N950AT

Part: NONE — NONE (NONE) · airframe 61,774 hrs · 44,129 cycles

SHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)

Part: PAN — CRACKED (ZONE 100) · airframe 60,986 hrs · 43,369 cycles

SHIP 9509 INITIAL INSPECTION: CRACK ON FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT. CORRECTIVE ACTION: FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT WERE REPAIRED PER ERA 626981-14 REV. ORIGINAL, SECTION I, PERMANENT REPAIR AND PRI 626981-14 REV . 2 (1058299)

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

CORROSION ON INTERCOSTALS BTW STA Y=1022 & Y =1037 AT LONG 30 & LONG 29R BILGE AREA AT AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05- 0G AND SRM 51-41-02 .

Part: FRAME ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

CORROSION ON FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. WERE REPLACED PER DWG 9919605-15.

Part: GUIDE VANE — WORN (ZONE 600 FLAP) · airframe 60,970 hrs · 43,356 cycles

WEAR ON GUIDE VANE BEHIND HINGUE FLAP 1 AT RH WING. CORRECTIVE ACTION: GUIDE VANE WAS REPAIRED PER B717-200 SRM 57-53-01.

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 60,970 hrs · 43,356 cycles

DENT OUT OF LIMITS, AT LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX (2 INCHES FROM T.E. AND 12 INCH FROM L.E.): W=WIDTH, Y =DEPTH (NO MORE 0.060 INCH), RATIO W/Y= MUST BE 10 OR MORE, DENT #17: W=2.0 INCH, Y=0.090 INCH AND W/Y= 22.22 PER B717-200 SRM 57-53-01-1A ALLOWABLE DAMAGE 1 PAR. 3. A. (1) TO (3) AT LH WING. LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CORROSION AT LOWER SKIN DOOR JAMB ON MIDDLE DOORSTOP (AFT CARGO COMPARTMENT). CORRECTIVE ACTION: (CORROSION LEVEL 2) DOOR JAMB ON MIDDLE DOOR TOP (AFT CARGO COMPARTMENT) WAS REPLACED PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-01-0G.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1034104)

Part: FRAME — CRACKED (ZONE 200) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1033875)

Part: PAN — CRACKED (ZONE 800) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CRACK ON PAN NEAR TO BEAM NBR 2 AFT EDGE AT PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP 1032719)

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CORROSION WAS FOUND ON DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. CORRECTIVE ACTION: DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP 1031776)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CORROSION ON LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029594)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CORROSION ON INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029591)

Part: LONGERON — CRACKED (ZONE 200) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CRACK ON LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX) WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP 1022148)

Part: PAN — CRACKED (ZONE 100) · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, AFTER SEAL RETAINERS REMOVAL, CRACK ON INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS FOUND. CORRECTIVE ACTION: INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 4 FIG. 201. (LP 1013153)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,970 hrs · 43,356 cycles

AIRCRAFT 9509, CORROSION ON RH CUSP WEB UPPER & LOWER FACE ON STA Y=373 AT CABIN PAX. CORROSION LEVEL 2, CUSP WEB ON STA Y=373 AT CABIN PAX WAS REAPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP1011516)

Part: INSPECTION — NONE (NONE) · airframe 60,970 hrs · 43,356 cycles

SHIP 9509 COMPLY WITH ERA 623616-14AD RH WING/ REAR SPAR/ LOWER CAP CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 623616-14AD (0978229)

Part: STRUCTURE — WORN (WING ROOT) · airframe 60,970 hrs · 43,356 cycles

SHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)

Part: NONE — NONE (NONE) · airframe 60,970 hrs · 43,356 cycles

SHIP 9509 INSTALL LH INBOARD AND CENTER BUTE DOORS. CORRECTIVE ACTION: C/W ER/A 623425-14AD (0972844)

Part: SPAR — CRACKED (ZONE 500) · airframe 60,967 hrs · 43,355 cycles

CRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER WING BOOST PUMP PANEL TO F.O.M. PER B717 AMM 28-00. RE-INSTALLED TANK PLATE 520CB PER B717 AMM 28-00. RE-INSTALLED FUEL LINES PER B717 AMM 28-10. LEAK CHECK GOOD. ASSOCIATED AA 5720-01103 ADDED FOR AC 9509. ASSOCIATED ER/A 14-623253 ADDED FOR AC 9509. (LP #6939592)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 60,966 hrs · 43,354 cycles

CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2ND FASTENER INBOARD OF FLAP HINGE FITTING EXTERIOR FROM TRAILING EDGE THROUGH FASTENER INTO RADIUS. MARKED. COMPLIED WITH PRI 623253-14 REV ORIGINAL ON LOG 6939592. (LP #6939586)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,927 hrs · 40,690 cycles

PUNCTURE IN FUSELAGE RT SIDE AFT OF FORWARD CARGO DOOR. THIS WAS ORIGINALLY DOCUMENTED IN LP #4849328 AND TRANSFERRED TO THIS LOG PAGE. MAINTENANCE REMOVED THE DAMAGE, DRILLED DOUBLER REF B717 53-03-01-2R PROCEDURE 1 REPAIR 1 CLASS 2 FIG 202 SHT 3, FABRICATED REPAIR DOUBLER PER B717 SRM 53-03-01-2R PROCEDURE 1, AND INSTALLED REPAIR DOUBLER PER B717 SRM 53-03-01-2R PROCEDURE 1 CLASS 2 FITG 202 SHT 3. INSTALLED REPAIR PER B717 SRM 53-03-01-2R PROC 1 CLASS 2 FIG 202 SHT 3 PERMANENT REPAIR WITH REPETITIVE INSPECTION REQUIREMENTS. REQUIRES EXTERNAL LEFC OR EXTERNAL ULTRASONOC INITIAL 28,000 CYCLES REPETITIVE 15,000 CYCLES REF B717 SRM 53-03-01-2R-1 TABLE 202 CLAS 2 REPAIR METHOD 1 PAGE 12. (LP #2916616)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,675 hrs · 40,466 cycles

THE CEILING EMERGENCY EXIT LIGHT COVER FELL OFF AT ROW 22. MAINTENANCE RESECURED THE LIGHTING COVER. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8310082)

Part: NONE — NONE · corrosion level 2 · airframe 56,877 hrs · 39,736 cycles

LT SLANT PANEL HAS CORROSION ON IT AT NUT PLATE LOCATION SEEN FROM THE INSIDE. BOTTOM ROW APPROX. LBL27. SUMMARY SEE NRC 001-0196:5300-2005/001 00276: COMPLIED WITH ER/A PRI 606032-14 REV "0","1" INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 606032-14 REV ORIG SECTION I PERMANENT REPAIR INSTRUCTIONS WITH COMPLETED STEPS COMPLETED ON ER/A PRI 606032-14 REV "0","1". COMPLIED WITH ER/A PRI 606032-14 REV A, REV "0", INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 606032-14 REV A. SECTION I PERMANENT REPAIR INSTRUCTIONS WITH COMPLETED STEPS ON ER/A PRI 606032-14 REV A REV "0 ASSOCIATED ER/A 00-606032 ADDED FOR AC 9509. (LP #2641122)

Part: UNKNOWN — UNKNOWN · airframe 56,877 hrs · 39,736 cycles

C/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. (LP #2621093)

Part: DOOR SILL — DAMAGED · airframe 55,093 hrs · 38,131 cycles

FORWARD EDGE OF AFT CARGO DOOR FRAME SILL WAS DAMAGED BY BAGGAGE CREW WITH BELT LOADER. MAINTENANCE REMOVED DAMAGED SCUFF PLATE AND REFORMED PER B717 SRM 51-20-09-0G. INSPECTED SCUFF PLATE, NO CRACKS NOTED. COMPLIED WITH B717 SRM 53-00-15-2R. REINSTALLED SCUFF REF BOEING DWG 5910158. OK FOR SERVICE. (LP #8650878)

Part: NONE — NONE · airframe 55,019 hrs · 38,059 cycles

SHIP 9509 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING LANDING DUE TO THE RIGHT HYDRAULIC QUANTITY SHOWING A LOW INDICATION (BUT NOT EMPTY). CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE #3 BRAKE PRESSURE LINE HAD BEEN DAMAGED BY A BIRD STRIKE AND WAS LEAKING. THE LINE WAS REPLACED, THE SYSTEM WAS BLED, AND THE AIRCRAFT RETURNED TO SERVICE. (LP #8650837)

Part: NONE — NONE · corrosion level 2 · airframe 54,614 hrs · 37,686 cycles

CORROSION AROUND EXTERIOR SIDE OF VACUUM BLOWER FOR LAV TANK EXHAUST VENT -M-. SUMMARY SEE NRC 001-0247:2550-2003/001 00405: REPAIRED AREA AROUND VENT PER ER/A 597013-14 PRI REV 0 THROUGH REV 3 AND ER/A 597013-14 REV ORIGINAL. (LP #2118994)

Part: NONE — NONE · airframe 54,614 hrs · 37,686 cycles

FUSELAGE CROWN LIGHTNING STRIKE DAMAGE AT PREVIOUS BLEND OUT. NO REPAIR TAG PRESENT. -M-. SUMMARY SEE NRC 001-0249:5300-2018/003 00365: REPAIRED LIGHTNING STRIKE DAMAGE ON CROWN PER ER/A 597099-14 PRI REV. 0 THROUGH REV 1. AND ER/A 597099-14AD REV. ORIGINAL. (LP #2119957)

Part: NONE — NONE · airframe 54,614 hrs · 37,686 cycles

WHILE PERFORMING INSPECTION OF APU ENCLOSURE FWD SKIN ASSY. STA 1064 FOUND -2 REPAIR DOUBLER TO BE MISSING UPPER RH FASTENER PER ERA 540237-14 REV. O FIG. 2. SUMMARY SEE NRC 007-0001:21-0553-8- 7617/001 00320: REPAIRED PER ERA 540237-14 AND UPDATED LOG 2167684 AS REQUIRED. (LP #2110560)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,747 hrs · 35,576 cycles

CORROSION ON FLOOR FITTINGS G-7 (CPAX). CORROSION LEVEL 2, FLOOR FITTING OF G-7 WAS REPLACED PER ER/A 535099-14MA REV H AND CMM 25-30-16 REPAIR SECTION.

Part: CARGO TRACK — CORRODED (BS 813-1022) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

SEVERAL POINTS OF CORROSION ON LH TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT (CCT). NRC 00271: CORROSION LEVEL 2, CORROSION ON TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR.5 FIG.3 (SHEET 1 AND 2), ON LH TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT (CCT) NOMINAL THICKNESS IS 0.100", MAXIMUM REMAINING THICKNESS IS 0.012" THEREFORE ITS OUT OF LIMITS AND WAS REPLACED PER B-717-200 SRM 53-20-52-1A-2-FIG 101 AND B717-200 SRM 51-41-01-0G. TOOLS USED PANAMETRICS 38 DL PLUS OLYMPUS EXP DATE 22FEB19 S/N 171455902 TRANSDUCER SONOPEN V260-RM S/N 1090377. (LP #0930725)

Part: CARGO TRACK — CORRODED (BS 813-954) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

SEVERAL POINTS OF CORROSION ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT). NRC 00272: CORROSION LEVEL 2, ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT), TIE TRACK WAS REPLACED PER B717-200 SRM 51-40-08-0G AND B717-200 SRM 51-41-01-0G. (LP #0930152)

Part: DOUBLER — CORRODED (BS 851) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

DURING INSPECTION OF A REPAIRED AREA AT FUSELAGE SKIN STA 851; L29L-29R, SOME CORROSION WAS FOUND. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929471)

Part: ACCESS PANEL — CORRODED (LAV SERVICE) · airframe 51,743 hrs · 35,574 cycles

CORROSION ON LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE. (FUS). NRC 00059: LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-02 AND 51-41-05. (LP #0928367)

Part: SKIN — CORRODED (BS 851) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION WAS FOUND AT FUSELAGE SKIN STA 851; L29L-29R. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. PERFORM ACOMPLISH ER/A 540245-14 REV. ORIGINAL SECTION I. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929473)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

EXFOLIATION TYPE CORROSION ON FLOOR SUPPORT STA 655 BTW L28L TO L28R 5331-2007 (CCD). NRC 00291: CORROSION LEVEL 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND DWG #5971111 REV. F. (LP #0925601)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R AT AFT CARGO COMPARTMENT 5331-2001. NRC 00224: CORROSION LEVEL 2, PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R WAS REPAIRED PER ETI-17-19-003 REV 2 AND ER/A 574867-14 REV ORIGINAL. PERMANENT REPAIR FOLLOWED UNDER LOG #0917043. (LP #0924239)

Part: LONGERON — NOT REPORTED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

REMOVE LONGERON 25L BETWEEN STA 974/994 (IN REF NRC 00059) FOR SPLICE REPAIR PER SRM 53-00-05-2R-2. LONGERON 25L WAS REPAIRED PER SRM 53-00-05-2R-2. (LP #0922514)

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,019 hrs · 35,779 cycles

CRACK ON LT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00500: LT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. DOUBLER WAS INSTALLED PER SRM 51-41-05-0G AND 56-10-02-2R. (ET) HFEC INSPECTION WAS ACOMPLISHED ON LT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120, PER NDT SPM 06-10-01.001 AND SRM 56-10-02-2R-1 FIG 201 SHEET 11 FLAG NOTE B 3. NO CRACK WAS FOUND BEYOND STOP DRILL. (LP 0922488)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,921 hrs · 35,697 cycles

TWO CRACKS ON FWD TOP SKIN AND ONE CRACK ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369. (CAT). NRC 00513: CRACKS (2) ON FWD TOP SKIN AND CRACK (1) ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369 WERE REPAIRED PER ETI-17-19-009 REV. 1 AND ER/A 574739-14 REV. ORIG. ACCOMPLISH ER/A 574739-14 REV ORIGINAL SECTION II: REPETITIVE INSPECTIONS EVERY C-CHECK OR WITHIN EVERY 24 MONTHS, WHICHEVER OCCURS FIRST, AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR UNDER LOG #0916858. ASSOCIATED ER/A 17-574739 ADDED FOR AC 9509. (LP #0922463)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION TYPE EXFOLIATION ON SPLICE STA Y=898.500 BTW L27R TO L26L AT AFT CARGO COMPARTMENT AMDS 5331-2001. (CCT). NRC 00165: CORROSION LEVEL 2. SPLICE STA Y=898.500 BTW L27R TO L26L WAS REPLACED PER SRM 51-41-05. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG. 3 (SHEET 1 AND 2) ON SPLICE STA Y= 898.500 BTW L27R TO L26L AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.080" AND REMAINING THICKNESS IS 0.016" THEREFORE IT IS OUT OF LIMITS AND MUST BE REPLACED PER 53-00-00-1A FIG 103. TOOLS USED: 38 DL PLUS EXP 20AUG19 S/N: 140939908, TRANSDUCER V260-RM S/N: 1087478. (LP #0921207)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00499: RT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-01-02-0G, AND 51-41-05-0G. (ET)(HFEC) WAS ACCOMPLISHED ON RT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. AFTER STIFFENER REMOVAL AND NO CRACKS WERE FOUND PER NDTSPM PART 6. 06-10-01.001 (EQUIP. 600 N/C 1601 EXP. 15MAR19). (LP #0921334)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON FLOOR PANEL STA 120 (CPAX). NRC 00514: CORROSION LEVEL 2, FLOOR PANEL STA 120 WAS REPLACED PER DWG #9957828 REV: Y. (UT) ACCOMPLISHED PER NDT 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2 ON FLOOR PANEL STA 120. ORIGINAL THICKNESS IS 0.100" AND MAXIMUM REMAINING THICKNESS IS 0.047" THEREFORE IT IS OUT OF LIMITS PER SRM 53-00-00-1A FIG 103. TOOLS USED: 38 DL PLUS S/N: 151215011 EXP. 16NOV19 TRANSDUCER V260-RM S/N: 1087464. (LP #0921210)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14R. (FUS). NRC 00047: CRACK AT FUSELAGE SKIN WAS REPAIRED PER ETI-17-19-001 R2 AND ER/A 574710-14 REV. ORIGINAL SECTION: I PERMANENT REPAIR. ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR FOLLOWED UNDER LOG #0914525. ASSOCIATED ER/A 14-574710 ADDED FOR AC 9509. (LP #0920102)

Part: BEAM — CRACKED (NLG WW) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RT NLG DOOR JAMB BEAM STA Y=40. (NLG). NRC 00155: RT NLG DOOR JAMB BEAM STA Y=40 WAS REPAIRED PER ER/A 495600-14MA REV. C.(ET)(HFEC) WAS ACCOMPLISHED ON RT NLG DOOR JAMB BEAM STA Y=40.(NLG) AND CRACK WAS DIMENSIONED WITH 1.500" LENGTH PER NDTSPM 06-10-01.001 EQUIP. (600 N/C 1601 EXP. 15MAR19).(ET)(HFEC) WAS ACCOMPLISHED ON RT DOOR JAMB BEAM STA Y=40 NLG NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM PART 6 06-10-01.001 (EQUIPMENT C/N 2309 EXP. 09AUG2019). PERFORM A DVI OF THE BLIND BOLTS INSTALLED PER SECTION I LOOKING FOR LOOSE / MISSING DISTRESSED FASTENERS PER ER/A 495600-14MA REV C SECTION II. EVERY 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT. ASSOCIATED ER/A 14-495600 ADDED FOR AC 9509. (LP #0920055)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION AT LONGERON 28L FROM STA 200 TO 220 (E/E). NRC 00377: CORROSION LEVEL 2, SECTION OF LONGERON 28L FROM STA 157 TO 228 WAS REPLACED PER SRM 51-41-02 AND 51-41-05. (LP #0917467)

Part: GUSSET — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R AT PAX CABIN. (CPAX). NRC 00482: GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R AT PAX CABIN WAS REPAIRED PER ETI-17-19-004 REV. 1 AND ER/A 574801-14 REV ORIGINAL. ASSOCIATED ER/A 00-574801 ADDED FOR AC 9509. (LP #0917302)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION AT LONGERON 29L FROM STA 200 TO 220 (E/E). NRC 00376: CORROSION LEVEL 2, SECTION OF LONGERON 29L FROM STA 157 TO 228 WAS REPLACED PER SRM 51-41-02 AND 51-41-05. (LP #0917473)

Part: LONGERON — WORN (RT COWLING) · airframe 51,743 hrs · 35,574 cycles

WEAR AT FRAME AND SKIN AT RT ENGINE UPPER COWLING AT HINGE AREA. NRC 209: LONGERONS WERE REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G AND SKIN WAS REPAIRED PER CV19-00214, ER/A 574759-14 REV. ORIGINAL. ASSOCIATED ER/A 17-574759 ADDED FOR AC 9509. (LP #0916826)

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 51,743 hrs · 35,574 cycles

CRACKED AND WORN COCKPIT FLOOR PANEL 211LF. NRC 00508: CRACK ON FLOOR PANEL 211LF WAS REPAIRED PER SRM 53-00-00-2R AND WEAR ON SAME FLOOR PANEL WAS BLENDED OUT AND MEASURED (UT). WAS FOUND TO BE WITHIN LIMITS PER SRM 51-10-02-0G PAR 8(F) AND DWG #9957802 REV AJ. EQUIPMENT PANAMETRICS 38 DL PLUS EXP DATE 22FEB19 S/N 171455902 TRANSDUCER V260-RM S/N 1090377. (LP #0916044)

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 51,743 hrs · 35,574 cycles

CRACK AT COCKPIT FLOOR PANEL 211PF. (CPIL). NRC 00366: COCKPIT FLOOR PANEL 211PF WAS REPAIRED PER SRM 53-00-00-2R. (LP #0916071)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACKED DOOR JAMB WEB STA Y=207 LONG 11L AT PAX CABIN LT SIDE. NRC 00259: DOOR JAMB WEB STA Y=207 LONG 11L WAS REPAIRED PER SRM 53-10-15-2R-1. (LP #0916241)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON PAX CABIN SEAT TRACK FORM STA=200 TO STA=222 AT X=22 (CPAX). NRC 00441: CORROSION LEVEL 2, SEAT TRACK FROM STA=200 TO STA=222 AT X=22 WAS REPLACED PER SRM 51-41-01-0G. (UT) WAS ACCOMPLISHED ON PAX CABIN SEAT TRACK FORM STA=200 TO STA=222 AT X=22 PER NDT SPM 04-00-07 PAR 5 FIG 3 (SHEET 1 AND 2) AND FOUND TO BE OUT OF LIMITS PER SRM 53-20-52 FIG 101. TOOLS USED: 38 DL PLUS S/N: 151215011 EXP. 16NOV19 TRANSDUCER V260-RM S/N: 1087464. (LP #0916218)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

DELAMINATION AT FLOOR PANELS #222CF, 222UF, AND 222GF. (CAB. PAX). NRC 00465: FLOOR PANEL #222CF, 222UF, AND 222GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0916220)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

DELAMINATED FLOOR PANEL #223FF. (CAB-PAX). NRC 00471: FLOOR PANEL #223FF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0916225)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

DELAMINATED FLOOR PANEL #221AF (W-1). NRC 00460: FLOOR PANEL #211AF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0915163)

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 51,743 hrs · 35,574 cycles

DELAMINATED FLOOR PANEL #211ANF. COCKPIT (CPIL). NRC 00472: FLOOR PANEL #211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0916213)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON PAX CABIN SEAT TRACK FORM STA=200 TO STA=206 AT X=-22 (CPAX). NRC 0442: CORROSION LEVEL 2, SEAT TRACK WAS REPLACED STA=200 TO STA=256 AT X=-22 (CPAX) PER SRM 51-41-01 AND 51-41-05. (LP #0914402)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK AT LT CUSP WEB LOWER SURFACE BETWEEN STA 218/223 AND X 44/ X 46. (CPAX). NRC 00523: CRACK AT LT CUSP WEB LOWER SURFACE BETWEEN STA 218/223 AND X 44/ X 46 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 222. (LP #0913878)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACKED INTERCOSTAL BTW FLOORBEAMS STA 1002-1022 AND X=0 AT PAX CAB. (CPAX). NRC 00387: INTERCOSTAL BTW FLOORBEAMS STA 1002-1022 AND X=0 AT PAX CAB WAS REPAIRED PER SRM 51-70-11-2R REPAIR 1.(ET) HFEC INSPECTION WAS PERFORMED ON INTERCOSTAL BTW FLOORBEAMS STA 1002-1022 AND X=0 AT PAX CAB. (CPAX) ON CUT OUT. NO CRACKS WERE FOUND. PER NDT SPM PART 6 06-10-01.001. (EQ. C/N 1601. EXP. 15MAR19). (LP #0914785)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON LT NLG DOOR JAMB BEAM STA Y=40. (NLG). NRC 00156: LT NLG DOOR JAMB BEAM STA Y=40 WAS REPAIRED PER SRM 53-10-14-2R-2 REP. 2. (ET)(HFEC) WAS ACCOMPLISHED ON LT NLG DOOR JAMB BEAM STA Y=40. (NLG) AND CRACK WAS DIMENSIONED WITH 1.375" LENGTH PER NDTSPM 06-10-01.001 EQUIP. (600 N/C 1601 EXP. 15MAR19). (ET)(HFEC) WAS ACCOMPLISHED ON LT NLG DOOR JAMB BEAM STA Y=40. (NLG) AFTER TRIMMED OUT AND NO CRACK WERE FOUND PER SRM 53-10-14-2R-2 REP.2 FLAG NOTE A.(4) AND NDTSPM 06-10-01.001 EQUIP. (600 N/C 1601 EXP. 15MAR19). (LP #0914769)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RT CUSP WEB BTW STA 794-813 AT PAX CABIN (CPAX). NRC 00502: MEMBRANE WAS REPAIRED PER SRM 53-00-55-2R-4 FIGURE 207 TABLE 2. (LP #0914399)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON CABIN FLOOR SUPPORTS 2 EA STA Y=150 BTW X=-33 AND X=-60. (CPIL). NRC 00488: CORROSION LEVEL 2, FLOOR SUPPORTS 2 EA STA Y=150 BTW X=-33 AND X=-60 WERE REPLACED PER SRM 51-41-02-0G. (LP #0914902)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON PAX CABIN FLOOR SUPPORT FROM X=38 TO X=16 AT STA=197 (CPAX). NRC 00438: CORROSION LEVEL 2, FLOOR SUPPORT FROM X=38 TO X=16 AT STA=197 (CPAX) WAS REPLACED PER SRM 53-10-51-0I-2 FIG. 1. (LP #0910994)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON PAX CABIN FLOOR SUPPORT FROM STA=197 TO STA=160 AT X=56 (CPAX). NRC 00440: CORROSION LEVEL 2, PAX CABIN FLOOR SUPPORT FROM STA=197 TO STA=160 AT X=56 (CPAX) WAS REPLACED PER SRM 51-30-07-0G. (LP #0912313)

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

PUNCTURE AT CUSP WEB BEHIND FITTING BWTEEN STA 197/160 LT SIDE X=56 IN REF NRC 00440. NRC 00529: PUNCTURE WAS REPAIRED PER SRM 53-00-00-2R. (LP #0911012)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PANELS #520CT AND 620CT. NRC 428: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-22-01-01 ITEM 065. (LP #0910383)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON RT CUSP WEBS UPPER/LOWER SURFACE BTW STA 918-925 AND X=-54.5 TO X=-60PER NRC 00321. NRC 00518: CORROSION LEVEL 2, RT CUSP WEB BTW STA 918-925 AND X=-54.5 TO X=-60. WAS REPAIRED PER SRM 53-00-55-2R-4.FIG. 216. (ET)(HFEC) WAS ACCOMPLISHED ON RT CUSP WEB SURFACE BTW STA 918-925 AND X=-54.5 TO X=-60, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM PART 6, 06-10-01.001 (LP #0907816)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RT CUSP WEB BTW STA 720-725 AT PAX CABIN (CPAX). NRC 00503: RT CUSP WEB BTW STA 720-725 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R FIG 216. (ET) HFEC INSPECTION OK, NO CRACKS ON RT CUSP WEB BTW STA 720-725 AT PAX CABIN ON TRIM OUT PER NDT SPM 06-10-01.001. (LP #0907525)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RT CUSP WEB BTW STA 940-946 AT PAX CABIN (CPAX). NRC 00501: RT CUSP WEB BTW STA 940-946 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 215. (ET) HFEC INSPECTION OK, NO CRACKS ON RT CUSP WEB BTW STA 940-946 AT PAX CABIN ON TRIM OUT PER NDT SPM 06-10-01.001. (LP #0906910)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RING PAN (FWD LOWER CORNER) STA Y=618 AND Y=637 AT PAX CABIN LT SIDE. NRC 00253: RING PAN (FWD LOWER CORNER) STA Y=618 AND Y=637 AT PAX CABIN LT SIDE WAS REPAIRED PER SRM 56-20-02 REPAIR 1. (LP #0905900)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RING PAN (AFT UPPER CORNER) STA Y=832, Y=851, AND Y=870 AT PAX CABIN LT SIDE. NRC 00251: RING PAN (AFT UPPER CORNER) STA Y=832, Y=851, AND Y=870 AT PAX CABIN LT SIDE WAS REPAIRED PER SRM 56-20-02 REPAIR 1. (LP #0906907)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RING PAN (AFT LOWER CORNER) STA Y=908 AT PAX CABIN LT SIDE. NRC 00252: RING PAN (AFT LOWER CORNER) STA Y=908 AT PAX CABIN LT SIDE WAS REPAIRED PER SRM 56-20-02 REPAIR 1. (LP #0905903)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RING PAN (FWD UPPER CORNER) STA Y=757 AT PAX CABIN LT SIDE. NRC 00254: RING PAN (FWD UPPER CORNER) STA Y=757 AT PAX CABIN LT SIDE WAS REPAIRED PER SRM 56-20-02 REPAIR 1. (LP #0905883)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,743 hrs · 35,574 cycles

CRACK ON RING PAN (FWD UPPER CORNER) STA Y=738 AND (AFT UPPER CORNER) STA Y=832 AT PAX CABIN RT SIDE. NRC 00258: RING PAN (FWD UPPER CORNER) STA Y=738 AND (AFT UPPER CORNER) STA Y=832 AT PAX CABIN RT SIDE WAS REPAIRED PER B717-200 SRM 56-20-02 REPAIR 1. (LP #0905806)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,743 hrs · 35,574 cycles

CORROSION ON FLOOR SUPPORT UPPER/LOWER SURFACE BTW STA 1022-1053 AND X=-44.5 (RT) AT AFT WET AREA (AMDS 5300-2010). (W2). NRC 00383: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA 1022-1053 AND X=-44.5 (RT) AT AFT WET AREA WAS REPLACED PER SRM 51-41-05-0G. (LP #0901513)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,660 hrs · 34,090 cycles

BOTH THE AFT OVERWING EXIT HATCH LOCATION LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-230 INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW AMM 33-51. OPS CHECKED NORMAL. THE AIRCRAFT RETURNED TO SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 46,947 hrs · 32,171 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN DIFFUSER COVER WAS MISSING. MAINTENANCE REPLACED THE COVER AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,374 hrs · 31,755 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,288 hrs · 31,689 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL OF THE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,129 hrs · 30,787 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING BY THE FIRST CLASS LAVATORY HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 43,653 hrs · 29,733 cycles

AFT CEILING EMER EXIT LIGHT BULB MISSING. INSTALLED BULB IAW AMM.

Part: BRACKET — BROKEN (CABIN) · airframe 43,653 hrs · 29,733 cycles

ROW 1 CEILING EMER EXIT LIGHT LENS CRACKED & MOUNT BRACKET BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BRACKET — CRACKED (EXIT SIGN) · airframe 43,653 hrs · 29,733 cycles

CEILING EMER EXIT SIGN AT OVERWING EXIT MOUNT BRACKET CRACKED. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,653 hrs · 29,733 cycles

TAIL COMPARTMENT AFT HANDRAIL EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 42,007 hrs · 28,615 cycles

OVERWING EMER EXIT SIGN LIGHT CRACKED. R & R SIGN IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,007 hrs · 28,615 cycles

LEFT WING NR 3 SLAT, MID TRACK CUT OUT LE EDGE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

CUSP WEB CRACKED AT BS 797, LBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 469, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

CUSP WEB CORRODED AT BS 525, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 545 - 560, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

CUSP WEB CORRODED BETWEEN BS 564 - 568, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 450 TO 460, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 488, RBL 56. R & R CUSP WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

L1 DOOR AFT INNER SKIN CORRODED. R & R SKIN IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 530 - 590, RBL 44. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 530 TO 590, LBL 44. R & R SEAT TRACK IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORMER CRACKED AT BS 674, LBL 37. REPAIRED FORMER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT INBD SEAT TRACK CORRODED BETWEEN BS 823 - 646. R & R SEAT TRACK IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORMER CRACKED AT BS 696, LBL 27. REPAIRED FORMER IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT OTBD SEAT TRACK CORRODED BETWEEN BS 590 - 646. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT OTBD SEAT TRACK CORRODED BETWEEN BS 900 - 1023. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

RIGHT OTBD SEAT TRACK CORRODED, BETWEEN BS 1023 TO 900. R & R SEAT TRACK SECTION IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT OTBD SEAT TRACK CORRODED, BETWEEN BS 823 - 900. R & R SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

AFT CARGO FWD BULKHEAD HORIZONTAL PANEL SUPPORT INTERCOSTAL CRACKED AT BS 815. R & R INTERCOSTAL IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

AFT CARGO FORMER CORRODED AT BS 954, BETWEEN LONGERON 30R - 29R. REPAIRED FORMER IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT WW DOOR, LOWER FWD END CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORMER CORRODED AT BS 946, BETWEEN LONGERON 30R - 29R. REPAIRED FORMER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

RIGHT WING TO BODY, INBD SIDE OF THE MOST INBD FLAP TRACK, CARRIAGE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

RIGHT WW DOOR, LOWER FWD END CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 42,007 hrs · 28,615 cycles

LEFT WING FIXED LE OTBD SIDE OF NR 3 SLAT TRACK ANGLE CRACKED. REPAIRED ANGLE IAW SRM & DWG.

Part: FAIRING — CRACKED (LT HORIZ STAB) · airframe 42,007 hrs · 28,615 cycles

LEFT HORIZONTAL STABILIZER, UPPER BANANA FAIRING SKIN, CRACKED AT LOWER FWD EDGE. REPAIRED FAIRING IAW EA.

Part: STRAP — CRACKED (SLAT TRACK) · airframe 42,007 hrs · 28,615 cycles

LEFT WING FIXED LE OTBD SIDE OF NR 3 SLAT TRACK DOUBLER STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT WW FWD DOOR CUTOUT INBD FITTING CRACKED. R & R FITTING IAW DWG & SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LONGERON CORRODED BETWEEN BS 908 - 927, 29L. R & R LONGERON IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

AFT CARGO BILGE, FORMER CORRODED AT BS 927, BETWEEN LONGERON 29R TO 28L. R & R FORMER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 150 - 180, LBL 0. REPAIRED SUPPORT IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORMER CRACKED AT BS 674, RBL 631. REPAIRED FORMER IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

STRINGER CLIP CORRODED AT BS 1053, LONGERON 29L. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

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

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

WING TO BODY INTERNAL FORMER CRACKED AT BS 696, RBL 24. R & R FORMER IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORMER CORRODED AT BS 1002, BETWEEN LONGERON 29L - 29R. R & R FORMER IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

INTERCOSTAL CORRODED, BETWEEN BS 1022 - 1037, LONGERON 30R. REPAIRED INTERCOSTAL IAW EA.

Part: STRAP — CRACKED (RT WING) · airframe 42,007 hrs · 28,615 cycles

RIGHT WING LE INBD FAIRING PANEL ATTACH STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORWARD WET AREA PARTITION MOUNT FITTING, CORRODED AT BS 157, RBL 51. R & R FITTING IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

AFT CARGO FRAME CORRODED AT BS 1037, BETWEEN LONGERON 30R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FRAME CORRODED AT BS 1022, BETWEEN LONGERON 29L - 29R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED AT BS 168, 18L. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED AT BS 180, BL 0. REPAIRED SUPPORT IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FORWARD PARTITION FLOOR MOUNT CORRODED AT BS 157, RBL 11. R & R FITTING IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

SHEAR TIE CORRODED AT BS 1022, BETWEEN LONGERON 29L - 29R. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 150 - 180, RBL 0. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED AT BS 180, BETWEEN RBL 0 - RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED AT BS 218, BL 0. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

MAIN CABIN FLOORBOARD SUPPORT CORRODED AT BS 237, BL 0. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 140 - 180, RBL 0. R & R SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

R1 DOOR WEB CORRODED AT BS 187, RBL 7. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FLOORBOARD SUPPORT CORRODED AT BS 1701, RBL 0. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 42,007 hrs · 28,615 cycles

R1 DOOR FWD GIRT BAR FITTING CORRODED, BETWEEN BS 148 - 190, BL 0. R & R FITTING IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

AFT CARGO COMPARTMENT DOOR JAMB LOWER PANE CORRODED. REPAIRED JAMB IAW SRM.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

R1 DOOR PANEL SUPPORT CORRODED, BETWEEN BS 160 - 190, RBL 0. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

FRAME CRACKED AT BS 715, RT SIDE. R & R FRAME IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

RIGHT CUSP WEB CRACKED, BETWEEN BS 655 - 715. REPAIRED CUSP WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

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

Part: STRAP — CRACKED (LT WING) · airframe 42,007 hrs · 28,615 cycles

LEFT WING LE INBD END FAIRING STRAP TOP SIDE CRACKED. R & R STRAP IAW SRM & DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LONGERON CORRODED AT BS 954, LONGERON 30R. R & R LONGERON IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT SIDE FRAME CRACKED AT BS 715. R & R FRAME IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,007 hrs · 28,615 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 655 - 715. R & R CUSP WEB IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,673 hrs · 29,743 cycles

FRAME CRACKED AT BS 715 RT. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,673 hrs · 29,743 cycles

FRAME CRACKED AT BS 674 RT SIDE. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,673 hrs · 29,743 cycles

CABIN FRAME CRACKED AT BS 715 LT SIDE. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,673 hrs · 29,743 cycles

FRAME CRACKED AT BS 696 RT. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,007 hrs · 28,615 cycles

LEFT WING NR 3 SLAT MID TRACK CUT OUT LE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 43,059 hrs · 29,325 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,165 hrs · 28,721 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACKS INOPERATIVE. R & R BATTERY PACK IAW TC.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,165 hrs · 28,721 cycles

FORWARD EMERGENCY EXIT LIGHT BATTERY PACKS INOPERATIVE. R & R BATTERY PACK IAW TC.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 40,754 hrs · 27,819 cycles

VERTICAL STABILIZER RAM AIR INLET FAIRING CRACKED LT HAND & RT HAND AT PREVIOUS WELD REPAIRS. REPAIRED FAIRING IAW SRM.

Part: RETAINER — DIRTY (R1 DOOR) · airframe 39,485 hrs · 27,018 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STICKING IN FLOOR FITTING. CLEANED GALLEY DOOR GIRT BAR RETAINER AS NEEDED.

Part: RIB — CRACKED (LE SLAT) · airframe 38,724 hrs · 26,572 cycles

RIGHT WING NR 5 SLAT O/B RIB CRACKED AT FASTENER HOLE. REMOVED AND REPLACED RIB IAW SRM.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 38,724 hrs · 26,572 cycles

RIGHT ATTACH ANGLE FOR VERTICAL STABILIZER TO FUSELAGE SKIN FWD FAIRING CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 38,724 hrs · 26,572 cycles

DORSAL FIN L/E PANEL CRACKED ON LEFT SIDE OF PANEL. REMOVED AND REPLACED PANEL IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 38,724 hrs · 26,572 cycles

L-1 DOOR INTERNAL, NR 2 BEAM CRACKED AT THE AFT END LOWER SURFACE. REPAIRED BRACKET IAW SRM.

Part: DOOR SEAL — MISSING (EMERGENCY EXIT) · airframe 38,724 hrs · 26,572 cycles

LEFT AFT OVERWING EMERGENCY EXIT DOOR AFT SIDE SEAL ON DOOR MISSING. INSTALLED SEAL IAW AMM.

Part: LENS — DAMAGED (CABIN) · airframe 37,699 hrs · 25,921 cycles

RIGHT EEPLS DAMAGED AT ROW 1. REMOVED AND REPLACED LENS IAW AMM.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 37,506 hrs · 25,794 cycles

AFT TAILCONE SLIDE CONTAINER SIGHT GLASS BROKEN. REMOVED AND REPLACED SLIDE PER AMM.

Part: VALVE — STUCK (FUEL SYSTEM) · airframe 51,195 hrs · 30,463 cycles

CROSS FEED VALVE COB POPPED WITH CROSS FEEDING. CROSS FEED VALVE STUCK OPEN. REMOVED AND REPLACED CROSS FEED VALVE PER MM.

Part: WIRE — BROKEN (COCKPIT)

F/O'S CHART LIGHT SPARKING WHEN PUSHED AGAINST YOKE. REPAIRED BROKEN WIRE - OPS CHECKED NORMAL. REF SWPM 20-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOTH OVERWING EMERGENCY EVACUATION LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY POWER SUPPLY IAW B717 AMM 33-51. OPERATIONAL TEST PASSED.

Part: LIGHT — IMPROPER PART (CABIN)

AFT ACCESSORY COMPARTMENT EMERGENCY SLIDE OVERHEAD FLOOD LIGHT HAS 1 EACH DIM BULB. REPLACED BULB WITH CORRECT TYPE BULB AS REQUIRED OPS CHECK OF EMERGENCY LIGHT SYSTEM NORMAL IAW AMM 33-51-01.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO LOWER FUSELAGE DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB SPLICE REPAIR PER B717 SRM 53-20-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CARGO FLOOR SUPPORT, STA 370 TO 427, LONG R29, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-10-04 AND 51-41-09.

Part: SKIN — DAMAGED (TE FLAP)

LT WING INBOARD FLAP LOWER PANEL UPPER SURFACE SKIN, DAMAGED. ACCOMPLISHED FLAP LOWER PANEL UPPER SURFACE SKIN DOUBLER REPAIR PER B717 SRM 51-70-13 AND 51-41-01.

Part: HOLDER — BROKEN (GIRT BAR)

R1 DOOR GIRT BAR HOLDER BROKEN. REMOVED AND REPLACED R1 DOOR GIRT BAR HOLDER REF AMM 52-42-02-1.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ENGINE NACELLE EMERGENCY LIGHTS STAY ON ALL OF THE TIME. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY ASSY IAW MM 33-51.

Part: SKIN — CORRODED (FUSELAGE)

LOWER FUSELAGE SKIN, STA 851, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-02144IR. SEE NR 3705 AND 3733.

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 AIRTRAN TASK CARD 17-5310-2975.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: LONGERON — CRACKED (FUSELAGE)

FUSELAGE LONGERON, STA 1153, LONG R2, CRACKED. ACCOMPLISHED FUSELAGE LONGERON SPLICE REPAIR PER B717 SRM 53-00-05. SEE NR 3716.

Part: STRAP — CORRODED (FUSELAGE)

RIGHT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 3673 AND 3729.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, RBL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5920.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5900.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 275, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5906.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 170, RBL 8 TO RBL 48, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5902.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 235, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02157IR. SEE NR 5908.

Part: DOOR FRAME — CORRODED (CARGO BAY)

FWD CARGO DOOR JAMB PAN, STA 372 TO 425, CORROSION. ACCOMPLISHED CARGO DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 6 FIG 201. SEE NR 3634 AND 3728.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 1022 TO 1053, LBL 18, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-01. SEE NR 5926.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 255, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02155IR. SEE NR 5907 AND 5932.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 8 TO RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5911.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5912.

Part: STRAP — CORRODED (FUSELAGE)

LEFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 832, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 3675.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 8 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5910.

Part: STRAP — CORRODED (FUSELAGE)

RIGHT EXTERIOR WING TO BODY SUPPORT STRAP, STA 832, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 3674.

Part: RUB STRIP — CORRODED (RT WING)

RIGHT WING ACCESS PANEL 620CT RUB STRIP, CORROSION. ACCOMPLISHED WING ACCESS PANEL 620CT RUB STRIP REPLACEMENT REPAIR PER B717 SRM 51-41-02 AND B717 SRM 57-10-01. SEE NR 2674.

Part: GUSSET — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT DOUBLER GUSSET, STA 994, LONG L28R, CORROSION. ACCOMPLISHED CARGO COMPARTMENT DOUBLER GUSSET REPLACEMENT REPAIR PER B717 SRM 51-41-05 AND B717 SRM 51-41-01. SEE NR 3658.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-01. SEE NR 5895.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-01. SEE NR 5896.

Part: STRAP — CORRODED (FUSELAGE)

LEFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 3677.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, LBL 8 TO RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT REPAIR PER B717 SRM 51-41-02. SEE NR 5897.

Part: BATTERY PACK — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51.

Part: ENGINE — FAILED (NR 2)

DURING CLIMBOUT OF 14,500 HEARD A LOUD BANG. LOST NR 2 ENGINE. NORMAL DESCENT. RAN QRH. LANDING WEIGHT 102,400, MAX TGT 1148. REMOVED AND REPLACED NR 2 ENGINE ON TASK CARD 603 AS REQUIRED. LEAK AND OPS CHECKED GOOD. POWER ASSISTANCE TEST PASSED.

Part: WIRE — BROKEN (CABIN)

ROWS 27, 28, AND 29 EMERGENCY PATH LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT QUICK DISCONNECTS AT ROWS 27, 28, AND 29 IAW SWPM 20-31-00. OPS CHECK NORMAL IAW AMM 33-51-00.

Part: FRAME — CRACKED (FUSELAGE)

SMALL CRACK AFT FUSELAGE INTERNAL LT CANTED FRAME STA 1200.019. INSTALLED REPAIR 15" X 2" AS REQ 51-70-11 MATERIAL USED 7075.0 .063 HEAT TREATMENT TO 7075 T6 .063 AS PER SRM 51-32.01.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

GEAR DOOR OPEN ALERT ON CONFIG PAGE. LUBED GEAR DOORS, PERFORMED EMERGENCY GEAR EXTENSION AND SWUNG GEAR SEVERAL TIMES WHILE ON JACKS. SERVICED HYD'S, A/C OK FOR SERVICE REF AMM 32-00 AND 12-00.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE)

FLT OPERATING RT PACK ONLY CRUISING AT40 HAD PRESSURE THUMP FOLLOWED BY CABIN PRESS CLIMB AT 1300 FPM. INITIATED EMERGENCY DESCENT, INITIAL CLEARANCE TO 11K. CABIN PRESS ROSE FROM 6K-7-7K DURING DESCENT. CABIN INFLO LVL 2 ALERT WAS INTERMITTENT DURING REMAINDER OF FLT. PRESSURE STABILIZED AFTER DESCENT, NORMAL APPROACH AND LANDING. OUTFLOW VLV WAS FULL CLOSED THROUGHOUT THE LANDING WHEN IT WENT FULL OPEN CABIN PRESS WAS AT FIELD ELEV, NORMAL TAXI TO GATE. SECURED DUCT COUPLING OF GROUND AC AFTER CHECK VLV REF 21-00MM.

Part: FRAME — CRACKED (BS 1178)

AFT FUSELAGE COMPARTMENT CANTED FRAME 1178 AND LEFT HAND LONGERON 17, AREA HAS CRACK. CUT OUT DAMAGE ON CANTED FRAME STA 1178 LEFT SIDE L-17L TO 18L (2.5 X 1.375 INCHES) IAW B717 SRM 51-70-11 FIG 201. FABRICATED REPAIR ANGLE AND FILLER MATERIAL USED 7075. T6 .080 11 X 2.5 INCHES. PO 021701. HEAT TREATMENT TO T-6 IAW 98 PMS 247 OS 01 AS PER SRM 51-30-01.

Part: PAN — CRACKED (FUSELAGE)

REPAIR OF AFT FUSELAGE LEFT SIDE VENT BOX DRAIN PAN. STOP DRILL CRACK IAW B717 SRH 51-00-07. INSTALLED DOUBLER REPAIR AT AFT FUSELAGE LEFT SIDE VENT BOX IAW EO 17-5320-2022 MATERIAL USED 7075 T6 .040 LOT 7Y1DUJNV PO 83110438.

Part: SKIN — DAMAGED (R1 DOOR)

R-1 DOOR DOUBLER REPAIR. INSTALLED DOUBLER REPAIR AND FILLER REPAIR AT R-1 DOOR. MATERIAL USED 2024 T3 .063 SIZE 9 X 8.875 INCHES, PO 622084 2024 T3 .050 2 X 2 INCHES PO 022199 AS PER RES 06-0484.

Part: BONDING STRAP — DAMAGED (LT ELEVATOR OB)

PERMANENT REPAIR LEFT ELEVATOR OUTBOARD TRAILING EDGE STATIC WICK BONDING STRAP. BLENDED OUT AREA DAMAGE IAW B717 RES 06-0254. INSTALLED PERMANENT REPAIR AT LEFT ELEVATOR AFT O/B TRAILING EDGE STATIC WICK BONDING STRAP.