N608AT

Part: SLIDE — DISLODGED (ZONE 800) · airframe 52,009 hrs · 44,698 cycles

L1 EVACUATION SLIDE COMPARTMENT OPEN, SLIDE DISMOUNTED. INSTALLED L1 DOOR EVACUATION SLIDE IAW AMDS WORKCARD 2561-9004. (7796904)

Part: DOOR — DAMAGED (L1) · airframe 49,819 hrs · 42,761 cycles

CONT OF LOG #693782 L1 DOOR FWD LOWER DOOR DAMAGED. FABRICATED REPAIR DOUBLER AND FILLER PER B717 SRM 52-10-01-2R PROC 1. COMPLETED FWD PASSANGER DOOR LOWER FWD CORNER SKIN REPAIR PER B717 SRM 52-10-01-2R PROC 1 REPAIR 1. A/C OK FOR SERVICE. (LP #0680895)

Part: SKIN — DENTED (L1 DOOR) · airframe 49,819 hrs · 42,761 cycles

RAMP REPORTS DENT ON L1 DOOR BOTTOM FWD CORNER. ATEMPTED TO REWORK/STRAIGHTEN DOOR EDGE PER B717 SRM 52-00-00-2R -3. FOUND CRACK APPOX 1/4" LONG 1/4" FROM BOTTOM OF DOOR. REMOVED DAMAGE AREA OF DOOR SKIN PER B717 SRM 52-10-01-2ER-PROCEDURE 1. ACCOMPLISHED DAMAGE CONTAINMENT HFEC PER B717 NDT PART 6 51-00-01 PROC 2. NO CRACK IND NOTED. QC5289 329603. COMPLETED REPAIR SEE NON ROUTINE CARD 0680895. (LP #6937832)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,254 hrs · 42,256 cycles

AIRCRAFT 9576, EXT OVERHEAD IND NEEDS RELAMPED. CORRECTIVE ACTION: RELAMPED EXT IND OVERHEAD. OPS CK GOOD. (LP 5945559)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,851 hrs · 40,231 cycles

SHIP 9576 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "ANTI-SKID FAIL' MESSAGE ILLUMINATING DURING APPROACH. THE LANDING WAS UNEVENTFUL, AND THE AIRCRAFT TAXIED TO THE GATE. CORRECTIVE ACTION: MAINTENANCE FOUND THE ANTI-SKID CONNECTOR #R5-6020 TO BE LOOSE. ONCE THE CONNECTOR WAS RE-SECURED PROPERLY, THE ANTI-SKID SYSTEM FUNCTIONED NORMALLY. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4950228)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,825 hrs · 40,209 cycles

CORROSION ON INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y 954-994. SUMMARY OF NRC 00180: INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y 954-994 WAS REPAIRED ER/A 610521-14 REV ORIG, SECTION 1 PERMANENT REPAIR. ASSOCIATED ER/A 14-610521 ADDED FOR AC 9576. (LP #2897914)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,825 hrs · 40,209 cycles

CRACK ON FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING. (AD) SUMMARY OF NRC 00051: FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING WAS REPAIRED PER ER/A 610662-14 REV. ASSOCIATED ER/A 14-610662 ADDED FOR AC 9576. (LP #2898258)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,825 hrs · 40,209 cycles

CRACK ON ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR. SUMMARY OF NRC 00198: ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR WAS REPLACED PER DWG 4981366 REV ORIGINAL AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. ALSO TO GET ACCESS TO AREA THE SPOILER HOLD DOWN ACTUATOR WAS REMOVED / INSTALLED PER B717-200 AMM 27-67-06. TEST OK. (LP #2898009)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,825 hrs · 40,209 cycles

CORROSION ON LOWER SILL STRUCTURE BTW STA 954 TO STA 994 OF AFT DOOR AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00089: CORROSION LEVEL 2. LOWER SILL STRUCTURE (DOOR JAMB) BTW STA 954 TO STA 994 OF AFT DOOR AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2894338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,825 hrs · 40,209 cycles

CRACK WAS FOUND ON LH OVERWING FRAME STA Y=696, GREATER THAN 0.125IN IN REF TASK CARD 5310-01436-01B JOB #078-0002 STEP 10. SUMMARY OF NRC 00181: LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 TASK CARD 5310-01436-03A JOB 107-0001. ASSOCIATED AA 5310-01436 ADDED FOR AC 9576. (LP #2891795)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,825 hrs · 40,209 cycles

CORROSION AT ANGLES (2 EA) WAS FOUND DURING DOOR JAMB DISASSEMBLY. SUMMARY OF NRC 00196: CORROSION LEVEL 2. ANGLES (2 EA) WERE FABRICATED AND INSTALLED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 AND 51-41-05-0G. (LP #2886801)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,825 hrs · 40,209 cycles

CORROSION ON LOWER DOOR JAMB AT FWD CARGO COMPARTMENT BTW STA Y370 AND STA Y427 (INNER AND OUTER SIDE). SUMMARY OF NRC 00081: CORROSION LEVEL 2. LOWER DOOR JAMB AT FWD CARGO COMPARTMENT BTW STA Y370 AND STA Y427 WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2888223)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,825 hrs · 40,209 cycles

CRACK WAS FOUND ON EDGE OF CUSP MEMBRANE. SUMMARY OF NRC 00190: CUSP MEMBRANE WAS FABRICATED PER B717 SRM 53-00-55-2R-4 TABLE 2 AND INSTALLED WITH CARD 5310-01436-02B " AD". ASSOCIATED AA 5310-01436 ADDED FOR AC 9576. (LP #2882958)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,825 hrs · 40,209 cycles

DURING LH CUSP MEMBRANE STA 655-715 REMOVAL, CRACK WAS FOUND ON EDGE. SUMMARY OF NRC 00192: LH CUSP MEMBRANE STA 655-715 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 203. ASSOCIATED AA 5310-01436 ADDED FOR AC 9576. (LP #2876206)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,825 hrs · 40,209 cycles

CORROSION ON AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00563: CORROSION LEVEL 2. AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT WERE FABRICATED PER B717-200 SRM 53-20-15-2R PROC 7 AND INSTALL SPLICE IS ACCOMPLISH NRC 00240. (LP #2872784)

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 45,457 hrs · 39,017 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING. EXIT SIGN AT 1ST CLASS BULKHEAD MISSING THE ENTIRE LIGHT COVER. MAINTENANCE DETERMINED THAT ONLY THE EXIT SIGN COVER TO BE MISSING. LOCATED IN AN OVERHEAD BIN AND RE-INSTALLED THE COVER IAW AMM 33-51. OPS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (AFT CARGO) · airframe 45,157 hrs · 38,751 cycles

SHIP 9576 -ATB- DUE TO A CABIN INFLOW MESSAGE. CORRECTIVE ACTION: MAINTENANCE ADJUSTED THE AFT CARGO DOOR, PERFORMED A SUCCESSFUL DECAY CHECK AND RETURNED TO SERVICE.

Part: NONE — NONE · airframe 44,581 hrs · 38,227 cycles

THE F/A REPORTS THAT THE 1R DOOR GIRT BAR KEEPS SLIPPING OUT WHEN IN THE ARMED POSITION DURING FLIGHT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE DOOR 1R RH GIRT BAR FITTING PER B717 AMM 25- 61. VERIFIED GIRT BAR FLOOR FITTING LATCH WAS INSTALLED PER B717 AMM 25-61. OPERATIONAL CHECK WAS GOOD. (LP #8829568)

Part: SCUFF PLATE — DAMAGED (CARGO DOOR) · airframe 43,929 hrs · 37,643 cycles

FOUND AFT CARGO DOOR EXTERIOR SCUFF PLATED DAMAGED. FWD EDGE PULLED AWAY FROM FUSELAGE. INSPECTED AREA AROUND SCUFF PLATE, NO OTHER DAMAGE NOTED TO SKIN OR CARO DOOR REF B717 AMM 52-31. PERFORMED TEMP REPAIR OF SCUFF PLATE PER ER/A 598362-14 REV ORIGINAL. PERMENANT REPAIR DUE WITHIN 30 DAYS AND PRIOR TO CLOSING LOG. (LP #8542250)

Part: NOT REPORTED — NOT REPORTED · airframe 43,879 hrs · 37,596 cycles

THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS AND TAIL EXIT IDENTIFIER ARE INOPERATIVE. MAINTENANCE DETERMINED THAT THE POWER SUPPLY, B5-119, WAS INOPERATIVE. THE POWER SUPPLY AND BATTERY WERE REPLACED PER B717 AMM 33- 51-03. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #8542226)

Part: NONE — NONE · airframe 46,022 hrs · 39,499 cycles

ERA 586819-14AD INSTALLED A REPAIR STRAP COMMON TO RH SPAR CAP O N VERTIAL STABILIZER, ERA REVISION A IS CURRENT. ACCOMPLISH ERA 586819-14AD REV A SECTION II AT 4600 CYCLES AFTER SECTION I, THEN 2400 CYCLE INTERVALS THEREAFTER. ASSOCIATED AA 5530-01048 ADDED FOR AC 9576. ASSOCIATED ER/A 00-586819 ADDED FOR AC 9576. ERA 586819-14AD REV B IS CURRENT. NO CHANGES TO FOLLOW ON ACTION SCHEDULING. COMPLETED DVI AND HFEC PER ERA 586819-14AD REV B SEC II. NO DEFECTS NOTED. RESTORED FINISH PER ERA 586819-14AD REV B SEC II. MONITORED ASSY A/C: Y ENG POS: APU: LRU: 95-2000-9-0001 SER: 09576 MON, 95 REP, 2068607; 2400C; HFEC; ERA 586819-AD; 09576 00-0555-8-0480 09576 X 11APR23 215.00 L (LP #2068607)

Part: WIRE — SHORTED (PUMP CONNECTOR) · airframe 41,621 hrs · 35,647 cycles

THE AIRCRAFT WAS RETURNED TO THE GATE DUE TO THE LEFT AFT BOOST PUMP CIRCUIT BREAKER TRIPPING WITH REPORTED SMOKE AND ODOR. CORRECTIVE ACTION: MAINTENANCE FOUND R5-6001 CONNECTOR WIRES SHORTED. R5-6001 WAS REPLACED, PER SWPM 20-31-15. BONDING CHECK WAS GOOD, PER SWPM 20-50-01. OPERATIONAL CHECK OF THE LEFT AFT & FORWARD PUMPS AND THE LEFT WING LIGHTS WAS NORMAL. COMPLIED WITH SFAR88/CDCCL, PER B717 AMM 28-22.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,241 hrs · 35,335 cycles

MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE OVER WING EXIT ROW 21 WERE INOPERATIVE. THE BATTERY, B5-230, WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: LANYARD — BROKEN (L1 GIRT BAR) · airframe 41,073 hrs · 35,169 cycles

THE GIRT BAR CABLE LANYARD AT L1 DOOR BROKE. MAINTENANCE REPLACED DAMAGED LANYARD ASSY FROM L1 DOOR, PER B717 AMM 25-61-03. NO RII.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 40,459 hrs · 34,608 cycles

DURING OPN 5530-01048-02 STEP 14, OPEN HOLE HFEC FOUND CRACK INDICATION IN BOLT HOLE ON RH VERT STAB FRONT SPAR CAP. 1ST HOLE UP FROM SPLICE. DISCONNECTED UPPER AND LOWER ANTENNA ON VERT STAB. ALL FURTHER MAINTENANCE COMPLIED WITH ON PRI / ER/A 586819-14AD AND AMDS CARD 5530-01048-02. (LP #1557404)

Part: NONE — NONE · airframe 43,551 hrs · 37,313 cycles

ER/A 586819-14AD REV ORIGINAL HAS BEEN ISSUED FOR CRACKING DISCOVERED DURING ACCOMPLISHEMENT OF AMDS WC 5530-01048-02. THE SUBJECT SECTION I REPAIR IS TIME LIMITED. FOLLOW ON ACTION REQUIRED. ASSOCIATED ER/A 95-586819 ADDED FOR AC 9576. ERA 586819-14AD REV A IS CURRENT. REF NEW LP 2068607, THIS LOG MAY BE CLOSED. ASSOCIATED AA 5530-01048 ADDED FOR AC 9576. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 30DEC21 AND LOG COMMENTS. (LP #1557381)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,527 hrs · 33,872 cycles

THE 01C CEILING EMERGENCY LIGHT COVER IS MISSING. MAINTENANCE REPLACED THE 01C EMERGENCY ESCAPE LIGHT LENS PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. MCO/PLACARD REMOVED. (LP #1364543)

Part: PANEL — CRACKED (LT WING SPOILER)

HIDDEN CRACK ON O/B SPOILER PANEL NEAR TO HINGE FITTING.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 38,416 hrs · 33,050 cycles

CORROSION ON AREA SETTLEMENT AND COUNTERSUNK AT FUEL TANK ACCESS PLATES #620FT, 620LB, AND 620DB ON RT WING (AD). NRC 00368: CORROSION LEVEL 2, CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK ACCESS PLATES #620 FT, 620LB, AND 620DB OF RT WING WERE REPLACED AND PART NUMBERS VERIFIED PER IPC 57-22-01-01 ITEMS 15, 220, AND 430. (LP #1092423)

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 38,416 hrs · 33,050 cycles

ELONGATED HOLES ON FUEL TANK ACCESS PLATE #520LB ON LT WING (AI). NRC 00365: ACCESS PLATE WAS REWORKED WITH COUNTERSINK BUT THE EXCESSIVE DAMAGE IS OUT OF LIMITS PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II. FUEL ACCESS PLATE #520LB WAS REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-23-01-01 ITEM 220. (LP #1092448)

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,416 hrs · 33,050 cycles

CRACK AT FUSELAGE SKIN STA 1133 BETWEEN LONG 2/3 RT. (FUS). CRACK WAS REPAIRED PER ETI-17-19-065 R4 AND ER/A 578449-14AD REV. ORIGINAL. ASSOCIATED ER/A 00-578449 ADDED FOR AC 9576. (LP #1091843)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,416 hrs · 33,050 cycles

CORROSION ON AREA SETTLEMENT AND COUNTERSUNK AT FUEL TANK ACCESS PLATES #520DB, 520CB, AND 520DT ON LT WING (AI). NRC 00363: CORROSION LEVEL 2, CORROSION ON FUEL TANK ACCESS PLATES #520DB, 520CB, AND 520DT ON LT WING WERE REPLACED AND PART NUMBERS VERIFIED PER IPC 57-23-01-01 ITEMS 15, 430, AND 465. (LP #1092427)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,416 hrs · 33,050 cycles

CORROSION ON RT TIE TRACK FROM STA Y=813 TO Y=954 AND STA Y=994 TO Y=1028 IN REF AMDS 5314-2001. (CCT). NRC 00253: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER SRM 51-41-01-0G. (LP #1091207)

Part: PANEL — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON RT HORIZONTAL STABILIZER LE PANEL #340DT (EHV). NRC 00170: CORROSION LEVEL 2, RT HORIZONTAL STABILIZER LE PANEL #340DT WAS REPAIRED PER ETI -17-19-073 REV. ORIGINAL AND ER/A 578193-14 REV ORIGINAL. ASSOCIATED ER/A 14-578193 ADDED FOR AC 9576 (LP #1086463)

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK AT FUSELAGE SKIN STA 1076 BETWEEN LONG 13/14 RT. (FUS). NRC 00128: FUSELAGE SKIN STA 1076 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-063 R2 AND ER/A 578372-14 REV. ORIGINAL. SECTION I. ASSOCIATED ER/A 00-578372 ADDED FOR AC 9576 (LP #1086983)

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG 13/14 RT. (FUS). NRC 00126: FUSELAGE SKIN STA 1022 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-064 R3 AND ER/A 578307-14 REV. ORGINAL. ASSOCIATED ER/A 00-578307 ADDED FOR AC 9576 (LP #1086861)

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK AT FUSELAGE SKIN STA 1037 BETWEEN LONG 13/14 RT. (FUS). NRC 00127: FUSELAGE SKIN STA 1037 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-064 R3 AND ER/A 578307-14 REV. ORGINAL. ASSOCIATED ER/A 00-578307 ADDED FOR AC 9576. (LP #1086863)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON AFT BULKHEAD PANEL LOWER SUPPORT STA Y=1028 BTW LONG 23L TO 23R IN REF. AMDS 5314-2001. (CCT) NRC 00259: CORROSION LEVEL 2, AFT BULKHEAD PANEL LOWER SUPPORT STA Y=1028 BTW LONG 23L TO 23R WAS REPAIRED PER SRM 53-00-00-2R-1 FIG 201. (LP #1085882)

Part: SKIN — WORN (EMERGENCY EXIT) · airframe 38,415 hrs · 33,049 cycles

WEAR AT AFT EMERGENCY EXIT DOOR SKIN ON LOWER LT/RT SIDES. (PTAS). NRC 00314: SPLICE ANGLE AT AFT EMERGENCY EXIT DOOR ON LOWER LT SIDE WAS REPLACED AND INNER ANGLE AT AFT EMERGENCY EXIT DOOR ON LOWER RT SIDE WAS REPAIRED PER SRM 52-10-02-2R REPAIR 16, 51-41-02-0G, 51-41-05-0G, AND DWG #9929480 REV. BW. (LP #1086784)

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 38,415 hrs · 33,049 cycles

CRACK RT MLG DOOR NEXT TO LATCH FITTING DOOR (FYT). NRC 00386: INNER SKIN OF THE RT MLG DOOR NEXT TO LATCH FITTING DOOR WAS REPAIRED PER ER/A 578325-14 REVISION ORIGINAL AND ETI-17-19-069 REVISION 2. ASSOCIATED ER/A 14-578325 ADDED FOR AC 9576. (LP #1086773)

Part: GUSSET — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK ON GUSSET STA 1022 LONG 7L. (CPAX). NRC 00370: GUSSET STA 1022 LONG 7L WAS REPAIRED PER ETI-17-19-067 R1 AND ER/A 578227-14 REV ORIGINAL. ASSOCIATED ER/A 14-578227 ADDED FOR AC 9576. (LP #1084843)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON OUTBOARD F/O SEAT TRACK. (CPIL). NRC 00423: CORROSION LEVEL 2, OUTBOARD F/O SEAT TRACK WAS REPLACED PER SRM 51-41-01-0G. (LP #1076941)

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK ON AFT BULKHEAD FITTING SUPPORT ABOVE LONGERON 24L AT FWD CARGO COMPARTMENT (CCD). NRC 00395: FITTING SUPPORT WAS REPLACED PER SRM 51-41-05-0G. (LP #1076667)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON FLOOR SUPPORTS FROM STA 200/157 AND X0/X56. (CPAX). NRC 00426: CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=157-200, X=56, Y=157-200, X=44, Y=190-200, X=54, AND Y=196, X=22 TO X=44 WERE REPLACED PER SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #1073591)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON RT CUSP WEB FROM STA 389 TO 427 AT PAX CABIN (CPAX). NRC 00208: CORROSION LEVEL 2, CUSP WEB FROM STA 389 TO 541 WAS REPLACED PER SRM 51-41-02-0G, SRM 51-41-01-0G, AND SRM 51-41-05-0G. (LP #1074893)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON FLOOR WEB BETWEEN STA 200/190 AND X0/X56 (CPAX). NRC 00427: CORROSION LEVEL 2, FLOOR WEBS ON STA Y=200 TO Y=190 AND X=0 TO X=56 WERE REPAIRED PER SRM 51-70-10-2R. (LP #1073569)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON AREA SETTLEMENT AND COUNTERSUNK AT FUEL TANK ACCESS PLATES 520CT AND 620CT ON LT/RT WING (AI)(AD). NRC 00366: CORROSION LEVEL 2, FUEL ACCESS PLATES 520CT AND 620CT WERE REPLACED PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. PART NUMBER VERIFIED PER IPC 57-22-01. (LP #1071891)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON LONG 29L FROM STA Y=907 TO Y=954, ALSO ON LONG 28R STA Y=889 AT AFT CARGO COMPARTMENT IN REF 5314-2001. (CCT). NRC 00243: LONGERON 29L SECTION FROM STA 907 TO Y=954 WAS REPLACED PER SRM 53-20-05-2R-1. (LP #1068927)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION LOWER AREA OF AFT CARGO COMPARTMENT DOOR JAMB IN REF 5300-2007. (CCT). NRC 00230: CORROSION LEVEL 2, AFT CARGO COMPARTMENT DOOR JAMB PAN WAS REPLACED PER SRM 51-41-02-0G, 51-41-05-0G, 51-41-01-0G, AND 53-20-15-2R-7. (LP #1068577)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK ON LONGERON 5R STA 1022. (CPAX). NRC 00371: CRACK ON LONGERON 5R STA 1022 WAS REPAIRED PER SRM 53-00-05-2R. (LP #1067709)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK ON RT CUSP WEB BTW STA 851-870 AT PAX CABIN (CPAX). NRC 00204: CUSP WEB WAS REPAIRED BTW STA 851 TO 870 RT AT PAX CABIN PER SRM 53-00-55-2R-4. (LP #1068823)

Part: FORMER — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACKED CANTED KEEL FORMERS (3EAS) RT SIDE FROM STA Y=674 TO Y=715.(FYT). NRC 00328: CANTED KEEL FORMERS (3EAS) RT SIDE WERE REPAIRED PER SRM 51-70-11-2R REP 1. (LP #1068767)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON FLOOR SUPPORTS X7/X-7 BETWEEN STA 200/149 (CPAX). NRC 00430: CORROSION LEVEL 2, FLOOR SUPPORTS X7/X-7 BETWEEN STA 200/149 WERE REPLACED PER SRM 51-41-01-OG. ORIGINAL THICKNESS IS 0.125" AND REMAINING THICKNESS IS 0.080". THEREFORE ITS OUT OF LIMITS PER SRM 53-00-00-1A FIG. 103. (LP #1068829)

Part: FORMER — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACKED CANTED KEEL FORMERS (3EAS) LT SIDE FROM STA Y=674 TO Y=715.(FYT). NRC 00329: CANTED KEEL FORMERS (3EAS) LT SIDE FROM STA Y=674 TO Y=715 WERE REPAIRED PER SRM 51-70-11 FIG 201 REP 1. (LP #1068776)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB FROM STA 382 TO STA 389 AT PAX CABIN (CPAX). NRC 00504: CORROSION LEVEL 2, CORROSION ON RT CUSP WEB FROM STA 382 TO STA 389 WAS REPAIRED PER SRM 51-70-10 2R PROCEDURE 2. (LP #1067507)

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

TWO HOLES WERE FOUND ON THE RT CUSP WEB STA 351 (CPAX). NRC 00502: TWO HOLES ON RT CUSP WEB STA 351 (CPAX) WERE REPAIRED PER SRM 53-00-55-2R-4 FIG 211. (LP #1067245)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

CORROSION ON FLOOR SUPPORT STA Y=180, X=-7 TO X=-44 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-00-1A. NRC 00518: CORROSION LEVEL 2, FLOOR SUPPORT STA Y=180, X=-7 TO X=-44 WAS REPLACED PER SRM 51-41-02-0G. (LP #1067038)

Part: PAN — CRACKED (PAX DOOR) · airframe 38,415 hrs · 33,049 cycles

CRACK ON FWD PASSENGER DOOR PAN AFT/UPPER CORNER (L1). NRC 00069: CRACK WAS REPAIRED PER SRM 52-10-02-2R REPAIR 3. (LP #1065730)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,415 hrs · 33,049 cycles

DELAMINATED FLOOR PANELS 221QF AND 221VF, PAX CABIN (CPAX). NRC 00377: FLOOR PANEL 221QF AND 221VF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1063276)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,415 hrs · 33,049 cycles

DELAMINATED FLOOR PANEL 223FF, PAX CABIN (CPAX). NRC 00384: FLOOR PANEL 223FF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1063300)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,415 hrs · 33,049 cycles

FLOOR SUPPORT STA 130 BTW X-44 TO X-52 HAD EXCESSIVE CORROSION THAT WHEN REMOVED, WAS FOUND TO BE OUT OF LIMITS(CPAX). NRC 00515: CORROSION LEVEL 2, FLOOR SUPPORT STA 130 BTW X-44 TO X-52 (W1) (CPAX) WAS REPLACED PER SRM 51-41-02-0G. (LP #1063594)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,415 hrs · 33,049 cycles

FLOOR PANEL CRACKED 221LF. PAX CABIN (CPAX). NRC 00378: FLOOR PANEL 221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1064008)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,415 hrs · 33,049 cycles

FLOOR PANELS 222ABF, 222CF, AND 222DF ARE CRACKED. PAX CABIN (CPAX). NRC 00381: FLOOR PANEL 222ABF, 222CF, AND 222DF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1064016)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,415 hrs · 33,049 cycles

DELAMINATED FLOOR PANELS 222TF, 222WF, AND 222ARF PAX CABIN (CPAX). NRC 00382: FLOOR PANEL 222TF, 222WF, AND 222ARF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1063293)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,415 hrs · 33,049 cycles

CRACK ON RT CUSP WEB BTW STA 813-832 AT PAX CABIN (CPAX). NRC 00205: RT CUSP WEB BTW STA 813-832 WAS REPLACED PER SRM 51-41-02. (LP #1064564)

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 38,415 hrs · 33,049 cycles

THE COCKPIT FLOOR PANEL 211ANF IS DELAMINATED (CPIL). NRC 00374: FLOOR PANEL 211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1063106)

Part: CLAMP — LOOSE (AIR/GROUND) · airframe 34,600 hrs · 30,353 cycles

DIVERTED THE AIRCRAFT DUE TO A CABIN ALTITUDE WARNING MESSAGE. A YELLOW EMERGENCY WAS DECLARED, THE QRH WAS COMPLIED WITH, AND A FLIGHT IDLE, SPOILER DEPLOYED DESCENT TO 11,000 FEET WAS ACCOMPLISHED. MAINTENANCE FOUND THAT THE GROUND AIR CONNECTION DUCT CLAMP IN THE TAIL CONE WAS LOOSE. THE CLAMP WAS SECURED. MAINTENANCE WAS ABLE TO RECERTIFY THE PRESSURIZATION SYSTEM. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: DUCT — SEPARATED (A/C PACK) · airframe 34,480 hrs · 30,285 cycles

F/A REPORTED A STRONG BURNING ODOR AND SMALL WHITE PARTICLES BLOWING OUT OF DUCTS. FOUND A BLOWN A/C DUCT ABOVE SEAT ROW 29. ATTACHED THE DUCT. LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,295 hrs · 30,169 cycles

FOUND THE AFT EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW FIM 33-50-00 810-801. FOUND EMERGENCY FLOOR LIGHTS POWER SUPPLY BATTERY B5-119 INOPERATIVE. REPLACED THE BATTERY PER B717 AMM 33-51-03. OPS CHECKED OK. AIRCRAFT IS OK FOR SERVICE.

Part: SKIN — CRACKED (BS 1087) · airframe 33,462 hrs · 29,550 cycles

FUSELAGE SKIN HAS HAS A .750 LONG CRACK THRU FASTENER HOLE AT BS 1087, 2.5 INCHES ABOVE SKIN LWR EDGE, NEAR LONGERON 14R. HFEC IAW NDT SPM. NR 001-0229:5300-2019/010 00062. REPAIRED IAW PRI 558866-14, REVISION 0, AND ER/A 558866-14, REV ORIGINAL.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 33,462 hrs · 29,550 cycles

VERTICAL STAB LE AT ZFS 52 HAS MANY WORN FASTENER HOLES, COUNTER SINKS, AND LOOSE FASTENERS. LT & RT SIDES, ABOVE & BELOW THE SEAM. REPAIRED IAW PRI 558868-14, REV 0.

Part: CONTROL VALVE — MALFUNCTIONED (SLAT SYSTEM) · airframe 30,897 hrs · 27,662 cycles

DURING SLAT EXTENSION SLAT DISAGREE MSG ENUNCIATED AND ACFT ROLLED TO THE RT. FLIGHT CREW DECLARED AN EMERGENCY, FOLLOWED QRH PROCEDURES NO SLATS NO FLAP LANDING. MAINTENANCE R & R SLAT CONTROL VALVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,643 hrs · 27,457 cycles

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

Part: ELEVATOR SYSTEM — MALFUNCTIONED · airframe 28,971 hrs · 26,170 cycles

DUE TO A ELEVATOR SPLIT MESSAGE AFTER TAKEOFF. AN EMERGENCY WAS DECLARED. PERFORMED TROUBLESHOOTING IAW FIM 27-30. FCC 2 ELEVATOR POSITION READINGS WERE INCONSISTANT WITH FCC NR 1. SWAPPED FCC'S AND PROBLEM FOLLOWED. RETURNED FCC'S TO ORIGINAL POSITIONS. REPLACED FCC NR 2 AND ALL ELEVATOR POSITION READINGS WERE WITHIN TOLERANCE IAW AMM. ACCOMPLISHED NR 1 & NR 2 FCC AUTOLAND TESTS WITH POSITIVE RESULTS.

Part: LENS — MISSING (CABIN) · airframe 28,793 hrs · 26,015 cycles

AFT CEILING EMER LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,793 hrs · 26,015 cycles

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

Part: WIRE — LOOSE (AC BAY) · airframe 28,793 hrs · 26,015 cycles

TAIL COMPARTMENT CTR OVERHEAD EMER LIGHT WIRE LOOSE. SECURED WIRE IAW SWPM.

Part: HOUSING — CRACKED (R1 DOOR) · airframe 27,686 hrs · 25,251 cycles

R1 DOOR EMER EXIT IDENTIFIER LOWER AFT OF R1 DOOR HOUSING ASSEMBLY CRACKED. R & R LIGHT IAW AMM.

Part: TAB — DEBONDED (RT AILERON) · airframe 27,686 hrs · 25,251 cycles

RIGHT WING AILERON CONTROL TAB DEBONDED AT TE. R & R TAB IAW MM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

RIGHT MAIN CABIN CUSP WEB CRACKED BETWEEN BS 635 - 715. REPAIRED CUSP WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 256 BETWEEN LONGERON 29L & 30. R & R SHEAR TIE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

MAIN CABIN SEAT TRACK CORRODED AT BS 927, RBL 22. R & R SEAT TRACK IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

RIGHT CUSP WEB CRACKED AT STATION 387 - 408. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

LEFT CUSP WEB UPPER SURFACE CORRODED BETWEEN BS 636 - 656. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

LEFT CUSP WEB UPPER SURFACE CORRODED BETWEEN BS 446 - 465. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

LEFT CUSP WEB CORRODED AT STATION 851 - 870. REPAIRED CUSP WEB IAW EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO COMPARTMENT LT FWD CARGO FLOOR TRACK CORRODED AT STATION 218 - 370. R & R TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO COMPARTMENT FRAME AFT LOWER FLANGE CORRODED AT BS 294, BETWEEN LONGERON 29L TO LONGERON 29R. R & R FLANGE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO COMPARTMENT FRAME AFT LOWER FLANGE CORRODED AT BS 332, BETWEEN LONGERSON 28L - 28R. R & R FLANGE IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO COMPARTMENT RT FWD CARGO FLOOR TRACK CORRODED AT STATION 579 - 655. R & R TRACK IAW SRM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 27,686 hrs · 25,251 cycles

L1 DOOR UPPER FRAME CRACKED AT AFT EDGE. R & R FRAME IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO INTERCOSTAL ATTACH CLIP CRACKED AT BS 236. R & R CLIP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

FORWARD CARGO STATION 236 RT INTERCOSTAL ATTACH CLIP CRACKED. R & R CLIP IAW SRM.

Part: SIGN — BROKEN (ROW 1) · airframe 27,686 hrs · 25,251 cycles

THE CENTER AISLE EXIT SIGN IS BROKEN AT ROW 1. R & R THE SIGN ASSY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

C1 DOOR SURROUND STRUCTURE INSIDE AFT WEB ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 27,686 hrs · 25,251 cycles

C1 DOOR PAN CRACKED AT AFT LATCH CAM. REPAIRED PAN IAW EA.

Part: SUPPORT FITTING — CORRODED (R1 DOOR) · airframe 27,686 hrs · 25,251 cycles

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

Part: ANGLE — CRACKED (WING) · airframe 27,686 hrs · 25,251 cycles

CENTER WING FRONT SPAR TOP CTR TIME ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

MAIN CABIN SEAT TRACK SUPPORT FITTING CRACKED AT BS 737, LBL 44. R & R FITTING IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

MAIN CABIN SEAT TRACK SUPPORT FITTING CRACKED AT BS 737, RBL 44. R & R FITTING IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

AFT CARGO COMPARTMENT LOWER FRAME TO FUSELAGE SKIN SHEAR CLIP CORRODED AT BS 1002, BETWEEN STRINGER 30 - 30R. R & R SHEAR CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

RIGHT WING FUSELAGE EXTERIOR WING TO BODY FITTING CRACKED AT STRINGER 22. REPAIRED FITTING IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 27,686 hrs · 25,251 cycles

LEFT SEAT TRACK CUSP WEB CRACKED BETWEEN BS 655 - 715. R & R CUSP WEB IAW EA.

Part: RETAINER — BROKEN (L1 DOOR) · airframe 26,809 hrs · 24,706 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER BROKEN. R & R RETAINER IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 26,794 hrs · 24,695 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. R & R COVER IAW AMM.

Part: CYLINDER — FAULTY (NLG WW) · airframe 259,160 hrs · 24,128 cycles

ON INITIAL EXTENSION OF LG THE NOSE GEAR DID NOT COME DOWN. THE MAIN DID COME DOWN, WITH TWO GREEN LIGHTS, THE NOSE GEAR LIGHT REMAINED RED, WE CYCLED THE GEAR & ALL 3 CAME DOWN LIKE NORMAL. R&R NOSE LANDING GEAR BOGIE CYLINDER IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 24,768 hrs · 23,415 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 24,511 hrs · 23,256 cycles

L1 SLIDE NOT SECURE. REPLACED L1 DOOR SLIDE PER AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

GALLEY WEB HAD CORROSION AT STA 200 TO 218 RBL 25. R & R IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

CARGO DOOR JAMB LOWER HAD CORROSION. R & R PAN IAW SRM.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

MAIN CABIN - CORROSION ON FLOOR SUPPORT AT STA 200 LBL 2, LBL 21 AND LBL 29. REMOVED, FABRICATED AND INSTALLED NEW FALSE TRACK AT STA 200 RBL 7, IAW B717 SRM 51-41-01, 51-10-04 AND DRAWING 9936534.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

MAIN CABIN SEAT TRACK HAD CORROSION ON SEAT TRACK AT STA 256 TO 246, RBL 54. R & R SEAT TRACK IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

MAIN CABIN - STIFFENER CRACKED AT STA 218 LONG 15L. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER AND FILLER ON MAIN CABIN STIFFENER IAW B717 SRM 51-70-10 REPAIR 2 AND 51-10-04.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

MAIN CABIN - WEB CRACKED AT STA 229 RBL 38. REMOVED CRACKED CUSP WEB SECTION AT STATION 229 AND RBL 44, FABRICATED AND INSTALLED NEW REPAIR SECTION IAW B717 SRM 53-20-51 FIG 1, 51-41-02, 53-00-55 REPAIR 4 AND 51-10-04

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,878 hrs · 22,869 cycles

MAIN CABIN HAD CORROSION ON SEAT TRACK AT STA 229 TO 256 RBL 24. R & R SEAT TRACK IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,878 hrs · 22,869 cycles

RIGHT EMERGENCY BATTERY PACK INOP AT SEAT ROW 21. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 23,737 hrs · 22,778 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER AMM.

Part: SLIDE — DEFECTIVE (TAIL) · airframe 22,943 hrs · 22,247 cycles

TAIL ASSEMBLY EMERGENCY EVAC SLIDE GAUGE UN-READABLE. EMERGENCY T-HANDLE ON SLIDE LOOSE. REMOVED AND REPLACED TAIL CONE SLIDE ASSY AS PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,688 hrs · 22,065 cycles

RIGHT EEPLS INOP AT ROW 10. REMOVED AND REPLACED BATTERY SUPPLY CHARGER PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,688 hrs · 22,065 cycles

RIGHT EEPLS INOP BETWEEN ROW 1 TO ROW 3. REMOVED AND REPLACED BATTERY SUPPLY CHARGER PER AMM.

Part: SKIN PANEL — PUNCTURED (VERTICAL STAB)

VERTICAL FIN LEADING EDGE TOP CAP SKIN PANEL, PUNCTURED. ACCOMPLISHED TOP CAP SKIN PANEL REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS ON CATWALK IN TAIL CONE AND ABOVE BULKHEAD DOOR DO NOT WORK. T/S PER FIM 33-50 TASK 801. FOUND POWER SUPPLY B5-260 INOP. REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-03. ALL EMERGENCY / LIGHT NOW CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SHORTED OUT AFT CABIN EMERGENCY FLOOR PATH LIGHTING BATTERY POWER SUPPLY RELAMPING A SEAL LIGHT. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW 717 MM 33-51, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR PATH LIGHT OUT AT SEAT 28. RELAMPED FLOOR PATH LIGHT AT SEAT 28 IAW 717 AMM 33-51, OPS NORMAL.

Part: LOCK — DEFECTIVE (RT MLG DOOR)

GEAR DOOR OPEN AFTER GEAR RETRACTION ON CLIMBOUT RT MAIN GEAR DOOR DISPLAYS RED WITH HANDLE UP. REMOVED AND REPLACED HARDWARE FOR RT MLG DOOR LATCH ASSY. REMOVED AND REPLACED LOCK ASSY RT MLG DOOR IAW B717MM 32-34-01 AND / CMM 32-31-10 RESPECTIVELY. PERFORMED OPS CHECK/CYCLED LANDING GEAR, OPS CHECKS NORMALLY, LIGHTS OPS CHECK GOOD REF B717MM / 07-11-00.

Part: LIGHT — SHORTED (CABIN)

EMERGENCY LIGHTS AT ROW 1, 2 AND 3 INOP. FOUND LAMPS AT ROW 2 SHORTED. RELAMPED AND REPLACED POWER SUPPLY B5-118 . SYSTEM POS CHECKED GOOD REF MM 33-51.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN)

FOUND AFT FUSELAGE EMERGENCY LIGHTS TO REMAIN ON IN THE OFF POSITION AND ON IN THE ARMED POSITION. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY IAW B717 AMM 33-51-06, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

O/W EXIT EMERGENCY LIGHT AT FLOOR WILL NOT ILLUMINATE BOTH SIDES AFT EXIT. REPLACED POWER SUPPLY AT STA 803 OPS CK GOOD REF AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND EMERGENCY LIGHTS ON SEATS 20 TO AFT ROW INOP. FOUND EMERGENCY LIGHT POWER SUPPLY INOP B5-110. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD REF 33-51.