N132EV

Part: CHANNEL — CRACKED · airframe 36,488 hrs · 26,673 cycles

CRACK ON CHANNEL BTW ACCESS PANEL 195DL AND 196DR. CHANEL (P/N: CC690-39251-1) WAS REPLACED AND VERIFIED PER CRJ-900 SRM 53-82-83-001-001-A02. FIGURE 53-82-83-995-802. ITEM 120.

Part: LUG — CORRODED (AILERON) · airframe 36,488 hrs · 26,673 cycles

RTN FINDING IN REF TO CARD 900-27-900-910: AFTER BEARING AND BUSHINGS REMOVAL ON LH AILERON, CORROSION WAS FOUND ON ALL LUGS BORES AT LH AILERON CENTER FITTING LUGS BORES L1, L2, L5 AND L6 AT LH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-107 REV - B AND LUGS BORES L3 AND L4 WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,488 hrs · 26,673 cycles

INITIAL INSPECTION: CORROSION ON FLOOR BEAMS SPACER FS 310.00 LBL 11 AND FS 333.00 RBL 8 AT FWD PAX CABIN (W1) CORROSION ON FLOOR BEAMS SPACER FS 310.00 LBL 11 AND FS 333.00 RBL 8 AT FWD PAX CABIN (W1) WAS REMOMED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 THEREFORE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: STRAP — CRACKED · airframe 36,488 hrs · 26,673 cycles

CRACK ON JOINT STRAP BTW ACCESS PANEL 195DL AND 196DR STRAP ASSY (P/N: CC690-39171-5) WAS VERIFIED PER CRJ-900 IPC 53-82-83-10 AND REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.

Part: FITTING — CORRODED (ZONE 900) · airframe 36,488 hrs · 26,673 cycles

CORROSION ON GALLEY FITTINGS (5 EAS) FS 288.00 LBL 37, FS 295.00 RBL 3, FS 316.00 RBL 4 AND FS 285.00 RBL 17 AND RBL 38 APROX AT PAX CABIN GALLEY FITTINGS (5 EAS) FS 288.00 LBL 37, FS 295.00 RBL 3, FS 316.00 RBL 4 AND FS 285.00 RBL 17 AND RBL 38 APROX AT PAX CABIN WERE REPLACED DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-20-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (ZONE 100) · airframe 36,488 hrs · 26,673 cycles

CORROSION ON ANGLE OF ATTACH POINT BONDING JUMPER AT FWD SERVICE ACCESS DOOR CORROSION ON ANGLE OF ATTACH POINT BONDING JUMPER AT FWD SERVICE ACCESS DOOR WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ-900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE ANGLE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: ANGLE — CORRODED (ZONE 100) · airframe 36,488 hrs · 26,673 cycles

INTIAL INSPECTION: CORROSION ON INTERNAL ANGLE AND BEHIND OF ANGLE AT FWD TOILET SERVICE ACCESS EXTERNAL FUSELAGE CORROSION ON INTERNAL ANGLE AT FWD TOILET SERVICE ACCESS EXTERNAL FUSELAGE WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 , INTERNAL ANGLE WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,488 hrs · 26,673 cycles

INITIAL INSPECTION:CORROSION (SEVERAL POINTS) ON RH SEAT TRACK RBL 10 BTW FS 349.00 TO 379.00 ALSO CORROSION ON LH SEAT TRACK LBL 10 BTW FS 374.00 TO 409.00 AND LBL 27 BTW FS 364.00 FWD END AT PAX CABIN DUE TO EXCESIVE DAMAGE ON RH SEAT TRACK RBL 10 BTW FS 349.00 TO 379.00 AND LH SEAT TRACK LBL 10 BTW FS 374.00 TO 409.00 AND LBL 27 BTW FS 364.00 FWD END AT PAX CABIN WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 THEREFORE WERE REPLACED PER CRJ 900 AMM 53-00-49-400-801-A07

Part: RETAINER — CRACKED (ZONE 100) · airframe 36,488 hrs · 26,673 cycles

CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND LBL & RBL 34). MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND LBL & RBL 34) WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801 (CONFIG A01)

Part: RETAINER — CRACKED (ZONE 100) · airframe 36,488 hrs · 26,673 cycles

CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH (FS 797.00 AND LBL & RBL 34). MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH (FS 797.00 AND LBL & RBL 34) WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801 (CONFIG A01)

Part: ANGLE — CRACKED (ZONE 300) · airframe 36,488 hrs · 26,673 cycles

CRACK ON LEFT & RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT & RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01 AND (ET) HFEC INSPECTION WAS PERFORMED ON LEFT & RIGHT VERTICAL STABILIZER FWD DRAG ANGLE NO CRACKS WERE FOUND PER CRJ700/900/1000 NDT MANUAL PART 01, 51-20-006-250-A01

Part: CONTACT — FAULTED (ZONE 200) · airframe 35,211 hrs · 25,576 cycles

NH OVERWING EMERGENCY EXIT LIGHT LOCATED ON PANEL 171CL INOP BELOW AFT EMERGENCY EXIT DOOR INOP IF FLIGHT OPS CHARGEABLE THEN NOT REPORTABLE. OKAY TO DEFER LH OVERWING EMERGENCY EXIT LIGHT PER MEL 33-51-2B PLACARD INSTALLED. REMOVED AND REPLACED BROKEN CRIMP CONTACT ON LT. WING EXTERIOR PANEL 171CL EMER. LIGHT W/SERV. PART IAW ESPM 20-16-05 AMM 33-51-15. OPS CHECK GOOD.

Part: BEAM — CHAFED (ZONE 200) · airframe 35,091 hrs · 25,477 cycles

DURING INSPECTION IN CWA, MAINTENANCE FOUND CHAFE DAMAGE ON THE FS1000.00 TO FS1047.00 AFT CARGO DOOR CROSS BEAM AS SHOWN IN FIG. 1. THE CHAFE DAMAGE MEASURES A MAXIMUM MATERIAL LOSS OF 0.060Ï¿½ DEEP. THE BEAM IS FORMED FROM 0.063Ï¿½ 7075-T62 CLAD AL ALLOY. MAINTENANCE CONTACTED ENGINEERING FOR EVALUATION AND DISPOSITION COMPLETED APPROVED REPAIR ON AFT CARGO DOOR CROSS BEAM, FS1000.00 - FS1047.00 IAW EA CRJ953-17815. PN: MM670-35502-010, CL600-2D24 DOCUMENTED ON NON-ROUTINE CARD 924298 & COMPLETED ON 11/24/2024 **THIS IS A MAJOR REPAIR**

Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 34,347 hrs · 24,849 cycles

L/H FWD EMERGENCY EXIT DOOR UPPER LUG CRACKED. REPAIRED THE L/H FWD EMRGENCY DOOR TOP EDGE MEMBER IAW ENDEAVOR AIR EA CRJ952-16837 REV. IR DATED 6-25-24.

Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 34,347 hrs · 24,849 cycles

UPON REMOVAL OF THE RH AFT OVER WING EMERGENCY EXIT SH670-36600 SN# SB0910 A VISUAL CRACK CAN BE SEEN UNDER THE UPPER AFT LUG. REPAIRED THE R/H AFT EMERGENCY EXIT TOP EDGE MEMBER AFT LUG IAW ENDEAVOR AIR EA CRJ952-16903REV IR DATED 6-25-24

Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 34,347 hrs · 24,849 cycles

L/H AFT EMERGENCY EXIT DOOR UPPER LUG CRACKED. REPAIRED THE L/H AFT EMERGENCY DOOR TOP EDGE MEMBER IAW ENDEAVOR AIR EA CRJ952-16836 REV. IR DATED 6-25-24.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,347 hrs · 24,849 cycles

LBL 9 SEAT TRACK FROM FS 693 TO FS 847 IS CORRODED. REMOVED AND REPLACED LBL 9 SEAT TRACK FROM FS 693 TO FS 847 IAW CRJ-900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,347 hrs · 24,849 cycles

RBL 9 SEAT TRACK FROM FS 693 TO FS 847 IS CORRODED. REMOVED AND REPLACED RBL 9 SEAT TRACK FROM FS 693 TO FS 847 IAW CRJ-900 SRMS 53-00-49-201-002-A01 AND 51-40-11-001-001-A01.

Part: IDG — MAKING METAL (NR 1) · airframe 31,341 hrs · 22,257 cycles

ON SHORT APPROACH AC ESS BUS CAUTION MSG FOLLOWED BY LOSS OF ALL AC PWR. ADG DEPLOYED. APU WAS OFF UPON LANDING. COMPLETED ALL STEPS OF TECHNICAL ACTION PLAN (TAP) #0441, REFER TO NRWC #822795. COMPLETED WIRING CHECKS STEP 3 ON NRWC #822799 AND STEP 4 ON NRWC #822798 NO DEFECTS NOTED PER WDM 24-21-03. DURING STEP 7 TEST, #1 IDG FAILS (FOUND MAKING METAL). #1 IDG (PN 766277B, SN 1400) AND FILTERS REPLACED PER AMM 24-11-01. REPLACED #2 IDG (PN 766277B, SN 1109) AND FILTERS DUE TO RELATED B1-007112 AND B1-007108 CODES. REPLACED SSPC1 (K124)(PN 310CZ01Y00, S/N 2301) DUE TO CHATTERING AND RELATED B1-006197. ADG INSPECTED AND STOWED PER AMM 05-51-19. ALL REQ'D OPS AND LEAK CHECKS GOOD.

Part: DOUBLER — CHAFED · airframe 29,684 hrs · 20,885 cycles

LH UPPER TRANSCOWL FWD LATCH HOUSING DOUBLER IS CHAFED AND HAS SHEERED RIVETS. - REMOVED AND REPLACED AFT CHANNEL IAW CRJ 900 SRM 51-42-13-001-001-A01 AND COMPLIED WITH ENDEAVOR AIR EA CRJ 954-12843 DATE 2/9/22 REV A.

Part: INTERCOSTAL — CORRODED · airframe 29,684 hrs · 20,885 cycles

GALLEY SERVICE DOOR INTERCOSTAL AT STGR 20R BETWEEN F.S. 310 TO F.S. 349 IS CORRODED. - REMOVED AND REPLACED 2 EA INTERCOSTALS AT STR 20R BETWEEN FS 310 AND FS 349 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-41-02-001-001-A01, 51-26-00-001-001-A01, 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: ANGLE — BENT · airframe 29,684 hrs · 20,885 cycles

PAX DOOR SIDE LIGHTNING DIVERTER PANEL SUPPORT BEAM/ANGLE BENT AND RIVETS SHEARED. FS 319-333 - REMOVED AND REPLACED PAX DOOR LIGHTNING DIVERTER PNL SUPPORT BEAM/ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED BEAM ANGLE AND CLEAF IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 29,684 hrs · 20,885 cycles

GALLEY SERVICE DOOR INTERCOSTAL AT STGR 20R BETWEEN F.S. 310 TO F.S. 349 IS CORRODED. - REMOVED AND REPLACED 2 EA INTERCOSTALS AT STR 20R BETWEEN FS 310 AND FS 349 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-41-02-001-001-A01, 51-26-00-001-001-A01, 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: CLEAT — BENT · airframe 29,684 hrs · 20,885 cycles

PAX DOOR SIDE LIGHTNING DIVERTER PANEL SUPPORT BEAM/ANGLE BENT AND RIVETS SHEARED. FS 319-333 - REMOVED AND REPLACED PAX DOOR LIGHTNING DIVERTER PNL SUPPORT BEAM/ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED BEAM ANGLE AND CLEAF IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED · airframe 29,684 hrs · 20,885 cycles

INTERCOSTAL AT FS 349 IS CORRODED FROM STRG 27-26R - FOUND TO BE FRAME 349 STR 26L-24R CORRODED, NOT INTERCOSTAL. LOCATED AND DRILLED AND INSTALLED NEW FRAME SECTION IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. WVAC EMP STAMP # 794 MTC. INSTALLED NEW FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AT FS 349 STGR 23R-23L.

Part: FRAME — CORRODED · airframe 29,684 hrs · 20,885 cycles

INTERCOSTAL AT FS 295, STRG 25R IS CORRODED. - FOUND DAMAGE TO BE ON FRAME 295, NOT ON INTERCOSTAL. REPAIRED FRAME 295 IAW ENDEAVOR EA CRJ 953-12674 REV IR DATED 1/1/22. REMOVED AND REINSTALLED VERTICAL POST AT FS 295 RBL20 AND INTERCOSTAL BETWEEN FS 280 AND 295 RBL 37 IAW CRJ 900 SRM 51-42-21-001-001-A01.

Part: NONE — CORRODED · airframe 29,684 hrs · 20,885 cycles

RH CABIN FLOOR SILL HAS CORROSION FS 316, RBL 42. - INSTALLED NUTPLATE ON SERVICE DOOR SILL AT FS 316 RBL42 IAW CRJ 900 SRM 51-42-15-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 21R IS CORRODED BETWEEN F.S. 319 TO F.S. 349. - REPLACED STGR 21R FROM FS 280-379 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND ENDEAVOR EA CRJ953-12707 REV IR DATED 1/15/22.

Part: LONGERON — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 25R CORRODED FS 280 TO FS 349 - REMOVED AND REPLACED STR 25R FROM FS280-333, LONGERON FROM FS333-364 AND SPLICE PLATE AT FS333 STR25R IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND ENDEAVOR EA CRJ953-12663 REV IR, DATED 12/29/21

Part: CLEAT — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 21R IS CORRODED BETWEEN F.S. 319 TO F.S. 349. - REPLACED STGR 21R FROM FS 280-379 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND ENDEAVOR EA CRJ953-12707 REV IR DATED 1/15/22.

Part: JOINT — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 25R CORRODED FS 280 TO FS 349 - REMOVED AND REPLACED STR 25R FROM FS280-333, LONGERON FROM FS333-364 AND SPLICE PLATE AT FS333 STR25R IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND ENDEAVOR EA CRJ953-12663 REV IR, DATED 12/29/21

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 25R CORRODED FS 280 TO FS 349 - REMOVED AND REPLACED STR 25R FROM FS280-333, LONGERON FROM FS333-364 AND SPLICE PLATE AT FS333 STR25R IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND ENDEAVOR EA CRJ953-12663 REV IR, DATED 12/29/21

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRG 26R CORRODED FROM FS 349 TO 364. 53-190-507 - REPLACED STGR 26R FROM FS 349-364 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 26R HAS MULTIPLE SPOTS OF CORROSION FROM FS 280-FS 333 AND JOINT PIECE AT 26R FS 333 - REPLACED STR 26R AT FS 280-333 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. REPLACED JOINT PEICE AT FS 333 IAW CRJ900 SRM 31-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 22R IS CORRODED BETWEEN FS 333 & FS 349 TCI- 53-20-320 - REMOVED AND REPLACED STR 22R BETWEEN FS 333 AND FS 349 IAW CRJ900 SRM'S 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REPLACED CANON PLUG BRACKET IAW CRJ900 SRM'S 51-40-11-001-001-A01 AND 51-41-02-001-001-A01

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 24R CORRODED BETWEEN FS 333 AND FS 354. - REPAIRED STRINGER 24R FROM FS 333-354 IAW CRJ 900 SRM 53-00-03-201-001-A02, REPAIR SOLUTION II, REMOVED AND REINSTALLED CLEAT @ FS 333 IAW CRJ 900 SRM 51-42-01-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 24R FROM FS 280 TO 333 AND JOINT PIECE AT FS 333, STR 24R ARE HEAVILY CORRODED. - REPLACED STRINGER 24R FROM FS 280-333 AND JOINT PIECE AT FS 333 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 22R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. - REMOVED AND REPLACED STR22R AND SPLICE JOINT FROM FS280-FS333 IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-21-16-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 20R IS CORRODED BETWEEN F.S. 295 TO F.S. 310 - REMOVED & REPLACED STGR 20R BETWEEN F.S. 280- F.S. 319 IAW CRJ900 SRM 51-40-11-001-001-A01/ 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: ANGLE — CRACKED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR AFT WEB IS CRACK NEEDS REPLACED P/N 601R317071-11 - LOCATED & DRILLED NEW AFT WEB P/N 601R317-071-11 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED ATTACHNG ANGLES IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 7-25-20

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

FS 295 TO FS 310 STGR 19R IS CORRDED. - REMOVED AND REPLACED STR 19R BETWEEN FS 280 AND FS 319 IAW ENDEAVOR AIR CRJ953-12652. REMOVED AND REPLACED 1 EA CLEAT AND 10 WIRE CLIPS ON STR 19R IAW CRJ-900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: PANEL — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR TOP COVER PLATE IS CORRODED IN MULTIPLE AREA. - REMOVED AND REPLACE PAX DOOR TOP COVER PLATE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: COVER — CRACKED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR OUTER HANDLE FLAPPER IS CRACK P/N: 601R317045-1. - LOCATED & DRILLED PAX DOOR OUTER HANDLE FLAPER P/N 601R317045-1 IAW 900 SRM 51-40-11-001-001-A01, INSTALLED NEW FLAPER IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 38 07/25/20.

Part: FORMER — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR FWD FORMER AT FS 311.75 CORRODED - LOCATED & DRILLED NEW FWD PAX DOOR FORMER IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW FORMER P/N 601R318031-5 IAW CRJ900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01 REV 38 7-25-20.

Part: BRACKET — CRACKED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR AFT GAS SPRING BRACKET CRACKED - LOCATED & DRILLED NEW PAX DOOR AFT GAS SPRING BRACKET P/N 601R318011-1 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW BRACKET IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 7-25-20.

Part: BRACKET — CRACKED · airframe 29,684 hrs · 20,885 cycles

STIFFENER ON PAX DOOR AFT WEB FOR POWER ASSIST MOTOR IS CRACK P/N 601R317745-7 - LOCATED & DRILLED NEW STIFFENER P/N 601R317745-7 IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW STIFFENER IAW CRJ900 SRM 51-42-22-001-001-A01 REV 38 7-25-20

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS 565 TO FS 661+16. - REPLACED WITH NEW SERVICEABLE TRACK EXTRUSION IAW CRJ 900 AMM 53-00-49-000/400-801-A07, SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS 785 TO 797. - REMOVED AND INSTALLED SEAT TRACK FROM FS 785-797 RH SIDE IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 23R CORRODED BETWEEN FS 349.00 & FS 364.00. - REPLACED STRINGER 23R FS 349-364 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01.

Part: ANGLE — CRACKED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR AFT DRAG ANGLE IS CRACK P/N 601R31772-5S - LOCATED & DRILLED AFT DRAG ANGLE P/N 601R31772-5S IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-22-001-001-A01 REV 38 7-25-20

Part: PANEL — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR FWD STAIR WEB CORRODED - REMOVED AND REPLACED PAX DOOR FWD STAIR WEB IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: SKIN — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR INNER SKIN CORRODED IN MULTIPLE LOCATION - REMOVED AND REPLACED PAX DOOR INNER SKIN IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FORMER — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR AFT FORMER AT F/S 347.25 CORRODED - LOCATED A&DRILLED PAX DOOR NEW AFT FORMER P/N 601R318034-5 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW AFT FORMER IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 07-25-20

Part: INTERCOSTAL — CORRODED · airframe 29,684 hrs · 20,885 cycles

INTERCOSTAL DD7A FWD CENTER 1ST FROM HINGE P/N 601R318083-1 IS CORRODED - LOCATED & DRILLED PAX DOOR INTERCOSTAL DD7A P/N 601R318083-1 IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 07-25-20 WVAC EMP # 574780

Part: INTERCOSTAL — CORRODED · airframe 29,684 hrs · 20,885 cycles

PAX DOOR INTERCOSTAL 3ND FROM HINGE ON FWD SIDE AT DD5 P/N 601R318091-5 IS CORRODED - LOCATED & DRILLED NEW INTERCOSTAL P/N 601R318091-5 IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 07-25-20

Part: JOINT — CORRODED · airframe 29,684 hrs · 20,885 cycles

STGR 23R IS CORRODED BETWEEN FS 333 TO FS 349. - FOUND CORROSION TO BE ONLY ON STGR JOINT PIECE AT FS 333, REPLACED PART IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,684 hrs · 20,885 cycles

STRINGER 23R CORRODED BETWEEN FS 310.00 & FS 333.00 - REPLACED STGR 23R FROM FS 310-333 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 785 TO FS 797. - REMOVED & REPLACE SEAT TRACK AND RETAINER IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: RETAINER — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 785 TO FS 797. - REMOVED & REPLACE SEAT TRACK AND RETAINER IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS847+16 TO FS 847.7. - LOCATED, DRILLED NEW SEAT TRACK IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 53-00-49-201-002-A01. REMOVED OLD TRACK AND INSTALLED NEW TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

VISIBLE SEAT TRACK AT RBL 9 IS CORRDED BELOW THE GALLEY AND LAV WALL MOUNTING LUGS BETWEEN FS 349.00 & 379.00. - REPLACED AND FABRICATE SEAT TRACK AT RBL9 AT FS 349 TO 453 IAW CRJ 900 AMM 53-00-49-000-801-A07, SRM 53-00-49-201-002-A01, SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801-A07

Part: NONE — CORRODED · airframe 29,684 hrs · 20,885 cycles

CLIP AT FS 327 DD7A P/N: 601R318058-1 IS CORRODED. - LOCATED & DRILLED NEW CLIP P/N 601R318058-1 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW CLIP IAW CRJ 900 SRM 51-42-00-001-001-A01 INSTALLED NEW CLIP IAW CRJ 900 SRM 51-42-00-001-001-A01 REV 387-2520.

Part: RETAINER — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 677 TO FS 720. - REMOVED & REPLACE SEAT TRACK & RETAINER IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: ANGLE — CORRODED · airframe 29,684 hrs · 20,885 cycles

ANGLE ON CENTER OF PAX DOOR AT DD7A IS CORRODED PN 601R317057-1. - LOCATED & DRILLED NEW PAX DOOR ANGLE P/N 601R317052-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW ANGLE IAW CRJ 900 SRM 51-40-06-001-001-A01 REV 38 7/25/20.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 677 TO FS 720. - REMOVED & REPLACE SEAT TRACK & RETAINER IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS 474 TO FS 566. - REMOVED ADN REPLACED RH SIDE SEAT TRACK FROM FS 474 TO FS 566 IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS 661+16 TO FS 677. - REMOVED, LOCATED, DRILLED & INSTALLED SERVICEABLE SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07 & SRM 53-00-49-201-002-A01 & 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 761.85 TO F.S. 744.15 - INSTALLED NEW SEAT TRACK RAIL BTWN F/S 744.15-761.85 IAW CRJ900 AMM 53-00-49-400-801(CONFIG A07) (P/N SH690-36285-1)

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 847+16 TO F.S. 847.7 - REPLACED AND FABRICATE SIDE SEAT TRACK R/H BETWEEN FS 847 TO FS 865 IAW CRJ900 AMM 53-00-49-000-801-A07 SRM 51-40-11-001-001-A01 SRM 53-00-49-201-002-A01 AMM 53-00-49-400-801-A07 WVAC EMP STAMP # 776 MTC

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 474 TO FS 565. - REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS 474 TO FS 565 IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT TRACK IS CORRODED BETWEEN FS 565 TO FS 661+16. - REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS 565 TO FS 661+16 WITH NEWLY FABRICATED SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN F.S. 744.15 TO F.S. 761.85 - INSTALLED NEW SEAT RAIL L/H SIDE @ FS 744.15- FS 761.85 P/N SH690-36285-1 IAW CRJ900 AMM 53-00-49-400-801-CONFIG A07

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 661+16 TO F.S. 677. - REMOVED, FABRICATED, & INSTALLED SERVICEABLE TRACK IAW CRJ AMM 53-00-49-000/400-801(A07) & SRM 53-00-49-201-A01 & 51-40-11-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 29,684 hrs · 20,885 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 677 TO F.S. 720. TCI 53-20-245 - REMOVED,LOCATED,DRILLED, & INSTALLED SERVICEABLE SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801(A07) & SRM 53-00-49-201-002(A01) & 51-40-11-001-001-A01

Part: LIGHT — BROKEN (CABIN) · airframe 23,163 hrs · 15,621 cycles

EMER FLOOR LIGHTING STRIP BROKEN ADJACENT SEAT 1A. R&R BROKEN EMER FLOOR LIGHTING STRIP AT SEAT 1A IAW AMM 33-51-01. OPS TEST NORMAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

STA 295 STR 27 TO 26R WEB / INTERCOSTAL CORRODED. REPAIRED FRAME STA 295 STR 27 TO 26R WEB/ INTERCOSTAL IAW EA CRJ953-07102.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

AFTER REMOVAL OF CAP STRIP ON LBL 27 FOUND CORROSION AT FS 1031 FLOORBEAM. REPAIRED FLOORBEAM IAW GREO 670-53-00-029 REV A.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 22,613 hrs · 15,203 cycles

AFTER REMOVAL OF CAP STRIP AT LBL 9, FOUND CORROSION AT BS 1031 FLOORBEAM. REPAIRED THE FLOORBEAM IAW GREO 670-53-00-029.

Part: STRIP — CRACKED (CABIN) · airframe 22,613 hrs · 15,203 cycles

SEVERAL EMERGENCY PATH LIGHTING STRIPS THROUGHOUT CABIN WORN AND CRACKED. REPLACED EMERGENCY PATH STRIPS AT CABIN IAW AMM 33-51-01-400- 801.

Part: SUPPORT STRAP — CRACKED (CABIN) · airframe 22,613 hrs · 15,203 cycles

DADO PANEL 252 TRW AFT SIDE SUPPORT STRAP CRACKED (PR). REMOVED AND REPLACED SUPPORT STRAP IAW CRJ900 SRM 51-42-06.

Part: SUPPORT STRAP — CRACKED (CABIN) · airframe 22,613 hrs · 15,203 cycles

DADO PANEL 271SLW AFT SIDE SUPPORT STRAP CRACKED (PR). REMOVED AND REPLACED SUPPORT STRAP IAW SRM 51-42-06.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

LT AFT WTB FAIRING 195DL LANDING CRACKED AND CORRODED. REMOVED AND REPLACED C CHANEL LANDING IAW SRM 51-42-13.

Part: STRAP — CRACKED (PANEL 195DL) · airframe 22,613 hrs · 15,203 cycles

BOTH FWD AND AFT PANEL LANDING STRAP ON PANEL 195DL HAVE CORROSION SPOTS, AND IS CRACKED. FABRICATED A NEW STRAP IAW SRM 51-24-36, AND INSTALLED.

Part: PLATE — CRACKED (E/E BAY) · airframe 22,613 hrs · 15,203 cycles

MOUNT PLATE FOR JB6 IN FWD EQUIPMENT COMPARTMENT WAS CRACKED. REMOVED AND REPLACED MOUNT PLATE IAW SRM 51-42-06.

Part: FIRESHIELD — CRACKED (RT COWLING) · airframe 22,613 hrs · 15,203 cycles

RH AFT CORE COWL HEAT SHIELD IS CRACKED. REPAIRED HEAT SHIELD IAW SRM 54-13-00 PG201.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

TWO DOUBLERS BETWEEN BS 364 - 379, STRINGER 20R DAMAGED. REPLACED THE TEMP REPAIR DOUBLERS IAW REO 690-53-21-1005.

Part: GUARD — CRACKED (MLG WHEEL WELL) · airframe 22,613 hrs · 15,203 cycles

RIGHT MLG WHEEL WELL ANGLED GRAVEL GUARD PLATE WAS CRACKED AT 2 SPOTS. REMOVED AND REPLACED THE GRAVEL GUARD IAW SRM 51-42-15, SRM 51-44-11, AND AMM 20-21-00.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 22,613 hrs · 15,203 cycles

FOUND THE BS 280 BULKHEAD WEB CORRODED. REPLACED THE BULKHEAD WEB IAW SRM 51-42-06, SRM 51-42-13, AND SRM 51-42-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

LT 280 BEAM CORRODED. REPLACED LT 280 BEAM IAW SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

RT 280 BEAM CORRODED. REPLACED RT 280 BEAM IAW SRM 51-42-06, SRM 51-42-13, AND SRM 51-42-21.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

280 BEAM CORRODED AT FLIGHT DECK ENTRYWAY. REPLACED 280 BEAM SUPPORT ANGLE IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,613 hrs · 15,203 cycles

CLIP ON RT AFT SIDE OF FS 202.75 AND WL 79.50 IS CRACKED. R&R CLIP ON RT AFT SIDE OF FS 202.75 REF SRM 51-24-21 AND SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PASSENGER DOOR) · airframe 22,613 hrs · 15,203 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED PAX DOOR DRAG ANGLE IAW SRM 52-11-04, AND 51-42-13.

Part: PULLEY BRACKET — CRACKED (PASSENGER DOOR) · airframe 22,613 hrs · 15,203 cycles

PAX DOOR SUPPORT WHEEL CABLE PULLEY BRACKET WAW CRACKED. REMOVED & REPLACED THE PULLY BRACKET IAW SRM 51-42-06.

Part: HANDLE — BROKEN (OXYGEN MASK) · airframe 22,106 hrs · 14,834 cycles

CAPTAIN`S OXYGEN MASK RED HANDLE BROKEN. REMOVED & REPLACED THE OXYGEN MASK IAW AMM 35-11-12

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 20CD) · airframe 21,960 hrs · 14,733 cycles

PAX OXYGEN UNIT DISLODGED ON BOARDING, 20CD. REPACKED THE MASK AT SEAT 20 CD IAW AMM 35-21-09. NO DEFECTS NOTED.

Part: SMOKE DETECTOR — INOPERATIVE (FWD LAVATORY) · airframe 21,829 hrs · 14,641 cycles

FWD SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED THE FWD SMOKE DETECTOR IAW AMM 26-16-01.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 21,817 hrs · 14,632 cycles

DURING MORNING WAKE-UP, FOUND THE FIRST OFFICERS 02 MASK LEAKING. REMOVED AND REPLACED FO 02 MASK IAW AMM 35-11-12. OPS & LEAK CHECKED GOOD.

Part: TUBE — BENT (EXTINGUISHER) · airframe 21,696 hrs · 14,545 cycles

FOUND FWD LAVATORY EXTINGUISHER DISCHARGE TUBES WERE BENT AND DAMAGED. REMOVED AND REPLACED THE FWD LAVATORY FIRE EXTINGUISHER IAW AMM 26-26-01.

Part: SKIN — DENTED (BS 338) · airframe 21,673 hrs · 14,525 cycles

THREE DENTS BELOW GALLEY SEVICE DOOR BS 338, STRINGER 19R. COMPLIED WITH EA 953-06233.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 21,673 hrs · 14,525 cycles

EMERGENCY EXIT LIGHTS AT ROW 13 FLICKER. REMOVED AND REPLACED THE BATTERY PACK NR 3 BS 705 IAW AMM 33-51-17, 33-51-17-000-801, AND 33-51-17-400-801. OPS CHECKED GOOD IAW AMM 33-51-17-710-801.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 20,595 hrs · 13,730 cycles

SKIN DAMAGED BETWEEN FS 1015-1031 AND BETWEEN STRINGER 14R-15R. COMPLIED WITH EC/TC EO 900-53-30-00001.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 20,595 hrs · 13,730 cycles

SKIN DAMAGED BETWEEN FS 1015-1031 AND BETWEEN STR 14R-15R. C/W EC/TC EO900-53-30-00001 REV A. C/W WITH EC/TC EO900-53-30-00001

Part: LIGHT — BURNED (CABIN) · airframe 19,902 hrs · 13,278 cycles

SEVERAL PASSENGERS SAW SMOKE & FA REPORTED SMELL OF ELECTRICAL SMOKE FROM SEAT 6 A/B. REMOVED AND REPLACED THE BURNT SIDEWALL LIGHT ON SEAT 6 A/B IAW AMM 33-21-07-000-801. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 19,186 hrs · 12,775 cycles

FOUND COROSSION ON THE FLOOR SUPPORT IN FORWARD MAIN CABIN. APPLIED PERMENANT REPAIR IAW EA 32-2016-217.

Part: FRAME — CHAFED (BS 1162) · airframe 19,165 hrs · 12,760 cycles

DURING SCHEDULED MAINTENANCE DAMAGE WAS DISCOVERED IN THE AFT EQUIPMENT BAY IN THE AREA OF BS 1162 FRAME STRINGERS 7 - 8L CHAFED FROM A HYDRAULIC LINE GROUP STANDOFF. THE DAMAGE INCLUDED GOUGING OF STRINGER 6L, 7L, 7R ( AND END CAP), FRAME 1162, AND FUSELAGE SKIN BETWEEN BS 1144 AND 1162. REPAIRED IAW REOS 670-53-71-047, 690-53-61-637, 690-53-61-638, AND 690-53-61-639. MAJOR REPAIR IAW SOP5702. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: MEGAPHONE — NOT REPORTED (CABIN) · airframe 17,895 hrs · 11,850 cycles

MEGAPHONE NEEDS REPLACEMENT FOR EO 700-25-0166. R & R MEGAPHONE IAW AMM 25-61-14.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 17,890 hrs · 11,847 cycles

RIGHT ENGINE AUTO SHUTDOWN DUE TO LIGHTNING STRIKE. R & R RT ENGINE ACFT RETURN TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 17,688 hrs · 11,707 cycles

WE FOUND A SECTION OF EMERGENCY LIGHTING IN THE F/A BAG STORAGE CLOSET. THERE IS ALSO A SECTION OF EMERGENCY LIGHTING MISSING JUST FWD OF THE FORWARD LAV. RESECURED EMERGENCY LIGHT FWD CABIN BY LAV, OK IAW AMM 33-51-01.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 17,375 hrs · 11,497 cycles

FWD CARGO DOOR SEAL RETAINER DAMAGED AT LOWER FWD AND AFT CORNERS. REPAIRED DAMAGED FWD CARGO BAY SEAL RETAINER IAW EC/TC REO 690-52-35-013. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-2.

Part: MEGAPHONE — FAILED (CABIN) · airframe 16,800 hrs · 11,059 cycles

MEGAPHONE DAMAGED, R & R MEGAPHONE IAW AMM 25-61-14.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,496 hrs · 10,831 cycles

FWD PAX DOOR EXIT LIGHT COVER MISSING. REPLACED PAX DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-05. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 15,940 hrs · 10,445 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE. F/A FLASHLIGHT, OPS CHECKED GOOD IAWAMM 25-60-00.

Part: BUTTON — STUCK (CALL PANEL) · airframe 15,293 hrs · 10,026 cycles

WHILE TESTING PA CHIME, CALL EMERGENCY FUNCTIONS OF AUDIO PANEL, THE EMERGENCY BUTTON WAS STUCK AND FLASHING ON FOR 15 MINUTES BEFORE IT EXTINGUISHED ITSELF OR RESET ITSELF. OPS CK GOOD IAW AMM 33-51-00, NO DEFECTS NOTED.

Part: LIGHT — CRACKED · airframe 15,191 hrs · 9,954 cycles

EMERGENCY TRACK LIGHTING HAS SOME PHOTOLUMINSCENT LIGHTS THAT ARE DEAD AND COVERS ARE CRACKED AND WORN. REPLACED ALL COVERS AND CLEANED AND REPLACED FADED EMERGENCY FLOOR PATH LIGHT TRACKS SNAPPING COVERS INTO PLACE IAW 33-51-01-400-801-A01.

Part: FLOORBEAM — CRACKED · airframe 15,191 hrs · 9,954 cycles

FLIGHT DECK LT SIDE FLOORBEAM CRACKED ABOVE AFT FLOOR SUPPORT BRACKET. COMPLIED WITH REO 690-53-11-734, REV A. RECEIVED AND COMPLIED WITH ECTC REO 690-53-11-734.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,160 hrs · 9,933 cycles

FLOORBEAM BS 280 CORRODED RBL 6. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-10-001-001-A01, 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 15,160 hrs · 9,933 cycles

PASSENGER DOOR LOWER SILL HAS CORROSION ON LOWER ANGLE AND UPPER SILL. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21-000-A01 & SRM 51-42-06-001-001-A01.

Part: STRUCTURE — CORRODED (BS 333) · airframe 15,160 hrs · 9,933 cycles

BS 333 RBL9 PACKER CORRODED. INSTALLED NEW SERVICEABLE PACKER IAW DWG SH670-32120 & SRM 51-42-06-001-001.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 15,160 hrs · 9,933 cycles

AFT CARGO DOOR SILL CORRODED. REPAIRED IAW REO670-53-61-913 AREAS BLENDED WITHIN ALLOWABLE LIMITS. REPAIRED AFT CARGO DOOR SILL IAW REO 670-53-61-913.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK CORRODED BS 349 - 485, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-400-801, CONFIG A07 AND REO 670-53-00-014.

Part: ANGLE — CORRODED · airframe 15,191 hrs · 9,954 cycles

SERVICE DOOR SILL LOWER ANGLE CORRODED. REMOVED CORROSION ON LOWER SILL ANGLE IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-041.

Part: SEAT TRACK — CORRODED (BS 797) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK CORRODED BS 797. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A02 AND 53-00-49-400-801-802.

Part: STRUCTURE — CORRODED (BS 319) · airframe 15,189 hrs · 9,953 cycles

RT SIDE SILL CORRODED AT FS 319.70 AND RBL 40. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01, REPLACEMENT REQUIRED. REMOVED RT FLOOR SILL BETWEEN FS 280-FS 319.70 IAW SRM 51-42-06-001-001, SRM 51-42-13-001-001 AND SRM 51-42-21-001-001. LOCATED AND DRILLED NEW FLOOR SEAL IAW SRM TASK 51-40-11-001-001-A01. COMPLETED INSTALLATION OF NEW FLOOR SILL FROM STA 280-319 IAW DWG SH690-32170 AND SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,160 hrs · 9,933 cycles

COCKPIT AFT FLOORBEAM ANGLE CORRODED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-01-A01, SRM 51-42-06-001-001, DWG CC670-34095 AND SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK CORRODED. INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, REV G, AND DWG SH690-36285.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 15,160 hrs · 9,933 cycles

FLOORBEAM CORRODED AT BS 349 AND RBL 40. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK BS 847 FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-02-001-001 AND AMM 53-00-49-400-801 A07.

Part: SKIN — DENTED (PAX DOOR) · airframe 15,160 hrs · 9,933 cycles

PASSENGER DOOR LOWER CORNERS OF DOOR DENTED AND WORN RIVET LT SIDE/RT SIDE. COMPLY WITH PASSENGER DOOR SKIN AND PLATING. REPAIRED IAW SRM 52-11-01-201-004-A01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK CORRODED. INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, REV G, AND DWG SH690-36285.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK BS 847 FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 797) · airframe 15,160 hrs · 9,933 cycles

SEAT TRACK BS 797 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A07.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 15,160 hrs · 9,933 cycles

FLOOR SUPPORT CRACKED UNDER ADG STOW PUMP. REPAIRED IAW REO 670-53-11-509 AND GREO 670-53-11-509, REV B.

Part: SKIN — GOUGED (NR 2 SLAT) · airframe 15,189 hrs · 9,953 cycles

GOUGE ON LT 2 SLAT ON OTBD SIDE CAUSED BY SCREW STICHING OUT. BLENDED DAMAGE TO SMOOTH CONTOUR IAW SRM 51-12-00-001-001-A01. RECEIVED STS EA 32-2015-034 01-26-15. COMPLIED WITH PERMANMENT REPAIR OF STS EA 32-2015-034, DATED 1/26/2015. RECEIVED ECTC EA-32-2015034 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON NON-ROUNTINE WC.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 14,830 hrs · 9,722 cycles

CABIN PRESSURE WARNING, CABIN DEPRESSURIZED, ACFT RETURNED TO DEPARTURE AFTER T/O EMERGENCY ACTIONS. R & R RT SAFETY VALVE & OUTFLOW VALVE & OXYGEN GENERATORS, OK FOR SERVICE IAW AMM 21-32-03. REFER TO AIPC 21-32-03 FIG 1 ITEM 5A. & AMM 35-21-03. REFER TO AIPC 35-21-03 FIG 1J, ITEMS 50A AND 45A.

Part: LIGHT — MISSING (CABIN) · airframe 13,320 hrs · 8,698 cycles

EMERGENCY LIGHT MISSING FROM GALLEY FLOOR. REPLACED MISSING EMERGENCY LIGHT IAW AMM 33-51-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 12,087 hrs · 7,930 cycles

LEFT AFT OVER WING EMERGENCY LIGHT INOPERATIVE. R & R LT AFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51-15.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 12,087 hrs · 7,930 cycles

LEFT OVERWING AFT EXIT EMERGENCY LIGHT INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-15. REPAIRED WIRE IAW ESPM 20-17-10. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 11,799 hrs · 7,762 cycles

MEGAPHONE BATTERY INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.

Part: LIGHT — MISSING (CABIN) · airframe 11,688 hrs · 7,697 cycles

EMERGENCY ESCAPE PATH STRIP MISSING AT ROW 12CD. SECURED EMERGENCY ESCAPE LIGHTING STRIP IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 11,440 hrs · 7,546 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-15 AND REF 33-51-15, FIG 1, ITEM 22.

Part: GLOWSTRIP — MISSING (GALLEY) · airframe 10,706 hrs · 7,070 cycles

PHOTOLUMINSENT STRIP MISSING IN GALLEY. REINSTALLED GALLEY PHOTOLUMINESENT STRIP IAW AMM 33-51-01. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,069 hrs · 6,715 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS OUT. R & R LEFT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15.

Part: FLOORBEAM — CRACKED (BS 275) · airframe 10,011 hrs · 6,680 cycles

FLOORBEAM LBL 12 AT BS 275 IS CRACKED. REPAIRED IAW REO 690-53-11-471.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 10,011 hrs · 6,680 cycles

CABIN FLOOR SUPPORT CORRODED RT SIDE FS 349. REPAIRED IAW REO 690-53-21-436 AND FORMED REPAIR PARTS IAW SRM 51-24-16 AND 51-24-36.

Part: FLOORBEAM — CRACKED (BS 275) · airframe 10,010 hrs · 6,679 cycles

FLOORBEAM RBL AND LBL 12, CRACKED BS 275. COMPLIED WITH REO 690-53-11-471.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,010 hrs · 6,679 cycles

FS 280 FWD FLOORBEAM ANGLE CORRODED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001. DRILLED AND COUNTER SUNK NEW ANGLE IAW SRM 51-40-11-001-001. INSTALLED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001 AND DWG CC670-34095.

Part: WEB — CORRODED (BS 280) · airframe 10,010 hrs · 6,679 cycles

FS 280 WEB ON LT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND REO 670-53-11-594, REV-.

Part: SEAT TRACK — CORRODED (BS 744.15-752.5) · airframe 10,002 hrs · 6,674 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 744.15 - 752.5. R & R SEAT TRACK SECTION IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 744.15-752.5) · airframe 10,002 hrs · 6,674 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 744.15 - 752.50. R & R SEAT TRACK SECTION IAW SRM 51-41-02-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,002 hrs · 6,674 cycles

ASD LOWER SILL UPPER ANGLE CORRODED. REMOVED UPPER MID CAP ANGLE REF SRM 51-41-02-001-001. RECEIVED SERVICABLE ANGLE AND PICKED UP AND COUNTERSUNK ALL HOLES ON ANGLE REF SRM 51-40-11. INSTALLED NUTPLATES ON MID CAP ANGLE REF SRM 51-42-06-001-001 AND 51-42-15-001-001. INSTALLED MID CAP ANGLE ON ASD SILL REF SRM 51-42-06-001-001 AND 51-41-02-001-001 AND DWG SH670-31825.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,002 hrs · 6,674 cycles

ASD LOWER SILL CORRODED. REMOVED LOWER SILL ANGLE REF SRM 51-42-06-001-001. RESECURED NEW ANGLE AND PICKED UP HOLES AND COUNTERSUNK AS REQUIRED REF SRM 51-40-11-001-001. INSTALLED ASD LOWER ANGLE REF SRM 51-42-06-001-001 AND DWG SH670-31875.

Part: INTERCOSTAL — CORRODED (BS 342-364) · airframe 10,002 hrs · 6,674 cycles

INTERCOSTAL AT FS 342 TO 364, STR 27L CORRODED AT AFT END. REPAIRED IAW SRM 51-42-06-001-001, 53-21-23-101-003-A01, 53-21-23-100-003-A01.

Part: INTERCOSTAL — CORRODED (BS 342-364) · airframe 10,002 hrs · 6,674 cycles

INTERCOSTAL AT FS 342 TO 364, STR 27R CORRODED ART AFT END. REMOVED CORRODED INTERCOSTAL DUE TO NO DAMAGE ALLOWED. DRILLED NEW INTERCOSTAL IAW SRM 53-21-101-003-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 53-21-23-101-003-A01 & 51-42-06-001-001-A01 & DWG SH670-32075.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 10,002 hrs · 6,674 cycles

RT SIDE FLOOR SUPPORT CORRODED AT FS 280. REPAIRED IAW SRM 53-21-43-201-002-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 10,002 hrs · 6,674 cycles

FS 280 CROSSBEAM CORRODED UNDER SACRIFICIAL ANGLE ON RT SIDE. REMOVED RT CROSSSBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW CROSSBEAM ON RT SIDE IAW SRM 51-40-11-001-001. INSTALLED NEW BEAM IAW SRM 51-42-06-001-001 AND DWG CC670-34094.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 10,002 hrs · 6,674 cycles

FS 280 CROSSBEAM CORRODED UNDER SACRIFICIAL ANGLE ON LT SIDE. REMOVED CROSSSBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW CROSSBEAM IAW SRM 51-40-11-001-001. INSTALLED NEW BEAM IAW SRM 51-42-06-001-001 AND DWG CC670-34094.

Part: WEB — CORRODED (BS 208) · airframe 10,002 hrs · 6,674 cycles

FS 208 WEB ON RT SIDE OTBD EDGE CORRODED. REPAIRED IAW REO 670-53-11-594 01 AND REO 670-53-11-594 REV.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 9,443 hrs · 6,318 cycles

EMERGENCY LIGHTS ON, MESSAGE ILLUMINATED WITH SWITCH IN ARM POSITION. FOUND CIRCUIT BREAKER U3 PANEL 2 TRIPPED. RESET CIRCUIT BREAKER & OPS CHECKED GOOD. REF AMM 33-51-00. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,947 hrs · 6,005 cycles

RT OVERWING EMERGENCY EXIT LIGHT NOT WORKING. R & R EMERGENCY LIGHT ASSY IAW ESPM 20-16-05. OPS CHECKED GOOD, NO DEFECTS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,947 hrs · 6,005 cycles

LT SIDE WING EMERGENCY EXIT LIGHT NOT WORKING. R & R LT SIDE OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-15. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 8,806 hrs · 5,916 cycles

CIRCUIT BREAKER P2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE, ALL CABIN EMERGENCY LIGHTS WENT DARK AFTER 30 MINUTES LATER. RESET CIRCUIT BREAKER P2 U3 IAW FIM. NO FURTHER ACTION IS REQUIRED.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 8,806 hrs · 5,916 cycles

BREAKER BB2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE RESET CIRCUIT BREAKER. PERFORMED OPERATION TEST OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,703 hrs · 5,860 cycles

STATUS MESSAGE: EMERGENCY LIGHTS ON, BREAKER U3 TRIPPED. R & R K198 RELAY IAW ESPM 20-39-00 AND R & R PS37, PS38 AND PS43 BATTERY CHARGERS AND PS37 BATTERY IAW AMM 33-51-17-000/400-801. PERFORMED OPERATIONAL TEST OF THE EPSU IAW AMM 33-51-17-710-801 NO DEFECTS NOTED. SDR CLOSED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,964 hrs · 5,352 cycles

PAX DOOR AFT DRAG ANGLE HAS APPROX .750 INCH CRACK AT DOOR ASSIST CABLE PULLEY BRACKET. COMPLIED WITH REO 690-52-11-026 REV B TEMP REPAIR FOR ZONE 3.

Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 7,964 hrs · 5,352 cycles

MEGAPHONE MISSING BLUE TAG. R & R MEGAPHONE IAW AMM 25-61-14.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,964 hrs · 5,352 cycles

PAX DOOR AFT DRAG ANGLE HAS APPROX 1INCH CRACK AT ASSIST CABLE PULLEY BRACKET. (OPEN)

Part: LIGHT — MISSING (CABIN) · airframe 7,891 hrs · 5,298 cycles

EMERGENCY LIGHT MISSING AT SEAT 13A. INSTALLED EMERGENCY LIGHT IAW AMM 33-51-01.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 7,873 hrs · 5,287 cycles

ENROUTE, EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED, EMERGENCY LIGHT OFF STATUS MESSAGE. RESET CIRCUIT BREAKER IAW FIM RESET PROCEDURE PAGE 12,

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 7,873 hrs · 5,287 cycles

EMERGENCY LIGHTS CIRCUIT BREAKER TRIPPED 30 MINS INTO FLIGHT, EMERGENCY LIGHTS OFF STATUS MESSAGE. REPLACED AFT EMERGENCY BATTERY PACK AMM 33-51-17 AND OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 7,839 hrs · 5,258 cycles

EMERGENCY LIGHT CIRCUIT BREAKER (2U3) POPPED IN FLIGHT AND WILL NOT RESET. EMERGENCY LIGHTS CB RESET IAW FIM RESET PROCEDURE. IAW MCC, NO FURTHER ACTION IS REQUIRED.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 7,839 hrs · 5,258 cycles

EMERGENCY LIGHTS CIRCUIT BREAKER TRIPPED IN FLIGHT RESET ON GROUND AFTER LANDING. PERFORMED RESET AND OPS CHECKED IAW FIM 33-51-00. ALL CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 7,442 hrs · 5,005 cycles

EMERGENCY FLOOR LIGHTING NEAR FORWARD LAV DAMAGED. R & R EMERGENCY FLOOR PATH MARKING RIGHT AT OTBD FWD LAV DOOR REF AMM 33-51-01.

Part: LANDING GEAR — VIBRATION · airframe 6,983 hrs · 4,721 cycles

ON TAKEOFF ROLL, 105 KTS, SHIMMY WAS FELT, NO DIRECTIONAL CONTROL. CONTROL LOSS SUSPECTED, TIRE BLOWN NO ADVERSE ENGINE INDICATION. EMERGENCY DECLARED. R & R BOTH LT INBD AND OTBD MLG TIRE AND WHEEL ASSEMBLYS IAW AMM 32-41-01. AC OK FOR RETURN TO SERVICE REF REO 690-52-82-073.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,863 hrs · 4,650 cycles

DURING LC2 INSPECTION, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-51-17 & LEAK CHECKED GOOD,

Part: LIGHT — MISSING (CABIN) · airframe 6,609 hrs · 4,511 cycles

EMERGENCY LIGHT MISSING IN FRONT OF GALLEY RT CLOSET AREA. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 6,335 hrs · 4,344 cycles

EMERGENCY LIGHT ON THE SERVICE DOOR UNSECURE. R & R EMERGENCY LIGHT AND LENS ON THE SERVICE DOOR IAW AMM 33-51-05 AND IPC 33-51-05 ITEM 115 AND ITEM 360. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,154 hrs · 4,230 cycles

EMERGENCY LIGHTS AND EXTERIOR SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R NR 2 EPSU BATTERY PACK IAW MM 33-51-17-000-801-A02 AND -400-801-A02. OPS TESTED OK IAW 33-51-17-710-801-A02.

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 5,741 hrs · 3,958 cycles

ON LANDING, RIGHT INBD BRAKE WENT TO 20 AND RECEIVED A WARNING. WHEN SITTNG STILL, WENT TO 1. WHEN MOVING AGAIN IT INCREASED TO 2. EMERGENCY DECLARED, EICAS BRAKE TEMPERATURE MONITORING READOUTS - (1) PER SIDE - FOR INDICATION. R & R RT INBD HARNESS ASSY IAW AMM 32-61-05. OPS CHECKED GOOD.

Part: DETECTOR — UNSERVICEABLE (TE FLAPS) · airframe 5,677 hrs · 3,913 cycles

AFTER FLAP RETRACTION IN FLIGHT RECEIVED FLAP HALF SPEED STATUS MESSAGE, FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. (FIRE RESCUE CALLED TO STAND-BY AS A PRECAUTION) R & R LT OTBD FLAP ASSY SKEW DET IAW AMM 27-52-45. OPS CHECK GOOD IAW AMM 27-50-00. MSG CLEARED AT THIS TIME, ACFT OK FOR SERVICE. (CLOSED)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 5,245 hrs · 3,606 cycles

FLIGHT DECK CTR FLOOR PANEL, AFT CTR ANGLE/CHANNEL CORRODED FS280, SEVERAL FASTENER HOLES MISDRILLED. REMOVED 24 FASTENER HOLES BETWEEN LBL+RBL9 ON FS280 TRANSVERSE BEAM IAW SRM 51-40-11-001-001-A01. COMPLY WITH STEP 2 OF REO 690-53-11-257 THE (2) -8 RIVETS STILL NEED TO BE INSTALLED. COMPLIED WITH STEP 2 OF REO 690-53-11-257. CONFIRMED ALL STEPS OF EC/TC REO 690-53-11-257- HAVE BEEN COMPLIED WITH AS WRITTEN. ASA RII CG5500018 RII FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED · airframe 5,239 hrs · 3,602 cycles

FLIGHT DECK CTR FLOOR PANEL AFT CTR ANGLE CHANNEL HAS CORROSION FS280. FLIGHT DECK CTR FLOOR PANEL AFT CTR ANGLE CHANNEL HAS CORROSION FS280. COMPLY WITH STEP 3 OF REO690-53-11-258. COMPLIED WITH STEP 3 OF REO 690-53-11-258 NO INDICATIONS NOTED AT THIS TIME. WAITING ON EC/TC. RECEIVED EC/TC REO 690-53-11-258 AND CONFIRMED ALL STEPS HAVE BEEN COMPLIED WITH AND DOCUMENTED ACCORDINGLY. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 364) · airframe 5,238 hrs · 3,600 cycles

SEAT TRACK AT FLT STA 364.00 FWD LAV HAS CORROSION RBL9. REMOVED CORROSION AND TREATED AREA IAW REO 670-53-00-013.

Part: ANGLE — CORRODED (BS 280) · airframe 5,238 hrs · 3,600 cycles

FLIGHT DECK CENTER FLOOR PANEL AFT CTR ANGLE HAS CORROSION FS 280. REPAIRED IAW REO 690-53-11-258.

Part: ATTACH ANGLE — BROKEN (FUSELAGE) · airframe 5,238 hrs · 3,600 cycles

AT BELLY FAIRING 195DB, FOUND CTR ATTACH ANGLE TO BE BROKEN. REMOVED STIFFNER ANGLES CC690-39251-1 AND CC690-39250-1 FROM STRAP CC690-39171-5 AND REMOVED ALL NUT PLATES FROM-5 STRAP IAW SRM 51-42-13-001-001, 51-45-00-001-001. REINSTALLED STIFFNER ANGLES CC690-39250-1 TO NEW STRAP IAW SRM 51-42-13-001-001-A01 AND REINSTALLED EXISTING NUTPLATES TO NEW STRAP IAW SRM-51-42-06-001-001-A01. THIS IS A MINOR REPAIR. FABRICATE STRAP CC690-39171-5 IAW EO 900-53-0004. FABRICATED STRAP IAW EO 900-53-0004. COMPLY WITH EO 900-3-0004. COMPLIED WITH EC/TC EO 900-53-0004 IAW DWG CC690-39171 AND AMM 52-82-83. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,331 hrs · 3,018 cycles

HALF EMERGENCY CEILING LIGHTS INOP. OPS TESTED EMERGENCY EXIT LIGHTS IAW AMM 33-51-00-710-802. OPS CHECKED GOOD IAW AMM.

Part: MEGAPHONE — WEAK (CABIN) · airframe 4,170 hrs · 2,910 cycles

F/A REPORTS MEGAPHONE WEAK. R & R MEGAPHONE IAW MM 25-61-14.

Part: DOOR — BINDING (CARGO) · airframe 3,755 hrs · 2,624 cycles

RAMP UNABLE TO OPEN FWD CARGO DOOR. OPS CHECK GOOD IAW AMM 52-35-00. (CLOSED)

Part: FILTER — CONTAMINATED (RECIRC FAN) · airframe 3,706 hrs · 2,592 cycles

ODOR ON ACFT HAS MADE ENTIRE CREW NEED TO EXIT ACFT. R & R LT & RT RECIRULATION FAN FILTERS. OPS CHECKED NORMAL IAW AMM 21-22-12. (CLOSED)

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 3,706 hrs · 2,592 cycles

DURING FLIGHT, THERE IS A CHEMICAL ODOR THAT FILLS THE CABIN & COCKPIT. CHECKED AFT EQUIPMENT BAY. CHECKED GOOD. RAN NR 2 ENGINE & PACKS. NO PROBLEM NOTED AT THIS TIME IAW AMM 21-51-00.

Part: LIGHT — BROKEN (CABIN) · airframe 2,967 hrs · 2,110 cycles

EMERGENCY EXIT LIGHT OVER SERVICE DOOR BROKEN. R & R EMERGENCY LIGHT OVER SERVICE DOOR IAW MM900 33-51-00. OPS GOOD (SDR CLOSED)

Part: LIGHT — DAMAGED (CABIN) · airframe 2,852 hrs · 2,033 cycles

ABOUT 18 INCHES OF EMERGENCY LIGHTING STRIP DAMAGED IN FRONT OF GALLEY CARTS. PROTECTIVE COVER IS MISSING FROM DAMAGED AREA. R & R FLOOR EMERG LIGHTING IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: BUSS — OVERHEATED (AC SYSTEM) · airframe 1,727 hrs · 1,306 cycles

AT 35000 FT, LOUD POP AND ODOR OF SMOKE ON CAPT SIDE. THEN ESS AC BUSS FAIL. RAN QRH AND WOULD NOT TRANSFER TO GEN 2. ALSO NR1 TEN ON SYN PAGE WAS PURPLE IN COLOR AND ALL DASHES FOR KVA VOLTS AND HERTZ. BUSS NR 1 WAS ALSO PURPLE IN COLOR. LANDED DUE TO MTC.