N934AT

Part: STRAP — DAMAGED (ZONE 500) · airframe 58,759 hrs · 43,030 cycles

COMPLY WITH ER/A 626909-14AD SECTION IV LT WING REAR SPAR LOWER STRAP REPAIR. COMPLIED WITH ER/A 626909-14AD REV. E SECTION IV AND PRI 626909- 14AD REV. E REV 0 - 4. LH WING REAR SPAR LOWER STRAP REPAIR. (1212786)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 58,759 hrs · 43,030 cycles

LEFT WING REAR SPAR, LOWER CAP, AFT FLANGE CRACKED NEAR XRS = 164. REPAIRED PER ER/A 00-626909. (1156447)

Part: GIRT BAR — DETACHED (ZONE 800) · airframe 58,343 hrs · 42,667 cycles

SHIP 9565 GIRT BAR DETACHED FROM 1R DOOR. CORRECTIVE ACTION: RE ATTACHED LANYARD ASSY. IAW 717 AMM 25-61 (6588676)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 58,281 hrs · 42,606 cycles

AIRCRAFT 9565, WHILE MAINTENANCE IN DTW WAS ACCOMPLISHING AA WORKCARD 5720-01103-01A, MTC DISCOVERED A CRACK COMMON TO THE LH WING LOWER SPAR CAP (P/N 5911301-507), COMMON TO THE LH WING REAR SPAR INSTL (P/N 9910010-511) AFT FLANGE NEAR XRS 164.000. CORRECTIVE ACTION: REPAIR STRAP TO BE INSTALLED ON AFT TANG UPPER SURFACE. FABRICATED ONE (1 QTY) TAPERED SHIM TO BE USED UNDER THE HORIZONTAL FLANGE OF THE 9957454-9 RIB CLIP. INSTALLED REPAIR PARTS AND FASTENERS PER 717 SRM 51-40-02 AND ER/A 626909-14AD. (LP 6588638)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 58,281 hrs · 42,606 cycles

SHIP 9565 CRACK FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP AFT LEG. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REF FC 5720-01103. BOLT LOCATION XRS158. CRACK AT 1OCLOCK POS LOOKING DOWN ON BOLT AND IS 3/8" FROM CENTER OF BOLT. CORRECTIVE ACTION: REPAIRED PER 626648-14 REV 3 (0994229)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,533 hrs · 41,947 cycles

THE EMERGENCY LIGHTS ARE INOPERATIVE AT THE FWD LIGHT ATTENDANT STATION. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IN THE AFT CARGO COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733983)

Part: CONTROL VALVE — MALFUNCTIONED (SLAT SYSTEM) · airframe 55,511 hrs · 40,170 cycles

SHIP 9565 -ATB/DE- THE CREW PERFORMED AN AIR TURNBACK AND DECLARED AN EMERGENCY WITH ATC DUE TO A SLAT DISAGREE. THE AIRCRAFT REQUIRED SIGNIFICANT AILERON CORRECTION FOR WINGS LEVEL ATTITUDE. THE QRH WAS COMPLIED WITH, AND THE RESULT WAS A NORMAL SLAT EXTENSION FOR A NORMAL APPROACH AND LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE SLAT CONTROL VALVE AND RETURNED THE AIRCRAFT TO SERVICE. (LP #5603766)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

ELONGATED HOLES ON FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE. (IN REF TO NRC: 00238). SUMMARY OF NRC 00298: FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE WAS REPAIRED PER ER/A 613199-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613199 ADDED FOR AC 9565. (LP #0096881)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

WEAR ON LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING. SUMMARY OF NRC00114: LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING WAS REPAIRED PER ER/A 613673-14 REV ORG SECTION I: PERMANENT REPAIR. (LP #0092117)

Part: SKIN — CORRODED (BS 710-756) · corrosion level 2 · airframe 55,489 hrs · 40,151 cycles

CORROSION ON UPPER SKIN OF CENTER WING AREA BTW STA 710 TO STA 756 AND X=-40 TO X=-56 AT CPAX. SUMMARY OF NRC 00354: CORROSION LEVEL 2. UPPER SKIN OF CENTER WING AREA BTW STA 710 TO STA 756 AND X=-40 TO X=-56 WAS REPAIRED PER ERA 613363-14 REV ORIGINAL SECTION I. PERMANENT REPAIR. ASSOCIATED ERA 14-613363 ADDED FOR AC 9565. (LP #0090006)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

INAPPROPRIATE HOLES ON VERTICAL BEAMS STA Y=817 AND STA X=0, X=13, 25, X=-13, -25 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00184: VERTICAL BEAMS ON STA Y=817, X=13, X=25, X=-13, X=-25 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B717 SRM 51-70-11-2R-2. BEAM X=0 WAS REPLACED WITH NRC 00182. (LP #0088159)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R. SUMMARY OF NRC 00259: PERMANENT REPAIR ON FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R WAS PERFORMED PER PRI 613338-14 REVISION 0 AND ERA 613338-14, REVISION ORIGINAL, SECTION I. (LP #0087503)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 AT AFT PAX CABIN. SUMMARY OF NRC 00250: CORROSION LEVEL 2. LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 WAS REPAIRED PER ER/A 613464-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II OF ER/A 613464-14 REV ORIGINAL: REPETITIVE GVI INSPECTIONS FOR BLIND FASTENERS PRIOR TO 47,844 TOTAL FLIGHT CYCLES AND THEN REPETITIVELY EVERY 8,000 FLIGHT CYCLES THEREAFTER. LOG PAGE #0085887. (LP #0086610)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

WEAR ON AFT HINGE. ALSO WEAR ON INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR. SUMMARY OF NRC 00075: INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR WAS REPAIRED PER ERA 613609-14 REV ORIGINAL. SECTION 1 PERMANENT REPAIR AND PRI 613609-14 REV 1. AFT HINGE AT FWD CARGO COMP DOOR WAS BLENDED OUT AND MEASURED AS FOLLOW; WITH AN ORIGINAL THICKNESS OF 0.120" AND WITH A REMAINING THICKNESS OF 0.110", THE MAXIMUM DEPTH ALLOWED SHOULD NOT EXCEED 20% OF THICKNESS, THEREFORE IT'S WITHIN LIMITS PER B717-200 SRM 52-00-00-1A PAR 4C (2) FIG 103. ASSOCIATED ER/A 14-613609 ADDED FOR AC 9565. (LP #0086553)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK AT FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT IN COCKPIT. SUMMARY OF NRC 00583: FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ERA 613859-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613859 ADDED FOR AC 9565. (LP #0087496)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON RH TIE TRACK BTW STA Y=813/954 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00215: CORROSION LEVEL 2. RH TIE TRACK BTW STA Y=813/954 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 AND 51-41-01-0G PAR 9. (LP #0087493)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON LH TIE TRACK BTW STA Y=813/1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC S/N 00217: CORROSION LEVEL 2. LH TIE TRACK BTW STA Y=813/1022 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G PAR 8. (LP #0084915)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

DENT FOUND ON RUDDER CONTROL TAB, RH SURFACE BTW STA ZR=43 TO ZR=52 9.5" FROM T/E. SUMMARY OF NRC 00614: RUDDER CONTROL TAB RH SURFACE BTW STA ZR=43 TO ZR=52 9.5" FROM T/E WAS REPAIRED PER B717-200 SRM 51-70-02-0G WITH REFERENCE TO 55-41-01-2R-1 PAR 5 B (1) AND (2). (LP #0084219)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION FOUND OUT OF LIMITS ON RH SEAT TRACK (X=-54) STA Y=395-397, Y=748-755, AND Y=765-773 AT PAX CABIN. SUMMARY OF NRC 00555: CORROSION LEVEL 2. RH SEAT TRACK (X=-54) STA Y=395-397 WAS REPAIRED WITH PLUG PER B717 53-20-52-2R-1 REPAIR 1. SECTION SEAT TRACK (X=-54) STA Y=685 TO Y=803 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R, REPAIR 5, FIGURE 201. (LP #0077561)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

AFTER PADS WERE REMOVED, PUNCTURE AND CRACKS WERE FOUND ON LOWER MOVABLE FLAP VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00407: MOVABLE FLAP VANE OF RH WING WAS REPAIRED PER ER/A 613241-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613241 ADDED FOR AC 9565. (LP #0077974)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CUSP WEB BTW STA Y=715 TO STA Y=756 AND X=-40 TO X=-56 AT PAX CABIN WAS NOTED TO HAVE CRACKS IN THE WEB. SUMMARY OF NRC 00613: CUSP WEB BTW STA Y=715 TO STA Y=756 AND X=-40 TO X=-56 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIG 211. (LP #0072824)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X=56 AT CABIN PAX. SUMMARY OF NRC 00598: CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X =56 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIG 211. (LP #0070354)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK WAS FOUND AT CUSP WEB ON FUSELAGE STA 218, X= 56. SUMMARY OF NRC 00609: LH CUSP WEB ON FUSELAGE STA 218, X=56 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIG 201. (LP #0071687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON RH CUSP MEMBRANE WEB BTW STA 484 TO STA 503, ALSO BTW STA 655 TO STA 725 AT PAX CABIN. SUMMARY OF NRC 00331: RH CUSP MEMBRANE WEB ON STA 655 TO STA 715 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 204. ON STA 484 TO STA 503 GVI WAS PERFORMED AND NO DAMAGE WAS FOUND PER B717-200 SRM 51-10-02-0G. ON STA 715 TO STA 725 IS ACCOMPLISHED WITH NRC 00613. (LP #0071342)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON LH CUSP WEBS STA Y=292 TO 294 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. LH CUSP WEB STA Y=292 TO 294 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 211. (LP #0068683)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

WEAR ON AFT EDGE NEAR OF AFT LATH ON AFT CARGO DOOR. SUMMARY OF NRC 00083: AFT EDGE (INNER PAN) NEAR OF AFT LATH ON AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R, PROCEDURE 8, REPAIR 8. (LP #0070156)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON LH CUSP MEMBRANE WEB STA 597. SUMMARY OF NRC 00603: LH CUSP MEMBRANE WEB STA 597 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 PAR. 5, FIGURE 211. (LP #0070121)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION WAS FOUND AT JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 LH. SUMMARY NRC 00604: CORROSION LEVEL 2. JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 WAS REPAIRED PER B717 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, PAR 4 FIG 201. (LP #0067252)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON LH CUSP MEMBRANE WEB BTW STA Y=891 TO Y=908 AT PAX CABIN WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 PAR 4 FIG 101. (ORIGINAL THICKNESS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.008 IN). SUMMARY OF NRC 00589: CORROSION LEVEL 2. LH CUSP MEMBRANE WEB BTW STA Y=891 TO Y=908 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 207. (LP #0068116)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON FLOOR SUPPORTS IS OUT LIMITS AT STA Y=148 BTW X=-44 AND X=-51, STA Y=200 BTW X=-9 AND X=-44, STA Y=173 TO STA Y=191 AND X=55, AND STA Y=210 AND X=-10. SUMMARY OF NRC 00561: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=148 BTW X=-44 AND X=-51, STA Y=200 BTW X=-9 AND X=-44, STA Y=173 TO STA Y=191 AND X=55, AND STA Y=210 AND X=-10 WERE REPLACED PER B717 SRM 51-41-08-0G PAR 7 AND 51-41-05-0G PAR 8. (LP #0067928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON CUSP WEBS RH STA Y=953 TO Y=955 AND Y=958 TO Y=963. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CORROSION ON CUSP WEBS RH STA Y=953 TO Y=970 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 223. (LP #0065452)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON RH CUSP WEBS STA Y=580 TO 590 AND STA Y=597 IN REF NRC 00551. SUMMARY OF NRC 00573: CORROSION LEVEL 2. CORROSION ON RH CUSP WEBS STA Y=580 TO 590 AND STA Y=597 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 216. (LP #0065239)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK FLOOR BEAM STA Y=737 AND X=53 APROX AT PAX CABIN. SUMMARY OF NRC 00262: FLOOR BEAM STA Y=737 AND X=53 APROX WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #0063896)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON FLOOR MEMBRANES STA Y=198 X=-15, Y=198 X=-20, Y=180 X=-15, Y=184 X=-20, Y=183 X=-6, AND Y=197 X=50. SUMMARY OF NRC 00547: CORROSION LEVEL 2. CORROSION ON FLOOR MEMBRANES STA Y= 198 X=-15, Y=198 X=-20, Y=180 X=-15, Y=184 X=-20, Y=183 X=-6, AND Y= 197 X=50 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 AT PAX CABIN. SUMMARY OF NRC 00327: LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0062288)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

OUT OF LIMITS CUSP MEMBRANE WEB STA 944, X=58 AND STA 948, X=50 AT CABIN PAX. SUMMARY OF NRC 00564: CORROSION LEVEL 2. CUSP MEMBRANE WEB STA 944, X=58 AND STA 948, X=50 WERE REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 215. (LP #0062291)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION LH CUSP MEMBRANE WEB BTW STA Y=562 TO Y=579 IS OUT OF LIMITS. SUMMARY OF NRC 00570: CORROSION LEVEL 2. MEMBRANE WEB BTW STA Y=562 TO Y=579 WAS REPAIRED PER B717 SRM 53-00-55-2R-4, PAR 5, FIGURE 216. (LP #0058082)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON WEB BTW STA Y=190 TO 180 X=55 APROX AT CABIN PAX. SUMMARY OF NRC 00574: WEB BTW STA Y=190 TO 180 X=55 APROX WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2 PAR 4 AND FIGURE 201. (LP #0058091)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON PAN BTW BEAM 1-3 STA 160 AT FWD PASS DOOR. SUMMARY OF NRC 00050: PAN WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0059117)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,124 hrs · 39,844 cycles

CORROSION ON CUSP WEBS RH STA Y=1026 TO Y=1030. SUMMARY OF NRC 00490: CORROSION LEVEL 2. CUSP WEB RH STA Y=1026 TO Y=1030 WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-01-0G. (LP #0055282)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

CRACK ON FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN. SUMMARY OF NRC 00269: FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0054020)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,124 hrs · 39,844 cycles

BROKEN UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR (L1). SUMMARY OF NRC 00383: UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR WAS REPAIRED PER B717 SRM 53-00-00-2R-1. (LP #0053120)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,822 hrs · 38,718 cycles

AFT CARGO DOOR FRAME STRUCK BY BELT LOADER IN MSP. REMOVED DAMAGE DOUBLER, DAMAGE CONTAINED. ACCOMPLISHED HFEC INSPECTION OF CUT-OUT IAW NDT SPM 06-10-01.01. NO CRACKS NOTED. REMOVED DAMAGE SEAL DEPRESSOR. DAMAGE CONTAINED. REPAIRED SKIN PER B717 SRM 53-20-15 OPTION 2. INSTALLED FILLER WASHERS PER B717 SRM 53-20-15 OPTION 2 SHEET 3. INSTALLED SEAL DEPESSOR REPAIR ALL RII COMPLETED PER SRM B717 23-20-15. PERMANENT REPAIR #10 DEFERRED TO MON VISUAL AT 8,000 CYCLES AND REPETITIVE AT 8,000 CYCLES. (LP #2697684)

Part: LIGHT — INOPERATIVE · airframe 53,148 hrs · 38,152 cycles

THE OVER WING EMERGENCY EXIT LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE (FWD LIGHTS). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND THE EMERGENCY BATTERY POWER SUPPLY UNIT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #9513984)

Part: NONE — NONE · airframe 50,713 hrs · 35,930 cycles

THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN COVER IS MISSING AT DOOR 1R. MAINTENANCE INSTALLED EXIT SIGN COVER. OPERATIONAL CHECK WAS GOOD. (LP #2026799)

Part: NONE — NONE · corrosion level 2 · airframe 50,543 hrs · 35,774 cycles

FLOOR SUPPORT AT RBL 12 AND STA 160 TO STA 200 HAS AREAS OF LIGHT CORROSION. SUMMARY SEE NRC 061-0023:5310-2005/006 00477: REMOVED CORROSION ON SUPPORT AND FOUND IT TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED A NEW SUPPORT PER B717 SRM 53-00 -00-1A. (LP #1987608)

Part: NONE — NONE · airframe 50,543 hrs · 35,774 cycles

SHEAR TIE CRACKED OUTBD OF TOMBSTONE FITTING AFT SIDE OF FR 1152. SUMMARY SEE NRC 001-0316:5300-2004/006 00073: COMPLIED WITH ER/A 594673-14 REV. 0. REPAIRED FRAME PER ER/A 594673-14 REV. ORIG. (LP #1984278 )

Part: NONE — NONE · corrosion level 2 · airframe 50,526 hrs · 35,756 cycles

AFT CARGO DOOR SILL HAS LIGHT CORROSION AND PAINT MISSING FROM FWD END TO AFT END. SUMMARY SEE NRC 001-0372:5230-2002/006 00022: REPLACED AFT CARGO DOOR JAMB PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #1978711)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,954 hrs · 35,275 cycles

DURING A-CHECK, 3 EMERGENCY EXIT IDENTIFIERS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-119 BATTERY PACK IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6904403)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 46,236 hrs · 32,520 cycles

MAINTENANCE FOUND A CRACK INDICATION COMMON TO THE 1ST FASTENER HOLE ON THE LT AND 2ND FASTENER HOLE ON THE RT BELOW THE ZFS 52.26 IN THE SKIN LAYER ONLY. REPAIRED IAW ER/A 520320-14AD, REV B.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,509 hrs · 29,947 cycles

SIDEWALL LIGHT LENS MISSING OVER RIGHT SIDE EMERGENCY EXIT WINDOWS. INSTALLED A NEW LENS. OK FOR SERVICE.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 42,364 hrs · 29,862 cycles

AFT CARGO TRACK FOUND TO BE CORRODED AND CHAFED IN SEVERAL LOCATIONS. BLENDED AREAS OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE CARGO TRACK AFT OF DOOR IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

LEFT SEAT TRACK X-54.5 STATION 465-565 HAS AREAS OF MISSING PAINT AND CORROSION BLEND/ CHECK LIMITS SRM 53-20-52. REPLACED TRACK FROM STA 456 TO 587 WITH SPLICE REPAIR PER SRM 53-20-52-2R-5. TRACK WAS FOUND TO BE OUT OF LIMITS REMOVED .025 OF ORIGINAL .115 PER SRM 53-20-52-1A-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

FS 819 LBL 60 CUSP WEB CRACKED. VERIFIED WITH HFEC IAW NTSPM PART 6, 06-10-01.001 PROCEDURE 1 REPAIR IAW SRM CH 53-00-55. REPAIRED CKED CUSP WEB AT STA 819 LBL 60 IAW SRM 53-00-55 REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CORROSION ON RIGHT O/B SEAT TRACK (RBL 56) IN SEVERAL AREAS FROM STA 256 TO STA 351. BLEND CHECK LIMITS IAW SRM CH 53-20-52. BLENDED RT OTBD FWD SEAT TRACK REMOVED .010" FROM TOP .105" REMAINING WITHIN LIMITS IAW SRM 53-20-52 GAUGE TAG 2736. BLENDED RT OTBD SEAT TRACK REMOVED .035" FROM TOP REMAINING .080" OUT OF LIMITS IAW B717 SRM 53-20-52. REPLACED SEAT TRACK STA 200 TO STA 305 IAW SRM 53-20-52-2R PROCEDURE 5.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

ALC DOOR CUTOUT LWR PAN HAS CORROSION AROUND BARREL NUT HOLES BLEND AND CHECK LIMITS. BLENDED CORROSION ON ALC DOOR CUTOUT LOWER PAN, NOMINAL =.050 REMAINING =.025 OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED LOWER PAN IAW SRM 53-20-15 REPAIR 7.

Part: LONGERON SPLICE — CORRODED (BS 946-956) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CORROSION AT BS 946 - 956 LONGERON 30L. BLENDED CORROSION IAW SRM 51-10-04 PG 38. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00 FIG 103. REMOVED AND REPLACED THE SPLICE IAW SRM 53-00-05, REPAIR 2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

CRACK FOUND ON CUSP WEB AT STA 595 LBL 56 UPON INSTALLATION OF SEAT TRACK REPAIR IAW SRM. REMOVED DAMAGE FROM CUSP WEB IAW SRM 53-00-55 REPAIR 4. FABRICATED REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4. INSTALLED REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4 AT STA 595 LBL 56.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CORROSION FLC FRAME STA 484 L30 - L29R. REPAIRED FLC FRAME AT STA 484 L30-L29R IAW SRM 53-20-07 FIG 201 SHEET 7 REPAIR 3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

LT CUSP WEB O/B HAS 4 CRACKS 1 EA AT STA 656 & 3 EA AT STA 672 REPAIR CUSP WEB IAW 53-00-55 R4. CRACK AT STA 656 TO BE REPAIRED ON ORNRC 74570-0200-0307. INSTALLED WEB REPAIR AT STA 672 LT. INSTALLED REINFORCEMENT DOUBLER AT LT STA 672 IAW SRM 53-00-55 REPAIR 4 SRM 51-41-02, 51-41-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT/OUTBOARD SEAT TRACK BL56R HAS AREAS OF CORROSION AND MISSING PAINT AT STATIONS 465-565. REPLACED SEAT TRACK FROM FIG 465R TO 565R RBL 56 IAW SRM 53-20-52 PG 4 (K) L-L.

Part: FLOORBEAM — CORRODED (BS 256) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

FLOORBEAM BS 256 LBL 22 TO RBL 22 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. . REMOVED IAW SRM 51-41-02. FABRICATED, ALODINED, PRIMED, AND TOP COATED IAW AMM 51-10-00 370-803. INSTALLED IAW SRM 51-41-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT HAND CUSP WEB HAS WIDESPREAD CORROSION BETWEEN FRAMES AT STA 446 AND STA 503 OUTBOARD OF RIGHT HAND OUTBOARD SEAT TRACK. REPAIRED CORROSION ON CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: CUSP WEB — CRACKED (BS 636-655) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT CUSP WEB CRACKED AND CORRODED FROM BS 636 - 655. REPLACED THE CUSP WEB IAW SRM 51-41-02 AND SRM 51-41-05.

Part: CABLE — BENT (TAILCONE RELEASE) · airframe 42,358 hrs · 29,857 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY TAILCONE RELEASE CABLE HAD BENT ENDS WHERE THE CABLE GOES TO THE EXTERNAL HANDLE. THE TAILCONE RELEASE CABLE FOR THE EXTERNAL HANDLE PIN WAS REPLACED AND OPERATIONALLY CHECKED SATISFACTORY.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

CRACK ON LT CUSP WEB AT STA 656. REPAIRED CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

CENTER SEAT TRACK ANGLE TO TRACK SUPPORT CRACKED AT BOTTOM STA 715 RT SIDE (M). REPLACED CENTER RT SEAT TRACK ANGLE TO TRACK SUPPORT AT STA 715 IAW SRM 51-41-05 AND DWG 9923417.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

CUSP WEB CRACKED AT LT STA 650. REPAIRED CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: LONGERON — CORRODED (BS 948) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CORROSION LONGERON 28L BS 948. BLENDED CORROSION IAW SRM 53-00-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-05. REPAIRED IAW SRM 53-00-05 REPAIR 3.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

LOWER SEAT TRACK SUPPORT LT SIDE STA737 CRACKED AT BOTTOM (M). REPLACED LT SIDE SEAT TRACK SUPPORT IAW SRM 51-41-05 AND DRAWING 3925812 WITH SEAT TRACK SUPPORT.

Part: MEMBRANE — DAMAGED (BS 170) · airframe 42,358 hrs · 29,857 cycles

HOLE IN FORWARD WET AREA MEMBRANE AT BS 170 AND RBL 5 UNDER OUTBOARD FLANGE OF RIGHT CENTER SEAT TRACK. REPAIRED IAW SRM 53-00-00 REPAIR 2.

Part: LONGERON — CORRODED (BS 1002) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CORROSION BS 1002, LONGERON 24R END CAP. REPLACED THE END CAP IAW SRM 51-41-05. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. DWG 5911424.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,358 hrs · 29,857 cycles

LOWER SEAT TRACK SUPPORT RT SIDE STA737 CRACKED AT BOTTOM (M). REPLACED CRACKED SEAT TRACK SUPPORT WITH NEW SEAT TRACK SUPPORT IAW SRM 51-41-05 AND DRAWING 3925812 AT FS 737 RT SIDE.

Part: SKIN — DAMAGED (RUDDER) · airframe 42,358 hrs · 29,857 cycles

RUDDER SKIN IS CREASED ON RT SIDE ABOVE TRIM TAB. REPAIRED THE SKIN IAW SRM 51-10-04, 51-22-01 PAGE 5, AND 51-70-13 REPAIR 1 PAGE 206.

Part: CUSP WEB — DAMAGED (BS 832) · airframe 42,358 hrs · 29,857 cycles

UPPER CABIN RT SIDE CUSP WEB AT BS 832 DAMAGED. REPAIRED THE CUSP WEB IAW SRM 53-00-55.

Part: SEAT TRACK — CORRODED (BS 945) · airframe 42,358 hrs · 29,857 cycles

BS 945 SEAT TRACK WORN AT CURTAIN HOLD DOWN LOCATION. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

LEFT INBOARD SEAT TRACK HAS AREAS OF CORROSION BS 200 TO 256. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 PG 104. INSTALLED A REPAIR IAW SRM 53-20-52 FIG 201 REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 565-665) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT INBD SEAT TRACK RBL 22 HAS AREAS OF CORROSION BS 565 - 665. BLENDED AND FOUND TO BE WITHIN LIMITS IAW SRM 51-30-01 PG 93 FIG 18, SRM 53-20-52 PG 104 FIG 101.

Part: CUSP WEB — DAMAGED (BS 522) · airframe 42,358 hrs · 29,857 cycles

RIGHT CUSP WEB HAS A HOLE IN IT AFT OF FRAME AT BS 522 UNDER OUTBOARD OF THE SEAT TRACK. CUT OUT DAMAGE IAW SRM 53-00-55 2R-4, FABRICATED CUSP WEB RING DOUBLER IAW SRM 53-00-55 2R-4, AND 51-40-08 06 PG 3 TABLE 6. INSTALLED THE REPAIR IAW SRM 53-00-55 2R-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT HAND CUSP WEB NUT CLIP BRACKET JUST AFT OF FRAME 636 IS CORRODED. REPAIRED CUSP WEB AT RT STA 656 IAW SRM 53-00-55 REPAIR 4 RT CUSP WEB NUT CLIP BRACKET TO BE REPLACED ON ORNRC 74570-0200-0308.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RIGHT HAND CUSP WEB CRACKED, BENT, AND CORRODED AT FLANGE AROUND LIGHTENING HOLE (RD HOLE AFT OF FRAME 617) DAMAGE MARKED IN RED. REPAIRED CUSP WEB RT STA 617 IAW SRM 53-00-55 REPAIR 4 PG 218.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

FIRST OFFICERS OUTBOARD AFT SEAT TRACK CORRODED. (MARKED). REPLACED FIRST OFFICERS OUTBD AFT SEAT TRACK IAW SRM 51-41-01, AND DWG 9936533.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CROSS MEMBER FLOORBEAM BETWEEN RIGHT CENTER AND INBOARD SEAT TRACKS AT STA 256 HAS AREAS OF CORROSION. BLEND AND CHECK LIMITS. REPLACED FLOOR SUPPORT AT FS 256 RBL 25 TO 41 IAW SRM 51-41-05, DWG 5940663.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

CROSS MEMBER FLOOR STRUCTURE AT STA 148 X RBL32.5 TO RBL44.5 HAS AREAS OF CORROSION BLEND AND CHECK LIMITS. REPLACED FLOOR SUPPORT AT FS 148 RBL 32.5 TO 44.5 IAW SRM 51-41-05 DWG 9936533.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

INSIDE GALLEY SERVICE DOOR SUB FLOOR CORRODED AT THE FOLLOWING STATIONS: 160, RBL 48, RBL 54, RBL 57, STA 165, RBL 45, RBL 54, STA 173, RBL 45, STA 177, RBL 46. MARKED. REPAIRED CORRODED GALLEY SERVICE DOOR SUB FLOOR IAW ER/A 551819-14MA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

RT/IB SEAT TRACK BL22R HAS AREAS OF CORROSION AND MISSING PAINT AT STATIONS 465-565. REPAIRED SEAT TRACK RBL 22 STA 560 IAW SRM 53-20-52 REPAIR 1 PG 202. DUE TO SEAT BEING OUT OF LIMITS ITEM 3 SEAT TRACK FROM STA 465-560 CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-20-52 ORIGINAL T= .115 REMOVED .015.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 42,358 hrs · 29,857 cycles

BS 1022 BETWEEN LONGERONS 13 & 14R AFT SHEAR TIE IS CRACKED. . REPLACED THE SHEAR TIE IAW DWG 9912243, SRM 51-41-02, & 51-41-05.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 42,358 hrs · 29,857 cycles

CABIN BS 1022 BETWEEN STRINGERS 13 - 14R FORWARD SHEAR TIE CRACKED . REPLACED THE SHEAR TIE IAW DWG 9912243, SRM 51-41-02, & 51-41-05.

Part: FLOOR SUPPORT — CORRODED (BS 157-189) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

BS 157 - 189, RBL 48 FLOOR SUPPORT CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. FABRICATED A NEW FLOOR SUPPORT. ALODINED, PRIMED, AND TOP COATED IAW AMM 51-10-00-370-803. INSTALLED THE FLOOR SUPPORT IAW SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 182) · corrosion level 2 · airframe 42,358 hrs · 29,857 cycles

FLOORBEAM BS 182, RBL 10 TO 42.5 CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS. REMOVED IAW SRM 53-00-00 FIG. 103. FABRICATED A NEW FLOORBEAM. ALODINED, PRIMED, AND TOP COATED IAW AMM 51-10-00-370-803. INSTALLED THE FLOORBEAM IAW SRM 51-41-02.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 39,845 hrs · 27,982 cycles

AFT CARGO HAS CORROSION ON DOOR FRAME FORWARD SIDE AND ON LOWER SILL. REMOVED CORROSION IAW SRM 53-20-15, REPAIR 7.

Part: FLOOR PANEL — DISTORTED · airframe 38,651 hrs · 26,991 cycles

RETURNED TO DEPARTURE DUE TO BINDING AILERON CONTROL SYSTEM ISSUES DURING CLIMBOUT. ACCOMPLISHED COMPLETE INSPECTION OF AILERON SYSTEM CABLES, PULLEYS, AND FAIRLEADS. FOUND FOWARD CARGO CEILING PANELS 121HC AND 121EC DISTORTED UPWARD AND INTERFERRING WITH AILERON CABLE RUN/TURNBARREL. REPOSITIONED PANELS AND SUPPORT STRUCTURE IAW AMM AND GROUND CHECKS WERE NORMAL. PERFORMED FUNCTIONAL VERIFICATION FLIGHT WITH SATISFACTORY RESULTS. THE ACFT HAS RETURNED TO SERVICE.

Part: SKIN — DELAMINATED (FLT SPOILER) · airframe 1,430 hrs · 1,315 cycles

FLIGHT SPOILER FOUND DEBONDED AND DELAMINATED ALONG THE UPPER AND LOWER SURFACES.

Part: PIN — MISINSTALLED (DOOR SLIDE) · airframe 38,153 hrs · 26,556 cycles

DURING SERVICE CHECK, FOUND PIN INSTALLED IN L1 DOOR ESCAPE SLIDE. REMOVED PIN. PERFORMED VISUAL INSPECTION AND VERIFIED PART EFFECTIVITY IAW IPC. REINSTALLED DOOR SLIDE IAW AMDS WORK CARD 2561-9004 AND COMPLETED REQUIRE INSPECTION. THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,863 hrs · 25,518 cycles

DURING A LINE CHECK OF THE EMERGENCY LIGHTS, IT WAS NOTED THE CEILING MOUNTED EMERGENCY LIGHTS FROM ROWS 23-29 WERE INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPS THEN CHECKED NORMALLY.

Part: PITOT TUBE — MALFUNCTIONED · airframe 36,629 hrs · 25,322 cycles

PERFORMED AN AIR TURN BACK WHILE ENROUTE DUE TO VARYING INDICATIONS FROM ALL THREE AIRSPEED INDICATION SYSTEMS AS WELL AS MULTIPLE CORRESPONDING AIR DATA FAILURE/FAULT ANNUNCIATIONS. MAINTENANCE REPLACED ALL THREE PITOT PROBES AND PERFORMED THE REQUIRED LEAK AND FUNCTIONAL CHECKS. THE AUTOFLIGHT RTS CHECKS ALSO PASSED. THE ACFT HAS RETURNED TO SERVICE.

Part: CABLE — DAMAGED (TAILCONE SLIDE) · airframe 35,450 hrs · 24,219 cycles

TAILCONE SLIDE DEPLOYMENT CABLE AT CONECTION TO TAILCONE DEPLOYMENT SYSTEM LANYARD MISSING HEAT SHRINKABLE TUBING. INSTALLED HEAT SHRINKABLE TUBING ON TAILCONE SLIDE DEPLOYMENT SYSTEM LANYARD IAW AMM 25-61-02-400-801.

Part: PANEL — CRACKED (RT WING) · airframe 35,433 hrs · 24,203 cycles

RT WING FUEL ADAPTER VLV PANEL 610VB CRACKED. R & R PANEL IAW SRM.

Part: SLIDE — OUT OF POSITION (TAIL CONE) · airframe 35,433 hrs · 24,203 cycles

TAIL CONE SLIDE SIGHT OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW AMM.

Part: COVER — CRACKED (CABIN) · airframe 35,433 hrs · 24,203 cycles

CEILING EMERGENCY EXIT LIGHT CRACKED AT ROW 1. REPAIRED COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,433 hrs · 24,203 cycles

LT FWD OVERWING BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 35,433 hrs · 24,203 cycles

AFT EMERGENCY FLASHLIGHT LOOSE. SECURED FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,228 hrs · 24,067 cycles

RT OVERWING LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 35,228 hrs · 24,067 cycles

L1 DOOR EMERGENCY EXIT LIGHT SIGN BROKEN. R & R SIGN IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

CABIN FLOOR PANEL 223FF DELAMINATED. R & R PANEL IAW SRM & AMM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR PANEL DELAMINATED WITH EXPOSED HONEYCOMB PANEL 223 BF. R & R PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

SEAT TRACK CORRODED ON FLANGE AT STATION 200, RBL 22. R & R PANEL IAW MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FWD ENTRY HAT CHANNEL CORRODED BETWEEN BS 149 TO BS 200, RBL 8. R & R SUPPORT TRACK IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222AMF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222LF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FAIRING — CRACKED (RT ELEVATOR) · airframe 35,228 hrs · 24,067 cycles

RT ELEVATOR TAB ROD FAIRING CRACKED AT FASTENER HOLE. REPAIRED DOUBLER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222JF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 221WF DELAMINATED. REMOVED PANEL IAW AMM & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN LBL 15 TO LBL 38. R & R SUPPORT IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222AGF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222AVF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

G2 GALLEY MOUNT CORRODED AT STATION 218 RBL 10. R & R MOUNT IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222ATF DELAMINATED. REMOVED PANEL IAW AMM & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FWD ENTRY WEB CORRODED UNDER FLOOR SUPPORT AT STATION 200, RBL 50. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR SUPPORT CORRODED AT STATION 200, BETWEEN LBL 6 TO RBL 6. R & R SUPPORT IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

SEAT TRACK ON FLANGE CORRODED AT STATION 218, RBL 44. R & R SEAT TRACK IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222FF DELAMINATED. REMOVED PANEL IAW AMM & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 200 TO BS 168, LBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FWD ENTRY FLOOR SUPPORT CORRODED AT STATION 200, BETWEEN RBL 10 TO RBL 45. R & R SUPPORT IAW SRM & DRAWING. .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR SUPPORT CORRODED AT STATION 229, BETWEEN BL0 TO LBL 15. R & R SUPPORT IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222PF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR PANEL 221 BF CRACKED. R & R PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FWD ENTRY FLOOR SUPPORT CORRODED AT STATION 180, BETWEEN RBL 10 TO RBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 200 TO BS 218, LBL 15. REPAIRED SUPPORT IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222BF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,228 hrs · 24,067 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

MAIN ENTRANCE DOOR SCUFF PLATE SILL SUPPORT ANGLE CORRODED BETWEEN STATION 170 TO STATION 180, LBL 54. REPAIRED SUPPORT IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

LT WW FWD DOOR CUTOUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

AFT ACCESSORY COMPARTMENT LONGERON CRACKED AT BS 1133, 2R. REPAIRED LONGERON IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 35,228 hrs · 24,067 cycles

LT WW AFT BULKHEAD BELOW TRAPEZOIDAL SUPPORT ANGLE CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

AFT ACCESSORY COMPARTMENT CLIP CRACKED AT BS 1152, LONGERON 2L. R & R CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

LT VENT LOUVER INBD LOWER FWD CLIP CRACKED ON CANTED FRAME. R & R CLIP IAW SRM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 35,228 hrs · 24,067 cycles

FWD CARGO DOOR SKIN CREASED 33 TO 36 INCHES FROM UPPER EDGE. R & R DOOR IAW MM.

Part: PANEL — CRACKED (RT WING) · airframe 35,228 hrs · 24,067 cycles

RT WING INBD BUTTE DOOR LOWER WING PANEL CRACKED. R & R PANEL IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

AFT ACCESSORY COMPARTMENT CLIP CRACKED AT BS 1152, LONGERON 2R. R &R CLIP IAW SRM & DRAWING.

Part: PANEL — CRACKED (RT MLG WW) · airframe 35,228 hrs · 24,067 cycles

RT MLG WW AFT BULKHEAD WEB PANEL CRACKED. R & R WEB PANEL IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 35,228 hrs · 24,067 cycles

RT WW AFT BULKHEAD BELOW TRAPEZOIDAL ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CHIPPED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

AFT CARGO DOOR CUTOUT AFT EDGE SKIN CHIPPED AT LONGERON R26. REPAIRED DOUBLER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,228 hrs · 24,067 cycles

EMPENNAGE, LT VENT LOUVER BOX PAN CRACKED & VERTICAL ANGLE. R & R ANGLE IAW DRAWING.

Part: SIGN — UNSECURE (CABIN) · airframe 34,985 hrs · 23,901 cycles

LT EMERGENCY EXIT SIGN FELL OFF AT ROW 1. REINSTALLED SIGN IAW SIP.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 23,567 hrs · 23,566 cycles

RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. R&R RT GEAR UP/LATCH SENSOR IAW MM.

Part: RETAINER — OUT OF POSITION (L1 DOOR) · airframe 34,088 hrs · 23,371 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOCKING PIN OUT OF POSITION. REPOSITIONED RETAINER PER AMM.

Part: FUSE — BLOWN (CABIN) · airframe 33,877 hrs · 23,238 cycles

EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 25 TO ROW 31. REMOVED AND REPLACED FUSES PER AMM.

Part: SPRING — MISSING (R1 DOOR) · airframe 31,583 hrs · 21,766 cycles

R1 DOOR SLIDE GIRT BAR STOWAGE RETAINER MISSING TENSION SPRINGS. REPLACED GIRT BAR STOWAGE RETAINER TENSION SPRING PER MM.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 31,500 hrs · 21,715 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOWAGE BRACKET BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO LONGERON, STA 974 TO 994, LONG 30, CORROSION. ACCOMPLISHED LONGERON REPLACEMENT PER B717 SRM 53-00-05 AND 51-41-08.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT SHEAR TIE, STA 974, LONG 30 TO 29L, CORROSION. ACCOMPLISHED SHEAR TIE REPLACEMENT PER B717 SRM 51-20-9, 53-00-06, 51-41-02 AND 51-41-05.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 1022, LONG 28L TO 28R, CORROSION. ACCOMPLISHED FRAME REPLACEMENT PER B717 SRM 53-20-07.

Part: PAN — CORRODED (BS 954-994)

AFT CARGO DOOR JAMB FLOOR PAN, STA 954 TO 994, CORRODED. ACCOMPLISHED DOOR PAN REPLACEMENT PER SRM 53-20-15 AND 51-40-08.

Part: PAN — CORRODED (BS 320-427)

FWD CARGO DOOR JAMB FLOOR PAN, BS 320 TO 427, CORRODED. ACCOMPLISHED DOOR PAN REPLACEMENT PER SRM 53-20-15 AND 51-40-08.

Part: COMPRESSOR — STALLED (RT ENGINE)

NUMEROUS COMP STALL ON RIGHT ENGINE. NO OVER TEMP OR EXCEEDANCE. REMOVED AND REPLACED NR 2 ENG REF WO 255695 T/C 603.

Part: PIN — BACKED OUT (CABIN)

E-PATH LIGHTS AT ROW 16 INOP-RELAMP, NO HELP. FOUND PUSHED PIN AT SIDEWALL/SEAT ROW DISCONNECT. RESEATED PIN IAW SWPM 20-31-13. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-51-00 AND FOUND NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ROW 25 TO ROW 31 SEAT TRACK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY ASSEMBLY AND BATTERY AT OVERHEAD BIN ROW 24 REF B717 AMM 33-51 OPS CHECK GOOD.

Part: COMPRESSOR — STALLED (LT ENGINE)

LEFT ENG COMPRESSOR STALL IN FLIGHT. SHUT DOWN LEFT ENGINE IAW CHECKLIST. WOULD NOT RUN SMOOTHLY ABOVE IDLE. REMOVED AND REPLACED NR 1 ENG REF W/O 235947. T/C 603. ALL OPS CHECKS GOOD.

Part: COVER — MISSING (CABIN)

ESCAPE PATH LIGHTING COVER AT 20D, E, F MISSING. INSTALLED COVER REF M/M 33-51, OK FOR SERVICE.

Part: LENS — MISSING (CABIN)

EMERGENCY LIGHT COVER MISSING AT SEAT 22D. INSTALLED LENS COVER AT 22D. OPS CHECK NORMAL REF MM 33-51.

Part: COVER — MISSING (CABIN)

AISLE PATH LIGHTING 10D MISSING COVER ON LIGHT. REPLACED COVER IAW B717 MM 33-51.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS)

EXTERIOR EMERGENCY LIGHTS WILL NOT TURN OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK B5-125. REF AMM 33-50. OPS CHECK NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN)

OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED (WITH SWITCH OFF). PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM. NO DEFECTS NOTED, REF AMM 33-57-00.

Part: CONNECTOR — DAMAGED (CABIN)

ROW 23 EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR AT SEAT 23-F. OPS CHECK NORMAL PER MM 33-51.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP AT LOWER AFT OVERWING EXIT DOORS. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY AT 24 DEF OVERHEAD BIN IAW B717MM 33-51. OPS CHECKED GOOD.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

R1 DOOR SLIDE PARTIALLY EXPOSED. RECONNECTED DEPLOYMENT LANYARD PER AMM 25-61.

Part: BATTERY — DISCHARGED (CABIN)

EPL WILL NOT LIGHT ON SEAT 20-24. REMOVED AND REPLACED BATTERY SUPPLY ASSY B5-118. OPS CHECK GOOD, REF AMM 33-51.

Part: LENS — BROKEN (CABIN)

ESCAPE PATH LIGHTING ON 10D, FIXTURE MISSING AND BROKEN. INSTALLED EMERGENCY PATH LIGHTING LENS COVER AT 10D. LIGHTS OPS NORMAL.

Part: SKIN — CORRODED (FUSELAGE)

LOWER FUSELAGE SKIN, STA 851, LONG L29R, CORROSION. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-02268IR.

Part: STRUCTURE — CRACKED (FUSELAGE)

CABIN CENTER FLOOR, STA 688.5, CRACKED. ACCOMPLISHED CENTER FLOOR DOUBLER REPAIR PER B717 SRM 51-41-08 AND 53-20-50.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 239, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F.

Part: RIB — GOUGED (COWLING)

NR 5 LOWER ENGINE COWLING RIB, GOUGED. ACCOMPLISHED ENGINE COWLING RIB ANGLE AND FILLER REPAIR PER B717 SRM 54-20-05.

Part: PANEL — CORRODED (CABIN)

CABIN FILLER PANEL, STA 160 TO 200, RBL 56, CORROSION. ACCOMPLISHED FILLER PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 160, RBL 12 TO RBL 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 167 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 204 TO 243, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, RBL 10 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01.

Part: STRAP — CORRODED (FUSELAGE)

LEFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG 28L, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: STRAP — CORRODED (FUSELAGE)

RIGHT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG 28R, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 181 TO 190, RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN CUSP WEB, STA 522 TO 541, CORROSION. ACCOMPLISHED CABIN CUSP WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, LBL 14 TO RBL 20, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 19, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: WIRE — BROKEN (CABIN)

SEAT 27F ESCAPE PATH WIRE BUNDLE LOOSE. FOUND ESCAPE PATH LIGHTING WIRE BROKEN. PERFORMED TRA 17-33-TR00024 SECTION 1; OPS CHECK GOOD; OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTING ROWS 25-31 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK REF MM 33-51.

Part: BATTERY — DISCHARGED (CABIN)

E-LIGHTS ON SEATS 1 DF - 3DF INCLUDED NR 2 GALLEY INOP (NOT TURN ON). REPLACED BATTERY SUPPLY ASSY AND BATTERY ASSY PER B717 MM33, OP'S TEST OK.

Part: STRINGER — CORRODED (FUSELAGE)

AFT BAG BIN STA 954 STR 30 CORROSION. CUT OUT DAMAGED SECTION ON STR 30 AND REPAIRED PER B717 SRM 53-00-05.

Part: ACTUATOR — FAILED (LT MLG)

FELT SMALL THUMP IN FLOOR FOLLOWED BY LEVEL 2 ALERT, "RIGHT HYD QUANTITY LOW." COMPLETED NON-NORMAL CHECK LIST AND EXTENDED EMERGENCY GEAR EXTENSION LEVER (ALSO STOWED GEAR LEVER AS PER MX). REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR CYLINDER.

Part: SPRING — BROKEN (MLG UPLATCH)

UNSAFE GEAR INDICATION (LEFT MAIN) AFTER GEAR RETRACTION, 3 GREEN LIGHTS WHEN EXTENDED. REMOVED AND REPLACED LEFT MLG UPLATCH PROXIMITY SENSOR CRANK ASSEMBLY SPRING. CYCLED GEAR NUMEROUS TIMES, ALL LIGHTS NORMAL. NO FAULT NOTED. OK FOR SERVICE AT THIS TIME REF 32-61 AMM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

PIN SHOWING ON R1 SLIDE. REMOVED AND REPLACED R1 SLIDE ASSY. REF MM 25-61.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT INOP AT SEAT ROWS 1DF, 2DF, 3DF AND 10DEF. REMOVED & REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY AT STA 398 PER B717 AMM 33-51, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (ROW 23)

ROW 23 EPL INOPERATIVE, REMOVED AND REPLACED EPL ASSY AND POWER SUPPLY IAW 33-00 REPAIRED SEAT ROW 23 FLOOR CONNECTOR IAW SWP.

Part: BRACKET — LOOSE (CURTAIN ROD)

CURTAIN ROD AT BUSINESS CLASS FELL OF DURING TAKEOFF, HITTING PASSENGER. FOUND RIGHT SIDE BRACKET LOOSE ON HEADER ASSY, RESECURED AS NEEDED.