N971AT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00095: PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3. IN THE PROCESS, DOOR REMOVAL/INSTALL WAS NEEDED AND IT WAS PERFORMED PER B717 AMM B717 AMM 52-11-01. (LP #0092179)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMPARTMENT (C1). SUMMARY OF NRC 00730: CORROSION LEVEL 2. LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMPARTMENT WAS REPLACED PER B717-SRM 51-41-05-0G. (LP #0086710)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON WING BOX UPPER SURFACE STA Y=684 X=-59. SUMMARY OF NRC 00398: CORROSION LEVEL 2. WING BOX UPPER SKIN SURFACE STA Y=684 X=-59 WAS REPAIRED PER ER/A 612910-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612910 ADDED FOR AC 9533. (LP #0086025)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON PAN (2 EA) AFT UPPER SIDE BEAM 5, STA Y 425 APROX FWD UPPER SIDE STA Y 389 APROX (HINGE DOOR) AT FWD CARGO DOOR. SUMMARY OF NRC 00137: PAN AFT UPPER SIDE BEAM 5, STA Y 425 APROX FWD UPPER SIDE STA Y 389 APROX (HINGE DOOR) AT FWD CARGO DOOR WAS REPAIRED PER ERA 612903-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 612903-14 REV 4. ASSOCIATED ER/A 14-612903 ADDED FOR AC 9533. (LP #0084360)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON HOLE UPPER SURFACE NBR 28 AT RH HORIZONTAL STABILIZER CENTER BOX PLATE. SUMMARY OF NRC 00492: CORROSION LEVEL 2. HOLE UPPER SURFACE NBR 28 AT RH HORIZONTAL STABILIZER CENTER BOX PLATE WAS REPAIRED PER PRI 612928-14 REV 6 AND ER/A 612928-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS: REPAIR APPROVAL IS LIMITED TO 24 MONTHS ONLY, AFTER 06-NOV-2023 ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE ANALYSIS (DTA) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FACC AC 120-93. LOG PAGE #0053860 ASSOCIATED ER/A 14-612928 ADDED FOR AC 9533. (LP #0083286)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00706: CRACK ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT INNER SKIN WAS REPAIRED PER ER/A 613654-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613654 ADDED FOR AC 9533. (LP #0078943)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION (SEVERAL PLACES) ON TIE TRACK UPPER AND LOWER FACE BTW LONGERONS 27 TO 28 LH/RH BTW STA 817 TO STA=946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00357: CORROSION LEVEL 2. TIE TRACK UPPER AND LOWER FACE BTW LONGERONS 27 TO 28 LH/RH BTW STA 817 TO STA=946 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP #0068560)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON FRAME STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT IN REF TO NRC 00254. SUMMARY OF NRC S/N 00654: CORROSION LEVEL 2. FRAME AT STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R REP. 3, 51-41-02-0G, AND 51-41-05- 0G PAR. 8. (LP #0067245)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT CARGO (C2). SUMMARY OF NRC 00160: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT CARGO (C2) WAS REPAIR PER B717 SRM 53-20-15-2R-7. (LP #0067279)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON UPPER SKIN STA XOS 395 AT RH WING. SUMMARY OF NRC 00080: CORROSION LEVEL 2. UPPER SKIN STA XOS 395 AT RH WING WAS REPAIRED PER ER/A 612778-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612778-14 REV 2. ASSOCIATED ER/A 14-612778 ADDED FOR AC 9533. (LP #0066744)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00707: CRACK ON INNER SKIN ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B-717 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0063939)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO (C1). SUMMARY OF NRC 00222: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO (C1) WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 6. (LP #0062282)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON UNION SKIN BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00702: CORROSION LEVEL 2. UNION SKIN (FINGER DOUBLER) BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT WAS FABRICATED AND INSTALLED PER B-717 SRM 51-41-02- 0G PAR 4. (LP #0059552)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

EXFOLIATION UPPER SKIN OF CENTRAL TANK ON REAR SPAR AREA STA Y=748 AND STA XCW 1 TO 3, XCW 24 TO 26, ALSO XCW 42 TO 52 APROX AT LH MLG WHELLWELL. SUMMARY OF NRC 00195: CORROSION LEVEL 2. UPPER SKIN OF CENTRAL TANK ON REAR SPAR AREA STA Y=748 AND STA XCW 1 TO 3, XCW 24 TO 26, ALSO XCW 42 TO 52 APROX AT LH MLG WHELLWELL WAS REPAIRED PER ERA 612925-14 REV ORIGINAL SECTION I, PERMANENTE REPAIR. ASSOCIATED ERA 14-612925 ADDED FOR AC 9533. (LP #0057921)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL) BTW STA 851-870 LONG 28L IN REF TO NRC 00671. SUMMARY OF NRC 00705: CORROSION LEVEL 2. FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL) BTW STA 851-870 LONG 28L WAS REPAIRED PER B-717 SRM 53-20-70-2R PROCEDURE 1 REPAIR 1. PERFORM GVI INSPECTION EVERY 8000 CYCLES PER B717 SRM 53-20-70-2R PROCEDURE 1 REPAIR 1. (LP #0057916)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION SKIN WEB STA=201 BTW LONG 18LH TO 17LH ALSO CORROSION ON HORIZONTAL STRAP BTW STA Y=201-208 AT PAX CABIN. SUMMARY OF NRC 00674: CORROSION LEVEL 2. SKIN WEB STA=201 BTW LONG 18LH TO 17LH WAS REPAIRED PER ERA 613271-14 REV ORIGINAL SECTION I. PERMANENT REPAIR AND PRI 613271-14 REV 1. (LP #0057487)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON SEAT TRACK X=-44 BTW STA 218 TO STA 237 AT PAX CABIN. SUMMARY OF NRC 00553: CORROSION LEVEL 2. SEAT TRACK AT X=-44 BTW Y=200 TO 341 WAS DRILLED, ADJUSTED, AND REPLACED PER B717 SRM 51 -41-01-0G, PAR 6, 51-41-02-0G, 51-41-05-0G PAR 8, AND 51-40-08-0G. (LP #0049676)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

WEAR AND CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=674 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00678: CORROSION LEVEL2. FLOOR SUPPORT STA Y=674 AND X=56 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0044262)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON FRAME STA Y=1037 LONGERON 17 LH AT CPAX (W2). SUMMARY OF NRC 00407: FRAME STA 1037 LONGERON 17 LH AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 4. (LP #0043842)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

HFEC INSPECTION WAS PERFORMED ON UPPER RADIUS OF THE FRAME TAB STA Y=715 AND 01 CRACK WAS FOUND OF 0.097IN. PER CARD 5310-01436-04B. STEP 13. SUMMARY OF NRC 00194: FRAME STA 715 LH WAS REPAIRED PER AMDS CARD 5310-01436-02A. STEPS 4,7,10,14,15,16, AND 17. ASSOCIATED AA 5310-01436 ADDED FOR AC 9533. (LP #0043304)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK WAS FOUND ON WEB BTW STA Y=715 TO 756 X=44 TO X=60. SUMMARY OF NRC 00601: WEB BTW STA Y=715 TO 756 X=44 TO X=60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0041807)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

DENT ON PREVIOUS REPAIR AT LH AFT MOVABLE FLAP VANE. SUMMARY OF NRC 00539: LH AFT MOVABLE FLAP VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1, 51-70-02-2R-3, AND 51-70-02-0G REPAIR GENERAL. (LP #0041842)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN. SUMMARY OF NRC 00393: CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN WAS MANUFACTURED AND REPAIRED PER DGW 9910151-116 PER B717 -200 SRM 53-00-55-2R-4 REPAIR 4 FIG 226. (LP #0041174)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

WEAR AND DENT ON RH LOWER ANGLE NEAR TO LOWER HINGE AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00110: RH LOWER ANGLE NEAR TO LOWER HINGE AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R-16 AND DENT WAS ATTENDED WITH NRC 00651 WITH LOG #0039485. (LP #0040560)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2). SUMMARY OF NRC 00408: FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2) WAS REPAIRED PER B717-200 SRM-53-20-07-2R-4. (LP #0039065)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON LH FLOOR SUPPORTS BTW STA 160 TO STA 196 BTW X=43, STA 196 TO STA 200 BTW X=53. SUMMARY OF NRC 00683: CORROSION LEVEL 2. FLOOR SUPPORT STA 160 TO STA 196 BTW X=43 WAS ADJUSTED AND DRILLED PER B717-200 51-40-08-0G AND FLOOR SUPPORT STA 196 TO STA 200 BTW X=53 WAS FABRICATED PER DWG 9910078 REV JC AND WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0039420)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON SUPPORT BTW STA Y=1056-1022 X=-54 AT CPAX. SUMMARY OF NRC 00672: CORROSION LEVEL 2. SUPPORT BTW STA Y=1056-1022 X=-54 WAS FABRICATED AND REPLACED PER DRAWING 9981474 REV H, B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0038822)

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 58,733 hrs · 41,217 cycles

CORROSION WAS FOUND AT HINGE HOLES AT LH WING. SUMMARY NRC 00598: FLAP HINGE WAS REPLACED PER B717-200 AMM 57-55-25 AND EFECTIVITY WAS VERIFIED PER B717-200 IPC 57-51-32-01. (LP #0039472)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

WEAR ON PAN STA 954 AND 990 BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2. SUMMARY OF NRC 00134: INNER PAN ON STA 954 AND 990 BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2 WAS REPAIRED PER B717-200 SRM 52-30-02-2R-8. SEAL RETAINER (STA 954) BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2 WAS MANUFACTURED AND REPLACED PER DWG 5910157 REV CW. ALSO SEAL RETAINER (STA 990) BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2, MANUFACTURATED IN THE NRC 00140, WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0034836)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,283 hrs · 40,857 cycles

CORROSION ON WEB, BOTH SIDES, BTW STA 178 TO STA 218, BTW X=-44 AND -52 RH SIDE AT CPAX. SUMMARY OF NRC 00366: CORROSION LEVEL 2. CUSP WEB BTW STA 178 TO STA 218, BTW X=-44 AND -52 RH SIDE WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1 FIG 201. (LP #0033204)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON INNER PAN (2 EA) BEAM 5 UPPER FWD SIDE, BEAM 3 AFT SIDE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00146: INNER PAN (2 EA) ON BEAM 5 UPPER FWD SIDE AND ON BEAM 3 AFT SIDE AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0034108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON CUSP WEB STA Y=341 WAS FOUND AFTER SEAT TRACK STA Y=-44 REMOVAL. SUMMARY OF NRC 00606: CUSP WEB STA Y=-44 STA Y=341 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 221. (LP #0025272)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON CUSP WEB STA 636 AND X=50 AT CPAX. SUMMARY OF NRC 00396: CUSP WEB WAS REPAIRED PER B717 SRM 51-70-10 2R PROCEDURE 2 PAR 4. (LP #0025277)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,283 hrs · 40,857 cycles

CRACK ON CUSP WEB (BELOW) BTW STA Y=252 AND X=-46 AT CABIN PAX. SUMMARY OF NRC 00390: CUSP WEB STA Y=252 AND X=-46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-REPAIR 4 FIG 221. (LP #0023628)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,754 hrs · 40,391 cycles

LIGHTNING STRIKE DAMAGE LOCATED ON STATION 1166, LH SIDE OF FUSELAGE. (LABELED #7) COMPLIED WITH ER/A 610530-14 REV ORIG. ALL PRI REVISION INSTRUCTIONS ARE COMPLIED WITH AND MATCH FINALE ER/A 610530-14 REV ORIG SECTION I PERMANENT REPAIR INSTRUCTIONS. FUSELAGE / TAIL SECTION / SKIN / CANT STA 1178.225 AND BELOW L-25L / LIGHTNING STRIKE DAMAGE PERMANENT REPAIR. ASSOCIATED ER/A 14-610530 ADDED FOR AC 9533. (LP #2871607)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,754 hrs · 40,391 cycles

LIGHTNING STRIKE DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L. (LABELED #1) REPAIRED SKIN DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L PER B717 SRM 53-03-01-2R PROCEDURE 1. CLASS II REPAIR ZONE 1. EXTERNAL LFEC OR EXTERNAL ULTRASONIC INITIAL INSPECTION AT 28,000 CYCLES AND REPETITIVE INSPECTION AT 15,000 CYCLES REFERENCE B717 SRM 53-03-01 PAGE 12 202. (LP #2869857)

Part: POWER SUPPLY — INOPERATIVE · airframe 55,338 hrs · 38,214 cycles

THE LEFT AFT OVERWING EXIT ILLUMINATOR IS INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EXIT POWER SUPPLY. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51-06. (LP #8628970)

Part: ANTI-SKID SYS — WARNING MESSAGE · airframe 55,338 hrs · 38,214 cycles

SHIP 9533 - DUE TO THE "ANTI-SKID FAIL" MESSAGE CYCLING ON & OFF AT LEAST THREE TIMES ON APPROACH, A GO-AROUND WAS EXECUTED. THE MESSAGE HAPPENED AGAIN ON THE SECOND APPROACH, SO THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. THIS IS A REPEAT OF AN EARLIER ODI EVENT THE SAME DAY. CORRECTIVE ACTION: MAINTENANCE PERFORMED A BITE CHECK OF THE BCU AND NO FAULTS WERE FOUND. THE RELAYS R2-5037 & R2-5052 WERE REPLACED AS A PRECAUTION. MULTIPLE GEAR SWING WERE ALL GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #8628964)

Part: ANTI-SKID SYS — WARNING MESSAGE · airframe 55,338 hrs · 38,214 cycles

SHIP 9533 - WHILE ON APPROACH, THE CREW NOTICED THE "ANTI-SKID FAIL" MESSAGE WAS CYCLING ON & OFF. A GO-AROUND WAS EXECUTED, BUT MESSAGE PERSISTED SO AN EMERGENCY WAS DECLARED BY ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: CONTRACT MAINTENANCE PERFORMED A BITE CHECK OF THE BCU AND NO FAULTS WERE FOUND. THE AIRCRAFT CONTINUED IN SERVICE ONLY TO REPEAT AT THE NEXT APPROACH FOR LANDING. (LP #8628962)

Part: NONE — NONE · airframe 55,166 hrs · 38,055 cycles

SHIP 9533 - THE CREW DECLARED AN EMERGENCY FOR AN ANTI-SKID FAIL MESSAGE ON FINAL APPROACH. THE QRH WAS COMPLIED WITH, AND ON THE NEXT APPROACH, THE FAILURE MESSAGE DID NOT RETURN. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT LANDING GEAR INTERLOCK RELAY (R2-5052) AND THE ANTI-SKID BRAKE CONTROL UNIT PER B-717 AMM 32-45-00. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #8549756)

Part: NONE — NONE · airframe 54,217 hrs · 37,200 cycles

SHIP 9533 - THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE "RT GEAR UNSAFE" INDICATION ILLUMINATING SHORTLY AFTER TAKEOFF. ON APPROACH, THE GEAR WAS SELECTED DOWN AND THREE GREEN "DOWN & LOCKED" INDICATIONS ILLUMINATED. CORRECTIVE ACTION: THE AIRCRAFT WAS FERRIED TO ATL WHERE MAINTENANCE FOUND ONE OF THE RT MLG UP-LOCK SPRINGS MISSING. THE SPRING WAS REPLACED, THE PROX SENSOR WAS ADJUSTED, AND GEAR SWINGS WERE PERFORMED WITHOUT ANY FURTHER FAULTS. (LP #8421858)

Part: NONE — NONE · airframe 54,037 hrs · 37,032 cycles

THE OVERHEAD CABIN CEILING EMERGENCY LIGHTS ARE OUT AT ROWS 1-4 AND 10-13CDE. MAINTENANCE REPLACED THE BATTERY PACK AT 10CDE PER B717 AMM 33-51. THE EMERGENCY LIGHTS OPERATIONAL CHECK IS GOOD. (LP #5362028)

Part: NONE — NONE · airframe 53,992 hrs · 36,992 cycles

REF NRC 503: CRACK FOUND ON APU EXHAUST DUCT MATING FLANGE. MARKED. NRC 503: COMPLIED WITH PRI 594460-14 REV 3 AND ERA 594460- 14 REV ORG (PRI AND ERA MATCH). (LP #1977938)

Part: NONE — NONE · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

CORROSION AFT CARGO STR30 STA870-990. (MKD). SUMMARY SEE NRC 056-0008:5331-2001/002 00294: REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1971678)

Part: NONE — NONE · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

CORROSION AFT CARGO STR29L STA870-960. (MKD). SUMMARY SEE NRC 056-0008:5331-2001/001 00293: REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1971674)

Part: NONE — NONE · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

SHEAR TIE @ STA 974 IS CORRODED BETWEEN STR 29L AND STR 30. LSUMMARY SEE NRC 056-0008:5331-2001/009 00449: REPLACED PER DWG #9958215 AND B-717 SRM 51-40-02. (LP #1968275)

Part: NONE — NONE · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

SHEAR TIE @ STA 954 IS CORRODED BETWEEN STR29L AND STR30. SUMMARY SEE NRC 056-0008:5331-2001/010 00450: REPLACED PER DWG #9958214 AND B717 SRM 51-40-02. (LP #1968271)

Part: NONE — NONE · airframe 53,999 hrs · 36,997 cycles

AFT CARGO DOOR CUTOUT: SKIN CRACKED AND BENT LOCATED DIRECTLY FWD OF THE STOP FITTING SECOND FROM THE BOTTOM AFT SIDE. MARKED. COMPLIED WITH B717 SRM 53-20-15-2R PROCEDURE 10 OPTION 2. (LP #1967266)

Part: DOUBLER — CORRODED (BS 1053) · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

SEVERE CORROSION FOUND ON L-DOUBLER UNDER FRAME 1053. SUMMARY SEE NRC 055-0022:5310-2014/007 00470: REPLACED PER DWG# 9915561. (LP #1967265)

Part: NONE — NONE · corrosion level 2 · airframe 53,955 hrs · 36,960 cycles

CORROSION FWD / LWR / CTR. (MKD). SUMMARY SEE NRC 055-0022:5310-2014/001 00292: REPLACED TRIANGLE DOUBLER PER DWG #5910130. BLENDED AND CHECKED LIMITS ON P-DOME SKIN PER B717 SRM 53-20-08-2R. (LP #1964541)

Part: REGULATOR — FAULTED (TAIL) · airframe 53,487 hrs · 36,538 cycles

SHIP 9533 - THE FLIGHT CREW RECEIVED A "TAIL MANIFOLD FAIL" TWICE ON DESCENT IN TO AVL AND DIVERTED TO CLT. AN EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MAINTENANCE REPLACED THE TAIL PRESSURE REGULATING AND SHUTOFF VALVE AND RE-SECURED PNEUMATIC SENSE LINE ON TAIL ANTI-ICE VALVE. (LP #7645696)

Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 52,487 hrs · 35,721 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS DAMAGED OR MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY L2-791 FIRST CLASS MIDDLE AISLE, REF SWPM CH 20 AND B717 WDM 33-51-12. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,455 hrs · 35,697 cycles

THE EMERGENCY OVERHEAD LIGHT AND EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT AT THE L1 DOOR WAS NOTED BY THE FLIGHT ATTENDANT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235, PER B717 AMM 33-56. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 51,684 hrs · 35,029 cycles

THE LT OVERWING EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LT OVERWING EMERGENCY LIGHT IAW AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: FRAME — CRACKED (BS 696) · airframe 48,754 hrs · 32,801 cycles

L/H OVERWING FRAME AT STA 696 CRACKED REF 5310-01436-04A STEP #10. NRC 034-0001:5310-01436-04A/001 00021: REPLACED FRAME PER ROUTINE CARD 5310-01436-03A. (LP #0957078)

Part: DOOR SILL — DAMAGED · airframe 48,754 hrs · 32,801 cycles

DURING BUY BACK OF BLEND REPAIR FOUND LOW SPOT ON AFT CARGO COMPTARTMENT DOOR SILL AFT OF DOOR DOWN STOP FITTING. MKD. NRC 001-0307:5231-2002/006 00178: REPLACED DOOR JAMB REF B717 SRM 53-20-15-2R PROCED 7. (LP #0955479)

Part: RETAINER — BROKEN (TAILCONE SLIDE) · airframe 48,096 hrs · 32,359 cycles

WHILE WORKING WORK CARD, THE TAILCONE ESCAPE SLIDE SAFETY PIN INSPECTION REVIELED THAT THE TAIL CONE SLIDE COVER CLIP RETAINER WAS BROKEN. A NEW TAILCONE ESCAPE SLIDE COVER CLIP RETAINER WAS INSTALLED PER ZODIAC AEROSPACE CMM 25-66-20. (LP #4860405)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,644 hrs · 30,712 cycles

ON SERVICE CHECK, MAINTENACE FOUND FOUR EMERGENCY EXIT LIGHTS, IN THE TAIL COMPARTMENT PASSAGE WAY TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-260) IAW AMM 33-51. OPS CHECK WAS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 44,272 hrs · 29,763 cycles

STANDBY DIFFUSER LENS IS MISSING AT ROW 27. INSTALLED SERVICEABLE LENS COVER ON EMERGENCY LIGHT AT ROW 27, OPS CK NORMAL.

Part: SKIN — CRACKED (BS 1133) · airframe 43,628 hrs · 29,301 cycles

SKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 ON THE RIGHT SIDE OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555587-14AD, REV O.

Part: SKIN — CRACKED (BS 1133) · airframe 43,628 hrs · 29,301 cycles

SKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 TO THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555586-14AD REV 0.

Part: SKIN — CORRODED (BS 737) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

LARGE AREA OF BLOW OUT CORROSION BS 737 TO SLANT PANEL LBL 4. REPAIRED THE AREA IAW ERA 555592-14 REV 0.

Part: PAN — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

FWD CARGO DOOR FRAME CORRODED IN SEVERAL PLACES. REPAIRED CARGO FRAME PAN IAW SRM 53-20-15-2R.

Part: SKIN — CRACKED (BS 1152) · airframe 43,628 hrs · 29,301 cycles

SKIN CRACKED ON THE TOP OF THE FUSELAGE AT BS 1152 ON THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN CRACK IAW ER/A 555585-14, AND PRI 555585-14, REV 0 AND 1.

Part: FRAME — CORRODED (BS 946) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

CORROSION FRAME BS 946 BETWEEN LONGERONS 29 - 30R. REPAIRED IAW SRM 53-00-06-2R-2, AND 51-32-01.

Part: ANGLE — CORRODED (BS 158-229) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

R1 DOOR FRAME LOWER TRIANGLE POCKETS HAVE CORROSION. REPLACED RIGHT CUSP ANGLE FROM BS 158 TO 229 IAW SRM 53-00-55, REPAIR 3, SRM 51-41-02, & SRM 51-41-05.

Part: SEAT TRACK — DAMAGED (BS 200-256) · airframe 43,628 hrs · 29,301 cycles

SEAT TRACK BS 200 - 256, RBL 44.5, GOUGED AND CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 53-20-52-1A-1, FIG 201, SRM 51-40-02-0G, 51-40-04, 51-41-08-0G, AND 51-41-05-0G.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 43,628 hrs · 29,301 cycles

RIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REMOVED FWD VANE, REPAIRED THE DELAMINATED AREA WITH A DOUBLER IAW SRM 57-53-01-2R-1, PARA 4B-4C, AND SRM 51-70-07-0G. INSTALLED THE VANE IAW AMM 27-50-03 400-801.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,628 hrs · 29,301 cycles

STA 1022 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED AT FORMER LWR FWD FASTENER (EXTERNAL). HFEC VERIFIED IAW NDT SPM 06-10-01-.001 ETHF PROCEDURE 1, CUT OUT REGION OF EXTERNAL SKIN AND INTERNAL DOUBLER AND INSTALLED REPAIR AT FS 1022 ABOVE LONGERON 14L IAW ER/A 555589-14.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 43,628 hrs · 29,301 cycles

RIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REPAIRED THE VANE IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G. RESTORED FINISH IAW AMM 51-10-00 370-805.

Part: ATTACH ANGLE — CHAFED · airframe 43,628 hrs · 29,301 cycles

ATTACH FLANGE UNDER PANEL 370AL CHAFED. THE ATTACH ANGLE WAS FOUND TO BE CRACKED, REPLACED THE ATTACH FLANGE IAW DWG 5910242, AND SRM 51-41-02.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,628 hrs · 29,301 cycles

LT CANTED KEEL FORMERS ARE CRACKED O/B ENDS STA 674, 696, 715. REPAIRED LT CANTED KEEL FORMERS IAW ER/A 545683-14MA REV 0.

Part: SEAT TRACK — DAMAGED (BS 756-856) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

LEFT CENTER SEAT TRACK BS 756 - 856, LBL 44.5 HAS SCRATCHES, AND CORROSION. BLENDED THE SEAT TRACK. REPAIRED IAW 53-20-52 REP 5.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

CORROSION ON RT SIDE CUSP WEB AT FUSELAGE SKIN SPLICE BETWEEN FRAME STA 579-598 BELOW FLOOR. FOUND CORROSION TO BE ON CUSP ANGLE SPLICE ONLY. REPLACE CUSP ANGLE SPLICE IAW DWG 9910151 AND SRM 51-40-02.

Part: CUSP WEB — CRACKED (BS 814) · airframe 43,628 hrs · 29,301 cycles

FOUND CRACKED CUSP WEB AT BS 814, LBL45. REMOVED THE DAMAGED SECTION OF THE CUSP WEB AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 221.

Part: SKIN — CRACKED (BS 1087) · airframe 43,628 hrs · 29,301 cycles

BS 1087 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED. HFEC VERIFIED IAW NDT SPM 06-10-01.001 ETHF PROCEDURE 1. REPAIRED IAW ERA 555590-14 REV 0.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

CUSP MEMBRANE AT RT STA 180 CORRODED. BLENDED CORROSION OUT OF LIMITS IAW SRM 53-00-55 FIG 101 ORIGINAL THICKNESS .020, .020 REMOVED. REPAIRED CUSP MEMBRANE IAW ER/A 551819-14MA2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

UPPER FUSELAGE, RIGHT INBD SEAT TRACK, STA 200 TO STA 256 BL22R, GOUGED AND CORRODED METAL. CORROSION AT STA 235 RBL 22 EXCEEDED 50% OF ORIGINAL THICKNESS, FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 1A-1, 51-30-07-0G. INSTALLED NEW SECTION OF SEAT TRACK RBL 22 STA 200-307 IAW SRM 51-41-01 & 51-41-05. INSTALLED NEW SPLICE STA 307 IAW SRM 51-41-05 & 53-20-52 2R-5.

Part: SEAT TRACK — CORRODED (BS 429) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

RIGHT INBD SEAT TRACK, RBL 22, BS 429 IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-20-52-2R.

Part: SEAT TRACK — CORRODED (BS 358-456) · corrosion level 2 · airframe 43,628 hrs · 29,301 cycles

RIGHT INBD SEAT TRACK, RBL 22, BS 358 - 456 HAS AREAS OF LIGHT CORROSION AND MISSING PAINT. BLENDED THE SEAT TRACK. FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK BS 400-403 IAW SRM 53-20-52-2R.

Part: CUSP WEB — DAMAGED (BS 612) · airframe 43,628 hrs · 29,301 cycles

CRACK AND CORROSION AT THE UNDERSIDE OF THE CUSP WEB AT BS 612, RBL 56. REPAIRED THE CUSP WEB IAW SRM 53-00-55 2R-4.

Part: PAN — CRACKED (DOOR) · airframe 43,628 hrs · 29,301 cycles

FLC DOOR FWD SIDE AT LOCKING LATCH BRACKET LOOSE AND DOOR PAN CRACKED. REPAIRED THE PAN IAW SRM 52-30-02-2R PROCEDURE 4, FABRICATED A REPAIR DOUBLER IAW SRM 51-22-01, PAGES 2 - 5. TIGHTENED LATCH BRACKET IAW SRM 51-41-01, FIG 1.

Part: PAN — CRACKED (DOOR) · airframe 43,628 hrs · 29,301 cycles

FLC DOOR AFT SIDE AT LOCKING LATCH BRACKET LOOSE AND CRACKED DOOR PAN. REPAIRED THE DOOR PAN IAW SRM 52-30-02-2R PROCEDURE 4.

Part: TERMINAL — LOOSE (BATTERY PACK) · airframe 43,314 hrs · 29,094 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY CONNECTION WAS LOOSE. THE BATTERY CONNECTOR WAS SECURED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,426 hrs · 28,473 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LANYARD — DISCONNECTED (L1 DOOR SLIDE) · airframe 41,824 hrs · 27,964 cycles

F/A DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A DISCONNECTED LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REINSTALLED THE DOOR SLIDE LANYARD IAW AMM 25-61.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,350 hrs · 27,575 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 1-5 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LANYARD — UNSECURE (L1 DOOR SLIDE) · airframe 40,697 hrs · 27,063 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE LANYARD AT THE 1L DOOR WAS NOT SECURED. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR SLIDE LANYARD WAS RESECURED.

Part: FIRE DETECTOR — FALSE ACTIVATION (LT NACELLE) · airframe 40,408 hrs · 26,830 cycles

RETURNED TO DEPARTURE DUE TO LT ENGINE FIRE WARNING. CREW ACCOMPLISHED QRH PROCEDURES. BOTH FIRE BOTTLES WERE UTILIZED AND FIRE WARNING REMAINED WITH ENGINE SHUTDOWN. MAINTENANCE REPORTED FIRE INDICATION ILLUMINATED AFTER ACFT ARRIVED AT THE GATE. DISCONNECTED LT ENGINE FIRE DETECTOR CONTROL UNIT AND FIRE INDICATION EXTINGUISHED. R & R FDCU AND ACCOMPLISHED CHECK OUTS IAW AMM. R & R BOTH FIRE BOTTLE ASSEMBLIES IAW AMM. C/W ENGINE IFSD CHECKOUTS IAW AMM.

Part: DOOR FRAME — CRACKED (BS 715) · airframe 39,889 hrs · 26,423 cycles

DURING LT OVERWING FRAME 715 INSPECTION, HFEC CONFIRMED CRACK .125" DEEP. REPAIRED IAW AMDS WC 5310-01436-03A.

Part: CUSP WEB — DAMAGED (BS 674-715) · airframe 39,889 hrs · 26,423 cycles

DURING OVERWING FRAME INSPECTION, FOUND CUSP WEB FROM BS 674 - 715 LT SIDE DAMAGED. REPAIRED IAW ER/A 533035-14MA AND SRM 51-02, PAGE 1.

Part: CUSP WEB — CRACKED (BS 591) · airframe 39,887 hrs · 26,422 cycles

CUSP WEB UNDER SEAT TRACK SPLICE AT STA 591, LBL 55 IS CRACKED. REPAIRED IAW DWG 9910151-115.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,130 hrs · 25,822 cycles

FUSELAGE SKIN AT STA 189 229; L15L L18L. REPAIR IAW ERA 534894-14 LOG 1888058.

Part: COVER — WRONG PART (SLIDE CABLE) · airframe 39,130 hrs · 25,822 cycles

DURING THE PRIOR TO SERVICE, PART 121 INSPECTION, IT WAS NOTED THE HEAT SHRINK PROTECTIVE COATING AROUND THE TAIL SLIDE CABLE WAS NOT THE CORRECT TYPE MATERIAL. IT WAS WHITE AND SHOULD BE CLEAR. THE HEAT SHRINK AROUND THE TAIL SLIDE CABLE WAS REPLACED WITH THE PROPER TYPE MATERIAL. LP 1896830.

Part: SKIN PANEL — DENTED (RT WING) · airframe 47,256 hrs · 31,806 cycles

DENT INSPECTION RT WING PANEL, UPPER SKIN - QTY 7. PANEL 630ZB, APPROX 12.5" FROM I/E AND 7.5" FROM T/E STA XRS 49022.5" FROM T/E. PANEL 630ZB ,APPROX 54" FROM I/E AND 3.5" FROM T/E. PANEL 630ZB, APPROX 44.5" FROM I/E AND 5.5 FROM T/E. PANEL 630ZB, APPROX 53" FROM I/E AND 4" FROM T/E. PANEL 630ZB, APPROX 45" FROM I/E AND 7" FROM T/E. PANEL 630ZB, APPROX 10.5" FROM I/B AND 8" FROM T/E. RT WING PANEL 630ZB WAS REPLACED ON ORNRC.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,976 hrs · 25,715 cycles

TAIL COMPARTMENT AFT LT RAIL EMER EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 38,976 hrs · 25,715 cycles

AFT CARGO DOOR FWD HOLD OPEN BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,976 hrs · 25,715 cycles

AFT EMER EXIT BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,976 hrs · 25,715 cycles

AFT LT OVERWING EMER EXIT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,976 hrs · 25,715 cycles

TAIL COMPARTMENT CAT WALK EMER EXIT LIGHT NR 41 BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,976 hrs · 25,715 cycles

TAIL COMPARTMENT CAT WALK EMER EXIT LIGHT NR 31 BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,976 hrs · 25,715 cycles

AFT FLIGHT ATTENDANT STATION LOWER EMER EXIT SIGN LIGHT BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 38,976 hrs · 25,715 cycles

TAIL COMPARTMENT LT VENT BOX UPPER PANEL COVER CRACKED. R & R PANEL IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,976 hrs · 25,715 cycles

TAIL COMPARTMENT AFT HAND RAIL EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 38,976 hrs · 25,715 cycles

CEILING EMER EXIT SIGN LIGHT LENS CRACKED AT ROW 1. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,976 hrs · 25,715 cycles

AFT LT OVERWING EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,699 hrs · 24,847 cycles

L1 DOOR EMER EXIT LOWER LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR EMER EXIT LOWER LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,699 hrs · 24,847 cycles

AFT CABIN EMER SIGN BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW AMM. PN OFF 803925-1, SN OFF 21024, PN ON 803925-1 & SN ON 20568.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 37,699 hrs · 24,847 cycles

TAIL CONE RELEASE SYS KEVLAR CABLE FRAYED. R & R CABLE IAW AMM.

Part: NUT PLATE — DAMAGED (L1 DOOR) · airframe 37,699 hrs · 24,847 cycles

L1 DOOR FWD & AFT GIRT BAR FITTING ATTACH NUTPLATE DAMAGED. R & R NUTPLATE IAW SRM.

Part: NUT PLATE — MISSING (R1 DOOR) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR FWD GIRT BAR FITTING MISSING NUTPLATE. INSTALLED NUTPLATE IAW SRM.

Part: NUT PLATE — MISSING (R1 DOOR) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR AFT GIRT BAR FITTING MISSING NUTPLATE. INSTALLED NUTPLATE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

CO-PILOT AFT OTBD SEAT TRACK SUPPORT, RAIL, CORRODED. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

FLIGHT COMPARTMENT FLOOR SKIN WEB CORRODED BETWEEN CO-PILOT SEAT AFT SEAT TRACKS. R & R SKIN IAW SRM & DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR EMER EXIT IDENTIFIER ASSEMBLY CRACKED. R & R R1 DOOR EMER EXIT IDENTIFIER ASSEMBLY IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 37,699 hrs · 24,847 cycles

RIGHT AFT OVERWING EMER EXIT IDENTIFIER ASSEMBLY CRACKED. R & R IDENTIFIER ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,699 hrs · 24,847 cycles

RIGHT FWD OVERWING EMER EXIT IDENTIFIER ASSEMBLY INOPERATIVE. R & R IDENTIFIER ASSEMBLY IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 237, BETWEEN LBL 12 - RBL 12. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

FLOORBOARD 211ALF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FAIRING — CRACKED (AILERON TAB) · airframe 37,699 hrs · 24,847 cycles

LEFT WING AILERON FWD TRIM TAB FAIRING 530HA CRACKED ON PARTS RACK. R & R FAIRING IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

FALSE TRACK UNDER PANEL 221CF, CORRODED BETWEEN BS 160 - 200, LBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 37,699 hrs · 24,847 cycles

CUSP WEB CRACKED BETWEEN BS 218 - 227, BETWEEN RBL 44.5 - 60. R & R CUSP WEB IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR, LOWER JAMB AREA FLOOR PANEL UPPER SURFACE CORRODED FWD & AFT OF ESCAPE SLIDE GIRT BAR FITTINGS. R & R SURFACE IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (R1 DOOR) · airframe 37,699 hrs · 24,847 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR AFT FLOOR MOUNT FITTING CORRODED. R & R FITTING IAW & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 37,699 hrs · 24,847 cycles

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

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 37,699 hrs · 24,847 cycles

RIGHT WING INBD SPOILER LOWER SURFACE DELAMINATED NEAR CTR. R & R PANEL IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,866 hrs · 25,642 cycles

RIGHT EEPLS INOPERATIVE AT ROW 1. RELAMPED EEPLS IAW AMM.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 38,095 hrs · 25,118 cycles

FORWARD FLASHLIGHT FAULTY. R & R BATTERY IAW MM.

Part: PANEL — DAMAGED (NLG)

DURING LINE CHECK, NOTED THE NOSE GEAR HORSESHOE PANEL, WAS DAMAGED BY FOD. THE PANEL WAS REPLACED IAW DWG 5913421, SHEET 1, ZONE 2. THE INSTALLATION WAS INSPECTED AS REQUIRED.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 37,938 hrs · 25,010 cycles

FORWARD EMER FLASHLIGHT BATTERY LOW. R & R BATTERY IAW AMM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 37,086 hrs · 24,453 cycles

DIVERSION RT ENG SURGED, COMPRESSOR STALLED ENROUTE. R & R NR 2 ENG IAW MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,812 hrs · 24,279 cycles

AFT NR 1 FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: WIRE — EXPOSED (COCKPIT) · airframe 35,572 hrs · 23,493 cycles

AIR TURNBACK ELECTRICAL SMELL AFTER DEPARTURE IN FLIGHT DECK. FOUND EXPOSED WIRE ON CAPTAINS YOKE MAP LIGHT. REPAIRED WIRE ON YOKE MAP LIGHT IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 35,149 hrs · 23,242 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

CUSP WEB CRACKED AT STA 674, LBL 45. REPAIRED WEB IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 34,429 hrs · 22,794 cycles

LEFT WING PANEL 520CB CRACKED FASTENER HOLE TO FASTENER HOLE. R & R PANEL IAW AMM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED BETWEEN BS 427 TO BS 399, RBL 44.5. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED AT BS 579, LBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

SEAT TRACK CORRODED BETWEEN STA 617 TO STA 646, LBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: PANEL — CORRODED (RT WING) · airframe 34,429 hrs · 22,794 cycles

RIGHT WING PANEL 620FT CORRODED. R & R PANEL IAW SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED AT STA 484, RBL 44.5. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED AT BS 427, LBL 44.5. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOOR PANEL CORRODED BETWEEN STA 389 TO STA 408, RBL 44.5. REPAIRED PANEL IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

SUPPORT FITTING CRACKED STA 737, LBL 44. REMOVED & REPLACED FITTING IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

SEAT TRACK CORRODED BETWEEN STA 280 TO STA 427, RBL 44. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

SUPPORT FITTING CRACKED AT STA 737, RBL 44. REMOVED & REPLACED FITTING IAW SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED AT STA 465, RBL 44.5. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FLOORBOARD CORRODED AT STA 285, RBL 44.5. REMOVED AND REPLACED PANEL IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 34,429 hrs · 22,794 cycles

RIGHT WING L/E BONDING STRAPS CRACKED. REMOVED AND REPLACED STRAP IAW SRM & DWG.

Part: BRACKET — CRACKED (NLG WW) · airframe 34,429 hrs · 22,794 cycles

NLG WHEEL WELL HYDRAULIC LINE BRACKET CRACKED AT STA 69. REMOVED AND REPLACED BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (SLAT TRACK) · airframe 34,429 hrs · 22,794 cycles

RIGHT WING NR 12 SLAT TRACK L/E INBOAR SIDE ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 34,429 hrs · 22,794 cycles

RIGHT WING TO BODY SUPPORT FITTING CRACKED AT STA 665, LONGERON 22R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,429 hrs · 22,794 cycles

MAIN CABIN FLOOR PANEL 221UF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,429 hrs · 22,794 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,429 hrs · 22,794 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,429 hrs · 22,794 cycles

MAIN CABIN FLOOR PANEL 222AAF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 34,429 hrs · 22,794 cycles

LEFT WING TO BODY TO FUSELAGE ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,429 hrs · 22,794 cycles

MAIN CABIN FLOOR PANEL 222JF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LEFT CUSP WEB CORRODED AT STA 418. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FRAME CRACKED AT STA 674 FRAME BELOW CUSP WEB. REMOVED AND REPLACED FRAME IAW DWG.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FUSELAGE SKIN EXTERIOR SPLICE PLATE CORRODED AT STA 813, BETWEEN LONG 28L TO LONG 28R. R & R SPLICE PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LEFT NLG STRUT DOOR AFT HINGE CUTOUT SKIN CRACKED. REPAIRED DOUBLER IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FORWARD CARGO AFT BULKHEAD VERTICAL STIFFENER CRACKED LBL 40. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 560 TO STA 579. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT RUB STRIP CRACKED AT STA 851, LONGERON 19R. REMOVED & REPLACED RUB STRIP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED STA 508. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CRACKED AT STA 1144, LONGERON 2R. REMOVED AND REPLACED LONGERON IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 484 TO STA 465. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LEFT SIDE LOWER I/B LOWER ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LEFT CUSP WEB CORRODED BETWEEN STA 794 TO STA 813. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

OUTBOARD OF FWD CARGO AREA PAN FWD AND AFT SPLICE CORRODED. REMOVED AND REPLACED ANGLES IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CRACKED AT STA 1133, LONGERON 2R. REMOVED AND REPLACED LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CRACKED AT STA 1144, LONGERON 1. REMOVED AND REPLACED LONGERON IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT NLG STRUT DOOR, AFT HINGE CUTOUT SKIN CRACKED. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED STA 527. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 541 TO STA 560. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LEFT CUSP WEB CORRODED BETWEEN STA 503 TO STA 522. REPAIRED WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CRACKED AT STA 1133, LONGERON 2L. REPAIRED LONGERON IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT RUB STRIP CRACKED AT STA 889, LONGERON 20R. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 503 TO STA 484. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN STA 946 TO STA 954, L30. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CORRODED BETWEEN STA 947 TO STA 986, L30. REPAIRED LONGERON IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,129 hrs · 23,229 cycles

FRAME CORRODED AT STA 974, BETWEEN LONGERON 28R & 28L. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CORRODED BETWEEN STA 954 TO STA 964, L29L. REPAIRED LONGERON IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

AFT CARGO FRAME CORRODED AT STA 908, BETWEEN LONGERON 29R TO LONG 29L. REMOVED ANAD REPLACED FRAME IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CORRODED STA 974, BETWEEN LONG 28R TO LONG 28L. REPAIRED LONGERON IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

LONGERON CORRODED BETWEEN STA 947 TO STA 948, L30. REPAIRED LONGERON IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,429 hrs · 22,794 cycles

FRAME CORRODED AT STA 908. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,129 hrs · 23,229 cycles

AFT CARGO FRAME CORRODED AT STATION 908. REMOVED AND REPLACED FRAME IAW SRM.

Part: PANEL — CRACKED (CARGO BAY) · airframe 34,429 hrs · 22,794 cycles

AFT CARGO RIGHT SLANT PANEL JUST OF CARGO DOOR CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER IAW SRM.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 34,429 hrs · 22,794 cycles

FORWARD F/A SEAT EMERGENCY FLASHLIGHT BRACKET BROKEN. REMOVED AND REPLACED BRACKET IAW AMM.

Part: CABLE — LOOSE (R1 DOOR) · airframe 33,163 hrs · 21,964 cycles

R1 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE PER AMM.

Part: HANDSET — MELTED (CABIN)

AFT F/A HANDSET MELTING AND HAS A FRAYED CORD (REMOVED BY MX). REPLACED AND OPS CHECKED AFT F/A HANDSET REF AMM 23-41.

Part: LIGHT — INOPERATIVE (CABIN)

EPL LIGHT INOP AT 1DF SEAT ROW. RELAMPED EPL LIGHT AT 1DF SEAT ROW IAW MM 33-50-0. OP'S CHECKED OK.

Part: CABLE — OUT OF POSITION (GIRT BAR)

FORWARD PASSENGER ENTRANCE DOOR SLIDE GIRT BAR CABLE DISPLACED OVER SLIDE PACK. REROUTED GIRT BAR CABLE PER AMM TASK 25-31. OPS CHECK OK.

Part: DOOR FRAME — CRACKED (FUSELAGE)

RIGHT MAIN INBD DOOR FWD FUSELAGE FRAME CRACKED. INSTALLED NEW JAMB RT MLG FWD CHANNEL PER EA-17-53-03403IR SEC 2 OPS CHECK DOOR FOR FIT & CLEARANCE REF MM 32-10.

Part: LIGHT — MISSING (CABIN)

SEAT 1D EMERGENCY ESCAPE PATH LIGHT LENS AND ONE BULB MISSING, LIGHT OPERATES NORMALLY. INSTALLED LIGHT LENS AND BULB, OPS CHECK NORMAL IAW B-717 AMM 33-51-04.

Part: HANDSET — DEFECTIVE (CABIN)

AFT FLT ATTENDANT HANDSET WAS EXTREMELY HOT AND MELTING. CORD WAS VERY HOT TO TOUCH. INSTALLED AFT CABIN ATTENDANT HANDSET IAW AMM 23-41-07. INSTALLED AFT CABIN ATTENDANT HANDSET IAW AMM 23-41-07. INSTALLED AFT CABIN ATTENDANT INTERPHONE CRADLE ASSEMBLY AS REQUIRED. OPS CHECK OF SERVICE INTERPHONE, FLIGHT INTERPHONE & PA SYSTEMS NORMAL IAW AMM'S 23-41-00, 23-51-00 & 23-31-00. MDDR CLEARED. PLACARD REMOVED.

Part: SHELF — CORRODED (GALLEY)

GALLEY COMPARTMENTS 102, 103, 106 SHELF, CORROSION. ACCOMPLISHED SHELF REPLACEMENT PER EA 17-25-03119IR.

Part: DOOR FRAME — CORRODED (FUSELAGE)

INTERNAL AFT CORNER, FWD AIRSTAIR DOOR FRAME, CORROSION. ACCOMPLISHED FRAME REPLACEMENT PER B717 SRM 51-41-02.

Part: ATTACH ANGLE — BENT (ENTRY DOOR)

FORWARD ENTRY DOOR LINER LOWER ATTACH ANGLE, BENT AND ELONGATED HOLE. ACCOMPLISHED LOWER ATTACH ANGLE REPLACEMENT PER B717 SRM 51-70-11.

Part: SKIN — DENTED (FUSELAGE)

LEFT SIDE AFT OF L1 DOOR FUSELAGE SKIN, DENTED. ACCOMPLISHED FUSELAGE SKIN SKIN REPAIR PER B717 SRM 51-41-01, 51-10-04, AND 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 179 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 32 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 179 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FITTING — CORRODED (GIRT BAR)

MAIN CABIN R1 DOOR FORWARD AND AFT GIRT BAR FITTING, CORROSION. ACCOMPLISHED FORWARD AND AFT GIRT BAR FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 200, RBL 9 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 179, RBL 9 TO RBL 21, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: DOUBLER — CRACKED (FUSELAGE)

PASSENGER ENTRANCE DOOR JAMB AFT FACE DOUBLER TAB, STA 215, LONG L15L, CRACKED. ACCOMPLISHED TAB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: SIGN — OUT OF POSITION (CABIN)

OVERHEAD FORWARD EXIT SIGN FELL OFF. RESECURED AS REQUIRED.

Part: SIGN — DISLODGED (CABIN)

EXIT SIGN ABOVE BUSINESS CLASS CASE IS DISLODGED. RESECURED EXIT SIGN IN BUSINESS CLASS - REF 33-50.

Part: HOLDER — BROKEN (GIRT BAR)

GIRT BAR STOWAGE UNIT HOLDER BROKEN. REPLACED SLIDE COVER AND LANYARD AT R-1 DOOR. OK FOR SERVICE. REF 25-61.

Part: CONNECTOR — DISCONNECTED (CABIN)

THE 19 DEF EMERGENCY LIGHT INOP. RE-CONNECTED CONNECTOR AS REQUIRED. OPS CHECK GOOD.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER JAMB PAN HAS CORROSION. REMOVED CORRODED AREA AND REPLACED JAMB PAN AND REPAIRED PER B717 SRM 52-20-15 F201.

Part: DOOR FRAME — CORRODED (CARGO DOOR)

FORWARD CARGO COMPARTMENT DOOR LOWER JAMB HAS CORROSION. REMOVED CORRODED AREA AND REPLACED WITH JAMB PAN SPLICE PER B717 SRM 52-20-15.