N936AT

Part: LANDING GEAR — MALFUNCTIONED · airframe 58,913 hrs · 43,121 cycles

LANDING GEAR DID NOT DEPLOY ALL RED INDICATIONS NO FAULT MESSAGES DISPLAYED. AFTER GO AROUND GEAR DEPLOYED NORMAL ON 2ND ATTEMPT. GEAR HANDLE FULL DOWN HYD PRESS NML, NML DOOR INDICATIONS NO FAULTS ON PSEU BITE IAW B717 FIM 32-60. (8154976)

Part: ACCESS PANEL — DAMAGED · airframe 58,465 hrs · 42,707 cycles

IN REF NRC 124 AFTER CLEAN ELONGATED HOLE FOUND ON FUEL ACCESS PLATE 520 JB. FUEL ACCESS PLATE 520JB WAS REPAIRED PER ER/A 628967-14AD (1183419)

Part: BATTERY — NO TEST (ZONE 200) · airframe 58,428 hrs · 42,672 cycles

SHIP 9563 AFT BULKHEAD EMERGENCY EXIT LIGHT FLICKERING. CORRECTIVE ACTION: REMOVED AND REPLACED EMERG BATT ASSY B5-260.PER B717 AMM 33-51 AND BATT PER B717B AMM 33-51 OPS CHK OK. (6671296)

Part: NONE — NONE (NONE) · airframe 58,383 hrs · 42,632 cycles

SHIP 9563 LOGPAGE CREATED TRACKING SECTION II INSPECTIONS TO ER/A 610356- 14AD. CORECTIVE ACTION: C/W ER/A 571712-14AD. (1037974)

Part: GENERATOR — FAILED (ZONE 400) · airframe 57,882 hrs · 42,162 cycles

ABORTED TAKE-OFF DUE TO A LEFT ENGINE GENERATOR FAILURE MESSAGE: REPLACED GROND RELAY AND AUX POWER RELAY. TEST GOOD.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 57,487 hrs · 41,806 cycles

THE EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE B5-235 EMERGENCY BATTERY POWER SUPPLY/CHARGER REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7237017)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 56,592 hrs · 41,020 cycles

MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN TAIL COMPARTMENT TO BE INOPERATIVE. DETERMINED THAT THE BATTERY PACK B5-116 WAS BAD. BATTERY PACK WAS REPLACED REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6585244)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,913 hrs · 38,694 cycles

CRACK ON UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE. SUMMARY OF NRC 00066; UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE WAS REPAIRED PER B717-200 SRM 54-00-00-2R PROCEDURE 1 REPAIR 1. (LP #2933305)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,774 hrs · 38,577 cycles

THE CABIN OVERWING EMERGENCY EXIT LIGHTS B5-121/P9 AND B5-121/P11 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #4711630)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,703 hrs · 38,526 cycles

FOUND ONE CRACK INDICATION ON RH VERTICAL STAB WHILE PERFORMING AA5530-01048 AND AD 2018-10-08 (MARKED). ONE CRACK INDICATION RH VERTICAL STAB IN SPAR AND WHILE REINSPECTING AREA IN QUESTION WHILE PERFORMING AA5530-01048 AND AD2018-10-08. COMPLIED WITH ER/A 610356-14AD REV ORIGINAL SECTION 1. TIME LIMITED REPAIR. RII COMPLIED WITH. ASSOCIATED ER/A 14-610356 ADDED FOR AC 9563. (LP #4711600)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,703 hrs · 38,526 cycles

R/H VERTICAL STAB, WHILE ACCOMPLISHING INSPECTION PER WORK CARD 5530-0148-02 FAA AD 2018, FOUND A CRACK INDICATION TO ONE HOLE OF THE FRONT SPAR CAP. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 0. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 1. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 2. COMPLIED WITH PRI 610356-14AD REV 3. COMPLIED WITH PRI 610356-14AD REV 4. FINALE ERA 610356-14AD REV O, COMPLETE AND MATCHES PRI 610356-14AD REV 0,1,2,3,4. ASSOCIATED ER/A 14-610356 ADDED FOR AC 9563. (LP #2861584)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,709 hrs · 38,531 cycles

WHILE PERFORMING AA 5530-01048 AND AD 2018-10-08, FOUND 3 CRACK INDICATIONS ON LT. LOWER FIXED LEADING EDGE SKIN (MARKED). COMPLIED WITH ER/A 610352-14AD REV ORIGINAL PRI REV 0. COMPLIED WITH PRI 610352-14AD PRI REV 1, ER/A 610352-14 REV. ORIGINAL MATCHES PRI 610352-14AD REVISIONS 0 & 1. C/W ER/A 610352-14 REV. ORIGINAL. (LP #2861437)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,709 hrs · 38,531 cycles

FOUR CRACK INDICATIONS ON LH VERTICAL STAB WHILE PERFORMING AA5530- 01048 AND AD 2018-10-08 (MARKED). REINSPECTED AREA FOUND 3 CRACK INDICATIONS IN LOWER SPAR CAP WHILE PERFORMING AA5530-01048 AND AD 2018-10-08. THE ABOVE 3 CRACK INDICATIONS ARE ON LT LOWER SKIN FIXED L/E ONLY. COMPLIED WITH ER/A 610352-14 REV. ORIGINAL, SECTION1: PERMANENT REPAIR. (LP #4733899)

Part: NONE — NONE · airframe 51,859 hrs · 36,911 cycles

THE J HOOK FOR THE GIRT BAR TO SLIDE WAS DISCONNCTED AT DOOR 1R. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RESECURED GIRT BAR PER B717 AMM 25-61 R1 DOOR. (LP #9063162)

Part: NONE — NONE · airframe 50,390 hrs · 35,590 cycles

NICK ON FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 (CCD). SUMMARY OF NRC 00017: FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 WAS REPAIRED PER B717 SRM 53-20-15-2R REP. 6. (LP #2110946)

Part: NONE — NONE · corrosion level 2 · airframe 50,390 hrs · 35,590 cycles

CORROSION ON AFT CARGO DOOR JAMB LOWER AREA (CCT). SUMMARY OF NRC #00013: AFT CARGO DOOR JAMB LOWER AREA WAS REPAIRED PER B717 SRM 53-20-15-2R, REPAIR 7. (LP #2111475)

Part: NONE — NONE · airframe 50,390 hrs · 35,590 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN OUT OF LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01. (LP #2110434)

Part: NONE — NONE · airframe 50,222 hrs · 35,440 cycles

SHIP 9563 -DIV/INFLT SHUTDN- TO MSY DUE TO RIGHT ENGINE FIRE WARNING. CREW PULLED FIRE HANDLE AND DISCHARGED BOTH BOTTLES. CORRECTIVE ACTION: MAINTENANCE REPLACED NUMBER 1 AND 2 FIRE BOTTLES PER B717 AMM 26-21 AND REPLACED RIGHT ENGINE FDCU PER B717 AMM 26-11.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 49,434 hrs · 34,706 cycles

MAINTENANCE FOUND THAT THE B5235 EMERGENCY BATTERY PACK WAS DEAD. THE B5235 EMERGENCY BATTERY PACK WAS REPLACED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #7930220 )

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,146 hrs · 34,446 cycles

THE OVERWING EMERGENCY EVACUATION LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK B5-125 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7803975)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,770 hrs · 34,144 cycles

THE LOWER EXIT SIGNS AT DOORS 1L AND 1R NOT WORKING. MAINTENANCE FOUND THE BATTERY 35-118 TO BE INOPERATIVE. THE BATTERY WAS REPLACED, PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.

Part: SKIN — NICKED (LT WING) · airframe 46,096 hrs · 31,946 cycles

NICKS AT LT WING LOWER SKIN, LOWER SURFACE AROUND FUEL ACCESS PLATES, #520EB, 520LB, AND 520MB. NRC 00603: NICKS AROUND FUEL ACCESS PLATES #520EB AND 520LB WERE REPAIRED PER ETI- 17-19-105 REV. 1 AND ER/A 579383-14 REV. ORIG SECTION I. NICK ON FUEL ACCESS PLATE #520MB WAS BLENDED OUT PER SRM 57-00-00- 1A FIG. 103 AND MEASURED. (LP #1146461)

Part: PIN — MISSING (TAILCONE) · airframe 46,096 hrs · 31,946 cycles

DURING INSTALLATION OF TAILCONE SLIDE, PIN P/N MS20392-2C9 WAS NOT FOUND IN REFERENCE TO 5352-4002 STEP 6 ( CPAX). NRC 0721: NEW PIN FOR THE TAILCONE SLIDE WAS INSTALLED PER AMM 25-61-02-400-801 STEP D 1 (I). (LP #1146033)

Part: SKIN — DENTED (AILERON TAB) · airframe 46,103 hrs · 31,952 cycles

INITIAL INSPECTION, DENT ON AILERON CONTROL TAB UPPER FACE AT RT WING. AILERON CONTROL TAB RT P/N 5910047-410 S/N 518 WAS REMOVED PER AMM 27-10-02 AILERON CONTROL TAB P/N 5910047-502 S/N NSN1 WAS INSTALLED PER AMM 27-10-02. TAB, AILERON, C OFF 09-5750-9-0002 05078 ON 09-5750-9-0002 99001. (LP1146079)

Part: SKIN — NICKED (TE FLAP VANE) · airframe 46,096 hrs · 31,946 cycles

NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING (AD). NRC 00236: NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING WERE REPAIRED PER SRM 57-53-01-2R-1 AND 51-70-02-0G. (LP #1145757)

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, 51-41-02-0G, AND 51-41-05-0G E. (LP #1143799)

Part: STIFFENER — CORRODED (BS 1053) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00322: CORROSION LEVEL 2, STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9915561 REV. CG. (LP #1143074)

Part: RETAINER — CRACKED (WINDOW FRAME) · airframe 46,092 hrs · 31,944 cycles

CRACK AT AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS FOUND (CPIL). NRC 00654: AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R. (LP #1142006)

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, 51-41-02-0G, AND 51-41-05-0G E. (LP #1143060)

Part: FRAME — CORRODED (BS 1002) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT AFT CARGO COMPARTMENT. NRC 00267: CORROSION LEVEL 2, FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, 53-20-07-2R REPAIR 3 PAR 4 TABLE 201, AND 53-20-07-0I-3. (LP #1143050)

Part: INTERCOSTAL — CORRODED (BS 1037-) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION ON INTERCOSTAL STA Y=1037 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00315: CORROSION LEVEL 2, INTERCOSTAL WAS REPLACED PER B717-200 SRM 53-20-51-0I 7 ITEM 12 AND 51-41-02-0G. (LP #1142061)

Part: SKIN — CRACKED (BS 1087) · airframe 46,092 hrs · 31,944 cycles

CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH (FUS). NRC 597: CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.

Part: SKIN — DAMAGED (BS 832) · airframe 46,092 hrs · 31,944 cycles

DAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPAIR IAW SRM 53-02-01- 2R FIG. 202 (SHEET 13).

Part: SKIN — CRACKED (BS 1076) · airframe 46,092 hrs · 31,944 cycles

CRACK AT FUSELAGE SKIN BS 1076 BETWEEN LONGERON 13 & 14R. THE SKIN WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.

Part: LONGERON — CORRODED (BS 1022) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

LONGERON 30 CORROED BS 1022. THE LONGERON WAS REPLACED IAW SRM 53-20-05 PROCEDURE 3 ITEM 9, 51- 41-02-OG, AND 51-41-05-OG.

Part: LONGERON — CORRODED (BS 1002-1037) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION BTW LONGERON 25L, BS 1002 - 1037 AT CARGO COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2 AND SRM 51-40-08-0G.

Part: FRAME ANGLE — CORRODED (BS 1022) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLEATED FRAME CLIP ON STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00302: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9912243 REV. JS. (LP #1139466)

Part: FRAME — CRACKED (BS 696) · airframe 46,092 hrs · 31,944 cycles

AD 2013-19-22 CRACK ON FRAME STA 696 RH SIDE. NRC 00371: FRAME STA 696 RH SIDE WAS REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03B. (LP #1137896)

Part: SKIN — CORRODED (BS 851) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30. CORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30 WAS REPAIRED PER B-717-200 SRM 53-20-70-2R-1 FIG .201.

Part: FRAME — CRACKED (BS 696) · airframe 46,092 hrs · 31,944 cycles

CRACK ON FRAME BS 696 LH SIDE.FRAME REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03A.

Part: FRAME ANGLE — CORRODED (BS 1002) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FRAME CLIP STA Y=1002 BTW LONG 26LH-25LH AT AFT CARGO COMPARTMENT (C2). NRC 0711: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1002 BTW LONG 26LH-25LH WAS REPAIRED PER B717-200 SRM 51-41-02-0G, 53-00-06-2R REPAIR 2 PAR. 4. A. FIG. 201, AND DWG #9957739 REV. DT. (LP #1137991)

Part: CARGO TRACK — DAMAGED (BS 954) · airframe 46,092 hrs · 31,944 cycles

ELONGATED HOLES ON RH TIE TRACK STA 954 AT AFT CARGO COMPARTMENT. NRC 00277: TIE TRACK RH ON STA 895 TO STA 954 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-51-0I-7 IDENTIFICATION 7, ITEM 8, FIG.2 (SHEET 2), PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G.

Part: SKIN — CORRODED (BS 708) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON UPPER SKIN STA Y=708 X=-24 AND Z-10 AT WING BOX. NRC 00482: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.

Part: DOUBLER — CORRODED (BS 767-748) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON DOUBLER FROM STA Y=737 TO Y=748 BTW X=44 TO X=60 AND Z-10 AT WING BOX. NRC 00486: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL.

Part: SKIN — CORRODED (BS 715-737) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON UPPER SKIN FROM STA Y=715 TO Y=737 BTW X=44 TO X=60 AND Z=-10 AT WING BOX. NRC 00481: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113.

Part: SKIN — CORRODED (BS 717) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON UPPER SKIN STA Y=717 X=-19 AND Z-10 AT WING BOX. NRC 00483: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.

Part: FRAME — CORRODED (BS 1037) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION ON FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT. NRC 00296: CORROSION LEVEL 2, FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R.

Part: BARRIER — CORRODED (BS 715-767) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON VAPOR BARRIER STA X=22 AND STA Y=715 TO STA Y=737 AT PAX CAB (CPAX). NRC 00534: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I.

Part: LONGERON — CORRODED (BS 984-1010) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT IN REFERENCE NRC 00284. (C2). NRC 683: CORROSION LEVEL 2, SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 53-00-05-2R-2 REPAIR 2 FIG. 201. (LP #1135049)

Part: FRAME — CORRODED (BS 889) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FRAME STA 889 LONG 30 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A FIG 103. CORROSION LEVEL 2, FRAME AT STA 889 LONG 30 WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIGURE 201, SHEET 1.

Part: BARRIER — CORRODED (BS 715) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON VAPOR BARRIER LH SIDE STA X=22 AND STA Y=715 AT PAX CAB (CPAX). NRC 00535: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113 ADDED FOR AC 9563. (LP #1136277)

Part: FRAME ANGLE — CORRODED (BS 927) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION FRAME CLIP STA Y=927 BTW LONG 24LH TO LONG 26RH AT AFT CARGO COMPARTMENT. NRC 00192: CORROSION LEVEL 2, FRAME CLIP AT STA Y=927 BTW LONG 26LH AND 26RH WAS REPLACED PER B717-200 DWG #9915524 REV. P, PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G.

Part: SKIN — DAMAGED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14R. FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14RH (FUS) WAS REPAIRED PER ERA/A 579005-14 REV. ORIGINAL, SECTION I PERMANENT REPAIR AND ETI-17-19-077 REV. 3.

Part: BARRIER — CORRODED (BS 663-715) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON VAPOR BARRIER STA X=54 AND STA Y=663 TO STA Y=715 AT PAX CABIN. CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579177-14 REV. ORIGINAL: SECTION I.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 46,092 hrs · 31,944 cycles

CRACK ON PAN BTW BEAM 1 TO BEAM 2 AND STA 994 AT AFT CARGO DOOR (C2). NRC 00439: AREA WAS REPAIRED PER ER/A 579043-14 REV. ORIG. AND ETI-17-19-074, REV 2. (LP #1133339)

Part: BEAM — CRACKED · airframe 46,092 hrs · 31,944 cycles

CRACKED LH NOSE LANDING GEAR JAMB BEAM AROUND STA: Y-47 (FYT). NRC 00569: LH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER B-717-200 SRM 53-10-14-2R FIG. 201 REP. 2.

Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 46,092 hrs · 31,944 cycles

CRACKED RH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47. RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER ER/A 495600-14MA REV C.

Part: DOUBLER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION DOUBLER ON LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT. NR 00325: CORROSION LEVEL 2, EXFOLATION CORROSION ON DOUBLER AT LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT WAS ATTENDED PER ER/A 578898-14 REV. ORIGINAL. ASSOCIATED ER/A 14-578898 ADDED FOR AC 9563. (LP #1132702)

Part: FRAME ANGLE — CORRODED (BS 1037) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION ON FRAME CLIP STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT. NRC 0316: CORROSION LEVEL 2, FRAME CLIP FROM STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9958238-85 REV. CM. (LP #1132202)

Part: FINGER DOUBLER — CORRODED (BS 943-1044) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FINGER DOUBLER FROM STA Y=943 TO 960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFT CARGO COMPARTMENT WAS FOUND OUT OF LIMITS. NRC 00691: CORROSION LEVEL 2, SECTION OF FINGER DOUBLERS STA Y=943 TO Y=960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFT CARGO COMPARTMENT WAS REPLACED PER B 717-200 SRM 53-03-01-2R-1 FIG 212 AND 51-41-02-0G. (LP #1132777)

Part: INTERCOSTAL — CORRODED (BS 1032) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT. NRC 00317: CORROSION LEVEL 2, INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG #5936071 REV. W AND PER B717-200 SRM 51-41-02-0G. (LP #1132805)

Part: DOOR FRAME — CORRODED (BS 954-994) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT. NRC 00324: LOWER DOOR JAMB AND SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 AND 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #1131248)

Part: BEAM — CRACKED (BS 767) · airframe 46,092 hrs · 31,944 cycles

CRACK ON BEAM STA Y=737, X= 54 AND Z=-2 LH SIDE AT WING BOX. NRC 00467: FLOOR BEAM WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G .

Part: PAN — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 REASON FOR RE-WRITE WRONG MEASSUREMENT. (CCD). NRC 00679: CORROSION LEVEL 2, FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 WAS REPLACED PER B717-200 SRM 53-20-15-2R-6.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,103 hrs · 31,952 cycles

EXFOLATION ON SPLICE CLIP STA Y=898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO COMPARTMENT. NRC 00171: CORROSION LEVEL 2, SPLICE CLIP STA Y= 898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO WAS REPLACED PER SRM 53-20-01-0I AND 51-41-05-0G. (LP #1131371)

Part: DOUBLER — CORRODED (BS 1053) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON DOUBLER STA 1053 OVER PROJECTION STG 30 ON LOWER BULHEAD AREA AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-20-08-0I- 2 FIG. 1.

Part: REINFORCEMENT — CRACKED (WINDOW) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER AT FLIGHT COMPARTMENT (CPIL). NRC 00475: BRACKET LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #1130511)

Part: LONGERON — CORRODED (BS 1003) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT. NRC 0304: CORROSION LEVEL 2, DUE TO CORROSION OUT OF LIMITS LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1127877)

Part: FRAME ANGLE — CORRODED (BS 908) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXFOLATION ON FRAME CLIP STA Y=908 BTW LONGERON 26LH TO LONGERON 28RH BOTH FACES AT AFT CARGO COMPARTMENT. NRC 0174: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26LH TO LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-41-02-0G. (LP #1128065)

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON CLIP FRAME LONG 14RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00401: FRAME CLIP WAS REPLACED PER B717-200 SRM 51-41-05-0G.

Part: GUSSET — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON GUSSET PROJECTION LONGERON 7RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00397: GUSSET PROJECTION LONG 7RH STA 1022 AT AFT FACE OF BULKHEAD WAS REPAIRED PER ER/A 578999-14 REV.ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIATED ER/A 00-578999 ADDED FOR AC 9563.

Part: CUSP WEB — CRACKED (BS 653-655) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LH CUSP WEB BETWEEN STA 655/653 IN REF NRC 00647. (CPAX). NRC 00675: LH CUSP WEB BETWEEN STA 655/653 WAS REPLACED PER B717-200 SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G.

Part: FRAME — CRACKED (BS 1037) · airframe 46,092 hrs · 31,944 cycles

CRACK ON FRAME, LONG 17RH STA 1037 (CPAX). NRC 00404: FRAME, LONG 17RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1124857)

Part: CUSP WEB — CRACKED (BS 655) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER. (CPAX). NRC 00647: LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 211.

Part: GUSSET — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON GUSSET PROJECTION LONGERON 7LH STA 1022 (CPAX). NRC 00398: GUSSET PROJECTION LONG 7LH STA 1022 WAS REPAIRED PER ER/A 57899-14 REV. ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIATED ER/A 14-578999 ADDED FOR AC 9563. (LP #1124972)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXCESSIVE CORROSION ON FUEL ACCESS PLATE #520LB.(AI). NRC 00666: CORROSION LEVEL 2, CORROSION ON FUEL TANK ACCESS DOOR #520LB OF LH WING FUEL TANK WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND B717-200 SRM 57-10-01- 2R REPAIR 2 PAR. 5.; DIAMETER OF COUNTERSINK HOLES FOUND TO BE OUT OF LIMITS PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 C. (CONDITION III) TABLE 201 AND PAR.5 D. FUEL TANK ACCESS DOOR #520LB OF LEFT WING WAS REPLACED AND PART NUMBER WAS VERICATED PER B717-200 AIPC 57-23-01-01 ITEM 220. (LP #1124966)

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 6RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00396: SECTION OF LONGERON 6RH BTW STA 996 TO 1053 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1124449)

Part: CUSP WEB — CANNING (BS 889-908) · airframe 46,092 hrs · 31,944 cycles

OIL CANING ON CUSP WEB AT BTW STA 889/908 LH X= 44/60 (FUS). NRC 00361: CUSP WEB DAMAGED BTW STA 889 TO 908 LH, X =-44 TO X=-60, WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #1124292)

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 4LH STA 1022 (CPAX). NRC 00388: SECTION LONGERON 4 LH FROM STA. 1010 TO STA. 1053 WAS REPAIRED PER B-717-200 SRM 53-00-05-2R.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON F.O. LOWER OUTBOARD SEAT TRACK. NRC 00559: CORROSION LEVEL 2, SEAT TRACK WAS REPLACED PER B717-200 SRM 51-41-01-0G.

Part: FRAME — CRACKED (BS 1037) · airframe 46,092 hrs · 31,944 cycles

CRACK ON FRAME, LONG 17LH STA 1037 (CPAX). NRC 00402: FRAME STA 1037 AT LONG 17LH WAS REPAIRED B717-200 SRM 53-20-07-2R-4. (LP #1120245)

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON CLIP FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00398: FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9912243 REV. JS. (LP #1120252)

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON CLIP FRAME LONG 5LH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00393: FRAME CLIP LONG 5LH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #1117079)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

EXCESSIVE CORROSION ON FUEL ACCESS PLATES #520PB AND #520DT.(AI). NRC 00667: CORROSION ON FUEL TANK ACCESS DOORS #520DT AND 520PB OF LH WING WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND 57-10-01-2R REPAIR 2 PAR. 5. REMAINING THICKNESS WAS OUT OF LIMITS AND FUEL TANK ACCESS DOORS #520PB AND #520DT WERE REPLACED. PART NUMBER WAS VERIFIED PER B717-200 AIPC 57-23-01-01 ITEM 130J AND B717-200 AIPC 57-22-01-01 ITEM 15. (LP #1118096)

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 (CPAX). NRC 00432: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 WAS REMOVED PER B717-200 SRM 51-10- 04 PAR 26. REMAINING THICKNESS OF 0.003" IS OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG. FLOOR SUPPORT AT STA 200 FROM X=7 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1118247)

Part: FRAME — CRACKED (BS 832) · airframe 46,092 hrs · 31,944 cycles

CRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN (CPAX). NRC 00242: CRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 56-20-02 REPAIR 1. (LP #1118572)

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 3RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00394: SECTION OF LONGERON 3RH FROM STA 1010 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1115922)

Part: FLOORBEAM — CORRODED (BS 148) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FLOOR SUPPORT AT STA 148 FROM X=-31/-44 (CPIL). NRC 00560: LEVEL CORROSION 2, FLOOR SUPPORT AT STA 148 FROM X=-31/-44 WAS REPLACED PER B717-200 SRM 51-41-02-0G. ORIGINAL THICKNESS WAS 0.040" REMAINING THICKNESS IS 0.019", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 51-10-02 PAR. 8(F) AND DWG #9936533-35. (LP #1116739)

Part: CUSP WEB — CORRODED (BS 936-942) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

RH CORROSION CUSP MEMBRANE BTW STA Y=936 TO Y=942 AT CPAX IN REFERENCE NRC #341 IS OUT OF LIMITS. NRC 00613: CORROSION LEVEL 2, CUSP MEMBRANE BTW STA Y=936 TO Y=942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215.

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 5LH STA 1022 (CPAX). NRC 00387: SECTION LONGERON 5LH FROM STA 986 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1116805)

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FUEL TANK ACCESS DOOR #520CT AND #620CT OF WING LEFT -RIGHT. (AI) (AD). NRC 00609: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND #620CT WERE REPLACED AND PART NUMBER WAS VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 065.

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 5RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00395: SECTION OF LONGERON 5RH BTW STA 1010 TO 1053 WAS REPAIRED PER SRM 53-00-05-2R. (LP #1115229)

Part: CUSP WEB — CRACKED (BS 660) · airframe 46,092 hrs · 31,944 cycles

CRACK AT CUSP WEB STA 660 RH X=-44/-60 (FUS). NRC 00366: CRACK AT CUSP WEB STA 660 RH X=-44/-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114893)

Part: LONGERON — CRACKED (BS 1022) · airframe 46,092 hrs · 31,944 cycles

CRACK ON LONGERON 6LH STA 1022 (CPAX). NRC 00386: SECTION LONGERON WAS REPLACED PER B717-200 SRM 53-00-05-2R-2. (ET) HFEC INSPECTION WAS PERFORMED ON LONGERON 6LH STA 1022 (CPAX) ON TRIM OUT. NO CRACKS WERE FOUND PER B717 NDT SPM PART 6. 06-10-01.001. (EQ. NORTEC C/N 1891. EXP 27AUG19). (LP #1115063)

Part: CUSP WEB — CORRODED (BS 559-562) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION CUSP MEMBRANE BTW STA Y=559 TO Y=562 AT CPAX IN REFERENCE NRC #338 IS OUT OF LIMITS. NRC 00612: CUSP MEMBRANE BTW STA Y=559 TO Y=562 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114952)

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 46,092 hrs · 31,944 cycles

CRACK ON FLOOR PANEL #223GF PAX CABIN. FLOOR PANEL #223GF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1113427)

Part: BEAM — CRACKED (R1 DOOR) · airframe 46,092 hrs · 31,944 cycles

CRACKED BEAM #4 FWD EDGE AT FWD GALLEY SERVICE DOOR (R1) (PTAS). NRC 00342: BEAM #4 AT FWD GALLEY SERVICE DOOR WAS REPLACED PER B717-200 SRM 51-41-01-0G , 51-41-02-0G, AND 51-41- 05-0G. (LP #1106564)

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 46,092 hrs · 31,944 cycles

CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 (CPAX). NRC 00433: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 WAS REMOVED PER B717-200 SRM 51-10-04 PAR 26 DUE TO BEING OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG 103. FLOOR SUPPORT AT STA 200 FROM X=09/13 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #1102447)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,560 hrs · 30,907 cycles

BOTH FORWARD OVERWING FLOOR EXIT IDENTIFIER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE B5-118 BATTERY PACK AND OPERATION OF THE LIGHTS RETURNED TO NORMAL REF AMM 33-51. (LP 5114264)

Part: FLANGE — CRACKED (VERTICAL STAB) · airframe 44,375 hrs · 30,783 cycles

STAB INSPECTION 5530-01048-01 FOUND CRACK INDICATION IN 1 EA HOLE OF THE RT VERT STAB FWD FLANGE JUST BELOW THE LEADING EDGE SKIN SPLICE AT STA ZFS 52.267. REPAIRED PER ER/A 571712-14AD REV ORIG.

Part: SEAL DEPRESSOR — CORRODED (AFT CARGO) · corrosion level 2 · airframe 39,547 hrs · 27,325 cycles

AFT CARGO LOWER SEAL DEPRESSORS CORRODED. REPAIRED IAW RI 551356-14 REV A SEC IV.

Part: DOOR SILL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 39,547 hrs · 27,325 cycles

AFT CARGO LOWER DOOR SILL DOUBLERS CORRODED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,185 hrs · 27,085 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,160 hrs · 27,067 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT EXIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,000 hrs · 26,932 cycles

DURING PRE-FLIGHT CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT EXIT ROW 19E WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: CONTROL UNIT — FAULTY (FIRE DETECTION) · airframe 38,911 hrs · 26,853 cycles

FLIGHT CREW DIVERTED THE AIRCRAFT AFTER THE NR 1 ENGINE FIRE INDICATION ILLUMINATED, ACCOMPANIED WITH AURAL WARNINGS. THE QRH PROCEDURE WAS COMPLIED WITH AND THE NR 1 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND NO EVIDENCE OF ANY ACTUAL FIRE AND REPLACED THE NR 1 ENGINE NOSE FIRE CONTROL UNIT, NR 1 VIA, AND BOTH FIRE BOTTLES FOR THE NR 1 ENGINE, HAVING BEEN DISCHARGED. ALL FIRE DETECTION, INDICATION, AND SUPPRESSIONS SYSTEMS CHECKED NORMAL.

Part: CONTROL UNIT — FAULTY (FIRE DETECTION) · airframe 38,901 hrs · 26,843 cycles

CREW DIVERTED THE ACFT TO RDU WITH THE NR 1 ENGINE SHUTDOWN FOLLOWING A FIRE WARNING INDICATION. DURING CRUISE AT FL330, THE EAD DISPLAYED NR 1 ENGINE FIRE AND IT WAS ACCOMPANIED BY THE AUDIBLE ALERT. CREW STATES THAT THE NR 1 ENGINE FIRE HANDLE WAS NOT ILLUMINATED AND THAT THE NR 1 GENERATOR DID NOT SHUTDOWN. THERE WERE NO ENGINE INSTRUMENT DEVIATIONS AND NO OTHER ELECTRICAL SYSTEM ANNUNCIATIONS WERE PRESENT. THE NR 1 ENGINE SHOWED NORMAL FUEL FLOW, EXHAUST TEMPERATURES, AND COMPRESSOR SPEEDS. THE CREW SHUTDOWN THE NR 1 ENGINE AND DIVERTED THE FLIGHT TO RDU. IT WAS NOTED THAT THE NR 1 ENG FIRE WARNING ILLUMINATED AGAIN AFTER LANDING. MAINTENANCE VERIFIED THERE WAS NOT ANY FIRE AT ANY TIME AROUND THE NR 1 ENGINE. MAINTENANCE COULD NOT FIND ANY DEFECTS TO EXPLAIN THE FALSE FIRE WARNING BUT REPLACED THE FIRE DETECTION CONTROL UNIT AND SENT IT TO ENGINEERING FOR EVALUATION. OPERATION AFTER REPAIR WAS NORMAL AND THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,263 hrs · 26,321 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT BOTH FORWARD DOORS, L1 & R1, AND THE COCKPIT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,244 hrs · 25,552 cycles

TAIL COMPARTMENT CATWALK, AFT EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,058 hrs · 24,742 cycles

FLIGHT STATION EMER LIGHT INOPERATIVE AT BS 123. RECONNECTED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,058 hrs · 24,742 cycles

FORWARD OVERWING EXIT IDENTIFIERS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

INTERCOSTAL CRACKED AT BS 954, LONGERON 30R. R & R INTERCOSTAL IAW DWG.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,058 hrs · 24,742 cycles

EXIT IDENTIFIER SIGNS, LIGHT INOPERATIVE. R & R SIGN IAW AMM.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN FLOOR SUPPORT BROKEN AT BS 256, BETWEEN RBL 22 - 44. R & R SUPPORT IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

CANTED KEEL FORMER CRACKED AT BS 679 RT SIDE. REPAIRED FORMER IAW EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FORWARD WET AREA MEMBRANE DOUBLER CORRODED, BETWEEN BS 160 - 180 & RBL 41 - 60. R & R DOUBLER IAW DWG.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FORWARD WET AREA MEMBRANE CRACKED, BETWEEN BS 157 - 200, BETWEEN RBL 41 - 60. REPAIRED MEMBRANE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

RIGHT CUSP ANGLE CORRODED AT BS 218, RBL 59. REPAIRED CUSP IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

CUSP MEMBRANE AT BS 218, RBL 54.5. REPAIRED MEMBRANE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBEAM CORRODED AT BS 218, RBL 55. REPAIRED FLOORBEAM IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 218 - 237. R & R CUSP WEB IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

WING TO BODY ANGLE CLIP CORRODED AT BS 832, LONGERON 30. R & R CLIP IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

WING TO BODY T ANGLE CLIP, CORRODED AT BS 820, LONGERON 30. R & R ANGLE CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

WING TO BODY T ANGLE CLIP, CORRODED AT BS 807, LONGERON 30. R & R ANGLE CLIP IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

LEFT CANTED KEEL BEAM FORMER CRACKED AT BS 695, LONGERON 26L. REPAIRED FORMER IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

CANTED KEEL BEAM FORMER CRACKED AT BS 678, LONGERON 25L. REPAIRED FORMER IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FRAME ATTACH ANGLE CRACKED AT BS 1174, AFT FACE LONGERON 2L. R & R ANGLE IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FORMER CRACKED AT BS 695, LONGERON 30. R & R FORMER IAW DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FRAME ATTACH ANGLE CRACKED AT BS 1116, LONGERON 15R. REPAIRED ANGLE IAW SRM & DWG.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

LEFT OTBD SEAT TRACK CORRODED, BETWEEN BS 588 - 890, LBL 55. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

LEFT OTBD SEAT TRACK CORRODED, BETWEEN BS 218 - 588, LBL 55. R & R SEAT TRACK IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FORMER CRACKED AT BS 1152, BETWEEN LONGERON 1 - 2R. R & R FORMER IAW DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

AFT CARGO COMPARTMENT, LONGERON END CAP SHOVEL CLIP CORRODED AT BS 1002, LONGERON 25R. R & R SHOVEL CLIP IAW DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

AFT CARGO BILGE AREA LONGERON CORRODED AT BS 954, LONGERON 30. REPAIRED LONGERON IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FORMER CORRODED AT BS 946, BETWEEN LONGERON 30R - 29R. R & R FORMER IAW DWG.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 36,058 hrs · 24,742 cycles

RIGHT PYLON RIB ATTACH ANGLE CRACKED AT BS 1133, UPPER & LOWER END. R & R ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

LEFT INBD SEAT TRACK CORRODED, BETWEEN BS 588 - 890, LBL 22. R & R SEAT TRACK IAW DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

AFT CARGO LONGERON CORRODED AT BS 1004, LONGERON 27L. R & R LONGERON IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

CENTER FLOORBOARD SUPPORT CORRODED AT BS 200, BL 0. R & R SUPPORT IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

SEAT TRACKS CORRODED, BETWEEN BS 589 - 899, RBL 55. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 145 - 200, RBL 7. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

L1 DOOR AREA FLOORBOARD SUPPORT CORRODE, BETWEEN BS 150 - 185, LBL 55. R & R FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED AT BS 200, RBL 32. R & R FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 150 - 180, RBL 44.5. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 36,058 hrs · 24,742 cycles

LEFT WING FIXED LE OTBD SIDE OF VORTILON ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 36,058 hrs · 24,742 cycles

RIGHT WING INBD SIDE OF INBD FLAP TRACK, CARRIAGE ON FUSELAGE ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 150 - 185, LBL 44.5. R & R SUPPORT IAW SRM & DWG.

Part: STRAP — CRACKED (LT WING) · airframe 36,058 hrs · 24,742 cycles

LEFT WING OTBD SIDE OF VORTILON, LE DOUBLER STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 200 - 256, LBL 15. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOORBOARD SUPPORT CORRODED AT BS 165, BETWEEN RBL 10 - RBL 22. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN SEAT TRACKS CORRODED, BETWEEN BS 323 - 533, RBL 55. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

SEAT TRACKS CORRODED, BETWEEN BS 823 - 899, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 589 - 646, RBL 22. R & R SEAT TRACK IAW DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

AFT CARGO LONGERON SUPPORT SHOVEL CLIP CORRODED, BETWEEN BS 1002 - 1006, STRINGER 24R. R & R CLIP IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN SEAT TRACKS CORRODED, BETWEEN BS 265 - 589, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

SEAT TRACKS CORRODED, BETWEEN BS 646 - 822, RBL 22. R & R SEAT TRACK IAW DWG.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 36,058 hrs · 24,742 cycles

RIGHT FWD EMER EXIT DOOR, LOWER AFT FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,244 hrs · 25,552 cycles

MAIN CABIN FRAME CRACKED AT BS 674, RT SIDE. R & R FRAME IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

FLOOR SUPPORT CORRODED AT BS 200, LBL 53. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 674 & RBL 45 - 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 674 & LBL 45 - 54. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 36,058 hrs · 24,742 cycles

CUSP WEB CRACKED AT BS 696, RBL 45. REPAIRED CUSP WEB IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 36,058 hrs · 24,742 cycles

LEFT WING REAR SPAR WEB XRS 309.00 CRACKED. REPAIRED WEB IAW FAS EA.

Part: SUPPORT — BROKEN (R1 DOOR) · airframe 35,937 hrs · 24,661 cycles

R1 DOOR EMER EVAC SLIDE FWD & AFT GIRT BAR FITTINGS ATTACH SUPPORTS BROKEN. R & R SUPPORTS IAW AMM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,937 hrs · 24,661 cycles

FRAME LOWER FWD FLANGE CORRODED AT BS 180, BETWEEN LONGERON 29L TO LONGERON 29R. REPAIRED FRAME IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 35,937 hrs · 24,661 cycles

R1 DOOR JAMB CORRODED ON GIRT BAR ATTACH PLATE. R & R PLATE IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 35,937 hrs · 24,661 cycles

C2 DOOR JAMB CORRODED AROUND STOP FITTINGS. R & R JAMB PAN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,937 hrs · 24,661 cycles

FRAME FWD LOWER FLANGE CORRODED AT BS 200, BETWEEN LONGERON 29L TO LONGERON 29R. REPAIRED FRAME IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,674 hrs · 24,487 cycles

L1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: LANYARD — DISCONNECTED (R1 DOOR) · airframe 35,589 hrs · 24,433 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD DISCONNECTED. SECURED LANYARD IAW AMM.

Part: LANYARD — DISCONNECTED (L1 DOOR) · airframe 34,030 hrs · 23,431 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD DISCONNECTED. CONNECTED LANYARD IAW MM.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 33,758 hrs · 23,261 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: DOOR — CRACKED (LE SLAT) · airframe 32,703 hrs · 22,623 cycles

LEFT WING NR 10 SLAT TRACK LOWER COVER CRACKED. R & R SLAT DOOR ASSY IAW SRM.

Part: STRAP — LOOSE (L1 DOOR) · airframe 33,459 hrs · 23,070 cycles

L1 DOOR SLIDE STRAP ASSY LOOSE. SECURED STRAP PER MM.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FORWARD CARGO CUTOUT LOWER DOOR JAMB, CORROSION. ACCOMPLISHED JAMB SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-20-15.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO LOWER DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 53-20-15.

Part: COVER — MISSING (CABIN)

ROW 26 MISSING EPL COVER (WHITE). REPLACED MISSING COVER IAW AMM 33-51.

Part: COVER — DISLODGED (EMERGENCY LIGHT)

EXIT SIGN COVER (ON CEILING) FELL OFF DURING TAKEOFF. INSTALLED COVER PER MM 33-00.

Part: SLIDE — LOW PRESSURE (L1 DOOR)

L1 PACK PRECHARGE APPEARS LOW. REMOVED AND REPLACED L1 DOOR SLIDE REF MM 25-61-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

RIGHT OUTBOARD CABIN SEAT TRACK CORROSION SPOTS FROM FS 256 THROUGH FS 579. REPLACED SECTION OF SEAT TRACK FROM FS 256 THROUGH FS 579 REF B717 SRM 53-20-52 AND EA 17-53-01734IR.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FWD CABIN SEAT TRACK AT RBL 24 CORROSION SPOTS FROM FS 198 THROUGH FS 239. CUT OUT DAMAGED SECTION OF SEAT TRACK RBL 24, INSTALLED NEW SECTION WITH SPLICE AT STA 265 PER REF DC9 SRM 53-05 FIG 4F-7001 INSTALLATION AND EA 17-53-01734IR.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.

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: BATTERY PACK — DISCHARGED (CABIN)

DURING OVERNIGHT SERVICE CHECK FOUND EMERGENCY SEAT LIGHTS ROW 21-25 INOP. REPLACED BATTERY PACK ASSEMBLY AT SEAT 3DF AND OPS CHECK GOOD PER AMM 33-51.

Part: STRUCTURE — DAMAGED (FUSELAGE)

WHILE DOWNJACKING A/C AFT JACK FAILED AND DAMAGED A/C. INSTALLED REPAIR DOUBLER, TRIPLER, FILLER AND FINGER DOULBER.

Part: SKIN — DAMAGED (FUSELAGE)

WHILE DOWN JACKING A/C AFT JACK FAILED AND DAMAGED A/C. INSTALLED FILLER, DOUBLER, AND TRIPLER. INSTALLED HL18PB6 HI-LOKS WET WITH PR1422 B1/2. INSTALLED CR3223-5 BLIND FASTENERS FOR AFT TWO FASTENER ROWS COMMON TO THE APB TEE CAP REAR TANG. MAINTAINED 4-6D FASTENER SPACING AND 2D MIN EDGE DISTANCE.

Part: THRUST REVERSER — INOPERATIVE (RT)

ENG RH REV FAULT ANNUN IN FLIGHT FOLLOWED BY AMBER RT U/L LIGHT COMPLETED PROCEDURE IAW QRH. REMOVED AND REPLACED RT THRUST REVERSER REF MM 78-30. OPS CK OK FOR SERVICE.

Part: WIRE — BURNED (HANDSET)

AFT HANDSET CORD MELTED AND PRODUCED STRONG ELECTRICAL ODOR. REMOVED AND REPLACED AFT F/A HANDSET, OPS CHECKS NORMAL, NO OTHER DISCREPANCIES NOTED, REF AMM 23-41. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY SUPPLY REF 717 AMM 33-51-06, OPS CHECK GOOD (IN AFT CARGO COMPARTMENT).