N939AT

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,697 hrs · 33,624 cycles

DURING SVC CHECK FOUND LT AFT OVERWING EXIT IDENTIFIER INOP, RT AFT OVERWING EXIT IDENTIFIER INOP, AND AFT CABIN EXIT IDENTIFIER INOP. AFT CABIN EXIT IDENTIFIER OPS CKS GOOD. R/R NEW BATTERY PACK AND BATTERY REF B717 AMM 33-51. (7960791)

Part: WINDOW — CRACKED (ZONE 200) · airframe 45,248 hrs · 32,248 cycles

DURING CRUISE, THE CA NOTED AN ARC AND THE WINDSHIELD DEVELOPED A CRACK. MAINTENANCE REPLACED THE CAPT FWD WINDSHIELD REF B717 AMM 56-11. ALL CHECKS WERE GOOD. WINDOW HEAT TEST GOOD REF B717 AMM 30-41. INSTALLED WINDOW WIPER REF B717 AMM 30-42. AIRCRAFT IS OK FOR SERVICE. (LP #7401844)

Part: DIMMER — FAILED (ZONE 200) · airframe 45,100 hrs · 32,106 cycles

SHIP 9562 -ATB/FUME/DE- THE CREW PERFORMED AN AIR TURN BACK TO PNS DUE TO STRONG ELECTRICAL FUMES IN THE COCKPIT WITH LIGHTING CONTROL ISSUES. AN EMERGENCY WAS DECLARED WITH ATC, THE LIGHT CONTROL WAS TURNED OFF, AND THE LANDING BACK AT PNS WAS UNEVENTFUL. NO SMOKE OR FIRE WAS OBSERVED BUT THE FUMES PERSISTED UNTIL AFTER THE AIRCRAFT WAS DEPLANED. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE PEDESTAL LIGHTS DIMMER U1-3029 WAS BURNT. THE DIMMER WAS REPLACED, AND THE OPERATIONAL CHECK WAS GOOD. (LP #7135640)

Part: BULKHEAD — ABNORMAL (REAR CANTED BULK) · airframe 44,333 hrs · 31,427 cycles

-AD- ACCOMPLISH ER/A 558098-14AD REV A SEC II. ACCOMPLISH ER/A 558098-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-558098 ADDED FOR AC 9562. ACCOMPLISHED ERA 558098-14AD REV A SECTION II ALTERNATIVE INSPECTION FOR AD 2024-20-02. NO FURTHER DEFECTS NOTED. CLOSED LOG AND REMOVED MONITOR INSPTION. (LP #0670988)

Part: ACCESS PANEL — MISSING (LT WING) · airframe 42,967 hrs · 30,262 cycles

SHIP 9562 -PDA- DURING PREFLIGHT INSPECTION FOUND MISSING ACCESS PANEL ON LEFT HAND OUTER PORTION OF WING NEAR NAVIGATION LIGHT. PERFORMED TEMP REPAIR IAW SECTION 1 OF ERA 617613-14, WITH PERMANENT REPAIR TO BE COMPLIED WITH IN 1 FLT CYCLE. ATL MAINTENANCE INSTALLED THE LH WING LOWER SURFACE ACCESS PANEL PER B717 AMM 33-42. OK TO CLOSE. RII: N. CLOSED LOG AND REMOVED MONITOR INSPECTION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,771 hrs · 30,096 cycles

DURING CHECK OF THE EXTERIOR LIGHTS, THE LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258406)

Part: SPAR — CRACKED (RT WING) · airframe 42,771 hrs · 30,096 cycles

CRACK ON REAR SPAR APPROX XW151 AT RH WING. SUMMARY OF NRC 00175: REAR SPAR, LOWER CAP APPROX XW151 AT RH WING WAS REPAIRED PER ERA 614420-14AD REV ORIGINAL AND PRI 614420-14 REV 16. TIME CONTROLLED ITEMS. SECTION DTA: PENDING DTA, NOT TO EXCEED 07/MAR/2026, MONITORING UNDER LOGPAGE #0240765. ASSOCIATED ERA 14-614420 ADDED FOR AC 9562. (LP #0247015)

Part: INTERCOSTAL — CRACKED (BS 184) · airframe 42,771 hrs · 30,096 cycles

CRACK INTERCOSTAL ON INNER STRUCTURE STA Y=184 BTW BEAMS #4 & 5 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00107: INTERCOSTAL ON INNER STRUCTURE STA Y=184 BTW BEAMS #4 & 5 AT PASSENGER DOOR (L1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0231270)

Part: FRAME — CRACKED (BS 1022 L7) · airframe 42,771 hrs · 30,096 cycles

CRACK ON MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX. SUMMARY OF NRC 00355: MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX WAS REPAIRED PER ERA 614511-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614511 ADDED FOR AC 9562. (LP #0184100)

Part: FRAME — CRACKED (BS 674) · airframe 42,771 hrs · 30,096 cycles

A.D. CRACK OF 0.500 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF. CARD 5310-01436-04B). SUMMARY OF NRC 00253: FRAME TAB OVERWING FRAME AT STA Y=674.000 LH WAS REPLACED CARD 5310-01436-03A. ASSOCIATED AA 5310-01436 ADDED FOR AC 9562. (LP #0180676)

Part: CUSP WEB — CRACKED (BS 655) · airframe 42,771 hrs · 30,096 cycles

CRACK ON CUSP MEMBRANE ON STA 655 WAS FOUND IN REFERENCE TO CARD 5310-01436-03B STEP 3. SUMMARY OF NRC 00568: CUSP MEMBRANE ON STA 655 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 AND INSTALL CUSP MEMBRANE MUST BE INSTALLED PER CARD 5310-01436-04B STEP 17 AND 18. ASSOCIATED AA 5310-01436 ADDED FOR AC 9562. (LP #0180729)

Part: FRAME — CRACKED (BS 696) · airframe 42,771 hrs · 30,096 cycles

CRACK ON UNDER THE FASTENER OF THE FRAME TAB OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-04C). A.D. A.A. SUMMARY OF NRC 00306: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9562. (LP #0176028)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 42,771 hrs · 30,096 cycles

CORROSION AT FLOOR SUPPORT ON X=56 BTW STA Y=160/200 PAX CABIN. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORT ON X=56 BTW STA Y=160 TO Y=200 WAS FABRICATED AND REPLACED PER DWG 9936534 REV BW AND B717-200 SRM 51-41-05-0G PAR 8. (LP #0162459)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 42,771 hrs · 30,096 cycles

CORROSION ON FLOOR SUPPORTS COORDINATE X=-56, BTW STA Y=200 TO 210, COORDINATE X=-44 BTW STA Y=160 TO 200 AND COORDINATE X=0 TO COORDINATE X=-44, STA Y=200. SUMMARY OF NRC 00686: CORROSION LEVEL 2. FLOOR SUPPORTS COORDINATE X=-56, BTW STA Y=200 TO 210, COORDINATE X=-44 BTW STA Y=160 TO 200 AND COORDINATE X=0 TO COORDINATE X=-44, STA Y=200 WERE FABRICATED AND INSTALLED PER DWG 5952262 REV L, DWG S2929169 REV B, AND B717-200 SRM 51-41-08-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0155188)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,771 hrs · 30,096 cycles

PUNCTURES ON DIAPHRAGM UNDER FLOOR SUPPORT STA 180-192 X=54 AT PAX CABIN IN REF NRC 455. SUMMARY OF NRC 00659: DIAPHRAGM UNDER FLOOR SUPPORT STA 180-192 X=54 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0152829)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,771 hrs · 30,096 cycles

CRACK ON LONGERON 6L STA Y1020 AT PASSENGER CABIN. SUMMARY OF NRC 00419: LONGERON SECTION 6 LH FROM STA Y=1012 TO STA Y=1053 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0140959)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 42,771 hrs · 30,096 cycles

CORROSION AT FLOOR SUPPORTS ON X=-7 BTW STA.Y=158/200 PAX CABIN. SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR SUPPORT ON X=-7 BTW STA.Y=158/200 WAS FABRICATED PER DRAWING 9936534 REV BW AND REPLACED B717 SRM 51-41-01-0G. (LP #0133905)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,771 hrs · 30,096 cycles

AFT CABIN FLOOR INTERCOSTAL CRACKED 3 PLACES AT UPPER FLANGE NEAR NUT PLATE HOLES, STATION 1002-1037 BL0. SUMMARY OF NRC 00641: FLOOR INTERCOSTAL STA 1002-1037 BL0 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1, REPAIR 1, REPAIR CATEGORY "A". (LP #0122544)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,438 hrs · 29,834 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND THE TAIL COMPARTMENT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY ASSEMBLY, B5-260, IAW B717 AMM 33-51-04. OPERATOIONAL CHECK WAS GOOD. (LP #4341609 )

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,353 hrs · 29,766 cycles

THE DOOR R1 EMERGENCY EXIT TOP SIGN IS INOPERATIVE. MAINTENANCE FOUND A BROKEN PIN IN THE IN-LINE JUNCTION. REPINNED AND REPLACED THE IN-LINE JUNCTION REF BOEING SWPM CHP 20-20-02. EMERGENCY LIGHT OPS NORMAL AS PER B717 AMM 33-51. (LP #4782462)

Part: NONE — NONE · airframe 40,051 hrs · 27,698 cycles

FOUND THAT THE AFT OVERWING EXIT MARKER LIGHTS WERE INOPERATIVE ON THE SERVICE CHECK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION B5-119 PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #9115777)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON PANEL FROM STA Y=168 TO Y=200 BTW X=-53 AND X=-58 AT W1 AREA. (CPCP CARD 2021-2001). SUMMARY OF NRC 00200: CORROSION LEVEL 2, FLOOR PANEL FROM STA Y=168 TO Y=200 BTW X=-53 AND X=-58 AT W1 AREA WAS REPLACED PER B717 SRM 51-41-01-0G AND 51-41-02-0G. (LP #2025092)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON MEMBRANE FROM STA Y=184 TO Y=200 BTW X=-50 AND X=-53 AT W1 AREA. (CPCP CARD 2021-2001). SUMMARY OF NRC 00199: CORROSION LEVEL 2, REPAIR WAS PERFORMED ON MEMBRANE FROM STA Y=184 TO Y=200 BTW X=-50 AND X=-53 AT W1 PER B717 SRM 51-70-10-2R PROCEDURE 2. (LP #2023780)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON CLIPS FRAME STA=907 AND STA=909 BTW STRINGERS 29LH TO 29RH (SM). SUMMARY OF NRC 00121: CORROSION LEVEL 2, CLIP FRAME STA=907 AND STA=909 BTW STRINGERS 29LH TO 29RH WAS REPAIRED PER B717 SRM 53 -20-06-2R PROCEDURE 2. (LP #2023947)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON STRINGER 30 BTW STA=890 AND STA=895 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00119: CORROSION LEVEL 2, STRINGER 30 BTW STA=890 AND STA=895 AFT CARGO COMPARTMENT WAS REPAIRED PER ETI-17- 21-037 REV. ORIGINAL AND ERA 595526-14 REV. ORIG. SECTION I: PERMANENT REPAIR . (LP #2022867)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON AFT CARGO DOOR JAMB (CCT). SUMMRY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB WAS REPAIRED (PERMANENT REPAIR) PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #2022650)

Part: NONE — NONE · corrosion level 2 · airframe 38,230 hrs · 26,039 cycles

CORROSION ON STRINGER 30 BTW STA=992 TO STA=995 AT AFT CARGO COMPARTMENT IN REF NRC 00124. SUMMARY OF NRC 00203: CORROSION LEVEL 2, PERMANENT REPAIR WAS PERFORMED ON STRINGER 30 BTW STA=992 TO STA=995 AT AFT CARGO COMPARTMENT PER B717 SRM 53-00-05-2R PROCEDURE 3. (LP #2020310)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,863 hrs · 23,420 cycles

EMERGENCY EXIT SIGN IS INOPERATIVE AT 20A. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. LOCATION PASS SEATS: 20A (LP #1016254)

Part: FINGER DOUBLER — DAMAGED (BS 446-484) · airframe 33,282 hrs · 22,402 cycles

FINGER DOUBLER DAMAGED AT THE LAP SEAM LONGERON 26L, BS 446 - 484. CUT OUT THE DAMAGED FINGER DOUBLER DIM 30". INSTALLED A NEW FINGER DOUBLER IAW ER/A 596015-14, REV ORIGINAL.

Part: FINGER DOUBLER — DAMAGED (BS 475) · airframe 33,282 hrs · 22,402 cycles

FINGER DOUBLER WAS DAMAGED AT BS 475, LONGERON 26L. CUT OUT THE DAMAGED FINGER DOUBLER, DIM 45. INSTALLED NEW FINGER DOUBLER IAW ER/A 596015-14, REV ORIGINAL.

Part: LONGERON — BENT (BS 446-484) · airframe 33,282 hrs · 22,402 cycles

LONGERON 26L WAS BENT BETWEEN BS 446 - 484. REPAIRED THE LONGERON IAW ER/A 596015-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 458-475) · airframe 33,276 hrs · 22,395 cycles

FUSELAGE SKIN WAS CRACKED AND CREASED BETWEEN BS 458 - 475, LONGERON 26L - 28L. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 6.

Part: SKIN — DAMAGED (BS 389-484) · airframe 33,276 hrs · 22,395 cycles

FUSELAGE SKIN BETWEEN BS 389 - 484, LONGERON 22L - 26L WAS DAMAGE. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 6.

Part: FRAME — DAMAGED (BS 427) · airframe 33,276 hrs · 22,395 cycles

FRAME BS 427 BETWEEN LONGERONS 24L AND 26L WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-41-02, AND DRAWING 3912348, REV E.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,276 hrs · 22,395 cycles

EMERGENCY EXIT SIGNS OVER THE LT & RT AFT OVERWING EXIT HATCHES WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED SATISFACTORILY IAW AMM 33-51-00.

Part: FORMER — DAMAGED (BS 465) · airframe 33,276 hrs · 22,395 cycles

FORMER, BS 465, BETWEEN LONGERONS 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.

Part: FORMER — DAMAGED (BS 465) · airframe 33,276 hrs · 22,395 cycles

FORMER, BS 465, LONGERON 27L WAS DAMAGED. ACCOMPLISHED A FORMER REPAIR IAW SRM 53-00-06, REPAIR 2.

Part: FORMER — DAMAGED (BS 427) · airframe 33,276 hrs · 22,395 cycles

FORMER AT BS 427 BETWEEN LONGERONS 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.

Part: FORMER — DAMAGED (BS 465) · airframe 33,276 hrs · 22,395 cycles

FORMER STA 465 BETWEEN LONGERONS 25L - 26L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.

Part: FORMER — DAMAGED (BS 446) · airframe 33,269 hrs · 22,387 cycles

FORMER BS 446 BETWEEN LONGERONS 25L - 26L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, DRAWING 9911526, REV AZ, AND REV AN.

Part: FORMER — DAMAGED (BS 408) · airframe 33,269 hrs · 22,387 cycles

FORMER BS 408 BETWEEN LONGERONS 24L - 25L APPEARS TO BE BENT. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.

Part: FORMER — DAMAGED (BS 446) · airframe 33,269 hrs · 22,387 cycles

FORMER BS 446, LONGERON 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-40-02, AND DRAWING 9911526, REV AN, AND REV AZ.

Part: FORMER — DAMAGED (BS 446) · airframe 33,282 hrs · 22,402 cycles

DAMAGED FORMER AT BS 446, LONGERON 27L. ACCOMPLISHED A PERMANENT REPAIR TO THE FORMER IAW SRM 53-00-06, REPAIR 2, AND DRAWING 9912454, REV K.

Part: LONGERON SPLICE — CRACKED (BS 361-397) · airframe 33,269 hrs · 22,387 cycles

LONGERON 23L AT FWD SPLICE REPAIR WAS CRACKED AT BS 389 - 408. ACCOMPLISHED A PERMANENT REPAIR TO THE LONGERON BETWEEN BS 361 TO 397 IAW SRM 53-00-05, REPAIR 2.

Part: LONGERON — DAMAGED (BS 389-490) · airframe 33,269 hrs · 22,387 cycles

LONGERON 24L WAS FOUND DAMAGED BETWEEN BS 389 - 490. CUT OUT THE SECTION OF THE LONGERON. FABRICATED REPAIR SPLICES AND CUT A NEW LONGERON. WORK ACCOMPLISHED IAW SRM 53-00-05, REPAIR 2. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001, NO CRACKS INDICATED. INSTALLED THE NEW LONGERON IAW SRM 53-00-05, REPAIR 2, AND ER/A 570705-14, REV 0.

Part: LONGERON — DAMAGED (BS 427-490) · airframe 33,269 hrs · 22,387 cycles

LONGERON 25L WAS FOUND DAMAGED BETWEEN BS 427 - 490. CUT AND REMOVED THE SECTION OF THE LONGERON . ACCOMPLISHED HFEC IAW NDT SPM 06-10-01. 001, NO CRACKS INDICATED. FABRICATED A REPLACEMENT LONGERON AND SPLICES. INSTALLED THE LONGERON SECTION IAW SRM 53-00-05, REPAIR 2, AND PRI ER/A 570705-14, REV 0.

Part: RELEASE CABLE — OUT OF POSITION (TAILCONE) · airframe 33,236 hrs · 22,369 cycles

AFT INTERNAL TAILCONE RELEASE SYSTEM FAILED THE DROP TEST. IT REQUIRED MORE THAN 35LBS PULL TO ACTIVATE. MAINTENANCE REROUTED THE INTERNAL HANDLE RELEASE CABLE TO THE PROPER ROUTING IAW AMM 53-52-01. TAILCONE RELEASE REPEAT OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (CABIN) · airframe 30,937 hrs · 20,748 cycles

DURING SVC CHECK FOUND EMERGENCY LIGHT DIFFUSER LENS MISSING AT SEAT 12B. FWD TO NEF 33-51-02. REPLACED MISSING LENS COVER.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,795 hrs · 20,653 cycles

THE FLIGHT CREW FOUND THEY COULD NOT CONTROL THE EMERGENCY PATHWAY LIGHTING IN THE CABIN: IT WOULD FLICKER ON AND OFF ON ITS OWN. MAINTENANCE CALLED IT AN ANOMALY AND DID NOT DO ANY FURTHER TROUBLESHOOTING.

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

AFT CARGO BAY HAD CORROSION ON DOOR FRAME PAN. A REPAIR WAS ACCOMPLISHED IAW ETI 17-17-062, REV 3 AND ER/A 558101-14, REV ORIGINAL.

Part: REPAIR — DAMAGED (VERTICAL STAB) · airframe 29,992 hrs · 20,045 cycles

ELONGATED SEVERAL HOLES ON PREVIOUS REPAIR DOUBLER AT VERTICAL STABILIZER LE SPLICE AT STA ZFS=52.267. REPAIR WAS ACCOMPLISHED PER ETI-17-17-060 REV 3 AND ER/A 535894-14AD REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,992 hrs · 20,045 cycles

CRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONG 1 TO 3 RT AFT ACCESSORY COMPARTMENT. REPAIR WAS ACCOMPLISHED PER ETI-17-17-052 REV ORIGINAL AND ER/A 558094-14 REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,992 hrs · 20,045 cycles

CRACKS ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 3L TO 3R AFT ACCESSORY COMPARTMENT. CRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 1 TO 3 LT AFT ACCESSORY WAS REPAIRED PER SRM 53-30-08-2R PROCEDURE 10 REPAIR 10. HFEC INSPECTION WAS ACCOMPLISHED ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 1 TO 3 LT AFT ACCESSORY COMPARTMENT AFTER TRIM OUT AND NO CRACKS WERE FOUND PER SRM 53-30-08-2R-10 PAR 5 A (1) (C) AND NDT SPM REV 14 06-10-01.001.

Part: DOOR — WORN (MLG) · airframe 29,992 hrs · 20,045 cycles

WEAR ON INNER SURFACE OF LT MLG STRUT DOOR. RT MLG DOOR STRUT WAS REPAIRED IN ACCORDING ETI. 17-17-060 REV ORG AND ER/A 558089-14 REV ORIG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,992 hrs · 20,045 cycles

CRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L. CRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L WAS REPAIRED PER ETI-17-17-052 REV. ORIGINAL AND ER/A 558094-14 REV ORIGINAL.

Part: FRAME — CORRODED (BS 974) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORROSION ON FRAME ANGLE BS 974 BETWEEN LONGERONS 24L - 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-01-3, AND DWG 9958215, REV AM.

Part: DOOR FRAME — CRACKED (NLG) · airframe 29,992 hrs · 20,045 cycles

CRACKED DOOR FRAME BEAM LT SIDE OF NOSE GEAR WHEEL WELL NEAR BS 69.550. REPAIRED IAW ETI-17-17-057, REV 3, AND ER/A 558076-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 29,992 hrs · 20,045 cycles

CRACK DOOR JAMB BEAM RT SIDE OF NOSE GEAR WHEEL WELL NEAR STA Y=69.550. REPAIR WAS ACCOMPLISHED PER SRM 53-10-14-2R.

Part: HINGE — WORN (FWD CARGO DOOR) · airframe 29,992 hrs · 20,045 cycles

FREE PLAY ON AFT HINGE AT FWD CARGO DOOR. REPAIRED AIW ER/A 558081-14, REV ORIGINAL.

Part: WEB — DAMAGED (R1 DOOR) · airframe 29,992 hrs · 20,045 cycles

ELONGATED HOLES ON R1 DOOR WEB AND PAN UPPER/FWD CORNER. REPAIRED IAW ER/A 556413-14, REV ORIGINAL, AND ETI-17-17-051, REV ORIGINAL.

Part: ANGLE — CRACKED (BS 1158) · airframe 29,992 hrs · 20,045 cycles

CRACK ON ANGLE AFT FACE BS 1158 LONGERON 2L IN THE AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-41-05, AND 51-41-02.

Part: INTERCOSTAL — DAMAGED (BS 1225) · airframe 29,992 hrs · 20,045 cycles

CRACKED AND BENT ON INTERCOSTAL FWD FACE BS 1225, LONGERON 22L AFT ACCESSORY COMPARTMENT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND 51-10-05, AND DWG 9917701, REV.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORROSION ON FUEL ACCESS PANEL COUNTERSINK. CORROSION REMOVED PER B717 SRM 57-10-01-2R-2 PAR 5 CONDITION II (2) AND (3).

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORROSION ON RUBSTRIPS OF FUEL ACCESS PANEL ON THE LT WING. THE RUBSTRIP WAS REPLACED PER B 717-200 SRM 57-10-01 REP 3 PAR 6.

Part: SKIN — CRACKED (BS 1022) · airframe 29,992 hrs · 20,045 cycles

FUSELAGE SKIN CRACKED BS 1022, LONGERON 14L. REPAIRED IAW ETI-17-17-050, REV ORIGINAL, AND ER/A 556410-14, REV ORIGINAL.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 29,992 hrs · 20,045 cycles

BROKEN FLOOR PANEL 221SP. REPAIRED IAW SRM 53-20-50-2R-5.

Part: FRAME — CRACKED (BS 679) · airframe 29,992 hrs · 20,045 cycles

CRACKED FRAME BS 679, BETWEEN LONGERONS 25 - 28L IN KEEL BEAM AREA. REPAIRED IAW SRM 51-70-11-2R, REPAIR 1.

Part: FRAME — CRACKED (BS 679) · airframe 29,992 hrs · 20,045 cycles

CRACKED FRAME BS 679 BETWEEN LONGERON 25 - 28R. THE FRAME WAS REPAIRED IAW SRM 51-70-11-2R.

Part: FRAME — CRACKED (BS 1022) · airframe 29,992 hrs · 20,045 cycles

CRACKED MAIN FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 AND 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06R, 51-41-05, AND DWG 9912243, REV JS.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 29,992 hrs · 20,045 cycles

CRACKED CHANNEL OF FLOOR PANEL 222AFF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50-2R-5.

Part: ANGLE — CORRODED (BS 120-148) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORRODED ANGLE, BELOW THE RT CONSOLE, BETWEEN BS 120 - 148, RBL 54 IN THE COCKPIT. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND DWG 9936533, REV CM.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 29,992 hrs · 20,045 cycles

CRACKED FUSELAGE ACCESS PANEL 370AR. THE ACCESS PANEL WAS REPAIRED SRM 55-00-00-2R, REPAIR 1, PROCEDURE 1, AND 51-41-02 HFEC INSPECTION WAS ACCOMPLISHED ON ACCESS PANEL 370 AR, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-01.001.

Part: ANGLE — CORRODED (BS 737-756) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORROSION ON RT CUSP ANGLE LOWER SURFACE FROM BS 737 - 756. A NEW CUSP ANGLE WAS REPLACED IAW SRM 51-41-02.

Part: PAN — CRACKED (FUSELAGE) · airframe 29,992 hrs · 20,045 cycles

CRACKED WINDOW RING PANS ON FOLLOWING LOCATIONS. LWR RT STA 909, UPPER LT STA 850, UPPER LT STA 831. CRACKED WINDOW RING PANS WERE REPAIRED PER SRM 56-20-02-2R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,992 hrs · 20,045 cycles

CORROSION ON RT FLOOR SUPPORT STA Y=180 BTW X=-9 TO X=-42 FWD WET AREA. DUE TO EXCESSIVE CORROSION ON FLOOR SUPPORT WAS REPLACED PER SRM 51-41-05 AND 51-40-08-0G AND 51-10-04 PAR 15 AND 21.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,148 hrs · 19,432 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE CATWALK WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD. (LP #9077376)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,233 hrs · 18,804 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT COMPARTMENT DOOR WAS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING AND REPLACED THE CHARGER B5-260. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (LP #8920821)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,909 hrs · 18,518 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 15-19 OF THE CABIN AND THE AFT TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE SKIN DAMAGE BETWEEN STA 1095 AND STA 1116, L-21L AND L-23L REF EMPOWER NR 35, RII ENTRY, REF NR 35 REPAIRS MADE IAW ER/A 547473-14, REV A. ASSOCIATED ER/A 14-547473 ADDED FOR AC 9562.

Part: FRAME — DENTED (FUSELAGE) · airframe 27,870 hrs · 18,484 cycles

CANTED FRAME 1189 IS DENTED AT SKIN CUTOUT FOR REPAIR OF DAMAGE AT STR-11R. REPAIRED IAW ER/A 547985-14, REV A, SECTION 2, FRAME DAMAGE PERMANENT REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,870 hrs · 18,484 cycles

FUSELAGE DENT ON LT SIDE, STA 1087 AT L-20L. CW ER/A 547473-14, REV A, FINAL ER/A MATCHES ALL PRI REVISIONS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,870 hrs · 18,484 cycles

DAMAGE TO EMPENNAGE SKIN STA 1178-1144 FROM LONGERON 3R-9R MULTIPLE LOCATIONS. REPAIRED SKIN IAW ER/A 547582-14, REV ORIGINAL ER/A MATCHES ALL PRIS.

Part: SKATE ANGLE — DEFORMED (FUSELAGE) · airframe 27,870 hrs · 18,484 cycles

RT SIDE VERTICAL STABILIZER ATTACH SKATE ANGLE IS DEFORMED. REPAIRED IAW ER/A 547541-14, REV ORIGINAL ER/A MATCHES ALL PRIS.

Part: SKIN PANEL — DAMAGED (VERTICAL STAB) · airframe 27,870 hrs · 18,484 cycles

VERTICAL STABILIZER, RT L/E LOWER MAIN SKIN PANELS DENTED AND GOUGED. REPAIRED SKIN IAW ER/A 547396-14, REV ORIGINAL, ER/A MATCHES ALL PRIS.

Part: SKIN — DAMAGED (BS 1155) · airframe 27,870 hrs · 18,484 cycles

FUSELAGE SKIN DAMAGED AT APPROXIMATELY BS 1155 L-20L. COMPLETED REPAIR, REF SRM 53-03-01, FIG 204. CLASS 1, REF NR 27 SUMMERY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

DAMAGE TO VERTICAL STABILIZER RT SKATE ANGLE AND SKIN BETWEEN L2R AND L4R, BETWEEN STA 1103 AND 1145. ACCOMPLISHED HFEC INSPECTION OF CRACK IAW NDT/SPM 06-10-01.001, MARKED THE END OF THE CRACK END AND VERIFIED AFT CRACK EXTENDS INTO CENTER OF A RIVET HOLE OTBD OF SKATE ANGLE. CONTAINED DAMAGE BY STOP DRILL .2500". APPLIED SPEED TAPE AND IDENTIFIED AS ENGINEERING APPROVED IAW ER/A 547090-14, REV ORIGINAL SECTION II. REPAIRED RT SKATE ANGLE IAW ER/A 547541-14, REV ORIGINAL. ER/A MATCHES ALL PRIS. REPAIRED SKIN BETWEEN L2R AND L4R, BETWEEN BS 1103 AND 1145 IAW ER/A 547396-14, REV ORIGINAL. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — GOUGED (BS 1159) · airframe 27,870 hrs · 18,483 cycles

LT FUSELAGE GOUGE / DENT 3" X 8" BS 1159, STR 19-20L .0625" DEEP. BLENDED IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACKS NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISHED UT INSPECTION IAW NDT/SPM 04-00-03. ALODINE AND PRIMED; IDENTIFIED AS ENGINEERING APPROVED IAW ER/A 547070-14. ASSOCIATED ER/A 00-547070 ADDED FOR AC 9562.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE SKIN PUNCTURED BETWEEN CANTED STA 1103 AND 1131 BETWEEN L6R AND L7R. CUTOUT DAMAGED SKIN. ACCOMPLISHED HFEC INSPECTION OF CUTOUT IAW NDT/SPM 06-10-01.001. NO CRACKS NOTED. INSTALLED DOUBLER IAW INSTRUCTIONS OF ER/A 547090-14, SECTION III. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A, ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — DENTED (BS 1159) · airframe 27,870 hrs · 18,483 cycles

LT FUSELAGE DENT 3" X 2", .0937" DEEP. BS 1159, STR 20-21L. BLENDED IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACKS NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISHED UT INSPECTION IAW NDT/SPM 04-00-03. ALODINE AND PRIMED; IDENTIFIED AS ENGINEERING APPROVED IAW ER/A 547070-14, REV ORIGINAL. ASSOCIATED ER/A 00-547070 ADDED FOR AC 9562.

Part: SKIN — GOUGED (BS 1076-1087) · airframe 27,870 hrs · 18,483 cycles

LEFT FUSELAGE GOUGE, DENT 3" X 2.5" X .1250" DEEP BETWEEN BS 1076-1087, STR 20L. DURING CLEAN-UP OF GOUGE NOTICED RIVET SHEARED. REMOVED REMAINING FASTENER. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACK NOTED. ACCOMPLISHED GVI WITH NO VISABLE DAMAGE NOTED. ACCOMPLISHED UT THICKNESS IAW NDT, SPM 04-00-03. INSPECTION OF OPEN HOLE IAW NDT/SPM 06-10-01.003, NO CRACK NOTED. INSTALLED BLIND FASTENER IAW ER/A 547070-14, REV ORIGINAL. ASSOCIATED ER/A 00-547070 ADDED FOR AC 9562.

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

SEVERE GOUGE AT FS 1133 BETWEEN L-8R AND L-9R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE SKIN PUNCTURED AT FS 1087, L-7R AND L-8R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

MULTIPLE GOUGES AND DENTS AT L-3R BETWEEN FS 1095 AND FS 1144. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

DENT IN FUSELAGE AT FS 1076 BETWEEN L-7R AND L-9R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — DENTED (BS 1087-1116) · airframe 27,870 hrs · 18,483 cycles

FUSELAGE SKIN DENTED BETWEEN BS 1087-1116, STRINGERS 22 -23L. BLENDED AREA IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 6-10-01.001. NO CRACK NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISH UT THICKNESS IAW NDT/SPM 04-00-03. ALODINE AND PRIMED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

DENTS AND GOUGES BETWEEN FS 1116 AND FS 1144, BETWEEN L-7R AND L-8R, 2 EACH. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

MULTIPLE GOUGES FROM FS 1095 TO FS 1144 BETWEEN L-4R AND L-7R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01. 001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: SKIN — DENTED (BS 1053-1076) · airframe 27,870 hrs · 18,483 cycles

RIGHT FUSELAGE DENTED BETWEEN BS 1053-1076. STRINGERS 22-23R. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001. NO CRACKS NOTED.

Part: SKIN — DENTED (BS 1022-1037) · airframe 27,870 hrs · 18,483 cycles

RIGHT FUSELAGE DENTED AT BS 1022 - 1037, L21 - 22R. BLENDED AREA FOR HFEC. IAW SRM 53-01-01. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ACCOMPLISHED UT THICKNESS OF AREA IAW NDTSPM 04-00-03.

Part: SKIN — DENTED (APU DOOR) · airframe 27,870 hrs · 18,483 cycles

RT APU DOOR DENTED 7.0312" DEEP. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED. ALODINE AND PRIMED.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

MULTIPLE DENTS AT FUSELAGE STA 1087 BETWEEN L-3R AND L-7R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE SKIN PUNCTURED. APPROXIMATELY 2" AFT OF FS 1087, BETWEEN L-3R AND L-4R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSP IAW ALERT.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 27,893 hrs · 18,506 cycles

DENT AND GOUGES IN RT VERTICAL STABILIZER SKIN APPROXIMATELY 12" ABOVE FUSELAGE BETWEEN CS 1103 AND CS 1131. BLEND AREA OF PAINT FOR HFEC. REF SRM 53-01-01. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREA IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINE AND PRIMED ALL BARE AREAS. IDENTIFIED AS ENGINEERING APPROVED IAW ER/A 547104-14, REV ORIGINAL. REPAIRED SKIN IAW ER/A 547396-14-14, REV ORIGINAL. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE PUNCTURE BETWEEN FS 1095 AND FS 1116, AT L-8R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC PER NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,893 hrs · 18,506 cycles

FUSELAGE SKIN GOUGE AND PUNCTURE JUST AFT OF FS 1178, L-11R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A, ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT.

Part: STRUCTURE — DAMAGED (LT NACELLE) · airframe 27,870 hrs · 18,483 cycles

LT ENGINE LOWER APRON DAMAGED AFT EDGE 3" X .5". REPLACED LT ENGINE FIXED COWLING APRON IAW AMM 71-14-01-400-801.

Part: CABLE — DAMAGED (TAILCONE RELEASE) · airframe 27,870 hrs · 18,483 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE KEVLAR CABLE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: WIRE HARNESS — DAMAGED (NR 2 ENGINE) · airframe 27,870 hrs · 18,483 cycles

THE FLIGHT WAS DIVERTED FOLLOWING THE SHUTDOWN OF THE NR 2 ENGINE. ALSO, ALL OF THE ENGINE COWLING EXITED THE ACFT WHILE IN FLIGHT. MAINTENANCE REPAIRED THE FUSELAGE DAMAGE AND REPLACED THE NR 2 ENGINE DUE TO WIRE HARNESS DAMAGE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,349 hrs · 16,453 cycles

AFT EMER EXIT LIGHT HAS BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: FLASHLIGHT — DISCONNECTED (CABIN) · airframe 25,349 hrs · 16,453 cycles

AFT EMER FLASHLIGHT INOPERATIVE. CONNECTED FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,349 hrs · 16,453 cycles

RIGHT AFT OVERWING DOOR EMER EXIT SIGN LIGHT BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,349 hrs · 16,453 cycles

EMERGENCY EXIT LIGHT ABOVE R1 INOPERATIVE BULB. RELAMPED SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,995 hrs · 15,545 cycles

AFT BULKHEAD DOOR EMER LIGHT BATTERY PACK INOPERATIVE AT BS 1053. R & R BATTERY PACK IAW CMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

CUSP WEB CRACKED AT BS 598, FWD OTBD CORNER. REPAIRED CUSP WEB IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

R1 DOOR AFT GIRT BAR FITTING CORRODED. R & R FITTING IAW DWG.

Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LOWER HALF OF THE TAIL CONE DELAMINATED. R & R TAIL CONE IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT CUSP WEB CRACKED AT BS 655, LBL 54. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 503 - 522, LBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT CUSP WEB CORRODED AT BS 370 - 389. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

CUSP WEB CRACKED AT BS 674, RBL 44. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 541 - 560. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 579 - 598. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 484 - 503. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

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

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 23,995 hrs · 15,545 cycles

RIGHT WW INBD SIDE OF INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 23,995 hrs · 15,545 cycles

LEFT WW FWD DOOR CUT OUT INBD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: CAP — CRACKED (LE SLAT) · airframe 23,995 hrs · 15,545 cycles

RIGHT WING NR 5 SLAT END CAP CRACKED. R & R END CAP IAW SRM & DWG.

Part: FITTING — CRACKED (LT MLG DOOR) · airframe 23,995 hrs · 15,545 cycles

LEFT MLG WW DOOR AFT UPPER INTERNAL FITTING CRACKED. R & R FITTING IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

LEFT FRAME CRACKED AT BS 696, LONGERON 18L. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

RIGHT FRAME CRACKED AT BS 674, LONGERON 18R. R & R FRAME IAW DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 23,995 hrs · 15,545 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,352 hrs · 16,454 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,352 hrs · 16,454 cycles

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

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 24,862 hrs · 16,127 cycles

R1 DOOR SLIDE INADVERTENTLY DEPLOYED DURING REMOVAL. R & R SLIDE IAW MM.

Part: COVER — MISSING (CABIN) · airframe 24,522 hrs · 15,896 cycles

RIGHT OVERHEAD EMER LIGHT COVER MISSING AT ROW 14. INSTALLED COVER IAW AMM.

Part: PANEL — CRACKED (LT WING) · airframe 23,175 hrs · 15,014 cycles

LT WING TE AREA PANEL ADJACENT OF INBD BUTE DOOR AT OTBD AREA OF HINGE AT BS 180 APPROXIMATELY LOWER AREA CRACKED. REPAIRED PANEL IAW DRAWING & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

FLOOR SUPPORT CRACKED AT BS 655, BL 0. R & R SUPPORT IAW DRAWING.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 23,175 hrs · 15,014 cycles

MAIN CABIN FLOOR PANEL 222ADF FLEX JOINT & COVER CRACKED ON LT SIDE. R & R PANEL IAW SRM & DRAWING.

Part: FITTING — CRACKED (NLG WW) · airframe 23,175 hrs · 15,014 cycles

LT WW FWD DOOR CUTOUT OTBD SIDE CLIP CRACKED. R & R CLIP IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

WEB CORRODED BETWEEN BS 168 TO BS 200, BETWEEN LBL 1 TO LBL 14. R & R WEB IAW SRM.

Part: DOUBLER — CRACKED (LT WING) · airframe 23,175 hrs · 15,014 cycles

LT WING INBD BUTE DOOR DOUBLER CRACKED AT INBD DOOR CORNER. REPAIRED DOUBLER IAW EA.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

LT WING TO BODY SUPPORT BRACKET CORRODED BETWEEN BS 832 TO BS 847, LONGERON 30L. R & R FORMER IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

FORMER CORRODED AT BS 832, BETWEEN LONGERON 30L TO LONGERON 27L. R & R FORMER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

FWD ENTRY SEAT TRACK CORRODED AT BS 229, RBL 27. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,175 hrs · 15,014 cycles

AFT GALLEY SEAT TRACK CORRODED AT BS 229, RBL 44. R & R SEAT TRACK IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,613 hrs · 14,636 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: FITTING — DIRTY (L1 DOOR) · airframe 22,555 hrs · 14,601 cycles

L1 DOOR EMERGENCY EVAC SLIDE FLOOR FITTINGS DIRTY. CLEANED FITTINGS IAW MM.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 21,490 hrs · 13,933 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK INADVERTENTLY FELL OUT. REINSTALLED GIRT BAR PER AMM.

Part: COVER — BROKEN (R1 DOOR) · airframe 20,641 hrs · 13,418 cycles

R-1 DOOR SLIDE COVER HINGE IS BROKEN CAUSING COVER NOT TO BE SECURE. REPLACED R-1 DOOR SLIDE COVER. OPS CHECK GOOD AT THIS TIME REF AMM. PART NUMBER VERIFIED.

Part: COVER — BROKEN (R1 DOOR) · airframe 19,952 hrs · 12,993 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BROKEN. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — LOOSE (L1 DOOR) · airframe 19,666 hrs · 12,804 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER AMM.

Part: PIN — MISSING (EVAC SLIDE) · airframe 19,408 hrs · 12,636 cycles

L1 DOOR EMERGENCY EVAC SLIDE PINS MISSING. REMOVED AND REPLACED SLIDE PER MM.

Part: DOOR — MALFUNCTIONED (CARGO BAY)

C2 DOOR, HARD TO OPEN AND MAKES POPPING SOUND. ACCOMPLISHED DOOR REPLACEMENT PER SRM 52-31-01.

Part: PAN — CRACKED (CARGO DOOR)

C2 CARGO DOOR FWD SIDE DOOR PAN, CRACKED. ACCOMPLISHED DOOR REPLACEMENT PER SRM 52-31-01.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY)

C-2 CARGO DOOR LOWER JAMB, CORROSION. ACCOMPLISHED LOWER JAMB SPLICE REPAIR PER SRM 53-20-15 AND 53-00-15.

Part: DEPRESSOR — CRACKED (CARGO DOOR)

C-2 CARGO DOOR AFT SIDE SEAL DEPRESSOR, CRACKED. ACCOMPLISHED SEAL DEPRESSOR REPLACEMENT PER. SEE NR 25090.

Part: RELEASE MECH — FAILED (TAILCONE)

TAIL CONE CAM RELEASE MECHANISM, FAILED DURING DEPLOYMENT. ACCOMPLISHED CAM RELEASE MECHANISM ADJUSTMENT PER B717 MM 53-52-03 AND 53-52-01. SEE NR 25139.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY SUPPLY ASSY AT B5-123 IAW AMM 33-51. OP'S CHECK GOOD.

Part: LOCK — OBSTRUCTED (GIRT BAR)

GIRT BAR FLOOR FITTING WILL NOT CLOSE WITH GIRT BAR ARMED. CLEANED GIRT BAR LOCK AND SPRING, OPS NORM.

Part: COVER — CRACKED (EVAC SLIDE)

L1 DOOR SLIDE - GAUGE COVER CRACKED. REMOVED AND REPLACED L-1 SLIDE REF M/M 28-61 AWI.

Part: SKIN — DAMAGED (BS 1029)

SKIN DAMAGE CAUSED BY BELTLOADER AFT CARGO DOOR NEAR STATION 1029. REPAIRED PER EA-17-53-0120IR SECTION 1 STEPS 1 THRU 7 AND PERFORMED PRESSURE CK PER B717 MM 21-30, NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY B5-118 REF WDM 33-51-14 AND OPS CHECK EMERGENCY LIGHTS REF AMM 33-51.