N945AT

Part: CABLE — MISINSTALLED (GIRT BAR) · airframe 65,688 hrs · 47,582 cycles

GALLEY SERVICE DOOR R1 DOOR GIRT BAR CABLE MAY BE IMPROPERLY INSTALLED. REPOSITIONED CABLE REF AMM 25-61, OK TO CONTINUE (8385642)

Part: SKIN — PUNCTURED (ZONE 300 ELEV) · airframe 65,338 hrs · 47,265 cycles

PUNCTURE ON LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136. LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136 WAS REPAIRED PER SRM 51-70-13 (1293791)

Part: LONGERON — CRACKED (ZONE 200) · airframe 65,338 hrs · 47,265 cycles

CRACKED LONGERON 2R AT BS 1133. LONGERON 2R REPAIRED IAW SRM 53-00-05. (1277454)

Part: COMPRESSOR — STALLED (ENGINE) · airframe 65,200 hrs · 47,141 cycles

SHIP 9505 GOING THRU 10,000 ON CLIMBOUT WE GOT COMPRESSOR STALL TGT HAD AN X OFF AND ON. CORECTIVE ACTION: EPLACED HARNESS PER B717 AMM 77-21. REPLACED ALL 6 TGT PROBES PER B717 AMM 77-21. (7417510)

Part: BULKHEAD — NO DISCREPANCY (NOT REPORTED) · airframe 64,949 hrs · 46,890 cycles

SHIP 9505 DUE TO HARD LANDING ON FL1405, PERFORM DETAILED INSP IAW ER/A 565522-14AD. CORRECTIVE ACTION: INSPECTED A/C 9505 CANTED BULKHEAD IAW ER/A 565522-14AD. (1053477)

Part: LANYARD — SEVERED (ZONE 800) · airframe 64,391 hrs · 46,394 cycles

FOUND R1 DOOR SLIDE RELEASE LANYARD CABLE SEVERED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE R1 DOOR SLIDE RELEASE LANYARD ASSEMBLY REF B717 AMM 25-61-03. (LP #6874454)

Part: DOUBLER — CRACKED (ZONE 200) · airframe 63,453 hrs · 45,582 cycles

-AD- STA 1178.225 LONGERON 3L BULKHEAD DOUBLER CRACKED. ACCOMPLISH ER/A 565522-14AD REV A SECTION IV FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-565522 ADDED FOR AC 9505. C/W SECTION 4 OF ERA 565522-14AD REV A ALTERNATIVE INSPECTION FOR AD 24-20-02. OK TO CLOSE & MONITOR REMOVED. (LP #0646034)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,254 hrs · 44,508 cycles

THE EMERGENCY EXIT SIGN ON ROW 19CDE IS INOPERATIVE. MAINTENANCE THE FOUND POWER SUPPLY INOPERATIVE. THE POWER SUPPLY (B5-121) WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4343895)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,241 hrs · 43,687 cycles

MULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE TAIL COMPARTMENT CEILING. MAINTENANCE REPLACED THE BATTERY AND THE PSU AT THE RIGHT AFT LAVATORY CEILING. TAIL COMPARTMENT EMERGENCY LIGHTS CHECKED GOOD PER B717 AMM 33-51-10. (LP #4295229)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,180 hrs · 43,638 cycles

THE EMERGENCY CEILING LIGHTS ROW 24-27 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTER PACK AT SEAT 25 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4480888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,040 hrs · 43,513 cycles

CRACK INDICATION AT LEFT OVERWING FRAME STA 696 WHILE PERFORMING AMDS 5310-01436-01B STEP 10. COMPLIED WITH AMDS CARD 5310-01436-03A FOR L/H OVER-WING FRAME REPLACEMENT STA 696. SEE NRC 162. (LP #2949537)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,040 hrs · 43,513 cycles

L1 DOOR SLIDE FOUND LACED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REPLACED SLIDE PER B 717 AMM 25-61-01. (LP #2946641)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,871 hrs · 44,182 cycles

FLOOR SUPPORT CORRODED JUST I/B OF R-1 DOOR UNDER FLOOR PANEL 221EF- MARKED. SUMMARY SEE NRC 087-0025:5310-2005/009 00399: REPLACED FLOOR SUPPORT REF BOEING DWG 9936534. (LP #2927991)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,789 hrs · 43,296 cycles

THE EMERGENCY EXIT LIGHT LENS COVER AT ROW 19 NEEDS TO BE REATTACHED. MAINTENANCE ATTACHED THE EMERGENCY LIGHT LENS COVER AT ROW 19CDE. THE AIRCRAFT IS OK FOR SERVICE. (LP #4642349)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,748 hrs · 43,255 cycles

SHIP 9505 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE RIGHT HYDRAULIC QUANTITY READING LOW. THE CREW WAS ABLE TO PRESSURIZE THE R HYD SYSTEM BETWEEN 5,000-10,000 PSI PER THE QRH. DURING THIS TIME WHEN THE R HYD LIGHT WENT OUT AND PRESS WAS NORMAL, THE CREW LOWERED THE LANDING GEAR NORMALLY. THEN THE R HYD LIGHT ILLUMINATED AGAIN, PRESSURE REMAINED AT 3000 PSI. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND AN AFT HYDRAULIC LINE ON INBOARD FILTER HOUSING LEAKING AND REPLACED AN O-RING. LEAK AND OPERATIONAL CHECKS WERE GOOD. (LP #4642322)

Part: FRAME — DAMAGED · airframe 58,696 hrs · 41,402 cycles

FRAME AT STA 994 SHOWS EVIDENCE OF DAMAGE CAUSED BY BELT LOADER IMPACT. NRC 002-0001:0514-2001/013 00013: REPAIRED FRAME PER B717 SRM 51-70-11-2R-1. (LP #2358780)

Part: SKIN — DAMAGED · airframe 58,696 hrs · 41,402 cycles

B717-200-FUSELAGE SKIN DAMAGE BETWEEN STA 994 1002 AND STR 24R 26R. NRC 002-0001:0514-2001/001 00001: REPAIRED PER ER/A 601169-14 REV. ORIGINAL (PRI 601169-14 REV. 1-7 MATCH ER/A 601169-14 REV. O.) (LP #2358789)

Part: THRESHOLD — DAMAGED · airframe 58,696 hrs · 41,402 cycles

THE AFT CARGO DOOR JAMB WEB JUST AFT OF STA 994 WAS DAMAGED FROM BELT LOADER IMPACT. NRC 002-0001:0514-2001/006 00006: REPAIRED WEB PER ERA 601169-14 REV ORIG. (LP #2358778)

Part: SKIN — DAMAGED · airframe 58,696 hrs · 41,402 cycles

COMPLY WITH PRI/ERA 601064-14 REPAIR OF FUSELAGE SKIN DAMAGE AFT OF AFT CARGO DOOR. COMPLIED WITH STEPS 1,2,3, AND 4 OF PRI 601064-14 REV ORIGINAL PRI REV 0. PERFORMED RII INSPECTION OF PRI 601064-14 REV O. ERA REV ORIG STEPS 1,2,3, & 4. NO ADDITIONAL DAMAGE NOTED. C/W STEPS 2 & 5 OF PRI 601064-14 REV. 1 RII. C/W STEPS 7 THRU 15 OF PRI 601064-14 REV ORG. ISSUED COMPAIRED TO PRI 601064-14 REVS 0-2 ALL STEPS. (INSP 406306) FINAL ERA 601064-14 REV ORG C/W RII STEPS C/W PER ERA 601064-14 ORG. (LP #9212190)

Part: NONE — NONE · airframe 58,190 hrs · 40,944 cycles

A CRACKED AFT BULKHEAD IN THE NOSE LANDING GEAR WHEEL WELL STA 110 WAS FOUND (IN REF NRC 00167). SUMMARY OF NRC 00169: BULKHEAD WAS REPAIRED PER ERA 598690-14 REV. ORIGINAL SECTION I: TEMPORARY REPAIR. ACCOMPLISH THE SECTION II: REPETITIVE INSPECTIONS EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: TEMPORARY REPAIR. UNDER LP #2196268. ACCOMPLISH THE SECTION III: PERMANENT REPAIR WITHIN 48 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: TEMPORARY REPAIR. UNDER LP #2196268. ASSOCIATED ER/A 14-598690 ADDED FOR AC 9505. (LP #2197601)

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 58,187 hrs · 40,942 cycles

CORROSION ON AFT DOOR JAMB OF AFT CARGO DOOR (SM). SUMMARY OF NRC 00007: CORROSION LEVEL 2, PREVIOUS REPAIR AT DOOR JAM OF AFT CARGO WAS REPLACED PER B717 SRM 53-20-15-2R REPAIR 7. PERFORM A DECAL CONDITION INSPECTION EVER C-CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #2187649)

Part: NONE — NONE · airframe 58,048 hrs · 40,834 cycles

THE FUSELAGE INTERCOSTAL WAS FOUND CRACKED AT BEND STA 1212 STA 1225, WHICH AFFECTED THE TAILCONE DEPLOYMENT CABLE ATTACH POINT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. A TEMPORARY REPAIR WAS INSTALLED PER R.I. ERA 596685-14 REV 0 SECTION I: TIME-LIMITED REPAIR INSTRUCTIONS. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE NO ADDITIONAL DICREPANCIES ARE FOUND OUTSIDE OF THOSE FOUND IN THE INTRODUCTION. NO DISCREPANCIES FOUND. ENSURED BENT AREA IS SMOOTH AND FREE FROM GAUGES, CREASES, SCRATCHES, AND CRACKS. NO DISCREPANCIES FOUND. PERFORMED HFEC AT BENT AREA PER STEP 3 R.I. ERA 596685-14. NO DEFECTS NOTED. IN THE CRACKED AREA ON THE INTERCOSTAL, CAREFULLY SLOTTED OUT, TRIMMED OUT, THE CRACK AS SHOWN IN FIG 3. COMPLIED WITH HFEC PER STEP 5 OF R.I. ERA 596685-14. NO DEFECTS NOTED. FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED AN "L" ANGLE FOR THE EXTERIOR SIDE OF THE INTERCOSTAL AS SHOWN IN FIG 3 AND PER SRM 5110-04. INDENTIFIED REPAIR AS ENGINEERING APROVED PER DAL P.S . 9005-1, NO. 4. (LP #2088931)

Part: CAM — MISINSTALLED (TAILCONE RELEASE) · airframe 55,274 hrs · 38,449 cycles

THE TAIL CONE RELEASE CAM MECHANISM IS NOT INSTALLED CORRECTLY. THE ROLLERS DO NOT ENGAGE CAM WHEN TURNED. MAINTENANCE ADJUSTED THE TAILCONE RELEASE MECHANISM CAM, PER B717 AMM 53-52-03 820-801. OK FOR SERVICE.

Part: CABLE — MISROUTED (TAILCONE LOCK) · airframe 53,215 hrs · 36,752 cycles

TAIL CONE LOCK IS CABLE ROUTED INCORRECTLY TO THE EXTERIOR RELEASE HANDLE. MAINTENANCE REROUTED THE LOCKING CABLE CORRECTLY TO EXTERIOR HANDLE ASSEMBLY IAW B717 AMM 53-52-01 830-802. RII COMPLETED BY QC2045. (LP #1236960 )

Part: TRAY — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

SPOTS OF CORROSION ON WASTE SRVC TRAY PANEL. CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G AND REMAINING THICKNESS IS 0.030"; OUT OF LIMITS IAW SRM 53- 00-00-1A ALLOWABLE DAMAGE PAR. 4 FIG-.103. WASTE SRVC TRAY PANEL WAS REPLACED IAW DWG 5965767-7, SRM 51-41-05-0G, AND 51-41-02-0G.

Part: DOUBLER — CORRODED (BS 1022) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON INTERNAL PRODUCTION DOUBLER BTW STA 1022 AND LONG 29RH AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED PER ER/A 580391-14 REV ORIG AND ETI -17-19-122 REV 2.

Part: SLIDING WINDOW — CRACKED (LEFT) · airframe 53,169 hrs · 36,720 cycles

CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE (CPIL). NRC 00575: CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1.

Part: FRAME ANGLE — CRACKED (BS 1152) · airframe 53,169 hrs · 36,720 cycles

CRACKED FRAME CLIP ON STA 1152 AND X=9 CROWN AREA, AFT ACCESORY COMPARTMENT (CAT). NRC 00422: AREA WAS REPAIRED PER ER/A 580410-14 REV ORIG AND ETI-17-19-141 REV 1. ASSOCIATED ER/A 14-580410 ADDED FOR AC 9505. (LP #1219535)

Part: FRAME — CORRODED (BS 890) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FRAME ON BS 890, STRINGER 25L IS OUT OF LIMITS AT AFT CARGO COMPARTMENT, MINIMUM REMAINING THICKNNES IS 0.032" AND OUT OF LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE 1, PAR 4, FIG 103. DUE TO FRAME OUT LIMITS, THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R-3, FIG 201.

Part: SKIN — DELAMINATED (RT TE FLAP VANE) · airframe 53,169 hrs · 36,720 cycles

DELAMINATED AREA WAS FOUND ON LOWER SKIN DENTED. DELAMINATED AREA (0.875 IN X 0.625) ON LOWER SKIN AT RT UPPER MOVABLE VANE WAS REPAIRED IAW ETI-17-19-143 REV. 2 AND ER/A 580374-14 REV. ORIG, SECTION I, PERMANENT REPAIR.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 53,169 hrs · 36,720 cycles

ELONGATED SCREW HOLES ON LH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER INNER SKIN AND PAN AT LH FWD OVERWING EMERGENCY EXIT DOOR REPAIRED IAW ETI-17-19-134 REV 2, AND ER/A 580350-14, REV ORIGINAL, SECTION I, PERMANENT REPAIR.

Part: CARGO TRACK — CORRODED (BS 899-1022) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON LH TIE TRACK BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-04-0G PAR 26. MAXIMUM REMAINING THICKNESS IS 0.038 AND THEREFORE IT IS OUT OF LIMITS IAW SRM 53-20-52-1A-2 FIG 101. LT TIE TRACK WAS REPLACED IAW SRM 51-40-05-0G, 51-41-01-0G, AND 51-40-08-0G PAR 3.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 53,169 hrs · 36,720 cycles

ELONGATED SCREW HOLES ON LH AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. LT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-135 REV 1 AND ER/A 580351-14 REV ORIGINAL SECTION I PERMANENT REPAIR.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 53,169 hrs · 36,720 cycles

ELONGATED SCREW HOLES ON RH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-137 REV ORIGINAL AND ER/A 580352-14 REV ORIGINAL SECTION I PERMANENT REPAIR.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 53,169 hrs · 36,720 cycles

ELONGATED SCREW HOLES ON THE RT AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-138 REV ORIGINAL AND ER/A 580353-14 REV ORIGINAL SECTION I, PERMANENT REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 36,795 cycles

FUSELAGE / SKIN / DOUBLER / STA Y=1022.091 AND L29R / ARE CORRODED. ASSOCIATED ER/A 00-580391 ADDED FOR AC 9505. (LP #1214643)

Part: DOOR FRAME — CRACKED (NLG DOORWAY) · airframe 53,169 hrs · 36,720 cycles

CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00404: CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211487)

Part: DOOR FRAME — CRACKED (NLG DOORWAY) · airframe 53,169 hrs · 36,720 cycles

CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00402: CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211495)

Part: FRAME — CRACKED (BS 1037) · airframe 53,169 hrs · 36,720 cycles

AWR HIDDEN CRACK: AFTER REMOVAL OF LONGERON IN REFERENCE NRC 00484 CRACK ON FRAME WAS FOUND STA Y 1037 AND LONG 17 LH. AREA WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4 (ET) HFEC INSPECTION WAS PERFORMED ON FRAME STA Y 1037 AND LONG 17LH. NO CRACKS WERE FOUND AFTER TRIM OUT PER B717-200 S.R.M. 53-20-07-2R REPAIR 4, PARAGRAPH 5.A.(2) AND DC-MD/BOEING NDT SPM PART 6, 06-10-01.001. (LP1212809)

Part: GUSSET — CRACKED (BS 1022 BULKHEAD) · airframe 53,169 hrs · 36,720 cycles

CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD (CPAX). NRC 00530: CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD WAS REPAIRED PER ETI-17-19-126 REV 1 AND ER /A 580279-14 REV ORIG. SECTION I : PERMANENT REPAIR. ASSOCIATED ER/A 14-580279 ADDED FOR AC 9505. (LP #1210721)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FUEL ACCESS PANELS (620CB & 620GB) ON COUNTERSINK AND SETTLEMENT AREA. (FUS). NRC 00619: LEVEL CORROSION 2, FUEL ACCESS PANELS #620CB & 620GB ARE OUT OF LIMITS AND WERE REPLACED. EFFECTIVITY WAS VERIFIED PER B717-200 IPC 57-23-01- 01 AND MUST BE INSTALLED PER AMDS 2040-0012 JOB 001-0333.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,169 hrs · 36,720 cycles

CRACKED LONGERON 7L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,169 hrs · 36,720 cycles

CRACK ON LONGERON 17L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,169 hrs · 36,720 cycles

CRACKED LONGERON 6R, BS 1022, AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,169 hrs · 36,720 cycles

CRACKED LONGERON 5R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: CUSP WEB — CRACKED (BS 794-813) · airframe 53,169 hrs · 36,720 cycles

TWO CRACKS AT THE RT PREVIOUS REPAIR CUSP WEB BETWEEN BS 794 TO 813 AND -44 TO -54. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-01, AND DWG 9910151-150 REV CH.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,169 hrs · 36,720 cycles

CRACKED LONGERON 4R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: FRAME — CRACKED (BS 908) · airframe 53,169 hrs · 36,720 cycles

CRACK ON LOWER FWD CORNER OF LH RING PAN BTW STA Y=889 TO 908 AT PASSENGER CABIN (CPAX). NRC 00636: CRACK ON LOWER FWD CORNER OF LH RING PAN BTW STA Y=889 TO 908 AT PASSENGER CABIN DAMAGE AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202, 51-41-02-0G, AND 51-41-05-0G. (LP #1201587)

Part: FRAME — CRACKED (BS 851) · airframe 53,169 hrs · 36,720 cycles

CRACKED RINGPAN WINDOW BTW STA 832 TO STA 851 AT AFT UPPER CORNER SIDE (CPAX). NRC 00454: DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202, 51-41-02-0G, AND 51-41-05-0G. (LP #1201536)

Part: WINDOW FRAME — CRACKED (BS 908) · airframe 53,169 hrs · 36,720 cycles

CRACKED RINGPAN WINDOW BTW STA 908 TO STA 889 AT AFT UPPER CORNER SIDE (CPAX). NRC 00447: CRACKED RINGPAN WINDOW DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202, 51-41-02-0G, AND 51-41-05-0G. (LP #1201530)

Part: FRAME — CRACKED (BS 870) · airframe 53,169 hrs · 36,720 cycles

CRACKED RINGPAN WINDOW BTW STA 851 TO STA 870 AT AFT UPPER CORNER SIDE (CPAX). NRC 00453: CRACKED RING PAN WINDOW DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202, 51-41-02-0G, AND 51-41-02-05-0G. (LP #1201546)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FUEL ACCESS PANELS #520CT AND #620CT AT SETTLEMENT AREA. NRC #00658: CORROSION LEVEL 2, UPPER WING ACCESS DOOR #520CT AND #620CT WERE REPLACED PER B717-200 SRM 57-10-01 AND VERIFIED PER IPC 57-22-01-01 IMAGE 065. (LP #1199639)

Part: VANE — DELAMINATED (TE FLAP) · airframe 53,169 hrs · 36,720 cycles

DELAMINATION WAS FOUND FROM STA XF 91 TO XF 99, AT LEFT INBD FLAP AFT MOVABLE VANE IN REF NRC 00337. AI. NRC 00655: REPAIR WAS PERFORMED ON DELAMINATION AREA FROM STA XF 91 TO XF 99, AT LEFT INBD FLAP AFT MOVABLE VANE PER SRM 51-70-02-0G PAR.15.A.(1) TO (15) AND TABLE 6 IN REFERENCE SRM 57-53-01-2R-1 PAR.4.D. (LP #1198313)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 53,169 hrs · 36,720 cycles

DELAMINATED FLOOR PANELS #222DF, 222GF, 222KF, 222ACF, AND 222AAF. PAX CABIN. (CAB PAX). NRC 00605: FLOOR PANELS #222DF, 222GF, 222KF, 222ACF, AND 222AAF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1196723)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 53,169 hrs · 36,720 cycles

CRACK AND DELAMINATION ON FLOOR PANELS #222ARF AND 223BF. PAX CABIN. (CAB. PAX). NRC 00666: FLOOR PANEL #222ARF AND 223BF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20- 50-2R-3. (LP #1196590)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 53,169 hrs · 36,720 cycles

CRACK ON LT CUSP WEB BTW STA Y=218 AND X=44 (IN REF TO 5300-2020). (CPAX). NRC 369: CRACK ON LT CUSP WEB BTW STA Y=218 AND X=44 DAMAGED AREA ON LT CUSP WEB BTW STA Y=218 AND X=44 WAS TRIMED OUT PER SRM 53-00-55-2R FIGURE 212. REPAIR PARTS WERE FABRICATED AND INSTALLED PER SRM 53-00-55-2R FIGURE 212 AND 51-41-05-0G. (LP #1194678)

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 53,169 hrs · 36,720 cycles

BROKEN FLOOR PANNEL 221MF (CPAX). NRC 00547: FLOOR PANEL 221MF WAS REPAIRED PER SRM 51-70-09-2R-10. (LP #1189353)

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 53,169 hrs · 36,720 cycles

CRACKED CHANNEL ON FLOOR PANEL #221TF (CPAX). NRC 00133: CHANNEL ON FLOOR PANEL #221TF WAS REPAIRED PER SRM 53-20-50-2R-5. (LP #1187777)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FLOOR SUPPORT BTW STA 195 AND X=45, FWD WET AREA (W1). NRC 00468: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT BTW STA 195 AND X=45 WAS REMOVED PER SRM 51-10-04-0G PAR 26 AND WAS FOUND THAT IT IS OUT OF LIMITS PER SRM 53-00-00-1A. FLOOR SUPPORT BTW STA 195 AND X=45 WAS REPLACED PER SRM 53-10-51-0I-2, 51-40-08-0G, AND 51-41-02-0G. (LP #1187793)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FLOOR SUPPORT BTW STA 196 AND X=24, FWD WET AREA (W1). NRC 00467: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA 196 AND X=24 WAS REPLACED PER SRM 53-10-51-0I-2, 51-40-08-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #1187599)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FLOOR SUPPORT BTW STA 180 AND X=-9 TO X=-42, FWD WET AREA (W1). NRC 00465: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA 180 AND X=-9 TO X=-42 WAS REPLACED PER SRM 51-40-08-0G, 53-10-51-0-2 FIG. 1, 51-41-02-0G, AND 51-41-05-0G. (LP #1185741)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,169 hrs · 36,720 cycles

CORROSION ON FLOOR SUPPORT BTW STA 200 AND X=15 TO X=-08, FWD WET AREA (W1). NRC 00466: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA 200 AND X=15 TO X=-08 WAS REPLACED PER SRM 51-40-08-0G, 53-10-51-0-2 FIG. 1 AND 51-41-02-0G. (LP #1184730)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,169 hrs · 36,720 cycles

CRACK ON LT CUSP WEB STA Y=854 AT CABIN PASSENGER (CPAX) (AMDS 5300-2020). NRC 00189: CRACK DAMAGED AREA WAS REMOVED PER SRM 53-00-55-2R FIGURE 215. REPAIR PARTS WERE FABRICATED AND INSTALLED PER SRM 53-00-55-2R FIGURE 215 AND SRM 51-41-05-0G. (LP #1184602)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,186 hrs · 35,980 cycles

THE EMERGENCY LIGHTS AT EXIT ROW 18 ARE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT THE OVERHEAD PANEL AND REPLACED THE BATTERY PACK AND BATTERY. OPERATIONAL CHECK WAS GOOD PER B717 WDM 33-51 AND SWPM 20-20.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,469 hrs · 35,460 cycles

THE EMERGENCY LIGHTS IN THE TAILCONE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,469 hrs · 35,460 cycles

THE EMERGENCY LIGHTS IN CEILING PANELS ROWS 2 - 6 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-227 PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: NONE — NONE (NONE) · airframe 51,493 hrs · 35,476 cycles

DURING LIGHTNING STRIKE INSPECTION, FOUND DAMAGE AND CORROSION TO THE RIGHT ELEVATOR AND TAB ASSEMBLY. ALSO FOUND CORROSION TO THE TORSION BAR SPINES. REPLACED THE UPPER AND LOWER ELEVATOR SKINS PER SRM 51-70-13-2R AND REPLACED THE TORSION BAR PER CMM 27-30-1 DELAT REV # 88 DELTA REV DATE 08/14/2018

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,021 hrs · 35,162 cycles

EMERGENCY LIGHTS FROM AFT OVERWING EXIT TO AFT LAVS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACKS AT B5-230 & B5-231. OPERATION IS NOW NORMAL IAW AMM 33-51. AIRCRAFT IS OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,219 hrs · 34,573 cycles

R1 DOOR EMERGENCY LIGHT LENS FOUND MISSING. MAINTENANCE INSTALLED A NEW LENS, RETURNED TO NORMAL.

Part: ACTUATOR — OUT OF RIG (MLG DOORS) · airframe 49,674 hrs · 34,182 cycles

LT GEAR UNSAFE LIGHT ILLUMINATED WITH THE LANDING GEAR RETRACTED. WHEN THE CREW LOWERED THE GEAR RECEIVED 3 DOWN AND LOCKED GREEN INDICATIONS. AN EMERGENCY WAS DECLARED FOR THE RETURN TO DEPARTURE. MAINTENANCE RIGGED BOTH OF THE MLG DOOR ACTUATORS, BOTH OF THE MLG DOOR LATCHES, AND ADJUSTED BOTH THE MLG UPLOCK SENSORS. OPS CHECKED GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (STABILIZER) · airframe 49,654 hrs · 34,163 cycles

CRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, RIGHT HAND SIDE. HOLE 6 TOP TO BOTTOM, MARKED. 5530-01048-01/010 00252: PRI 565466-14AD REV O-4 MATCHES ER/A 565466-14AD REV O STEPS 1-12. COMPLY WITH STEP 13 OF ER/A 565466-14AD REV O ON THIS NRC.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,655 hrs · 34,166 cycles

RIGHT SIDE OF THE VERTICAL STAB, UPPER SEGMENT, UPPER ROW OF FASTENERS, COUNTERSINKS ELONGATED. REPAIRED IAW ERA 565657-14AD, REV O.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,654 hrs · 34,163 cycles

LEFT HAND VERTICAL STAB L/E AT ZFS 52.267: LOWER 2EA ROWS FASTENERS HAVE ELONGATED HOLES AND COUNTERSINKS. REF: AA5530-01048 AND AD 2016-09-05. NRC 018-0001:5530-01048-01/001 00200: REPAIR COMPLIED WITH ON ER/A 565657-14AD REV O. ATTACHED TO NRC 254.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,655 hrs · 34,166 cycles

VERTICAL STAB RIGHT SIDE AT ZFS 52.267, UPPER L/E SEGMENT LOWER ROW OF FASTENER HOLES FROM L/E AFT HAVE DEFORMED HOLES. REPAIRED IAW ER/A 565657-14AD, REV O.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 49,654 hrs · 34,163 cycles

VERTICAL FWD LT SPAR CAP IS CRACKED AT APPROX AT ZFS 52.267 NRC 018-0001:5530-01048-01/011 00254: PRI 565362-14AD REV O-5 MATCHES ER/A 565362-14AD REV O STEPS 1-22 AND 24 COMPLIED WITH STEP 23 OF ER/A 565362-14AD REV O ON THIS NRC. PRI 565657-14AD REV O-4 MATCHES ER/A 565657-14AD REV O. PRI 565446-14AD REV O-1 MATCHES ER/A 565446-14AD REV O.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,655 hrs · 34,166 cycles

RIGHT SIDE OF VERTICAL STAB AT XFS 52.267, RIGHT LOWER SEGMENT LOWER ROW OF FASTENERS, ELONGATED COUNTERSINKS. REPAIRED IAW ER/A 565657-14AD, REV O.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,655 hrs · 34,166 cycles

VERTICAL STAB L/E LOWER ROW OF FASTENERS, RIGHT SIDE HAVE ELONGATED HOLES AND COUNTERSINKS, AT ZFS 52.267. REPAIRED IAW ERA 565657-14AD, REV O.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,655 hrs · 34,166 cycles

L/E OF VERTICAL STAB, RIGHT SIDE LOWER SEGMENT, UPPER ROW OF FASTENERS COUNTERSINKS ELONGATED. REPAIR IAW ER/A 565657-14AD, REV O.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 49,654 hrs · 34,163 cycles

CRACK IN VERTICAL STAB SKIN LT SIDE AFT OF SPAR CAP. NRC 018-0001:5530-01048-01/007 00234: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.

Part: SKIN PANEL — CRACKED (STABILIZER) · airframe 49,654 hrs · 34,163 cycles

CRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, LEFT HAND SIDE. HOLE 1, 2, 6, 7, 8, AND 9, TOP TO BOTTOM. NRC 018-0001:5530-01048-01/009 00251: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 49,654 hrs · 34,163 cycles

INTERNAL WEB AT VERTICAL FWD LT SPAR CAP IS CRACKED AT APPROX. AT ZFS 52.267. NRC 018-0001:5530-01048-01/012 00255: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.

Part: STRUCTURE — CRACKED · airframe 49,654 hrs · 34,163 cycles

A CRACK WAS FOUND AT CF 1200, RT FWD SIDE JUST FORWARD OF THE RUDDER HYD SHUTOFF VALVE. REPAIRED IAW ER/A 565689-14, REV ORG.

Part: SKATE ANGLE — CRACKED (BS 1189) · airframe 49,654 hrs · 34,163 cycles

FOUND A CRACK ON THE FORWARD CANTED FRAME BS 1189, AT THE LEFT SKATE ANGLE. REPAIRED IAW ER/A 565522-14, REV ORG.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 57,634 hrs · 40,491 cycles

A CRACK WAS FOUND FORWARD OF THE VERTICAL STABILIZER CANTED FRAME AT STA 1189 AT LH SKATE ANGLE ATTACH FASTENER. ACCOMPLISH SECTION II: INITIAL INSPECTION 3800 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION III: REPETITIVE INSPECTION EVERY 3800 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION III INITIAL INSPECTION. ASSOCIATED ER/A 00-565522 ADDED FOR AC 9505. SUMMARY: GENERAL VISUAL INSPECTION WAS PERFORMED OR PERMANENT REPAIR AND NO FURTHER DAMAGE NOTED PER ERA 565522-14 REV. ORIG. SECTION III. ATL 23DEC21 INSPECTED STA 1178.225 LONGERON 3L BULKHEAD DOUBLER PER ERA 565522-14 ORIG SEC III. NO FURTHER DAMAGE NOTED. (LP #0421415)

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 49,654 hrs · 34,163 cycles

BEHIND THE FORWARD MOUNT OF THE UPPER RIGHT FAIRING, A FASTENER BARREL NUT SHOWED SIGNS OF CORROSION ON THE RIGHT HORIZONTAL STABILIZER. REMOVED THE FASTENER, AND REPAIRED THE BARREL NUT HOLE IAW PRI 565416-14, REV ORG.

Part: SKIN PANEL — WORN (VERTICAL STAB) · airframe 49,654 hrs · 34,163 cycles

NON REMOVABLE VERTICAL STAB L/E PANEL IS WORN/FRETTED ON SKIN LOWER SURFACE AT ZFS 52.267, CENTER UPPER END OF PANEL. RESTORED FINISH PER SRM 55-30-01-1A.

Part: LIGHT — MISSING (CABIN) · airframe 46,686 hrs · 32,047 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT STRIP WAS MISSING. MAINTENANCE INSTALLED AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,096 hrs · 31,620 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19, IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,756 hrs · 31,317 cycles

DURING PREFLIGHT CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE FIRST CLASS SECTION WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPS CHECK WAS GOOD.

Part: LATCH — MISINSTALLED (TAILCONE) · airframe 44,726 hrs · 30,445 cycles

TAILCONE DOOR COVER LATCH, LEFT SIDE, DOES NOT OPERATE NORMALLY. IT APPEARS TO BE MOUNTED BACKWARDS. MAINTENANCE REINSTALLED QTR TURN LATCH FOR THE COVER OF THE AFT CABIN DOOR EMERGENCY OPERATING HANDLE, REF AMM 52-52.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,667 hrs · 30,400 cycles

ABOVE R1 DOOR EMER LIGHT BULB INOPERATIVE. R & R LAMP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,667 hrs · 30,400 cycles

TAIL COMPARTMENT OVERHEAD EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,667 hrs · 30,400 cycles

TAIL COMPARTMENT AFT CATWALK EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 44,667 hrs · 30,400 cycles

AFT EMER SIGN LIGHT CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: WEDGE — CRACKED (RT SPOILER) · airframe 43,162 hrs · 29,389 cycles

RIGHT WING OTBD SPOILER TE WEDGE CRACKED. R & R SPOILER IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 794 - 813. REPAIRED CUSP WEB IAW SRM.

Part: WEB — CRACKED (BS 145) · airframe 43,162 hrs · 29,389 cycles

MEMBRANE CRACKED AT MAIN CABIN BS 145, RBL 16. REPAIRED MEMBRANE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

RIGHT MAIN CABIN CUSP WEB CRACKED, AT STATION 756 - 794. REPAIRED WEB IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

AFT CARGO FORMER CORRODED AT BS 946, BETWEEN LONGERON 30R - 29R. R & R FORMER IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FRAME CRACKED AT BS 715, STRINGER 17L. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,698 hrs · 30,419 cycles

LEFT OVERWING CABIN FRAME CRACKED AT BS 715. R & R FRAME IAW DWG.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MEMBRANE CRACKED AT BS 200, RBL 44. REPAIRED MEMBRANE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CANTED FRAME CLIP CRACKED AT BS 1200, LONGERON 17L OF THE AFT ACCESSORY COMPARTMENT. R & R CLIP IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

LEFT KEEL BEAM, FORMER CRACKED AT BS 674, OTBD END. REPAIRED FORMER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

LEFT WW FWD DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: FORMER — CRACKED (BS 696) · airframe 43,162 hrs · 29,389 cycles

RIGHT KEEL BEAM FORMER AT BS 696, OTBD END OF FORMER CRACKED. R & R FORMER IAW EA.

Part: BRACKET — CRACKED (FLAP TRACK) · airframe 43,162 hrs · 29,389 cycles

LEFT WW INBD SIDE OF INBD FLAP TRACK ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: FORMER — CRACKED (BS 696) · airframe 43,162 hrs · 29,389 cycles

RIGHT KEEL BEAM FORMER AT BS 696, OTBD END OF FORMER CRACKED. R & R FORMER IAW EA.

Part: ISOLATOR — BROKEN (RT PYLON) · airframe 43,162 hrs · 29,389 cycles

RIGHT PYLON SNUB PLATE, UPPER, AT FWD VIBRATION ISOLATOR BROKEN. R & R ISOLATOR IAW AMM.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 43,162 hrs · 29,389 cycles

RIGHT PYLON STRUT, REAR ENG MOUNT REAR FITTING CRACKED. R & R FITTING IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,162 hrs · 29,389 cycles

RIGHT HORIZONTAL STABILIZER, UPPER BANANA FAIRING CRACKED SKIN AT REAR EDGE. REPAIRED SKIN IAW EA.

Part: SUPPORT FITTING — CRACKED (RT AILERON) · airframe 43,162 hrs · 29,389 cycles

RIGHT WING AILERON OTBD HINGE, T SUPPORT FITTING CRACKED. R & R FITTING IAW SRM.

Part: SLAT TRACK — CRACKED (RT WING) · airframe 43,162 hrs · 29,389 cycles

RIGHT WING FIXED LE OTBD SIDE OF NR 8 SLAT TRACK CRACKED. R & R NR 8 SLAT TRACK IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

LONGERON CORRODED, BETWEEN BS 908 - 1002, LONGERON 30. R & R LONGERON IAW SRM & DWG.

Part: SIGN — CRACKED (CABIN) · airframe 43,162 hrs · 29,389 cycles

AFT ACCESSORY COMPARTMENT, TAIL CONE EMER EXIT HANDLE SIGN CRACKED. R & R SIGN IAW SRM.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR BRACKET BROKEN, BETWEEN BS 946 - 954, BETWEEN LONGERON 30R TO 29R. R & R BRACKET IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FORWARD CARGO DOOR JAMB WEB CUT OUT CORRODED. R & R WEB IAW SRM & DWG.

Part: CABLE — DENTED (TAIL CONE) · airframe 43,162 hrs · 29,389 cycles

TAIL CONE RELEASE CABLES DENTED AT 10 O'CLOCK POSITION. R & R CABLE ASSEMBLY IAW MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 160, BETWEEN LBL 7 TO RBL 7. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,162 hrs · 29,389 cycles

FLOOR PANEL 221AQF DAMAGED. R & R THE FLOOR PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 237, BL 0. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 195, LBL 53. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,162 hrs · 29,389 cycles

FLOOR PANEL 221KF DAMAGED. R & R THE FLOOR PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED, BETWEEN BS 148 - 200, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

AFT CARGO FWD BULKHEAD RT SIDE PANEL ATTACH FRAME CRACKED. R & R INTERCOSTAL IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 7 TO RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,162 hrs · 29,389 cycles

FLOOR PANEL 221AF DAMAGED. R & R THE FLOOR PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 43,162 hrs · 29,389 cycles

L1 DOOR JAMB FLOOR SUPPORT PLATE CORRODED. R & R SUPPORT PLATE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

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

Part: HEAT SHIELD — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FUSELAGE FRAME, HEAT SHIELD CRACKED AT BS 1053, STRINGER 18R. R & R HEAT SHIELD IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SUPPORT ANGLE CRACKED AT BS 1053, STRINGER 18. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

AFT CARGO, FWD BULKHEAD LT SIDE PANEL, ATTACH FRAME CRACKED. R & R INTERCOSTAL IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 210, RBL 11. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CORROSION ON FLOOR SKIN PANEL, STATION 200, RBL 52. R & R SKIN PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 7 - 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 160, BETWEEN LBL 7 TO LBL 54. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 899 - 1022, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 647 - 827, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

L1 DOOR CUT OUT AFT WEB CRACKED AT BS 200, STRINGER 11. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 587 - 647, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 899 - 1022, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 827 - 899, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 237 - 313. R & R CUSP WEB IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 200 - 587, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 647 - 827, RBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 587 - 647, RBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 200 - 58, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 218 - 237. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 899 - 1022. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (BS 313-389) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN STATION 313 - 389, RT SIDE. REPAIRED CUSP WEB IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 827 - 899, RBL 44. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,162 hrs · 29,389 cycles

FORWARD CABIN AREA FLOOR SUPPORT CORRODED AT STATION 200, LBL 10. REPAIRED SUPPORT IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN SEAT TRACK & FITTING CORRODED AT BS 218, RBL 55. R & R FITTING IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 200 - 587, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 899 - 1022, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 389 - 408. R & R CUSP WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CABIN SEAT TRACK CORRODED, BETWEEN BS 646 - 823, LBL 44. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CABIN SEAT TRACK CORRODED, BETWEEN BS 823 - 899, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 823 - 899, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 899 - 1022, LBL 22. R & R SEAT TRACK IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 587 - 646, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 587 - 646, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CABIN SEAT TRACK CORRODED, BETWEEN BS 200 - 587, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 832 - 851. REPAIRED CUSP WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

SEAT TRACK CORRODED, BETWEEN BS 646 - 823, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

R1 DOOR FILLER PLATE AT GIRT BAR FITTING CORRODED. R & R FILLER PLATE IAW SRM & DWG.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FALSE TRACK CORRODED, BETWEEN BS 148 - 200, RBL 7. REPAIRED FALSE TRACK IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 43,162 hrs · 29,389 cycles

R1 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING ATTACH PLATE CORRODED. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 44 TO RBL 54. R & R SUPPORT IAW DWG.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

FALSE TRACK CORRODED, BETWEEN BS 148 - 200, LBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: PLATE — CORRODED (R1 DOOR) · airframe 43,162 hrs · 29,389 cycles

R1 DOOR EMER EVAC SLIDE, FWD GIRT BAR FITTING ATTACH PLATE CORRODED. R & R PLATE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 889 - 908, LBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CUSP WEB CORRODED, BETWEEN BS 883 - 908, RBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 715, BETWEEN LBL 55 - 60. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 908 - 954, RBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

RIGHT CUSP WEB CORRODED, BETWEEN STATION 389 & 503. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 655 - 715, BETWEEN RBL 60 TO 46. R & R WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 598 - 579, RBL 60. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 596 - 636, LBL 60. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 813 - 832. R & R CUSP WEB IAW SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP ANGLE SPLICE CORRODED AT BS 899, LBL 60. R & R SPLICE IAW SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB ANGLE SPLICE CORRODED AT BS 646, LBL 60. R & R SPLICE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

CUSP WEB CORRODED AT BS 551, LBL 60. R & R CUSP WEB IAW DWG & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 715 - 756, LBL 60. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 794 - 813, RBL 60. REPAIRED CUSP WEB IAW SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB ANGLE SPLICE, CORRODED AT BS 899, RBL 60. R & R SPLICE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 503 - 579, RBL 60. R & R CUSP WEB IAW DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,162 hrs · 29,389 cycles

AFT CARGO DOOR JAMB LOWER PAN CORRODED. REPAIRED PAN IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,273 hrs · 28,820 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK CABLE OUT OF POSITION. R & R SLIDE IAW AMM.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 41,789 hrs · 28,516 cycles

RT EEPLS WIRE OUT OF POSITION AT ROW 15. R & R EEPLS IAW MM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 40,519 hrs · 27,703 cycles

AT AFT CARGO DOOR CUTOUT, LOWER LIP AFT DEPRESSOR SPLICE PLATE CRACKED. R&R PLATE IAW SRM & DRAWING.

Part: CABLE — LOOSE (R2 DOOR) · airframe 40,519 hrs · 27,703 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER CABLE LOOSE. SECURED CABLE IAW AMM.

Part: PAN — CORRODED (FUSELAGE) · airframe 40,519 hrs · 27,703 cycles

AFT CARGO DOOR PAN CORRODED IN SEVERAL AREAS. R&R JAMB PAN IAW SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 38,172 hrs · 26,209 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER AMM.

Part: FITTING — LACK OF LUBE (L1 DOOR) · airframe 38,054 hrs · 26,129 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS INOP. CLEANED & LUBED FITTINGS PER AMM.

Part: MODULE — MALFUNCTIONED (FUEL SYSTEM) · airframe 37,272 hrs · 25,626 cycles

DIVERSION - INITIAL LOSS OF FUEL QTY IND ALL TANKS BOTH A AND B CHANNELS. REMOVED AND REPLACED SEM PER MM.

Part: PANEL — WORN (LT WING)

LEFT WING O/B FIXED LEADING EDGE I/B OF WING TIP PANEL, WORN. ACCOMPLISHED PANEL REPLACEMENT PER B717 SRM 51-41-02.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS IN AFT ACCESSORY COMPT INOP. REMOVED AND REPLACED POWER SUPPLY ASSY & BATTERY OPS CHECK GOOD IAW MM 33-51.

Part: BATTERY — DISCHARGED (CABIN)

AFT ACCESSORY COMPT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY IAW B717 AMM 33-51-03. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SERVICE CHECK FOUND AFT ACCESSORY COMPARTMENT EMERGENCY EXIT LIGHTING INOP. REMOVED AND REPLACED AFT ACCESSORY COMPARTMENT LIGHTING POWER SUPPLY & CHECKED REF B717 AMM 33-51-03 F/C GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SIDE OF SEAT 3D DOES NOT ILLUMINATE. RELAMPED & OPS CHECKED REF AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN)

LT AFTER OVERWING EXIT HATCH LWR EMERGENCY EXIT LIGHTED SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY & BATTERY ASSY IAW AMM 33-51-03.

Part: LIGHT — INOPERATIVE (CABIN)

LT SIDE AFT EMERGENCY SLIDE EMERGENCY EXIT LIGHT HAS 3 OUT OF 5 LAMPS INOP. RELAMPED EMERGENCY EXIT LAMPS REQ'D OPS CHECK NORMAL IAW AMM 33-51-00.

Part: ACTUATOR — MALFUNCTIONED (NLG)

DURING FINAL APPROACH, NO NOSE GEAR LOCK INDICATION WHEN LANDING GEAR HANDLE PLACED IN DOWN POSITION. CONFIRMED WITH RED NOSE GEAR UNSAFE INDICATOR, AND NO AUDIBLE NOISE OF NOSE GEAR EXTENDED. CONDUCTED GO AROUND. TROUBLESHOT USING QRH PROCEDURES, USED EMERGENCY GEAR EXTENSION LEVER TO EXTEND NOSE GEAR. EMERGENCY EXTENSION LEVER WOULD NOT STOW. REMOVED AND REPLACED NOSE GEAR BUNGEE ACTUATOR AND NOSE GEAR RETRACT CYLINDER PER B717 AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT STA 200 TO STA 256 LBL 15 CORRODED. REPLACED FLOOR SUPPORT STA 200 TO STA 256 LBL 15, REF B717 SRM 51-41-01 AND 51-41-02.

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: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT DOOR CUTOUT CORRODED. CUT OUT DAMAGED LOWER SECTION AND INSTALLED LOWER SECTION AND SPLICE REPAIR PER REF B717 SRM 53-20-15 REPAIR 6 FIG 201.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FLOOR SEAT TRACK WITH GALLEY SUPPORT ABOVE AT STA 239 RBL 44 CORRODED. CUT OUT DAMAGED SECTION OF FLOOR TRACK RBL 44 FROM STA 200 TO STA 245, INSTALLED NEW TRACK SECTION AND SPLICE REPAIR REF DC9 SRM 53-05 4F AND EA 17-53-01776IR.

Part: SLIDE — OUT OF POSITION (L1 DOOR)

L1 ESCAPE SLIDE FELL OUT OF COMPARTMENT WHEN MAIN DOOR OPENED. REMOVED AND REPLACED L1 DOOR SLIDE REF B717 M/M 25-61-01.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYSTEM)

RIGHT HYDRAULIC QUANTITY LOW ALERT, THEN RIGHT HYDRAULIC SYSTEM FAILURE. REMOVED AND REPLACED AUXILIARY HYDRAULIC PUMP PRESSURE LINE.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR)

R1 DOOR SLIDE DEPLOYED. INSTALLED R-1 DOOR SLIDE IAW AMM 25-61.

Part: SKIN — CORRODED (FUSELAGE)

AFT LOWER CARGO COMP DOOR CUTOUT HAS CORROSION AT LOWER JAMB. INSTALLED PAN AFT CARGO DOOR JAMB IAW B717 SRM 53-20-15.

Part: PAN — CORRODED (AFT CARGO AREA)

AFT CARGO COMPARTMENT DOOR CUT OUT HAS CORROSION OUT OF LIMITS PER SRM 53-00-00. REPLACED LOWER DOOR PAN.

Part: SKIN — DENTED (FUSELAGE)

DENT ON LEFT FUSELAGE AT APPROX FS 256L ABOVE L19 (3" X 1.5" X .033"). INSTALLED REPAIR ON LT SIDE STA 256 ABOVE LONG 19L PER SRM 53-00-01 FIG 204.

Part: TIRE — SEPARATED (NR 3 MLG)

BLOWN RETREAD OFF NR 3 MLG TIRE ON TAKEOFF, FOD DAMAGE. REMOVED AND REPLACED NR 3 TIRE AND WHEEL ASSEMBLY.

Part: ENGINE — FAILED (NR 2)

ENGINE FAILURE ON CLIMBOUT, LOUD BANG. ENGINE RPM LOW, RUNAWAY TGT, STARBOARD ENGINE. REMOVED AND REPLACED NR 2 ENGINE.

Part: BATTERY PACK — UNSERVICEABLE (EXTERIOR)

EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FUSELAGE EMERGENCY LIGHTS. OPS CHECK GOOD B717 AMM 33-51.

Part: DISPLAY — ODOR (COCKPIT)

ELECTRICAL FUMES IN COCKPIT ON TAKEOFF. RETURNED TO AIRPORT. LDG WT 102.5.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND AFT ACCESSORY COMPARTMENT LOWER WALKWAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW 717 AMM 33-51-03.

Part: PCU — DAMAGED (MLG DOOR)

ON TAKEOFF AT ROTATION PFD CLICKED OFF AND ON SEVERAL TIMES THEN WENT BLANK. LOST ALL COMMAND ELECTRICAL. NO PA, NO NR 1 COMM. HAD FIRST OFFICERS PFD AND STATUS PAGE. ISIS OPERATED NORMAL, USED AIRSPEED FROM ISIS, RADIOS WENT DARK AND UNABLE TO GET BACK. UPON WALK-AROUND FOUND LEFT AND RIGHT MAIN LANDING GEAR DOORS DAMAGED. REMOVED AND REPLACED LEFT HAND PCDU AND REMOVED AND REPLACED LEFT AND RIGHT MAIN LANDING GEAR DOORS IAW B717 MM 24-21 AND 32-14.

Part: CONNECTOR — LOOSE (SEAT 17)

SEAT 17 EMERGENCY PATH LIGHTING WOULD NOT ILLUMINATE. RE-SEATED CONNECTOR AT INBOARD SEAT LEG IAW MM 20-31-0, OPERATIONAL CHECK NORMAL.