N923AT

Part: SKIN — CRACKED (ZONE 500 FLAP) · airframe 48,068 hrs · 34,448 cycles

LEFT FLAP TRAILING EDGE CRACK AND DELAMINATION. REPAIRED PER ER/A 631162-14. (8401817)

Part: NONE — NONE (NONE) · airframe 47,902 hrs · 34,283 cycles

DTA ER/A 618121-14 REV A SECTION I MONITOR LOG REQUIRES DTA STATE 3 APPROVAL ON OR BEFORE 82,000 TOTAL CYCLES. C/W ER/A 00-618121 (1304050).

Part: LONGERON — DAMAGED (ZONE) · airframe 47,058 hrs · 33,531 cycles

AIRCRAFT 9559, LONGERON BETWEEN ST 256 & 275 DAMAGED. REMOVED DAMAGE SECTION OF LONGERON IAW B717 SRM 53-00-05-2R PRO 2. FABRICATED LONGERON AND HATS P717 SRM 53-00-05-2R PROCEDURE 2. PERFORMED BHEC OF REMOVED FASTENERS IAW B717 NDT SPM PART 6, 06-10-01.003 NO FINDINGS. TREATED AND PAINTED REPAIR PIECES. INSTALLED REPAIR SPLICE PER B717 SRM 53-00-05-2R.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 45,816 hrs · 32,394 cycles

THE FOUR LOWER OVERWING EXIT LIGHTS, LEFT AND RIGHT, ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY R5-119 PER B717 AMM 33-51-03. SYSTEM NOW OPERATIONALLY CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6976208)

Part: BEAM — CRACKED (AFT BULKHEAD) · airframe 44,579 hrs · 31,353 cycles

CRACKS ON INTERNAL BEAM #1 AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00356: INTERNAL BEAM #1 (UPPER WEB) AT AFT CABIN BULKHEAD DOOR (CPAX) WAS FABRICATED AND REPLACED PER DWG 9915565 REV BD, B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0381964)

Part: FUEL TANK — CORRODED (BS 748) · corrosion level 2 · airframe 44,579 hrs · 31,353 cycles

-AD- CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. SUMMARY OF NRC 00777: LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL WAS REPAIRED PER ER/A 618121-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 618121-14 REV 7. TIME OF ACOMPLISHMENT: REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 28MAY24. ADDITIONAL ENGINEERING AUTHORIZATION REVISION IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM REPAIR ACCOMPLISHMENT.UNDER LOG PAGE #0366678 PER ER/A 618121- 14AD REV ORIGINAL. ASSOCIATED ER/A 14-618121 ADDED FOR AC 9559. (LP #0367243)

Part: ATTACH FITTING — CORRODED (MLG) · corrosion level 2 · airframe 44,579 hrs · 31,353 cycles

RUSTED ON LUG AT ATTACH FIXED STRUT, ALSO ON FITTING TO RH LANDING GEAR. SUMMARY OF NRC 00731: RUSTED ON FITTING TO RH LANDING GEAR WAS REMOVED PER BOEING OM 57-40-1 REPAIR PAR 2 G (6) (B), (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FITTING TO RH LANDING GEAR WITH ORIGINAL THICKNESS IS 1.500 INCHES AND MINIMUM REMAINING THICKNESS IS 1.499 INCHES THEREFORE IT IS WITHIN LIMITS PER BOEING OM 57-40-1 REPAIR PAR 2 G (6) (B) TABLE 606 AND DC-MD/BOEING NDT SPM PART 4, 04-00-06 PAR 4. FIG 9 AND STRUT ASSY-FIXED SIDE LINK RH WAS REPLACED PER B 717-200 IPC 57-11-03-01. INSTALLATION WAS ACCOMPLISHED UNDER NRC 00378. (LP #0342803)

Part: JACKSCREW — NICKED (HORIZONTAL STAB) · airframe 44,579 hrs · 31,353 cycles

-AD- A NICK WAS FOUND ON THREAD OF THE ACME SCREW AT THE HORIZONTAL STAB. SUMMARY OF NRC 00485: HORIZONTAL STABILIZER ACTUATOR JACKSCREW ASSY WAS REPLACED FOR SERVICEABLE ACTUATOR JACKSCREW. WAS INSTALLED PER B717 AMM 27-41-04 AND TESTED OK. ALSO, TRIM GEARBOX WAS REPLACED AND INSTALLED PER B717 AMM 27-41-07 AND LP #0315260. (LP #0336526)

Part: NOT REPORTED — SCRATCHED (HORIZONTAL STAB) · airframe 44,579 hrs · 31,353 cycles

-AD- SCRATCHES WERE FOUND AT FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER. SUMMARY OF NRC 00666: FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER (HOLE #19) WAS REPAIRED PER PRI 617393-14 REV 1 AND ER/A 617393AD REV ORIG SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 25-APR-2024. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION SECOND/THIRD STAGE IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93 PER ERA 617393-14AD REV ORIGINAL. LOG PAGE #0320071 REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 02-APR-2024. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: NEW AMOC TO AD 2004-03-21 PAR (B) IS REQUIRED PRIOR TO 24 MONTHS IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. PER ERA 617393-14AD REV: ORIGINAL LOG PAGE #0320079. (LP #0321744)

Part: PAN — CRACKED (AFT CARGO) · airframe 44,579 hrs · 31,353 cycles

CRACKS WERE FOUND ON PAN, BTW BEAMS 3/4 AND AFT SIDE AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00348: AFT INNER PAN ON BEAM #3 AND BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 617066-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617066-14 REV 2. ASSOCIATED ER/A 14-617066 ADDED FOR AC 9559. (LP #0312288)

Part: NONE — NONE (NONE) · airframe 44,579 hrs · 31,353 cycles

-AD- AMOC ER/A 617393-14AD MONITOR LOG REQUIRES DTA WITH NEW AMOC ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024 PENDING A NEW AMOC WITH STAGE 2/3 DTE. ASSOCIATED ER/A 00-617393 ADDED FOR AC 9559. **REDEFERRED LOG TO QC, ESTAB MON INSP 00-0555-8-7598 S/N 09559 L/L. (LP #0320079)

Part: NONE — NONE (NONE) · airframe 44,579 hrs · 31,353 cycles

-AD- DTA ER/A 616393-14AD MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING . DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-24 PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-617393 ADDED FOR AC 9559. **REDEFERRED LOG TO QC, ESTAB MON INSP** 00-0555-8-7562 S/N 09559 L/L. (LP #0320071)

Part: SKIN — CRACKED (BS 1078 L14R) · airframe 44,579 hrs · 31,353 cycles

CRACK ON FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R. SUMMARY OF NRC 00041: FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R WAS REPAIRED PER ERA 617080-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR PER ERA 617080-14 REV: ORIGINAL, LOG PAGE #0302431. ASSOCIATED ER/A 14-617080 ADDED FOR AC 9559. (LP #0308681)

Part: DIAPHRAGM — CRACKED (BS 171-172) · airframe 44,579 hrs · 31,353 cycles

CRACK ON DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX (W1). SUMMARY OF NRC 00689: DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10- 2R REPAIR 2 FIG 201. (LP #0300282)

Part: CUSP WEB — CORRODED (BS 369-462) · corrosion level 2 · airframe 44,579 hrs · 31,353 cycles

CORROSION ON CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BTW STA Y=429 AND Y=434, AND BTW STA Y=459 AND Y=462 X-56 (IN REFERENCE TO NRC 00542). SUMMARY OF NRC 00661: CORROSION LEVEL 2. CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BTW STA Y=429 AND Y=434, AND BTW STA Y=459 AND Y=462 X-56 WERE REPAIRED PER B717-200 SRM 53-00-55-2R REP 4 FIG 215. (LP #0298549)

Part: BEAM — CRACKED (FWD CARGO DOOR) · airframe 44,579 hrs · 31,353 cycles

CRACKS 2 EA ON FWD PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00243: FWD PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296705)

Part: BEAM — CRACKED (FWD CARGO DOOR) · airframe 44,579 hrs · 31,353 cycles

CRACKS ON FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00245: FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296713)

Part: BEAM — CRACKED (FWD CARGO) · airframe 44,579 hrs · 31,353 cycles

CRACKS ON FWD PANE BEAM 3 AT FWD CARGO DOOR. SUMMARY OF NRC 00244: FWD PANE BEAM 3 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0292323)

Part: BEAM — CRACKED (BS 161-197) · airframe 44,579 hrs · 31,353 cycles

CRACK ON BEAM #1 STA 161 AND STA 197 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00216: DAMAGED SECTIONS (STA 161 AND STA 197) OF BEAM #1 AT PASSENGER ENTRANCE DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7, FIG 201 AND FIG 202. (LP #0289422)

Part: BEAM — CRACKED (FWD CARGO) · airframe 44,579 hrs · 31,353 cycles

CRACK ON AFT PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00242: AFT PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0287685)

Part: WEB — CRACKED (BS 674 L14L) · airframe 44,579 hrs · 31,353 cycles

CRACK ON OUT WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR. SUMMARY OF NRC 00252: OUTER WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R REPAIR 1. (LP #0288528)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,612 hrs · 30,508 cycles

AFT CARGO SLANT PANEL DAMAGED LT SIDE FWD OF CARGO DOOR. REMOVED SLANT FLOOR PANEL PER B717 AMM 25-58. FABRICATED AND INSTALLED PANEL PER ER/A 612079-14 REV 0 SECTION I PERMANENT REPAIR. OK FOR SVC. (LP #4095470)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,129 hrs · 30,095 cycles

SEVERAL EMERGENCY LIGHTS IN THE CABIN COMPARTMENT ARE INOPERATIVE OR DIE IN LESS THAN 30 SECONDS AT TAXI. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-51. BATTERY PACK LOCATIONS REPLACED ARE B5-116, -227, -120, -230, AND -231. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #4783266)

Part: NONE — NONE · airframe 41,398 hrs · 28,570 cycles

SHIP 9559 - DE/HYD - THE CREW DECLARED AN EMERGENCY ON DESCENT FOR LANDING DUE TO THE RIGHT HYDRAULIC SYSTEM FLUID LOSS. THE ALTERNATE LANDING GEAR EXTENSION PROCEDURES WERE COMPLIED WITH AS PER THE QRH. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDING GEAR DOORS MAKING CONTACT WITH THE RUNWAY (DUE TO MANUAL EXTENSION). CORRECTIVE ACTION: MAINTENANCE FOUND THE RIGHT AUX ELECTRIC HYDRAULIC PUMP PRESSURE AND RETURN LINES WERE CHAFFED THROUGH. BOTH OF THOSE HYDRAULIC LINES AND BOTH MAIN GEAR DOOR BUMPERS WERE REPLACED. (LP #8790546)

Part: NONE — NONE · airframe 40,015 hrs · 27,292 cycles

DURING THE EMERGENCY LIGHT CHECK ON A SERVICE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT OVER WING EVACUATION LIGHTS TO BE INOPERATIVE. SUMMARY SEE NRC 053-0001:0514-2001/006 00431: MAINTENANCE REPLACED THE OVER WING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER B717 AMM 33-51-06-400 801. OPERATIONAL CHECK WAS GOOD. (LP #2143236)

Part: NONE — NONE · airframe 39,988 hrs · 27,269 cycles

THE TAILCONE RELEASE LANYARD IS WORN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/001 00429: REPLACED LANYARD REF B717 AMM 53-52-01 AND RIG TO BE ACCOMPLISHED ON AMDS 5352-4002. (LP #2141050)

Part: NONE — NONE · corrosion level 2 · airframe 39,988 hrs · 27,269 cycles

SUPPLEMENTAL INFORMATION: 001-0210:5300-1001/001 00403 INSTALLED FWD CARGO, LOWER DOOR PAN PER B717 SRM 53-20-15-2R PROCEDURE 6. CORROSION LEVEL CLASSIFIED AS LVL 1. CLOSING REQUIREMENTS RII: INSPECTOR 00899097. FORWARD CARGO COMPARTMENT, LOWER DOOR JAM HAS MULTIPLE AREAS OF CORROSION AROUND DOOR STOPS AND SCUFF PLATE ATTACH HOLES. MARKED AND PHOTO. SUMMARY SEE NRC 001-0210:5300-1001/001 00403. (LP #2139553)

Part: NONE — NONE · airframe 39,988 hrs · 27,269 cycles

SHIP 9559 - THE CREW DIVERTED THE AIRCRAFT TO LAX DUE TO ALL THREE GEAR NOT RETRACTING WHEN SELECTED. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE GEAR HANDLE WAS DIFFICULT TO OPERATE. THE GEAR WAS CLEANED AND FUNCTIONALLY CHECKED ON JACKS SEVERAL TIMES WITHOUT ANY BINDING OF THE GEAR HANDLE. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #7008599)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 38,007 hrs · 25,722 cycles

THE AFT DOOR EMERGENCY LIGHT LESN MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.

Part: SPOILER — DELAMINATED (RT WING)

RT WING SPOILER DELAMINATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,324 hrs · 31,130 cycles

FUSELAGE SKIN DAMAGE AFT OF R1 DOOR. CUTOUT DAMAGED SECTION OF SKIN APPROX. 3" X 7.4" PER B717 SRM 53-03-01-2R-1 REPAIR 1. CUTOUT CONTAINMENT ACCOMPLISHED PER NDTSPM 06-10-01.001 QC2018. FABRICATED & ROLLED NEW DOUBLER. COUNTERSUNK, DEBURRED, TREATED, & PRIMED ALL REPAIR PARTS. INSTALLED FINGER DOUBLERS & COMPLETE REPAIR PER BOEING 717 SRM 53-03-01-2R-1 REPAIR 1 REFERENCE FIG 202 & 203 AND ERA 567881-14 REV A. SPRAY CORROSION PROTECTION ON THE INSIDE OF THE REPAIR, AND COMPLETED INSTALLED GALLEY, PAINTED OUTSIDE OF THE REPAIR PER PRI 567881-14 REV A. JOB COMPLETE. OK FOR SERVICE. (LP #0526484)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,552 hrs · 25,414 cycles

THE EMERGENCY LIGHTS AT STA 389 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE BATTERY PACK PER B717 AMM 33-51-03. (LP #5456807)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,990 hrs · 24,320 cycles

LOWER OVERWING EXIT SIGNS ARE INOPERATIVE DURING EEPLS TEST. MAINTENANCE REPLACED THE BATTERY PACK B5-119. CHECK IS OK REF AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,859 hrs · 24,237 cycles

DURING A SERVICE CHECK, MAINTENANCE THE FOUND L1 AND R1 DOOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-55. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,688 hrs · 24,116 cycles

MULTIPLE CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-121 AND B5-235 REF AMM 33-51. OPERATIONAL CHECK IS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,252 hrs · 22,334 cycles

THE EMERGENCY EXIT LIGHTS AT THE FORWARD DROP CEILING, EXIT IDENTIFIER IN FIRST CLASS CABIN AND THE SERVICE DOOR OVERHEAD LIGHT ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-529 IAW AMM 33-51. ALL CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 32,932 hrs · 22,099 cycles

EMERGENCY LIGHT LENS MISSING. INSTALLED THE LIGHT LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,370 hrs · 21,655 cycles

FOUND LT EMERGENCY LIGHT INOP. REPLACED THE LAMPS IAW AMM 33-51. OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: SKIN — CRACKED (BS 1133) · airframe 31,921 hrs · 21,308 cycles

SKIN CRACKED BS 1133 OTDB OF LONGERON2L. REPAIRED THE SKIN IAW ER/A 553669-14AD REV 0.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,929 hrs · 21,314 cycles

FORWARD CARGO HAS CORROSION ON SKIN INBOARD OF LONGERON 28L BETWEEN STA 636 AND STA 655. REMOVED CORRODED INTERNAL DOUBLER AND INSTALLED NEW INTERNAL DOUBLER BETWEEN STATIONS 636 AND 655 IAW SRM 51-41-02 AND 51-41-05 AND DWG 5940882.

Part: DOOR — CORRODED (AIRSTAIRS) · corrosion level 2 · airframe 31,929 hrs · 21,314 cycles

L1 PASSENGER DOOR AIRSTAIR DOOR HAS CORROSION IN FORWARD AND AFT LOWER CORNERS AND AROUND AND INCLUDING NUT CLIPS AND GOUGES IN LOWER FLANGE. INSTALLED NEW AIRSTAIR DOOR IAW AMM 52-63-01 420-801, AND SRM 51-40-02, 51-40-04.

Part: FRAME — CRACKED (BS 1022 BULKHEAD) · airframe 31,920 hrs · 21,307 cycles

BS 1022 BULKHEAD REAR FRAME ANGLE IS CRACKED STRINGER 7L, VERIFIED WITH HFEC . REPAIRED IAW SRM 51-70-11 REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 900-986) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

SEAT TRACK RBL 44.5 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 900 - 986. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-30-07 FIG 18, 53-00-00-1A. LOCATED AND DRILLED REPLACEMENT SEAT TRACK IAW SRM 51-40-08, INSTALLED IAW SRM 53-20-52-2R-5, 51-41-01, 51-41-02, AND 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN CUSP WEB FOUND CRACKED AT STA 832 LBL 58. UPPER CABIN CUSP WEB CRACK REPAIRED IAW SRM 53-00-55-R2-4. REMOVED AND INSTALLED SEAT TRACK TO ACCESS, IAW SRM 51-40-04-06. ALODINED AND PRIMED AREA, IAW SRM 51-10-04 PG 10. 17-21. CUSP REPAIR PERFORMED AT STA 832 LBL 58.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 31,920 hrs · 21,307 cycles

LEFT VERTICAL STAB L/E SPLICE VSS 52.267. FIRST ROW BELOW SPLICE HAD 21 LOOSE FASTENERS AND HAS 18 OVERSIZED/ELONGATED HOLES. REPAIRED ALL LOOSE FASTENERS, OVERSIZED, AND ELONGATED HOLES IAW DWG SG9555001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

RIGHT CENTER SEAT TRACK STA 556-656 RBL 44.5 HAS CORROSION AND NEED PAINT TOUCHED UP. REPAIRED SEAT TRACK SECTION RBL 44.5 BETWEEN STA 581-644 BLENDED OUT OF LIMITS IN SEVERAL AREA'S .048 MAT LOSS FROM .100 ORG IAW B717 SRM 53-20-52 FIG 101 & REPAIR 5/7001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

LEFT CENTER SEAT TRACK HAS AREAS OF CORROSION, GOUGING, AND AREAS OF MISSING PRIMER AND TOPCOAT FROM STA 556 TO STA 656. REPAIRED SEAT TRACK SECTION 44.5 BETWEEN STA 533-646 BLENDED TRACK OUT OF LIMITS MAT LOSS WAS .050 FROM .100 ORIGINAL TAG 2736 IAW SRM 53-20-52 FIG 101 AND REPAIRS 5/7001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK AT STA 520 RBL 44.5 FOUND TO BE CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK AT FS 520 RBL 44.5 WITH 3 LIP PLUG REPAIR IAW SRM 53-20-52-2R REPAIR 1 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

RIGHT CENTER SEAT TRACK STA 356 - 456, RBL 44.5 HAS CORROSION, NEEDS PAINT TOUCHED UP, GOUGES, & SCRATCHES. REPAIRED SEAT TRACK AT FS 361-365 RBL 44.5 IAW SRM 53-20-52-2R REPAIR 1 FIG 201, PRIME AND TOPCOAT APPLIED IAW AMM 51-10-00 370-803.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK AT STA 490RBL 44.5 FOUND TO BE CORRODED OUT OF LIMITS. REF NR 0200-0194. REPAIRED SEAT TRACK RBL 44.5 STA 490 IAW SRM 53-20-52-2R-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

RT INBD SEAT TRACK STA 427 CORRODED BEYOND LIMITS REQUIRES REPAIR. PERFORMED 3 LIP PLUG REPAIR AT SEAT TRACK FS 427 RBL 22 IAW SRM 53-20-52-R2 REPAIR 1 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK FOUND TO BE CORRODED OUT OF LIMITS AT STA 430-434 RBL 44.5. PERFORMED 3 LIP PLUG REPAIR AT FS 430-434 RBL 44.5 IAW SRM 53-20-52-2R REPAIR 1 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK FOUND TO BE OUT OF LIMITS AT STA 401-404 RBL 44.5. REPAIRED SEAT TRACK AT FS 401-404 RBL 44.5 WITH 3 LIP PLUG REPAIR IAW SRM 53-20-52-2R REPAIR 1 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK AT STA 552 RBL 44.5 FOUND TO BE CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK AT FS 552 RBL 44.5 IAW SRM 53-20-52-2R REPAIR 1 FIG 201 3 LIP PLUG REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

UPPER CABIN SEAT TRACK AT STA 460 RBL 44.5 FOUND TO BE CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK AT FS 460 RBL 44.5 WITH 3 LIP PLUG REPAIR IAW SRM 53-20-52-2R REPAIR 1 FIG 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

LT CENTER SEAT TRACK BL44.5L IS CORRODED AND GOUGED IN SEVERAL AREAS FROM STATION 900 TO 986 (M). REPAIRED SEAT TRACK AT FS 959 LBL 44.5 WITH 3 LIP PLUG REPAIR IAW SRM 53-20-52-2R REPAIR 1 FIG 201. BLENDED CORROSION FROM FS 900-986 ALL AREAS WITHIN LIMITS IAW B717 SRM 53-20-52-1A -1.

Part: RETAINER — CORRODED · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

TWO SPLICES FOR SEAL RETAINER HAVE LIGHT CORROSION AT BOTTOM AREA OF DOOR PAN. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICES IAW DWG 5910158 AND INSTALLED IAW SRM 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

FLC CEILING STATION 636 BL0 ANGLE CRACKED. REPAIRED CRACKED ANGLE IAW SRM 51-70-11 REPAIR 1 AND IAW DWG 9936580.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,920 hrs · 21,307 cycles

SMALL AREAS OF LIGHT CORROSION AND MISSING PAINT ON SEAT TRACK AT BL 22L STATION 197-256, UNDER GALLEYS AND LAVATORIES, MARKED. BLENDED CORROSION ON SEAT TRACK STA 197-256 BL 22L. FOUND TO BE OUT OF LIMITS. BLENDED 0.050". FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-22-01-01, 53-20-52, SRM 51-10-04 PG 24 PARA 21, 51-10-04 PG 16, PARA 12, 51-22-01 PG 5 PARA 4, 53-22-01-401.

Part: STRUCTURE — PUNCTURED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

COCKPIT FLOOR, TWO SMALL PUNCTURE HOLES WERE FOUND UNDER FLOORBOARD 211 AKF. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-00-2R-R FIG 201, ALSO ALODINE, PRIMED, AND TOPCOATED IAW SRM 51-22-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,920 hrs · 21,307 cycles

1022 BULKHEAD REAR FRAME ANGLE IS CRACKED AT STR 7R VERIFIED WITH HFEC. REPAIRED 1022 BULKHEAD REAR FRAME ANGLE AT STR 7R IAW SRM 51-70-11 REPAIR 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,302 hrs · 19,317 cycles

MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT DOOR L1 AND ALSO BETWEEN ROWS 26-29 CDE IN THE CABIN WERE INOPERATIVE. REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,187 hrs · 18,492 cycles

DURING LINE CHECK, NOTED FLIGHT DECK OVERHEAD EMERGENCY LIGHT INOPERATIVE. FOUND BATTERY PACK AND POWER SUPPLY AT B6-123 BAD AND REPLACED.

Part: FRAME — CRACKED (BS 715) · airframe 28,167 hrs · 18,474 cycles

LEFT OVERWING FRAME AT BS 715, CRACKED GREATER THAN .125". HFEC VERIFIED. REPLACED THE FRAME IAW AMDS CARD 5310-01436-03A.

Part: COVER — LOOSE (CABIN) · airframe 26,267 hrs · 17,086 cycles

EMERGENCY EXIT AISLE LIGHT LOOSE AT SEAT 19D. R & R LIGHT COVER ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,220 hrs · 17,052 cycles

RIGHT EEPLS INOPERATIVE AT ROW 2. RELAMPED EEPLS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,219 hrs · 17,051 cycles

RIGHT EEPLS LIGHT ASSEMBLY INOPERABLE AT ROW 2. RE LAMPED EEPLS IAW SIP.

Part: CONNECTOR — LOOSE (CABIN) · airframe 25,223 hrs · 16,425 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 19. SECURED CONNECTOR IAW SWPM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,554 hrs · 16,002 cycles

FWD FLASHLIGHT LOWER BATTERY INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 22,488 hrs · 14,710 cycles

EMERGENCY STANDBY LIGHT LENS COVER BROKEN AT OVERHEAD CEILING PANEL AT ROW 2. R & R COVER IAW AMM.

Part: RETAINER — CORRODED (R1 DOOR) · airframe 22,488 hrs · 14,710 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CORRODED FWD AND AFT. R & R FITTINGS IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 22,488 hrs · 14,710 cycles

C1 DOOR CUTOUT LOWER WEB SKIN CORRODED AROUND TAIL OF FASTENER STA 385. R&R JAMB PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 22,488 hrs · 14,710 cycles

C1 CUTOUT LOWER SILL PAN CORRODED. REPAIRED JAMB PAN IAW SRM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 23,268 hrs · 15,184 cycles

LEFT AILERON OUTBOARD TAB UPPER SURFACE DELAMINATED. REMOVED AND REPLACED TAB AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 210,530 hrs · 13,799 cycles

TAIL EMERGENCY EXIT OVERHEAD LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 20,957 hrs · 13,737 cycles

TAIL CONE EMERGENCY EVAC SLIDE LANYARD AFT ATTACH POINT GUIDE LOOSE. RE-SECURED LANYARD PER MM.

Part: ATTACH FITTING — LOOSE (L1 DOOR) · airframe 20,905 hrs · 13,705 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT TO SLIDE LOOSE. SECURED ATTACHMENT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 20,306 hrs · 13,313 cycles

AIRCRAFT REQUIRED EXCESSIVE RIGHT WING TRIM ON FINAL TO MAINTAIN DIRECTIONAL CONTROL, TRIM READING 72 PERCENT. FOUND LEFT LEADING EDGE FLAP DELAMINATED. REPAIRED FLAP PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT ACCESSORY COMPT WALK WAY UPPER FWD EMERGENCY LIGHT INOP AT STA 1123 CTR. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK (RT AFT LAV OVHD) AT STA 1043R IAW B717 AMM 33-15. OPS CHECK GOOD. P/N OFF/ON 803925-1 S/N OFF 95122 ON / 20720.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

TAIL COMPT OVERHEAD FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY OVER RT LAV AT STD 1043R IAW AMM 33-51. OPS CHECK GOOD. P/N OFF/ON 803925-1 S/N OFF 20307 ON 95122.

Part: CHANNEL — DAMAGED (RT MLG WW)

RIGHT MLG DOOR JAMB CHANNEL, DAMAGED. ACCOMPLISHED DOOR JAMB CHANNEL REPLACEMENT PER B717 SRM 51-41-02.

Part: STRUCTURE — CORRODED (FUSELAGE)

E/E COMPARTMENT CABIN FLOOR, STA 200, LBL 5 TO RBL 8, CORROSION. ACCOMPLISHED CABIN FLOOR DOUBLER REPAIR PER B717 SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 160 TO 200, RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: SUPPORT FITTING — CRACKED (VERTICAL STAB)

LEFT VERT STAB SUPPORT FITTING METAL CLIP, STA 1152, LONG L2L, CRACKED. ACCOMPLISHED METAL CLIP REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: CHANNEL — CRACKED (LT MLG WW)

LEFT MLG DOOR JAMB CHANNEL, CRACKED. ACCOMPLISHED DOOR JAMB CHANNEL REPLACEMENT PER B717 SRM 51-41-02.

Part: CHANNEL — CRACKED (LT MLG WW)

LEFT MLG DOOR JAMB CHANNEL, CRACKED. OPEN DEFECT.

Part: PAN — CORRODED (FUSELAGE)

FORWARD CARGO DOOR JAMB LOWER PAN, CORROSION. OPEN DEFECT.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FORWARD OVERHEAD EMERGENCY EXIT LIGHT IN AFT COMPARTMENT INOP. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASS AT B5-116 IAW AMM 33-51-03. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

TWO EMERGENCY LIGHTS INOP STA 1254 IN AFT ACCESSORY ABOVE TAIL CONE SLIDE. FOUND ON OVERNIGHT MAINTENANCE CHECK. REMOVED AND REPLACED BATTERY PACK B5-116 AT STA 1045R, OPS CHECKS GOOD.

Part: SIGN — OUT OF POSITION (CABIN)

EXIT SIGN FOUND ON AIRCRAFT FLOOR. RE-SECURED REF MM 33-28.

Part: HOLDER — BROKEN (GIRT BAR)

STATION REPORTED THAT THE R-1 DOOR SLIDE GIRT BAR HOLDER WAS BROKEN. REMOVED AND REPLACED GIRT BAR HOLDER PER MM 25-61-03 REPACKED SLIDE REF 25-61-03 (AWI).

Part: LENS — MISSING (CABIN)

EPL LENS COVER MISSING AT 2D. INSTALLED EPL LENS COVER AT 2D IAW 717 AMM 33-50.

Part: COVER — LOOSE (CABIN)

OVERHEAD ROW 21 EMER LIGHT COVER MISSING-NOT EMER LIGHT COVER IT IS A STANDBY LIGHT COVER AND IS SECURED. R&R LIGHT ASSY IAW AMM 33-51

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT ROWS 21, 22 AND 27-31 INOPERATIVE. EMERGENCY BATTERY PACK ASSEMBLY REMOVED AND REPLACED PER B717 MM 33-51.

Part: SHUTOFF VALVE — INOPERATIVE (ANTI-ICE SYS)

ON APPROACH 'WING ANTI-ICE OFF' ALERT ILLUMINATED. ACCOMPLISHED CHECK LIST AFTER LANDING "WING HEAT FAIL" ALERT ILLUMINATED. REMOVED AND REPLACED PODS CONTROLLER AND WING ANTI-ICE PROSV, AND CONNECTOR LEAK CHECKED WING TEE AREA FOUND NO DEFECTIVE WIRING TIGHTEN FITTING ON RT A/I SENSE LINE REF: B 717 36-30-11, OPS CHECK GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT)

EMERGENCY LIGHTS ON SEAT ROWS 1, 2, 3 AND 10 INOPERATIVE. REPLACED BATTERY SUPPLY ASSY.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP LOWER NR 2 GALLEY AND 1ST CLASS. REMOVED AND REPLACED POWER PACK ASSY AT STA 341, OPS CHECKED GOOD REF AMM 33-51.

Part: LANYARD — BROKEN (EVAC SLIDE)

L1 DOOR GIRT BAR LANYARD BROKEN (WHERE GIRT BAR SLIDES THROUGH LANYARD). REPLACED LANYARD IAW MM 25-61-01.