N607LR

Part: DOUBLER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

DOUBLER AT STRINGER 27 BETWEEN FS 295.00 AND 310.00 IS CORRODED. REMOVED, LOCATED AND DRILLED NEW SERVICEABLE TCAS DOUBLER P/N: SH670-32364-7S IAW CRJ 900 51-40-11-001-001-A01, AND INSTALLED IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: SUPPORT BEAM — CHAFED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

AFT CARGO DOOR FWD AND AFT ENDS OF SUPPORT BEAM ARE CHAFED. CHAFES ARE APPROX 0.125 WIDE, 0.125 WIDE, AND 0.050 DEEP. REPAIRED AFT CARGO DOOR SUPPORT BEAM IAW ENDEAVOR AIR EA CRJ953-15861

Part: BUTTSTRAP — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

F.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 26L AND STGR 26R. REPAIRED IAW ENDEAVOR AIR EA CRJ953-15722 REV A

Part: FRAME — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

WHERE STRINGER 22R MEETS FRAME AT FS349.00 THERE IS CORROSION ON FRAME INSTALLED NEW FRAME AT FS 349 BETWEEN STR 24R TO STR 18R IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 P/N SH670-32035-1

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 22R IS CORRODED BETWEEN FS 333.00 AND 349.00. REMOVED AND REPLACED CLIP PN SH670-35625-2 AT STGR 22R BETWEEN FS 333-349 IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — DEFORMED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FOUND ELONGATED HOLES AT THE INTERCOSTAL AND 2 CLEATS AT LEVEL OF FS 333.00 AND STR 20R. REMOVED DAMAGED INTERCOSTAL AND CLEATS (2 E/A) LOCATED BETWEEN FS 319 TO FS 349 AND STR 20R IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL ( PN SH670-32004-1) AND CLEATS (P/N SH670-32014-2S AND SH670-32014-1) (2E/A) FS 319 TO FS 349 AND STR 20R IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

AFTER REMOVAL OF INTERCOSTAL FOUND CORROSION AT STR20R BETWEEN FS 319 TO FS 349. REMOVED STR20R BETWEEN FS 319 TO FS 349 IAW CRJ-900 SRM 51-42-06-001-001-A01 CORRECTIVE ACTION: INSTALLED STR20R BETWEEN FS 319 TO FS 349 IAW CRJ 900 SRM 51-42-06/21-001-001-A01.

Part: WEB — CORRODED (PAX DOOR) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR FWD STAIR WEB CORRODED. REMOVED FWD STAIR WEB STIFFENING ANGLES, LOCATED AND DRILLED NEW SERVICEABLE FWD STAIR WEB PN 601R317071-12 AND INSTALLED STIFFENING ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REFERENCE HN00119928 FOR INSTALLATION OF WEB ONTO PAX DOOR.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 21R IS CORRODED BETWEEN FS 394.00 TO 409.00, FS 421.00 TO 437.00, AND FS 469.00 TO 485.00. REMOVED AND REPLACED STRINGER 21R (PN SH670-31385-1) IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

LH FS280 CROSS BEAM HAS MINOR CORROSION INSTALLED NEW SERVICEABLE L/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND REFERENCED SB 670BA-53-041 REV M FOR FASTENER CALL OUT

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

CORROSION FOUND AT STRINGER 19R BETWEEN FS 319 TO FS 349 REMOVED AND REPLACED STRINGER 19R, PN SH670-32427-1, BETWEEN FS 319-349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01

Part: WEB — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR AFT STAIR WEB CORRODED. REMOVED AFT STAIR WEB STIFFENING ANGLES, LOCATED AND DRILLED NEW SERVICEABLE AFT STAIR WEB PN 601R317071-11 AND INSTALLED STIFFENING ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REFERENCE HN00119928 FOR INSTALLATION OF WEB ONTO PAX DOOR.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 20R IS CORRODED BETWEEN FS 581 AND FS 597 REPAIRED IAW ENDEAVOR AIR EA NO CRJ953-15749

Part: STRINGER — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

STRINGER 19 IS CORRODED BETWEEN FS 437.00 TO 453.00 AND FS 469.00 TO 486.00 REMOVED AND INSTALLED NEW STGR 19R BETWEEN F.S 349 - F.S. 477 IAW CRJ 900 SRM 51-42-06-001-001-A01 (UPON FURTHER INVESTIGATION, CORROSION ON STGR 19R AT F.S. 469 - F.S. 486 IS ACTUALLY ON STRINGER 19R F.S. 477 JOINT SPLICE. CORRECTIVE ACTION: REFERENCE NON ROUTINE HN00119883 FOR REPLACEMENT OF SPLICE PIECE.)

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 20R IS CORRODED BETWEEN FS 364.00 TO 333.00 AND FS 394.00 TO 394.00. REMOVED,LOCATED AND DRILLED NEW STGR 20R (P/N SH670-31405-2) AT F.S. 333 TO F.S. 477 IAW CRJ900 SRM 51-40-11-001-001-A01 AND INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

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

Part: CLEAT — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR CLEAT ON FRAME AT FS 313.56 AND DD4 CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR CLEAT P/N:600-31902-269 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

L/H FLOOR SILL F.S.985-1000 CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 985 TO FS 1000 LH SIDE FLOOR LEVEL IAW EA NO: CRJ953-15782 REV IR DATED:11/18/2023.

Part: ANGLE — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR CLIP AT DD7A FWD SIDE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE CLIP AT DD7A FWD P/N:601R318058-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

AT F.S.1000, RBL27-36 CROSS BEAM IS CORRDED AT NUT PLATE. REPAIRED CROSS BEAM AT F.S.1000 IAW ENDEAVOR AIR EA NO: CRJ953-15733

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR INTERCOSTAL DD5 FWD SIDE FOUND CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FWD INTERCOSTAL DD5 P/N:601R318091-5 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: ANGLE — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR ANGLE Ï¿½CÏ¿½ AT DD7A MID CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR ANGLE Ï¿½CÏ¿½ AT DD7A P/N:601R317052 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR DD4 AFT CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR DD4 AFT INTERCOSTAL P/N:601R31902-317A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

SIDE SEAT RAIL BETWEEN FS 572 AND FS 661+16 AT STGR 15R IS CORRODED. INSTALLED NEW SIDE SEAT RAIL AT FS 572 AND FS 661+16 AT STGR 15R IAW CRJ900 AMM 53-00-49-400-801(CONFIG A07).

Part: ANGLE — CRACKED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

FS 280 ANGLE AT LBL 12 IS CRACKED INSTALLED NEW SERVICEABLE ANGLE P/N CC670-34099-1SB COMMON TO LBL 12 INTERCOSTAL AND FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: GUSSET — DEFORMED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

"GUSSETS ON L/H AND R/H SIDES COMMON TO FWD ""J"" ANGLE AND COCKPIT FLOORBOARD HAS ELONGATED HOLES. REMOVED, LOCATED AND DRILLED, INSTALLED NEW GUSSETS P/N CC670-33467-1, CC670-33467-2 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06/21-001-001-A01. RESTORED SURFACE FINISH IAW CRJ SRM (TR51-0068) 51-21-16-001-001-A01."

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 24R IS CORRODED BETWEEN FS 280 AND FS 333. REMOVED CORRODED STRINGER 24R P/N:SH670-31212-2, IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE STRINGER 24R P/N:SH670-31212-2U, IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

STRINGER 24R SPLICE AT F.S. 333 IS HEAVILY CORRODED. REMOVED CORRODED STRINGER SPLICE AND INSTALLED A NEW STRINGER SPLICE #24 (P/N: SH670-32429-4) IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 23R IS CORRODED BETWEEN FS 364.00 AND 379.00. REMOVED STGR 23R FROM FS 333-379 AND INSTALLED NEW STGR 23R PN: SH670-31380-1 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CRACKED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

RH FS280 CROSSBEAM CORROSION CAP ANGLE IS CRACKED. REMOVED CORRODED WEB AT LBL 12 AND INSTALLED A FABRICATED FS 280 LOWER WEB AND BUTT STRAP. COMPLIED WITH STEPS 5B (1-2) OF CRJ 900 SRM 53-11-10-201-004-A01 FOR REPAIR OF L/H FS 280 LOWER WEB. REFERENCE HN00118584 FOR INSTALL OF NEW CORROSION CAP.

Part: BRACKET — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FWD CARGO CENTER DOOR SURROUND STRUCTURE FWD H BRACKET AT F.S. 629 IS CORRODED. REMOVED AND REPLACED FORWARD CARGO CENTER DOOR SURROUND STRUCTURE FWD H BRACKET AT F.S. 629 IAW SRM 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.

Part: WEB — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

R/H FS 280 LOWER WEB IS CORRODED AT RBL 12 REMOVED CORROSION AT RBL 12 ON FS 280 LOWER WEB IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS OF LOWER WEB IS .040, REMOVED .024 OF MATERIAL AND REMAINING THICKNESS IS .016, WHICH IS OUT OF LIMITS IAW CRJ 900 SRM 53-00-00-101-001-A01. LOWER WEB REQUIRES REPLACEMENT OR REPAIR. REMOVED AND REPLACED R/H FS 280 LOWER WEB AND BUTT STRAP IAW CRJ 900 SRM 51-24-36-001-001-A01, SRM 51-40-11-001-001-A01 AND USING SRM 53-11-10-201-004-A01 FOR MATERIAL CALLOUT. PO# FOR METAL IS 5-4871

Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

INTERCOSTAL AT 26L BETWEEN FS 865.00 AND 881.00 IS CORRODED. REMOVED CORROSION AT INTERCOSTAL AT 26L BETWEEN FS 865.00 AND 881.00 IAW CRJ900 SRM 51-21-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 25R LONGERON IS CORRODED BETWEEN FS 349 AND FS 364 REMOVED AND REPLACED STRINGER 25R LONGERON BETWEEN F.S.333 TO F.S.364.

Part: WEB — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

L/H FS280 LOWER WEB IS CORRODED AT LBL 12 REMOVED CORROSION AT LBL 12 ON FS 280 LOWER WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS OF WEB WAS .040, REMOVED .015 OF MATERIAL AND REMAINING THICKNESS IS .025, WHICH IS OUT OF LIMITS IAW CRJ 900 SRM 53-00-00-101-001-A01. LOWER WEB REQUIRES REPLACEMENT OR REPAIR. REMOVED AND REPLACED L/H FS 280 LOWER WEB AND BUTT STRAP IAW CRJ 900 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01 AND USING SRM 53-11-10-201-004-A01 FOR MATERIAL CALLOUT. PO# FOR METAL IS 5-4871. PAINTED AND APPLIED CIC TO L/H FS 280 LOWER WEB IAW CRJ 900 SRM 51-25-16-001-001-A01 AND SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FRAME AT F.S. 533 STGR 17L TO STGR 18L IS CORRODED ON THE FWD AND AFT SIDE. REPAIRED FRAME AT F.S.533 IAW CRJ-900 SRM 53-00-06-201-001-A03

Part: FRAME — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FS 549 FRAME SECTOR IS CORRODED AT STGR 17L-18L REPAIRED FRAME SECTOR IAW CRJ900 SRM 53-00-06-201-001-A03

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

STRINGER 23R IS CORRDED BETWEEN FS 280 AND FS333 REMOVED AND REPLACED STRINGER 23R FROM FS 280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: FRAME — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

FRAME AT F.S. 645 STGR 17L TO STGR 18L IS CORRODED ON THE FWD AND AFT SIDE. REMOVED CORRODED FRAME AT F.S.645 FROM STGR 17L TO STGR 18L AND INSTALLED NEW SERVICABLE FRAME P/N SH690-33126-1B IAW CRJ 900 SRM 53-00-06-201-001-A03.

Part: NUT PLATE — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

4 NUT-PLATES ARE CORRODED BETWEEN F.S. 661+16 TO F.S.661+32 BETWEEN STGR 26L AND 24R. INSTALLED 4 FASTENERS AND 1 RETAINER PLATE P/N SH670-39095-7 FROM F.S. 661+16 TO F.S. 661+32 BETWEEN STGR 26L TO STGR 24R IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: CLEAT — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR CLEAT ON FWD DD4 AND FS 320 CORRODED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR CLEAT P/N:600-31902-269 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: DOOR FRAME — CORRODED (AFT CABIN) · airframe 34,193 hrs · 24,553 cycles

PAX DOOR AFT FORMER CORRODED WHERE POWER ASSIST MOTOR PULLEY BRACKET IS LOCATED RECEIVED AND COMPLIED WITH ENDEAVOR EA CRJ953-15781 REV A.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,193 hrs · 24,553 cycles

PAX DOOR FWD INTERCOSTAL DD1 CORRODED REMOVED AND REPLACED WITH NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD1 P/N:601R318054-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: STUB FRAME — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FS 661 STUB FRAME UNDER CENTER CARGO DOOR SILL IS CORRODED BETWEEN STGR 25L AND 26L REMOVED AND REPLACED STUB FRAME P/N SH670-33824-1 IAW CRJ 900 SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,193 hrs · 24,553 cycles

PAX DOOR FWD INTERCOSTAL DD3 CORRODED REMOVED AND REPLACED WITH NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD3 P/N:601R318054-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: STRINGER FITTING — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

STRINGER 23R SPLICE AT F.S. 333 IS HEAVILY CORRODED. REMOVED CORRODED STRINGER SPLICE AND INSTALLED A NEW STRINGER SPLICE #23 (P/N: SH670-32429-4) IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

LBL 9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 364 TO F.S. 485 THE SEAT RAIL AT LBL 9 BETWEEN F.S. 364 TO F.S. 485.AT WAS REMOVED AND REPLACED IAW CRJ900 AMM 53-00-49-000/400-801 A07.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

DESCRIPTION: LBL 9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 364 TO F.S. 485 THE SEAT RAIL AT LBL 9 BETWEEN F.S. 364 TO F.S. 485.AT WAS REMOVED AND REPLACED IAW CRJ900 AMM 53-00-49-000/400-801 A07.

Part: STRINGER SPLICE — CORRODED (BS 477 S19R) · airframe 34,193 hrs · 24,553 cycles

STRINGER 19R SPLICE AT F.S. 477 CIRC. JOINT IS CORRODED. REPLACED STRINGER 19R SPLICE P/N SH670-33264-1 AT F.S. 477 JOINT IAW CRJ-900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01

Part: STRIKER — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

GALLEY SERVICE DOOR SEAL STRIKER IS CORRODED RECEIVED, LOCATED, DRILLED AND DEBURRED NEW FITTING SEAL STRIKER P/N SH670-31412-7 ON PLACE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR, IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW FITTING SEAL STRIKER P/N SH670-31412-7 ON PLACE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR, IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PASSENGER DOOR 7A AFT CLIP CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR CLIP AT DD7A AFT SIDE P/N:601R318058-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01

Part: FRAME — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

FOUND CORROSION ON FS 501 SECTOR FRAME BTWN STGR 25L TO STGR 23L REMOVED AND INSTALLED NEW SECTOR FRAME P/N SH690-33774-3 FS 501 BETWEEN STGR 19L TO STGR 25L IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

INTERCOSTAL AT STGR 20R BETWEEN FS 349.00 AND 364.00 IS CORRODED. REMOVED AND REPLACED STGR 20R INTERCOSTAL BETWEEN F.S. 349.00 TO F.S. 364.00 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01.

Part: BRACKET — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

"J830 CONNECTOR BRACKET AT STGR 19R F.S. 349 - F.S. 409 IS HEAVILY CORRODED. REMOVED FABRICATED, LOCATED AND DRILLED AND INSTALLED SERVICEABLE CONNECTOR BRACKET FOR STGR 19R BETWEEN F.S. 349 - F.S. 409 IAW CRJ 900 SRM 51-24-21-001-001-A01, 51-40-11-001-001-A01. 53-42-06-001-001-A01 PART MADE OF 2024-T3 .040"" (PO# 5-4713) AS PER DWG NO. SH670-50807 REV. NC."

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

TOP OF FLOOR CROSS BEAM AT FS 349.00 IS CORRODED BETWEEN LBL 9 AND RBL9. REMOVED PACKER P/N: SH670-32167-3 AT FS 349 RBL9 IAW CRJ-900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PACKER P/N: SH670-32167-3 AT FS 349 RBL9 IAW CRJ-900 SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

"RH FLOOR SILL IS CORRODED IN MULTIPLE LOCATION BETWEEN FS 280.00 AND 319.00. REMOVED CORRODED SILL P/N: SH670-32172-9. F.S280 TO F.S.319. AND ATTACHED PART FOR ACCESS IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-13-001-001-A01. INSTALLED A""NEW"", FLOOR SILL P/N: SH670-32172-9. F.S. 280 - F.S. 319 IAW CRJ900 SRM 51-42-06/13-001-001-A01."

Part: BRACKET — CRACKED (ZONE 700) · airframe 34,193 hrs · 24,553 cycles

FWD BRACKET IS CRACKED FOR SYS. 3 BRAKE ACCUMULATOR. REMOVED FWD O/B, I/B CRACKED BRACKET AT SYS. 3 BRAKE ACCUMULATOR .IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED O/B, I/B FWD BRACKET AT SYS 3 BRAKE ACCUMULATOR . IAW CRJ 900 SRM 51-40-11-001-001-A01; SRM 51-42-06-001-001-A01. ( P/N OF NEW PART: CC670-75604-4 AND -3).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

L/H SIDE SEAT TRACK CORRODED BETWEEN F.S. 677 TO F.S. 720. REMOVED AND REPLACED SEAT TRACK IAW CRJ900 AMM 53-00-49-000/400-801 A07

Part: STUB FRAME — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

FWD CARGO DOOR FWD LOWER STUB FRAME BETWEEN STGR 26L TO STGR 25L AT F.S. 533 IS CORRODED. REMOVED STUB FRAME IAW CRJ900 SRM 51-42-21-001-001-A01, INSTALLED STUB FRAME AT FS533 BETWEEN STGR 26L - STGR 25L IAW CRJ900 SRM 51-42-21--001-001-A01

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

F.S. 280 O/B CLIP IS CRACKED AT RBL11. REMOVED CRACKED ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE P/N CC670-34099-2 COMMON TO RBL 12 INTERCOSTAL AND FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SKIN — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PAX DOOR INNER SKIN IS CORRODED IN MULTIPLE LOCATIONS. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER SKIN P/N:601R318024-11 IAW CRJ900 SRM 51-40-11-001-001-A01. REFERENCE BARCODE HN00119928 FOR REMOVAL AND INSTALLATION.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

R/H F.S. 280 BEAM APPEARS TO BE CRACKED BETWEEN RBL 12 TO RBL 16 AND AT RBL 36. LOCATED AND DRILLED NEW FS 280 RH CROSSBEAM PN: CC670-34094JP-2S IAW CRJ900 SRM 51-40-11-001-001-A01 AND SB 670BA-53-041 REV M INSTALLED NEW SERVICEABLE R/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND SB 670BA-53-041 REV M

Part: FRAME — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

FWD CARGO BAY CENTER CARGO DOOR F.S. 645 STUB FRAME IS CORRODED BETWEEN STGR 26L TO STGR 25L. REMOVED AND REPLACED STUB FRAME P/N SH670-33824-1 IAW CRJ 900 SRM 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

F.S. 280 FWD J ANGLE IS CORRODED. REMOVED FWD J ANGLE IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01 INSTALLED NEW SERVICEABLE FWD J ANGLE ON FS 280 CROSSBEAMS BETWEEN LBL 12 AND RBL 12 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

SUPPORT INTERCOSTAL IS CORRODED RIGHT OF STGR 27 BETWEEN FS 394.00 AND 409.00. INSTALLED NEW SERVICEABLE PART SH670-32075-3S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 34,193 hrs · 24,553 cycles

SUPPORT INTERCOSTAL IS CORRODED LEFT OF STGR 27 BETWEEN FS 394.00 AND 409.00. INSTALLED NEW SERVICEABLE PART SH670-32075-4S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRUCTURE — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

CORROSION ON BOTH LBL9 AND RBL9 INBOARD PACKERS AT FS333.00 INSTALLED NEW SERVICEABLE PARTS #SH670-32167-3 IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 34,193 hrs · 24,553 cycles

"STRINGER 25R IS CORRODED BETWEEN F.S. 645 TO F.S. 661+8.40. PERFORMED PERMANENT REPAIR ON STR25R P/N SH690-33215-5 BETWEEN FS 613 TO FS 661+32"", IAW CRJ-900 SRM IAW CRJ900 SRM 53-00-03-201-001-A02 SOLUTION II STEP 5.A(4-13), EXTRUSION PO# 5-7622, SHIM PO# W91214."

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,193 hrs · 24,553 cycles

SIDE SEAT RAIL BETWEEN FS 379 AND FS 485 AT STGR 15L IS CORRODED. REMOVED L/H SIDE SEAT TRACK F.S 379 TO F.S.485 IAW CRJ 900 AMM 53-00-49-000-801-A07. LOCATE, TRIM TO FIT DRILL AND INSTALLED NEW L/H SIDE SEAT TRACK F.S 379 TO F.S.485 IAW CRJ900 AMM 53-00-49-400-801-A07

Part: RETAINER — CORRODED (E/E DOOR) · airframe 34,193 hrs · 24,553 cycles

MAIN AVIONICS DOOR FWD L/H AND R/H SEAL RETAINERS ARE CORRODED. MAIN AVIONICS DOOR FWD L/H AND R/H SEAL RETAINERS WERE INSTALLED (REPLACED) IAW CRJ900 SRM TASK 51-42-06-001-001-A01.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 34,193 hrs · 24,553 cycles

MAIN AVIONICS DOOR FWD L/H AND R/H SEAL RETAINERS ARE CORRODED. MAIN AVIONICS DOOR FWD L/H AND R/H SEAL RETAINERS WERE INSTALLED (REPLACED) IAW CRJ900 SRM TASK 51-42-06-001-001-A01.

Part: FORMER — CORRODED (ZONE 800) · airframe 34,193 hrs · 24,553 cycles

PAX DOOR FWD FORMER CORRODED IN MULTIPLE PLACES. REMOVED AND REINSTALLED PAX DOOR FWD MID, UPPER, AND LOWER SEAL RETAINER AND FWD SUPPORT ANGLE FOR ACCESS IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER P/N:601R318031-5S IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: COVER — MISSING (EXIT SIGN) · airframe 29,085 hrs · 20,191 cycles

REAR FACING EXIT SIGN IN PAX CABIN MISSING. INSTALLED EXIT SIGN COVER IAW AMM 33-51-07.

Part: FUEL FILTER — NOT REPORTED (LT ENGINE) · airframe 28,826 hrs · 19,933 cycles

ON THE APPROACH INTO KTYS CREW OBSERVED L MAIN EJECTOR, L ENGINE FLAME OUT CAUTION MSG'S BOTTLE ARMED PUSH TO DISCHARGE ILLUMIATED ON GLARES- HEILD L ENGINE DID FLAMEOUT TEMPORARILY BUT RESTARTED ON ITS OWN, ALL MSGS CLEARED AS WELL. CLEANED COLLECTOR TANKS IAW AMM 51-26-00 R/R LH AND RH ENGINE FUEL FILTERS REF NRCC 130490 R/R APU FUEL FILTER RED NRCC 130488 SEE NRWC 7603- 65 FOR FURTHER MAINTENANCE ACTIONS. COMPLIED WITH WORK SCOPE ISSUED BY MOTR DEPARTMENT PERFORMED POWER ASSURANCE RUNS IAW AMM 71-00-00. OPER- ATIONAL CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,988 hrs · 19,246 cycles

"AWR; HIDDEN CORROSION: [ DURING REMOTION OF LOOR PANEL SUPPORT ANGLE RELATED WITH NRC 00162 ]: CORROSION ON FLOOR BEAM [ FWD FACE ] IN STA.FS= 280 BETWEEN 01LBL TO 07LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) TCI: 53-10-219 "NEW FLOOR BEAM IN STA. FS= 280 LBL WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01.PAR.6.C. AND 51-42-21-001-001-A01.PAR.6.C.

Part: CHANNEL — CRACKED (DOOR FRAME) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CRACKED UPPER / LOWER BRACKETS END OF CHANNEL AT FWD EDGE AFT BAGGAGE BAY DOOR CUTOUT ( CCT ) ""SUMMARY: ON NRC. 00333, CHANNEL BRACKET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 MM670-35507-001

Part: FRAME — CORRODED (BS 295) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON FRAME FS295 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY: ON NRC. 00189, CORROSION LEVEL 2. FRAME FS295 BTW STGR 25LH O 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-09882 REV. IR "

Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,988 hrs · 19,246 cycles

"AWR; HIDDEN CORROSION: [ DURING REMOTION OF LOOR PANEL SUPPORT ANGLE RELATED WITH NRC 00162 ]: CORROSION ON FLOOR BEAM [ FWD FACE ] IN STA. FS= 280 BETWEEN 01LBL TO 07LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) TCI: 53-10-219 "NEW FLOOR BEAM IN STA. FS= 280 LBL WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01.PAR.6.C. AND 51-42-21-001-001-A01.PAR.6.C. "

Part: CHANNEL — CRACKED (DOOR FRAME) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CRACKED UPPER / LOWER BRACKETS END OF CHANNEL AT FWD EDGE AFT BAGGAGE BAY DOOR CUTOUT ( CCT ) "SUMMARY: ON NRC. 00333, CHANNEL BRACKET WERE REPLACED PER CRJ-900 SRM51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 MM370-35507-001

Part: INTERCOSTAL — CORRODED (BS 311-347) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION. CORROSION ON INTERCOSTAL DD6 BETWEEN FS= 311 FS= 347 AT MAIN PASSENGER DOOR. (L1) (PTAS) (TCI: 52-10-301). "SUMMARY OF NRC 00101: INTERCOSTAL DD6 ( P/N 601R318057-1 ) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6 . C AND SRM 51-42-21-001-001-A01 PAR, 6. C "

Part: INTERCOSTAL — CORRODED (BS 311-347) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION. CORROSION ON INTERCOSTAL DD6 BETWEEN FS= 311 FS= 347 AT MAIN PASSENGER DOOR. (L1) (PTAS) (TCI: 52-10-301). "SUMMARY OF NRC 00101: INTERCOSTAL DD6 ( P/N 601R318057-1 ) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6 . C AND SRM 51-42-21-001-001-A01 PAR, 6. C

Part: FRAME — CORRODED (BS 310) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON FRAME FS310 BTW STGR 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY OF NRC 00188: |CORROSION LEVEL 2| FRAME FS 310 BTW STGR 24LH TO 25RH WAS REPAIRED PER REO 690-53-21-1169 REV

Part: HINGE — DAMAGED (PAX DOOR) · airframe 27,988 hrs · 19,246 cycles

"LATE FINDING: ELONGATED HOLES AND WEAR ON PIANO HINGE OF EXTERNAL SURROUND STRUCTURE AT MAIN PASSENGER DOOR (SM) ""SUMMARY: DAMAGED PIANO HINGE OF EXTERNAL SURROUND STRUCTURE AT MAIN PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 53-21-23-201-010-A01 "

Part: FRAME — CORRODED (BS 333) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON FRAME FS333 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) " "SUMMARY: ON NRC. 00165, CORROSION LEVEL 2. FRAME FS333 BTW STGR 25LHTO 25RH AT MAIN AVIONICS COMPARTMENTWAS REPAIRED PER EA NO. CRJ953-09880 REV. IR

Part: INTERCOSTAL — CORRODED (BS 310-349) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CORROSION ON INTERCOSTAL 21LH BTW FS310 TO FS349 OF THE MAIN AVIONICS COMPARTMENT (SM) "SUMMARY NRC 00291: INTERCOSTALS STRG 21LH BTW FS310 TO FS349 AND CLIPP/N 570-31867-1 AND BRAKET P/N SH670-32682-1 OF THE MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR.6-C,S.R.M. 51-42-20-001-001-A01 PAR.6-C AND EA CRJ 953-09908 REV. IR AND EA CRJ 953-09910 REV.IR SH670-31823-1

Part: FRAME — CORRODED (BS 295) · airframe 27,988 hrs · 19,246 cycles

"AWR, MPEDV [IN REF NRC 00189]: FRAME FS295 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. ( E/E ). ""SUMMARY : REPAIR PARTS WERE FABRICATED PER EA CRJ953-09882 REV. IR "

Part: FRAME — CORRODED (BS 364) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON FRAME FS364 FWD ATTACHED FLANGE BTWSTGR 26RH TO 27 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "COMPLETE: SUMMARY: ON NRC: 00166, CORROSION LEVEL 2. FRAME FS364 BTW STGR 26RH TO 27 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 EA CRJ953-09927 REV. IR

Part: CLEAT — CORRODED (BS 311) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION. CORROSION ON INTERCOSTAL DD6 CLEAT FS= 311 AT MAINPASSENGER DOOR. (L1) (PTAS) (TCI: 52-10-301). ""SUMMARY : DAMAGE CLEAT WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 "

Part: ACCESS PANEL — CORRODED · airframe 27,988 hrs · 19,246 cycles

"PART RACKS : WEAR ON FLAP ACCESS PANELS NBR 584ET, 584GB, 584EB, 584LB AND 584JB, 684LB, 684EB, 684CB AND 684GB. "SUMMARY OF NRC 00385: ACCESS PANEL (5 EAZ): (1) 584ET , (2) 684CB , (3) 584EB,(4) 684 EB, (5 ) 584JB WAS REPAIRED PER EA NO. CRJ957-09938 REV IR, PER EA NO. CRJ957-09939 REV IR, PER EA NO. CRJ957-09940 REV IR,PER EA NO. CRJ957-09941 REV IR, PER EA CRJ953-09937 REV-A. AND ACCESS PANELS (4 EAZ) 584GB, 584LB, , 684LB AND 684GB WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01.AND REWORKED AREAS ON ACCESS PANEL 584B, 584LB, , 684LB AND 684GB WERE MEASURED WITH THE FOLLOWING DIMENTION S (4EAZ) : (1) 684GB L=2.150"" W=0.700"" OT=0.090"" RMT=0.084"", (2) 584LB L=2"" W=0.800"" OT=0.090"" MRT= 0.083"" THEREFORE IT'S WITHIN LIMITS PERCRJ 900 SRM 57-52-01-101-001-A01. AND ACCESS PANELS (3) 684LB L=2.163"" W=0.900"" OT=0.090"" RMT=0.038"" AND (4) 584GB L=2.050 W=0.600"" OT=0.090 "" RMT=0.037"" THEREFORE ARE OUT OF LIMITS PER CRJ 900 SRM 57-52-01-101-001-A01. EQUIPMENT DIAL INDICATOR PART NO. 543-783, S/N 18200766, CALIBRATION DUE DATE MAR/19-20. THEREFORE ACCESS PANEL 684LB AND 584 GB WERE VERIFIED PER AIPC 57-51-32 FIGURE-1

Part: STRINGER — CORRODED (BS 349-364) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR 27 BTW FS349 TO FS364 AT MAINAVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY: STGR 27 BTW FS349 TO FS364 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01. LEVEL CORROSION II. "

Part: LATCH — CRACKED (RT NACELLE DOOR) · airframe 27,988 hrs · 19,246 cycles

"INITAL INSPECTION : CRACKED COAMING LATCH DOOR AT LOWER HALF TRANSCOWL, RH ENGINE ( MOT 2 ) "SUMMARY: ON NRC. 00076, COAMING LATCH DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 "

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,988 hrs · 19,246 cycles

"MPEDV: REPAIR PARTS OF LONGITUDINAL BEAM RBL12. AT FS.280 IN REF NRC00203. "SUMMARY : REPAIR PARTS OF LONGITUDINAL BEAM RBL12. WERE FABRICATED PER CRJ-900 SRM 53-11-43-201-003-A01

Part: ANGLE — CORRODED (BS 310-349) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON MID CAP ANGLE [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "SUMMARY OF NRC: 00315 ANGLE MID CAP WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 "

Part: ELECTRICAL BOX — CRACKED · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS) ""SUMMARY: DAMAGED IN RECEPTACLE PLATE AT FUSELAGE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR.6 "

Part: POST — CORRODED (BS 277-280) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON LH POST IN STA. FS= 277 TO FS= 280 AND 11LBL IN COCKPIT DOOR CUT-OUT AREA AT PAX CABIN FWD WET AREA. (W1) (CPAX) "SUMMARY: OF NRC. 00296, CORROSION LEVEL 2 ON LH POST IN STA. FS= 277 TO FS= 280 AND 11LBL IN COCKPIT WAS REPAIRED PER CRJ-900 SRM 53-11-10-201-006-A01

Part: STRINGER — CORRODED (BS 295-333) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR 25RH BTW FS295 TO FS333 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) " SUMMARY OF NRC:00191 CORROSION LEVEL# 2 ON STRINGER 25RH BTW FS295 TO FS333 AT MAIN AVIONICS COMPARTMENT ( E/E ). STRINGER 25RH BTW FS295 TO FS333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 310-364) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CORROSION ON INTERCOSTAL 310 TO 364 AT STGR 20RH OF THE MAIN AVIONICS COMPARTMENT (SM) "SUMMARY OF NRC 00284: INTERCOSTALS FS=310 TO FS=319, FS=319 TO FS=349 AND FS=349 TO FS=364 AT STGR 20RH WERE REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: STRINGER — CORRODED (BS 295-333) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR 26RH BTW FS295 TO FS333 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY OF NRC:00190; CORROSION LEVEL # 2 ON STGR 26RH BTW FS295 TO FS333. STRINGER 26RH BTW FS295 TO FS333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. "

Part: STRAP — CORRODED (FAIRING) · airframe 27,988 hrs · 19,246 cycles

"HIDDEN DAMAGE: CORROSION ON LH/RH SENTTLEMENT AREA AT PANEL 193AB. (FUS). "SUMMARY: UNDERWING FAIRING STRAPS LH/RH (2 EA) AT ACCESS PANEL 193AB WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.

Part: POST — CORRODED (BS 277-280) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON RH POST IN STA. FS= 277 TO FS= 280 AND 11RBL IN COCKPIT DOOR CUT-OUT AREA AT PAX CABIN FWD WET AREA. (W1) (CPAX) "SUMMARY: ON NRC. 00297 CORROSION LEVEL 2, ON RH POST IN STA. FS= 277TO FS= 280 AND 11RBL IN COCKPIT WAS REPAIRED PER CRJ-900 SRM 53-11-10-201-006-A01 "

Part: STRINGER — CORRODED (BS 333-364) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR 26RH BTW FS333 TO FS364 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY OF NRC: 00167 STRINGER 26RH BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. "

Part: SKIN — CORRODED (PAX DOOR) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION. CORROSION ON INNER SKIN AT PASSANGER DOOR. (L1) (PTAS) (TCI: 800-07). "SUMMARY: LEVEL CORROSION 2 AREA DAMAGE ON INNER SKIN AT PASSENGER WAS REPAIRED PER EA: CRJ952-09928 REV. IR "

Part: STRINGER — CORRODED (BS 280-310) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CORROSION ON STGR 20RH BTW FS 280 TO 310 OF THE MAIN AVIONICS COMPARTMENT (SM) "SUMMARY:STGR 20RH BTW FS 280 TO 310 OF THE MAIN AVIONICS COMPARTMENT (SM) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-0001-A01 AND SRM 51-42-21-001-001-A01

Part: STRAP — CORRODED (BS 319) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON FRAME STRAP IN FS= 319 BETWEEN STGR 17RH TO 18RH AND 41RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) ""NEW STRAP IN FS= 319 BETWEEN STGR 17RH TO 18RH AND 41RBL AT PAX CABINFWD WET AREA. (W1) (CPAX) WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 PAR. 6C

Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON FLOOR SUPPORT FS280 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY OF NRC 00193: DUE CORROSION LEVEL 2 ON ANGLE SUPPORT, CRAWLWAY FLOOR FS280 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01

Part: STRINGER — CORRODED (BS 280-349) · airframe 27,988 hrs · 19,246 cycles

CORROSION FOUND ON STRINGER 21R, BS 280 TO 349 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR SPLICE 26RH AND 25RH AT FRAME FS333 MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY: ON NRC. 00170 CORROSION LEVEL 2, STGR SPLICE 26RH AND 25RH AT FRAME FS333 MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 SRM51-42-06-001-001-A01 "

Part: STRINGER — CORRODED (BS 333-364) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION : CORROSION ON STGR 26LH BTW FS333 TO FS364 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09) "SUMMARY: STRINGER 26LH BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 (CORROSION LEVEL 2). "

Part: SUPPORT — CRACKED (BS 797-807) · airframe 27,988 hrs · 19,246 cycles

"AWR; PER MTC REQUEST: [ DURING REMOTION OF MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5 ]: CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL. (FYT) "LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL.WAS REPLACED PER CRJ 900 SRM 51-42-02-001-001-A01 "

Part: STRINGER — CORRODED (BS 280-349) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CORROSION ON STGR22 BTW FS280 TO FS349 AT MAIN AVIONICS COMPARTMENT (SM) "SUMMARY: ON NRC. 00397 CORROSION LEVEL 2, STRINGER 22 RH BTW FS=280 AND FS=349 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "

Part: STRINGER — CORRODED (BS 280-319) · corrosion level 2 · airframe 27,988 hrs · 19,246 cycles

CORROSION FOUND ON STRINGER 19R BETWEEN BS 280 - 319 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 280-295) · airframe 27,988 hrs · 19,246 cycles

"INITIAL INSPECTION: CORROSION ON STGR 18RH BTW FS 280 TO FS 295 AT MAIN AVIONICS COMPARTMENT (SM)M) "SUMMARY: STGR 18RH BTW FS 280 TO FS 295 AT MAIN AVIONICS COMPARTMENTWAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 (CORROSION LEVEL 2). "

Part: ANGLE — CORRODED (BS 310-349) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON KICKPLATE ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "ANGLE KICKPLATE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "

Part: SKIN — DAMAGED (BS 280-295) · airframe 27,988 hrs · 19,246 cycles

"DAMAGE T: CREASE ON FUSELAGE SKIN BTW STA FS:280 AND FS:295 STGR 17RH TO 18RH . (FUS) "SUMMARY: CREASE ON FUSELAGE SKIN BTW STA FS:280 AND FS:295 STGR 17RH TO 18RH,THE DAMAGE MEASURES L:5.600"",W:0.300"" AND D:0.027"" WAS REPAIRED AND WAS FOUND WITHIN LIMITS PER EA N° CRJ953-09923 REV IR

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 27,988 hrs · 19,246 cycles

"AWR; [ TASK R53520 STEP 7 ]: CORROSION ON FLOOR SEAT RAIL IN SECTIONS [ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN FWD WET AREA. (W1) (CPAX) "SUMMARY OF NRC:00303 CORROSION LEVEL 2 ON FLOOR SEAT RAIL IN SECTIONS[ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN FWD WET AREA.(W1)(CPAX) WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG.A07) AND SRM 51-41-02-001-001-A01.

Part: EXHAUST FAN — FAULTY (CABIN) · airframe 26,423 hrs · 18,150 cycles

ON INITIAL DESCENT GOT STRONG BURNING TYPE ODOR WHICH FLIGHT ATTENDANTS ALSO OBSERVED BRIEFLY IN GALLEY WHICH THEN DISSAPATED QUICKLY IN BOTH FLIGHT DECK AND GALLEY. RUN BOTH ENG'S WITH FLIGHT CREW AND RUN LT & RT PACK'S FOR 5-6 MINS. NO ODOR NOTICED. MDC FLAGS EXU FAN DEF GALLEY FAN IAW MEL 21-23-1 PER MOC 96184. PLACARD INSTALLED. (C/B B8 PULLED) REMOVED AND REPLACED GALLEY/LAV EXHAUST FAN IAW AMM 21-23-93 OPS CK GOOD NO ODOR NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,348 hrs · 18,056 cycles

EMERGENCY EXIT SIGNS (LOWER) NOT ILLUMINATED AT ROW 12. BOTH SIDES NOT ILLUMINATED. REMOVED BATTERY PACKS NR 3 AND NR 5, AND INSTALLED SERVICEABLE IAW AMM 33-51-17. EMERGENCY LIGHT OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE. NR 3 PS37 P/N ON/OFF AD-2013-1A S/N OFF 79988 S/N ON 141157. NR 5 PS43 P/N OFF AD-2013-1A P/N ON 2013-1A S/N OFF 71917 S/N ON 98215.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 26,096 hrs · 17,856 cycles

ON WALK AROUND FOUND RH FWD OVERWING EMER LIGHT INOP DEFERRED RH FWD OVRWING EMER LIGHT IAW CRJ 900 MEL 33-51-2C. MM02 UPD ATED PLACARD PLACED MOC # 96211 NOTIFIED.////CLEARING MEL 33-51-2A ( E MER LIGHT) IAW CRJ 900 AMM 33-51-15. MMO2 UPDATED. PLACARD REMOVED/ MO C# 96211 NOTIIFIED. OPS CHECK GOOD AT THIS TIME. A/C OK FOR SVC.

Part: LIGHT — MALFUNCTIONED (LT OVERWING) · airframe 26,096 hrs · 17,856 cycles

ON WALK AROUND FOUND LH AFT OVR WING EMER LIGHT INOP DEFERRED LH AFT OVRWING EMER LIGHT IAW CRJ 900 MEL 33-51-2A. MM02 UPDA TED PLACARD PLACED MOC #96211 NOTIFIED.//// RELAMPED LH AFT EMER LIGHT IAW CRJ 900 AMM 33-51-15. OPS CHECK GOOD MM02 UPDATED PLACARD REMOVED MOC # 96211 NOTIFIED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,911 hrs · 17,698 cycles

UPON INSPECTION FOUND EXTERIOR EMERGENCY LIGHTS 5 AND 6 INOP. FOUND BATTERY PACK 4 NOT WORKING FOR EXTERIOR EMERGENCY LIGHTS 5 AND 6, REMOVED AND REPLACED NR 4 BATTERY PACK (POSITION PS38) IAW JOBCARD 33-900-701 PART B. OPERATIONAL TEST GOOD NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 24,186 hrs · 16,453 cycles

CEILING EMERGENCY LIGHT INOPERATIVE IN THE FIRST CLASS CABIN. FOUND A CONNECTOR PLUG LOOSE AT P5437. OPS TESTED GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 24,082 hrs · 16,382 cycles

RETUREND TO DEPARTURE AFTER TAKEOFF DUE TO FUMES DEVELOPED IN COCKPIT AND CABIN. FUMES WERE STRONG AND RUBBER-LIKE IN NATURE. FUMES CLEARED BEFORE LANDING. COMPLIED WITH FIM 21-21-00, & 21-22-00. NO ABNORMAL ODORS NOTED. OK FOR SERVICE. PERFORMED OF AIR CONDITIONING DISTRIBUTION SYS IAW AMM 21-51-00. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 23,930 hrs · 16,274 cycles

DURING DESCENT THROUGH 16,000 FT, A SMOKE AFT LAVATORY WARNING MESSAGE. WENT BACK TO THE AFT LAV AND CONFIRMED NO PRESENCE OF SMOKE OR FIRE. DUE TO A REPEAT DISCREPANCY OF THE SAME LAVATORY, REMOVED & REPLACED THE AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. CHECKED NORMAL.

Part: FAN — FAILED (AFT LAVATORY) · airframe 23,928 hrs · 16,273 cycles

AFTER DEPARTURE, SMELLED PRESENCE OF SMOKE. RECIEVED A MASTER WARNING FOR SMOKE IN THE AFT LAVATORY. RETURNED TO DEPARTURE. R & R THE AFT LAVATORY FAN AND PERFORMED AN OPS CHECK IAW AMM 21-23-93. AFTER REPLACEMENT, PERFORMED HIGH POWER RUNS FOR APPROXIMATELY 30 MINUTES WITH NO FURTHER DEFECTS NOTED. THE ODOR DISSIPATED, NO SMOKE NOTED, AND EICAS REMAINED CLEAR OF MESSAGES.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 23,928 hrs · 16,272 cycles

PILOTS REPORT LAVATORY SMOKE WITH WARNING ON INCOMING. PERFORMED AN OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM IAW AMM 26-16-00, OPS CHECKED GOOD.

Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 23,726 hrs · 16,112 cycles

CREW REPORTED THE EMERGENCY LIGHTS KEEP TURNING ON AND OFF. MX DISCONNECTED AND CONNECTED ELECTRICAL CONNECTORS ON BATTERY CHARGERS 1, 2, 3, 4, 5. REMOVED AND REPLACED RELAY K198. OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,414 hrs · 14,474 cycles

PILOT REPORTED AFT LAV SMOKE WENT OFF IN FLIGHT. RESET AND DISCREPANCY NO LONGER EXIST. PER MCC NO FURTHER ACTION REQUIRED.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 20,683 hrs · 14,002 cycles

LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. SWAPPED LT FWD & AFT OVERWING EMERGENCY EXIT LIGHTS IAW AMM 33-51-15. AFT EMERGENCY LIGHT OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,347 hrs · 13,755 cycles

EMERGENCY LIGHT ABOVE GALLEY INOPERATIVE, EXTERNAL EMERGENCY LIGHT BESIDE PAX DOOR INOPERATIVE, EXTERNAL EMERGENCY LIGHT LT SIDE AFT OVERWING INOPERATIVE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK CHARGER ASSEMBLY IAW AMM 33-51-17-000-802-A02, & AMM 33-51-17-400-802-A02. OPS TESTED GOOD. EMERGENCY LIGHT ABOVE GALLEY AND EXTERNAL AT PAX DOOR IAW 33-51-00-710-801-A01. FOUND WIRE TO LIGHT UNSECURE. SECURED THE WIRE TO LIGHT ASSY IAW ESPM 20-16. OPS TESTED OF EXTERNAL EMERGENCY LIGHT LT SIDE AFT OVERWING GOOD IAW AMM 33-51-00-710-801-A01.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 20,347 hrs · 13,755 cycles

LT OVERWING EMERGENCY LIGHT HAS DAMAGED CONNECTION TERMINAL PIN & BROKEN WIRES. REMOVED DAMAGED TERMINAL AND REPAIRED BROKEN WIRES IAW ESPM 20-161, AMM 35-51-15-000-801-A08, AND AMM 33-51-15-400-801-A01. OPS GOOD IAW AMM 33-51-15-710-801-A01.

Part: ANGLE — CORRODED · airframe 20,347 hrs · 13,755 cycles

SERVICE DOOR WEB FLOOR PROTECTORS CORRODED (4EA PROTECTOR PLATE MOUNTING ANGLES). REMOVED 4EA DISCREPANT WEB FLOOR PROTECTORS(PROTECTOR PLATE MOUNT ANGLES) FROM SERVICE DOOR SILL REF CRJ900 SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN 4EA NEW, SERVICABLE WEB FLOOR PROTECTORS IAW SRM 51-42-06-001-001-A01 AND ATTACHED TO 4EA ATTACH ANGLES IAW SRM 51-+42-06-001-001-A01. INSTALLED 8EACH NUTPLATES ON 4EA WEB FLOOR PROTECTOR ANGLES IAW SRM 51-42-06-001-001-A01( 2 PER ANGLE AND SEALED IAW SRM TEMP REV 51-0056. ATTACHED 4EA SERVICE DOOR WEB PROTECTORS TO SERVICE DOOR SILL STRUCTURE IAW SRM 51-42-06-001-001 AND TOUCHED UP FASTENHEADS IAW SRM 51-21-16-001-001-A01.

Part: SPLICE PLATE — CORRODED (BS 280) · airframe 20,347 hrs · 13,755 cycles

HEAVY CORROSION ON SPLICE PLATE AFT OF BS 280 AND BETWEEN STRG 26L AND 26R. REMOVED CORROSION FROM BS 280 BUTTSTRAP, UPPER SURFACE BETWEEN FS280-284, STR 26L-26R IAW SRM 51-21-06-001-001 A01. COMPLIED WITH EC/TC EO 32-2016-109 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NONROUTINE WORK CARD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

LT PRESSURE FLOOR SILL FS 693.00-847.00 HAS CORROSION. REMOVED CORROSION ON LT PRESSURE FLOOR SILL FS 693.00-847.00 IAW SRM 51-21-03-001-001 A01. COMPLIED WITH REPAIR EA45-2016-052. COMPLIED WITH ECTC EA 45-2016-052.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

RT PRESSURE FLOOR SILL FS 693.00-847.00 HAS CORROSION. REMOVED CORROSION ON RT PRESSURE FLOOR SILL FS 693.00-847.00 IAW SRM 51-21-06-001-001 A01. COMPLIED WITH REPAIR EA 32-2016-113. RECEIVED & COMPLIED WITH EC/TC EA 32-2016-113.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SIDE SEAT RAIL HAS CORROSION DAMAGE, FS 661.0+16 FS 661.01+90, LT SIDE. EVALUATED LT SIDE SEAT RACK FS 661.0+16-FS 661.0+90. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SEAT RAIL FS 661.0+16-FS 661.0+90 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW FABRICATED SEAT RAIL LT SIDE FS 661.0+16-FS 661.0+90 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

CORROISON ON INTERCOSTAL AT 27L AND BETWEEN FS349-FS364. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11-001-001 A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001 A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOORBEAM AT LBL9, F/S 1015.00 TO F/S 1031.00 HAS CORROSION AROUND BOLT HEAD AND NON BEAM. COMPLIED WITH EC/TC REO 670-53-00-0029, REPAIRED FLOORBEAM AT FS 1015-FS 1031, LBL9 IAW EO 900-53-0023. REMOVED DAMAGED SECTION OF BEAM SECTION TRIMMED NEW SECTION OF BEAM TO FIT & STARTED DRILLING UP BEAM & ANGLE SPLICES AT FWD & AFT SIDE REF SRM 51-40-11-001-001, A01 & REO 670-53-00-029. REPAIRED FLOORBEAM IAW SRM 53-00-41-991-830, & REO 670-53-00-029.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

PASSENGER DOOR THRESHOLD HAS CORROSION ON LOWER FLOOR SUPPORT. REMOVED PASSENGER DOOR LOWER FLOOR SUPPORT IAW SRM 51-42-06-001-001 A01. DRILLED AND INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01 & DWG SH670-31810.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOORBEAM AT LBL 27, F/S 1015.00 TO 1031.00 HAS CORROSION AROUND BOLT HEAD AND NON BEAM. REPAIRED FLOORBEAM AT FS 1031, LBL 27, EECTC EO 900-53-0024 & REO 670-53-00-029.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

CORROSION AT SERVICE DOOR ON UPPER FLOOR SUPPORT. REMOVED AND DRILLED UP NEW UPPER FLOOR SUPPORT AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. INSTALLED NEW UPPER FLOOR SUPPORT ANGLE ON LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-39150, SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

CORROSION ON INTERCOSTAL AT 27R AND BETWEEN FS 349-364. REMOVED INTERCOSTAL IAW SRM 42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED EW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

PAX DOOR THRESHOLD HAS CORROSION ON UPPER FLOOR SUPPORT. REMOVED PAX DOOR UPPER FLOOR SUPPORT IAW SRM 51-42-06-001-001 A01. DRILLED & INSTALLED ANGLE IA AMM 51-42-06-001-001-A01, DWG SH670-31810.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SERVICE DOOR HAS 3 ATTACH ANGLES CORRODED. REMOVED AND DRILLED UP 4 EA NEW ATTACH ANGLES AT SERVICE DOOR IAW SRM 51-42-06-001-001, A01 AND 51-40-11-001-001, A01. ON FURTHER INSPECTION, FOUND 4 EA ATTACH ANGLES THAT WERE CORRODED. INSTALLED THE 4 EA ATTACH ANGLES, LOWER SILL ANGLES TO THE SILL STRUCTURE IAW SRM 51-42-06-001-001, A01 AND DWG SH670-31950. ATTACHED THE 4 EA ATTACH ANGLES TO THE FLOOR PROTECTOR ANGLES IAW SRM 51-42-06-001-001, A01, DWG SH670-31950. RESTORED FINISH, SEALED ATTACH ANGLES AS REQUIRED IAW SRM TEMP REV 51-0056, 51-21-16-001-001, A01 AND APPLIED CIC IAW SRM 51-21-11-001-001, A01.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 20,347 hrs · 13,755 cycles

SERVICE DOOR EXCEEDED MAX FORCE OF 35LBF, MEASURED 45LBF. LUBRICATED GALLEY SERVICE DOOR IAW AMM 12-20-52-640-801-A01. PERFORMED FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR IAW AMM 52-41-00-720-801-A01 TEST GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 847+30-FS 897.79 LT HAS CORROSION DAMAGE. EVALUATED LT SIDE SEAT TRACK FS 847+30-FS 897.79 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK FS 847+30-FS 897.79 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW FABRCIATED SIDE SEAT RAIL LT SIDE FS 847+30-FS 897+79 IAW AMM 53-00-4-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 847.00+64 & 977.00 RT HAS CORROSION DAMAGE. EVALUATED SEAT TRUCK FS847.00+64-FS977.00 RT FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02 SRM 53-51-49-101-001-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN. R & R SEAT STA 847.00+64-977.00 RT IAW AMM 53-00-49-000-801 & 53-00-49-400-801, CONFIGURATION A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK AT LBL9, FS 813.70-847+62 HAS CORROSION. SEAT TRACK AT LBL9, FS 813.70-847+62 IS CORRODED OUT OF LIMITS IAW SRM 53-31-49-01-001-A02. R & R SEAT TRACK AT LBL9, FS 813.70-847+62 IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK AT RBL9, FS 813.70-847+12 HAS CORROSION. REMOVED SEAT TRACK, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02 AMM 53-00-49-000-801-A017. REPLACED SEAT TRACK ON RBL9, FS 813.70 -847+62 IAW AMM 53-00-49-400-01-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 847.00+8.39 & 847.00+64 RT HAS CORROSION DAMAGE. EVALUATED SIDE SEAT TRACK FS 847.00+8.39-FS 847.00+64 RT FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SIDE SEAT TRACK FS 847.00+8.39 - 847.00+64 RT IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07. COMPLIED WITH ECTC GREO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 785-14 & FS 847.00+839 RT HAS CORROSION DAMAGE. EVALUATED RT SIDE SEAT RAIL BETWEEN FS 785.14-FS 847.00 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN. REMOVED RT SIDE SEAT TRACK AT FS 785.16-8614.00 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801, CONFIGURATION A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 662 AND 720.85 LT HAS CORROSION DAMAGE. EVALUATED LT SIDE SEAT RACK FS662-720.85, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SEAT RAIL FS662-FS720.85 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW FABRCIATED SEAT RAIL LT SIDE FS 662-720.85 IAW AMM 53-00-4-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 744-14 & FS 761-86 RT HAS CORROSION DAMAGE. EVALUATED RT SIDE SEAT TRACK FS 744.14-FS 761.86. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-10-001-A02. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN. REMOVED SEAT TRACK AT FS 744.14 & FS 761.86 RT IAW AMM 53-00-49-000-801-A07. INSTALLED SEAT TRACK AT FS 744.18 & FS 761.86 RT IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS485-FS581, LBL27. SEAT TRACK OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. R & R SEAT RAIL AT FS 485-581, LFL27 IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

280 CROSSBEAM HAS CORROSION DAMAGE BETWEEN LBL9 AND RBL9. REMOVED 280 CROSSBEAM FORWARD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-20-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW 280 CROSSBEAM FORWARD SUPPORT ANGLE IAW SRM 51-40-11-001-001 A01, 51-42-20-001-001 A01 AND 51-42-06-001-001-A01 REF SB 670BA-53-041.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 20,347 hrs · 13,755 cycles

VERTICAL STABILIZER RT AFT DRAG ANGLE CRACKED AT FWD END. REMOVED CRACKED RT AFT DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, LOCATED HOLES IN NEW DRAG ANGLE IAW SRM 51-40-11-001-001-A01. COUNTER SUNK AND STARTED TO INSTALL IAW SRM 51-42-21-001-001 A01 AND 51-42-22-001-001-A01. FINISHED INSTALLING AFT DRAG ANGLE IAW SRM 51-12-21-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS 379-FS 485, RBL9. EVALUATED FLOOR SEAT TRACK, RBL 9, FS 379-FS 485 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02, SRM 53-21-49-400-101-001-A01. R & R FLOOR SEAT RAIL ON RBL9 AT FS 379-485 IAW SRM 53-00-49-000-801-A07, 53-00-49-400-801-A01. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: RETAINER — CHAFED (CARGO DOOR) · airframe 20,347 hrs · 13,755 cycles

FWD CARGO DOOR LOWER OTBD SEAL RETAINER FWD END CHAFED AFT END CHAFED AND DENIED. COMPLIED WITH EC/TC REO 690-52-35-013, PERMANENT REPAIR FOR DAMAGE TO FWD CARGO DOOR LOWER SRM RETAINER AND EO 670-52-35-013, REV B DATED 1/8/15 AS WRITTEN.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 897.79 & 954.00 LT HAS CORROSION DAMAGE. EVALUATED LT SIDE SEAT TRACK FS 897.79-FS 954.00 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK FS 897.79-FS 854 LT IAW AMM 53-00-49-000-801, CONFIGURATION A07 & 53-00-4-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS 379-FS 485, LBL27. EVALUATE FLOOR SEAT RAIL LBL27, FS 379-FS 485 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001 A01. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M. R & R SEAT RAIL IAW AMM 53-00-49-000-801 & 53-00-49-400-801 A07.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 20,347 hrs · 13,755 cycles

VERTICAL STABILIZER LT AFT DRAG ANGLE CRACKED AT FWD END. REMOVED ATTACHING FASTENERS WITH THE EXCEPTION OF 2 EA THAT STILL NEED REMOVED IAW SRM 51-42-21-001-001 A01, 51-42-13-001-001 A01 & 51-42-22-001-001 A01. LOCATED AND DRILLED NEW DRAG ANGLE IAW SRM 51-40-11-001-001 A01. REMOVED LAST 23 FASTENERS AND REMOVED OLD DRAG ANGLE IAW SRM 51-42-21-001-001 A01. COUNTERSINK FASTENER HOLES AND INSTALLED NEW VERTICAL STABILIZER LT AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-27-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT RAIL AT LBL 9 HAS CORROSION DAMAGE AT FS 349.00 AND FS 437.00. SEAT RAIL BEYOND ALLOWABLE LIMITS OF SRM 53-31-49-101-001-A02. R & R SEAT RAIL.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SERVICE DOOR THRESHOLD HAS CORROSION DAMAGE. LOCATED FASTENERS HOLES IN SERVICABLE MOUNTING ANGLE IAW SRM 51-42-06-00-001-001-A01 AND DWG SH670-31980, SRM 51-40-11-001-001-A01. INSTALLED THE LOWER MOUNTING ANGLE ON SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-+21-001-001-A01 AND DWG SH6470-31950. SEALED SERVICE DOOR MOUNTING ANGLE, RESTORED FINISH AND APPLIED CIC AS REQUIRED IAW SRM, REV 51-0056, 51-21-11-001-001-A01, 51-21-16-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS 661.0+32-FS693, RBL9. EVALUATED FLOOR SEAT RAIL, FS 661.00+32 -FS 693 RBL9 FOUND TO BE OUT OF LIMITS IAW REO 670-53-31-49 101-001-A07, 53-41-49-101-001-A02. REMOVED FLOOR SEAT RAIL FS 661.00+32-FS 693, RBL9 IAW REO 670-53-31-49, 101-001-A07, 53-41-49-000-001-A07. INSTALLED NEW FABRICATED SEAT RAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK BETWEEN FS 785.15-FS 830.54 LT HAS CORROSION DAMAGE. EVALUATED LT SIDE SEAT RACK 785.15-830.54 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT RAIL FS 785.15 AND 830.54 LT IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07 AND SRM 51-40-11-001-001-A01. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 20,347 hrs · 13,755 cycles

LEFT ELECTRICAL BAY FLOOR CRACKED FS 193. REPAIRED CRACKS IN FS 193 ELECTRICAL BAY FLOOR LT SIDE AND/OR RT SIDE IAW REO 670-53-11-509, REV C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS581-FS661.0+32, RBL9. EVALUATED FLOOR SIDE SEAT RAIL, FS 581-FS 661.0+32, RBL 9 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED CORRODED SEAT RAIL AT RBL9, FS 581-661+32 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M. INSTALLED SEAT RAIL AT RBL9 FS 581-661+32 IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK AT RBL9 FS 847+62-927.00 HAS CORROSION. REMOVED CORRODED SEAT TRACK AT RBL9 FS 847+62-977 IAW AMM 53-00-49-000-801 A07. INSTALLED NEW SEAT RAIL AT RBL9 FS 847+62-977 IAW AMM 53-00-49-400-801 A07. COMPLIED WITH EC/TC FREO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 20,347 hrs · 13,755 cycles

RT ELECTRICAL BAY FLOOR CRACKED, FS 193. REPAIRED CRACK IN FS 193 ELECTRICAL BAY FLOOR, RT SIDE IAW REO 670-53-11-509, REV C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE, FS581-FS661.0+32, LBL9. SEAT TRACK OUT OF LIMITS IAW SRM 53-31-49-101-001 A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M. REMOVED & INSTALLED SEAT RAIL IAW AMM 53-00-49-000-801 A07, 53-00-49-400-801 A07.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

CORROSION ON FRAME AT FS 333 ANDC ON LT AND RT SIDE OF STR 27. REMOVED CORROSION ON FRAME AT FS 333 IAW SRM 51-21-06-001-001-A01, EA 32-2016-104. RECEIVED EA 32-2014-105 HAS BEEN ACCOMPLISHED.

Part: SKIN — CORRODED (PAX DOOR) · airframe 20,347 hrs · 13,755 cycles

CORROSION FOUND ON PASSENGER DOOR INTERNAL SKIN AT CLOSING PLATE AREA. REMOVED CORROSION OFF PASSENGER DOOR INTERNAL SKIN IAW SRN 51-12-00-001-001-A01. COMPLIED WITH EC/TC EA 32-2016-105, REV D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

FLOOR SEAT RAIL HAS CORROSION DAMAGE FS485-FS581, RBL9. EVALUATED FLOOR SEAT RAIL FS 485-FS 581, RBL9 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. R & R SEAT RAIL AT FS 485-581 ON RBL9 IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07. COMPLIED WITH ECTC GREO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SIDE SEAT RAIL HAS CORROSION DAMAGE, FS 581-661.0+16, LT SIDE. EVALUATED SIDE SEAT RAIL, LT SIDE FS581 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. R & R SIDE SEAT RAIL, FS 581-661 LT SIDE IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SEAT TRACK AT LBL9, FS 847+62-927.00 HAS CORROSION. EVALUATED AND REMOVED SEAT TRACK AT LBL9, FS 847+62-FS 977 IAW AMM 53-00-49-00-801-A07 OUT OF LIMITS IAW SRM 53-51-49-101-001-A02 AND SRM 53-41-49-101-001-A02. INSTALLED NEW FABRICATED SEAT TRACK AT LBL9, FS 847+62- FS 977 IAW AMM 53-00-49-00-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,347 hrs · 13,755 cycles

SIDE SEAT RAIL HAS CORROSION DAMAGE, FS 661.0+16-FS 677.00, RT SIDE. SEAT TRACK OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. R & R SIDE SEAT RAIL FS 661-FS 677 RT SIDE IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-00-343.

Part: SKIN — DENTED (TAILCONE) · airframe 20,347 hrs · 13,755 cycles

DENT IN TAILCONE LEFT SKIN AT THE 6:00 POSITION. VERIFIED ALL STEPS OF PERMANENT REPAIR WERE COMPLIED WITH ON STS EA32-2014-308. AND COMPLIED WITH ECTC EA32-2014-308.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,176 hrs · 13,630 cycles

AFTER CHANGING BATTERY FOR MEGAPHONE, MEGAPHONE STOPPED WORKING. R & R AFT MEGAPHONE IAW AMM 25-61-14.

Part: MEGAPHONE — DAMAGED (NOT REPORTED) · airframe 19,020 hrs · 12,812 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,743 hrs · 12,611 cycles

RIGHT EXTRENAL EMERGENCY LIGHT AFT SERVICE DOOR WILL NOT TURN ON. R & R NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-17, REF IPC 33-51-17, FIG 1, ITEM 6. OPS CHECK GOOD.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 18,097 hrs · 12,104 cycles

FWD CARGO DOOR SEAL RETAINER BENT AT LOWER AFT CORNER. DRESSED BACK DAMAGE ON FWD CARGO SEAL RETAINER LOWER AFT CORNER IAW REO 670-52-35-127, REV C, PERMANENT REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,609 hrs · 10,414 cycles

EMERGENCY LIGHT INOPERATIVE AND COVER MISSING AFT OF SERVICE DOOR. EMERGENCY LIGHT R & R IAW AMM 33-51-11.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 14,593 hrs · 9,700 cycles

RIGHT OVERWING EMERGENCY LIGHTS NEG AND POS CONTACTS ARE BROKEN OFF IN THE RECEPTICALS. REMOVED BROKEN CONTACTS IAW ESPM 20-16-00. TERMINATED WIRES IAW ESPM 20-16-00. PERFORMED OPS TEST OF EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-15-710-801. OPS CHECKED GOOD.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 14,593 hrs · 9,700 cycles

CORROSION FOUND ON BS 280 BULKHEAD WEB. BLENDED CORRSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,593 hrs · 9,700 cycles

CORROSION FOUND ON FWD SIDE OF BS 280 FLOORBEAM, UPPER EDGE, COVERING AREA BL 0-RBL 10. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPLACED FLOORBEAM. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED · airframe 14,593 hrs · 9,700 cycles

RT FLOORBEAM FOUND CRACKED DURING NDI IAW SB670BA-53-01-041 01, ITEM 106 & 107. REPAIRED IAW REO 690-53-11-641. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 14,593 hrs · 9,700 cycles

FLOORBEAM FOUND CRACKED DURING NDI IAW SB670BA-53-041-01, ITEM 106 & 107. REPAIRED IAW REO 690-53-11-641, REV. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,593 hrs · 9,700 cycles

CORROSION FOUND ON FWD SIDE OF LT 280 FLOORBEAM, UPPER EDGE, BL 0 TO LBL 10. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01 DWG SH670-32153. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 14,593 hrs · 9,700 cycles

SEAT TRACK AT BS 785.15 & S15L CORRODED, SIDE WALL. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 14,593 hrs · 9,700 cycles

SIDE WALL SEAT TRACK BS 720.85 CORRODED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW EC/TC REO 670-53-00-013. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: DOUBLER — CORRODED (ANTENNA) · airframe 14,593 hrs · 9,700 cycles

TCAS ANTENNA DOUBLER CORRODED. REMOVED CORROSION IAW SRM 51-21-06 AT TCAS DOUBLER DETERMINED OUT OF LIMITS IAW SRM 53-00-00. REPLACED TCAS DOUBLER IAW SRM 51-42-06 DWG SH670-32364.

Part: FRAME — CORRODED (BS 333) · airframe 14,593 hrs · 9,700 cycles

FRAME BS 333 CORRODED ON FWD SIDE BETWEEN S26 & 27L. REMOVED CORROSION IAW SRM 51-26-06. DAMAGE IS IN A NO DAMAGE ALLOWED AREA IAW SRM 53-21-06. COMPLIED WITH REO 690-53-21-614.

Part: SEAT TRACK — CORRODED (BS 752) · airframe 14,593 hrs · 9,700 cycles

SIDEWALL SEAT TRACK AT BS 752.5 & S15L CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A07. INSTALLE SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 752) · airframe 14,593 hrs · 9,700 cycles

SIDEWALL SEAT TRACK AT BS 752.5 & S15R CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: FRAME — CORRODED (BS 319.7) · airframe 14,593 hrs · 9,700 cycles

FRAME BS 319.7 CORRODED ON FWD SIDE FROM S26L-26R REMOVED CORROSION IAW SRM 51-21-06. COMPLIED WITH REO 690-53-21-615. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 14,593 hrs · 9,700 cycles

SIDE WALL SEAT TRACK BS 785.15 & S15R CORRODED. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 785.15-847+16.00 IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 14,593 hrs · 9,700 cycles

SIDE WALL SEAT TRACK BS 720.85 CORRODED. FOUND CORROSION TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 14,593 hrs · 9,700 cycles

INTERCOSTAL S27 BS 364 CORRODED. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. DRILLED, LOCATED & INSTALLED NEW INTERCOSTAL IAW DWG SH670-32075 & SRM 51-42-06-001-001. MAJOR REPAIR.

Part: SKIN — CHAFED (BS 913-927) · airframe 14,593 hrs · 9,700 cycles

AFT LOWER BELLY SKIN CHAFED AT BS 913-927. COMPLIED WITH EC/TC 670-53-00-290 AT STA 913-927 AND REO 670-53-00-290, REV B. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 14,593 hrs · 9,700 cycles

FLOOR SUPPORT THAT ATTACHES TO BS 280 FLOORBEAM CORRODED. REMOVED OF FLOOR SUPPORT IAW SRM 51-42-06-001-001. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 14,593 hrs · 9,700 cycles

SEAT TRACK SEGMENT CORRODED LBL 9 AND BS 661+32 - 693. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, STEP 1-4. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: DOOR — LACK OF LUBE (LT OVERWING) · airframe 14,593 hrs · 9,700 cycles

LEFT FWD OVERWING EMERGENCY EXIT FAILED FUNCTIONAL CHECK AT 60 LB MAX IS 40. LUBED LT FWD OVERWING EMERGENCY EXIT IAW AMM 12-20-52, TASK 12-20-52-640-802. COMPLIED WITH EMERGENCY EXIT DOOR FUNCTIONAL CHECK, LEFT FRONT DOOR IAW AMM 52-21-00-720-802, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 14,550 hrs · 9,672 cycles

FORWARD GALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK, 60LB MAX IS 35LB. LUBED FWD GALLEY SERVICE DOOR IAW AMM 12-20-52, TASK 12-20-52-640-801 COMPLIED WITH FUNCTIONAL CHECK IAW MM 52-41-00, TASK 52-41-00-720-801, CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 14,155 hrs · 9,426 cycles

AFT EMERGENCY LIGHTS INOPERATIVE AND FLOOD LIGHTS INOPERATIVE. R & R NR 5 BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 12,961 hrs · 8,664 cycles

ILLUMINATED STRIPS AROUND GALLEY SERVICE DOOR DAMAGED/MISSING. PERFORMED VISUAL INSP OF ILLUMINATED STRIPS IAW AMM 33-51-01. ALL CHECKS GOOD AT THIS TIME.

Part: LOOP — OUT OF POSITION (WING) · airframe 11,520 hrs · 7,769 cycles

ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT IN ICING CONDITION, FOLLOWED AFTER APPROX 30 SECONDS BY ANTI-ICE DUCT CAUTION MSG. COMPLIED WITH QRH. EMERGENCY DECLARED, AND ACFT RETURNED TO DEPARTURE. MDC FLAGGED RT WING LOOP A AT SLAT STA 430R AND RT WING LOOP B AT SS 238R, FOUND LOOP AT BOTH LOCATIONS NEEDING TO BE REPOSITIONED. REPOSITIONED LOOP AT SS 430R IAW AMM 36-21-15 AND LOOPS AT SS238R IAW AMM 36-21-13. NO FURTHER DEFECTS NOTED WHILE RUNNING ENGINES.

Part: ACM — SMOKE (LEFT) · airframe 11,030 hrs · 7,469 cycles

SMOKE IN COCKPIT ON APPROACH. R & R LEFT ACM IAW AMM 21-51-08. CHECKED GOOD.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 8,960 hrs · 6,141 cycles

ANTI-ICE DUCT WARNING MSG INFLIGHT, RAN QRH AND ADVISED TO AVOID ICING CONDITIONS. (EMERGENCY DECLARED AS A PRECAUTION) TROUBLE SHOT IAW 36-21-07. PERFORMED AILC BYTE TEST IAW AMM 630-12-12. OPS CHECK GOOD. PERFORMED ENG RUN. OPS CHECK IAW AMM 30-12-00, ALL MSG CLEARED SYS, OPS CHECK GOOD. (SDR CLOSED)

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 8,847 hrs · 6,069 cycles

EMERGENCY LIGHTS ON FA STATION AND GALLEY AREA ARE INOPERATIVE. R & R EMERGENCY LIGHTS NR 1 BATTERY AND CHARGER ASSY IAW AMM 33-51-17-000-802 AND PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,847 hrs · 6,069 cycles

CRACK ON AFT DRAG ANGLE PAX DOOR. REPAIRED IAW SRM 52-11-04-201-002-A01 PARA 4. (3)-5A. THIS IS A MAJOR REPAIR.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 8,847 hrs · 6,069 cycles

RT WING EMERGENCY LIGHT ON PANEL 172CR HAS BROKEN WIRES. CRIMPED NEW PINS TO LIGHT ASSY IAW ESPM 20-16-00. PERFORM OPS TEST OF RT WING EMERGENCY LIGHT IAW AMM 33-51-00-710-801. PERFORMED OPS TEST OF THE RT WING EMERGENCY LIGHT IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: SKIN — CHAFED (BS 916) · airframe 8,847 hrs · 6,069 cycles

EXTERNAL AFT FUSELAGE SKIN CHAFED AT APROX. FS 916. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 349-379) · airframe 8,843 hrs · 6,065 cycles

SEAT TRACK AT RBL9, FS 349 TO 379 HAS SURFACE CORROSION ENTIRE LEGNTH AREA MARKED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A01 FOUND TO BE DAMAGED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: FITTING — BROKEN (LT PYLON) · airframe 8,843 hrs · 6,065 cycles

CLIP BROKEN TOP OF LT PYLON. R & R CLIP ON TOP LT PYLON IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001-A01 & SRM 51-21-11-001-001-A01 & SRM 51-25-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 790) · airframe 8,843 hrs · 6,065 cycles

SEAT TRACK SIDE RT AT FS 790 HAS SURFACE CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,435 hrs · 5,169 cycles

CRACK FOUND ON AFT DRAG ANGLE DUE REINSPECT. COMPLIED WITH REINSPECT OF THE CRACK FOUND, NO FURTHER DEFECTS NOTED. OK FOR CONTINUED SERVICE IAW REO 690-52-11-0026.

Part: CONTROLLER — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 7,227 hrs · 5,017 cycles

LT WING ANTI ICE CAUTION WHILE TROUBLESHOOTING ANTI ICE DUCT WARNING. (ENROUTE ACFT DIVERTED, DUE TO MX -- EMERGENCY DECLARED). PERFORMED OPS TEST OF ANTI ICE CONTROLLER AND INDICATING SYS IAW AMM 30-12-00 AND LEAK TEST OF WING ANTI ICE DUCT IAW AMM 30-11-00, NO DEFECTS NOTED, OK FOR SERVICE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 6,184 hrs · 4,350 cycles

CRACK FOUND ON AFT DRAG ANGLE OF PASSENGER DOOR NEAR FILLING. REPAIRED IAW SRM 52-11-04-201-002-A01

Part: HANDLE — BINDING (PAX DOOR) · airframe 5,906 hrs · 4,184 cycles

RAMP REPORTS PAX DOOR DIFFICULT TO OPEN. LUBRICATED DOOR HANDLE MECHANISM AND OPERATED DOOR SEVERAL TIMES. OPS CK GOOD IAW AMM 52-11-00. (CLOSED)

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 4,115 hrs · 2,988 cycles

F/A REPORTED MEGAPHONE INOP.

Part: WARNING SYSTEM — ACTIVATED (STEERING SYSTEM) · airframe 2,369 hrs · 1,778 cycles

NOSEWHEEL STEERING INOP MESSAGE ILLUMINATED UPON GEAR RETRACTION, EMERGENCY DECLARED.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 2,323 hrs · 1,739 cycles

NOSE WHEEL STEERING INOPERATIVE, LANDED WITH STEERING OFF.