N131EV

Part: HYDRAULIC LINE — LEAKING (ZONE 700) · airframe 35,014 hrs · 25,355 cycles

HYD SYSTEM 3 QUANTITY ZERO ON FINAL. PER QRH PULLED MANUAL GEAR EXTENSION. FOUND LEAK AT HYDRAULIC #3 GEAR DOWN LINE AT F.S. 355.00 AND REPAIRED LINE PER AMM 20-30-00. SERVICED HYDRAULIC #3 IAW AMM 12-12-29. LEAK CHECK GOOD. DUE TO LEAK REMOVED AND REPLACED PRESS MANIFOLD FILTER ELEMENT IAW AMM 29-12-15, CASE DRAIN FILTER ELEMENTS IAW AMM 29-12-36, AND RETURN MANIFOLD FILTER ELEMENT IAW 29-12-40 LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 34,784 hrs · 25,173 cycles

EMERG EXTERNAL LIGHT INOP REMOVED AND REPLACED EMERG EXTERNAL LIGHT IAW CRJ 900 AMM 33-51-15 OPS CHECK GOOD AT THIS TIME P/N ON/OFF 2LA006954-00

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 34,500 hrs · 24,914 cycles

DURING WALK AROUND FOUND RH EXTERNAL EMERGENCY LIGHT INOP R/R RH EXTERNAL EMERGENCY LIGHT BULB IAW CMM 33-51-02 OPS CHECK GOOD

Part: LUG — CRACKED (ZONE 800) · airframe 34,382 hrs · 24,812 cycles

R/H FORWARD EMERGENCY EXIT DOOR 843, P/N SH670-36600, S/N SB 0903 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16978 REV.IR, DATED 07/25/2024.

Part: LUG — CRACKED (ZONE 800) · airframe 34,382 hrs · 24,812 cycles

R/H AFT EMERGENCY EXIT DOOR 845, P/N SH670-36600, S/N SB 0901 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16979 REV.IR, DATED 07/25/2024.

Part: LUG — CRACKED (ZONE 800) · airframe 34,382 hrs · 24,812 cycles

L/H FORWARD EMERGENCY EXIT DOOR 835, P/N SH670-36600, S/N SB 0904 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16977 REV.IR, DATED 07/25/2024.

Part: NONE — CORRODED · airframe 29,793 hrs · 20,920 cycles

LBL 9 FLOOR BEAM IS CORRODED AT FS 661+32 - REPAIRED FLOOR BEAM AT LBL9 BETWEEN FS. 661+32 & FS. 693 IAW SNIEO SH670-33413-501 & MHIRJ REO: 690-53-31-647 & SNIEO: SH690-3340-501 REMOVED & REINSTALLED SPOT TRACK IAW CRJ900 AMM 53-00-49- 000/400-801-A07 FOR ACCESS. REMOVED & EINSTALLED SUPPORT AT AFT BULKHEAD OF FWD CARGO COMP IAW CRJ-900 SRM 51-42-06-001-001-A01, & REMOVED & REINSTALLED AIR CONDITIONING DUCT TO AVI FAN 1&2 IAW CRJ-900 AMM'S 21-24-16-000/400-802-A02 & 21-24-16-000/400-803-A02 FOR ACCESS. LEAK CHECK GOOD.

Part: FRAME — CORRODED · airframe 29,793 hrs · 20,920 cycles

FRAME AT FS 847+32 HAS MULTIPLE SPOTS OF CORROSION FROM STGR 26L TO 26R. - CORROSION REPAIRED IAW EA'S CRJ953-13109 REV IR DATED 3/24/2022, CRJ 953-13110 REV IR DATED 3/15/2022, AMM 21-23-38-000/400-804-A01, 21-23-00-790-801-A01, SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

2 INTERCOSTALS BETWEEN FS 333.00 & FS 364.00 AT STR. 20R ARE CORRODED - REMOVED AND INSTALLED WATER HOSE F.S. 333-349, CLEATS AND CANNON PLUG BRACKET, REPLACED INTERCOSTALS AND INSTALLED MOUNTING BRACKET AND APPLIED CIC IAW CRJ 900 AMM 38-32-01-400-801-A02, SRM 51-42-06-001-001 A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01 51-40-11-001-001-A01, 51-21-11-001-001-A01, AND AMM 51-80-00-760-801-A01. OPS AND LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

CONTINUATION OF JOB 81521761 OP 531; 2 INTERCOSTALS BETWEEN FS 333 AND FS 364 AT STR 20R ARE CORRODED. - REMOVED AND INSTALLED WATER HOSE F.S. 333-349, CLEATS AND CANNON PLUG BRACKET, REPLACED INTERCOSTALS AND INSTALLED MOUNTING BRACKET AND APPLIED CIC IAW CRJ 900 AMM 38-32-01-400-801-A02, SRM 51-42-06-001-001 A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01 51-40-11-001-001-A01, 51-21-11-001-001-A01, AND AMM 51-80-00-760-801-A01. OPS AND LEAK CHECKS GOOD.

Part: SPLICE — CORRODED · airframe 29,793 hrs · 20,920 cycles

22R STRINGER SPLICE AT FS 333 IS CORRODED. TCI#: 53-20-304. - REPLACED 22R STRINGER SPLICE IAW CRJ900 SRMS 51-42-06-001-001-A01 & 51-40-11-001-001-A01. REMOVED & REINSTALLED #2 DME TRANSCEIVER IAW CRJ900 AMMS 34-53-01-000/400-801-A01. OPS CHECK GOOD. REMOVED & REINSTALLED #2 GPS TRANSCEIVER IAW CRJ900 AMM 34-58-01-000/400-801-A02. OPS CHECK GOOD. REMOVED & REINSTALLED #2 DCU IAW CRJ900 AMMS 31-41-04-000/400-801-A01. OPS CHECK GOOD. REMOVED & REINSTALLED #2 MODE S TRANSPODER IAW CRJ900 AMMS 34-54-01-000/400-801-A01. OPS CHECK GOOD. AND REMOVED & REINSTALLED #2 DCU MOUNTING TRAY, #2 DME & MODE S TRANSPONDER MOUNTING TRAY & #2 GPS RECEIVER MOUNTING TRAY IAW CRJ900 AMMS 31-41-05-000/400-801-A01, 20-21-00-910-801-A01.

Part: NONE — CORRODED · airframe 29,793 hrs · 20,920 cycles

STGR 20L ATTACHMENT CLIP TO FS 295 FRAME IS CORRODED. - REPLACED CLIP AT FS 295 20L IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FRAME — CORRODED (ZONE 100) · airframe 29,793 hrs · 20,920 cycles

FS 364 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND 25R. TCI: 53-20-305 - REPAIRED FS 364 FRAME, INSTALLED AVI BAY PROX SWTICH, HYDRAULIC TUBE COVERS, INSTALLED LONGERON AT STGR 25R (FS 364-394), INSTALLED FITTINGS, AND PERFORMED EDDY CURRENT INSPECTION IAW CRJ 900 SRM 53-21-06-101-006(A02), SRM 53-21-23-201-008(A01), SRM 51-41-02-001-001(A01) AMM 29-17-00-400-801(A01) AND AMM 52-70-08-400-801(A02).

Part: FRAME — CORRODED · airframe 29,793 hrs · 20,920 cycles

FRAME AT FS1000 HAS MULTIPLE SPOTS OF CORROSION FROM STGR 24L TO 24R. - REMOVED AND INSTALLED DISTRIBUTION DUCT, REPAIRED FRAME FS 1000 24L-24R IAW CRJ 900 AMM 21-23-44-400-801-A01, CRJ 900 SRM 51-42-06-001-001-A01 AND EA CRJ 953-13089 REV A DATED 3/13/22.

Part: CLEAT — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 22R BETWEEN FS 319.70 TO FS 333 HAS 2 STRINGER CLIPS CORRODED. - FABBED CLEATS FOR 22R 319 - 333 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 53-00-06-001-001-A01, 51-40-11-001-001-A01, & DRAWINGS SH670-35625 & SH670-31253.

Part: DOOR SILL — CORRODED · airframe 29,793 hrs · 20,920 cycles

AFT BAGGAGE BAY DOOR SILL IS CORRODED BETWEEN FS 1000 TP FS 1047.00. - REPLCED SILL INSTALLED LOWER COAMING, TIEDOWN BRACKETS AND RELATED NUTPLATES AND BRACKETS AT AFT CARGO DOOR SILL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 54-42-20-001-001-A01, 51-42-13-001-001-A01, 51-25-00-001-001-A01, 51-24-26-001-0010-A01.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STGR 21R IS CORRODED BETWEEN FS 485 AND FS 501. - DISPLAYED AND REINSTALLED WIRE BUNDLE BETWEEN STGR 20R AND 22R AND BETWEEN FS 485 AND FS 501. REMOVED AND REPLACED AC CIC AND AC DCUT AND WIRING BETWEEN STGR 20R AND 21R AND FS 485 TO 51 REMOVED CORRODED SECTION OF STGR 21R FS 485. FORMED, LOCATED AND DRILLED NEW REPAIR PARTS AND INSTLLED STGR 21R SECTION AND SPLICES AND PAINTED AND APPLIED CIC IAW CRJ 900 SRM 51-41-02-001-001-A01, CRJ 900 SRM 51-21-06-001-001-A01 AND CRJ 900 SRM 53-31-03-101-013-A02, AND CRJ 900 SRM 53--03-201-001-A02.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

2 INTERCOSTALS BETWEEN FS 310.00 AND FS 333.00 AT STRINGER 20R ARE CORRODED. - REMOVED/LOCATED/DRILLED AND INSTALLED 2 SERVICEABLE INTERCOSTALS BETWEEN FS 310-333 STR 20R, ATTACHED BRACKET,WIRE BUNDLE,JB-10 MOUNTING TRAY AND CIC IAW CRJ 900 SRM 53-21-23-101-002-A02, 51-42-02-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-06/16-001-001-A01, 51-21-11-001-001-A01, AMM 24-05-01-000/400-801/802-A01, BOND CHECK GOOD, REFERENCE JOB:81521761 OP:549 FOR JB-10 OPS CHECK.

Part: FLOOR PANEL — CORRODED (FS 988-1088) · airframe 29,793 hrs · 20,920 cycles

RH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 988 TO FS 1088. - REPAIRED FLOOR SILL IAW EA CRJ 953-13092 REV IR, SRM 51-42-10-001-001-A01 AND SRM 51-25-10-001-002-A01.

Part: FLOORBEAM — CORRODED · airframe 29,793 hrs · 20,920 cycles

FLOOR BEAM AT RBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1088. - REPAIRED FLOOR BEAM RBL 27 FS 1000-FS 1088 IAW CRJ 900 SRM 51-25-01-001-001-A01, 51-41-02-001-001-A01, 53-00-41-201-001-A03, AMM 53-00-49-400 801-A07, AND EA CRJ 953-13075 REV IR 03/09/2022.

Part: FRAME — CORRODED · airframe 29,793 hrs · 20,920 cycles

FS 333 BETWEEN STR 18R AND 20R CORRODED. - WORK SUMMARY STATEMENT REQUIRED. WVAC 712 MTC 4/7/22 C/A: 9. REMOVED AND REPLACED FRAME SECTION AT FS 333 BETWEEN STGR 18R AND 20R IAW ENDEAVOR AIR EA CRJ 953-13229 REV IR DATE 4/4/2022 AND LOCATED AND DRILLED NEW GUSSET AND WATER LINE TRAY BRACKET AT FS 333 BETWEEN STGR 18R AND 20R AND INSTALLED GUSSET AND WATER LINE TRAY IAW CRJ900 SRM 51-40-11-001-001-A01, CRJ900 SRM 51-24-21-001-001-A01 AND REF DRAWING SH670-41538 REV C AND CRJ900 SRM 51-42-21-001-001-A01.

Part: NONE — CRACKED · airframe 29,793 hrs · 20,920 cycles

PASSENGER DOOR FWD AND AFT UPPER CORNERS ARE DENTED. - OUT OF LIMITS PER CRJ900 SRM 52-11-01-201-004-A01 FOR VISUAL CRACK. DRILLED & LOCATED SERVICEABLE CORNER COVER IAW CRJ900 SRM 51-401-11-001-001-A01. REF MWC JOB 81521761 OP: 561 FOR INSTALL OF FWD & AFT CORNER COVERS.

Part: RIB — CRACKED · airframe 29,793 hrs · 20,920 cycles

LEADING EDGE SKIN PANEL 522BL IS BENT NEAR FS 249.04 MARKED WITH RED TAPE - REPAIRED PROTRUDING DENT IAW ENDEAVOR EA CRJ 957-13243 REV IR & REPAIRED BROKEN RIB IAW ENDEAVOR EA CRJ 957-13204 REV IR & REMOVED TAPE

Part: NONE — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 9 FLOOR BEAM IS CORRODED AT FS 685. - REPAIRED IAW ENDEAVOR EA CRJ 953-13208 RV IR & RECEIVED, LOCATED, DRILLED , DEBURRED AND REPLACED FACTORY SPLICE IAW CRJ900 SRM'S 51-40-11-001-001-A01 & 51-42-21-001-001-A01.

Part: ANGLE — CORRODED · airframe 29,793 hrs · 20,920 cycles

FWD WATER WASTE SERVICE DOOR SURROUND DIAPHRAGM CORRODED JUST AFT OF FS 379.00, STR 23R. - REPLACED ANGLE P/N: SH670-32310-1 IAW CRJ-900 SRMS 51-40-11-001-001-A01 & 51-42-06-001-001-A01. REPAIRED DISCREPANT AREA IAW ENDEAVOR EA CRJ953-13159 REV IR DATED 3-24-2022

Part: BRACKET — CRACKED · airframe 29,793 hrs · 20,920 cycles

CABLE SUPPORT BRACKET ON FWD WEB OF PAX DOOR IS CRACKED WITH MATERIAL MISSING ON CORNER. (P/N B0816005-17359) - REMOVED AND REPLACED CABLE SUPPORT BRACKET ON FWD WEB, P/N B0816005-17359, IAW CRJ 900 SRM 51-42-13-001-001-A01.

Part: FITTING — NONE · airframe 29,793 hrs · 20,920 cycles

RH AILERON LUG MARKED "G" HAS OS BORE, REQUIRES FABRICATION OF BUSHING. - COMPLIED WITH BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.

Part: WEB — CRACKED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR FWD SIDE PANEL (WEB) FOUND TO BE CRACKED, INSIDE RADIUS BEHIND STOW CUP, & GOUGED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED FWD WEB P/N 601R317071-12 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-41-02-001-001-A01.

Part: DRAG ANGLE — NONE · airframe 29,793 hrs · 20,920 cycles

PAX DOOR AFT DRAG ANGLE HAS ELONGATED FASTENER HOLES WHERE POWER ASSIST PULLEY BRACKET ATTACHES. - REMOVED AND REPLACED AFT DRAG ANGLE P/N 601R31772-5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01

Part: DRAG ANGLE — NONE · airframe 29,793 hrs · 20,920 cycles

PASSENGER DOOR FWD DRAG ANGLE HAS TOOLING MARKS IN THE RADIUS. - REMOVED AND REPLACED FWD DRAG ANGLE P/N 601R31772-6 IAW CRJ 900 SRM 51-42-06-001-001-A01, 57-40-11-001-001-A01,AND 51-42-13-001-001-A0-A01.

Part: NONE — CRACKED · airframe 29,793 hrs · 20,920 cycles

RIBLET CRACKED ON RH L/E AILERON ASSEMBLY. - REPLACED CRACKED RIBLET ON RH AILERON IAW CRJ-900 SRMS 51-42-21-001-001-A01 & 51-40-11-001-001-A01.

Part: WEB — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR AFT WEB HAS CORROSION AT LOWER STEP AREA. - REMOVED AND REPLACED AFT WEB P/N 601R317071-11 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-02-001-001-A01.

Part: NONE — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR UPPER ANGLE AT DD7, JUST BELOW HINGE, IS CORRODED PN 601R317052-1. ALSO, FOUND CLIP ON FWD END OF ANGLE TO BE CORRODED PN 601R318058-1. - REMOVED, LOCATED, DRILLED NEW PAX DOOR UPPER ANGLE AND CLIP AND INSTALLED IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01.

Part: ANGLE — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR UPPER ANGLE AT DD7, JUST BELOW HINGE, IS CORRODED PN 601R317052-1. ALSO, FOUND CLIP ON FWD END OF ANGLE TO BE CORRODED PN 601R318058-1. - REMOVED, LOCATED, DRILLED NEW PAX DOOR UPPER ANGLE AND CLIP AND INSTALLED IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01.

Part: FORMER — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR AFT FORMER IS CORRODED. TCI: 800-07. - REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 61R318034-5 IAW CRJ 900 SRM 51-40-11-001-001-A01,51-42-06-001-001-A01,51-42-21-001-001-A01 AND 51-46-02-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STGR 20L IS CORRODED BETWEEN FS 295 TO FS 310. - REPAIRED STGR 20L FS 295-310 IAW EA CRJ953-13114 REV IR DATED 3/24/2022.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR FWD SIDE BETWEEN FS 311.750 TO FS 320.163 DD2 IS CORRODED. - REMOVED AND REPLACED INTERCOSTAL P/N 601R318051-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR INTERCOSTAL FWD SIDE BETWEEN FS 311.750 TO FS 320.163 DD3 IS CORRODED. - REMOVED AND REPLACED INTERCOSTAL P/N 601R318054-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: CLEAT — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR INTERCOSTAL DD4 IS CORRODED BETWEEN FS 329.476 TO FS 335.763. - CORROSION FOUND TO BE ONLY ON CLEAT P/N 600-31902-269 ONLY. REMOVED AND REPLACED CLEAT P/N 600-31902-269 IAW CRJ SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: BRACKET — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR FWD SIDE BETWEEN FS 311.750 TO FS 320.163 INTERCOSTAL IS CORRODED DD6. - REMOVED AND REPLACED INTERCOSTAL P/N 601R31902-485 AND BRACKET P/N 601R318084-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: CLEAT — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR AFT SIDE INTERCOSTAL DD6 ANGLE IS CORRODED BETWEEN FS 313.560 TO FS 347.250. - CORROSION FOUND TO BE ON CLEAT P/N 600-31902-269 ONLY. REMOVED AND REPLACED CLEAT P/N 600-31902-269 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 29,793 hrs · 20,920 cycles

PAX DOOR FWD SIDE BETWEEN FS 311.750 TO FS 320.163 INTERCOSTAL IS CORRODED DD6. - REMOVED AND REPLACED INTERCOSTAL P/N 601R31902-485 AND BRACKET P/N 601R318084-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 26R CORRODED BETWEEN FS 280 AND FS 364. TCI: 53-20-304 - REMOVED AND REPLACED STRINGER 26R 280-333 AND 333-364 AND FRAME CLEAT AT 333, INSTALLED CLIPS, SPLICE AND INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-16-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 26R CORRODED BETWEEN FS 280 AND FS 364. TCI: 53-20-304 - REMOVED AND REPLACED STRINGER 26R 280-333 AND 333-364 AND FRAME CLEAT AT 333, INSTALLED CLIPS, SPLICE AND INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-16-001-001-A01.

Part: JOINT — CORRODED (BS 280-364) · airframe 29,793 hrs · 20,920 cycles

STRINGER 25L IS CORRODED BETWEEN FS 280 AND FS 364. TCI: 53-20-304 - REMOVED & REPLACED STRINGER & JOINT IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: FRAME — CORRODED · airframe 29,793 hrs · 20,920 cycles

FS 549 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L - REPARIED FRAME 549 STGR 17L - 18L IAW CRJ 900 SRM 51-42-06-001-001-A01, 53-00-06-201-001-A03, 51-21-11-001-001-A01.

Part: FRAME — CORRODED · airframe 29,793 hrs · 20,920 cycles

FS 319.70 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 26L AND STGR 26R. TCI: 53-20-304 - REMOVED 4 CLEATS, REPLACED FRAME 319.70 STR 25L-23R AND INSTALLED CLEATS AND RESTORED FINISH IAW CRJ 900 SRM 53-00-06-201-006-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-16-001-001-A01.

Part: STRINGER — CORRODED (BS 280-365 S25L) · airframe 29,793 hrs · 20,920 cycles

STRINGER 25L IS CORRODED BETWEEN FS 280 AND FS 364. TCI: 53-20-304 - REMOVED & REPLACED STRINGER & JOINT IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: JOINT — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 26L IS CORRODED BETWEEN FS 280 AND FS 364, TCI: 53-20-304. - REPLACED STGR 26L 280-364 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-0A1, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-16- 001-001-A01, 51-21-11-001-001-A01, 51-25-16-001-001-A01.

Part: FLOORBEAM — CORRODED · airframe 29,793 hrs · 20,920 cycles

FLOOR BEAM AT RBL9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1070. - REPAIRED FLOOR BEAM RBL 9 F.S. 1000-1070 IAW CRJ 900 SRM 51-41-00-001-001-A01, AMM 53-00-49-400-801-A07, SRM 53-00-41-201-001-A03 AND EA CRJ 953-13076 REV A 3/9/2022.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 26L IS CORRODED BETWEEN FS 280 AND FS 364, TCI: 53-20-304. - REPLACED STGR 26L 280-364 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-0A1, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-16- 001-001-A01, 51-21-11-001-001-A01, 51-25-16-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,793 hrs · 20,920 cycles

STRINGER 26L IS CORRODED BETWEEN FS 280 AND FS 364, TCI: 53-20-304. - REPLACED STGR 26L 280-364 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-0A1, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-16- 001-001-A01, 51-21-11-001-001-A01, 51-25-16-001-001-A01.

Part: CLEAT — GOUGED · airframe 29,793 hrs · 20,920 cycles

RBL9 IB SHEAR BOX CLIP GOUGED AT FS 295. - REMOVED DAMAGE CLEAT DRILLED AND LOCATED HOLES AND INSTALLED SERVICEABLE CLEAT PART# SH690-33453-1 IAW CRJ900 SRM 51-42-21-001-001-A01 51-40-11-001-001-A01

Part: SPLICE PLATE — CORRODED · airframe 29,793 hrs · 20,920 cycles

LBL 9 FLOOR BEAM SPLICE AT FS 573 IS CORRODED. - REMOVED,FABRICATED,TREATED,PRIMED, AND PAINTED & INSTALLED SERVICEABLE SPLICE PLATE IAW CRJ-900 SRM 51-42-06-001-001-A01, 53-31- 43-001-001-A03, DRAWING #SH670-32161 REV NC, 51-21-11-001-001-A01, 51-25-06-001-001-A01 & 51-25-16-001-001-A01.

Part: SPLICE PLATE — CORRODED · airframe 29,793 hrs · 20,920 cycles

LBL 27 FLOOR BEAM SPLICE IS CORRODED AT FS 477 - REMOVED SPLICE PLATE IAW CRJ900 SRM 51-42-06-001-001-A01. FABRICATED SERVICABLE SPLICE PLATE IAW DRAWING #SH670-31775 REV NC. TREATED,PRIMED,PAINTED, INSTALLED SPLICE PLATE AND APPLIED CIC IAW CRJ900 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01, 51-42-06-001-001-A01, AND 51-21-11-001-001-A01

Part: SKIN — CHAFED · airframe 29,793 hrs · 20,920 cycles

LARGE CHAFE/DENT FOUND AFT OF SERVICE DOOR AT APPROX F.S 364.00 ON FUSELAGE SKIN. - REPAIRED I.A.W ENDEAVOR AIR EA CRJ 953-13056 REV IR DATED 3/19/22.

Part: SPLICE PLATE — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 9 FLOOR BEAM SPLICE AT FS 573 IS CORRODED. - SPLICE PLATE AT FS 573 WAS REMOVED IAW CRJ900 SRM 51-42-06-001-001-A01. CORROSION WAS REMOVED IAW CRJ900 SRM 51-21-06-001-001-A01 AND 53-31-43-101-001-A06. SERVICEABLE SPLICE PLATE WAS FABRICATED, PAINTED AND INSTALLED IAW DRAWIBG # SH680-33470 REV NC, CRJ900 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01 AND 51 51-42-06-001-001-A01.

Part: NONE — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 9 FLOOR BEAM SPLICE IS CORRODED AT FS 477. - FABRICATED REPLACEMENT SPLICE IAW DRAWING # SH690-33470 REV - NC. REMOVED & REPLACED SPLICE PLATE IAW CRJ-900 SRM 51-42-06-001-001-A01, RESTORED FINISH IAW CRJ-900 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, & 51-25-16-001-001-A01.

Part: DRAG ANGLE — CRACKED · airframe 29,793 hrs · 20,920 cycles

L/H VERTICAL STAB FWD DRAG ANGER IS CRACKED - REPAIRED IAW 55-31-00-201-001-A01 & RESTORED FINISH IAW CRJ-900 SRM'S 51-25-06-001-001-A01 & 51-25-16-001-001-A01.

Part: BRACKET — CORRODED · airframe 29,793 hrs · 20,920 cycles

FS 319 FRAME ATTACHMENT DOUBLER IS CORRODED AT STGR 17R. - REMOVED BRACKET FROM FUSELAGE 319 & REPLACED W/ NEW BRACKET. NEW BRACKET WAS DRILLED & INSTALLED FROM FS 319 STGR 17R IAW CRJ 900 SRM 51-42-20-001-001-A01 & CRJ 900 SRM 51-40-11-001-001-A01. HI LOK ON FWD SIDE FROM THE TOP WAS FOUND TO BE TOO LONG & WAS REPLACED PROPERLY IAW CRJ 900 SRM 51-42-20-001-001-(A01).

Part: SKIN — CRACKED · airframe 29,793 hrs · 20,920 cycles

PNL 443BT CRACKED - REPLACED PANEL SKIN IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-40-06-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 485 TO F.S. 565. - SEAT TRACK FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK RH SIDE BETWEEN FS 485 AND 565 IAW CRJ 900 AMM 53-00-49-000/400-801-A07

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

LBL 9 FS 581-FS 661+32 SEAT TRACK SEGMENT IS CORRODED. - REMOVED AND REPLACED SEAT TRACK AT LBL9 FS 581-661+32 IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: CLEAT — CRACKED · airframe 29,793 hrs · 20,920 cycles

LIGHTING DIVERTER ANGLE CLIP CRACKED AT LBL18 AND FS 364. - REMOVED AND REPLACED ANGLE CLIP AT LBL 18 AND FS 364 IAW CRJ 900 SRM 51-42-13-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 693 TO F.S. 708. - REMOVED & REPLACED SEAT TRACK AT 672-708 IAW CRJ-900 AMM'S 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 9 FS 581-FS 661+32 SEAT TRACK SEGMENT IS CORRODED. - FABRICATED REPLACEMENT SEAT TRACK IAW CRJ-900 SRM 53-00-49-201-002-A01. REMOVED & REPLACED SEAT TRACK IAW CRJ-900 AMM'S 53-00-49-000/400-801-A07 & 51-41-04-001-001-A01.

Part: PLATE — CORRODED · airframe 29,793 hrs · 20,920 cycles

FOUND CORROSION ON SERVICE DOOR STEP PLATE AND 2 BROKEN NUTPLATES - REMOVED CORROSION FROM SERV. DOOR STEP PLATE ORIG .063 LOSS MAT .023 REMAIN .040 FOUND OUT OF LIMITS IAW CRJ900 SRM 53-21-23-101-002-A01 AND 51-21-06-001-001-A01. LOCATED, DRILLED, AND ATTACHED NUTPLATES TO NEW STEP PLATE IAW CRJ900 SRM 51-40-11-001-001-A01, 51-45-00-001-001-A01

Part: FITTING — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 18, F.S. 280 TO F.S. 282 GALLEY MOUNT FITTING IS CORRODED. - R/R GALLEY MOUNT FITTING @ RBL 18 FS 280 TO FS 282 IAW CRJ-900 SRM 51-42-21-001-001-A01 & LOCATED AND DRILLED IAW CRJ-900 SRM 51-40-11-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

SEAT TRACK AT FS 364-477 LBL 27 HAS MULTIPLE SPOTS OF CORROSION - CORROSION ON FLOOR SEAT TRACK LBL 27 FS 364 TO 477 FOUND TO BE IN A DAMAGE ALLOWED AREA AND REQUIRES REPLACEMENT IAW CRJ 900 SRM 53- 21-49-101-001-A01 R/R LBL 27 @ FS 364-477 SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

RBL 9 FS 661+32-FS 693 SEAT TRACK SEGMENT IS CORRODED. - FABRICATED AND INSTALLED NEW SEAT TRACK FROM EXTRUSION MAT. 20276-288-0-0A IAW INSTRUCTIONS CRJ-900 SRM 53-00-49-201-002-A01 AND AMM 53-00- 49-400-801 A07

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

LBL 9 FS 661+32- FS 693 SEAT TRACK SEGMENT IS CORRODED. - FABRICATED AND INSTALLED NEW SEAT TRACK FROM EXTRUSION MAT. 20276-288-0-0A IAW CRJ-900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-801 A07

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 661+16 TO F.S. 677 - INSTALLED NEW RH SIDE SEAT RAIL AT FS 661.0+16" TO FS 677.0 IAW CRJ-900 AMM 53-00-49-400-801-A07

Part: NONE — CHAFED · airframe 29,793 hrs · 20,920 cycles

L/H WING I/B FLAP VANE CAP 584ET HAS CHAFE DAMAGE - REMOVED CHAFE DAMAGE ON FLAP VANE CAP; FOUND TO BE OUT OF LIMITS, DRILLED NEW PART AND PAINTED IAW CRJ-900 SRM 51-12-00-001-001-A01, 57-52-01-101-001-A01, 51-25-01-001-001-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 29,793 hrs · 20,920 cycles

SEAT TRACK AT FS 349-477 RBL9 HAS MULTIPLE SPOTS OF CORROSION - REMOVED & REPLACED RBL 9 SEAT TRACK & SEAT TRACK FITTING ASSYS (3EA.) FROM FS 349-FS 477 IAW CRJ-900 AMM 53-00-49-400-801-A07, 53-00-49-000-801-A07 AND SRM 57-41-02-001-001-A01.

Part: ANGLE — CRACKED · airframe 29,793 hrs · 20,920 cycles

RBL 9 OUTBOARD CLIP AT F.S. 280 IS CRACKED. - REMOVED AND REINSTALLED RH DRIP TRAY, REPLACED O/B CLIP AT 2PO RBL9 IAW CRJ 900 SRM 51-42-13-001-001-A01. 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-21-16-001-001-A01 AND 51-21-11-001-001-A01. WVAC EMP STAMP # 711 MTC. INSTALLED R/H DRIP TRAY DRAIN TUBE CLAMPS AND TIEDOWN STRAPS IAW CRJ 900 AMM 53-20-48-400-801(A06).

Part: PIN — MISSING (PAX DOOR) · airframe 28,901 hrs · 20,147 cycles

PAX DOOR WOULD NOT OPEN FROM INSIDE THE AIRCRAFT. RAMPERS HAD TO OPEN FROM THE OUTSIDE. INSP DOOR FOUND VENT DOOR ATTACH CABLE END MISSING HARDWARE. REF CRJ 900 IPC 52-11-15 FIG 1A ITEM 85, 90, 97. REPLACED HARDWARE PERFORMED OPS CHECK IAW CRJ 900 AMM 52-11-00-710-801. OPS CHECK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 27,882 hrs · 19,277 cycles

CABIN EMERGENCY LIGHTS INOPERABLE, SOME WORKED, MOST FORWARD LIGHTS FLASHED THEN WENT OUT. REMOVED & REPLACED EMERGENCY POWER SUPPLY UNITS (X4), IAW CRJ-900 AMM 33-51-17. PERFORMED OPERATIONS CHECK, OPERATIONS CHECK GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 26,292 hrs · 17,969 cycles

F/A REPORTS EMERGENCY EXIT LIGHTS NEAR GALLEY DOOR INOP OPERATIONAL CHECKS ON EMERGENCY EXIT LIGHT IAW CRJ 900 AMM 33-51-05 OPS CHECKS GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,112 hrs · 15,608 cycles

EMERGENCY LIGHTS IN THE RT GALLEY, THE BULBS WERE INOPERATIVE. R & R THE BULBS. OP CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — DISCONNECTED (C/P FLASHLIGHT) · airframe 22,825 hrs · 15,398 cycles

PILOT`S FLASHLIGHT WAS FOUND INOPERATIVE. ON FURTHER INVESTIGATION, FOUND THE BATTERY IN THE FLASHLIGHT WAS FOUND DISCONNECTED, CONNECTED THE FLASHLIGHT BATTERY IAW CMM 25-60-02, REV 10-21-18, PAGE 7003.

Part: STIFFENER — CRACKED (NOT REPORTED) · airframe 22,825 hrs · 15,398 cycles

PANEL 171CL AFT UPPER STIFFINER CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-02.

Part: PANEL — CRACKED (NOT REPORTED) · airframe 22,825 hrs · 15,398 cycles

AFTER REMOVING A DAMAGED STIFFENER, FOUND A CRACK ON PANEL 171CL. REMOVED AND REPLACED THE PANEL IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 1015) · airframe 22,825 hrs · 15,398 cycles

CORROSION FOUND ON THE FLOOR SUPPORT AT LBL 9, BS 1015. REPAIRED FROM BS 1006 TO 1039 IAW GREO 670-53-00-029, REV A, FIG 13.

Part: RETAINER — CRACKED (TE FLAP SEAL) · airframe 22,825 hrs · 15,398 cycles

PANEL 697 BB HAS CRACKED RETAINER . REMOVED AND REPLACED THE RETAINER IAW SRM 51-42-13.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 22,825 hrs · 15,398 cycles

PAX DOOR FWD FRAME IS CORRODED AT THE LATCH CAMS. REMOVED AND REPLACED THE PAX DOOR FWD FRAME IAW SRM 51-42-06, AND SRM 51-42-21.

Part: FRAME — CRACKED (BS 333) · airframe 22,825 hrs · 15,398 cycles

FOUND THE BS 333 FRAME CRACKED, BETWEEN STRINGERS 2R AND 3R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-11, SRM 51-42-21, AND SRM 51-42-06.

Part: STRINGER — CORRODED (BS 319.7-333) · airframe 22,825 hrs · 15,398 cycles

STRINGER 27 BETWEEN BS 319.7 AND 333 FOUND CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, AND 51-42-21.

Part: RISER — CRACKED (PAX DOOR) · airframe 22,825 hrs · 15,398 cycles

PAX DOOR AFT RISER IS CRACKED BY THE HANDRAIL RECEPTACLE. REPAIRED THE RISER IAW SRM 52-11-04.

Part: STRINGER — CORRODED (BS 319.7-333) · airframe 22,825 hrs · 15,398 cycles

STRINGER 27, BETWEEN BS 319.7 AND 333 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (PASSENGER DOOR) · airframe 22,825 hrs · 15,398 cycles

WHILE REPLACING THE PAX DOOR INNER SKIN FOUND THE UPPER AFT INTERCOSTAL CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 22,825 hrs · 15,398 cycles

WHILE REPLACING THE PAX DOOR INNER SKIN, FOUND UPPER, FWD INTERCOSTAL CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND SRM 51-42-21.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 22,671 hrs · 15,293 cycles

FWD LAVATORY, SMOKE POSTED AT 3500 FEET MSL.STOPPED WHEN THE FIRST OFFICER CLOSED THE LAVATORY DOOR. THE LAVATORY DOOR WAS OPEN WHEN ALARM BEGAN. OPS CHECKED THE SMOKE DETECTER IAW 26-16-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 22,668 hrs · 15,290 cycles

OXYGEN MASKS IN THE CABIN DEPLOYED INFLIGHT. INSPECTED, CLEANED, REPLACED, REPACKED & STOWED THE MASKS & GENERATORS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 22,668 hrs · 15,290 cycles

SMOKE FWD LAVATORY LIGHT ANNUNCIATOR DURING APPROACH. RAN QRH, LIGHT AND WARNING EXTINGUISHED WITH CIRCUIT BREAKER 1B PULLED IAW QRH. DO NOT BELIEVE FAN IS ACTUALLY BAD. PERFORMED AN OPS TEST OF THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00. CHECKED THE GALLEY & LAVATORY FAN AND GALLEY & LAVATORY LIGHTING. NO DEFECTS. ALL SYSTEMS NORMAL, RESET THE CIRCUIT BREAKER.

Part: FAN — FAILED (EXHAUST) · airframe 22,574 hrs · 15,227 cycles

PILOT REPORTED 80 MILES OUT AFT LAVATORY SMOKE DETECTOR WARNING MESSAGE APPEARED. PULLED B1 CODES FROM MDC:007306&006902. REMOVED AND REPLACED BOTH GALLEY AND LAVATORY EXHAUST FANS IAW AMM 21-23-93. REMOVED AND REPLACED AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS TESTED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,320 hrs · 15,035 cycles

CREW REPORTED CEILING EXIT SIGN FORWARD LIGHTS INOP. MX REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER ASSY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: DISCONNECT UNIT — STUCK (LT MLG BRAKE) · airframe 21,559 hrs · 14,474 cycles

AFTER LANDING LEFT INBOARD BRAKE BECAME STUCK. REMOVED AND REPLACED THE LT INBD BRAKE DISSCONNECT FITTING IAW AMM32-43-26 OPS TESTED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 21,228 hrs · 14,218 cycles

FS 295 FRAME HAS CORROSION BETWEEN STR 25R - 24R. BLENDED CORROSION AT FS 295 AND BETWEEN STR 25R TO 24R AND FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 51-21-06-101-002-A04. REPAIRED THE CORRODED AREA IAW REO 670-53-21-1281 AND EC/TC REO 670-53-21-1281. THIS IS A MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,228 hrs · 14,218 cycles

ASD AFT DRAG ANGLE CRACKED AROUND FASTENER LOCATION. REMOVED AND REPLACED CRACKED ASD AFT DRAG ANGLE WITH NEW SERVICEABLE PART IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND DWG 601R31772. ALL DEFECTS CORRECTED.

Part: RISER — CRACKED (PAX DOOR) · airframe 21,228 hrs · 14,218 cycles

PASSENGER DOOR AFT RISER BUCKLING AND CRACKED IN AREA OF TOP STEP. REMOVED CRACKED PASSENGER DOOR AFT RISER PANEL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE PASSENGER DOOR AFT RISER PANEL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND DWG 601R317071. ALL DEFECTS CORRECTED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 21,228 hrs · 14,218 cycles

NR 3 INTERCOSTAL NEAR STR26R BETWEEN FS 349 - 364 HAS CORROSION. REMOVED CORRODED INTERCOSTAL NR 3 NEAR STR26R IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, INSTALLED NEW SERVICEABLE NR 3 INTERCOSTAL NEAR STR26R IAW SRM 51-40-11-001-001-A01, AND 51-42-21-001-001-A01. ALL DEFECTS CORRECTED.

Part: BUTTSTRAP — CORRODED (BS 280) · airframe 21,228 hrs · 14,218 cycles

FS 280 BUTT STRAP HAS CORROSION BETWEEN STRINGERS 26L - 26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, AND 51-12-001-001-A01. COMPLIED WITH EA 05-2017-051, AND ECTC EA 05-2017-051. ALL DEFECTS CORRECTED.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 21,228 hrs · 14,218 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 333. REMOVED AND REPLACED THE JOINT SPLICE AT STRINGER 25R IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, AND DWG SH670-32103. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 295-310) · airframe 21,228 hrs · 14,218 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 295 - 310. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-161-002-A04. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, AND DWG SH670-31212-2U. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 21,228 hrs · 14,218 cycles

NR 2 INTERCOSTAL NEAR STRINGER 26L BETWEEN BS 349 TO 364 HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 21,228 hrs · 14,218 cycles

BS 310 FRAME HAS CORROSION BETWEEN STRINGERS 24 - 27R. BLENDED CORROSION. DAMAGE OUT OF LIMITS IAW SRM 51-21-06 -001-001-A01. REPAIRED THE CORRODED AREA IAW REO 670-53-21-1308 AND EC/TC REO 670-53-21-1308.

Part: HINGE — CORRODED (DOOR STEP) · airframe 21,228 hrs · 14,218 cycles

PAX DOOR TOP STEP HAS CORROSION AT UPPER HINGE ASSEMBLY. REMOVED AND REPLACED THE PAX DOOR TOP STEP UPPER HINGE ASSEMBLY IAW AMM 20-21-00-910-801-A01.

Part: SIGN — BROKEN (CABIN) · airframe 20,837 hrs · 13,949 cycles

CREW REPORTED EMERGENCY EXIT SIGN OVER THE SERVICE DOOR IS UNSECURED AT ONE END ATTACHMENT POINT. CONTRACT MX REMOVED AND REPLACED EMERGENCY EXIT SIGN OVER SERVICE DOOR WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ADC — FAILED (E&E BAY) · airframe 20,335 hrs · 13,613 cycles

NR 1 ADC FAILED IN FLIGHT, FOLLOWED QRH, RETURNED. REMOVED AND REPLACED ADC NR 1 IAW AMM 34-13-01 AND 34-11-00. OPS CHECKED GOOD.

Part: RETAINER — GOUGED (CARGO DOOR) · airframe 18,916 hrs · 12,562 cycles

SEAL RETAINERS DAMAGED AT BOTH LOWER CORNERS ON THE CENTER CARGO DOOR. BLENDED OUT GOUGE DAMAGE IAW REO 690-52-35-013, REV A, DISPOSITION FOR GOUGE PERMANENT REPAIR ITEM 1. COMPIED WITH HFEC EDDY CURRENT INSPECTIION IAW NDTM 51-20-006, PART 1 AND AS REQUIRED IAW ITEM 2 OF REO 690-52-35-013, REV A, PERMANENT REPAIR FOR GAUGES. NO DEFECT FOUND AT THIS TIME. REFINISHED REWORKED AREAS IAW REO 690-52-35-013 REV A STEP 3 OF PERMANENT REPAIR FOR GAUGES.

Part: RETAINER — GOUGED (CARGO DOOR) · airframe 18,916 hrs · 12,562 cycles

SEAL RETAINERS DAMAGED AT BOTH LOWER CORNERS ON THE FORWARD CARGO DOOR. BLENDED OUT GOUGE DAMAGE IAW REO 690-52-35-013, REV A DISPOSITION FOR GOUGE, PERMANENT REPAIR ITEM 1. COMPLIED WITH HFEC EDDY CURRENT INSPECTION IAW NDTM 51-20-006, PART 1 AND AS REQUIRED IAW ITEM 2 OF REO 690-52-35-013, REV A PERMANENT REPAIR FOR GAUGES, NO DEFECT FOUND AT THIS TIME. REFINISHED REWORKED AREAS IAW REO 690-52-35-013, REV A, STEP 3 OF PERMANENT REPAIR FOR GAUGES. CREATED IAW SOP 5702. REFER TO REO 690-52-35-013, REV A DISPOSITION FOR GAUGES PERMANENT REPAIR.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 18,552 hrs · 12,289 cycles

LENS CAP FOR EMERGENCY EXIT LIGHT AT BOTTOM RT OF SERVICE DOOR IS MISSING. INSTALLED NEW FLOOD LIGHT LENS CHECKS GOOD IAW AMM 33-51-11. CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,144 hrs · 11,259 cycles

PASSENGER EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. CABIN EMERGENCY LIGHTS: FLOOR LEVEL EMERGENCY FLOODLIGHTS. R & R LIGHT ASSY IAW MM 33-51-11 AND IPC REF 33-51-11, ITEM 15. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,442 hrs · 10,054 cycles

AFT EMERGENCY LIGHTS INOPERATIVE. R & R EPSU BATTERY PACK NR 4 IAW AMM 33-51-17, SUP 33-51-17, FIG 1, ITEM 6 AND EO 600-33-0032, REV O1. OP CHECKS GOOD. ACFT OK FOR SERVICE.

Part: WEB — CORRODED · airframe 15,380 hrs · 10,010 cycles

UPON REMOVAL OF SERVICE DOOR SILL ANGLE MOUNT FOUND 4EA FLOOR PROTECTOR WEBS CORRODED. REMOVED 4EA FLOOR PROTECTOR WEBS FROM SERVICE DOOR ENTRANCE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED 2 FWD FLOOR PROTECTOR WEBS REF SRM 51-42-06-001-001-A01. DWG SH670-31950, REV: U. INSTALLED REMAINING AFT FLOOR PROTECTORS WEBS REF SRM 51-42-06-001-001-A01 & DWG SH 670-31950, REV: U.

Part: ANGLE — CORRODED · airframe 15,380 hrs · 10,010 cycles

UPON REMOVAL OF SERVICE DOOR SILL ANGLE MOUNT FOUND LOWER SILL ANGLE TO BE CORRODED. R & R LOWER SILL ANGLE ON SERVICE DOOR IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31986.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,380 hrs · 10,010 cycles

RT 280 BEAM CRACKED. REMOVED RT BS 280 CROSSBEAM IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. LOCATED AND DRILLED NEW 280 BEAM THROUGH LOWER WEB IAW SRM 51-40-11-001-001. LOCATED AND DRILLED CENTER SECTION OF 280 BEAM IAW SRM 51-40-11-001-001. INSTALLED RT 280 BEAM IAW SRM 51-42-06-001-001 IAW DWG NR CC670-34010.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

RT 280 WEB CORRODED. FOUND RT 280 WEB TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003 WITH CORROSION FOUND UNDER FASTENER HEADS REPAIR IAW EC/TC REO 670-53-11-594 01. COMPLIED WITH ECTC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

LT 280 WEB CORRODED. FOUND LT 280 WEB TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003 WITH CORROSION FOUND UNDER FASTENER HEADS REPAIR IAW EC/TC REO 670-53-11-594. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11-594, REV.

Part: ANGLE — CORRODED (BS 333) · airframe 15,380 hrs · 10,010 cycles

ASD SILL CAP ANGLE CORRODED AT RS 333 & WL 72.50. REMOVED ASD SILL UPPER CAP ANGLE IAW SRM 57-42-06-001-001-A01. DRILLED UP NEW MID CAP ANGLE REF SRM 51-40-11-001-001 & DWG SH670-31825. INSTALLED NUT PLATES ON MID CAP ANGLE REF SRM 51-42-06-001-001 & DWG SH6700-31825. INSTALLED MID CAP ANGLE REF SRM 51-41-02-001-001-A02 & DWG SH670-31825. C/W CLOSEOUT STEPS 5D & 5E OF AMM 52-70-04-400-802-A02, OPS CK GOOD.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

UPON INCORPARATION OF SB670BA-53-041 FOUND LT FS 280 CROSSBEAM TO HAVE 2 SPOTS OF CORROSION AT RT NEAR LBL 11. BLENDED DAMAGE ON LT 280 BEAM AT LBL11 UPPER FLANGE EDGE REF SRM 51-21-06-001-001 DAMAGE OUT OF LIMITS REF SRM 53-00-00-101-001. REMOVED LT 280 CROSSBEAM IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. REMOVED INTERCOSTALS AT LBL37 & 20. BETWEEN FS 280 & 295 IAW SRM 51-42-21-001-001-A01. INSTALLED INTERCOSTALS AT LBL 37 & 20 IAW SRM 51-42-21-001-001-A01 IAW DWG CC670-34010. REMOVED INTERCOSTAL AT RBL37, BETWEEN FS 280 & 295 IAW SRM 51-42-21-001-001-A01. INSTALLED INTERCOSTAL AT RBL 37 IAW WSRM 51-42-21-001-001 IAW DWG CC670-34010. LOCATED AND DRILLED NEW 280 BEAM THROUGH LOWER WEB IAW SRM 51-40-11-001-001. LOCATED AND DRILLED CENTER SECTION OF 280 BEAM IAW SRM 51-40-11-001-001. INSTALLED NEW 280 BEAM IAW SRM 51-42-06-001-001 IAW DWG CC670-34010.

Part: FRAME — CORRODED (BS 310) · airframe 15,380 hrs · 10,010 cycles

CORROSION ON FS 310 FRAME AND BETWEEN STR 26L & 26R ON FRONT AND BACKSIDE OF FRAME FRAME BETWEEN 26L AND 26R HAS BEEN BLENDED PRIOR TO THIS WORK , THE CORROSION WASHER IN THE FLANGE, RADIUS ALSO THE WEB AREAS FRONT AND BACK BLENDED CORROSION IASW SRM 51-21-06-001-001-A01, FRAME 310 BETWEEN STR 26L AND 26R IS OUT OF LIMITS IAW SRM 53-21-06-101-002-A01 FORMED FRAMES ALLOWABLE DAMAGE LIMITS, GENERAL TABLE, NOTE: 1 PG 102. COMPLIED WITH STS EA32-2015-014 REPAIR, DATED 1/13/2015. COMPLIED WITH ECTC EA 32-205-014.

Part: ANGLE — CORRODED (BS 333) · airframe 15,380 hrs · 10,010 cycles

ASD BOTTOM SILL CAP ANGLE CORRODED AT FS 333 AND WL 72.50. EVALUATED CORROSION ON ASD BOTTOM SILL CAP ANGLE DAMAGE IS OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED ASD BOTTOM SILL CAP ANGLE IAW SRM 51-41-06-001-001-A01 & SRM 51-42-21-001-001-A01. REMOVED ASD FWD & AFT HANDRAIL FITTINGS IAW SRM 51-42-21-001-001-A01. INSTALLED ASD FWD & AFT HAND RAIL FITTIGS, REF SRM 51-42-21-001-001-A01 & DWG SH670-31810. REMOVED FWD & AFT ASD HANDRAIL ACTUATORS IAW AMM 52-11-05-000-801, CONFIG A01. INSTALLED FWD & AFT ASD HAND RAIL ACTUATORS IAW AMM 52-11-05-400-801-A01 & 52-11-05-400-802 A01. PICKED UP HOLES IN NEW ASD BOTTOM SILL ANGLE REF SRM 51-40-11-001-001 & DWG SH670-31875 & DWG SH670-31810. INSTALLED ALL RIVETS IN LOWER LEG OF BOTTOM SILL CAP ANGLE REF SRM 51-42-06-001-001 & DWG SH670-301810 & SH670-31875.

Part: CHANNEL — CORRODED (BS 302) · airframe 15,380 hrs · 10,010 cycles

CORROSION AT BS 302 AND STRG 27 AROUND ANTENNA BASE. REMOVED TCAS LOWER CHANNEL IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICABLE TCAS CHANNEL ASSY AND INSTALLED SAME AT FS 302, STR 27 REF SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01. INSTALLED FRAME TO STRINGER CLEAT AT STR 57, FS 295 IAW SRM 51-42-06-001-201-A01 AND DWG SH670-31630.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 15,380 hrs · 10,010 cycles

CORROSION AT FS 364 ON LT INTERCOSTAL. REMOVED LT INTERCOSTAL AT FS364 IAW SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. LOCATED AND DRILLED NEW INTERCOSTAL AT FS366 LT IAW SRM TASK 51-40-11-001-001-A01. INSTALLED SERVICEABLE INTERCOSTAL AT FS349-FS364 LT 27 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. RESTORED FINISH IAW SRM 51-21-16-001-001-A01.

Part: ANGLE — CORRODED (BS 310-349) · airframe 15,380 hrs · 10,010 cycles

SERVICE DOOR BOTTOM ANGLE CORRODED BETWEEN FS 310 ANS FS 349 AT WL 72.50 EVALUATED CORRODED AREA DAMAGE IS OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R SERVICE DOOR ANGLE MOUNT IAW SRM 51-42-06-001-001-A01 AND 51-42-34-001-001-A01 AND DWG SH670-31996.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,380 hrs · 10,010 cycles

RBL 9, SEAT TRACK SEGMENT FROM FS 581 TO 661+32 IS CORRODED AND OUT OF LIMITS. REMOVED SEAT TRACK AT RBL9, FS 581 TO 661+32 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL AT RBL9 FROM FS 581-661+32 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 15,380 hrs · 10,010 cycles

CORROSION AT FS 364 ON RT INTERCOSTAL. UPON EVALUATION RT INTERCOSTAL AT FS 364 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED RT INTERCOSTAL AT FS 364 IAW SRM TASK 51-42-06-001-001-A01 AMD 51-42-21-001-001-A01. LOCATED ANF DRILLED NEW INTERCOSTAL AT FS 364 IAW SRM TASKL 51-40-11-001-001-A01. INSTALLED SERVICEABLE INTERCOSTAL AT FS 349-364, STR27RT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, DWG SH670-31350, DWG SH670-32050 AND RESTORED FINISH IAW SRM 51-21-16-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 15,380 hrs · 10,010 cycles

RT FLOOR SUPPORT CORRODED AT FS 349 AND WL 72.50. BLENDED & EVALUATED CORROSION IAW SRM 53-00-00-101-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 & REO 670-53-00-390, REV.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,380 hrs · 10,010 cycles

RBL 9 SEAT TRACK SEGMENT FROM FS 661+32 TO 693 IS CORRODED AND OUT OF LIMITS. REMOVED SEAT TRACK AT RBL9 FS 661+32 TO 693 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT TRACK AT RBL9 FS 661+312 TO 693 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN.

Part: ATTACH BRACKET — CORRODED (BS 280-295) · airframe 15,380 hrs · 10,010 cycles

GALLEY 1 FWD INBD FLOOR ATTACHMENT BRACKET IS CORRODED AROUND BOTH HOLES. REMOVED INTERCOSTALS AT RBL 17.5 BETWEEN DS 280&295 IAW SRM 51-42-21-001-001-A01. INSTALLED INTERCOSTAL AT RBL 17.5 IAW SRM SRM 51-42-21-001-001 IAW DWG SH670-32149. REMOVED GALLEY 1 FWD INBD FLOOR ATTACHMENT BRACKET OFF OF INTERCOSTAL AT RBL 17.5 BETWEEN FS 280 & 295 IAW SRM 51-42-21-001-001-A01. LOCATED, DRILLED & INSTALLED NEW ATTC BRACKET TO INTERCOSTAL AT RBL 17.5 IAW SRM 51-42-21-001-001 A01 IAW DWG SH670-32149.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,380 hrs · 10,010 cycles

LBL 9, SEAT TRACK SEGMENT FROM FS 581 TO 661+32 IS CORRODED AND OUT OF LIMITS. REMOVED SEAT TRACK AT LBL9, FS 661+32 TO 693 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL AT LBL9, FS 581 TO FS 661+32 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN.

Part: FRAME — CORRODED (BS 250) · airframe 15,380 hrs · 10,010 cycles

CORROSION ON FS 250, FRAME AT STR 27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-015, SECTION 1. A, B, & D.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

FLOORBEAM ANGLE AT FS 280 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-12-00-001-001-A01, 51-21-06-001-001-A01. REMOVED AND INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, DWG CC670-34010, REV NC.

Part: FLOOR SUPPORT — CORRODED (BS 3210) · airframe 15,380 hrs · 10,010 cycles

RT FLOOR SUPPORT CORRODED AT FS 3210 AND WL 72.50. BLENDED & EVALUATED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 & REO 670-53-00-390, REV DATED 01/22/2014.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,380 hrs · 10,010 cycles

LBL 9 SEAT TRACK SEGMENT FROM FS 661+32 TO 693 IS CORRODED AND OUT OF LIMITS. REMOVED SEAT TRACK AT LBL9 FS 661+32 TO 693 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL LBL9 FROM FS 661+32 TO FS 693 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,380 hrs · 10,011 cycles

LBL 9 COCKPIT FLOORBEAM CRACKED FORWARD OF BS 280. REPAIRED IAW REO 690-53-11-726.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

RT FLOORBEAM BS 280 HAS ONE SPOT OF CORROSION AT FS 280. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,380 hrs · 10,010 cycles

BS 280 FLOORBEAM IS CORRODED. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,380 hrs · 10,011 cycles

COCKPIT FLOORBEAM CRACKED EIGHT INCHES FORWARD OF FS 280. REPAIRED IAW REO 690-53-11-726.

Part: LIGHT — MISSING (CABIN) · airframe 15,370 hrs · 10,003 cycles

F/A REPORTED MISSING EMERGENCY LIGHT STRIP IN GALLEY. SECURED THE STRIP IAW AMM 33-51-01, NO FURTHER DEFECT NOTED.

Part: WIRE — BROKEN (MEGAPHONE) · airframe 13,289 hrs · 8,612 cycles

MEGAPHONE CONTACTOR AND WIRES BROKEN. R & R MEGAPHONE ASSY IAW AMM 25-61-14 AIPC, FIG 1 ITEM 30.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 12,820 hrs · 8,316 cycles

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

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,726 hrs · 7,655 cycles

PHOTO LUMINESCENT LIGHTS IN GALLERY MISSING FLOOR LIGHTING. INSTALLED PHOTO LUMINESCENT STRIPS IN GALLEY IAW AMM 33-51-01.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 11,454 hrs · 7,480 cycles

FWD CARGO SEAL RETAINER BENT AND TORN. REPAIRED IAW REO 690-52-35-013. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 3-5.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 11,454 hrs · 7,480 cycles

CENTER CARGO SEAL RETAINER BENT AND TORN. REPAIRED IAW REO 690-52-35--013, REV "A". THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 3-5.

Part: WIRE — CRUSHED (EMERGENCY LIGHTS) · airframe 10,186 hrs · 6,701 cycles

RT O/W EMERGENCY LIGHT GROUND WIRE CRUSHED FWD. CRIMPED SERVICABLE CONTACT ON TO GROUND WIRE FOR THE FWD OVERWING EMERGENCY LIGHT VERIFY CONTINUITY CONNECT WIRE TO LIGHT TERMINAL WORK DONE IAW ESMP 20-16-00. COMPLIED WITH OPS TEST OF THE EMERGENCY LIGHTS IAW AMM TASK 33-51-00-710-801, NO DEFECTS NOTED.

Part: ACCESS PANEL — DAMAGED (A/C BAY) · airframe 10,170 hrs · 6,689 cycles

ACCESS PANEL DOOR 182BR ( GROUND AIR-CONTIONING CONNECTION) LOWER LATCH HAS MISSING AND LOOSE RIVETS. REMOVED ACCESS DOOR 182BR IAW AMM 52-45-53-000-801. INSTALLED NEW SERVICEABLE 182BR ACCESS PANEL DOOR IAW AMM 52-45-53-400-801. THIS REPAIR IS CLASSIFIED AS A MAJOR/MINOR REPAIR IAW ASA SOP 5702.

Part: WEB — CORRODED (BS 280) · airframe 10,170 hrs · 6,689 cycles

LT 280, WEB CORRODED. FOUND UPON 280 BEAM REMOVAL. REPAIRED IAW REO 670-53-11-594.

Part: FRAME — CORRODED (BS 310) · airframe 10,170 hrs · 6,689 cycles

CORROSION ON FWD FLANGE OF FRAME AT FS 310, STR 26L TO 26R. REMOVED CORROSION ON FWD FLANGE OF FRAME FS 310, STR 26L-26R IAW SRM 51-42-06-001-001 AND 51-21-06-001-001. RECEIVED AND COMPLIED WITH REO 690-53-21-423.

Part: FRAME — CORRODED (BS 319 S26L/R) · airframe 10,170 hrs · 6,689 cycles

CORROSION ON FWD FLANGE OF FRAME AT FS 319, STR 26L TO 26R. REMOVED CORROSION ON FWD FLANGE OF FRAME FS 319 STR 26L-26R IAW SRM 51-42-06-001-001 AND 51-21-06-001-001. RECEIVED AND COMPLIED WITH REO 690-53-21-423.

Part: FRAME — CORRODED (BS 349 S27) · airframe 10,170 hrs · 6,689 cycles

CORROSION ON FWD FACE OF FRAME AT FS 349, STR 27. REMOVED CORROSION ON FWD FACE OF FRAME 349 AT STR 27 IAW SRM 51-21-06-001-001. ORIGINAL MATERIAL THICKNESS .050" IAW SRM 53-21-06-991-806. RECEIVED AND COMPLIED WITH REO 690-53-21-423.

Part: SEAT TRACK — CORRODED (BS 752) · airframe 10,170 hrs · 6,689 cycles

SIDE WALL SEAT TRACK AT FS 752.50 ON LT SIDE CORRODED. REMOVED DAMAGED SEAT RAIL AT FS 744.15 TO FS 761.85 LT SIDE. INSTALLED A NEW SERVICEABLE SEAT RAIL IAW AMM 53-00-49-000-801/400-804 (A01) AND IPC 53-00-49, FIG 1.

Part: FLOOR SUPPORT — CORRODED · airframe 10,170 hrs · 6,689 cycles

FLOOR SUPPORT CORRODED RT SIDE FS 280 AT RBL 45. REPAIRED FLOOR SUPPORT IAW SRM 53-21-43-201-002-A01.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 10,170 hrs · 6,689 cycles

SEAT TRACK AT FS 349 & RBL 9 CORRODED. REMOVED CORRODED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801/400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,170 hrs · 6,689 cycles

COCKPIT BS 280 FLOORBEAM HAS CORROSION FROM LBL9 TO RBL9. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,170 hrs · 6,689 cycles

FS 280 FLOORBEAM HAS CORROSION UNDER LT WEB JUST OTBD OF LBL 9. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01. CLASSIFIED A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,170 hrs · 6,689 cycles

FS 280 FLOORBEAM HAS CORROSION UNDER RT WEB JUST OTBD OF RBL 9. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND IAW REO 690-53-11-032. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 10,170 hrs · 6,689 cycles

SEAT TRACK AT FS 349 & LBL 9 CORRODED. R & R SEAT TRACK IAW AMMS 53-00-49-000-801 AND 53-00-49-400-801.

Part: FRAME — CORRODED (BS 349) · airframe 10,170 hrs · 6,689 cycles

AFT FLANGE OF FRAME CORRODED AT FS 349, STR 26L TO 26R. REMOVED CORROSION IAW SRM 51-42-06-001-001 & 51-21-06-001-001. COMPLIED WITH REO 690-53-21-423.

Part: LONGERON — CORRODED (BS 364 S27R) · airframe 10,170 hrs · 6,689 cycles

LONGERON CORRODED AT FS364 RT SIDE OF STR 27. REMOVED LONGERON AT FS 364 RT SIDE OF STR27 IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW LONGERON AT FS 364 RT STR27 IAW SRM 51-40-11-001-001-A01. INSTALLED NEW LONGERON AT FS 364 RT OF STR27 IAW 51-42-06-001-001 & 51-42-21-001-001. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: DOUBLER — CORRODED (BS 280) · airframe 10,170 hrs · 6,689 cycles

CORROSION ON INNER SKIN DOUBLER AT FS 280, STR 26L TO 26R. REMOVED CORROSION ON INNER SKIN DOUBLER IAW SRM 51-42-06-001-001 & 51-21-06-001-001. COMPLIED WITH REO 690-53-21-423.

Part: FRAME — CORRODED (BS 333) · airframe 10,170 hrs · 6,689 cycles

AFT FLANGE OF FRAME CORRODED AT FS 333, STR 27 TO 26R. RECEIVED AND COMPIED WITH REO 690-53-21-423.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 10,186 hrs · 6,701 cycles

WIRE BROKEN ON LIGHT FROM OVERWING FAIRING FS768-FS801 PANEL 171CL. INSTALLED SERVICABLE CONTACT (PN 1841-1-5620) ONTO THE ELECTRICAL LEADS FOR THE EXTERNAL EMERGENCY LIGHT ON THE OVER WING FARING PANEL 171CL (AFT LIGHT) IAW ESPM 20-16-00 STEP 5 (LIGHT DS102). PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-802. OPS TEST GOOD.

Part: GLOWSTRIP — DAMAGED · airframe 10,170 hrs · 6,689 cycles

RT FWD PHOTOLUMINESCENT STRIP DAMAGED BEYOND SERVICEABLE. R & R GLOWSTRIP IAW AMM 33-51-01-000-801 AND AMM 33-51-01-400-801.

Part: LONGERON — CORRODED (BS 364 S27L) · airframe 10,170 hrs · 6,689 cycles

LONGERON CORRODED AT FS 364 LT SIDE OF STR 27. REMOVED LONGERON AT FS 364 LT SIDE STR27 IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FS 364 LT STR27 INTERCOSTAL (LONGERON) IAW SRM 51-40-11-001-001-A01. INSTALLED NEW LONGERON AT FS 364 LT OF STR 27 IAW SRM 51-42-06-001-001, 51-42-21-001-001. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FRAME — CORRODED (BS 295) · airframe 10,170 hrs · 6,689 cycles

CORROSION ON AFT FLANGE OF FRAME AT FS 295, STR 26L TO 26R. REMOVED CORROSION IAW SRM 51-42-06-001-001 & 51-21-06-001-001. COMPLIED WITH REO 690-53-21-423.

Part: DOOR — NO TEST (FWD SERVICE) · airframe 10,170 hrs · 6,689 cycles

FWD GALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK ON LATCH, EXCEEDED 25 LBF. FWD GALLEY SERVICE DOOR FUCTIONAL CHECK GOOD UNLATCH BELOW 35LBF IAW AMM 52-41-00-720-802.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,069 hrs · 5,377 cycles

CRACK ON PAX DOOR AFT DRAG ANGLE, BETWEEN STR11 AND STR13 JUST BELOW CABLE PULLEY. WORK COMPLETED IAW REO 670-52-11-287, REV A TEMP REPAIR, ZONE 3.

Part: LIGHT — MISSING (CABIN) · airframe 7,792 hrs · 5,192 cycles

EMERGENCY LIGHT AT LAVATORY, FOUND MISSING. REPLACED MISSING EMERGENCY LIGHT IAW AMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 7,792 hrs · 5,192 cycles

EMERGENCY LIGHT MISSING. REPLACED MISSING EMERGENCY LIGHT AT FWD LAVATORY DOOR IAW AMM 33-51-01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 7,716 hrs · 5,139 cycles

EMERGENCY EXIT SIGN LIGHT IN FRONT OF LT SIDE NR 1 FIRST CLASS SEAT IS OUT. FOUND ELECTRICAL CONNECTOR P341 DISCONNECTED, RECONNECTED ELECTRICAL CONNECTOR IAW ESPM 20-26-00, SYS OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 6,665 hrs · 4,522 cycles

IN FLIGHT, LEFT A/C PACK CYCLES OFF AND ON AT MID THRUST LEVELS ALSO ON FINAL COULD DETECT ODOR FROM PACKS. PERFORMED LT PACK OPS TEST IAW AMM 21-51-00. OPS CHECKED GOOD.

Part: A/C PACK — FAILED (LEFT) · airframe 6,573 hrs · 4,460 cycles

ON APPROACH, SAW AND SMELLED SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED AS A PRECAUTION. R & R LT PACK ACM AND OPS CHECKED GOOD IAW AMM 21-51-08.

Part: ATTACH ANGLE — CRACKED (BS 881) · airframe 5,108 hrs · 3,474 cycles

AFT BELLY FAIRING 195DB CENTER ATTACH ANGLE CRACKED AT BS 881. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 744.15-761.85) · airframe 5,108 hrs · 3,474 cycles

RT SIDE WALL SEAT TRACK FROM FS 744.15 TO 761.85 HAS ONE AREA OF CORROSION (MARKED). REMOVED PASSENGER SIDEWALL PANEL AT FS 744.15 TO 761.85 TO GAIN ACCESS TO SEAT RAIL. INSTALLED PASSENGER SIDEWALL PANEL AT FS 744.15 TO 761.85 IAW AMM 25-26-01-000-400. REMOVED RT FWD EMERGENCY EXIT SILL PLATE TO GAIN ACCESS TO SEAT RAIL. DONE IAW SRM 51-41-02-001-001. INSTALLED RT FWD EMERG EXIT SILL PLATE IAW SRM 51-41-02-001 THIS IS A MINOR REPAIR WR80085 (PB) MA: 3. REMOVED PASSENGER SEAT RAIL ON RT SIDE AT FS 744.15 TO 761.85 DUE TO CORROSION OUT OF LIMITS. REMOVED IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT RAIL ON RT SIDE AT FS 744.15 TO 761.85 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 785.15-847) · airframe 5,108 hrs · 3,474 cycles

RT SIDE WALL SEAT TRACK FROM FS 785.15 TO 847.00 + 8.40 HAS AREA OF CORROSION. BLENDED OUT CORROSION IAW REO 670-53-00-43. FOUND TO BE WITHIN ALLOWABLE LIMITS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 5,108 hrs · 3,474 cycles

AFT DRAG ANGLE CRACKED REINSPECT. COMPLIED WITH REINSPECT OF ASD AFT DRAG ANGLE IAW SRM 52-11-04. REINSPECT NEXT SERVICE CHECK.

Part: WIRE HARNESS — DAMAGED (BRAKES) · airframe 4,101 hrs · 2,841 cycles

ON DESCENT RECEIVED BRAKE OVERHEAT MSG/ LT OTBD POSITION (EMERGENCY DECLARED) R & R LT OTBD MLG PROX SENSOR HARNESS ASSY IAW AMM 32-61-05. OPS TEST GOOD. DEFER CLEARED PLACARD REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,054 hrs · 2,808 cycles

EMERGENCY EXIT SIGN, DS192, LIGHT OUT. R & R NR 3 BATTERY PACK, OPS CHECK GOOD IAW AMM 33-51-17.

Part: BRAKE — OVERHEATED (MLG) · airframe 3,267 hrs · 2,284 cycles

LT O/B BTMS WARNING MESSAGE EMERGENCY DECLARED. REMOVED AND REPLACED LT O/B TIRE AND WHEEL ASSY IAW AMM 32-41-01 AND LT O/B BRAKE ASSY IAW AMM 32-43-26, DEFER CLEARED, PLACRD REMOVED.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 3,010 hrs · 2,117 cycles

PHOTOLUMINESCENT STRIP IN FRONT OF SIDE GALLEY CARTS IS BROKEN IN 2 PLACES. REPLACED BROKEN PHOTO LUMINESCENTS STRIP IN FRONT OF GALLEY CARTS IAW AMM 33-51-01. (CLOSED)

Part: GLOWSTRIP — MISSING (CABIN) · airframe 2,717 hrs · 1,928 cycles

A PHOTOLUMINASCENT STRIP IS MISSING BY THE FWD LAV DOOR. REPLACED STRIP IAW AMM 33-51-01.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 2,581 hrs · 1,842 cycles

PHOTOLUMINESCENT STRIP NEAR GALLEY CARTS DAMAGED AND MISSING PLASTIC COVER. INSTALLED SERVICEABLE PHOTOLUMNISCENT STRIP AS REQUIRED WITH COVER ALREADY ATTACHED IAW AMM 33-51-01, ACFT OK FOR SERVICE.