) · airframe 41,118 hrs · 27,093 cycles

BROKEN FLOOR PANEL 211ANF. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R, REP 3 AND REPLACED.

Part: BEAM — CRACKED (NLG DOOR FRAME) · airframe 41,118 hrs · 27,093 cycles

CRACK ON THE RT NLG DOOR FRAME BEAM RBL 46 AT NLG W/W. REPAIRED IAW SRM 53-10-14, REP 2.

Part: LIGHT — DETACHED (SEAT 19B) · airframe 40,460 hrs · 26,610 cycles

EMERGENCY LIGHT DETACHED AT SEAT 19B ATTACHED THE EMERGENCY LIGHT. OK FOR SERVICE.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 40,161 hrs · 26,380 cycles

DURING LINE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EMERGENCY LIGHTING IN THE TAILCONE; THEY WOULD FLASH ON AND THEN GO OFF. MAINTENANCE REPLACED THE BATTERY AND THE OPERATIONAL CHECK WAS GOOD. (LP #9118010)

Part: DOOR — OUT OF ADJUST (L1) · airframe 40,047 hrs · 26,305 cycles

FLIGHT CREW REPORTED L1 DOOR HIT THE FUSELAGE AT TOP AFT CORNER. IAW AMM 52-11 DURING VERTICAL ADJUSTMENT FOUND PLAY IN VERTICAL ADJUSTMENT AREA. FOUND DOOR DAMAGE AT SEVERAL AREAS, REPLACED L1 DOOR IAW AMM 52-11. REBUSHED LOWER HINGE FITTING, PRESSURIZATION LEAK CHECKED GOOD. INSTALLED DOOR INTERIOR TRIM IAW AMM 52-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,735 hrs · 26,082 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE AFT OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,288 hrs · 25,802 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOOR L1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,834 hrs · 25,415 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 - 14. REPLACED THE BATTERY PACK AT B5-227 IAW AMM 33-51-03.

Part: SUPPORT BEAM — LOOSE (R1 DOOR) · airframe 36,354 hrs · 23,561 cycles

R1 DOOR EMER EVAC SLIDE CUT OUT LOWER SUPPORT BRACKET LOOSE. R & R BRACKET ASSEMBLY IAW SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 36,354 hrs · 23,561 cycles

STAND BY LIGHT INOPERATIVE AT ROW 12. REPAIRED WIRE IAW SWPM & AMM.

Part: FLASHLIGHT — OUT OF ADJUST (CABIN) · airframe 36,354 hrs · 23,561 cycles

FORWARD EMER FLASHLIGHT INOPERATIVE. ADJUSTED FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,354 hrs · 23,561 cycles

AFT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,354 hrs · 23,561 cycles

AFT OVERHEAD EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,354 hrs · 23,561 cycles

AFT CATWALK EMER LIGHT BULB INOPERATIVE. REPLACED BULB IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,354 hrs · 23,561 cycles

AFT CATWALK EMER LIGHT BULB INOPERATIVE. R & R BULB IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,354 hrs · 23,561 cycles

FORWARD OVERWING DOOR EMER LIGHT BULB INOPERATIVE. R & R LIGHT IAW MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MAIN CABIN FLOOR WEB DOUBLER LOCATED BETWEEN BS 160 - 180, RBL 50 CRACKED. R & R WEB IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MAIN CABIN UPPER CUSP ANGLE CORRODED BETWEEN BS 200 - 218, RBL 55. R & R CUSP ANGLE IAW SRM & EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

CUSP WEB CRACKED BETWEEN BS 636 - 655, RBL 44. R & R CUSP WEB IAW SRM & DWG.

Part: TRACK — CORRODED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

FORWARD CABIN FALSE TRACK CORRODED AT BS 173, RBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 34,879 hrs · 22,538 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 34,879 hrs · 22,538 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR FWD FLOOR FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MEMBRANE CORRODED AT BS 198, RBL 50. REPAIRED MEMBRANE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MAIN CABIN CUSP WEB CRACKED BETWEEN BS 579 TO 598, LBL 54. R & R MAIN CABIN CUSP WEB IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MEMBRANE CORRODED AT BS 204, RBL 58. R & R MEMBRANE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

LEFT WW FWD VERTICAL CHANNEL AT DOOR CUT OUT CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,879 hrs · 22,538 cycles

MAIN CABIN FRAME CRACKED AT BS 674, LONGERON 18R. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,357 hrs · 23,562 cycles

MAIN CABIN FRAME CRACKED AT BS 674, LONGERON 18R. R & R FRAME IAW DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,963 hrs · 21,944 cycles

MAIN CABIN FLOOR PANEL 222MF DELAMINATED AT BS 500, RBL 40. REPAIRED PANEL IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 33,963 hrs · 21,944 cycles

RT FORWARD OVERWING EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

CUSP WEB CRACKED BETWEEN BS 636 TO BS 655 RBL 44. REPAIRED WEB IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT CABIN WINDOW FRAME DOUBLER NR 35 CRACKED AT LOWER AFT CORNER OF WINDOW PANE. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LE SLAT) · airframe 33,963 hrs · 21,944 cycles

RT WING NR 5 SLAT INBD SIDE OF NR 12 TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT SIDE INTERIOR ANGLE CRACKED AT OTBD END AT BS 674. R & R ANGLE IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT CUSP WEB CORRODED BETWEEN BS 446 TO BS 465. R & R CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

UNDERWING BARREL KEEL BEAM LT SIDE INTERIOR ANGLE CRACKED AT BS 696. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

FRAME SUPPORT CRACKED AT BS 655 STRINGER 18L. R & R SUPPORT FROM IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT CUSP WEB CORRODED BETWEEN BS 408 TO BS 427. R & R CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT INTERIOR ANGLE CRACKED AT BS 696. REPAIRED ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT SIDE INTERIOR ANGLE CRACKED AT BS 715. REPAIRED ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT CUSP WEB CORRODED BETWEEN BS 484 TO BS 503. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT DOUBLER CUSP WEB CORRODED BETWEEN BS 579 TO STATION 598. R & R WEB IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT CUSP WEB CORRODED BETWEEN BS 465 TO BS 484. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

MAIN CABIN AFT PRESS BULKHEAD DOOR JAMB LT FITTING CRACKED. R & R FITTING IAW DRAWING.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT CABIN WINDOW FRAME DOUBLER NR 36 CRACKED AT UPPER FWD CORNER. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

MAIN CABIN PRESS BULKHEAD EMERGENCY EXIT SIGN COMPOSITE SUPPORT BROKEN. REPAIRED SUPPORT IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT CUSP WEB CORRODED BETWEEN BS 655 TO BS 715. R & R CUSP WEB IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT CABIN WINDOW FRAME DOUBLER NR 35 CRACKED AT LOWER AFT CORNER OF WINDOW PANE. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

SEAT TRACK CORRODED BETWEEN BS 671 TO BS 810 RBL 44. R & R SEAT TRACK IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

AFT PRESS BULKHEAD DOOR JAMB LT FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT CUSP WEB CORRODED BETWEEN BS 655 TO BS 715. R & R CUSP WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

AFT PRESS BULKHEAD DOOR JAMB RT FITTING CRACKED AT FASTENER HOLES. R & R FITTING IAW SRM.

Part: CLEVIS — CORRODED (TAILCONE) · airframe 33,963 hrs · 21,944 cycles

TAIL CONE LATCH RELEASE CABLE CLEVIS CORRODED. R & R CLEVIS IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

AFT RT VENT BOX DOUBLER ON AFT SIDE ATTACH TO FRAME CRACKED. R & R DOUBLER IAW SWA EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

FORMER CRACKED AT BS 1087 BETWEEN LONGERON 1L TO LONGERON 2L. R & R FORMER IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT MLG DOOR) · airframe 33,963 hrs · 21,944 cycles

LT MLG DOOR HINGE FWD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT FRAME CRACKED AT BS 715. R & R FRAME IAW DRAWING.

Part: SHROUD — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT WW SHROUD ON WING TO BODY FAIRING STRUCTURE DOUBLER CRACKED AT BS 800. REPAIRED STRUCTURE IAW SRM.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT WW FWD WING TO BODY FAIRING STRUCTURE CRACKED AT OTBD END BS 750. REPAIRED STRUCTURE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

LT FRAME CRACKED AT BS 696, CRACKED AT OVERWING FLOOR BEAM. R & R FRAME IAW DRAWING.

Part: ATTACH ANGLE — CRACKED (RT MLG DOOR) · airframe 33,963 hrs · 21,944 cycles

RT MLG DOOR HINGE FWD ATTACH ANGLE CRACKED. R & R ANGLE IAW DRAWING & SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,963 hrs · 21,944 cycles

RT JAMB CORRODED BETWEEN BS 370 TO BS 427. REPAIRED JAMB IAW SRM.

Part: LIGHT — MISSING (CABIN) · airframe 33,005 hrs · 21,330 cycles

RT EMERGENCY LIGHTS MISSING BETWEEN ROW 2 & ROW 3. INSTALLED LAMP IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 31,287 hrs · 20,266 cycles

ROW 2D EMERGENCY PATH LIGHT MISSING. REPLACED 2D EMERGENCY PATH LIGHT BULB OPS CHECKED GOOD IAW AMM. NO DEFECTS AT THIS TIME.

Part: LENS — MISSING (CABIN) · airframe 31,000 hrs · 20,084 cycles

EMERGENCY ESCAPE PATH LIGHTS LENS COVER MISSING AT SEAT 2D. INSTALLED LENS RSF MM.

Part: COVER — MISSING (CABIN)

SIGN COVER MISSING AT ROW 21/22 FELL OFF AND NOT FOUND. FOUND SIGN COVER EXIT SIGN AND RE-INSTALLED, OK FOR SERVICE REF 33-51 AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

R1 DOOR FLOOR SUPPORT FITTING, STA 196, RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 200, RBL 9 TO RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 200, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: PAN — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR PAN, STA 168, RBL 58, CORROSION. ACCOMPLISHED FLOOR PAN REPLACEMENT PER B717 SRM 51-40-08, 51-10-04 AND 51-41-02.

Part: STRAP — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR STRAP, STA 168 TO 200, RBL 56, CORROSION. ACCOMPLISHED FLOOR STRAP REPLACEMENT PER B717 SRM 51-41-01, 51-40-08 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 180, RBL 8 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 196, LBL 15 TO LBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-1-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 196 TO 210, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 148, RBL 39, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, LBL 58, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08 AND 53-10-51.

Part: SHEAR WEB — CORRODED (FUSELAGE)

FORWARD ENTRY SHEAR WEB, STA 200 TO 203, RBL 23 TO RBL 29, CORROSION. ACCOMPLISHED SHEAR WEB SPLICE REPAIR PER B717 SRM 51-70-10 AND 53-10-51.

Part: SHEAR WEB — CORRODED (FUSELAGE)

FORWARD ENTRY SHEAR WEB, STA 200 TO 203, RBL 40 TO RBL 43, CORROSION. ACCOMPLISHED SHEAR WEB SPLICE REPAIR PER B717 SRM 51-70-10 AND 53-10-51.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT SEATS 1D, 2D, 3D INOPERATIVE. REMOVED AND REPLACED BATTERY SUPPLY ASSEMBLY AT STA 341 PER AMM 33-51. CHECKS OK.

Part: PIN — MISSING (EVAC SLIDE)

PINS HOLDING ESCAPE SLIDE PACK AT L1 DOOR MISSING. REMOVED AND REPLACED SLIDE PACK PER MM 25-61-01.

Part: COMPRESSOR — STALLED (LT ENGINE)

COMPRESSOR STALL LEFT ENGINE AFTER TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD 603. LEAK AND OPS CHECK GOOD.

Part: GIRT BAR — BROKEN (ESCAPE SLIDE)

GIRT BAR RETAINER AT GALLEY DOOR BROKEN. REMOVED AND REPLACED GIRT BAR RETAINER AND INSTALLED BACK ON COVER DOOR FOR SLIDE IAW MM 26-61, OK TO CONTINUE SERVICE.

Part: LONGERON — CORRODED (BS 908-946 L30L)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 908 TO 946, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3041.

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: LONGERON — CORRODED (BS 946-974 L30L)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 946 TO 974, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3045.

Part: LONGERON — CORRODED (BS 908-946 L29L)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 908 TO 946, LONG L29L, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3040.

Part: FRAME — DAMAGED (BS 1178)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2985.

Part: SLIDE — LOW PRESSURE (L1 DOOR)

F/A REPORTS L1 DOOR SLIDE PRESSURE LOW. REPLACED L1 DOOR SLIDE PER AMM 25-61-01-6.

Part: BULKHEAD — CRACKED (FUSELAGE)

RUDDER SUPPORT BULKHEAD CRACKED AT 3 O`CLOCK POSITION STA 1178. REPAIRED RUDDER SUPPORT BULKHEAD CRACK AT STA 1178 L18 IAW B717 SRM 51-70-11. COMPLETED AAR N/R 5837 W/O 2000274 - OK FOR SERVICE.

Part: NONE — NONE

EMERGENCY LIGHT SYSTEM INOPERATIVE. FOUND ON F/A PANEL SWITCH IN ON POSITION. RESET SWITCH, SYSTEM OPS NORMAL AS REQUIRED.

Part: FRAME — CRACKED (FUSELAGE)

CRACK NOTICED AT AFT FUSELAGE INT LEFT CANTED BLKD STA 1178.225 L16L AFT OF HYD S/O VALVE. INSTALLED DOUBLE REPAIR AT AFT FUSELAGE INTERNAL LT CANTED BLKD STA 1178.225 L16L IAW B717 SRM 51-70-11 FIG 201 REPAIR 1, MEASURE 12" X 3".

Part: PAN — CORRODED (CARGO DOORWAY)

AFT CARGO DOOR CUT OUT LOWER PAN HAS CORROSION. FOUND CORROSION OUT OF LIMITS TRIMED OUT DAMAGE SECTION AND INSTALLED NEW SECTION AND SPLICES IAW B717 SRM 53-20-15 FIG 201.