N948AT

Part: PANEL — NOT REPORTED · airframe 64,897 hrs · 46,503 cycles

FABRICATED PANEL STILL NEEDS LIGHT ASSY INSTALLED. INSTALLED AFT COMPARTMENT LT PER B717 AMM 33-51. OP CHECK NORMAL . OK FOR SVC. (7724261)

Part: NONE — NONE (NONE) · airframe 64,869 hrs · 46,471 cycles

MONITOR LOG FOR ER/A 619015-14AD REV A SECTION II. COMPLY WITH SECTION II OF ER/A 619015-14AD (1275112)

Part: FAIRING — DAMAGED (ZONE 300 RUDDER) · airframe 64,588 hrs · 46,235 cycles

DAMAGE NOTED RUDDER FAIRING PANEL 370CR. ER/A 629084-14 CREATED TRACKING TEMPORARY REPAIR ACCOMPLISHMENT. (1191759)

Part: ACCESS PANEL — DAMAGED (ZONE 300 RUDDER) · airframe 64,588 hrs · 46,235 cycles

ENGINEERING CREATES LOGPAGE TRACKING DAMAGE TO RUDDER ACCESS PANEL PER ER/A 628805-14. ER/A 628805-14 LOGPAGE CREATED TRACKING TEMPORARY REPAIR TO RUDDER ACCESS PANEL. (1191716)

Part: NONE — NONE (NONE) · airframe 64,579 hrs · 46,225 cycles

ER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL. ER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL ON OR BEFORE 24 MONTHS FROM 26-AUG-2025. (1167637)

Part: PULLEY BRACKET — DAMAGED (ZONE 500) · airframe 64,579 hrs · 46,225 cycles

L/E CAVITY AFT OF LT #2 SLAT. REPLACED PULLEY BRACKET PER BOEING DWG 5920286 (1164395)

Part: NONE — NONE (NONE) · airframe 64,579 hrs · 46,225 cycles

SHIP 9508 TRACKING FOR DTE FOR 24 MONTHS FROM DATE OF REPAIR APPROVAL. CORRECTIVE ACTION: C/W ERA ERA 626897-14 REV ORIGINAL. (1033207)

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,579 hrs · 46,225 cycles

AFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. MARKED. SUMMARY SEE NRC 001-0319:5231-2002/001 00174: REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN, CORROSION DAMAGE SPLICE REPAIR. CHECKED AND REPLACED HI-SHEAR FASTENERS PER B717-200 SRM 51-41-04-0G AND RESTORED FINISH PER B717-200 SRM 53-00-15-2R REPAIR 1. (LP #0927921)

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,579 hrs · 46,225 cycles

AFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. REPAIRED PER REF B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN CORROSION DAMAGE SPLICE REPAIR CHECKED AND REPLACED HI-SHEAR FASTENERS PER REF B717-200 SRM 51-41-04-0G AND RESTORED FINISH PER REF B717-200 SRM 53-00-15-2R REPAIR 1. (LP #0927803)

Part: SKIN — CRACKED (HORIZONAL STAB) · airframe 63,737 hrs · 45,504 cycles

CRACK INDICATION NOTED WORKING STEP 12 OF CARD 5530-01048-02 (AD 2018-10-08) WHILE PERFORMING OPEN HOLE HFEC. RH STAB L/E CRACK INDICATION IN SKIN LAYER ONLY. COMPLIED WITH N/R CARD 001 AND ER/A 619015-14AD REV ORIGINAL SECTION I PERMANENT REPAIR.

Part: SKIN — CRACKED (VERTICAL STAB LE) · airframe 63,743 hrs · 45,509 cycles

AIRCRAFT 9508, WHILE ACCOMPLISHING HFEC INSPECTION PER WORK CARD 5530-01048-02 IN COMPLIANCE WITH FAA AD 2018-10-08, MTC FOUND THREE (3) FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE SKIN (P/N 5910189-15) BELOW ZFS 52.267 WITH CRACK INDICATIONS. THE DISCREPANT HOLES INCLUDE FASTENER HOLES 9,10 AND 12 BELOW ZFS 52.267 ON THE RHS LEADING EDGE SKIN. EACH FASTENER HOLE CRACK WAS VERIFIED TO BE ON THE SKIN LAYER ONLY. CORRECTIVE ACTION: OVERSIZE EACH DISCREPANT HOLE IN 1/64 INCREMENTS ON CENTER IN THE SKIN LAYER ONLY UNTIL THE HOLE IS CLEAN AND ROUND AND SHOWS NO CRACK INDICATIONS. FABRICATE AND INSTALL THE FLUSH COUNTERSINK REPAIR BUSHINGS IN HOLE #9, HOLE #10 AND HOLE #12 PER SG95550001. FABRICATE AN EXTERNAL REPAIR DOUBLER AND A STRUCTURAL SHIM FROM 0.125" THICK 7075-T6 CLAD SHEET WITH APPROXIMATE SIZES AND SHAPES SHOWN ON THE FIGURE 2 REPAIR SKETCH. SIZE THE REPAIR DOUBLER AND THE STRUCTURAL SHIM TO MAINTAIN 2D MINIMUM EDGE DISTANCE AT FASTENER HOLES. REPAIRED PER ER/A 619015-14AD. (LP 0413549)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,419 hrs · 44,351 cycles

THE EMERGENCY EXIT COVER IS MISSING AT 1R DOOR. MAINTENANCE INSTALLED A NEW EMERGENCY EXIT LIGHT COVER AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS NOW OK FOR SERVICE. (LP #4294606)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

DENTS (2 EA) ON INBR FIXED GUIDE VANE LOWER SKIN AT RH WING. SUMMARY OF NRC 00178: DENTS (2 EA) WITH THE MEASUREMENTS OF: DENT1 "D DIAMETER=2.000 IN, X DEPTH=0.0450, RATIO=44.444". DENT2 "D DIAMETER=1.200 IN, X DEPTH=0.0150, RATIO=80". (ET) HFEC WAS ACCOMPLISHED ON DENTED AREAS, NO CRACKS WERE FOUND AND (UT) TAP-TEST INSPECTION WAS ACCOMPLISHED 01 DISBONDS OF 1.8IN X 2.1IN WERE FOUND AND WAS REPAIRED. THEREFORE, THEY ARE NOW WITHIN LIMITS PER B717-200 SRM 57-53-01-1A-1 PAR 2 B., 57-53-01-1A PROCEDURE 1 PAR 3 A., B717 DC-MD/BOEING NDTSPM PART 9, 09-00-00, 57-53-01-1A, & DC-MD/BOEING NDTSPM PART 6, 06-10-01.001, AND 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 3. (LP #2846637)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

PUNCTURES (2 EA) ON CTR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00172: CTR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #2847265)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

PUNCTURES (4 EA) ON INBR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00033: INBR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #2846642)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

DISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE UPPER SKIN. SUMMARY OF NRC 00102: RH WING AFT MOVABLE VANE UPPER SKIN WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #2844542)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

DISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE LOWER SKIN. SUMMARY OF NRC 00103: REPAIR WAS PERFORMED ON RH WING AFT MOVABLE VANE LOWER SKIN PER B717-200 SRM 57-53-01-2R-1 PAR.4. (LP #2841425)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,608 hrs · 43,642 cycles

DISBONDS (2 EA) WERE FOUND ON LH WING INBD FIXED VANE LOWER SKIN. SUMMARY OF NRC 00104: REPAIR WAS PERFORMED ON LH WING INBD FIXED VANE LOWER SKIN PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #2841415)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 61,608 hrs · 43,642 cycles

CORROSION ON LOWER SIDE PLATE AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00122: CORROSION LEVEL 2. LOWER SECTION OF JAMB PAN WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #2837667)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 61,608 hrs · 43,642 cycles

CORROSION ON ANGLE ON AFT LOWER SEAL DEPRESSOR AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00124: CORROSION LEVEL 2. ANGLE ON AFT LOWER SEAL DEPRESSOR AT FWD CARGO COMPARTMENT DOOR JAMB WAS FABRICATED PER DWG 5910142 REV DJ AND REPLACED PER B717 SRM 51-41-02-0G. (LP #2834500)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 61,608 hrs · 43,642 cycles

CORROSION ON FLOOR SUPPORT WAS FOUND. SUMMARY OF NRC 00156: CORROSION LEVEL 2. FLOOR SUPPORT WAS FABRICATED PER DWG 993634-7 REV BW AND WAS REPLACED PER B717- 200 SRM 51-41-02-0G PAR 7, 51-41-05-0G PAR 8, AND 51-41-08-0G PAR 7. (LP #2834091)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,463 hrs · 43,502 cycles

THE LEFT FIXED FOWARD POSITION LIGHT LENSE COVER AND ATTACHING HARDWARE WAS DISCOVERED MISSING. THE LEFT FWD POSITION LIGHT LENS WAS FORWRDED TO CDL 33-42-03. ALL 'M' PROCEDURES WERE COMPLIED WITH. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9957992)

Part: LENS — MISSING · airframe 59,568 hrs · 41,836 cycles

THE THRESHOLD LIGHT LENS WAS MISSING ABOVE 29C. MAINTENANCE INSTALLED THE STANDBY LIGHT LENS COVER IN THE AFT CABIN REF B717 AMM 33-52. (LP #9299354)

Part: BATTERY — INOPERATIVE · airframe 59,013 hrs · 41,317 cycles

AFT UPPER OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-230 PER B717 AMM 33-51. (LP #8616540)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,815 hrs · 39,412 cycles

THE COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT STA 175 ABOVE R1 DOOR PER B717 AMM 33-51. (LP #7444921)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,502 hrs · 39,161 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 1C. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT COVER FOR THE FORWARD CABIN. OPERATIONAL CHECK WAS GOOD. (LP 1737515)

Part: STRUCTURE — DAMAGED (FWD CARGO DOOR) · airframe 55,885 hrs · 38,660 cycles

ON WALKAROUND FOUND DAMAGE ON FWD CARGO DOOR BOTTOM FWD CORNER. MAINTENANCE REMOVED FWD CARGO DOOR FROM A/C TO FACILITATE REPAIR, PER B717 AMM 52-31-01 020-001. CUT OUT DAMAGED AREA AS REQUIRED, PER B717 SRM 52-00-01-2R-8. PERFOREMED DAMAGE CONTAINMENT HFEC & BHEC, PER NDT SPM 06-10-01.001 AND 06-10-01.003, NO DAMAGE NOTED (QC 2013). FABRICATED AND INSTALLED REPAIR PARTS, PER B717 SRM 52-00-01-2R-8. REQUIRED INSPECTION ITEM COMPLETED (QC 5224). REINSTALLED FWD CARGO DOOR, PER B717 AMM 52-31-01420-801. GAP CHECK AND OPERATIONS CHECK GOOD. A/C OK FOR SERVICE.

Part: PLATE — MISSING (NR 2 COWLING) · airframe 55,023 hrs · 37,871 cycles

#2 ENG, UPPER COWL, INBOARD SIDE, HAS PLATE MISSING . MAINTENANCE ACCOMPLISHED SECTION I TIME LIMITED REPAIR PER ER/A 585840-14 REV ORIGINAL. COMPLIED WITH THE PERMANENT REPAIR PER ER/A 585840-14 REV O SEC II. THIS CLOSES THE MONITOR. AIRCRAFT IS OK FOR SERVICE. (LP #6935861)

Part: PLATE — MISSING (NR 2 NACELLE) · airframe 54,964 hrs · 37,830 cycles

THE #2 ENG UPPER COWL HAS A PLATE MISSING ON THE INBOARD SIDE. MAINTENANCE ACCOMPLISHED A TIME LIMITED REPAIR, PER ER/A 547093-14MA AND DEFERRED THE PERMANENT REPAIR TO MONITOR TO BE ACCOMPLISHED WITHIN 10 CALENDER DAYS OF SECT 1 ACCOMPLISHMENT. MONITOR,#2 ENG UPPER COWL HAS PLATE MISSING INBOARD. (LP #6935824)

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 54,808 hrs · 37,701 cycles

THE EMERGENCY EXIT LIGHT IS MISSING THE COVER. MAINTENANCE REPLACED THE EXIT COVER PER B717 AMM 52-22. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,685 hrs · 37,602 cycles

THE LT AND RT OVERWING EXIT IDENTIFIER SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY/ POWER PACK IAW AMM 33-51. OPERATIONAL CHECKS ARE NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 54,304 hrs · 37,325 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THAT THE CEILING MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 24 LEFT IS INOPERATIVE. RELAMPED WAS NO HELP. NO POWER TO LIGHT ASSEMBLY. FWD TO MEL 53-51-01A. PLACARDS INSTALLED. 21NOV19 RDU: FOUND PLUG P1-6724 WIRES PULLED OUT. RE-PINNED WIRING AND CONNECTOR AND NOW EMERGENCY EXIT CEILING LIGHT AT 24L WORKS REFERENCE B717 WDM 33-51-12. MEL CLEARED, PLACARD REMOVED. (LP #675427)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,270 hrs · 37,307 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT IDENTIFIERS WERE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED POWER SUPPLY B5-119. OPERATIONAL CHECK IS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6754276)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 36,655 cycles

CORROSION ON SPLICE BTW LONG 26L TO 26R AT STA Y=815 AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00421: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579396 ADDED FOR AC 9508. (LP #1168250)

Part: WINDOW FRAME — CRACKED (WINDOW) · airframe 53,358 hrs · 36,655 cycles

CRACK ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER. (CPIL). NRC 00528: REPAIR SECTION I WAS PERFORMED ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER PER ER/A 579524-14 REV ORIGINAL AND ETI-17-19-110 REV. 9. NO LEAKS WERE FOUND PER AMM 21-30-00 780-801. ASSOCIATED ER/A 00-579524 ADDED FOR AC 9508. (LP #1168456)

Part: WINDOW FRAME — CRACKED (WINDOW) · airframe 53,358 hrs · 36,655 cycles

CRACK ON FRAME OF CLEAR VIEW WINDOW LT, UPPER AFT CORNER. (CPIL). NRC 00527: CRACK WAS REPAIRED PER SRM 56-10-02-2R-1 REPAIR 1 FIG.201, PERFORM LEAK CHECK PRESSURIZATION PER AMM 21-30-00 780-801. NO LEAKS WERE FOUND. (LP #1168010)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 36,655 cycles

SEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579396 ADDED FOR AC 9508. (LP #1168257)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON FRAME STA 1225 CANT BTW 3/4 O CLOCK POSITION AT AFT FUSELAGE. SUMMARY: OF NRC 00412 AREA WAS REPAIRED PER ER/A 579525-14 REV. ORIGINAL AND ETI-17-19-118 REV 2 ( PERMANENT REPAIR). (LP1164569)

Part: HINGE — CRACKED (TE FLAP) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON INBD FLAP FAIRING HINGE AT STA. XRS =137. 750 AT LT WING. (AI). INB FLAP HINGE FAIRING WAS REPLACED SERVICEABLE PN: 5912150-509 PER DWG 5910134 AND AMM 20-50-01-911-801 TOOL USED P/N TE25AC S/N 1049 DUE DATE 21/AUG/19. (LP1163426)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

PART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATES NR 520DT AND 520GB. CORROSION LEVEL 2. FUEL ACCESS PLATES NR 520DT AND 520GB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015 AND IPC 57-23-01-01 ITEM 345. (LP1161708)

Part: SKIN — CRACKED (TE FLAP VANE) · airframe 53,342 hrs · 36,642 cycles

AWR IN REFERENCE MON 2071758 : A CRACK WAS FOUND ON DENT # 10 AT RT AFTER MOVABLE VANE LOWER SKIN (AD). SUMMARY OF THIS N.R.C. 00747": IN REFERENCE MON 2071758 CRACK IN DENT NO. 10 (LOCATION: 25" OF INBD EDGE AND 14" OF T/E) WAS REPAIRED AT LOWER SKIN AFT MOVABLE VANE RT WING PER SRM 57-53-01-2R-1 AND SRM 51-70-02-0G. (LP1161545)

Part: RELEASE CABLE — BROKEN (TAILCONE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM. BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM WAS REPLACED PER AMM 53-52-01-830-802. OPERATIONAL TEST WAS PERFORMED PER AMM 53-52-01-720-805 OPERATIONAL TEST OK. (LP1159874)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

AWR IN REF MON/9508/049-MON, 95 REP, L.P. 2070042: CORROSION ON PREVIOUS REPAIR SPLICE LOWER AREA OF AFT CARGO COMPARTMENT. LEVEL 2. PREVIOUS REPAIR SPLICE LOWER AREA WERE REPLACED OF AFT CARGO COMPARTMENT PER SRM 53-20-15-2R-7, SRM 51-41-04-0G AND SRM 51-41-05-0G. (LP1159922)

Part: ACCESS PANEL — DAMAGED (WING) · airframe 53,342 hrs · 36,642 cycles

PART RACKS: ELONGATED HOLES ON FUEL ACCESS PLATES NBR 141AL AND 520CB. ACCESS PLATES NBR 141AL AND 520CB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015, IPC 57-23-01-01 ITEM 465J. (LP1160237)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

PART RACKS: CORROCION ON COUNTERSINK AREA ON FUEL ACCESS PLATE NBR 620DT AND 620DB. CORROSION LEVEL 2. FUEL ACCESS PLATE NR 620DT AND 620DB WERE REPLACED PER SRM 57-10-01-2R REPAIR 2 PAR.5C CONDITION III TABLE 201, VERIFIED PER IPC 57-22-01-01 ITEM 020 AND IPC 57-23-01-01 ITEM 430J. (LP1160284)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON LT TIE TRACK, BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT. SUMMARY: OF NRC.00359 CORROSION LEVEL 2. LT TIE TRACK, WAS REPLACED BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT PER SRM 51-41-05-0G AND SRM 51-41-01-0G. (LP1158400)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON TIE TRACK BTW STA:994 TO STA: 1020 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2.TIE TRACK RT BTW STA:994 TO STA:1020 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 53-20-51-0I-7 AND 51-41-01-0G. (LP1156952)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON FRAME STA:1022 BTW STGR:27L AND STGR:28R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME WAS REPAIRED PER SRM 53-20-07-2R-3 REPAIR 3 CONFIGURATION -7005. PERFORM VISUAL INSPECTION INITIAL 25,000 CYCLES AND REPETITIVE 6,500 CYCLES PER SRM 53-20-07-2R-3, PAR 6. (LP1156945)

Part: HOUSING — WORN (PAX DOOR) · airframe 53,342 hrs · 36,642 cycles

AWR,HIDDEN WEAR: WEAR ON HOUSING OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. HOUSING OF HOLD LOCK AND OPENING LEVER WAS REPLACED PER SRM 51-41-02-0G. (LP1156264)

Part: SKIN — CRACKED (PAX DOOR) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK SKIN ON EXTERNAL AREA OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. SKIN ON EXTERNAL AREA OF OPENING LEVER WAS REPAIRED PER ER/A 579458-14 REV. ORIGINAL AND ETI-17-19-094 REV. 3. (LP1156212)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION CRACKED INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 AT PASSENGER DOOR FWD ENTRANCE. INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 WAS REPLACED PER DWG 9955763 REVISION M, SRM 51-41-02- 0G AND 51-41-05-0G. (LP1156196)

Part: CAP — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7R. CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7 RH WAS REPAIRED PER ETI-17-19-090 REV ORG. AND ERA 579434-14 REV. ORIG. (LP1156275)

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY CCK(NOT TO EXCEED 24 MONTHS) INTERVAL AFTER ACCOMPLISHMENT OF SECTION I. PER ER/A 579428-14 REV. ORIGINAL SEC. II. WILL BE PERFORMED UNDER LOG PAGE 1153262. (LP1155385)

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. 1087.060, LONGERON 14R SIDE. PERMANENT REPAIR FUSELAGE SKIN STA. 1087. LONGERON 14R WAS PERFORMED PER ERA 579432-14 REV. ORG. AND ETI 17-19-088 REV. 2 AND PERFORM A GVI WITHIN EVERY CCK (NOT TO EXCEED 24 MONTHS) UNDER LOG PAGE 1152047 . PER ERA 579432-14 REV. ORIGINAL, SECTION I. (LP1154982)

Part: TORQUE TUBE — CORRODED (RUDDER TAB) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON RUDDER CONTROL TAB TORQUE TUBE IN REF 2720-2004 JOB #001-0259. RUDDER CONTROL TAB TORQUE TUBE WERE REPLACED FOR NEW P/N:3917927-1 AND WAS INSTALLED PER 2720-2004 JOB# 001-0259. (LP1155397)

Part: PUSHROD — CORRODED (RUDDER) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON PUSH ROD OF HOOK AT RUDDER THROW LIMITER. PUSH ROD OF HOOK AT RUDDER THROW LIMITER WAS REPLACED, ADJUSTED AND TESTED PER AMM 27-26-01-000-801, AMM 27-26-01-400-801 AND 2720-2003. (LP1154990)

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1073 LONG 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1073 LONG 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY C CK (NOT TO EXCEED 24 MONTHS) INTERVAL AFTER ACCOMPLISHMENT OF SECTION I. PER ER/A 579428-14 REV. ORIGINAL SEC. II. WILL BE PERFORMED UNDER LOG PAGE # 1153262. (LP1155229)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON AFT BULKHEAD PRESSURE DOUBLER STA 1053 BTW STR 29L TO STR 29R AT AFT CARGO COMPARTMENT. OF NRC 00393 (CORROSION LEVEL 2) DOUBLER WAS REPLACED PER SRM 51-41-02-0G. (LP1153170)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON FRAME STA:889 AND STR:26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2, FRAME STA:889 AND STR: 26L WAS REPAIRED PER SRM 53-20-07-2R PROCEDURE 3, FIGURE 201 (SHEET 7). MAINTENANCE REQUIREMENTS ARE THE FOLLOWING. PERFORM VISUAL INSPECTION INITIAL AT 25,000 CYCLES AND REPETITIVE VISUAL INSPECTION EACH 6,500 CYCLES. PER SRM 53-20-07-2R PROCEDURE 3 PARAGRAPH 6. (LP1153231)

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION CRACK ON SKIN AND CHANNEL MAIN LANDING GEAR DOOR RT. INNER SKIN AT RH MAIN LANDING GEAR DOOR WAS REPAIRED PER ER/A 579454-14 REVISION ORIGINAL SECTION I AND ETI-17-19-093 REVISION 3. REPETITIVE INSPECTION WITHIN EVERY 3,000 CYCLES AFTER SECTION I: PERMANENT REPAIR PER ER/A 579454-14 REV. ORIGINAL SEC. II. WILL BE PERFORMED UNDER LOG PAGE 1151765. (LP1154030)

Part: BEARING — CORRODED (RUDDER) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: RUSTED BEARING ON RUDDER DRIVE SECTOR AT AFT ACCESORIES COMPARTMENT IN REF 2720-2003. RUDDER DRIVE SECTOR AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER AMM 27-21-02. AND RUDDER CONTROL CABLES SYSTEM WAS ADJUSTED UNDER 2720-2004 JOB#001-0259 STEP 15. (LP1154117)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON INNER SKIN BTW STA 1037 AND STA 1040, STGR 29L AND STGR 29R AT AFT CARGO COMPARTMENT. (CCT). NRC 00394: CORROSION LEVEL 2, AREA WAS REPAIRED PER SRM 53-02-01-2R-1 FIG. 202. (LP #1151051)

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION IN COUNTERSUNK AREA AT FUEL ACCESSES PLATE NRS 620CT AND 520CT. CORROSION LEVEL 2, FUEL ACCESS DOORS 520CT AND 620CT WERE REPLACE PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. AND PART NUMBER VERIFIED PER IPC 57-22-01-01 ITEM 065. (LP1152531)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

CRACKED LONGERON ON STA 1133 STR 2L ON AFT ACCESSORY COMPARTMENT. (CAT). NRC 00405: LONGERON WAS REPAIRED PER SRM 53-00-05-2R. (LP #1152295)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

PART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATE NBR 141AR (AD). FUEL ACCESS PLATE 141AR WAS REPLACED. (LP1152533)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

CRACK ON LONGERON 16R, STA 1022. (CPAX). NRC 00457: PERMANENT REPAIR WAS PERFORMED ON LONGERON 16R, STA 1022 PER SRM 53-00-05-2R. (LP #1151116)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON FRAME STA 1037 BTW STR 28L AND STR 28R AT AFT CARGO COMPARTMENT. (AMDS 5314-2001). (CCT). NRC 00371: CORROSION LEVEL 2, AREA WAS REPAIRED PER SRM 53-20-07-2R REPAIR 3 CONFIGURATION -7003. (LP #1150867)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

CRACKED FRAME ON STA Y=1037 BTW LONG 16R AND 17R (CPAX). NR 00703: FRAME ON STA Y=1037 BTW LONG 16R AND 17R WAS REPAIRED PER SRM 53-20-07-2R REP. 4. (LP #1151115)

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

CRACKED "L" FITTING ON STA Y=715, X=42-58 RT AT WING BOX AREA (CPAX). NRC 00184: "L" FITTING ON STA Y=715, X=42-58 RT AT WING BOX AREA WAS REPLACE PER SRM 51-41-05-0G, PAR. 8. AND DWG #5910464 REV: DE. (LP #1149523)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON SEAT TRACK RT, OF FIRST OFFICER'S SEAT, IN COCKPIT. (CPIL). NRC 00615: CORROSION LEVEL 2, SEAT TRACK RT OF FIRST OFFICER WAS REPLACED PER SRM 51-41-01-0G PAR. 6. (LP #1147833)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

CRACK ON LONGERON #16 STA 1022 LT SIDE. (CPAX). NRC 00444: LONGERON #16 STA 1022 LT WAS REPIARED PER SRM 53-00-05-2R. (LP #1145916 )

Part: FRAME — CRACKED (BS 1037) · airframe 53,342 hrs · 36,642 cycles

CRACK ON FRAME STA 1037 AND LONGERON 17 LH SIDE. (CPAX). NRC 00446: FRAME STA 1037 AND LONGERON 17 LH SIDE WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1144628)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,342 hrs · 36,642 cycles

CRACK ON LONGERON 17 RH STA 1022. NRC 00451: LONGERON 17 RH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 FIGURE 201 (SHEET 2). (LP #1144154)

Part: LONGERON — CRACKED (BS 1037) · airframe 53,342 hrs · 36,642 cycles

CRACK ON LONGERON 13RH STA 1037. (CPAX). NRC 00453: LONGERON 13RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1142255)

Part: DOOR FRAME — CRACKED (BS 208) · airframe 53,342 hrs · 36,642 cycles

CRACK ON WEB OF FUSELAGE DOOR FRAME STA. 208, LONGERON 11 LH. (CPAX). NRC 00530: WEB OF FUSELAGE DOOR FRAME WAS REPAIRED PER B717-200 SRM 53-10-15-2R PAR. 4. (LP #1142067)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,342 hrs · 36,642 cycles

CRACK ON LONGERON 4RH, STA 1022. (CPAX). NRC 00456: LONGERON 4RH, STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1142313)

Part: LONGERON — CRACKED (BS 1037) · airframe 53,342 hrs · 36,642 cycles

CRACKED LONGERON 13L, BS 1037. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2 FIG. 201 (SHEET 1).

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 53,342 hrs · 36,642 cycles

CRACKS ON FLOOR PANEL 211AKF AT FLIGHT COMPARTMENT. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, PROCEDURE 2, REPAIR 2.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,342 hrs · 36,642 cycles

CRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2, FIG. 201. (SHEET 2).

Part: CUSP WEB — CORRODED (BS 565-567) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON RH CUSP WEB BTW STA Y=565-567 IS OUT OF LIMITS. CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.215.

Part: PAN — CRACKED (CABIN) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RING PAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE. (CPAX). NRC 00535: CRACK ON RINGPAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: PAN — CRACKED (PAX WINDOW) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE. (CPAX). NRC.00536: CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (

Part: PAN — CRACKED (BS 908-927) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RINGPAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927, RH SIDE. CRACK ON RING PAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927 RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 579) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN. CRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 813-832) · airframe 53,342 hrs · 36,642 cycles

CRACKED RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN. RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.

Part: PAN — CRACKED (GALLEY DOOR) · airframe 53,342 hrs · 36,642 cycles

CRACKS ON PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R REPAIR 4 FIG. 201.

Part: PAN — CRACKED (BS 832-851) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE. RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: PAN — CRACKED (PAX WINDOW) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE. (CPAX). NRC 00533: CRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 813-832) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE. (CPAX). NRC 00539: RINGPAN OF PASSENGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1135004)

Part: PAN — CRACKED (BS 737-756) · airframe 53,342 hrs · 36,642 cycles

CRACKED RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN (CPAX). NRC 00627: RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1134973)

Part: PAN — CRACKED (PAX WINDOW) · airframe 53,342 hrs · 36,642 cycles

CRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE. (CPAX). NRC 00534: CRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1135983)

Part: PAN — CRACKED (BS 696-715) · airframe 53,342 hrs · 36,642 cycles

CRACKED LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN. LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.

Part: PAN — CRACKED (BS 889-908) · airframe 53,342 hrs · 36,642 cycles

CRACKED RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN. RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: BEAM — CRACKED (GALLEY DOOR) · airframe 53,342 hrs · 36,642 cycles

CRACK BEAM #4 FWD EDGE AT GALLEY SERVICE DOOR (R1) (PTAS). NRC 00144: BEAM #4 AT GALLEY SERVICE DOOR (R1) WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G.

Part: FLOORBEAM — CORRODED (BS 145) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON FLOOR SUPPORT STA 145 BETWEEN X=- 44 TO X=-53 RH SIDE. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-40-05 AND DWG #9936533 REV CM.

Part: CUSP WEB — CORRODED (BS 799) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON CUSP MEMBRANE BETWEEN STA RH SIDE IN STA 799 IS 0.010" REWORKED AREA IS OUT LIMITS. NRC 00606: CORROSION LEVEL 2, OUT OF LIMITS AREA WITH CORROSION CUSP MEMBRANE STA 799 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 216.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON FLOOR PANEL, BETWEEN STA 148 AND 200, BETWEEN STA X=-50 AND X=-56. FLOOR PANEL BETWEEN STA 148 AND 200, BETWEEN STA X=-50 AND X=-56 WAS REPLACED PER B737-200 SRM 51-40-08-0G AND SRM 51-10-04-0G PAR 21 AND 15.

Part: FLOOR SUPPORT — CORRODED (BS 120-148) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON FLOOR SUPPORT BETWEEN STA. 120 AND 148, X= -24 AND X= -36. (CPIL) LOG-PAGE UPDATED @ 21JUN19 2310 UTC 02 CORR BY MEJORADA G 00289765 QRO 21JUN19 ATA 5321 FLOOR SUPPORT BTW STA 120 AND 148, X=-24 AND X-36 WAS REPLACED PER B717-200 SRM 51-41- 02-0G, AND DWG 9936533 REV CM.

Part: CUSP WEB — CORRODED (BS 408-427) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON CUSP MEMBRANE BETWEEN STA 408 TO 427 RH SIDE. (CPAX). NRC 00302: CORROSION LEVEL 2, CUSP MEMBRANE BETWEEN STA Y=408 TO Y=427 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.203. (LP #1132920)

Part: CUSP WEB — CORRODED (BS 460-465) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON CUSP MEMBRANE (BULGING MEMBRANE) BETWEEN STA Y=460 TO Y=465 RH SIDE WAS FOUND OUT OF LIMITS IN REF NRC 00303. NRC 00596: CORROSION LEVEL 2, CUSP MEMBRANE (BULGING MEMBRANE) BETWEEN STA Y=460 TO Y=465 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG. 216. (LP #1132241)

Part: TORQUE TUBE — CORRODED (RUDDER) · airframe 53,342 hrs · 36,642 cycles

INITIAL INSPECTION: CORROSION ON RUDDER CONTROL TAB TORQUE TUBE IN REF 2720-2004 JOB #001-0259. RUDDER TORQUE TUBE ASSY P/N 5912802-507 S/N: UNK WAS REPLACED FOR SERVICEABLE P/N: 5912802-507 S/N: DL16 AND WAS INSTALLED UNDER 2720-2004 JOB# 001-0259. TUBE, TORQUE, R OFF 00000 ON 95-2721-9-0001 00016. (LP1132406)

Part: CUSP WEB — CORRODED (BS 851-870) · corrosion level 2 · airframe 53,342 hrs · 36,642 cycles

CORROSION ON CUSP MEMBRANE BETWEEN STA 851 TO 870. (CPAX). NRC 00296: CORROSION LEVEL 2, CUSP MEMBRANE BETWEEN STA 851 TO 870 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215. (LP #1130929)

Part: PAN — CRACKED (FWD CARGO) · airframe 53,342 hrs · 36,642 cycles

CRACK ON INNER PAN STA Y=370 IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR (C1). NRC 00127: CRACK ON INNER PAN STA Y=370 IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED REPAIR PER B717-200 SRM 52-30-02-2R REPAIR 1 FIG. 201. (LP #1129505)

Part: CUSP WEB — CRACKED (BS 355) · airframe 53,342 hrs · 36,642 cycles

CRACKED CUSP WEB ON STA Y=355 X=57 LH AT PASSENGER COMPARTMENT (CPAX). NRC 00452: AREA WAS REPAIRED PER B717-200 SRM 53-00- 55-2R-4 FIG. 215.

Part: SKIN — DEBONDED (SPOILER)

REMOVAL OF LARGE DISBOND/WEAR. REQUIRE FULL SKIN REPLACEMENT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,181 hrs · 35,804 cycles

L1, R1 AND OVERWING EXIT LOWER EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS B5-118 AND B5-119 REF. B717 AMM 33-51. OPS CHECK NORMAL. OK FOR SERVICE. (LP3758004)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,171 hrs · 35,100 cycles

THE EMERGENCY OVERWING LIGHT WOULD NOT TURN OFF. REPLACED OVERWING LIGHT BATTERY PACK PER AMM 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 50,181 hrs · 34,418 cycles

LEFT HAND AFT EMERGENCY EXIT OVERWING IDENTIFIER IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IAW AMM 35-51. OPERATIONAL CHECKS NORMAL. OK FOR SERVICE.

Part: COVER — LOOSE (EXIT SIGN) · airframe 49,612 hrs · 34,005 cycles

EMERGENCY EXIT SIGN COVER LOOSE. TRIM PIECE SURROUNDING EXIT SIGN AT AFT JUMP TAPED AND SECURE. REPLACED AFT EMERGENCY EXIT COVER BY REMOVING TWO SCREWS HOLDING IT IN PLACE. CHECKS GOOD. OKAY FOR SERVICE.

Part: ATTACH FITTING — MISSING (EXIT SIGN) · airframe 48,909 hrs · 33,546 cycles

EMERGENCY EXIT SIGN COVER LOOSE, LOCATIONS:601. EXIT SIGN POPS OFF AT EACH LANDING. MAINTENANCE FOUND THE ATTACHING STRIP FOR THE LENS WAS MISSING. REPLACED ATTACHING STRIP AND REINSTALLED THE LENS REF AMM 33-51.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STAB LE, ZFS 52 SEAM HAS MANY LOOSE FASTENERS AND MANY AREAS OF FASTENER & LARGE AREA WASHER WEAR. COMPLIED WITH PRI 559680-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559680-14, REV ORIG.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SECOND HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP RT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT FOURTH HOLE BELOW ZFS=52.267. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SEVENTH HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP RT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SECOND HOLE BELOW ZFS=52.267. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT THIRD HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER RT SIDE, HAS CRACK INDICATION AT SEVENTH HOLE BELOW ZFS=52.267 IN SKIN. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 48,586 hrs · 33,302 cycles

VERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS A CRACK INDICATION AT FIRST HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14, REV ORIG.

Part: PANEL — DAMAGED (LT WING) · airframe 48,021 hrs · 32,896 cycles

LEFT WING LEADING EDGE AT INBD END NR 3 SLAT HAS THREE LOOSE RIVETS AND LEADING EDGE SPLICE DOUBLER CRACKED. FABRICATED A SPLICE IAW DRAWING 9919376. INSTALLED THE NEW SPLICE IAW DRAWING #9919376.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,082 hrs · 30,652 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,036 hrs · 30,611 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT, OVERHEAD AT ROW 17, AND THE EXIT SIGNS AT THE AFT OVERWING HATCH WERE ALL INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,609 hrs · 30,260 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT MID-CABIN CEILING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 44,197 hrs · 29,937 cycles

EMERGENCY EXIT SIGN ABOVE TAIL CONE EXIT INOPERATIVE. SECURED CONNECTION ON AFT LIGHT ASSY.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 53,342 hrs · 36,642 cycles

SRM REPAIR INSPECTION AFT CARGO DOOR JAMB LOWER PAN SPLICE STA 954-994, L-27R. VISUAL INSPECTION OF LWR PAN REPAIR SPLICES WAS PERFORMED PER SRM 53-20-15-2R-7 PAR.6 AND CORROSION WAS FOUND ON BOTH SPLICES. SUMMARY: CORROSION LEVEL 2 PREVIOUS REPAIR SPLICE WERE REPLACED PER SRM 53-20-15-2R-7 UNDER NRC 00633 LOG PAGE 1159922. MAINTENANCE REQUERIMENTS WAS VERIFIED AND NO FURTHER ACTION IS REQUIRED PLEASE CLOSE THIS LOG. (LP2070042)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,982 hrs · 29,761 cycles

R1 DOOR EMERGENCY EXIT SIGN BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,982 hrs · 29,761 cycles

TAIL COMPARTMENT AFT HANDRAIL EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,982 hrs · 29,761 cycles

LEFT OVERWING DOOR AFT EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,982 hrs · 29,761 cycles

FORWARD LEFT OVERWING DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 237, BETWEEN RBL 22 TO LBL 22. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FORWARD CARGO FLOOR SUPPORT CORRODED AT BS 655, BETWEEN RBL 22 TO LBL 22. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

MAIN CABIN FWD WET AREA, FLOOR SUPPORT CORRODED AT BS 177, BL 0. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

MAIN CABIN INTERCOSTAL CRACKED BETWEEN BS 1002 TO 1022, BL 0. REPAIRED INTERCOSTAL IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

L1 DOOR JAMB MAIN CABIN FLOOR MEMBRANE CORRODED AT BS 200. REPAIRED MEMBRANE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

CUSP WEB CORRODED BETWEEN BS 237 TO 256, LBL 55. REPAIRED CUSP WEB IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FORWARD MEMBRANE WEB CORRODED AT BS 218, RBL 55. R & R WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SHEAR TIE CORRODED AT BS 927, BETWEEN LONGERON 28L - 28R. REPAIRED SHEAR TIE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 579 TO 598. REPAIRED CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 42,478 hrs · 28,726 cycles

AFT CARGO BARRIER DOOR FWD & AFT HEADER BRACKET CRACKED. R & R BRACKET IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT CARGO FWD BULKHEAD LT LOWER NUTPLATE SUPPORT INTERCOSTAL STRAP CRACKED AT BS 817. R & R STRAP IAW DWG & SRM.

Part: FRAME — CRACKED (BS 715) · airframe 42,478 hrs · 28,726 cycles

LEFT FRAME ANGLE CRACKED AT BS 715. R & R ANGLE IAW DWG & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 900 - 1022, RBL 22. R & R SEAT TRACK IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FRAME CRACKED AT BS 696. R & R FRAME IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 588 - 218, LBL 22. R & R SEAT TRACK IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FRAME CRACKED AT BS 674. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FRAME CRACKED AT BS 674. R & R FRAME IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 832 - 994, LBL 44. R & R SEAT TRACK IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SHEAR TIE CORRODED AT BS 946, BETWEEN LONGERON 29L - 29R. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT CARGO CEILING AREA INTERCOSTAL CRACKED AT BS 851, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SHEAR TIE CORRODED AT BS 954, BETWEEN LONGERON 30L TO 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 42,478 hrs · 28,726 cycles

LEFT WING LE SUPPORT, CRACKED AT STATION 560. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 828 - 900, RBL 22. R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 822 - 900, LBL 44. R & R SEAT TRACK IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FRAME CRACKED AT BS 696. R & R FRAME IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 828 - 900, RBL 44. R & R SEAT TRACK IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT BS 1116, LONGERON 15R. R & R FORMER IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 588 - 650, RBL 22. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 650 - 820, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

CUSP SPLICE CORRODED BETWEEN BS 579 TO 598, RBL 60. R & R SPLICE ANGLE IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,478 hrs · 28,726 cycles

L1 DOOR NR 2 BEAM AFT CORNER CRACKED. REPAIRED DOOR IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 655 - 588, LBL 22. R & R SEAT TRACK IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SHEAR TIE CORRODED AT BS 908, BETWEEN LONGERON 30L TO 29L. REPAIRED SHEAR TIE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 218 - 588, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 266 - 588, RBL 22. R & R SEAT TRACK IAW AMM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,478 hrs · 28,726 cycles

L1 DOOR NR 1 BEAM, FWD CORNER CRACKED. R & R NR 1 BEAM IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

MAIN CABIN AFT PRESS BULKHEAD DOOR LT JAMB ABOUT MID-SECTION FITTING CRACKED. R & R FITTING IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 655 - 820, LBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 832 - 994, LBL 22. R & R SEAT TRACK IAW AMM & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 665 - 820, LBL 22. REPAIRED SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 821 - 889, LBL 22. R & R SEAT TRACK IAW AMM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LONGERON CORRODED BETWEEN BS 905 - 1002, LONGERON 30R. REPAIRED LONGERON IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 588 - 655, LBL 44. R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

SEAT TRACK CORRODED BETWEEN BS 889 - 1022, RBL 44. R & R SEAT TRACK IAW AMM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FORMER CRACKED AT BS 1022, LONGERON 16R. R & R FORMER IAW SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT ACCESSORY COMPARTMENT SPLICE CRACKED AT BS 114, LONGERON 2R. REPAIRED SPLICE IAW SRM & DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT CARGO BILGE AREA, LONGERON CORRODED BETWEEN BS 927 TO 960, LONGERON 29L. R & R LONGERON IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

AFT OF R1 CUT OUT FLOORBOARD SUPPORT AT CUSP CORRODED. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED AT BS 167, RBL 22. R & R SUPPORT IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FIRST OFFICERS INBD SEAT TRACK SUPPORT CORRODED. R & R SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

CUSP WEB CORRODED AT BS 219, LBL 50. REPAIRED CUSP WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

WEB FINGER CRACKED AT BS 200, LONGERON 15L. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 148 - 178, LBL 22. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

L1 CUT OUT FLOOR PANEL 221AF SUPPORT CORRODED AT CUSP WEB. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED FWD OF BS 177, LBL 22. R & R SUPPORT IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FALSE TRACK CORRODED BETWEEN BS 157 TO 207. R & R TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 157 - 170, RBL 45. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED AT BS 150, RBL 22. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (RT WING) · airframe 42,478 hrs · 28,726 cycles

RIGHT WING TRAPEZOID INBD UPPER FITTING SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FALSE TRACK CORRODED BETWEEN BS 157 - 207. R & R FALSE TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED AT BS 207, BETWEEN BL 0 TO RBL 54. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 177 TO 256, LBL 17. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOORBOARD SUPPORT CORRODED AT BS 157, BL 0. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (RT WING) · airframe 42,478 hrs · 28,726 cycles

RIGHT WING TRAPEZOID INBD FITTING, FWD FLANGE OTBD SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,986 hrs · 29,762 cycles

MAIN CABIN FRAME TAB CRACKED AT BS 715, LT SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,986 hrs · 29,762 cycles

LEFT FRAME CRACKED AT BS 674. R & R FRAME IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 908 TO 927. R & R CUSP WEB IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

C2 DOOR CUT OUT LOWER JAMB CORRODED. REPAIRED JAMB IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 42,478 hrs · 28,726 cycles

RIGHT WING LE SUPPORT CRACKED AT WING TO BODY RIB AT STATION 560. R & R RIB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 636 - 655. R & R CUSP WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 42,478 hrs · 28,726 cycles

RIGHT WING FLAP TRACK INBD TE SUPPORT ANGLE INBD CRACKED. R & R ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

FLOOR WEB CORRODED AT BS 194, BETWEEN RBL 45 - 52. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 617 - 636. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 737 - 756. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 579 TO 598. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 870 TO 889. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 851 - 870. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 522 - 541. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT EMPENNAGE, LOWER PANEL BOX, COMPOSITE SECTION ATTACH AT LOWER AFT SIDE OF CANTED FRAME AT BS 1178.2, SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FLOOR CUSP WEB CORRODED BETWEEN BS 465 - 446. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FLOOR CUSP WEB CORRODED BETWEEN BS 446 - 427. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

LEFT FLOOR CUSP WEB CORRODED BETWEEN BS 579 - 560. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 446 - 465. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 465 TO 484. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

RIGHT FLOOR CUSP WEB CORRODED BETWEEN BS 484 TO 503. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

CUSP WEB CRACKED AT BS 674, RBL 48. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,478 hrs · 28,726 cycles

CUSP WEB CRACKED AT BS 674, LBL 48. R & R CUSP WEB IAW SRM & DWG.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,437 hrs · 29,380 cycles

FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,425 hrs · 28,691 cycles

REAR BULKHEAD OVER DOOR EMERGENCY EXIT SIGN INOPERATIVE. R & R BATTERY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 415,340 hrs · 28,121 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: WIRE — SHORTED (COCKPIT) · airframe 42,202 hrs · 28,778 cycles

WIRE FOR COPILOTS ANTI-FOG SHORTED & SPARKED. REPAIRED WIRE IAW SWPM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 39,407 hrs · 26,842 cycles

FORWARD GALLEY EXIT SIGN FELL OFF. RE-SECURED LENS PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 392,630 hrs · 26,743 cycles

F/A FWD FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 39,250 hrs · 26,735 cycles

LTW MDDR 22313T STABILIZER DORSAL FIN CRACKED AT FASTENER HOLE. REF EA 17-55-0370 41R. CUT OUT DAMAGED SECTION OF VERTICAL STABILIZER DORSAL FIN SKIN, FAB AND INSTALLED REPAIR DOUBLER AND FILLER IAW B-717 SRM 55-30-01 REPAIR 5 51-41-01, 51- 40-08, 51-10-04 51-20-05 AT NZC W/O 274696.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 38,582 hrs · 26,320 cycles

STABILIZER DORSAL FIN CRACKED AT AFT FASTENER HOLE. REF EA 17-55-037041R. CUT OUT DAMAGED SECTION OF VERTICAL STABILIZER DORSAL FIN SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B717 SRM 55-30*-01 REPAIR 5, 51-41-01, 51-40-08, 51-10-04, 51-20-05.

Part: LENS — CRACKED (CABIN) · airframe 38,582 hrs · 26,320 cycles

MULTIPLE EMERGENCY LIGHT LENS MISSING AND CRACKED. REMOVED & REPLACED MULTIPLE EMERGENCY LIGHT LENS AND PERFORMED GOOD OPS TEST IAW B717 AMM 33-51-00 AND 33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,582 hrs · 26,320 cycles

MULTIPLE EMERGENCY LGHTS ON SEATS INOP. REPLACED MULTIPLE EMERGENCY LIGHTS ON SEATS IAW B717 AMM 33-51-00. PERFORMED GOOD OPS TEST IAW B717 AMM 33-51-00 & 33-51-04.

Part: SKIN — CORRODED (RT WING) · airframe 38,582 hrs · 26,320 cycles

RIGHT MLG W/W UPPER WING SKIN CORRODED 24" OUT APPROX .750 WIDE, TOP SIDE (FROM I/B KEEL BEAM WEB) 004. REMOVED CORROSION ON CENTER WING SKIN RBL 19"-29". CORROSION HAS BEEN BLENDED ON THE AFT EDGE OF THE 5940741-6 SKIN WITH REMAINING THICKNESS OF .089"-.160". BLEND REPAIR HAS BEEN SHOWN TO COMPLY WITH THE TYPE CERTIFICATION OF THE AIRPLANE AND IS SATISFACTORY TO BOEING AS A PERMANENT REPAIR IAW FAS EA000739, PER EA 17-57-04059.

Part: NONSKID — MISSING (RT WING) · airframe 38,582 hrs · 26,320 cycles

RIGHT WING EMERGENCY EXIT PATH MISSING SMALL AREA OF NOSKID. REPAINTED OVERWING ESCAPE WALKWAY ARROW IAW B717 AMM 11-21-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,582 hrs · 26,320 cycles

LEFT NLG STRUT DOOR, AFT HINGE CUTOUT CRACKED NDT VERIFIED, MARKED. STOP DRILLED CRACK ON LEFT NLG AFT HINGE CUTOUT, AFT UPPER CORNER FABRICATED AND INSTALLED REPAIR DOUBLER IAW B717 SRM 53-10-01, REPAIR 6, FIG 201.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,582 hrs · 26,320 cycles

RIGHT NLG STRUT DOOR, AFT HINGE CUTOUT CRACKED NDT VERIFIED, MARKED. STOP DRILLED CRACK AT RIGHT NLG AFT HINGE CUTOUT, AFT UPPER CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B717 SRM 53-10-01, REPAIR 6, FIG 201.

Part: CYLINDER — OUT OF ADJUST (NLG) · airframe 38,930 hrs · 26,533 cycles

NOSE GEAR INDICATORS SHOWED RED AFTER 2 ATTEMPTS, 3RD ATTEMPT SHOWED GREEN ON CONFIG SYNOPTIC THEN GREEN ON THIRD ATTEMPT. RE-ADJUSTED NLG RETRACT CYLINDER JAM NUT PER MM.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 38,248 hrs · 26,091 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE FROM HOLDER. SECURED LANYARD PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,799 hrs · 25,793 cycles

AFT EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 37,451 hrs · 25,560 cycles

LEFT WING I/B SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: LENS — CRACKED (CABIN)

FWD AISLE OVERHEAD EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LENS. REF AMM 33-51.

Part: BATTERY — DISCHARGED (CATWALK)

AFT TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY & POWER SUPPLY ASSY PER AMM 33-51-03, OPS CHECKS GOOD.

Part: COVER — OUT OF POSITION (CABIN)

LIGHT COVER AIRCRAFT LEFT OVER EXIT ROW FELL OFF ON LANDING. REINSTALLED WINDOW LIGHT COVER PER 717 AMM 33-22.

Part: BATTERY — DISCHARGED (CABIN)

AFT TAIL CONE COMP CATWALK LIGHTS OUT. REMOVED AND REPLACED BATTERY SUPPLY ASSY IAW B717 AMM 33-51.

Part: LIGHT — MALFUNCTIONED (CABIN)

OVERHEAD LIGHT DID NOT ILLUMINATE WHEN EMER LT PLACED IN ON DURING PREFLIGHT INSPECTION. CYCLED EMERGENCY LIGHT SWITCH - EMERGENCY LIGHTS OPN NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT ACCESSORY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND EMERGENCY BATTERY AT (223GC) AFT DROP CEILING IN REF TC AMM 33-51-03, OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — CONTAMINATED (CABIN)

PER CDR WATER WAS DRIPPING FROM THE CEILING RIGHT ABOVE THE L-2 JUMPSEAT AND THE EXIT SIGN WAS FLICKERING ON AND OFF. THERE IS A SMALL LIGHT RIGHT ABOVE 3CD THE LIGHT THAT IS THERE WAS DOING THE SAME THING. FOUND WATER IN EMERGENCY LIGHT BATTERY PACK AND CHARGER. REMOVED AND REPLACED BATTERY PACK & CHARGER IAW AMM 33-51. ALSO PERFORMED BURN OUT OF A/C SYSTEM REF AMM 21-54. OK FOR SERVICE.

Part: RELAY — FAULTY (CABIN)

OVERWING EMERGENCY LIGHTS COME ON WITH COCKPIT OVERHEAD LIGHT SWITCH AT "OFF" POSITION. REMOVED AND REPLACED RELAY R2-273 CHECKED PER AMM 33-51 AND FOUND GOOD.

Part: BRACKET — CORRODED (FUSELAGE)

AFT CARGO DOOR FRAME BRACKET, STA 874, CORROSION. ACCOMPLISHED FRAME BRACKET REPLACEMENT PER B717 SRM 51-41-05.

Part: SPLICE — CORRODED (FUSELAGE)

LOWER AFT EDGE, AFT CARGO DOOR CUTOUT SPLICE, CORROSION. ACCOMPLISHED SPLICE REPLACEMENT PER B717 SRM 51-41-02.

Part: WIRE — DISCONNECTED (CABIN)

CABIN STANDBY LIGHT INOPERATIVE, ROW 28. FOUND WIRING UNPLUGGED IN OVERHEAD PANEL, RECONNECTED WIRING. OPS CHECKED GOOD, PER AMM 33-50.

Part: BATTERY — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND AFT EMERGENCY EXIT ROW THRESHOLD LIGHTS WOULD NOT COME ON. REMOVED AND REPLACED BATTERY SUPPLY ASSEMBLY REF AMM 33-51. BATTERY NUMBER B5-119. OPS CHECK GOOD.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW TASK CARD 17-5310-2975.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2987.

Part: CUSP WEB — CRACKED (FUSELAGE)

LEFT CABIN CUSP WEB, STA 240, LONG L18L, CRACKED. ACCOMPLISHED CABIN CUSP WEB REPAIR PER BOEING DWG SG09530003. SEE NR 3414 AND 3436.

Part: CUSP WEB — BENT (FUSELAGE)

LEFT CABIN CUSP LINE, STA 240, BENT. ACCOMPLISHED CABIN CUSP LINE DOUBLE TEE CUSP REPAIR PER B717 SRM 53-00-55. SEE NR 3428 AND 3431.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB, STA 954 TO 994, CORROSION. ACCOMPLISHED CARGO DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201. SEE NR 3343 AND 3430.

Part: SEAT TRACK — CORRODED (FUSELAGE)

GALLEY AREA SEAT TRACK, STA 237, RBL 20, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02116IR. SEE NR 5176 AND 5272.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 DOOR SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED L1 DOOR SLIDE REF B717 M/M 25-61-01.

Part: FLOOR PANEL — CORRODED (COCKPIT)

FLIGHT COCKPIT RIGHT HAND FLOOR PANEL NR 211 AMF HAS CORROSION AT I/B AFT CORNER - CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOULBERS 2" X 2.5" .040 AND FILLER (1 X 1 X.032) IAW B717 SRM 53-10-50. RO 046561 2024T3.040, PO 046316 2024T3 .032 AT I/B AFT OF PANEL 211AMF.

Part: SEAT TRACK — CORRODED (COCKPIT)

FIRST OFFICER'S AFT LOWER I/B SEAT TRACK CORRODED. FABRICATED SEAT TRACK FROM RAW STOCK, P/N IDI774T PER DRAWING 5971207 AND EA 17-53-008951R, REPLACED PER B717 SRM 51-41-01.

Part: CABLE — DISCONNECTED (R1 DOOR SLIDE)

R-1 SLIDE CABLE DISCONNECTED, POSSIBLY OUT OF ITS NORMAL CONDITION. REMOVED R-1 DOOR SLIDE AND FOUND PINS PULLED OUT. REPLACED SLIDE AS OUTLINED IN 717 M/M 35-61.

Part: STRUCTURE — DAMAGED (CATWALK)

AFT FUSELAGE CATWALK DAMAGED DURING APU REMOVAL. INSTALLED DOUBLER REPAIR AT AFT FUSELAGE IAW AIRTRAN RES 06-0424 DATED 04/07/06. MATERIAL USED 7076-T6 .072 30" X 19.5".

Part: SWITCH — INOPERATIVE (OXY MASK)

02 MASKED IN CABIN DROPPED AGAIN AT GATE. REMOVED AND REPLACE4D PASSENGER OXYGEN MASK ALTITUDE RELEASE SWITCH IAW B717 AMM 35-22-02. FUNCTIONAL TEST OF ALTITUDE MASK RELEASE SWITCH IAW B717 AMM 35-22-02 PG 501. OPS CHECKS GOOD.

Part: FRAME — CRACKED (FUSELAGE)

LEFT CANTED FRAME HAS A CRACK STA 1178. INSTALLED ANGLE REPAIR ON LEFT CANTED FRAME AT STA 1178 LONG 16. MATERIAL USED 0.080 7075.0 10 .5" X 2.5" IAW B717 SRM 51-40-02 AND SRM 51-41-01. HEAT TREATED TO T-6 PER AVBORNE 98PMS.247PS.01.

Part: HOSE — BURNED (LT ENGINE)

AFTER APPLYING POWER ON TAKEOFF BOTH PILOTS F/AS SMELLED A BURNING RUBBER ODOR. THE ODOR REDUCED WHEN POWER REDUCED. DECIDED TO RETURN AND LAND. ODOR WAS GONE BY LANDING. FIRST IMPRESSION WAS THAT IT WAS TIRE SMOKE FROM ANOTHER A/C BUT IT PERSISTED IN THE CABIN UNTIL POWER WAS REDUCED. ALL ENGINE, AIR SYSTEMS, ELECT WAS NORMAL. AFTER LANDING THE FIRE DEPT CHECKED A/C, THE RT ENG WAS SMOKING. RT ENG WAS SHUTDOWN. AFTER FURTHER INSPECTION, FOUND LT ENG SMOKING FROM THE VENT ON BOTTOM OF ENG. LT PACK IS INOP. REPLACED HOSE AT LT PACK DRAIN, LT PACK OPS GOOD REG 21-00 36-14-30.

Part: ENGINE — INOPERATIVE (NR 2)

DURING CLIMB OUT, AT ABOUT 18,500 FT, 2 LOUD BANGS HEARD, RT ENGINE SPOOLED DOWN, EGT ROSE, SEVERE DAMAGE SUSPECTED RAN QRH. REMOVED AND REPLACED NR 2 ENGINE IAW TC 603. ALL OPS NORMAL. A/C OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS IN AFT ACCESSORY COMPT INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD FWD OF AFT ACCESSORY COMPT DOOR REF 33-00. NOW CKS OK.

Part: FAIRING — BROKEN (CABIN)

EMERGENCY LIGHT FAIRING IN SEAT ARM REST BROKEN. REPLACED BROKEN LIGHT FAIRINGS IAW AVIO CMN 25-24.

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)

FOUND NACELLE EMERGENCY LIGHTS CAME ON WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS IAW B717 MM 33-50.