N391CA

Part: CONTACT — DAMAGED · airframe 40,907 hrs · 30,382 cycles

PASSENGER COMPARTMENT CEILING PANEL (243CLC) HAS A BROKEN WIRE FOR EMERGENCY LIGHTS NSTALLED NEW CONTACT ON P357 WIRE BUNDLE IAW CRJ 700 ESPM 20-16-11. OPS TEST GOOD.

Part: BULKHEAD — CORRODED · airframe 40,907 hrs · 30,382 cycles

AFT SIDE OF NLG BULKHEAD IS CORRODED AT F.S. 235.00 BETWEEN STGR 26L AND 26R. REPAIRED BULKHEAD FRAME AT F.S. 235.00 IAW MHIRJ REO 670-53-11-1800 REV -- DATED 5/23/22.

Part: FRAME — CORRODED · airframe 40,907 hrs · 30,382 cycles

F.S. 863.00 FRAME IS CORRODED BETWEEN STGR 26L AND 26R. REPAIRED F.S. 863.00 FRAME IAW ENDEAVOR EA CRJ753-13478 REV IR DATED 4/29/22.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

R/H SIDE SEAT TRACK BETWEEN F.S. 784.00 TO F.S. 861.00 IS CORRODED. REMOVED AND REPLACED SEAT TRACK I.A.W. BOMBARDIER CRJ700 AMM 53-00-49-000/400-801-A03.

Part: FRAME — CORRODED · airframe 40,907 hrs · 30,382 cycles

FRAME 364.00 IS CORRODED BETWEEN STRINGER 26R AND STRINGER 27. REPAIRED FRAME I.A.W. BOMBARDIER REO 670-53-21-687 REV.A, DATED 2016-06-06.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 9.00 SEAT TRACK IS CORRODED BETWEEN F.S. 1000.00 TO F.S. 1051.30. REMOVED AND REPLACED CORRODED L/H SEAT TRACK I.A.W. BOMBARDIER CRJ700 AMM 53-00-49-000/400-801-A03.

Part: BEAM — CORRODED · airframe 40,907 hrs · 30,382 cycles

FLOOR BEAM AT LBL 9.0 FS 1000-1033 HAS CORROSION ON UPPER SURFACE. BLENDED UPPER SURFACE OF FLOOR BEAM . FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-61-43-101-001-A01. REMOVED AND REPLACED FLOOR BEAM SEGMENT FROM FS 977.00 TO FS 1037.00 IAW CRJ 700 SRM 53-00-41-201-001-A01. REMOVED AND INSTALLED SEAT TRACK IAW CRJ 700 53-00-49-000/400-801-A03.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 27 FLOOR BEAM IS CORRODED BETWEEN F.S. 1015.00 AND 1096.00. BLENDED AND REPAIRED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01 AND ENDEAVOR EA# CRJ753-13566 REV IR DATED 5/8/22.

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

STRINGER 24R IS CORRODED BETWEEN F.S. 333.00 AND 364.00. REPAIRED STRINGER 24R IAW CRJ 700 SRM 53-00-03-201-001-A01.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

STRINGER CLIP CORRODED AT STRINGER 21R AND FS 379.00. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN F.S. 349.00 AND 364.00. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 9 SEAT TRACK IS CORRODED BETWEEN FS985 -FS1000. REMOVED RBL 9 SEAT TRACK. FABRIACTED SEAT TRACK AND INSTALLED A SERVICEABLE SEAT TRACK AT RBL 9 BETWEEN F.S. 985 TO F.S. 1000 IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A17.

Part: ANGLE — CRACKED · airframe 40,907 hrs · 30,382 cycles

221ALF R/H FLOOR SUPPORT ANGLE CRACKED. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

STGR20R IS CORRODED BETWEEN FS310 AND FS319 REPLACED STGR20R BETWEEN FS280 AND FS319 IAW CRJ-700 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: GUSSET — WORN · airframe 40,907 hrs · 30,382 cycles

UPON REMOVING FS319 AND FS333 CLEAT FOUND GUSSET AT FS319 TO HAVE ELONGATED HOLES. REPLACED GUSSET AT FS319 AND STGR20R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: SPLICE — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION FOUND ON STGR JOINT SPLICE AT FS333 AND STGR21R . REPLACED STGR JOINT SLPICE AT FS333 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION FOUND ON STGR23R BETWEEN FS364 AND FS379. REPLACED STGR 23R PN: SH670-31380-1 BETWEEN FS333 AND FS379 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: BRACKET — CORRODED · airframe 40,907 hrs · 30,382 cycles

AVIONICS BRACKET ON STGR21R BETWEEN FS349 AND FS364 IS CORRODED. REPLACED BRACKET ON STGR21R BETWEEN FS349 AND FS364 IAW CRJ-700 SRM 53-42-13-001-001-A01.

Part: CLEAT — CORRODED · airframe 40,907 hrs · 30,382 cycles

UPON GAINING ACCESS TO REMOVED FS295 FRAME FOUND GROUNDING POINT BRACKET AT FS333 STGR21R FOUND TO BE CORRODED. REPLACED GROUNDING POINT CLEAT PN: SH670-32605-2 AT FS333 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: CLEAT — CORRODED · airframe 40,907 hrs · 30,382 cycles

UPON GAINING ACCESS TO REMOVED FS295 FRAME FOUND GROUNDING POINT BRACKET AT FS319 STGR21R FOUND TO BE CORRODED. REPLACED GROUNDING POINT CLEAT PN: SH670-32695-7 AT FS319 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: CLEAT — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION FOUND AT STGR CLEAT LOCATED AT FS349 AND STGR21R. REPLACED STRG 21R CLEAT AT FS349 IAW CRJ-700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION FOUND AT STGR 21R BETWEEN FS333 TO FS349. REPLACED STRG 21R BETWEEN FS333 AND FS379 IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR LOWER SILL PLATE CORRODED. REPLACED PAX DOOR LOWER SILL PLATE IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-15-001-001-A01

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR LOWER SILL MID CAP ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL MID CAP ANGLE IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-15-001-001-A01

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR AFT HANDRAIL CLIP IS CORRODED. REPLACED PAX DOOR HANDRAIL CLIP LOCATED AT STGR 18L FS342 IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-15-001-001-A01

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR FWD HANDRAIL CLIP IS CORRODED. REPLACED PAX DOOR HANDRAIL CLIP LOCATED AT STGR 18L FS314 IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-15-001-001-A01

Part: CLEAT — CORRODED · airframe 40,907 hrs · 30,382 cycles

CLEAT AT STRINGER 20R IS CORRODED BETWEEN F.S. 310.00 AND F.S. 319.00. REMOVED AND REPLACED CLEAT I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A1 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION FOUND AT STRINGER 21R BETWEEN F.S. 319.00 AND F.S. 333.00. REMOVED AND REPLACED STRINGER SEGMENT I.A.W. BOMBARDIER CRJ700 SRM 53-21-03-101-002-A01.

Part: WEB — CORRODED · airframe 40,907 hrs · 30,382 cycles

FWD PAX DOOR WEB PANEL CORRODED ON UPPER SIDE AND LOWER SIDE. REMOVED & REPLACED PANEL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.

Part: DOUBLER — CORRODED · airframe 40,907 hrs · 30,382 cycles

DOUBLER AT STRINGER 26L BETWEEN F.S. 533.00 AND F.S. 581.00 IS CORRODED AND GOUGED. REPAIRED DAMAGE I.A.W. ENDEAVOR AIRLINES EA# CRJ753-13466 REV.IR, DATED 05/07/2022.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

L/H AND R/H JACK FITTING SUPPORT INTERCOSTALS BETWEEN F.S. 265.00 AND F.S. 280.00 ARE CORRODED. REMOVED AND REPLACED L/H AND R/H JACK FITTING SUPPORT INTERCOSTALS I.A.W. ENDEAVOR AIRLINES EA# CRJ753-13413 REV.IR, DATED 04/19/2022.

Part: WEB — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR AFT WEB CORRODED ON UPPER AND LOWER SIDES. REMOVED AND REPLACED PAX DOOR AFT WEB I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PASSENGER DOOR BOTTOM ANGLE FOUND TO BE CORRODED. REMOVED AND REPLACED PASSENGER DOOR BOTTOM ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FRAME — CORRODED · airframe 40,907 hrs · 30,382 cycles

FRAME CORRODED AT F.S. 250, BETWEEN STGR 26L AND 26R. SPLICE REPAIRED FRAME SECTOR IAW ENDEAVOR AIR EA CRJ753-13396.

Part: STIFFENER — CORRODED · airframe 40,907 hrs · 30,382 cycles

5 STIFFENERS ON TOP PANEL FOR PASSENGER DOOR FOUND TO BE CORRODED. REMOVED AND REPLACED STIFFENERS IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: NONE — CRACKED · airframe 40,907 hrs · 30,382 cycles

CRACK ABOVE RH AFT TRU BAY DOOR LATCH ON DOOR LANDING REMOVED &REPLACED LANDING IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: SKIN — CORRODED · airframe 40,907 hrs · 30,382 cycles

PASSENGER DOOR INNER SKIN IS CORRODED AT F.S.338.0 BETWEEN DOOR DATUM A1 AND 1 REMOVED AND REPLACED PASSENGER DOOR INNER SKIN IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01. AND 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL JUST LEFT OF STRINGER 27 BETWEEN F.S.349 AND F.S.364 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL LEFT OF STRINGER 27 BETWEEN F.S. 349 TO FS 364 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FITTING — CORRODED · airframe 40,907 hrs · 30,382 cycles

INSIDE CABIN AT F.S.310 LH SILL, PASSENGER DOOR FORWARD FRAME FLOOR LEVEL, TEAR STRAP IS CORRODED. REMOVED AND REPLACED FLOOR BEAM FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.

Part: NONE — CHAFED · airframe 40,907 hrs · 30,382 cycles

RIGHT HAND UPPER TRANS COWL LATCH DOOR AND DOOR CUT OUT IS CHAFED. REMOVED AND REPLACED LATCH DOOR CUT OUT IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND BOMBARDIER REO 670-54-21-1207.

Part: HINGE FITTING — CORRODED · airframe 40,907 hrs · 30,382 cycles

O/B PCU LUG "F" ON RH AILERON HAS CORROSION ON INNER BORE AND FOUND TO BE PREVIOUSLY OVERSIZED. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.

Part: HINGE FITTING — CORRODED · airframe 40,907 hrs · 30,382 cycles

CENTER HINGE PCU LUGS "C" AND "F" ON LH AILERON HAVE CORROSION ON INNER BORES BOTH HAVE BEEN PREVIOUSLY OVERSIZED. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.

Part: DOUBLER — CORRODED · airframe 40,907 hrs · 30,382 cycles

ANTENNA DOUBLER CORRODED BETWEEN FS 1031.00 AND FS 1047.00 RIGHT OF STGR 27. REMOVED & REPLACED DOUBLER IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.

Part: HINGE FITTING — NONE · airframe 40,907 hrs · 30,382 cycles

RH AILERON LUG MARKED "C" CAME IN WITH O/S BORE. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.

Part: DIAPHRAGM — CRACKED · airframe 40,907 hrs · 30,382 cycles

AFT CARGO DOOR, AFT DOOR TRACK DIAPHRAGM FOR DOOR TRACK IS CRACKED AT F.S. 1047.00. REMOVED AND REPLACED AFT CARGO DOOR TRACK DIAPHRAGM I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-52-21-001-001-A01.

Part: FITTING — CORRODED · airframe 40,907 hrs · 30,382 cycles

MACHINED FITTING AT F.S. 533.00 BETWEEN STGR 22L AND STGR 23L IS CORRODED. REMOVED AND REPLACED FITTING I.A.W. BOMBARDIER CRJ700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

AFT CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED SILL I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: DOUBLER — CORRODED · airframe 40,907 hrs · 30,382 cycles

H DOUBLER CORRODED AT STGR 26L FS 533.00 REMOVED AND REPLACED DOUBLER I.A.W. BOMBARDIER CRJ700 SRM 51-42-24-001-001-A01, 51-21-06-001-001-A01, 51-42-22-001-001-A01 AND 51-12-00-001-001-A01.

Part: STIFFENER — CORRODED · airframe 40,907 hrs · 30,382 cycles

UPON REMOVAL FOUND 2EA. SIDE PANEL STIFFENERS TO BE DAMAGED, REQUIRES REPLACEMENT. REMOVED AND REPLACED PASSENGER DOOR AFT WEB STIFFENERS IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FORMER — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR FORWARD DOOR FORMER IS CORRODED AT F.S. 311.00 BETWEEN DD5 AND DD6. REMOVED AND REPLACED FORMER I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR FRAME CORRODED BETWEEN DD4 AND DD5. APPROX. F.S. 313.56. REMOVED AND REPLACED FRAME I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR FWD FORMER SUPPORT ANGLE FOUND TO BE CORRODED (P/N: 601R318731-3). REMOVED AND REPLACED ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR INTERCOSTAL IS CORRODED AT DD4 BETWEEN F.S. 311.00 AND F.S. 320.00. REMOVED AND REPLACED INTERCOSTAL I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LH SIDE SEAT TRACK BETWEEN FS 785 TO FS 708 IS CORRODED REMOVED AND REPLACED SEAT TRACK I.A.W. BOMBARDIER CRJ700 AMM 53-00-49-000/400-801-A17.

Part: LONGERON — CORRODED · airframe 40,907 hrs · 30,382 cycles

LONGERON CORRODED AT STR 25R BETWEEN F.S. 333.00 AND F.S. 349.00. REMOVED AND REPLACED LONGERON I.A.W. BOMBARDIER CRJ700 SRM 53-21-23-101-003-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

UPON REMOVAL FOUND DRAG ANGLE TO BE CORRODED, REQUIRES REPLACEMENT. REMOVED AND REPLACED DRAG ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

PAX DOOR INTERCOSTAL CORRODED AT DD6 BETWEEN F.S. 311.00 AND F.S. 320.00. REMOVED AND REPLACED INTERCOSTAL I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 847 - FS 985. REMOVED & REPLACED SEAT RAIL IAW CRJ 700 53-00-49-000/400-801-A03.

Part: HINGE — WORN · airframe 40,907 hrs · 30,382 cycles

PAX DOOR HINGE (FUSELAGE SIDE) LANDINGS/BORES WORN BEYOND LIMITS, ROLL PIN DAMAGE ON AFT END. REPLACED PAX DOOR HINGE (FUSELAGE SIDE) IAW CRJ 700 SRM 53-21-23-201-007-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 27 SEAT TRACK IS CORRODED BETWEEN F.S. 909 TO F.S. 985. REMOVED CORRODED SEAT TRACK AT LBL 27. INSTALLED A SERVICEABLE SEAT TRACK AT LBL 27 BETWEEN F.S. 909 TO F.S. 985 IAW CRJ 700 A.M.M. 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS 708 TO FS 785. REMOVED & REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-000/400-801-A03.

Part: WEB — CRACKED · airframe 40,907 hrs · 30,382 cycles

FWD EQUIPMENT COMPARTMENT FLOOR IS CRACKED ON LH SIDE AT FS 193.00 REPAIRED IAW CRJ 700 SRM 53-11-43-201-001-A01.

Part: FITTING — CORRODED · airframe 40,907 hrs · 30,382 cycles

MACHINED FITTING AT FS 581.00 BETWEEN STRINGER 22L AND 23L IS CORRODED. REMOVED AND REPLACED FITTING IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 4 BETWEEN FS 338.00 AND 347.00 REMOVED AND REPLACED INTERCOSTAL DD4 PN# 601R31902-317 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: DOUBLER — CORRODED · airframe 40,907 hrs · 30,382 cycles

DOUBLER CORRODED AT STGR 27 BETWEEN FS 581.00 AND FS 597.00. REMOVED, FABRICATED AND REPLACED DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-24-16-001-001-A01 REFERENCING DRAWING SH670-33272 FOR FABRICATION.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 4 BETWEEN FS 323 AND FS 335 REMOVED, LCOCATED AND DRILLED NEW INTERCOSTAL DD4 BETWEEN FS 323-335 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED ON DOOR DATUM 2 BETWEEN FS 320 AND FS 338 REMOVED AND REPLACED DD2 WITH NEW AND SERVICEABLE PART BETWEEN FS 320-338 IAW CRJ 700 SRM 51-42-06/21-001-001-A01. REMOVED AND REINSTALLED SAME SERVICEABLE FORMER DD2 AT FS 329 IAW CRJ 700 SRM 51-42-06/21-001-001-A01

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

BELOW THE FLOOR, STGR 19R IS CORRODED BETWEEN FS 295- 310 STGR FOUND OUT OF LIMITS IAW CRJ 700 SRM 53-21-03-101-002-A01, REMOVED LOCATED, DRILLED AND INSTALLED NEW STGR 19R IAW 51-42-06-001-001-A01,51-42-21-001-001-A01 AND 51-40-11-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED DOOR DATUM 6 BETWEEN FS 338 AND FS 347.25 REMOVED AND REPLACED INTERCOSTAL PN# 601R31902-317 DOOR AT DATUM 6 BETWEEN FS 338 AND FS 347.25 IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED · airframe 40,907 hrs · 30,382 cycles

STRINGER 27 CORRODED BETWEEN F.S. 250.00 AND 265.00. REMOVED & REPLACED STRINGER IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 7A BETWEEN FS 320 AND FS 338 REMOVED AND REPLACED DD7A INTERCOSTAL AND DISPLACED AND INSTALLED FORMER AT FS 329 BETWEEN DD4 AND DD5 IAW CRJ 700 SRM 51-42-06/21-001-001A

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

FLOOR SEAT TRACK AT RBL9 BETWEEN FS 485.00 AND FS 581.00 IS CORRODED. REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-0049-000/400-801-A03

Part: CLEAT — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CLIP (CLEAT) IS CORRODED AT FS 323.00 AND DOOR DATUM 3. REMOVED AND REPLACED CLEAT PN# 600-31902-269 AT FS 323 DATUM 3 IAW CRJ 700 SRM 21-42-06-001-001-A01

Part: FORMER — CORRODED · airframe 40,907 hrs · 30,382 cycles

CORROSION ON DOOR FORMER CORRODED AT FS 329 BETWEEN DOOR DATUM 4 AND 5. REMOVED, LOCATED AND DRILLED NEW DOOR FRAME AT FS 329 BETWEEN DD4 AND DD5 IAW CRJ 700 SRM 51-42-06/21-001-001-A01 AND 40-11-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 2 BETWEEN FS 338 AND FS 347.25 REMOVED AND REPLACED INTERCOSTAL PN# 601R318052-1 AT DOOR DATUM 2 BETWEEN FS 338 AND FS 347.25 IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 7A BETWEEN FS 320 AND FS 327 REMOVED AND REPLACED DD7A INTERCOSTAL AT FS 350-327 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

INTERCOSTAL CORRODED AT DOOR DATUM 3 BETWEEN FS 329 AND FS 338 REMOVED, LCOCATED AND DRILLED NEW INTERCOSTAL DD3 BETWEEN FS 329-338 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 40,907 hrs · 30,382 cycles

IN AVIONICS BAY DOOR STRUCTURE MACHINE FITTING IS CORRODED AT FS 364 ON STGR 26R INTERCOSTAL. FOUND CORROSION AT INTERCOSTAL ON FS 364 STGR 26R TO BE OUT OF LIMITS, REPLACED INTERCOSTAL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 53-21-23-101-03-A01

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

FLOOR SEAT TRACK AT LBL9 BETWEEN FS 485.00 AND FS 581.00 IS CORRODED. REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-0049-000/400-801-A03

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RH SIDE SEAT TRACK BETWEEN FS 863 TO FS 985 IS CORRODED

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

FOUND REINFORCING ANGLE AT FS 265 BETWEEN STGR 26L AND 26R TO BE CORRODED LOCATED, DRILLED AND REPLACED REINFORCING ANGLE AT FS 265 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 565 TO F.S. 677. REMOVED, FBRACATED AND INSTALLED L/H SIDE SEAT TRACK BETWEEN F.S. 565 TO F.S. 677 IAW CRJ 700 SRM 53-00-49-201-002-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 9 SEAT TRACK IS CORRODED BETWEEN FS1000 -FS1047. FABRICATED SEAT TRACK SEGMENT AND REPLACED IAW CRJ 700 SRM 51-42-02-001-001-A01, 51-40-11-001-001-A01 AND AMM 53-00-49-400-801.

Part: CHANNEL — WORN · airframe 40,907 hrs · 30,382 cycles

LH DIAPHRAM CHANNEL ASSY IN WHEEL WELL HAS ELONGATED HOLE. REMOVED & REPLACED CHANNEL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN FS 485 TO FS 565. REMOVED & REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-000/400-801-A03.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

F.S. 319.70 FRAME ATTACHMENT CLIP IS CORRODED. REMOVED CORRODED F.S. 319.70 ATTACHMENT CLIP. INSTALLED A SERVICEABLE F.S. 319 ATTACHMENT CLIP IAW CRJ 700 SRM 51-42-21-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS 379 TO FS 485. REMOVED & REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-000/400-801-A03.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

FLOOR SEAT TRACK AT LBL9 BETWEEN FS 773.00 AND FS 830.00 IS CORRODED. REMOVED, FABRICATED & REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-000/400-801-A03 & SRM 53-00-49-201-002-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S. 985 - F. S.1000. FABRICATED SEAT TRACK SEGMENT AND REPLACED BETWEEN F.S. 985 - F.S. 1000 IAW CRJ 700 SRM 53-00-49-201-002-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS 485 TO FS 565. LOCATED AND DRILLED NEW SERVICEABLE SIDE SEAT TRACK FROM EXTRUSION P/N: 20276-280-0-0A IAW CRJ SRM 51-40-11-001-001-A01 AND SRM 53-00-48-201-002-A01

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 9 SEAT TRACK IS CORRODED BETWEEN FS985 -FS1000. REMOVED RBL 9 SEAT TRACK. FABRIACTED SEAT TRACK AND INSTALLED A SERVICEABLE SEAT TRACK AT RBL 9 BETWEEN F.S. 985 TO F.S. 1000 IAW CRJ 700 SRM 53-00-49-201-002-A01.

Part: ANGLE — CORRODED · airframe 40,907 hrs · 30,382 cycles

FS280 CROSSBEAM J ANGLE IS CORRODED. REMOVED & REPLACED ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: ANGLE — CRACKED · airframe 40,907 hrs · 30,382 cycles

FS 280.00 CROSSBEAM ANGLE AT RBL 12 IS CRACKED. REMOVED & REPLACED ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01.

Part: PANEL — CHAFED · airframe 40,907 hrs · 30,382 cycles

PANEL 684EB CHAFED NEAR VANE ACTUATOR. REMOVED CHAFED PANEL AND LOCATED AND DRILLED A SERVICEABLE PANEL 684EB IAW CRJ 700 SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 27 SEAT TRACK IS CORRODED BETWEEN FS985 -FS1000. REMOVED RBL 27 SEAT TRACK BETWEEN F.S. 985 TO F.S. 1000. INSTALLED A SERVICEABLE RBL 27 SEAT TRACK BETWEEN F.S. 985 TO F.S. 1000 IAW CRJ 700 53-00-49-000-802, AND 53-00-49-400-802.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS847 -FS969. REMOVED RBL 9 FLOOR SEAT TRACK BETWEEN F.S. 847 TO F.S. 969. INSTALLED A SERVICEABLE RBL 9 SEAT TRACK BETWEEN F.S. 847 TO F.S. 969 IAW CRJ 700 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS409 -FS421. REMOVED AND REPLACED CORRODED R/H SIDE SEAT TRACK BETWEEN FS409-FS421 IAW CRJ700 SRM 53-00-49-201-002-A01, AND CRJ700 AMM 53-00-49-400-801-A017 .

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS349 -FS477. REPLACED IAW CRJ 700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

LBL 27 SEAT TRACK IS CORRODED BETWEEN FS985 -FS1000. FABRICATED SEAT TRACK SEGMENT AND REPLACED IAW CRJ 700 SRM 53-00-49-201-002-A01 AN DAMM 53-00-49-400-802-A06.

Part: SEAT TRACK — CORRODED · airframe 40,907 hrs · 30,382 cycles

RBL 27 SEAT TRACK IS CORRODED BETWEEN F.S. 909 TO F.S. 985. REMOVED CORRODED SEAT TRACK AT RBL 27. INSTALLED A SERVICEABLE SEAT TRACK AT RBL 27 BETWEEN F.S. 909 TO F.S. 985 IAW CRJ 700 A.M.M. 53-00-49-801A03 AND 53-00-49-400-801A03.

Part: NONE — CORRODED · airframe 40,907 hrs · 30,382 cycles

RH FLOOR SILL IS CORRODED AROUND NUT PLATES AT FS 280. REMOVED AND REPLACED FLOOR SILL IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-15-001-001.

Part: WINDOW — FAILED · airframe 40,571 hrs · 30,056 cycles

WINDOW SHATTERD RAN QRH ALT DID NOT STABILIZE ALTITUDE CAUTION AND WARNING PASS OXY ON CAUTION. F.O FELT BREEZE AIR IN UPPER LEFT QUADRANT OF WINDOW MASK DEPLOYED AUTO - REMOVED & REPLACED RH SIDE WINDOW IAW JC 900-56-900-902 REMOVED & REPLACED 02 GENERATORS & CLEANED 02 MASK LH & RH ROWS 1-18 IAW AMM 35-21-03 ALL CHECKS GOOD

Part: RELAY — INOPERATIVE (CABIN) · airframe 38,277 hrs · 27,861 cycles

"DURING FLIGHT EMER LIGHTS CYCLED ON AND OFF INTERMITTENTLY ""DEFERRED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1A PLACARD INSTALLED ENTERED INTO MM02 PER MOC 96074$$$$R7R RELAY K135 PER CRJ 700 AMM 20-42-00 PERFORMED OPERATIONAL TEST PER CRJ 700 AMM 24-86-11 OPS CHECK GOOD NO OTHER DEFECTS NOTED AT THIS TIME MM02 UPDATED PLACARD REMOVED "

Part: LIGHT — DAMAGED (SEAT 4B) · airframe 36,373 hrs · 26,433 cycles

ANGLED SECTION OF EMERGENCY FLOOR PATH LIGHTING IN FRONT OF SEAT 4B IS BROKEN. REMOVED AND REPLACED 4B EMERGENCY FLOOR PATH IAW TS #006028B AMM 33-51-01. PN ON PL1100LH07 PN OFF PL1100LH07 SN ON N/A SN OFF N/A

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[[OUT OF LIMITS IN REF NRC 00250]] [ IN REFERENCE NRC 135 ] PER MTC REQUEST: CORROSION ON STRINGER 27 IN SECTION [ FS= 280 TO FS= 300 ] AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY: STRINGER WAS REPLACED FOR NEW ONE PER SRM 51-42-06-001-001-A01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON LIGHT CLIP SUPPORT ASSY IN STA. FS= 959 BETWEEN STR 23R TO 24R AT AFT LAVATORY SERVICE PANELS. (FUS) (TCI: 100-19) SUMMARY IN REFERENCE 292; LEVEL CORROSION 2; LIGHT CLIP SUPPORT ASSY IN STA. FS= 959 BETWEEN STR 23R TO 24R WAS REPLACED PER SRM 51-42-02-001-001-A01 PAR. 5.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 25R IN STA. FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY: IN REFERENCE OF NRC 252; LEVEL CORROSION 2; STRINGER SPLICE 25RH IN STA. FS= 327 TO FS= 337 WERE REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[[ OUT OF LIMITS IN REF NRC 00175 ]]: CORROSION ON STRINGER 27 IN STA. FS= 559 AT FWD BAGGAGE BAY. (CCD) (TCI: 100-10) STRINGER 27 IN STA. FS= 559 AT FWD BAGGAGE BAY WAS REPAIRED PER SRM 53-00-03-201-001-A01 PAR.5A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON FLOORBEAM 27LBL IN STA. FS= 1010 TO FS= 1047 AT AFT BAGGAGE BAY. (CCT) TCI 100-32 NEW SECTION BEAM AND SPLICER END FILLERS WERE INSTALLED PER SRM 53-00-41-201-001-A01, REO 670-53-61-1528, EA N° CRJ753-08516 REV. A, SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 923 BETWEEN STR 25L TO 25R AT PAX CABIN AFT WET AREA. (W2) (CPAX) TCI 100-31 FRAME IN STA. FS= 923 BETWEEN STR 25L TO 25R AT PAX CABIN AFT WET AREA WAS REPAIRED PER EA CRJ7530-08518 REV. IR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX LEVEL COROSION 2. SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RB WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SUPPORTS ANGLE IN STA. FS= 329 BETWEEN WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2. SUPPORTS ANGLE IN STA. FS= 329 BETWEEN WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STR 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 FRAME IN STA. FS= 295 BETWEEN STR 26L TO 26R AT MAIN AVIONICS COMPARTMEN WAS REPAIRED PER EA NO:CRJ753-08460, REV. IR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON INTERCOSTALS (2 EA´S) IN STA. FS= 349 TO FS= 364 BETWEEN STR 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 INTERCOSTALS (2 EA´S) IN STA. FS= 349 TO FS= 364 BETWEEN STR 26L TO 26R WERE REPLACED PER SRM 51-42-06-001-001-A01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX SUMMARY: SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL WAS REMOVED PER SRM 51-42-06-001-001-A01 PAR. 6D. AND CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 PAR. 5E. DAMAGE WAS MEASURED AND FOUND WITH THE FOLLOWING DIMENSIONS OT=0.063" DEPHT=0.014" THEREFORE ITS OUTSIDE OF LIMITS PER 53-00-00-101-001-A01 PAR. 4A. DIAL INDICATOR P/N:543-783 DATE. EXP: 16/JUL/19 N/C:2378 RCG. SUPPORT WAS INSTALLED PER SRM 51-42-20-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 565 BETWEEN STR 17L TO 18L AT FWD BAGGAGE BAY. (CCD) (TCI: 100-10) SUMMARY IN REFERENCE OF NRC 173; LEVEL CORROSION 2; FRAME IN STA. FS= 565 BETWEEN STR 17L TO 18L WAS REPAIRED PER EA CRJ753-08482 REV. IR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 549 BETWEEN STR 17L TO 18R AT FWD BAGGAGE BAY. (CCD) (TCI: 100-10) SUMMARY IN REFERENCE OF NRC 172; LEVEL CORROSION 2; FRAME IN STA. FS= 549 BETWEEN STR 17L TO 18L WAS REPAIRED PER EA CRJ753-08481 REV. IR.

Part: BRACKET — CRACKED (RT WING) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION : CRACKED CANISTER WELDED BRACKET ACCESS NR 651AB STA WS153.00 RT WING ( AD ) SUMMARY IN REFERENCE NRC 362; CANISTER WELDED BRACKET ACCESS NR 651AB STA WS153.00 RT WING WAS REPAIRED REO 670-57-42-577,REV. ORIG.

Part: BRACKET — CRACKED (LT WING) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION : CRACKED CANISTER WELDED BRACKET ACCESS NR 551AB STA WS153.00 LT WING ( AI ). SUMMARY IN REFERENCE NRC 363; CANISTER WELDED BRACKET ACCESS NR 551AB STA WS153.00 LT WING WAS REPAIRED PER REO 670-57-42-577,REV. ORIG.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: GOUGE ON SKIN IN STA. FS= 981 NEAR STGR 27 AT FUSELAGE SKIN. (FUS) SUMMARY OF NRC 295; GOUGE ON SKIN IN STA. FS= 981 NEAR STR 27 AT FUSELAGE SKIN WAS REPAIRED PER EA CRJ753-08463 REV. IR

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER 27 IN SECTION [ FS= 280 TO FS= 300 ] [ FS= 305 TO FS= 327] [ FS= 337 TO FS= 354 ] AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY IN REFERENCE OF NRC 250; LEVEL COOROSION 2: STRINGER 27 IN SECTION [ FS= 280 TO FS= 300 ] WAS REPLACED WITH NRC 00268; STRINGER 27 IN SECTION [ FS= 305 TO FS= 327 ] WAS REPLACED PER SRM 51-42-06-001-001-A01 AND STRINGER 27 ON SECTION [ FS= 337 TO FS= 354 ] WAS CLEANED PER SRM 51-26-00-001-001-A01. AFTER CLEANLINESS, STRINGER IN SECTION [ FROM STA. FS= 337 TO FS= 354 ] WAS RE-INSPECTED AND NO CORROSION WAS FOUND PER AMM 05-21-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER 26R IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 LEVEL CORROSION 2. STRINGER 26R IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER 27 IN SECTION [ FS= 280 TO FS= 300 ] [ FS= 305 TO FS= 327] [ FS= 337 TO FS= 354 ] AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY IN REFERENCE OF NRC 250; LEVEL CORROSION 2: STRINGER 27 IN SECTION [ FS= 280 TO FS= 300 ] WAS REPLACED WITH NRC 00268; STRINGER 27 IN SECTION [ FS= 305 TO FS= 327 ] WAS REPLACED PER SRM 51-42-06-001-001-A01 AND STRINGER 27 ON SECTION [ FS= 337 TO FS= 354 ] WAS CLEANED PER SRM 51-26-00-001-001-A01. AFTER CLEANLINESS, STRINGER IN SECTION [ FROM STA. FS= 337 TO FS= 354 ] WAS RE-INSPECTED AND NO CORROSION WAS FOUND PER AMM 05-21-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 26,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER 25L IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SUMMARY IN REFERENCE OF NRC 247; LEVEL CORROSION 2; STRINGER 25L IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

[ IN REFERENCE NRC 135 ] INITIAL INSPECTION: CORROSION ON STRINGER 25R IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 LEVEL CORROSION 2. STRINGER 25R IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; HIDDEN CORROSION; DURING REMOTION OF FLOOR PANEL SUPPORT ANGLE TO REMOVE CORROSION, A BEAM WAS FOUND CORRODED [ IN REFERENCE NRC 00136 ]: CORROSION ON FLOORBEAM FWD FACE [ INBD SIDE AND NEAR UPPER/AFT FLANGE ] IN STA. FS= 280, 2RBL AND 3.5RBL AT PAX CABIN FWD WET AREA. (W1)(CPAX) TCI: 53-10-219 SUMMARY OF NRC 226: LEVEL CORROSION 2; FLOORBEAM IN STA. FS= 280, 0.RBL AND 47 RBL AT PAX CABIN FWD WET AREA WAS REPLACED PER PER SRM 51-42-06-001-001-A01. PAR. 6. C. AND SRM 51-42-20-001-001-A01. PAR. 6. C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 581 TO FS= 683, 9LBL/RBL ] [ FS= 683 TO FS= 835, 9LBL/RBL ] [ FS= 835 TO FS= 987, 9LBL][ FS= 835 TO FS= 977, 9RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-245) COMPLETE: SUMMARY: NEW FLOOR SEAT RAILS IN SECTIONS [ FS= 581 TO FS= 683, 9LBL/RBL ] [ FS= 683 TO FS= 835, 9LBL/RBL ] [ FS= 835 TO FS= 987, 9LBL][ FS= 835 TO FS= 977, 9RBL] WERE REPLACED PER AMM 53-00-49-400-801-A17.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; HIDDEN CORROSION; DURING REMOTION OF FLOOR PANEL SUPPORT ANGLE TO REMOVE CORROSION, A BEAM WAS FOUND CORRODED [ IN REFERENCE NRC 00136 ]: CORROSION ON FLOORBEAM FWD FACE [ INBD SIDE AND NEAR UPPER/AFT FLANGE ] IN STA. FS= 280 AND 0LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) TCI: 53-10-219 COMPLETE: SUMMARY: CORROSION LEVEL 2 : FLOORBEAM FWD FACE AT PAX CABIN FWD WET AREA WAS ATTENDED PER EA CRJ753-08378 REV. IR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY IN REFERENCE OF NRC 209; LEVEL CORROSION 2; NEW SUPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL WAS REPLACED PER SRM 51-42-02-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,074 hrs · 26,236 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 675 TO FS= 713, STGR 15LH/RH ] [ FS= 785 TO FS= 853, STR 15L/R ] AT PAX CABIN. (CPAX) (TCI: 53-20-290) COMPLETE: NEW SECTIONS SEAT RAILS IN SECTIONS [ FS= 675 TO FS= 713, STR 15L/R ] [ FS= 785 TO FS= 853, STR 15L/R ] WERE REPLACED PER AMM 53-00-49-400-801 A17.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 35,238 hrs · 25,639 cycles

OXY MASK DEPLOYED IN THE LAV. RESTOWED LAV O2 MASKS PER AMM 35-21-17.

Part: RELAY — FAULTY (EMERGENCY LIGHT) · airframe 35,189 hrs · 25,607 cycles

EMERGENCY LIGHTS ARE INTERMITTENTLY ON AND OFF IN ARMED MODE. R&R K135 RELAY IAW AMM 24-06-11& ESPM 20-39-00. EMERGENCY LIGHTS OPS CHECKS GOOD IAW AMM 33-51-00-710-802 REF MM 409 604571 FOR DETAILS.

Part: STRAP — BROKEN (AFT FLASHLIGHT) · airframe 34,612 hrs · 25,178 cycles

REAR FA FLASHLIGHT STRAP WAS BROKEN. REMOVED AND REPLACED THE AFT FA FLASHLIGHT STRAP IAW CMM 25-60-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,406 hrs · 25,024 cycles

CENTER CEILING EMERGENCY LIGHT AT CONNECTOR PLUG P358 DOES NOT WORK. FOUND A BROKEN WIRE. REPAIRED THE BROKEN WIRE IAW ESPM 20-33-00, AND THE EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,390 hrs · 25,009 cycles

OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE AT THE ENTRANCE WAY. REMOVED AND REPLACED EPSU BATTERY PS35 IAW AMM 33-51-04.

Part: ESCAPE HATCH — LEAKING (COCKPIT) · airframe 34,269 hrs · 24,900 cycles

OVER HEAD ESCAPE HACH LEAKS WATER ON GROUND AND WHISTLES IN FLIGHT. CLEANED ACCESS WATER AND INSPECTED CREW ESCAPE HATCH SEAL IAW AMM 52-22-00. NO DAMAGE FOUND. OK FOR SVC AT THIS TIME.

Part: LAMP — INOPERATIVE (EXIT SIGN) · airframe 34,265 hrs · 24,896 cycles

CABIN OVERHEAD EXIT SIGN INOPERATIVE. REPLACED THE LAMPS.

Part: STRINGER — CRACKED (ZONE 100) · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK, WHILE PERFORMING SB670BA-53-040, FOUND STRINGER 3 TO BE CRACKED. REPAIRED THE STRINGER IAW REO 670-53-21-493, REV D. ACFT RETURNED TO SERVICE

Part: FRAME — GOUGED (BS 797) · airframe 33,517 hrs · 24,306 cycles

DURING A C CHECK, NUMBEROUS GOUGES ON AFT SIDE OF REAR FRAME AT BS 797. REPAIRED IAW REO 670-53-41-338, 670-53-41-339, AND 670-53-41-340. ACFT RETURNED TO SERVICE.

Part: FITTING — DAMAGED (POST) · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK, ON REMOVAL OF AFT POST FITTING AT BL 0 FOUND ONE OVERSIZED HOLE IN CENTER POST RT LOWER MEASURING APPROX .215. REPAIRED THE HOLE IAW REO 670-53-11-1329. THE ACFT RETURNED TO SERVICE.

Part: WEB — DAMAGED (BS 741) · airframe 33,517 hrs · 24,306 cycles

WHILE PERFORMING SB 670SH-53-042 ONE HOLE WAS ELONGATED AT BS 741, LBL 36, THRU DIAPHAM AND PRESSURE FLOOR. REPAIRED IAW REO 670-53-41-337. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — DAMAGED (BS 847) · airframe 33,517 hrs · 24,306 cycles

DURING A C CHECK, TWO OVERSIZED AND ELONGATED HOLES IN THE FLOOR SUPPORT AT BS 847, LBL 36. REPAIRED IAW REO 670-53-41-336. ACFT RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK , ON REMOVAL OF AT NLG FLOOR SPLICE ANGLE FOUND OVERSIZED HOLE AT LBL 7.5 OUTBOARD MEASURING .225. REPAIRED IAW REO 670-53-11-1328.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK, WHILE PERFORMING SB670BA-53-045 WE FOUND RIGHT FRAME SECTOR FS220 TO BE CRACKED. REMOVED AND REPLACED RIGHT SIDE FRAME SECTOR FS220 IAW SRM 51-42-06-001-001.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK, FS202.75 POST AT LBL 30 STIFFENER HAS AN INDICATION .1 LONG IN THE UPPER EDGE OF THE FLANGE FAILED NDT. REPAIRED POST AT FS 202.75 LBL 30 IAW SRM 53-11-10-201-005-A01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,517 hrs · 24,306 cycles

DURING C CHECK, FS202.75 POST AT RBL 30 STIFFENER HAS AN INDICATION .1 LONG IN THE UPPER EDGE OF THE FLANGE FAILED NDT. REPAIRED POST AT FS 202.75 RBL 30 IAW SRM 53-11-10-201-005-A01.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,145 hrs · 22,551 cycles

EXIT SIGN ON FORWARD BULKHEAD IS MISSING THE COVER. INSTALLED A NEW COVER. OPS CHECKED GOOD IAW AMM 33-51-05.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 29,450 hrs · 21,189 cycles

INTERIOR EMERGENCHY LIGHT FWD EXIT LOCATOR LT AND RT, EXTERNAL LIGHT FWD PASSENGER DOOR AND FWD SERVICE DOOR INOPERATIVE. R & R 31 EPSUU BATTERY CHARGER IAW AMM 33-51-17. IPC REF 33-51-177, FIG 1, ITEM 8. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,159 hrs · 20,966 cycles

12 AB LOWER EXIT SIGN HAS ONE BULB BURNED OUT. R & R THE BULB. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,159 hrs · 20,966 cycles

GALLEY AFT LOWER EXIT SIGN HAS ONE BULB BURNED OUT. R & R THE BULB. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,939 hrs · 20,777 cycles

SEVERAL EMERGENCY LIGHTS NOT WORKING AFT SECTION OF ACFT INSIDE AND OUTSIDE. TAIL STROBE AND NAVIGATION LIGHTS INOPERATIVE. REMOVED EPSU BATTERY PACK NR 4, AMM TASK 33-51-17-000-801, A01. INSTALLED SERVICEABLE EPSU BATTERY PACK NR 4 IAW AMM 33-51-17-400-801 A01. OP'S CHECK GOOD IAW AMM 33-51-17-710-801, A01.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,914 hrs · 20,758 cycles

WHITE LENS CAP IS MISSING FROM CEILING PANEL 263ELC'S EMERGENCY EXIT SIGN CALL LIGHTS. REMOVED AND INSTALLED NEW EMERGENCY EXIT SIGN CALL LIGHTS LENS ON CEILING PANEL 263ELC IAW AMM 33-51-01-000-400-801-A01.

Part: ANGLE — CRACKED (BS 280) · airframe 28,914 hrs · 20,758 cycles

BS 280 LT SIDE LOWER WEB ANGLE CRACKED. R & R THE ANGLE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 28,914 hrs · 20,758 cycles

BS 280 RT LOWER BULKHEAD WEB ANGLE WAS FOUND CRACKED. R & R THE ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (PAX DOOR) · airframe 28,914 hrs · 20,758 cycles

SKIN ON PAX DOOR UNDER PANEL 832AL CORRODED AND CRACKED. REMOVED CORROSION ON THE PAX DOOR INNER SKIN UNDER PANEL 332AL IN REF TO SRM 51-21-06-001-001-A01. BLENDED AREA IS OUT OF LIMITS IAW SRM 52-11-01-101-001-A01. PERFORMED EDDY CURRENT INSPECTION OF INNER SKIN IAW NDTM PT 1 51-20-006-250-A01. CRACK INDICATION EXTENDS TO NUTPLATE UPPER RIVET HOLE NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH EA-32-2015-266 P2 SECTION 1. RECEIVED AND COMPLIED WITH ECTC EA 32-2015-266.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,914 hrs · 20,758 cycles

LT SIDE LOWER FS 280.00 BULKHEAD WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11-594, REV A DATED 4-27-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 28,914 hrs · 20,758 cycles

RT FLOOR SUPPORT JUST AFT OF SERVICE DOOR CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. APPLIED CHEMICAL CONVERSION COATING TO BLENDED AREA IAW SRM 51-21-11-001-001-A01. COMPLIED WITH ECTC REO 670-53-00-390 AND REO 670-53-00-390, REV.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,914 hrs · 20,758 cycles

RT SIDE LOWER BS 280 BULKHEAD WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11-594, REV A.

Part: ANGLE — CORRODED · airframe 28,914 hrs · 20,758 cycles

SERVICE DOOR FLOOR TOP ANGLE OTBD SIDE HAS CORROSION. BLENDED CORROSION TO THE SERVICE DOOR TOP ANGLE IN REF TO SRM 51-21-06-001-001-A01. FOUND TO BE 100 PERCENT MATERIAL LOSS IN REF TO SRM 51-21-23-11-002-A01. R & R DOOR TOP ANGLE IN REF TO SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED FWD AND AFT LOWER SERVICE DOOR LATCH ASSY REF TO AMM 20-21-00-8910-801-A01, 53-21-27-000-802-A01.

Part: ANGLE — CORRODED · airframe 28,914 hrs · 20,758 cycles

SERVICE DOOR FLOOR TOP ANGLE HAS CORROSION ON TOP SIDE. R & R SERVICE DOOR TOP ANGLE IN REF TO SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-576) · airframe 28,914 hrs · 20,758 cycles

RT SIDE SEAT TRACK CORRODED FROM BS 485 - 576. REMOVED THE TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-576) · airframe 28,914 hrs · 20,758 cycles

LT SIDE SEAT TRACK CORRODED BS 485 - 576. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 437) · airframe 28,914 hrs · 20,758 cycles

RT SIDE SEAT TRACK CORRODED AT APPROXIMATELY BS 437. THE SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01 AND 51-21-06-001-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, ECTC REO 670-53-00-343, REV J, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-703) · airframe 28,914 hrs · 20,758 cycles

LT SIDE SEAT TRACK CORRODED BS 677 - 703. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 576-705) · airframe 28,914 hrs · 20,758 cycles

RT SIDE SEAT TRACK CORRODED FROM BS 576 - 705. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM SUP 53-31-49. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,914 hrs · 20,758 cycles

FWD CENTER FLOORBEAM CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R THE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01, AND 51-21-11-001-001-A01 AND DWG CC670-34010, REV J.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,604 hrs · 20,505 cycles

12AB LOWER SIDEWALL EXIT SIGN HAD ONE BULB BURNED. R & R THE BULB AT 12AB SIDEWALL EXIT LIGHT IAW AMM 33-51-05.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,603 hrs · 20,504 cycles

GALLEY AFT LOWER EXIT SIGN HAD ONE BULB OUT. R & R THE BULB AT GALLEY AFT EXIT SIGN IAW AMM 33-51-05.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 26,430 hrs · 18,808 cycles

RIGHT SIDE EXTERNAL FUSELAGE EMERGENCY LIGHT LENS ASSY BROKEN. R & R RT SIDE SERVICE DOOR EMERGENCY LIGHT COVER IAW AMM 33-51-15.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 25,152 hrs · 17,904 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF. RESET EMERGENCY LIGHT SWITCH. CHECKED GOOD IAW AMM 33-50-00.

Part: SKIN — CORRODED (BS 506-524) · airframe 24,873 hrs · 17,712 cycles

SKIN CORRODED UNDERNEATH ADF ANTENNA AT S27, FS 506 - 524. REPAIRED IAW SRM 57-42-06-001-001 & SRM 51-21-06-001-001 AND REO 670-53-31-297.

Part: SKIN — CORRODED (BS 302) · airframe 24,873 hrs · 17,712 cycles

FOUND EXTERNAL SKIN CORRODED AROUND TCAS ANTENNA CUTOUT S27, FS 302. REPAIRED IAW SRM 51-42-06-001-001 & SRM 51-21-06-001-001 AND REO 670-53-21-1001.

Part: FRAME — CORRODED (BS 333) · airframe 24,873 hrs · 17,712 cycles

FRAME BS 333 CORRODED FWD SIDE AT S37. REPAIRED IAW SRM 52-21-06-001-001-A01 AND RECEIVED REO 670-53-21-990.

Part: FRAME — CORRODED (BS 333) · airframe 24,873 hrs · 17,712 cycles

FRAME BS 333 CORRODED AFT SIDE AT S26-27R. BLENDED FRAME IAW SRM 51-21-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT BRACKET — CORRODED (SERVICE DOOR) · airframe 24,873 hrs · 17,712 cycles

SERVICE DOOR THRESHOLD SUPPORT BRACKET CORRODED. REMOVED SUPPORT BRACKET IAW SRM 51-42-06-001-001-A01. DRILLED AND INSTALLED SERVICEABLE SUPPORT BRACKET IAW SRM 51-43-11-001-001-A01, 51-42-06-001-001-A01, 51-25-16-001-001-A01.

Part: SKIN — DENTED (BS 297) · airframe 24,873 hrs · 17,712 cycles

EXTERNAL SKIN DENTED AT BS 297, S26L. REPAIRED IAW REO 670-53-21-987. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 295) · airframe 24,873 hrs · 17,712 cycles

FWD & AFT SIDE OF FRAME BS 295 CORRODED AT S27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 24,873 hrs · 17,712 cycles

SERVICE DOOR SILL INBD MOUNTING ANGLE IS CORRODED. REMOVED MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE MOUNTING ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01. COMPLIED WITH RIGGING AND OP CHECKED IAW AMM 52-41-00-220-801 AND 52-41-00-710-801. RIG AND OPS CHECKED GOOD. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (BS 342) · airframe 24,867 hrs · 17,706 cycles

STRINGER 26R CORRODED AT BS 342. R & R STRINGER AND STRINGER SPLICE FROM BS 333-364 IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,872 hrs · 17,711 cycles

INTERCOSTAL CORRODED AT BS 364 S27R. REMOVED INTERCOSTAL IAW SRM 53-21-33-101-003-A01 & 51-42-21-001-A01 & 51-42-06-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-40-11-001-001-A01 & DWG SH670-32075. INSTALLED INTERCOSTAL IAW DWG SH670-32075 & SRM 51-42-21-001-001.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 24,873 hrs · 17,712 cycles

SERVICE DOOR SILL PLATE ANGLE IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. REPLACED SILL ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

CRAWLWAY FLOOR PANEL 141ALF FWD FLOOR SUPPORT ANGLE CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. LOCATED, DRILLED & DEBURRED HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (BS 333) · airframe 24,867 hrs · 17,706 cycles

CIRCUMFERENTIAL JOINT AT FRAME BS 333, INTERNAL SKIN CORRODED AT S27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: LONGERON SPLICE — CORRODED (BS 333) · airframe 24,873 hrs · 17,712 cycles

LONGERON SPLICE 25R FS 333. REMOVED LONGERON SPLICE IAW SRM 51-42-06-001-001-A01. INSTALLED LONGERON SPLICE IAW SRM 51-42-06-001-001-A01, DWG SH670-32420. REPAIR CLASSIFIED AS MAJOR.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 24,867 hrs · 17,706 cycles

TCAS DOUBLER CORRODED AT STRINGER 27 BETWEEN BS 295 & 310. REPAIRED IAW SRM 51-42-06-001-001-A01 AND 51-23-00-001-001-A01. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,872 hrs · 17,711 cycles

INTERCOSTAL CORRODED AT BS 364 S26L. REPAIRED IAW SRM 53-21-101-003-A01 AND 53-21-03-101-006-A01 AND REO 670-53-21-995.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,872 hrs · 17,711 cycles

INTERCOSTAL CORRODED AT BS 364, S26R. REMOVED INTERCOSTAL IAW SRM 53-21-23-101-003-A01 & 51-42-06-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-40-11-001-001-A01 & DWG SH670-32077.

Part: FRAME — CORRODED (BS 295) · airframe 24,867 hrs · 17,706 cycles

FWD & AFT SIDE OF FRAME BS 295 CORRODED STRINGER 27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: STRINGER — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

STRINGER 26R CORRODED AT BS 280. REPAIRED IAW SRM 51-21-06-001-001-A01, 57-42-06-001-001-A01, 51-42-06-001-001-A01, DWG SH670-31634 AND REO 670-53-21-996.

Part: FRAME — CORRODED (BS 349) · airframe 24,872 hrs · 17,711 cycles

FRAME BS 349 CORRODED AT S27. REPAIRED IAW SRM 53-12-06-101-006-A01.

Part: FRAME — CORRODED (BS 319.7) · airframe 24,867 hrs · 17,706 cycles

FRAME BS 319.7, FWD SECTION CORRODED FROM S26L TO 26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH GREO REO 670-53-21-799. REV, DATED 2012-01-30.

Part: LONGERON — CORRODED (BS 342) · airframe 24,873 hrs · 17,712 cycles

LONGERON 25R CORRODED BS 342. REPAIRED IAW SRM 53-21-23-001-003-A01.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,872 hrs · 17,711 cycles

INTERCOSTAL CORRODED AT BS 364 S27L. REMOVED INTERCOSTAL AT FS 364-351 IAW SRM 53-21-23-101-003-A01 & 51-42-21-001-A01 & 51-42-06-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-40-11-001-001-A01 & DWG SH670-32075. INSTALLED INTERCOSTAL IAW SRM 51-42-21-001-001-A01 & DWG SH670-32075. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051.3) · airframe 24,867 hrs · 17,705 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FS 1051.3 - 1031. REPAIRED IAW SRM 53-61-43-201-001 AND REO 670-53-61-989. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

FLOOR PANEL 221ALF AFT FLOOR SUPPORT ANGLE WHICH ATTACHES TO FS280, FRAME IS CORRODED. LOCATED AND DRILLED THE AFT SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 24,867 hrs · 17,706 cycles

SEAT TRACK CORRODED MULTIPLE SPOTS, BS 677-830.4 RBL 9. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 REV D. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A03). INSTALLED NEW FABRICATED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 24,867 hrs · 17,705 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FS 1015 AND 1031. REPAIRED IAW REO 670-53-61-993, REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

LT WEB AT FS 280 AND LBL 9.0 IS CORRODED. REMOVED DAMAGED WEB IAW DWG 670-53-11-594. FABRICATED A REPLACEMENT WEB IAW DWG 670-53-11-594. INSTALLED WEB IAW DWG 670-53-11-594.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 24,867 hrs · 17,706 cycles

AFT CARGO DOOR SILL CORRODED. REPAIRED IAW OF REO 670-53-61-913.

Part: SEAT TRACK — CORRODED (BS 677-830.4) · airframe 24,867 hrs · 17,706 cycles

SEAT TRACK CORRODED, MULTIPLE SPOTS, BS 677-830.4 LBL 9. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, REV 'D'. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,867 hrs · 17,705 cycles

SEAT TRACK CORRODED MULTIPLE SPOTS FS 485-581 AND RBL 9. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM 53-00-49-400-801-A03.

Part: WEB — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

RT WEB AT FS 280 AND RBL 9 CORRODED. REPLACED WEB IAW SRM 51-1200-001-001: 51-21-02-001-001.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 24,867 hrs · 17,705 cycles

SIDE SEAT TRACK CORRODED MULTIPLE SPOTS AT FS 581 -677. R & R PASSENGERS SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 985-1000) · airframe 24,867 hrs · 17,706 cycles

LEFT FLOOR SUPPORT CORRODED BETWEEN FS 985 AND 1000. REMOVED CORROSION IAW SRM 53-61-58-101-001-A01. REPAIRED IAW REO 670-53-61-990. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 863-976) · airframe 24,867 hrs · 17,705 cycles

SIDEWALL SEAT TRACK CORRODED MULTIPLE SPOTS AT FS 863-976 AND S15L. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 24,867 hrs · 17,705 cycles

SEAT TRACK CORRODED MULTIPLE SPOTS FS 379-485 AND LBL 9. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1015) · airframe 24,867 hrs · 17,705 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FS 1000 AND 1015. REPAIRED IAW REO 670-53-61-993 IAW NDTM PT.1, 51-20-006. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,867 hrs · 17,705 cycles

SIDEWALL SEAT RAIL CORRODED MULTIPLE SPOTS AT FS 708-761.85 AND S15L. REMOVED AND INSTALLED SERVICABLE SIDEWALL SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-47-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,867 hrs · 17,705 cycles

SIDEWALL SEAT TRACK CORRODED MULTIPLE SPOTS AT FS 708-761.85 AND S15L. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 24,867 hrs · 17,706 cycles

SIDEWALL SEAT TRACK CORRODED MULTIPLE SPOTS AT BS 785.15-863 S15L. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,867 hrs · 17,706 cycles

FS 280 FLOORBEAM CORRODED. REMOVED FLOORBEAM IAW SRM 51-42-21-001-001-A01. LOCATED & DRILLED REPLACEMENT FLOORBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1051.3-1070.7) · airframe 24,867 hrs · 17,706 cycles

RT FLOOR SUPPORT CORRODED BETWEEN BS 1051.3 AND 1070.7. REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-61-43-201-001. REPAIRED IAW REO 670-53-61-993.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 24,867 hrs · 17,706 cycles

SIDEWALL SEAT RAIL CORRODED MULTIPLE SPOTS AT BS 677-708 AND S15R. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, REV 'D'. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,867 hrs · 17,705 cycles

SEAT TRACK CORRODED MULTIPLE SPOTS FS 485-581 AND LBL 9. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 24,867 hrs · 17,705 cycles

SIDE WALL, SEAT RAIL, CORRODED MULTIPLE SPOTS AT FS 785.15-863 AND S15R. CORRODED BEYOND LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,867 hrs · 17,706 cycles

RT FS 280 FLOORBEAM CRACKED AND CORRODED. REMOVED FLOORBEAM IAW SRMS 51-42-06-001-001-A01, 51-42-10-001-001-A01, AND 51-42-21-001-001-A01. LOCATED & DRILLED REPLACEMENT FLOORBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE FLOORBEAM IAW SRM 53-11-11-201-003-A01 & DWG PL 670-53-11-594 RH. MAJOR REPAIR.

Part: SKIN — CHAFED (BS 977) · airframe 24,867 hrs · 17,706 cycles

SKIN BS 977.00 UNDER PANEL 195DL HAVE CHAFED, STRINGER 27. REPAIRED IAW REO 670-53-61-994 AND REO 670-53-00-290, REV C.

Part: CHANNEL — CRACKED · airframe 24,867 hrs · 17,705 cycles

C-CHANNEL LOCATED UNDER PANEL 195DL IS CRACKED. REMOVED CHANNEL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW CHANNEL IAW SRM 51-42-13-001-001-A01.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 24,867 hrs · 17,705 cycles

GALLEY SERVICE DOOR SILL IS CORRODED. REMOVED LOWER SILL STRIKER FROM SERVICE DOOR IAW SRM TASK 51-42-06-001-001-A01. REMOVED SERVICE DOOR PROTECTOR PLATE FOR ACCESS TO REMOVE LOWER SEAL STRIKER IAW AMM TASK 53-21-23-000-801. INSTALLED SERVICE DOOR PROTECTOR PLATE IAW AMM 53-21-23-400-801. INSTALLED SERVICEABLE STRIKER SEAL IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01 DWG SH670-31950.

Part: MOUNT — CORRODED (FAIRING) · airframe 24,867 hrs · 17,705 cycles

BELLY FAIRING PANEL 193AB HAS CORROSION DAMAGE ALONG THE FWD MOUNTING FLANGE. R & R LT AND RT FWD FLANGES ON PANEL 193AB IAW SRM 51-42-13-001-001-A01.

Part: STRUCTURE — CRACKED (E/E BAY) · airframe 24,867 hrs · 17,705 cycles

FORWARD EQUIPMENT COMPARTMENT, RT SIDE AFT CORNER, CRACKED, GOING UNDER ADG HYD PUMP. REPAIRED IAW AMM 24-23-19-000-801 AND REO 670-53-11-509.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 24,237 hrs · 17,229 cycles

PLASTIC EXIT LENS COVER ON BULKHEAD IN FRONT OF SEAT 1A WILL NOT STAY SECURED. LENS IS CRACKED IN SEVERAL PLACES. RESECURED PLASTIC EXIT COVER IAW AMM 33-51-05. NO FURTHER ISSUES AT THIS TIME.

Part: RESERVOIR — FAILED (HYDRAULIC SYS) · airframe 22,269 hrs · 15,856 cycles

ON APPROACH INTO BOS HYDRAULIC SYSTEM NR 3 QTY 10 PERCENT AND BOTH 3A AND 3B PUMPS INOP. EMERGENCY DECLARED, A/C LANDED SAFELY AT BOS. REMOVED AND REPLACED NR 3 HYDRAULIC RESERVOIR. OPS CHECK GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

SERVICE DOOR SILL ANGLE CORRODED. REMOVED CORRODED SILL ANGLE AND INSTALLED REPLACEMENT ANGLE PER SRM 51-42-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

FLOOR SILL FWD OF SERVICE DOOR HAS CORROSION. REPAIRED FLOOR SILL P/N SH670-32172 FWD OF SERVICE DOOR BY CUTTING AWAY DAMAGE AND INSTALLING DOUBLER IAW REO 670-53-21-713.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

PAX DOOR THRESHOLD "L" ANGLE UNDER CAP ANGLE IS CORRODED. REMOVED AND REPLACED "L" ANGLE P/N SH670-31875-7 UNDER CAP ANGLE AT PAX DOOR THRESHOLD AREA IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

FWD MOST SEAT TRACK JUST TO THE RIGHT OF THE AISLE IS CORRODED. REPLACED SEAT TRACK IAW CRJ AMM 53-00-49.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

PAX DOOR SILL ANGLE HAS CORROSION. INSTALLED SERVICEABLE PAX DOOR SILL ANGLE IAW CRJ-SRM 51-42-06.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

RIGHT CROSSBEAM AT FS 280 CORRODED. REMOVED AND REPLACED CROSSBEAM IAW CRJ REO 670-53-11-265 AND REO 670-53-11-047.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

PAX DOOR FWD HANDRAIL CUP FITTING IS CORRODED. INSTALLED SERVICABLE FWD CUP FITTING IAW CRJ-SRM 51-42-20.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,885 hrs · 14,149 cycles

LEFT CROSSBEAM AT FS 280 CORRODED. REMOVED AND REPLACED CROSSBEAM IAW CRJ REO 670-53-11-265 AND REO 670-53-11-047.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 17,411 hrs · 12,455 cycles

ON DESCENT INTO DCA RECEIVED O/B SPOILERONS AND O/B SPOILERS CAUTION MSG'S. EMERGENCY DECLARED, A/C DIVERTED TO IAD AND LANDED SAFELY. PERFORMED RESET OF SSCU'S AND SELF TEST. MSG'S CLEARED, NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 17,406 hrs · 12,452 cycles

ON DESCENT INTO DHN RECEIVED I/B SPOILERS AND I/B SPOILERONS CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED RESET OF SSCU'S, MSG CLEARED. NO FURTHER DEFECTS NOTED.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 15,092 hrs · 10,809 cycles

FS 280 CRACKED AT RBL 9.00 FLOOR SUPPORT CROSSBEAM. REPAIRED CRACK AT FS 280 RBL 9.00 FLOOR SUPPORT CROSSBEAM IAW REO 670-53-11-045.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 15,092 hrs · 10,809 cycles

FS 280 CRACKED AT LBL 9.00 FLOOR SUPPORT CROSSBEAM. REPAIRED CRACK AT FS 280 LBL 9.00 FLOOR SUPPORT CROSSBEAM IAW REO 670-53-11-045.

Part: TRANSDUCER — FAILED (LT MLG) · airframe 14,705 hrs · 10,525 cycles

RECEIVED ANTI SKID CAUTION MSG ON TAKEOFF FROM PHL, AND REMAINED ON THROUGHOUT FLT. EMERGENCY DECLARED, A/C LANDED SAFELY IN CVG. REMOVED AND REPLACED LEFT I/B WHEEL SPEED TRANSDUCER.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,531 hrs · 10,402 cycles

EN ROUTE FROM CVG TO EWR LEFT WINDSHIELD CRACKED. EMERGENCY DECLARED, A/C LANDED SAFELY IN EWR. REMOVED AND REPLACED LEFT WINDSHIELD.

Part: ELEMENT — FAULTY (ANTI ICE SYS) · airframe 12,445 hrs · 8,975 cycles

FLIGHT 5100 - EN ROUTE PIT-CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, CREW DECLARED EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING INBOARD LEADING EDGE WING SENSING ELEMENT.

Part: ELEMENT — FAULTY (LT WING) · airframe 12,445 hrs · 8,975 cycles

FLIGHT 5100 - EN ROUTE PIT-CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, CREW DECLARED EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING CENTER LEADING EDGE WING SENSING ELEMENT.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 11,660 hrs · 8,481 cycles

FLIGHT 5420 - DURING TAXI OUT IN DFW PASSENGERS WERE EVACUATED DUE TO SMOKE IN CABIN ROWS 8.9 AND 10. FOUND RIGHT PACK TO BE THE CAUSE OF THE SMOKE. DEFERRED TIGHT PACK PER MEL 21-51-04-2.

Part: STRUCTURE — DENTED (TE FLAPS) · airframe 11,332 hrs · 8,260 cycles

RIGHT I/B FLAP HAS A 1 INCH DENT. REPAIRED FLAP IAW SRM 57-52-01.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 11,332 hrs · 8,260 cycles

FUSELAGE SKIN GOUGED BELOW SERVICE DOOR. REPAIRED DAMAGED AREA IAW REO 670-53-21-312.

Part: SKIN — DAMAGED (WING) · airframe 11,332 hrs · 8,260 cycles

WORKING RIVETS AND DAMAGED TOP WING SKIN O/B OF LEFT MULTI-FUNCTION SPOILERS. REPAIRED DAMAGED AREA IAW REO 670-51-73-002 AND EA 70-5557-01885.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,332 hrs · 8,260 cycles

PAX DOOR SURROUND MID CAP FLOOR EXTRUSION CORRODED. REPLACED FLOOR SUPPORT MID CAP EXTRUSION IAW SRM 51-21-33.

Part: MOUNT — CORRODED (GALLEY) · airframe 11,332 hrs · 8,260 cycles

AFT INBOARD MOUNT FOR GALLEY NR 1 IS CORRODED. REPLACED MOUNT IAW SRM 51-42-21.

Part: BULKHEAD — CORRODED (BS 280) · airframe 11,332 hrs · 8,260 cycles

FS 280 BULKHEAD AND CROSSBEAM CORRODED. BLENDED OUT CORROSION IAW SRM 53-21-43, 51-21-11, 51-25-06, 51-42-13 AND 53-11-10.

Part: NONE — NONE (WARNING MESSAGE) · airframe 11,390 hrs · 8,301 cycles

FLIGHT 5506 - RECEIVED ANTI-ICE DUCT WARNING AND RIGHT FUSELAGE DUCT RED ON SYNOPTIC PAGE. DECLARED EMERGENCY, PERFORMED QRH AND LANDED WITHOUT INCIDENT. RAN BOTH ENGINES AND PERFORMED OPS CHECK OF ANTI-ICE SYSTEM. NO FURTHER DEFECTS.

Part: ALTIMETER — ERRATIC (COCKPIT) · airframe 10,928 hrs · 7,975 cycles

FLIGHT 5257 - AFTER TAKEOFF RADAR ALTIMETER BECAME ERRATIC, FLUCTUATING FROM 300 TO 3000 FT. A TERRAIN ALERT WAS ALSO RECEIVED AT ABOUT 2000 FT. AIRCRAFT LANDED SAFELY BACK AT CVG. COULD NOT DUPLICATE ON GROUND. OHMED AND MEGGED CABLES, NO DEFECTS NOTED.

Part: FAN BLADE — VIBRATES (LT ENGINE) · airframe 8,432 hrs · 6,278 cycles

FLIGHT 5617 - EN ROUTE JAN-BOS DURING CLIMB ENCOUNTERED VIBRATION FROM THE LEFT ENGINE, FLIGHT DIVERTED TO CVG. REPLACED THE LEFT ENGINE FAN BLADES.

Part: CONTROL UNIT — FAULTY (AVIONICS BAY) · airframe 7,939 hrs · 5,991 cycles

FLIGHT 5212 - DURING CLIMBOUT OF SAT RECEIVED A RUDDER LIMITER FAULT MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED SSCU NR 2.

Part: WARNING MESSAGE — ILLUMINATED (RUDDER LIMITER) · airframe 7,880 hrs · 5,958 cycles

FLIGHT 5867 - AFTER TAKEOFF RUDDER LIMITER CAUTION MESSAGE AND RUDDER FAULT MESSAGE APPEARED, STAYED ON. RETURNED FOR LANDING PER QRH. PERFORMED SPOT 2 TEST, MESSAGE CLEARED, OPS NORMAL.

Part: CYLINDER — CORRODED (NLG STRUT) · airframe 7,685 hrs · 5,822 cycles

NLG OUTER CYLINDER HAS MINOR CORROSION. REPAIRED NLG OUTER CYLINDER CORROSION IAW BOMBARDIER REO 670-32-21-094 AND GOODRICH SCR 0008-07 REV C.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,685 hrs · 5,822 cycles

FS 280 TRANSVERSE BEAM CORRODED BEYOND REPAIRABLE LIMITS. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV D.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,685 hrs · 5,822 cycles

FS 280 RT BULKHEADS CORRODED BEYOND REPAIRABLE LIMITS. REPLACED THE RT BULKHEAD AT FS 280 IAW BOMBARDIER REO 670-53-11-052 REV A.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,685 hrs · 5,822 cycles

FS 280 LT BULKHEADS CORRODED BEYOND REPAIRABLE LIMITS. REPLACED THE LT BULKHEAD IAW BOMBARDIER REO 670-53-11-052 REV A.

Part: BLEED AIR SYS — CONTAMINATED · airframe 7,409 hrs · 5,660 cycles

FLIGHT 4985 - SMOKE FORWARD LAV WARNING MESSAGE CAME ON DURING TAXI THEN WENT OUT. INSPECTED FORWARD LAV NO EVIDENCE OF SMOKE OR FIRE. SUSPECT GLYCOL INGESTION IN BLEED SYSTEM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 7,102 hrs · 5,452 cycles

FLIGHT 5689 - EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY BATTERY PACK.

Part: CONTROL HANDLE — STUCK (TE FLAPS) · airframe 4,283 hrs · 3,316 cycles

FLIGHT 5670 FLAPS/SLATS CONTROL HANDLE IS STUCK. REPLACED FLAPS/SLATS SELECTOR LEVER.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 3,141 hrs · 2,400 cycles

FLIGHT 5451 FLIGHT SPOILERS AND SPOILERON CAUTION MESSAGE. COULD NOT DUPLICATE SYSTEM, TEST NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 2,777 hrs · 2,115 cycles

FLIGHT 5832 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 2,622 hrs · 1,995 cycles

FLIGHT 5048 RECEIVED A RIGHT THRUST REVERSER UNSAFE CAUTION DURING TAKEOFF ROLL, ABORTED AND RETURNED TO THE GATE. DEFERRED THE RIGHT THRUST REVERSER SYSTEM PER MEL 78-30-01.

Part: FLOW VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 2,242 hrs · 1,687 cycles

FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3B FLOW LIMITING VALVE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 1,266 hrs · 947 cycles

FLIGHT 5520 NR 3 HYDRAULIC SYSTEM LOW PRESSURE AND GEAR DISAGREE WARNING. REPLACED THE L/G SELECTOR VALVE.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 1,222 hrs · 913 cycles

FLIGHT 5299 GEAR DISAGREE WARNING DURING CRUISE. REPLACED THE PSEU.

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE SYSTEM) · airframe 1,162 hrs · 860 cycles

FLT 5213 LT WING ANTI ICE MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY.

Part: SEALANT — MISSING (DOOR AREA) · airframe 336 hrs · 264 cycles

FLIGHT 5717 CABIN DOOR MAKING LOUD NOISE, FA AND PASSENGER SAID THEY SMELLED SOMETHING BURNING. COULD NOT DUPLICATE - FOUND VERY SMALL AREA OF DOOR FRAME THAT WAS MISSING SEALANT. FILLED HOLE WITH SEALANT.