N606LR

Part: FITTING — CRACKED (ZONE 800) · airframe 35,146 hrs · 25,330 cycles

DURING OVERNIGHT VISIT, MAINTENANCE FOUND MAIN PASSENGER DOOR AFT CAM FITTING FOR THE AFT PULL IN LEVER CRACKED. REMOVED AND REPLACED CAM FITTING, PERFROMED OPERATIONAL CHECK OF MAIN PASSENGER DOOR AND ADJUSTMENT CHECK OF THE MAIN PASSENGER DOOR IAW AMM 53-21-23 AND AMM 52-11-00

Part: FITTING — OBSTRUCTED (ZONE 100) · airframe 34,674 hrs · 24,930 cycles

WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND RH FITTING PN CC670-33562-001SB CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING RIVET PATTERN ON FS202.75 BULKHEAD. TRIMMED FITTING AND OMITTED FASTENER IAW MHIRJ REO 690-53-11-1884 REVISION - - DATED 2024-11-07.

Part: NONE — NONE (NONE) · airframe 34,674 hrs · 24,930 cycles

WHILE INCORPORATING SB 670BA-53-036/670SH-53-043 WE HAVE DISCOVERED THAT TWO FACTORY PILOT HOLES WILL NOT ALIGN WITH EXISTING HOLES FROM THE LH PRESSURE BOX @ FS 843 LBL18 AREA. OVERSIZED FASTENER HOLES AND INSTALLED ALTERNATE FASTENERS IAW MHIRJ REO 690-53-41-505 REV -- DATE 2024-11-10.

Part: HINGE — BROKEN (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

TOP FOLDING STEP HINGE PN: 601R31980-63 THAT ATTACHES THE PANEL WITH LOGO TO PAX DOOR IS BROKEN ON BOTH FORWARD AND AFT ENDS. REMOVED PAX DOOR TOP FOLDING STEP HINGE IAW CRJ900 SRM 51-42-06-001-001-A01, LOCATED, DRILLED, AND INSTALLED NEW PAX DOOR TOP STEP FOLDING HINGE PN: 601R31980-63 IAW CRJ900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

CORROSION FOUND ON STGR BETWEEN FS 611+90-677 REMOVED CORRODED STRINGER 21R FROM F.S.661+74 TO F.S.693. FABRICATED, LOCATED AND DRILLED NEW SECTION STRINGER STR21R WITH S-MATERIAL P/N B0530020BF, PO# 5-8708 BETWEEN FS661+74Ï¿½ TO FS693, IAW CRJ-900 SRM 51-40-11-001-001-A01 AND INSTALLED NEW SERVICABLE STRINGER 21R IAW CRJ 900 SRM 53-00-03-201-001-A02.

Part: FRAME — CORRODED (BS 485 S20-26R) · airframe 33,123 hrs · 23,633 cycles

FRAME AT FS 485, S20R-S26R REQUIRES REMOVAL FOR STRINGER 21R REPAIR ACCESS PERFORMED FRAME SPLICE REPAIR (TO FACILITATE NEARBY STRINGER REPAIRS) AT F.S. 485 FRAME FROM STGR 20R TO STGR 26R BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-15905 REV IR DATED 12/20/2023.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,123 hrs · 23,633 cycles

FWD LAV/WASTE DOOR CUTOUT UPPER SILL ANGLE IS CORRODED REMOVED AND INSTALLED NEW SERVICEABLE FWD LAV/WASTE DOOR CUTOUT UPPER SILL ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 P/N SH670-32285-15

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,123 hrs · 23,633 cycles

FWD LAV/WASTE CUTOUT LOWER SILL ANGLE IS CORRODED REMOVED AND INSTALLED NEW SERVICEABLE LOWER SILL ANGLE OF FWD LAV/WASTE DOOR CUTOUT IAW CRJ-900 SRM 51-42-06-001-001-A01 P/N SH670-32284-3

Part: STRINGER SPLICE — CORRODED (BS 379-394 S21R) · airframe 33,123 hrs · 23,633 cycles

STGR 21R JOINT PLATE/WASTE DOOR SURROUND IS CORRODED BETWEEN FS 379 AND FS 394 REMOVED AND INSTALLED NEW SERVICEABLE STGR 21R JOINT PLATE BETWEEN FS 379 AND FS 394 PN SH670-32301-5 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,123 hrs · 23,633 cycles

MULTIPLE SPOTS OF CORROSION FOUND ON CLOSING SKIN AROUND FWD CARGO DOOR. REPAIRED IAW ENDEAVOR EA CRJ953-15863

Part: FRAME — CORRODED (BS 379 S20-25R) · airframe 33,123 hrs · 23,633 cycles

FS 379 FRAME IS CORRODED ON AFT SIDE AT LAV WASTE CUTOUT REMOVED AND INSTALLED NEW FRAME LOCATED AT FS 379 BETWEEN STR20R TO STR25R IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (BS 409-437 S21R) · airframe 33,123 hrs · 23,633 cycles

STRINGER 21R BETWEEN F.S.409 TO F.S.437 IS CORRODED. REMOVED AND INSTALLED NEW STRINGER IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, AND CRJ900 SRM 51-42-13-001-001-A01

Part: BRACKET — CRACKED (RT SLAT TRACK) · airframe 33,123 hrs · 23,633 cycles

RH SLAT TRACK1-3 CANISTER ATTACHMENT TAB IS CRACKED (INSIDE FUEL TANK) REPAIRED IAW BOMBARDIER REO 670-57-42- 577

Part: ANGLE — CORRODED (LAVATORY) · airframe 33,123 hrs · 23,633 cycles

LAV DOOR CUTOUT IMPACT ANGLE IS CORRODED. REMOVED AND INSTALLED NEW LAV. DOOR CUTOUT IMPACT ANGLE P/N SH670-32310-1 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (BS 847-985) · airframe 33,123 hrs · 23,633 cycles

LBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 847+48 TO F.S. 985. REMOVED LBL9 SEAT TRACK BETWEEN FS847+48 - 985 IAW CRJ900 AMM 53-00-49-000-801-A07 CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE LBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS847+48 - 985 IAW CRJ900 AMM 53-00-49-400-801-A07

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 33,123 hrs · 23,633 cycles

RH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IS CRACKED JUST O/B OF THE ADG RETRACTION PUMP. REPAIRED RH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IAW CRJ 900 SRM 53-11-43-201-001-A01.

Part: FITTING — CORRODED (BS 349) · airframe 33,123 hrs · 23,633 cycles

CROSSBEAM ATTACH FITTING AT F.S.349, LBL36 IS CORRODED. REMOVED FLOOR BEAM FITTING AT FS 349, LBL 36, IAW CRJ 900 SRM 51-42-21-001-001-A01. INSTALLED NEW FLOOR BEAM FITTING PN:SH670-31942-3 AT FS 349, LBL 36, IAW CRJ 900 SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (BS 333-349 S21L) · airframe 33,123 hrs · 23,633 cycles

INTERCOSTAL AT STGR 21L FROM F.S.333 TO F.S.349 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL/BACKUP SILL P/N SH670-31823-1 IAW CRJ-900 SRM 51-40-11-001-001-A01.

Part: BRACKET — CORRODED (BS 565) · airframe 33,123 hrs · 23,633 cycles

MACHINE FITTING AT F.S.565 STGR 26R IS CORRODED. REMOVED CORRODED FITTING AND INSTALLED NEW SERVICABLE MACHINE FITTING IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 847-969) · airframe 33,123 hrs · 23,633 cycles

RBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 847+48 TO F.S. 969. REMOVED RBL9 SEAT TRACK BETWEEN FS847+48 - 969 IAW CRJ900 AMM 53-00-49-000-801-A07 CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE RBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS847+48 - 969 IAW CRJ900 AMM 53-00-49-400-801-A07

Part: BRACKET — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

F.S. 333 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 26L AND STGR 27. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: BRACKET — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

FOUND HEAVY CORROSION ON WEB FLOOR PROTECTOR ANGLES (3EA), LOCATED BETWEEN FS 319.00 TO FS 349.00. AT SERVICE DOOR SILL AREA. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 310-333 S21L)

INTERCOSTAL AT STGR 21L FROM F.S.310 TO F.S.333 IS CORRODED. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: BEAM — CRACKED (PAX DOOR) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR AFT GAS SPRING BEAM CRACKED. REMOVED CRACKED PAX DOOR AFT COUNTERBALANCE BEAM. LOCATED, MATCH DRILLED, INSTALLED NEW SERVICEABLE COUNTERBALANCE MOUNT BEAM PN 601R318011-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: BRACKET — CRACKED (BS 335) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR, BRACKET CRACKED AT FS335, UNDER PANEL 832AB. REMOVED CRACKED PAX DOOR AFT COUNTERBALANCE BEAM. LOCATED, MATCH DRILLED, INSTALLED NEW SERVICEABLE COUNTERBALANCE MOUNT BEAM PN 601R318011-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: FLOOR SKIN — CRACKED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

LH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IS CRACKED JUST O/B OF THE BRAKE ACCUMULATOR GAUGES REPAIRED LH FLOOR WEB IAW CRJ900 SRM 53-11-43-201-001-A01. MATERIAL USED FOR DOUBLER AND SHIM 2024-T3 0.040Ï¿½ PO# 5-5501, CLEAT 2024-T3 0.032Ï¿½ PO# W89584. COMPLIED WITH HFEC IAW STEP 4A(2)(F) IAW CRJ900 SRM 53-11-43-201-001-A01. NO INDICATIONS NOTED AT THIS TIME.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR INTERCOSTAL DD1 (PN: 601R318067-3) IS CORRODED. REMOVED INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.LOCATED AND DRILLED NEW SERVICEABLE PART 601R318067-5 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL PN 601R318067-5 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FORMER — CORRODED (BS 320) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR FORMER FS 320 FOUND CORRODED BETWEEN DD5 AND DD7. INSTALLED NEW SERVICEABLE FORMER PN 601R318032-5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 52-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER 20R IS CORRODED BETWEEN FS 379 AND FS 477 AT APPROX. FS 453. REPLACED CORRODED SECTION OF STGR 20R BETWEEN F.S. 421 - F.S. 477 BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-15975 REV IR DATED 1/9/2024.

Part: ANGLE — CORRODED (ZONE 600) · airframe 33,123 hrs · 23,633 cycles

RH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER (BLOW OUT PANEL) ANGLE CORRODED INSTALLED NEW SERVICEABLE RH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-2) IAW CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-15-001-001-A01

Part: STRINGER — CORRODED · airframe 33,123 hrs · 23,633 cycles

STRINGER 26R BETWEEN F.S.333 TO F.S.364 IS CORRODED REMOVED AND REPLACED STRINGER 26R FROM F.S. 333 TO F.S. 364 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,123 hrs · 23,633 cycles

RBL 12 FLIGHT COMPARTMENT FLOOR BEAM IS CRACKED AT THE FWD SIDE OF F.S. 280. REPAIRED FLIGHT COMPARTMENT FLOOR BEAM AT F.S. 280 RBL 12 IAW CRJ 900 SRM 53-11-43-201-003-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER 21R IS CORRODED BETWEEN FS 280 AND FS 333 REMOVED AND REPLACED STRINGER 21R FS 280 TO 333 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE AT STGR 24R F.S. 333 IS CORRODED. LOCATED AND DRILLED NEW STGR 24R SPLICE PN SH670-32429-4S AT FS 333 IAW CRJ900 SRM 51-40-11-001-001-A01INSTALLED STGR 24R SPLICE AT FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER 26R IS CORRODED BETWEEN FS 280 AND FS 333 REMOVED AND REPLACED STRINGER 26R BETWEEN FS 280 AND FS 333 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER 25L BETWEEN F.S.280 TO F.S.333 IS CORRODED. REMOVED AND REPLACED STRINGER 25L FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER 21R BETWEEN F.S.379 TO F.S.333 IS CORRODED. REMOVED AND INSTALLED NEW STRINGER 21R FROM FS 333 TO FS 379 IAW CRJ900 SRM 51-42-06-001-001-A01

Part: HANDLE — INOPERATIVE (E/E BAY DOOR) · airframe 33,123 hrs · 23,633 cycles

AVIONICS BAY DOOR HANDLE HOUSING FAILED NDT WITH A 100% F.S.H INDICATION AROUND 1/2 THE CIRCUMFERENCE OF THE HOUSING. REMOVED AND REPLACED AVIONICS BAY DOOR HANDLE HOUSING IAW CRJ 900 SRM 51-42-21-001-001-A01

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE 21R AT F.S.477 IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE ON F.S. 477 STGR 21R P/N SH670-33252-1, IAW CRJ900 SRM 51-42-06-001-001-A01

Part: DOOR SILL — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

AFT BAGGAGE BAY DOOR LOWER SILL CORRODED BETWEEN FS1000 AND FS1047 MULTIPLE AREAS. REMOVED AND REPLACED LOWER SILL WITH PN MM670-35655-003 BETWEEN FS1000 AND FS1047 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (COVER) · airframe 33,123 hrs · 23,633 cycles

LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER (BLOW OUT PANEL) ANGLE CORRODED. MARKED WITH ORANGE TAPE. REPLACED FOR NEW SERVICEABLE LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-1) IAW CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-15-001-001-A01 INSTALLED NEW SERVICEABLE LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-1) IAW CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-15-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-1) IAW CRJ900 SRM 51-40-11-001-001-A01 LEAK CHECK GOOD IAW CRJ-900 AMM 28-11-00-790-801-A01. NO LEAKS NOTED

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

AFT CARGO AFT TIE DOWN SUPPORT ANGLE IS CRACKED. LOCATED AND DRILLED SERVICEABLE BEAM PN MM670-35328-003 IAW CRJ900 SRM 51-40-11-001-001-A01.INSTALLED SERVICEABLE BEAM WITH PN MM670-35328-003 AT TIE DOWN PLATE IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 597-613 S21R) · airframe 33,123 hrs · 23,633 cycles

STRINGER 21R CORRODED ON UPPER SURFACE OF ATTACHED FLANGE BETWEEN FS597.00 AND FS613.00. NO DAMAGE ALLOWED ON STR 21R BETWEEN FS 597 AND FS 613, IAW CRJ-900 SRM 53-31-03-101-003-A04, STRINGER STR21R P/N: SH690-33211-3 MUST BE REPAIR OR REPLACEMENT. FABRICATED, LOCATED AND DRILLED NEW SECTION STRINGER STR21R WITH S-MATERIAL P/N B0530020BF, PO# 5-8708 BETWEEN FS581TO FS629, IAW CRJ-900 SRM 51-40-11-001-001-A01. REMOVED SECTION STRINGER STR21R BETWEEN FS581 TO FS629, IAW CRJ-900 SRM 51-42-06-001-001-A01. INSTALLED SECTION STRINGER STR21R BETWEEN FS581 TO FS629, IAW CRJ-900 SRM 51-42-06-001-001-A01. PERFORM PERMANENT REPAIR ON STR21R BETWEEN FS581 TO FS629. COMPLETED PERMANENT REPAIR ON STR21R BETWEEN FS581 TO FS629, IAW CRJ-900 SRM 53-00-03-201-001-A02.

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 24R IS CORRODED BETWEEN FS 280 AND FS 333 LOCATED AND DRILLED NEW STGR 24R PN SH670-31212-2U FROM FS 280 TO FS 333 IAW CRJ900 SRM 51-40-11-001-001-A01INSTALLED STGR 24R FROM FS 280 TO FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01 AD 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

"FLOOR SEAT TRACK AT LBL9 BETWEEN FS 349.00 AND 485.00 IS CORRODED FABRICATED REPLACEMENT LBL9 SEAT TRACK PN 670-53-00-692-1 IAW REPAIR ""B"" STEP 1A OF REO 670-53-00-589 REV -C, DATED 2022-12-19 AND INSTALLED NEW SERVICEABLE LBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS349-485 IAW CRJ900 AMM 53-00-49-400-801-A07"

Part: FRAME — CORRODED (BS 364 S26-27R) · airframe 33,123 hrs · 23,633 cycles

FS 364 LOWER FRAME SECTOR IS CORRODED ON LOWER FLANGE BETWEEN STGR 26R AND STGR 27. INSTALLED NEW FS 364 SEGMENT (P/N-SH670-32090-9) THROUGH THE SKIN IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

"CORROSION FOUND ON SEAT TRACK LBL 9 BETWEEN FS 661+32-693 FABRICATED,LOCATED AND DRILLED NEW PART P/N 670-53-00-692-1 / SH690-33405-1 IAW MHIRJ REO 670-53-00-589 REV-C DATE 2023-02-08 REPAIR ""B"" 3.B REMOVED AND REPLACED FLOOR SEAT TRACK P/N SH690-33405-1 IAW CRJ900 AMM 53-00-49-000/400-801-A07"

Part: FRAME — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

"FS 533 FRAME IS CORRODED AT STGR 17L TO 18L. FABRICATED AND DRILLED ALL REPAIR PARTS IAW CRJ900 SRM 53-00-06-201-001-A03 STEP 6E-D-G FROM 7075-0 .080"" PO W91683, S1710-4, AND REPAIR FRAME SEGMENT P/N SH690-33121-5. INSTALLED A NEW SERVICEABLE FS 533 FRAME FROM 18L TO 16L AND ALL REPAIR PARTS IAW CRJ900 SRM 53-00-06-201-001-A03. INSTALLED A NEW SERVICEABLE STGR 16L CLEAT AT FS 533 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED AND INSTALLED BUSHING (P.N. SH670-33444-S0301) USING MATERIAL AMS5659 15-5 PH H1025 (P.O. 5-2901) IAW MHIRJ SNIEO SH670-33444 IDENTIFIER S03. RE-INSTALLED CROSS BEAM FITTING AT LH FS533 FRAME IAW CRJ900 SRM 51-42-001-001-A01, AND AMM 20-51-00-400-801-A01."

Part: BRACKET — CRACKED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

"LH SLAT TRACK 1-3 CANISTER ATTACHMENT TAB IS CRACKED (INSIDE FUEL TANK). FABRICATED, LOCATED, DRILLED AND INSTALLED SERVICEABLE SUPPORT BRACKET P/N CC670-12942-1 IAW BOMBARDIER DWG NO: CC670-12942 REV. NC, BOMBARDIER REO 670-57-42-577 REV-- DATED 2016-12-02. (MADE FROM 2024-T3 .050"", PO# W91105). COMPLIED WITH ALL REMAINING STEPS AND INSTALLED REPAIR PARTS AND FABRICATED SUPPORT BRACKET (P/N CC670-12942-1) IAW BOMBARDIER REO 670-57-42-577 REV-- DATED 2016-12-02 & CRJ 900 SRM 51-42-21-001-001-A01."

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

FLOOR SEAT TRACK AT RBL9 BETWEEN FS 349.00 AND 485.00 IS CORRODED. REMOVED RBL9 SEAT TRACK BETWEEN FS349-485 IAW CRJ900 AMM 53-00-49-000-801-A07 . INSTALLED NEW SERVICEABLE RBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS349-485 IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

FLOOR SEAT TRACK AT RBL9 BETWEEN FS 485.00 AND 581.00 IS CORRODED. REMOVED RBL9 SEAT TRACK BETWEEN FS 485-581 IAW CRJ900 AMM 53-00-49-000-801-A07. INSTALLED NEW SERVICEABLE RBL9 SEAT TRACK PN 20276-288-0-0A/SH690-33407-1 BETWEEN FS 485-581 IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: ANGLE — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR CAP ANGLE IS CORRODED BETWEEN FS 319.00 AND 333.00. LOCATED AND DRILLED NEW CAP ANGLE (P/N: SH670-31825-9S) IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW CAP ANGLE (P/N: SH670-31825-9S) IAW CRJ900 SRM 51-41-02-001-001-A01. AND SRM 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

CORROSION FOUND ON FLOORBOARD FITTING AT FS 661+46 AT STGR 27 REMOVED AND REPLACED WITH NEW FLOORBOARD (PLATE) FITTING P/N SH670-34082-7 AT FS 661+46 AT STGR 27 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-15-001-001-A01, 51-45-00-001-001-A01, AND 51-42-06-001-001-A01

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE 23R AT F.S.333 IS CORRODED. REMOVED STRINGER SPLICE AT STGR 23R F.S. 333 IAW CRJ-900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW STRINGER 23R SPLICE AT F.S. 333 P/N SH670-32429-4 IAW CRJ-900 SRM 51-40-11-001-001-A01INSTALLED STGR 23R SPLICE AT FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (JACK PAD) · airframe 33,123 hrs · 23,633 cycles

L/H AND R/H FWD JACK PAD INTERCOSTALS ARE CORRODED BETWEEN F.S.265 TO F.S.280. NOSE JACK PAD FITTING SUPPORT INTERCOSTALS ARE IDENTIFIED AS P/N CC670-32179-3 (L/H) AND CC670-32179-4 (R/H) AND HAVE HEAVY CORROSION ALONG ATTACHED FLANGE. NO ALLOWABLE DAMAGE LIMITS PROVIDED IN CRJ-900 SRM. SUPPORT INTERCOSTALS REQUIRE REPLACEMENT. LOCATED AND DRILLED L/H INTERCOSTAL CC670-32179-3 AND R/H INTERCOSTAL CC670-32179-4 AT BL 0 BETWEEN FS 280 AND FS 265 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW L/H INTERCOSTAL CC670-32179-3 AND R/H INTERCOSTAL CC670-32179-4 AT BL 0 BETWEEN FS 280 AND FS 265 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

GALLEY SERVICE DOOR SILL MID CAP ANGLE IS CORRODED LOCATED AND DRILLED REPLACEMENT PART # SH670-31986-1 GALLEY SERVICE DOOR SILL MID CAP ANGLE IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED MID CAP ANGLE IAW CRJ 900 SRM 51-42-06-001-001

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 23R FROM F.S.280 TO F.S.333 IS CORRODED. LOCATED AND DRILLED NEW STRINGER 23R AT F.S. 280 - F.S. 333 P/N SH670-31211-4U IAW CRJ-900 SRM 51-40-11-001-001-A01INSTALLED NEW SERVICEABLE STRINGER 23R AT F.S. 280 - F.S. 333 P/N SH670-31211-4 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: FORMER — CORRODED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR INTERCOSTAL (PN: 601R318088-3) INSIDE THE AFT SIDE OF THE DECOMPRESSION PANEL IS CORRODED. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FORMER P/N 601R318088-3 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

FUSELAGE FRAME 319.70 AT STGR 21L IS CORRODED. INSTALLED NEW SERVICEABLE FRAME 319 PN: SH670-31891-3S BETWEEN STRINGERS 18L TO 21L IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 27 BETWEEN F.S.333 TO F.S.349 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STRINGER 27 P/N SH670-31371-3 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 27 P/N SH670-31371-3 AT F.S. 333 - F.S. 364 IAW CRJ-900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 19R BETWEEN F.S.394 TO F.S.409 IS CORRODED. DRILLED UP NEW STRINGER PN SH670-31103-4 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED NEW STGR 19R PN SH670-31103-4 IAW CRJ900 SRM 51-42-06-001-001-A01 BETWEEN FS 349 AND FS 477

Part: BRACKET — CRACKED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

WIRE HARNESS BRACKET IS BENT AND APPEARS TO BE CRACKED AT RBL 36 BETWEEN F.S. 744 TO F.S. 752. REMOVED BENT AND CRACKED WIRE HARNESS BRACKET AT RBL 36 BETWEEN F.S. 744 AND F.S. 752 AND INSTALLED REPLACEMENT WIRE HARNESS BRACKET IAW CRJ 900 SRM TASK 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 19R BETWEEN F.S.295 AND F.S.310 IS CORRODED. LOCATED AND DRILLED STRINGER 19R FS 280 - FS 319 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED STRINGER 19R FS280 - FS319 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01

Part: STRIKER — CORRODED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

GALLEY SERVICE DOOR SILL LOWER SEAL STRIKER IS CORRODED LOCATED AND DRILLED REPLACEMENT PART # SH670-31412-7 GALLEY SERVICE DOOR LOWER SEAL STRIKER IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SEAL STRIKER P/N SH670-31412-7 AT GALLEY SERVICE DOOR. IAW CRJ 900 SRM 51-42Ï¿½06-001-001-A01;.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

INTERCOSTAL 27 R/H BETWEEN F.S.349 TO F.S.364 IS CORRODED. REMOVED UNSERVICEABLE R/H LATCH PIN INTERCOSTAL RIGHT OF STGR 27 AND BETWEEN FS 364 AND FS 349 IAW CRJ 900 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LATCH PIN INTERCOSTAL P/N SH 670-32075-4S JUST RIGHT OF STGR 27 AND BETWEEN FS 364 AND FS 349 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED R/H LATCH PIN INTERCOSTAL RIGHT OF STGR 27 AND BETWEEN FS 364 AND FS 349 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 23R BETWEEN F.S.333 TO F.S.379 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STRINGER 23R AT F.S. 333 - F.S. 379 P/N SH670-31380-1S IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE STRINGER 23R AT F.S. 333 - F.S. 379 P/N SH670-31380-1 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 22R BETWEEN F.S.333 TO F.S.349 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STRINGER 22R AT F.S. 333 - F.S. 349 P/N SH670-31379-1 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED STGR 22R P/N SH670-31379-1 BETWEEN FS 333 AND FS 349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

INTERCOSTAL AT STGR 20R BETWEEN F.S.349 TO F.S.364 IS CORRODED. REMOVED CORRODED INTERCOSTAL AND DRILLED UP NEW ONE PN 670-31994-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01 INSTALLED NEW INTERCOSTAL AT STR 20R BETWEEN F.S. 349 AND F.S. 364 PN SH 670-31994-1 IAW CJR-900 SRM 51-42-06-001-001-A01

Part: FRAME — CORRODED (BS 333 S26L/R) · airframe 33,123 hrs · 23,633 cycles

FUSELAGE FRAME F.S.333 FROM STGR 26L TO STGR 26R IS CORRODED. REPAIRED FS333 LOWER FRAME SECTOR IAW CRJ 900 SRM 53-00-06-201-006-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER 26L BETWEEN F.S.333 TO F.S.364 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE 26L STRINGER PN SH670-31372-3S FS 333 TO 364 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED STRINGER 26L AT FS 333 TO 364 IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (BS 333-364 S25L) · airframe 33,123 hrs · 23,633 cycles

STRINGER 25L BETWEEN F.S.333 TO F.S.364 IS CORRODED. INSTALLED NEW LONGERON P/N SH670-32103-3S LOCATED BETWEEN FS 333 TO FS 364 AND STR 25L/H, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 477 S20R) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE 20R AT F.S.477 IS CORRODED. STRINGER 20R SPLICE AT F.S. 477 IS IDENTIFIED AS P/N SH670-33264-1 AND IS HEAVILY CORRODED. NO ALLOWABLE DAMAGE LIMITS PROVIDED IN CRJ-900 SRM. PART REQUIRES REPLACEMENT. INSTALLED NEW STRINGER 20R SPLICE AT F.S. 477 P/N SH670-33264-1, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE 21R AT F.S.333 IS CORRODED. INSTALLED NEW STRINGER SPLICE AT FS 333 AND STR 21R P/N SH670-31197-1 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001--001-A01.

Part: HINGE ARM — CHAFED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

FWD CARGO DOOR AFT LOWER HINGE ARM IS CHAFED AT SEVERAL LOCATIONS. REMOVED DAMAGE FROM FWD CARGO DOOR AFT INNER HINGE ARM BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ952-15909 REV IR DATED 12/20/2023.

Part: ANGLE — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

GALLEY SERVICE DOOR FLOOR SILL ANGLE IS CORRODED LOCATED AND DRILLED REPLACEMENT PART # SH670-31996-3S GALLEY SERVICE DOOR LOWER SILL ANGLE IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED REPLACEMENT GALLEY SERVICE DOOR LOWER SILL ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STRINGER SPLICE 22R AT F.S.333 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STRINGER 22R SPLICE AT F.S. 333 P/N SH670-32429-4 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW STGR 22R SPLICE P/N SH670-32429-4 AT FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STGR 26L IS CORRODED BETWEEN F.S. 1015 TO F.S. 1031. REPAIRED IAW ENDEAVOR EA CRJ953-15838 REV. IR DATED 12/12/23 AND EA CRJ953-15839 REV. IR DATED 12/12/23

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

STGR 21L IS CORRODED BETWEEN F.S. 985 TO F.S. 1000. COMPLIED WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-15841 REV IR DATED 12/2/2023.

Part: STRINGER — CORRODED (BS 1015-1031) · airframe 33,123 hrs · 23,633 cycles

STGR 23L IS CORRODED BETWEEN F.S. 1015 TO F.S. 1031. ENGINEERING OR REPLACEMENT REQUIRED. RECEIVED AND COMPLIED WITH EA CRJ953-15842 REV. IR DATED 12-30-2023.

Part: STRINGER — CORRODED (BS 1015-1047) · airframe 33,123 hrs · 23,633 cycles

STGR 26L IS CORRODED BETWEEN F.S. 1015 TO F.S. 1047. REPAIRED IAW ENDEAVOR EA CRJ953-15868 REV. IR DATED 12/15/2023 AND EA CRJ953-15867 REV. IR DATED 12/15/2023.

Part: PANEL — CORRODED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

PAX DOOR AFT STAIR SIDE PANEL CRACKED UNDER PANEL 832AT LOCATED, MATCH DRILLED NEW SERVICEABLE AFT STAIR WEB PN 601R317071-11S. INSTALLED NEW WEB AND SAME SERVICEABLE STIFFENERS AND COUNTERBALANCE MOUNT IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-45-00-001-001-A01

Part: BRACKET — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

BRACKET IS CORRODED FOR WASTE WATER INDICATOR DS151. INSTALLED NEW SERVICEABLE BRACKET P/N SH670-37571-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. IAW CRJ-900 SRM 51-42-06-001-001-A01.

Part: SPLICE PLATE — CORRODED (ZONE 100) · airframe 33,123 hrs · 23,633 cycles

FWD WING TO FUSELAGE FAIRING ATTACHMENT STRUCTURE AT FS 661.00+58 IS CORRODED LOCATED AND DRILLED NEW SERVICEABLE SPLICE JOINT PLATE (P/N SH670-39054-3) AT FS 661.00+58 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW SPLICE JOINT PLATE (P/N SH670-39054-3) AT FS 661.00+58 IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A01

Part: TRACK — CHAFED (ZONE 800) · airframe 33,123 hrs · 23,633 cycles

AFT CARGO DOOR FWD DOOR TRACK IS CHAFED IN TWO LOCATIONS. FIRST LOCATION CHAFE IS APPROX 0.375 LONG, 0.375 WIDE AND 0.035 DEEP, SECOND LOCATION IS 0.250 LONG, 0.250 WIDE AND 0.035 DEEP. REMOVED AND REPLACED AFT CARGO FWD DOOR TRACK P/N CC670-38725-5 IAW CRJ-900 AMM 52-31-00-000-802-A01, AMM 52-31-00-400-802-A01

Part: SUPPORT BEAM — CHAFED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

AFT CARGO DOOR SUPPORT BEAM IS CHAFED ON THE FWD AND AFT END. FIRST CHAFE IS APPROX 0.125 LONG, 0.125 WIDE, AND 0.035 DEEP. SECOND CHAFE IS APPROX 0.125 LONG, 0.125 WIDE, AND 0.025 DEEP. INSTALLED REPAIRED BEAM ASSEMBLY BETWEEN FS1000 AND FS1047, AFT BAGGAGE BAY STRUCTURE IAW CRJ900 SRM 51-42-21-001-001-A01.

Part: BRACKET — CORRODED (ZONE 200) · airframe 33,123 hrs · 23,633 cycles

GALLEY SERVICE DOOR LOWER SILL ANGLE FOR PROTECTOR PLATE ATTACHMENT MOUNT IS CORRODED BETWEEN F.S. 319 TO F.S. 333. LOCATED AND DRILLED NEW SERVICEABLE GALLEY SERVICE DOOR LOWER SILL ANGLE PROTECTOR PLATE MOUNTING WEB AND ATTACH ANGLE IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE GALLEY DOOR LOWER SILL ANGLE PROTECTOR PLATE MOUNTING WEB AND ATTACH ANGLE. IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (THRUST REVERSER) · airframe 33,123 hrs · 23,633 cycles

L/H LOWER TRANS COWLING IS LEADING EDGE IS CHAFED. CHAFE IS APPROX 3 INCHES LONG , 0.375 WIDE AND 0.045 DEEP. REPAIRED IAW ENDEAVOR AIR EA# CRJ954-15900 REV IR DATED 12/9/2023.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 33,123 hrs · 23,633 cycles

L/H VERTICAL STAB, AFT DRAG ANGLE APPEARS TO BE CRACKED IN FWD RADIUS. PERFORMED HFEC OF LH VSTAB AFT DRAG ANGLE SUSPECTED CRACK AREA IAW CRJ 900 NDTM PART 1 51-20-006-250-A01 REV 36 DATED 2/8/22. FOUND 1 INDICATION 0.5"" LONG, 100% FSH, MARKED ON PART. FAILED NDT. REPLACED L/H VERTICAL STAB AFT DRAG ANGLE P/N: AV670-21186-003 IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.

Part: BRACKET — CRACKED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR, FWD ATTACH BRACKETS ARE CRACKED. REMOVED FWD ATTACH BRACKETS CRACKED ON LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR ON FS170 IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED NEW FWD ATTACH BRACKETS ( P/N CC670-75604-2 AND P/N CC670-75604-3) ON LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR ON FS170 IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: SUPPORT — CRACKED (ZONE 900) · airframe 33,123 hrs · 23,633 cycles

"GALLEY WATER FILL LINE CLAMP SUPPORT CLIP IS CRACKED AND GUSSET IS CORRODED AT FS 349, STGR 21R. LOCATED AND DRILLED NEW FS 349 STGR 21R GUSSET IAW CRJ900 SRM 51-40-11-001-001-A01 AND FABRICATED/DRILLED NEW SUPPORT CLIP PER DRAWING NO. SH670-41519-3 FROM 2024-T3 .032"" PO# 5-5501. GUSSET AND CLIP WILL BE INSTALLED ON JOB HN00124044 SN 00626."

Part: ATTACH BRACKET — CRACKED (UNKNOWN) · airframe 33,123 hrs · 23,633 cycles

LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR, FWD ATTACH BRACKETS ARE CRACKED. REMOVED FWD ATTACH BRACKETS CRACKED ON LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR ON FS170 IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED NEW FWD ATTACH BRACKETS ( P/N CC670-75604-2 AND P/N CC670-75604-2) ON LEFT NOSE HYDRAULIC BAY SYSTEM 3 ACCUMULATOR ON FS170 IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INNER HANDLE IS CRACKED INSTALLED A NEW PAX DOOR INNER HANDLE IAW CRJ 900 SRM 51-40-11-001-001-A01, SRM 51-41-02-001-001-A01 AND 52-11-00-710-801-A02. WVAC STAMP

Part: FORMER — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PASSENGER DOOR FWD FORMER IS CORRODED AROUND LOWER LATCH CAM. REMOVED FWD FORMER AND REPLACED WITH NEW SERVICEABLE FORMER (P/N: 601R318031-5) PAX DOOR FWD SIDE IAW CRJ 900 SRM 51-42-06/21-001-001-A01 REV 37 AUG 15/2019. WVAC

Part: FORMER — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR AFT FROMER AT FS 347.27 IS CORRODED (601R318034-3). REMOVED CORRODED PAX DOOR AFT FORMER AT FS 347.27 AND REPLACED WITH NEW SERVICEABLE FORMER IAW CRJ 900 SRM 51-42-06/13/21-001-001-A01 REV 37 AUG 15/2019. WVAC

Part: FITTING — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR CLIP CORRODED (601518058-1), LOCATED ON BOTTOM CENTER INTERCOSTAL. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318058-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: CLEAT — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR CLEAT CORRODED QTY: 1 (600-31902-269). LOCATED FWD SIDE BETWEEN FROMER AND DD4. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 600-31902-269 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR AFT UPPER INTERCOSTAL P/N 6014R31902-317 CORRODED. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R31902-317 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR AFT PULL-IN CAM DOUBLER P/N 601R318094-2 CRACKED. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318094-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 37 8-15-19. WVAC

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FRAME CORRODED AT FS 313.56 DD4 AND DD5 (601R-318086-1). DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318086-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INTERCOSTAL CRACKED DD7 (601R318825-1), LOCATED AFT SIDE BOTTOM OF DOOR. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW PART P/N 601R318825-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR LOWER MID INTERCOSTAL DD7A P/N 601R318083-1 IS CORRODED. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318083-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FWD WEB STIFFENER IS CRACKED (601R317742-1) FIT, DRILLED UP & INSTALLED NEW WEB STIFFENER P/N: 601R317742-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01 REV 37 AUG15/2019. WVAC STAMP

Part: RETAINER — BENT (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR LOWER SEAL RETAINER IS BEN/GOUGED/CRACKED DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW PART P/N 601R318722-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR AFT MID INTERCOSTAL P/N 601R31902-317 CORRODED DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW PART P/N 601R31902-317 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR MID INTERCOSTAL DD3 P/N 601R318056-1 CORRODED. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318056-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 37 8-15-19. WVAC

Part: BRACKET — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FWD LWR INTERCOSTAL BRACKET P/N 601R318824-1 IS CORRODED DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318824-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: CLEAT — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR CLEATS CORRODED (QTY: 3) LOCATED AFT SIDE OF DOOR BETWEEN UPPER INTERCOSTALS (600-31902-269). DRILLED & LOCATED NEW PARTS (3EA) IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED NEW PARTS (3EA) P/N 600-31902-269 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INTERCOSTAL DD2 (601R318053-3 CORRODED, LOCATED UPPER MID CENTER OF DOOR. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318053-3 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FWD INTERCOSTAL CORRODED DD3 (601R318054-1). LOCATED 5 FROM BOTTOM OF DOOR DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 37 8-15-19, INSTALLED NEW PART P/N 601R318054-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR AFT INTERCOSTAL IS CORRODED (DD1) (601R31902-318) DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R31902-318 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FWD INTERCOSTAL DD6 (601R31902-485) CORRODED, LOCATED 2ND FROM BOTTOM. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01, INSTALLED NEW PART P/N 601R31902-485 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INTERCOSTAL CORRODED (601R31902-317), LOCATED AFT SIDE 3RD FROM BOTTOM OF DOOR DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R31902-317 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INTERCOSTAL DD3 (601R318055-1) CORRODED, LOCATED AFT SIDE FIFTH FROM THE BOTTOM OF DOOR DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318055-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR FWD BOTTOM INTERCOSTAL IS CORRODED AND BENT FLANGES, DD7 (601R318826-1). DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318826-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: SKIN — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR INNER SKIN IS CORRODED REMOVED & REPLACED PAX DOOR INNER SKIN WITH A NEW SKIN IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06/13/15/21/22-001-001-A01 AND ENDEAVOR AIR EA# CRJ952-10502 REV B 3/11/2020. WVAC STAMP

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR LWR MID INTERCOSTAL DD6 P/N 601R318057-1 CORRODED. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW PART P/N 601R318057-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 37 8-15-19. WVAC

Part: FITTING — CORRODED (PAX DOOR) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR CLIP CORRODED QTY: 1 (600-31902-275), LOCATED LOWER CENTER BY HINGE. DRILLED & LOCATED NEW PART IAW CRJ 900 SRM 51-40-11-001-001-A01 REV 378-15-19, INSTALLED NEW ALT PART P/N 601R319034-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 REV 37 8-15-19. WVAC

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

R/H FLOOR SILL AT RBL 36 IS CORRODED BETWEEN F.S. 280.00 AND FS 310.00 REPLACED CORRODED RH FLOOR SILL AT RBL 36 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-A01. WVAC STAMP EMP# 752 MTC

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

F.S. 280.00 BULKHEAD AFT SIDE AT RBL 36 HAS CORROSION REMOVED & REPLACED FS 280 RH WEB IAW CRJ 900 SRM 53-11-10-201-004-AO1 WVAC EMP# 6027

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

STRINGER 3L IS CRACKED AT F.S. 280.00 REMOVED AND INSTALLED PANEL 221GLW AND 221CLC IAW CRJ 900 AMM 25-15-04-400-801 AND 25-15-04-000-801 AND COMPLIED WITH ENDEAVOR EO# R53568 REPAIR OF STR 3L. WVAC

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

UPON REMOVAL OF FS 280 CROSSBEAM & SHEAR BOX TOP PLATE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. WVAC REMOVED & REPLACED LH FS 280 CROSSBEAM & SHEAR BOX TOP PLATE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. WVAC

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

FOUND R/H 280 BEAM TO HAVE CORROSION AROUND FASTENER HOLES REQUIRES REPLACEMENT. REMOVED & REPLACED RH 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01. 51-42-13-001-001-A01, 51-42-22-001-001-A01. WVAC

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

FS 280 BULKHEAD WEB CORRODED LH SIDE LOWER. REMOVED & REPLACED FS 280 LH WEB & CORROSION CAP IAW CRJ 900 SRM 53-11-10-201-004-AO1 & 51-42-06-001-001-A01. WVAC EMP# 6027

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

FRAME AT F.S. 319 HAS CORROSION ON THE OUTBOARD CAP AND THE WEB BETWEEN STR 26L AND STR 27 REMOVED CORRODED FRAME SEGMENT AT F.S. 319. FABBED LOCATED AND DRILLED NEW FRAME SEGMENT AND INSTALLED AT F.S. 319 IAW CRJ 900 SRM 53-00-06-201-006-A01. WVAC

Part: CHANNEL — CRACKED (FAIRING) · airframe 27,800 hrs · 19,093 cycles

FOUND AFT FAIRING CHANNEL BROKEN REMOVED & REPLACED & MODIFIED AFT FAIRING CHANNEL IAW CRJ 900 SRM 51-42-13-001-001-A01 & IS670538200021 & ENDEAVOR EO# R53573. WCAC

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,800 hrs · 19,093 cycles

PAX DOOR SURROUND UPPER SILL KICKPLATE ANGLE AND LOWER MID CAP ANGLE CORRODED. REMOVED AND REPLACED LOWER MID CAP ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,164 hrs · 17,850 cycles

EMERGENCY EXIT SIGN AT 5DC INOP. R&R EMERGENCY BATTER #2(PS36) AND CHARGER IAW AMM 33-51-17. CHECKS GOOD. OTHER PARTS REMOVED FROM A/C: BATTERY CHARGER P/N 11-0049

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,745 hrs · 17,539 cycles

SUPPLEMENTAL INFORMATION (PART AND SERIAL NUMBER ADDED) - AT 19,000 CRUISE, SMELLED FUMES BURNING FOR 1 MINUTE THEN FO WINDSHIELD OUTER SHATTERED AROUND LOWER/BURNED - SEE JOBCARD 900-56-900-901 FOR REPLACEMENT OF RIGHT WINDSHIELD SEE JOBCARD 900-56-900-901 FOR REPLACEMENT OF RIGHT WINDSHIELD - RIGHT WINDSHIELD TEMP CONTROLLER NEEDS TO BE REPLACED DUE TO WINDSHIELD ARCING - REMOVED AND REPLACED RIGHT WINDSHIELD TEMPERATURE CONTROLLER IAW AMM 30-41-06

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,814 hrs · 16,870 cycles

EMER EXIT SIGN NO LIT ON BACK SIDE ABOVE SEAT 5C DEFERRED EXIT SIGN AT 5C IAW MEL 33-51-1E PLACARDS INSTALLED MMO2 UPDATED MOC NOTIFIED 98765 RESECURED CONNECTOR P5440 AT ROW 5 O/H PANEL.SYSTEM CHECKS GOOD PER AMM 33-50-01. MMO2 CLEARED+STICKER REMOVED. MOC 95909 NOTIFIED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 24,639 hrs · 16,754 cycles

JUMPSEAT MASK FOUND TO BE LEAKY INSIDE CASE SLOWLY. R&R OBS O2 STOWAGE BOX IAW AMM 35-11-15. OPS & LEAK CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,277 hrs · 16,477 cycles

REAR FACING EMERGENCY EXIT SIGN UNDER OVERHEAD BIN 4C/D INOP. REMOVED AND REPLACED NR 1 E-LIGHT CHARGER IAW AMM 33-51-17. OPS CHECK GOOD.

Part: SIGN — MISSING (CABIN) · airframe 24,231 hrs · 16,439 cycles

EXIT SIGN OVER EXIT ROW MISSING. MAINTENANCE PROCEDURES COMPLIED WITH. INSTALLED EMERGENCY EXIT SIGN COVER IAW AMM 335107. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (CABIN/COCKPIT) · airframe 20,827 hrs · 13,924 cycles

PILOT REPORTED AN AIR RETURN FOR SMOKE IN THE CABIN & COCKPIT, BOTH AFT & FWD HAVE SMOKE. TOILET MASTER CAUTION MESSAGE. RAN QRH. INTEROGATED MDC, FOUND LAV FAN FAIL CODE B1-007306. RAN BOTH ENGINES IAW AMM 71-00-00, COULD NOT DUPLICATE SMOKE IN COCKPIT OR CABIN. OPEN

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,735 hrs · 13,861 cycles

DURING OPS CHECK OF THE CABIN EMERGENCY LIGHTS ON A SCHEDULED CHECK THE NR 3 EMERGENCY LIGHT POWER SUPPLY FAILED. MAINTENANCE MOVED TO DMIL A738356 AND OPERATED IAW MEL 33-51-01-1. MAINTENANCE R & R THE EPSU BATTERY PACK IAW AMM 33-51-17 AND OPS CHECKED GOOD. DML CLEARED AND ACFT OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 20,467 hrs · 13,642 cycles

THE EMERGENCY LIGHT HAS BROKEN OFF PINS. REMOVED AND INSTALLED NEW SERVICBALE EMERGENCY LIGHT IAW AMM'S 33-51-15-000-801-A08 AND 33-51-15-400-801-A08.

Part: STRUCTURE — DAMAGED (NR 2 SLAT) · airframe 20,467 hrs · 13,642 cycles

LEFT WING NR 2 SLAT TOP TRAILING EDGE DAMAGED. BLENDED DAMAGE ON LT WING NR 2 SLAT TOP TRAILING EDGE IAW SRM 51-12-00-001-001-A01. RECIEVED AND COMPLIED WITH REO 690-57-42-399.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,467 hrs · 13,642 cycles

FOUND PAX DOOR SILL ANGLE TO BE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A02. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 , 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: SKIN — CRACKED (PAX DOOR) · airframe 20,467 hrs · 13,642 cycles

THE INNER SKIN OF THE PAX DOOR WAS FOUND TO BE CRACKED WHEN THE FWD RISOR PANEL WAS REMOVED. REPAIRED IAW REO 690-52-11-380.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 20,467 hrs · 13,642 cycles

AVIONICS BAY DOOR HAS CORROSION AROUND ON SEAL RETAINERS FWD SIDE. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 732-744) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDE PRESSURE FLOOR SUPPORT HAS CORROSION BELOW LT FWD EMERGENCY EXIT BS 732.5 - 744.15. : BLENDED CORROSION IAW SRM TASK 51-21-06-001-001-A01. COMPLIED WITH EA 32-2016-126.

Part: LIGHT — CRACKED (CABIN) · airframe 20,467 hrs · 13,642 cycles

CABIN EMERGENCY LIGHT TRACK IS CRACKED. REPLACED THE LIGHT IAW AMM 33-51-01-400-801 A58.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 744.15 - 761.85 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A01 AND 53-00-49-400-801 A02.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDEWALL SEAT TRACK SEGEMENT BS 785.15 - 847+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07 AND 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 677 - 720.85 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49 TASK 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-047 AND 583-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDEWALL SEAT TRACK BS 847+16 - 865 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A02. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 865-969) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDEWALL SEAT TRACK SEGEMENT BS 865-969 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A02. REMOVED AND REPLACED THE THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 904-969) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 904-969 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A02 AND TASK 53-51-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDE SEAT WALL SEGEMENT BS 677-720 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-000-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 570-661) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT RAIL SEGEMENT FS570-661+16 HAS CORROSION EVALAUTED THE LEFT SIDE WALL SEAT TRACK AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-31-49 TASK 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 & 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-904) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 847+16 - 904 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02 AND 53-51-49-101-001-A02. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07 & 53-00-49-000-801 A07.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 785+15 - 847+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49 TASK 53-41-49-101-001-A02. REMOVED AND REPLACED IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL SEAT TRACK SEGEMENT BS 661+16 - 661+90 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49 TASK 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 691-836) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT TRACK SEGMENT BS 691 - 836.5 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT LIMITS IAW SRM 53-41-49 TASK 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT RACK IAW AMM 53--00-49-000-801 A07, AND AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 581 - 661+32 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: FLOOR SUPPORT — CORRODED (BS 1013-1034) · airframe 20,467 hrs · 13,642 cycles

AFT CARGO BAY LBL 27 FLOOR SUPPORT CORRODED BETWEEN BS 1013 - 1034. REPAIRED THE FLOOR SUPPORT IAW EO 900-53-0026.

Part: SEAT TRACK — CORRODED (BS 691-836) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 691 - 836.5 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-47-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-47-00-801 AND AMM 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 20,467 hrs · 13,642 cycles

CORRODED INTERCOSTAL AT STRINGER 20L BETWEEN BS 310 & 319.7. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2016-123. COMPIED WITH ECTC EA 32-2016-123.

Part: ANGLE — CORRODED · airframe 20,467 hrs · 13,642 cycles

PAX DOOR LOWER SILL KICKPLATE ANGLE CORRODED. REMOVED AND REPLACED THE KICK PLATE ANGLE IAW SRM 51-47-02-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-690) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 661+88 - 690 CORRODED AT SEVERAL AREAS. REMOVED & REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 A07 & 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT TRACK SEGMENT BS 581 - 661+32 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-801 A07, AND AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 847-988) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT TRACK SEGMENT BS 847+51 - 988 CORRODED AT SEVERAL AREAS. THE SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW AMM 53-51-40-101-001 A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07 AND 53-00-49-400-801 A07.

Part: FLOOR SUPPORT — CORRODED (BS 1053) · airframe 20,467 hrs · 13,642 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 1053. REPAIRED IAW EC/TC ROE 670-53-00-390 AND REO 670-53-00-390 REV.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 20,467 hrs · 13,642 cycles

CORRODED PACKER AT FLOORBEAM BS 333, RBL 7. REMOVED AND REPLACED IAW AMM SRM 51-42-06-001-001-A01, AND DWG SH670-32167.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 20,467 hrs · 13,642 cycles

RIGHT FLOOR SUPPORT BS 280 - 319 HAS CORRSION. THE FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 485 - 581 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 20,467 hrs · 13,642 cycles

FLOOR SUPPORT BRACKET AT BS 349, RBL 37 CORRODED. REMOVED & REPLACED THE FLOOR SUPPORT BRACKET IAW SRM 51-42-21-001-001 A01.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1034) · airframe 20,467 hrs · 13,642 cycles

AFT CARGO LBL9 FLOOR SUPPORT CORRODED BETWEEN BS 1031-1034. REPAIRED THE FLOOR SUPPORT IAW EO 900-53-0025.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 661+32 - 661+88 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801A-07.

Part: FLOOR SUPPORT — CORRODED (BS 1032) · airframe 20,467 hrs · 13,642 cycles

AFT CARGO RBL 9 FLOOR SUPPORT CORRODED BS 1032. REMOVED CORROSION BETWEEN BS 1029 - 1033 IAW SRM 51-21-06-001-001A-01. DAMAGE BEYOND THE ALLOWABLE LIMITS OF SRM 53-61-43-101-001.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 661+32 - 661+66 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801A-07.

Part: SEAT TRACK — CORRODED (BS 836-847) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT RAIL SEGMENT BS 836.50 - 847+51 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-41-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-4-400-801-A07.

Part: FLOORBEAM — CORRODED (BS 1015) · airframe 20,467 hrs · 13,642 cycles

FLOORBEAM BS 1015 CORRODED RBL 42. BLENDED CORROSION IAW SRM 51-21-056-001-001 A01.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 20,467 hrs · 13,642 cycles

TCAS DOUBLER CORRODED AT STRINGER 27 BETWEEN BS 295 & 310. REMOVED AND REPLACED TCAS DOUBLER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 847+51 - 977 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801A-07, AND AMM 53-00-49-400-801-S07.

Part: INTERCOSTAL — CORRODED (BS 319-333) · airframe 20,467 hrs · 13,642 cycles

CORRODED INTERCOSTAL AT STRINGER 20L BETWEEN BS 319.7 & 333. REMOVED THE CORROSION IAW SRM 51-21-06-001-001A-01.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 20,467 hrs · 13,642 cycles

FLOOR SUPPORT CORRODED AT BS 349 RBL 17.5. REMOVED AND REPLACED IAW SRM 51-42-21-001-001 A01.

Part: FLOOR SUPPORT — CORRODED (BS 340-364) · airframe 20,467 hrs · 13,642 cycles

FLOOR SUPPORT CORRODED AT RBL 42 BETWEEN FRAMES 340 & 364. COMPLIED WITH ECTC REO 670-53-00-0390. DAMAGE AREA FOUND TO BE BEYOND LIMITS OF REO 670-53-00-0390. RECEIVED AND COMPLIED WITH EC/TC EA 32-2016-136 REV O.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT TRACK SEGMENT BS 661+32 - 661+66 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A01 AND 53-00-49-401-801-A07.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 20,467 hrs · 13,642 cycles

COCKPIT FLOORBEAM ANGLE CORRODED AT BS 280. REMOVED AND REPLACED THE AFT SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001 A01, 51-42-11-001-001 A01 & DWG CC670-34095.

Part: SEAT TRACK — CORRODED (BS 836-847) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT FS 836.5 - 847+51 CORRODED AT SEVERAL AREAS. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: STRINGER SPLICE — CORRODED (BS 319-333) · airframe 20,467 hrs · 13,642 cycles

STRINGER 25R CORRODED BETWEEN BS 319.7 - 333. CORORISON APPEARS TO BE CONTAIN TO THE STRINGER SPLICE ONLY. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, SRM 51-42-06-001-001-A01, AND DWG S4670-32420.

Part: FRAME — CORRODED (BS 280) · airframe 20,467 hrs · 13,642 cycles

BS 280 CIRCUMPERENTIAL JOINT CORRODED BETWEEN STRINGERS 26L AND 25R. REMOVED THE CORROSION IAW SRM 51-21-06-001-001 A01 AND SRM 51-42-06-001-001 A01.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 661+16 - 661+90. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-000-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 20,467 hrs · 13,642 cycles

LBL 9 SEAT TRACK SEGMENT BS 374 - 485 CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 ,SRM 53-31-49-101-001, A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 20,467 hrs · 13,642 cycles

FLOORBEAM ANGLE AT BS 280 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PARAGRAPH 5.E AND FOUND OUT OF LIMITS. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 744.15 - 761.85 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 20,467 hrs · 13,642 cycles

RBL 9 SEAT TRACK SEGMENT BS 349.5 - 485 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 570-661) · airframe 20,467 hrs · 13,642 cycles

RIGHT SIDE WALL SEAT TRACK SEGMENT BS 570 - 661+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-000-49-400-801-A07.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,467 hrs · 13,642 cycles

INTERCOSTAL FROM BS 349-364 AT STRINGER 27 HAVE CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-0041-A01, 51-42-21-001-001-A01.

Part: STRUCTURE — CORRODED (BS 1370) · airframe 20,467 hrs · 13,642 cycles

LEFT SIDEWALL STRUCTURE HAS CORROSION AT BS 1370. REMOVED CORROSION IAW SRM 51-12-00, 51-21-06. COMPLIED WITH EA 43-2016-026.

Part: STRINGER — CORRODED (BS 333) · airframe 20,467 hrs · 13,642 cycles

STRINGER 25R CORRODED BS 333. NO DAMAGE ALLOWED IAW SRM 53-21-03-101-002-A02. REPLACED THE STRINGER FROM BS 280 - 333 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND SRM 51-72-06-001-001-A01.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,416 hrs · 13,609 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC 25-61-14, ITEM 5.

Part: TAB — DETERIORATED (HORIZONTAL STAB) · airframe 19,614 hrs · 12,989 cycles

HORIZONTAL STABILIZER PIVOT JOINT, RT ANTI ROTATION TAB HAS WEAR DAMAGE. COMPLIED WITH SB 670BA-55-012, PART B FOR REMOVAL OF ANTI-ROTATION TAB. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: MEGAPHONE — NOT REPORTED (CABIN) · airframe 19,289 hrs · 12,765 cycles

CABIN COMPARTMENT MEGAPHONE REQUIRES REPLACEMENT. R & R CABIN COMPARTMENT MEGAPHONE IAW AMM 25-61-14 AND AIPC REF 25-61-14, FIG 1, ITEM 5.

Part: LIGHT — DAMAGED (CABIN) · airframe 17,626 hrs · 11,586 cycles

LEFT AFT EMERGENCY LIGHT ASSEMBLY DAMAGED. R & R LT AFT OVER WING EMERGENCY LIGHT IAW 33-51-15. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. GATE RETURN.

Part: NONE — NONE (NONE) · airframe 17,230 hrs · 11,330 cycles

TO COMPLY WITH EC/TC EO 700-25-0166, MEGAPHONE REQUIRES REPLACEMENT. R & R MEGAPHONE IAW AMM 25-61-14. REF IPC 25-61-14, FIG 1, ITEM 5.

Part: PANEL — CRACKED (PAX DOOR) · airframe 16,470 hrs · 10,839 cycles

DAMAGE FOUND BETWEEN STOW PANEL AND TOP STEP FWD AND AFT. C/W NDT INSPECTION IAW EA 25-2014-347 IAW NDTM 51-20-006 AND FOUND A CRACK INDICATION ON AFT SIDE PANEL RUNNING FROM EDGE OF PANEL INBD APPROXIMATELY .1250". SUBMITTED DAMAGE REPORT TO STS ENGINEERING FOR CRACK INDICATION, AFT SIDE WALL, MEASURING, .150" L IAW SRM 51-13-01. RECEIVED EA 25-2014-347, REV A. ALLOWING TO STOP DRILL AFT SIDE PANEL, STOP DRILLED, .125" HOLE, TO REMOVE END OF CRACK, REFER TO MCO A241741 FOR PERMANENT REPAIR, REFER TO MCO A241745 FOR TEMP DISPOSITION VALID FOR, 4185 FLT HRS. C-CHECK.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 15,310 hrs · 10,072 cycles

SEAL RETAINER ON AFT CARGO DOOR IS DAMAGED. REPAIRED IAW REO 690-52-35-013, REV "A".

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 15,291 hrs · 10,060 cycles

GALLEY AND ENTRANCE FLOOR LEVEL EMERGENCY EXIT FLOOD LIGHTS INOPERATIVE. FOUND FUSE ON NR 1 CHARGER BAD. R & R FUSE IAW VCMM 33-21-70.

Part: LIGHT — DAMAGED (GALLEY) · airframe 15,291 hrs · 10,060 cycles

GALLEY FLOOR LEVEL EMERGENCY FLOOD LIGHT DAMAGED. R & R FLOOD LIGHT IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: SKIN — DENTED (PAX DOOR) · airframe 14,669 hrs · 9,645 cycles

ASD HAS DENT IN OUTER SKIN AT FS 340 AND APPROX WL 125.0. COMPLIED REO 690-52-11-293. MAJOR REPAIR.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 14,669 hrs · 9,645 cycles

DENT DAMAGE TO NR 1 SLAT OUTER SKIN BETWEEN SLAT TRACK 1 AND 3 AND SS 187.50. COMPLIED WITH REO 690-57-42-282, REPAIRED IAW REO 690-57-42-282 AND ECTC REO 690-57-42-282.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 14,669 hrs · 9,645 cycles

SERVICE DOOR SILL FOWARD WEB FLOOR PROTECTOR AND LOWER SILL ANGLE CORRODED. R & R LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, DWG SH670-31950.

Part: SKIN — DENTED (LT WING) · airframe 14,669 hrs · 9,645 cycles

LT WING TIP, BOTTOM DAMAGED AND DENTED. DRILLED & COUNTERSUNK NEW SKIN IAW SRM 51-40-11 & DWG CC690-15116. INSTALLED NEW LOWER LT SKIN IAW SRM 51-42-21-001-001 & DWG CC690-15010.

Part: SKIN — DAMAGED (BS 263) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND AT BS 263 S26R. COMPLIED WITH EA 26-2014-030.

Part: DOOR FRAME — CORRODED (COCKPIT DOOR) · airframe 14,669 hrs · 9,645 cycles

AT COCKPIT DOOR OPENING, LT SIDE POST CORRODED ON AFT LOWER CORNER. R & R AREA LT SIDE DOOR POST OF CORROSION AND REPLACED WITH DOUBLER IAW REO 690-53-11-650 REO 690-53-11-650.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 14,669 hrs · 9,645 cycles

LEFT COCKPIT FLOOR SUPPORT CRACKED AT BACKUP ANGLE ATTACH AREA. R & R COCKPIT FLOOR SUPPORT AT LBL 12 AND COMPLIED WITH REO 690-53-11-643, REV A. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 14,669 hrs · 9,645 cycles

RT COCKPIT FLOOR SUPPORT CRACKED. R & R RT COCKPIT FLOOR SUPPORT AT RBL 12 IAW REO 690-53-11-643 AND ECTC REO 690-53-11-643.

Part: SKIN — DAMAGED (BS 258) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKES FOUND ON SKIN AT BS 258.2 & S26R. COMPLIED WITH EA 26-2014-030.

Part: SKIN — DAMAGED (BS 273) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND ON SKIN AT FS 273.8 & S26R. COMPLIED WITH EA 12-2014-059. MAJOR REPAIR .

Part: SKIN — DAMAGED (BS 252) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND ON SKIN AT BS 252.6 & S26R. COMPLIED WITH EA 26-2014-030.

Part: SKIN — DAMAGED (BS 257) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND ON SKIN AT BS 257 & S26R. COMPLIED WITH 26-2014-030.

Part: SKIN — DAMAGED (BS 259) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND ON SKIN AT BS 259.8 & S26R. COMPLIED WITH EA 26-2014-030.

Part: SKIN — DAMAGED (BS 251) · airframe 14,669 hrs · 9,645 cycles

LIGHTNING STRIKE FOUND ON SKIN, BS 251.8 & S26R. COMPLIED WITH EA 26-2014-030.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 14,669 hrs · 9,645 cycles

FLOOR SUPPORT AT BS 349, RBL45 IS CORRODED. DRILLED NEW FLOOR SUPPORT AND INSTALLED IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31950.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 14,661 hrs · 9,641 cycles

FS 349 FLOORBEAM HAS CORRODED RBL 9. R & R IAW SRM 51-42-06-001-A01, 51-42-21-001-A01 AND DWG SH690-32120.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,661 hrs · 9,641 cycles

RT SIDE OF BS 280 FLOORBEAM IS CORRODED OUT OF LIMITS. REMOVED RT BS 280 FLOORBEAM SECTION IAW SRM 51-42-22-001-001-A01, 51-42-22-001-001-A01, AND 51-42-21-001-001-A01. LOCATED IAW SRM 51-42-06-001-001, 51-42-21-001-001, 51-42-22-001-001-A01 AND DWG CC670-34010. INSTALLED IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01 AND RESTORED FINISH A023 IAW SRM 51-21-16-001-001-A01. MAJOR REPAIR.

Part: ARM — DAMAGED (PAX DOOR) · airframe 14,661 hrs · 9,641 cycles

PAX DOORS FOLLOW UP CAM ARM BASE HAS A GOUGE & WORN FROM DOOR FRAME CONTACT. COMPLIED WITH ECTC REO 670-52-11-138 AND REO 670-52-11-138, REV A. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,661 hrs · 9,641 cycles

AFT COCKPIT FLOORBEAM CORRODED. REMOVED FLOORBEAM ANGLE FROM BS 280 IAW ARM 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-42-1-001-001-A01. INSTALLED FASTENERS IN ANGLE IAW SRM 51-42-06-001-001-A01, RESTORED FINISH IAW SRM 51-21-16-001-001-A01 AND DWG CC670-33052.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 14,661 hrs · 9,641 cycles

PAX DOOR FWD WALL & RISER BOTTOM CORNER HAS A CRACK. COMPLIED WITH REO 690-52-11-291, MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 14,661 hrs · 9,641 cycles

SEAT TRACK RBL 9 BS 661+32 - 693 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK UAW AMM TASK 53-00-49-000-801.

Part: FAIRING — CRACKED (RT NACELLE) · airframe 14,661 hrs · 9,641 cycles

RT ENGINE UPPER HINGE LINE FAIRING AFT SECTION CRACKED. REMOVED HINGE LINE FAIRING DRILLED OF ATTACHING STIFFERS TO TRANFER TO NEW SKIN & TRANFERED HOLES TO NEW SKIN IAW SRM 51-42-06-001-001-A01. COUNTERSUNK NEW SKIN & ATTACHED STIFFENERS IAW SRM 51-42-06-001-001-A01 & DWG CN624-4265. ATTACHED RUB SKIN AND RESTORED FINISH IAW SRM 51-42-06-001-A01 & 51-21-16-001-001-A01. INSTALLED SERVICEABLE HINGE LINE FAIRING 443BT REF AMM TASK 54-12-01-400-802. CLEARANCE CHECK FOUND GOOD IAW AMM 54-12-01-400-802.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 14,661 hrs · 9,641 cycles

LEFT SIDE SEAT TRACK BS 785.15 - 847+13 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-800-A07 & 53-00-49-400-800-A07.

Part: FAIRING — CRACKED (LT NACELLE) · airframe 14,661 hrs · 9,641 cycles

LT ENGINE UPPER HINGE LINE FAIRING AFT SECTION CRACKED. REMOVED LT ENGINE FARING AND REMOVED SKIN FROM ATTACHED STIFFENERS AND SEALS AND TRANSFERED TO NEW SKIN IAW SRM 57-42-06-001-001-A01 SDRWG GN624-4265. INSTALLED NEW RUB STRIP AND RESTORED A023 FINISH TO LT UPPER HINGE LINE FAIRING IAW DWG CN6 24-4265 AND SRM 51-42-06-001-001-A01. INSTALLED SERIVCABLE HINGE LINE FAIRING 433BT REF AMM TASK 54-12-01-400-802. COMPLETED CLEARENCE CHECK REF AMM TASK 54-12-01-400-802, A02, STEP 4A1C, CLEARENCE CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 14,661 hrs · 9,641 cycles

RT CABIN FLOOR SUPPORT CORRODED AT FS 280. INSTALLED FLOOR SUPPORT BETWEEN BS 280-319.7 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 14,661 hrs · 9,641 cycles

SEAT TRACK LBL 9 BS 349 - 485 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801.

Part: THRESHOLD — CORRODED (DOORWAY) · airframe 14,661 hrs · 9,641 cycles

FUSELAGE THRESHOLD AT ASD HORIZONTAL LEG CORRODED BETWEEN FS 315-340. REMOVED THRESHOLD IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. INSTALLED THRESHOLD IAW DWG SH670-31875 AND SRM 51-42-06-001-001 AND 51-42-21-001-001.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 14,661 hrs · 9,641 cycles

SEAT TRACK RBL 9 BS 349 - 485 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: THRESHOLD — CORRODED · airframe 14,661 hrs · 9,641 cycles

FUSELAGE THRESHOLD AT ASD VERTICAL LEG CORRODED AT SCREW HOLES FOR TOP STEP. R & R IAW SRM 51-42-06-001-001-A01 & DWG SH670-31825.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 14,661 hrs · 9,641 cycles

ANTENNA DOUBLER CORRODED AT STRINGER 27, BETWEEN BS 295-310. REMOVED CORRODED DOUBLER IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURED HOLES IN NEW DOUBLER IAW SRM 51-40-11-001-001-A01. INSTALLED DOUBLER IAW DWG SH 670-32-364, SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-01-001-001-A01.

Part: FIRESEAL — TORN (APU TAILPIPE) · airframe 14,659 hrs · 9,640 cycles

APU TAILPIPE FIRE SEAL TORN AT THE TOP AND BOTTOM. COMPLIED WITH ECTC REO 670-49-81-006 AND REO 670-49-81-006, REV 0 3-8-14. THIS REPAIR IS RECLASSIFIED AND A MAJOR REPAIR IAW SOP 5702.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 14,659 hrs · 9,640 cycles

FWD CARGO DOOR FWD RT CORNER HAS DAMAGE AT INNER SEAL RETAINER BENT APPROX .7500". REMOVED DAMAGED INNER SEAL & RETAINER DRILLED NEW SEAL RETAINER IAW SRM 5140-11-001-001-A01. INSTALLED SEAL RETAINER IAW AMM 52-35-07-400-802-A02. LEAK TEST OF THE FWD BAGGAGE DOOR CHECKED GOOD IAW AMM 52-00-00-790-801.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 14,659 hrs · 9,640 cycles

SERVICE DOOR SILL CORRODED ON UNDERSIDE OF PANEL. DRILLED NEW SERVICE DOOR SILL IAW SRM TASK 51-40-11-001-A01, INSTALLED SERVICEABLE DOOR SILL IAW AMM 25-33-01-000-801.

Part: DRAG ANGLE — CRACKED · airframe 14,659 hrs · 9,640 cycles

LEFT FUSELAGE TO RUDDER DRAG ANGLE CRACKED AT WHERE WL 102.50 CROSSES REAR SPAR DATUM 67.50 PERCENT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CRACKED DRAG ANGLE IAW SRM 51-42-34-001-001-A01 LOCATED DRILLED AND DEBURRED NEW DRAG ANGLE ON LT FUSELAGE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-27-001-001-A01 AND DWG BA670-35002.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 14,669 hrs · 9,645 cycles

COCKPIT FLOOR PANEL DAMAGED. R & R COCKPIT FLOOR PANEL 221ALF IAW AMM 53-00-47.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,669 hrs · 9,645 cycles

PAX DOOR AFT DRAG ANGLE CRACK MEASURING 8" LONG IN ZONE 3. REPAIRED PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 670-52-11-072. MAJOR REPAIR.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 14,669 hrs · 9,645 cycles

DENT DAMAGE TO 1 SLAT OUTER SKIN BETWEEN SLAT TRACK 1 AND 3 AND SS 187.50. REPAIRED SKIN IAW EC/TC REO 57-42-282. MAJOR REPAIR.

Part: SKIN — DAMAGED (LT WING) · airframe 14,669 hrs · 9,645 cycles

LEFT WING TIP, BOTTOM, DAMAGED AND DENTED. R & R LT WING TIP LOWER SKIN IAW SRM 51-42-13. MAJOR REPAIR.

Part: WHEEL — LACK OF LUBE (PAX DOOR) · airframe 14,121 hrs · 9,290 cycles

F/A HAD A HARD TIME OPENING THE ENTRANCE DOOR AND THE SUPPORT WHEEL DOES NOT DEPLOY. CLEANED AND LUBED SUPPORT WHEEL PAX DOOR, OPS CKS OK IAW AMM 52-11-00 ACFT OK FOR SERVICE.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 13,387 hrs · 8,843 cycles

FWD CENTER CARGO DOOR SEAL RETAINER DAMAGED AT AFT LOWER CORNER. REPAIRED IAW REO 690-52-35-013 (REV B). THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 13,065 hrs · 8,643 cycles

F/A REPORTS MISSING PHOTO ILLUMINESCENT STRIP ON GALLEY FLOOR NEXT TO GALLEY 2 WALL. INSTALLED NEW PHOTO ILLUMINESCENT STRIP NEXT TO GALLEY ON RT SIDE IAW AMM 33-51-04. NO FURTHER DEFECTS NOTED.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 13,020 hrs · 8,614 cycles

EMERGENCY LIGHT LENS ON RT SIDE OF ACFT AFT LOCATION IS CRACKED .

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 13,020 hrs · 8,614 cycles

EXTERIOR EMERGENCY LIGHT LENS, RT SIDE FWD, CRACKED. R & R RT FWD EMERGENCY LIGHT LENS AMM 33-51-17. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,756 hrs · 8,453 cycles

POSSIBLE CRACK AT PAX DOOR AFT DRAG ANGLE COMPLIED WITH GREO TEMP REPAIR ZONE 3 IAW GREO 690-52-11-026, REV E.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 12,118 hrs · 8,072 cycles

PHOTO LUMINSENT STRIP MISSING FROM OPPOSITE GALLEY COURTS. REINSTALLED PHOTO LUMINESSCENT STRIP IAW AMM 33-51-01.

Part: COVER — DAMAGED · airframe 11,674 hrs · 7,819 cycles

EMERGENCY LIGHT COVER DAMAGED IN FOWARD CABIN. REPLACED FLOOR LEVEL LIGHTING IAW AMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 11,196 hrs · 7,529 cycles

F/A NOTICED EMERGENCY LIGHT MISSING IN GALLEY. FOUND & SECURED LIGHT. CHECKED GOOD IAW AMM 25-61-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 11,153 hrs · 7,505 cycles

CENTER CABIN AFT CEILING EXIT SIGN DOES NOT ILLUMINATE. FOUND ELECTRICAL CONNECTOR NOT FULLY SEATED. CORRECTLY INSTALLED ELECTRICAL CONNECTOR ON CENTER AFT CIELING EMERGENCY EXIT SIGN IAW AMM 33-51-07, LIGHT OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 10,733 hrs · 7,259 cycles

LT SIDE EXIT LIGHT OUTSIDE INOPERATIVE. RECONNECTED LIGHT BEHIND PASSENGER SIDE WALL, OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 10,075 hrs · 6,831 cycles

MISSING FLOOR TRACK PHOTOLUMINESCENT STRIPS FROM FRONT OF FIRST CLASS CABIN TO GALLEY. RESECURED PHOTOLUMINESCENT FLOOR STRIPS IN FRONT OF FIRST CLASS CABIN IN THE GALLEY IAW AMM 33-51-01.

Part: GLOWSTRIP — MISSING · airframe 9,910 hrs · 6,721 cycles

F/A REPORTS MISSING EMERGENCY EXIT TAPE ON FLOOR IN GALLEY. INSTALLED PHOTOLUMINESCENT STRIP ON AILSLEWAY IN GALLEY AREA IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED AT THIS TIME. (SDR CLOSED)

Part: HANDLE — SEPARATED (EMERGENCY EXIT) · airframe 9,448 hrs · 6,412 cycles

EMERGENCY EXIT HANDLE AT 12D FELL OFF. RESECURED EMERGENCY EXIT HANDLE COVER IAW AMM 51-22-61.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 8,974 hrs · 6,134 cycles

MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE WITH SERVICABLE MEGAPHONE IAW AMM 25-61-14, IPC REF 25-61-14, FIG 1T ALL CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,705 hrs · 5,968 cycles

RT AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE (EXTERIOR). R & R BULB ON RT AFT OVERWING EMERGENCY LIGHT ASSY IAW AMM'S 33-51-15-000-801 AND 33-51-15-400-801.

Part: LIGHT — DAMAGED (CABIN) · airframe 8,702 hrs · 5,964 cycles

RIGHT, NR 3 EMERGENCY LIGHT CRACKED AND DAMAGED. R & R EMERGENCY LIGHTING IAW AMM 33-51-01-400-801.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

CORROSION ON FS 280 BULKHEAD WEB AT FLOOR LINE WL 72. REPAIRED IAW REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

FS 280 FLOORBEAM HAS CORROSION LEFT SIDE. REPAIRED IAW SRM 51-21-11-001-001 AND REO 690-53-10-006.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

FS 280 FLOORBEAM HAS CORROSION RT SIDE. REPAIRED IAW REO 690-53-11-006.

Part: POST — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

COCKPIT DOOR POST AT 280 CORRODED. REMOVED CORROSION IAW SRM 57-21-06-001-001-A01.

Part: POST — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

FS 280 RT DOOR POST HAS CORROSION. REMOVED CORROSION IAW SRM 57-21-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

CORROSION FS 280 BULKHEAD RT SIDE WEB CORRODED AT FLOOR LINE WL 72. REMOVED BULKHEAD WEB IAW SRM 51-42-06-01-A02. INSTALLED BULKHEAD WEB IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 744.15) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK RT SIDE FROM FS 744.15 CORRODED. REMOVED CORROSION .065" FROM INNER SIDE OF LOBE. DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-41-49-101-001. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW AMM 20-21-00 PG 204 AND 53-00-49-000-801.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

CORROSION FS 280 BULKHEAD LT SIDE WEB CORRODED AT FLOOR LINE WL 72. REMOVED LT BULKHEAD WEB IAW SRM 51-42-06-001-A01, SRM 51-42-21-002-A02 & IAW REO 670-53-11-594, STEP NOTE 1 & 2, 3. INSTALLED WEB IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 785.15-799) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK FS 785.15 TO 799 CORRODED. REMOVED .055" FROM INNER SIDE OF LOBE, DAMAGE REMOVAL OUT OF LIMITS IAW SRM 53-41-49-101-001. R & R SEAT TRACK IAW AMM 20-21-00 AND 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 744.15) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK FS 744.15 CORRODED. REMOVED CORROSION .065" FROM INNER SIDE OF LOBE. DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-41-49-101-001. REMOVED OLD SEAT TRACK AND INSTALLED NEW TRACK IAW AMM 20-21-00 AND 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 785.15-799) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK FS 785.15 TO 799 CORRODED. REMOVED .050" FROM EDGE OF LOBE DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-41-49-101-001. REMOVED OLD SEAT TRACK AND INSTALLED NEW TRACK IAW AMM 20-21-00 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-382) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK LBL 9 FORM FS 379 TO 382 HAS CORROSION. REMOVED .040" FROM SURFACE OF SEAT TRACK. DAMAGE REMOVAL IS OUT OF LIMITS IAW SRM 53-21-49, FIG 53-21-49-991-804. R & R SEAT TRACK WITH SERVICEABLE IAW AMM TASK 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-469) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK RBL9 FROM FS 349.00 TO 469.00 HAS CORROSION AND GOUGED IN FLAT AREA OF TRACK. REMOVED .025" FROM SIDE OF SURFACE OF SEAT TRACK. DAMAGE REMOVAL IS OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49-000-801 A07 & AMM 53-00-49-400-801 A07.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

FS 280 FLOORBEAM HAS CORROSION RT SIDE. CORROSION OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 8,702 hrs · 5,964 cycles

FS 280 FLOORBEAM HAS CORROSION LEFT SIDE. FOUND FLOORBEAM CRACKED BEYOND REPAIRABLE LIMITS. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01. INSTALLED FLOORBEAM IAW SRM 51-42-06-001-001.

Part: SEAT TRACK — CORRODED (BS 744.15-761.85) · airframe 8,702 hrs · 5,964 cycles

SEAT TRACK FS 744.15 TO 761.85 CORRODED. REMOVED .057" FROM INNER SIDE OF LOBE, DAMAGE REMOVAL IS OUT LIMITS IAW SRM 53-41-19-101-001. R & R SEAT TRACK IAW AMM 20-21-00 & AMM 53-00-49-400-801.

Part: DOOR — NO TEST (MAIN PAX) · airframe 8,702 hrs · 5,964 cycles

PAX DOOR FAILED PULL TEST. REQUIRED 20 LBS TO UNLOCK. COMPLIED WITH ADJUSTMENT CHECK AND FUNCTIONAL CHECK NO DEFECT NOTED FUNCTIONAL AND OP'S CHECKED GOOD IAW AMM 52-11-00-820-801 AND 52-11-00-720-802.

Part: A/C PACK — FAILED (LEFT) · airframe 8,217 hrs · 5,662 cycles

SHORT FINAL LIGHT SMOKE IN CABIN AND COCKPIT LT PACK AUTO FAIL CAUTION MESSAGE SMOKE DISSIPATED. R & R LT PACK ACM IAW AMM 21-51-08. OPS CHECK GOOD DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: LIGHT — INTERMITTENT (CABIN) · airframe 8,182 hrs · 5,636 cycles

LT FWD EMERGENCY EXIT CAUTION LIGHT INTERMITTENTLY ON TAXI IN. R & R ENTRANCE LIGHTS IAW AMM 33-23-11. OPS CHECKED GOOD.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 6,331 hrs · 4,398 cycles

RAMP PERSONNEL REPORTED THE PAX DOOR WOULD NOT OPEN. (OPEN)

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 5,967 hrs · 4,187 cycles

MEGAPHONE INOP. R & R MEGAPHONE IAW AMM 25-60-01. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 5,374 hrs · 3,784 cycles

FWD F/A FLASHLIGHT INOP. INSTALLED BATTERIES IN FWD ATTND FLASH LIGHT OPS CHECK GOOD OK IAW AMM25-60-00.

Part: DOOR — OUT OF ADJUST (CARGO) · airframe 5,045 hrs · 3,566 cycles

FWD CARGO DOOR HARD TO OPEN. REMOVED FWD CARGO DOOR IAW AMM 52-35-00. REMOVED FWD CARGO DOOR IAW AMM 52-35-00. INSTALLED SERVICEABLE FWD CARGO DOOR UP TO STEP 5 (CLOSE-OUT) ITEM D. OF INSTALLATION IAW AMM 52-35-00. COMPLIED WITH INSTALLATION OF FWD CARGO DOOR FROM STEP 5. ITEM E TO END IAW AMM 52-35-00. COMPLIED WITH ADJUSTMENT OF FWD CARGO DOOR IAW AMM 52-35-00. PERFORMED OPS TEST OF FWD CARGO DOOR IAW AMM 52-35-00. NO DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 4,967 hrs · 3,518 cycles

F/A REPORTS MEGA PHONE IS INOP. TURNED UP MEGA VOLUME, OPS CHECK GOOD IAW AMM 25-60-00.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 4,827 hrs · 3,419 cycles

FLT 5155 ABOUT 4 FEET OF PHOTOLUMINESENT EMERGENCY FLOOR LIGHT DAMAGED OR MISSING NEAR GALLEY. REPLACED EMERGENCY FLOOR STRIP REF AMM 33-51-01

Part: SHAFT — OUT OF ADJUST (CARGO DOOR) · airframe 4,532 hrs · 3,237 cycles

FWD CARGO DOOR WILL NOT OPEN. ADJUSTED FWD CARGO DOOR SLEEK SHAFT IAW AMM 52-35-00. OPS CHECK GOOD. (CLOSED)

Part: DOOR — BINDING (MAIN CARGO) · airframe 4,427 hrs · 3,157 cycles

FWD CARGO DOOR WILL NOT OPEN.

Part: DOOR — BINDING (CARGO) · airframe 4,426 hrs · 3,157 cycles

C/W OPS CHECK OF FWD CARGO DOOR. OPS CHECK GOOD IAW AMM 52-30-00. ACFT OK FOR SERVICE. (CLOSED)

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 4,324 hrs · 3,092 cycles

EXIT SIGN OVER SERVICE DOOR FELL OFF. INSTALLED EXIT SIGN COVER REF AMM 33-51-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR LATCH)

PAX DOOR LATCH CAUTION MSG. MX OPS CHECKED GOOD. (K)

Part: SWITCH — DIRTY (PAX DOOR)

PAX DOOR CAUTION MESSAGE IN FLIGHT. MX RE-REPACKED PSCU AND CLEANED SWITCHES. (K)

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR)

PASSENGER DOOR LATCH, CAUTION MESSAGE AND PROX SYS FAULT 2. OPS CHECK GOOD. (K)