N197PQ

Part: LUG — CHIPPED (ZONE 500 AILERON) · airframe 35,293 hrs · 25,880 cycles

LEFT AILERON SIDE LUG LABELED D HAD A CHIP IN THE INSIDE OF THE BORE . COMPLIED WITH REO 690-57-61-476 REV-.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR MID INTERCOSTAL DD2 FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED PAX DOOR FORMER FS 329.50 FOR ACCESS IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REINSTALLED PAX DOOR FORMER FS 329.50 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED PAX DOOR MID INTERCOSTAL DD2 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED/DRILLED FASTENER HOLES IN NEW PAX DOOR MID INTERCOSTAL DD2 IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD2 IAW SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR AFT INTERCOSTAL DD2 FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED UNSERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 IAW SRM TASK 51-41-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 IAW SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 IAW SRM 51-42-06-001-001-A01

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR, BS 327.763 FRAME SEGMENT CORRODED BETWEEN DD6 AND DD7. PAX DOOR, FRAME SEGMENT CORRODED BETWEEN DD6 AND DD7. REMOVED UNSERVICEABLE PAX DOOR, FRAME SEGMENT BETWEEN DD6 & DD7 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FOUND PAX DOOR, FRAME SEGMENT BETWEEN DD6 AND DD7 TO HAVE 100% MATERIAL LOSS ON MULTIPLE SIDES AND REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR FRAME IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 LOCATED & DRILLED NEW SERVICEABLE PAX DOOR FRAME IAW SRM TASK 51-40-11-001-001-A01

Part: FORMER — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR AFT FORMER FS347.27 FOUND TO BE CORRODED REQUIRE REPLACEMENT. .REMOVED & REINSTALLED MID FITTING ASSY, AFT UPPER FITTING ASSY, AFT TOP CORNER SEAL RETAINER, AFT SIDE SEAL RETAINER, AFT UPPER CENTERING PLATE, AFT LOWER CENTERING PLATE, AFT PULL IN LEVER, PAX DOOR AFT SUPPORT ANGLE IAW SRM 51-42-06/21-001-001-A01/ AMM 52-11-02-000/400-806-A01. REMOVED & REPLACED PAX DOOR AFT FORMER FS347.27 IAW SRM 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT FORMER FS347.27 IAW SRM TASK 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR MID INTERCOSTAL DD4 FOUND TO BE CORRODED. REMOVED FASTENERS FROM MID INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED & DRILLED FASTENER LOCATIONS IN NEW PAX DOOR MID INTERCOSTAL DD4 IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD4 IAW SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: FORMER — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR AFT FORMER FS320.163 FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED & REINSTALLED PAX DOOR INTERCOSTAL DD6/ DD7 FWD IAW SRM TASK 52-42-06-001-001-A01. REMOVED AND REPLACED PAX DOOR FWD FORMER FS320.163 IAW SRM TASK 51-42-06-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR FWD FORMER FS320.163 IAW SRM TASK 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR AFT INTERCOSTAL DD1 FOUND TO BE CRACK REQUIRE REPLACEMENT REMOVED UNSERVICEABLE PAX DOOR AFT INTERCOSTAL DD1 IAW SRM 51-41-06-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD1 IAW SRM 51-42-06-001-001-A01 LOCATED & DRILLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD1 IAW SRM 51-40-11-001-001-A01

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,293 hrs · 25,880 cycles

LBL 12.00 COCKPIT FLOORBEAM PREVIOUS REPAIR IS CRACKED AT FS280.00. .REPAIRED LBL 12.00 COCKPIT FLOOR BEAM AT FS280.00 IAW CRJ900 SRM 53-11-43-201-003-A01.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR DD 6 INTERCOSTAL CORRODED BETWEEN BS 327.763 & 331. PAX DOOR INTERCOSTAL CORRODED BETWEEN BS 327.763 & 331.00 UPON FURTHER INVESTIGATION FOUND PAX DOOR DD 6 INTERCOSTAL BETWEEN TO BE 100% MATERIAL LOSS DUE TO EXCESSIVE CORROSION IN MORE THAN 2 SPOTS OF FLANGE & WEB. REMOVED UNSERVICEABLE PAX DOOR DD 6 INTERCOSTAL BETWEEN IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. REINSTALLED SERVICEABLE PAX DOOR FORMER AT BS 329.41 IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR DD 6 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-40-11-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR FWD INTERCOSTAL DD2 FOUND TO BE CORRODED REQUIRE REPLACEMENT REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD2 IAW SRM 51-42-06-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD2 IAW SRM 51-40-11-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,293 hrs · 25,880 cycles

PAX DOOR MID INTERCOSTAL DD7A FOUND TO BE CORRODED. REQUIRES REPLACEMENT PAX DOOR MID INTERCOSTAL DD7A FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED UNSERVICEABLE PAX DOOR MID INTERCOSTAL DD7A IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FOUND PAX DOOR MID INTERCOSTAL DD7A TO HAVE 100% MATERIAL LOSS ON MULTIPLE PLANES AND REQUIRES REPLACEMENT INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD7A IAW SRM TASK 51-42-06-001-001-A01. LOCATED AND DRILLED PAX DOOR MID INTERCOSTAL DD7A IAW SRM TASK 51-40-11-001-001-A01

Part: WEB — DAMAGED (ZONE 200) · airframe 33,710 hrs · 24,553 cycles

SPLICE WEB @FS 847 LBL9 I/B SIDE HAS PRE-EXISTING FASTENER HOLES THAT WILL NOT ALIGN WITH FACTORY PILOT HOLES. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: LUG — CRACKED (ZONE 800) · airframe 33,710 hrs · 24,553 cycles

L/H FWD EMERGENCY EXIT HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED LEFT FWD EMERGENCY DOOR IAW MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06.

Part: LUG — CRACKED (ZONE 800) · airframe 33,710 hrs · 24,553 cycles

L/H AFT EMERGENCY EXIT HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED LEFT AFT EMERGENCY DOOR IAW MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 33,710 hrs · 24,553 cycles

WHILE PERFORMING SB 670BA-53-036 REV F DATED FEB 07/2024 FOUND EXISTING PILOT HOLE MISSALIGNED IN RH FLOOR AT RBL36 FS 820. REPAIR BY REMOVING DAMAGE AND INSTALLING FREEZE PLUG IAW MHIRJ REO 690-53-41-527 REV -- DATED 2025-04-03.

Part: CHARGER — INOPERATIVE · airframe 28,128 hrs · 19,935 cycles

EMERGENCY LIGHTS ON FWD CABIN CEILING AND SERVICE DOOR EXTERIOR ARE VERY DIM. FOUND ESPU BATTERY PACK PS36 DISCHARGED TO 0.95 VOLTS. REMOVED AND REPLACED BATTERY CHARGER ASSY IAW CRJ 900 AMM 33-51-17. OPS TEST GOOD. REPLACED BATTERY PACK PS36 IAW CRJ 900 AMM 33-51-17. OPS TEST GOOD. BATTERY P/N OFF/ON 2013-1ASMI S/N OFF 13570 S/N ON 14727 CHARGER P/N OFF/ON 11-0049 S/N OFF 23220 S/N ON 15844

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

CORROSION FOUND ON STRINGER 20RH IN BETWEEN FS295.00 AND 310.00 BELOW FLOOR J/C:900-53-140-500 - COMPLIED WITH EA#CRJ-953-12968 REVIR DATED 2/24/2022 - REPLACED STRINGER PER EA CRJ953-12968.

Part: DOUBLER — CORRODED · airframe 27,743 hrs · 19,629 cycles

CORROSION FOUND ON STRINGER 17RH IN BETWEEN FS280 AND FS295.00 WL72.50 NEAR CONDITIONED AIR DUCT BELOW FLOOR J/C:900-53-140-500 - REMOVED AND REPLACED NEW DOUBLER PART#SH670-32183-1 NEAR AIR DUCT BELOW FLOOR ON STRINGER 17 R/H BETWEEN FS280-FS295 WL 77.50 IAW CRJ900 SRM 51-42-13

Part: SKIN — GOUGED · airframe 27,743 hrs · 19,629 cycles

THERE IS A DEEP GOUGE ON LHS OF TAIL CONE SKIN B/T STR 5L & 7L - REMOVED DAMAGE ON LHS OF TAILCONE SKIN B/T STR 5L AND 7L IAW CRJ900 AMM 70-42-01-350-801 AND FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-71-01-991-814 AND RESTORED FINISH IAW CRJ900 SRM'S 51-21-11, 51-25-06 AND 51-25-16

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

THERE ARE MULTIPLE AREAS OF CORROSION AT F.S349 STR 24R - REMOVED AND REPLACED NEW STRINGER 24R BETWEEN FS333.00-379.00 IAW CRJ 900 SRM 51-42-06

Part: SEAT TRACK — CORRODED · airframe 27,743 hrs · 19,629 cycles

SEAT TRACK CORRODED AT F.S 911.0 TO 977.0 LBL9.0 J/C#:900-53-900-126 - SEAT TRACK CORROSION MAX DEPTH OF .041" FOUND TO BE OUT OF LIMITS PER CRJ900 SRM. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS853.00-987.00 IAW CRJ900 AMM 53-00-49

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

THERE ARE MULTIPLE AREAS OF CORROSION AT F.S 333-319 ST R24R - REMOVED AND REPLACED CORRODED STRINGER 24R AND SPLICE FROM 280.00-333.00, REPAIR COMPLIED WITH EA#CRJ953-12863 REV IR DATED 2/24/22

Part: SEAT TRACK — CORRODED · airframe 27,743 hrs · 19,629 cycles

SEAT TRACK CORRODED AT F.S 911.0 TO 977.0 RBL 9.0 J/C:900-53-900-126 - SEAT TRACK CORROSION MAX DEPTH OF .039 FOUND TO BE OUT OF LIMITS PER CRJ 900 SRM. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 853.00-853.00 IAW CRJ900 AMM 53-00-49

Part: SEAT TRACK — CORRODED · airframe 27,743 hrs · 19,629 cycles

SEAT TRACK CORRODED AT F.S 817 TO F.S. 911.00 LBL 9.0 J/C:900-53-900-126 - SEAT TRACK CORROSION MAX DEPTH OF .043" FOUND TO BE OUT OF LIMITS PER CRJ900 SRM. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 833.00 853.00 IAW CRJ900 AMM 53-00-49

Part: SEAT TRACK — CORRODED · airframe 27,743 hrs · 19,629 cycles

SEAT TRACK CORRODED AT F.S 817 TO F.S. 911.00 RBL 9.0 J/C:900-53-900-126 - SEAT TRACK CORROSION MAX DEPTH OF .035" FOUND TO BE OUT OF LIMITS PER CRJ900 SRM. REMOVED AND REPLACED SEAT TRACK CHANNEL FROM FS833-853 IAW CRJ900 AMM 53-00-49

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

UNDER THE FORWARD SIDE OF THE ACCESS PANEL 192BB AT FS 661+62 STR 27-20R THERE IS AN AREA OF CORROSION J/C:91162 - REMOVED DAMAGED STRAP UNDER THE FORWARD SIDE OF THE ACCESS PANEL 192BB @F.S.661+62 STR 27-20R AND FABRICATED NEW STRAP OUT OF 2024 T3.032 THICK I.A.W. CRJ900 SRM 53-82-55 AND INSTALLED NEW PART I.A.W. CRJ900 SRM 51-42-06

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

MULTIPLE CORROSION SPOTS FOUND BETWEEN FS 364 AND FS379@ RH STGR 21R J/C:900-53-900-517 - REMOVED AND REPLACED NEW STRINGER 21R BETWEEN FS333.00-379.00 IAW CRJ 900 SRM 51-42-06

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

STGR 21R, BETWEEN FS333 AND FS319 HAS MULTIPLE AREAS OF CORROSION - REMOVED AND REPLACED CORRODED STRINGER AND SPLICE 21R FROM FS280.00-333.00 REPAIR COMPLIED WITH EA#CRJ953-12967 REV IR DATED 2/24/22

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

STGR 23R BETWEEN FS333 AND FS319 HAS MULTIPLE AREAS OF CORROSION - REMOVED AND REPLACED STRINGER 23R FROM F.S.280 TO F.S. 333 IAW CRJ900 SRM 51-42-06

Part: STRINGER — CORRODED · airframe 27,743 hrs · 19,629 cycles

STGR 22R, BETWEEN FS333 AND FS319 HAS MULTIPLE AREAS OF CORROSION - REMOVED AND REPLACED 22R CORRODED STRINGERS AND SPLICE BETWEEN FS 280.00-349.00 IAW CRJ900 SRM 51-42-06 REPAIR ALSO COMPLIED WITH EA#CRJ953-12966 REV IR DATED 2/24/22

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

CORROSION FOUND ON INBOARD CLOSING RIB FROM RT HAND WING FLAP J/C:900-57-690-506 - REMOVED AND REPLACED I/B CLOSING RIB ON O/B FLAP IAW CRJ AMM 57-53-32-400-801

Part: FLOORBEAM — CORRODED · airframe 27,743 hrs · 19,629 cycles

FUSELAGE FLOOR STRUCTURE LBL9 HAS CORROSION IN SEVERAL AREAS FROM FS 847.00 TO FS849.00 029 JC:900-53-180-503 - COMPLIED WITH EA NO. CRJ953-13011 DATED 2/25/2022 REV IR.

Part: FLOORBEAM — CORRODED · airframe 27,743 hrs · 19,629 cycles

FUSELAGE FLOOR STRUCTURE LBL9 HAS CORROSION IN SEVERAL AREAS FROM FS849.00 TO 977.00 028 JC:900-53-180-503 - COMPLIED WITH EA. CRJ953-12922 REV IR.

Part: FLOORBEAM — CORRODED · airframe 27,743 hrs · 19,629 cycles

FUSELAGE FLOOR STRUCTURE RBL9 CORROSION IN SEVERAL AREAS FROM FS847.00 TO FS 849.00 027 JC:900-53-180-503 - COMPLIED WITH EA NO:CRJ953-12975 DATED 2/25/2022 REV IR. - REMOVED CORROSION AND RESTORED FINISH TO REWORKED AREA PER EA CRJ953-12975.

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

FWD AND AFT JOINT PLATES IN FWD BAGGAGE BAY HAS CORROSION - REMOVED, FABRICATED AND REPLACED 2 EA CORRODED JOINT PLATES (FWD & AFT AT FWD LWR BAGGAGE BAY DOOR FRAME. IAW CRJ900 SRM 51-42-22

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

PAX DOOR HAS CORROSION UNDER PANEL 832FL ON FWD SIDE MARKED WITH RED DOT LM#018 J/C:91726 - REMOVED AND REPLACED PAX DOOR FWD FORMER FRAME IAW CRJ900 SRM 51-40-11 51-42-13, 51-42-21 AND EA#CRJ952-12969 ISSUE DATE 2/25/2022 REV IR

Part: DOOR SILL — CORRODED · airframe 27,743 hrs · 19,629 cycles

AFT CARGO DOOR CUTOUT SILL HAS CORROSION IN VARIOUS LOCATION JC:900-53-280-506 - REMOVED AND REPLACED AFT CARGO DOOR SILL IAW CRJ900 SRM 51-42-13

Part: SEAT TRACK — CORRODED · airframe 27,743 hrs · 19,629 cycles

SIDE SEAT RAIL-L/H SIDE FROM FS 669-40 TO FS 847 THERE ARE MULTIPLE SPOTS OF CORROSION AROUND SCREW HOLES AND OTHER LOCATIONS JC:900-53-900-120 - REMOVED AND REPLACED A 20" SECTION OF SIDE SEAT TRACK L/H FROM FS669+ 40 TO 709+40, FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 53-11-49. INSTALLED IAW CRJ900 SRM 51-40-00 AND 51-22-00

Part: HOUSING — CRACKED · airframe 27,743 hrs · 19,629 cycles

GALLEY SERVICE DOOR HAS CHAFING ON HANDLE RECESS NEAR SWIVEL POINT JC: 900-52-840 500 - REMOVED AND REPLACED OUTER HANGE HOUSING P/N 133107-3 IAW CRJ900 AMM 52-41-03 AND SRM 51-42-06

Part: ANGLE — CORRODED · airframe 27,743 hrs · 19,629 cycles

PAX DOOR FLOOR SILL HAS CORROSION IN A COUPLE OF SPOTS J/C:900-53-230-503 - AFTER FURTHER EVAL THE ANGLE KICK PLATE AND THE MID-CAP ANGLE HAVE BEEN FOUND OUT OF LIMITS. IAW CRJ900 SRM 53-21-23. REPLACED BOTH PARTS WITH NEW IAW CRJ900 SRM 51-42-06 AND 51-45-00

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

STRAP JOINT ON AFT BELLY FAIRING PANEL 196DR IS CORRODED IN SEVERAL PLACES - REMOVED AND REPLACED STRAP JOINT ON AFT BELLY FAIRING PANEL 196DR IAW CRJ900 SRM 51-24-36, 51-40-11, 51-42-06, AND 51-42-13

Part: SLAT — GOUGED · airframe 27,743 hrs · 19,629 cycles

R/H WING SLAT #3 ON INBOARD MOUNTING RIB OF #3 TRACK HAS MULTIPLE GOUGES REQUIRES EVAL. J/C:900-27-670-903 - REPAIRED R/H WING SLAT #3 ON I/B MOUNTING RIB OF #3 TRACK IAW MHI REO# 690-57-41-339 REV--DATED 2/2/2022.

Part: NONE — CRACKED · airframe 27,743 hrs · 19,629 cycles

R/H FLOOR SILL @ FS350 HAS AREA OF CORROSION - REPAIRED RH FLOOR SILL @ FS350 IAW EA# CRJ953-12760

Part: NONE — CORRODED · airframe 27,743 hrs · 19,629 cycles

280 FLOOR BEAM IS CORRODED BETWEEN RBL 9 AND BL 0 - REMOVED AND REPLACED 280 FLOOR BEAM R/H SIDE IAW CRJ900 SRM 51-42-06, 51-42-13, 51-42-21, 51-42-22

Part: SUPPORT ANGLE — CORRODED · airframe 27,743 hrs · 19,629 cycles

FWD FLOOR SUPPORT @ FS280 IS CORRODED BETWEEN RBL9 AND LBL9 JC:900-53-140-509 - REMOVED AND REPLACED FWD FLOOR SUPPORT @F.S.280 BETWEEN RBL9 AND LBL9 IAW CRJ900 SRM 51-42-06

Part: CHANNEL — CORRODED · airframe 27,743 hrs · 19,629 cycles

R/H SIDE SEAT RAIL MOUNTING CHANNEL @FS780 TO FS820 HAS AREAS OF CORROSION J/C:900-53-900-514 - COMPLIED WITH EA# CRJ953-12557, REV IR DATED 1/18/2022 - REPAIRED CHANNEL PER EA CRJ953-12557.

Part: FAIRING — DAMAGED · airframe 27,743 hrs · 19,629 cycles

UPER L/H TRANSCOWL HINGE FAIRING ASSY. IS DAMAGED AT THE AFT HINGE POINT J/C:900-54-430-300 - REMOVED UPPER TRANS COWL REPLACED WITH NEW IAW CRJ900 AMM 54-12-07

Part: SUPPORT BRACKET — CRACKED · airframe 27,743 hrs · 19,629 cycles

LT MLG. W/W BIN SUPPORT BRACKET ON FWD SIDE OF W/W CRACKED J/C:900-27-900-100 - REMOVED AND REPLACED NEW BRACKET IAW CRJ900 SRM 51-45-00,51-41-02

Part: NONE — CRACKED · airframe 27,743 hrs · 19,629 cycles

CHANNEL FAIRING, AFT CC690-39251-1 ON PANEL 196 DR IS CRACKED - REMOVED AND REPLACED AFT CHANNEL FAIRING ON PANEL 196DR IAW CRJ900 SRM 51-42-13

Part: SUPPORT BRACKET — CRACKED · airframe 27,743 hrs · 19,629 cycles

RT MLG, W/W BIN SUPPORT BRACKET ON FWD SIDE OF W/W CRACKED J/C:900-27-900-100 EMP#:394 DEA - REMOVE AND REPLACE MLG. W/W BIN SUPPORT BRACKET IAW CRJ900 SRM 51-41-02

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 22,920 hrs · 15,965 cycles

FIRST OFFICER`S OXYGEN MASK LEAKING, NOT SEALING. REPLACED THE OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.

Part: SIGN — DAMAGED (MAIN CABIN) · airframe 22,892 hrs · 15,948 cycles

EXIT SIGN ABOVE RT SERVICE DOOR DAMAGED, REPLACED THE SIGN IAW AMM 33-51-05-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 1031) · airframe 20,410 hrs · 14,072 cycles

FLOOR SUPPORT LBL 9, BS 1031 HAS CORROSION. REMOVED THE DAMAGED FLOOR SUPPORT BS 1031-1051.30, SPLICED IN NEW FLOOR SUPPORT IAW EC/TC EO 700-53-00005 AND EC/TC REO 690-53-61-659 REV A.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

FLOOR CROSSBEAM HAS CORROSION AT FS 333.00 RBL 9. COMPLIED WITH EC/TC REO 690-53-21-881 AND REO 690-53-21-881.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND AT FS 280.00 BUTT STRAP 26L-26R. COMPLIED WITH EC/TC REO 690-53-21-879 AND REO 690-53-21-879.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND ON FLOORBEAM AT FS 1031 RBL 9. CUT OUT DAMAGED FLOORBEAM AND SPLICED IN NEW SECTION IAW REO 670-53-00-029, EC/TC EO 900-53-10-00004, REO 690-53-61-660 AND EC/TC REO 690-53-61-660.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

FLOOR CROSSBEAM FROM RBL 27 TO RT FLOOR SILL FS 1051.30 HAS CORROSION. COMPLIED WITH EC/TC EA 30-2016-385 AND EA 30-2016-385 FOR REPAIR TO FLOOR BEAM RBL 27 TO RT FLOOR SILL AT FS 1051.30.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND AT FS 295.00 BETWEEN STR 26L-24R ON FRONT & BACK SIDE. REPAIRED FRAME AT FS 395.00 ON 26L-24R PER EC/TC REO 670-53-21-799 AND REO 670-53-21-799, EC/TC EO 900-53-0003 AND EO 900-53-10-00003, EC/TC REO 690-53-21-880 AND REO 690-53-21-880.

Part: FRAME — CORRODED (BS 364) · airframe 20,410 hrs · 14,072 cycles

CORROSION ON FRAME AT BS 364 BETWEEN STRINGERS 25 - 26R. REPAIRED THE FRAME IAW EC/TC REO 670-53-21-687 01 AND GREO 670-53-21-687.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,410 hrs · 14,072 cycles

INTERCOSTAL AT STRINGER 27L IS CORRODED BS 349 - 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-24-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND ON LBL 46 FS 987. COMPLIED WITH EC/TC REO 690-53-61-663. REO 690-53-61-663 HAS BEEN ACCOMPLISHED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STRINGER 25R CORRODED AT FS 280.00-333.00. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-31630.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STRINGER 26R CORRODED AT FS 295.00-333.00. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-31630.

Part: FLOOR SUPPORT — CORRODED (BS 732-773) · airframe 20,410 hrs · 14,072 cycles

FLOOR SUPPORT RBL 46 & BS 732.50 & 773.50 HAS 3 SPOTS OF CORROSION. REMOVED THE CORROSION IAW SRM 51-21-06-001-001-A01 AND PERFORMED UT THICKNESS AND EDDY CURRENT INSPECTION PROCEDURE 4.3 AND NDTM PT 1 51-20-006-250-A01. BLENDED AREAS ARE WITH IN ALLOWABLE LIMITS AND CRACK FREE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STRINGER 26R CORRODED AT FS 333.00-364.00. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-32050.

Part: FRAME — CORRODED (BS 349) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND ON FRAME AT BS 349 BETWEEN STRINGERS 26L-26R. REMOVED THE FRAME IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED A NEW FRAME IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

SHORT SEAT TRACK IN AFT CARGO BAY CORRODED AT FS 1000 LBL9. REMOVED THEN INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

TCAS ANTENNA DOUBLER CORRODED, LOWER. REMOVED AND REPLACED DOUBLER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND AT FS 280.00 FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT ON FS 280.00 IAW SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND AT FS 310.00 BETWEEN STRINGER 25L-26R FRONT & BACK SIDE. REPAIRED FRAME AT FS 310.00 ON STRINGER 25L-26R PER EC/TC REO 670-53-21-799 01 AND REO 670-53-21-799 01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

CORROSION FOUND AT FS 319.00 BETWEEN STRINGER 25L-25R FRONT & BACK SIDE. REPAIRED FRAME AT FS 319.00 ON STRINGER 25L-25R PER EC/TC REO 670-53-21-799 AND REO 670-53-21-799.

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

FS 319.00 CORRODED BETWEEN STR 25L-25R FRONT & BACKSIDE. REPAIRED FRAME AT FS 319.00 ON STRINGER 25L-25R PER EC/TC REO 670-53-21-799 AND REO 670-53-21-799.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STR 26R SPLICE CORRODED AT FS 333.00. REMOVED AND REPLACED SPLICE AT STR 26R AND FS 333.00 IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STRINGER 27 CORRODED AT FS 333.00-354.00 BTW STRINGER WED & FRAME TO STRINGER ATTACH ANGLE. REMOVED AND REPLACED STRINGER SECTION 27 FORWARD AT FS 354.00 AND 349.00 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH690-31350 REV G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

AFT COCKPIT FLOOR SUPPORT AT FS 280.00 LBL11-RBL11 CORRODED. REMOVED AND REPLACED AFT FLOOR SUPPORT ON FS 280.00 RBL11-LBL11 IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

STR 25R SPLICE CORRODED AT FS 333.00. REMOVED AND REPLACED SPLICE AT STR 25R AND FS 333.00 IAW SRM 51-42-06-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

LT FLOOR SILL CORRODED AT FS 1051.30-1069.75. REPAIRED FLOOR SILL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

LBL 46 SILL BETWEEN FS 927-942 IS CORRODED ON PLATE & SILL. REPAIRED FLOORBEAM BY COMPLYING WITH EC/TC EO 900-53-00-390 AND REO 670-53-00-390.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

FLOORSILL AT LBL 46 FS 732.50 &773.50 HAS 3 SPOTS OF CORROSION. COMPLIED WITH EC/TC EA 40-2016-391. DISCREPANT AREAS WERE BLENDED, PERFORMED NDT TO ENSURE NO PRESENCE OF CRACKS AND RESTORED FINISH.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND THE RT FLOOR SUPPORT HAS CORROSION BS 1015 - 1031. COMPLIED WITH EC/TC REO670-53-00-390 & REO670-53-00-390

Part: SHIM — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND AFT ALTIMETER ANTENNA MOUNT POINT HAS CORROSION BS 1069.75 - 1088.20. REMOVED AND REPLACED THE SHIMS IAW SRM 51-42-06-001-001-A01 AND DRAWING MM690-35007.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,410 hrs · 14,072 cycles

FWD WING TO FUSELAGE FAIRING SUPPORT HAS CORROSION ON MATING SURFACE. REMOVED AND REPLACED FUSELAGE FAIRING SUPPORT ANGLE IAW SRM 51-12-00-001-001-A01, 53-82-55-101-001-A01, 51-42-06-001-001-A01 AND NDTM 51-20-006 AND DRAWING SH69039650.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 20,410 hrs · 14,072 cycles

STRINGER 26L SPLICE CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER SLPICE IAW SRM 51-42-06-001-001-A01 AND DRAWING SH 670-32420.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 20,410 hrs · 14,072 cycles

AFT CARGO DOOR SEAL IS CORRODED AT BS 1000-1047. COMPLIED WITH REPAIR II IAW SRM 53-61-23-201-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 20,410 hrs · 14,072 cycles

STRINGER 26L IS CORRODED BS 319-333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-31630.

Part: SEAT TRACK — CORRODED (BS 830-847) · airframe 20,410 hrs · 14,072 cycles

DURING A C CHECK, FOUND RBL 9 SEAT TRACK SEGMENT FROM BS 830.40 TO 847.62 CORRODED IN FOUR AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-A07, AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND RBL 9 SEAT TRACK SEGMENT FROM BS 847.62 TO 977 CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-A07, AND AMM 53-00-49-400-801-A07.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,377 hrs · 13,360 cycles

FWD F/A EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHTS IAW AMM 33-23-21.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 18,221 hrs · 12,496 cycles

FWD CARGO BAY DOOR SEAL RETAINER BENT AT FWD LOWER CORNER. COMPLIED WITH EC/TC REO 690-52-35-013, PERMANENT REPAIR, THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: MEGAPHONE — DAMAGED (NOT REPORTED) · airframe 17,632 hrs · 12,104 cycles

MEGAPHONE DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 280) · airframe 17,255 hrs · 11,832 cycles

ONE BURN FOUND ON SKIN AT BS 280, STRINGER 26L. BLENDED OUT DAMAGE IAW SRM 51-12-00 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00, REV 53-0050, REPAIR TYPE 2. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 250-265) · airframe 17,255 hrs · 11,832 cycles

TWO BURNS ON SKIN BETWEEN BS 250 - 265, STRINGER 26L. BLENDED DAMAGE AND FOUND TO BE WITHIN LIMITS IAW TR 53-0050, 53-00-00. CLASSIFED AS MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 250-265) · airframe 17,255 hrs · 11,832 cycles

ONE BURN ON SKIN BETWEEN BS 250 - 265, STRINGER 26L. DRILLED OUT DAMAGE IAW TR 53-0050, 53-00-00. WET INSTALLED A FASTENER IAW TR53-0050, AND 53-00-00. CLASSIFED AS MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 280-295) · airframe 17,255 hrs · 11,832 cycles

TWO BURNS FOUND ON SKIN BETWEEN BS 280 - 295, STRINGER 26L. BLENDED OUT THE DAMAGE IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00, REV 53-0050, REPAIR TYPE 2. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 310-319) · airframe 17,255 hrs · 11,832 cycles

ONE BURN FOUND ON SKIN BETWEEN BS 310 - 319, STRINGER 26L. BLENDED OUT THE DAMAGE IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00, REV 53-0050, REPAIR TYPE 2. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 220) · airframe 17,255 hrs · 11,832 cycles

ONE BURN MARK AT BS 220, STRINGER 26L. BLENDED DAMAGE AND FOUND TO BE WITHIN LIMITS IAW TR 53-0050, 53-00-00. CLASSIFED AS MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 250-265) · airframe 17,255 hrs · 11,832 cycles

ONE BURN ON SKIN BETWEEN BS 250 - 265, BETWEEN STRINGERS 25 - 26L. BLENDED THE DAMAGE AND FOUND TO BE WITHIN LIMITS IAW TR53-0050, 53-00-00. CLASSIFED AS MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 235-250) · airframe 17,255 hrs · 11,832 cycles

ONE BURN ON SKIN BETWEEN BS 235 - 250, STRINGER 26L. BLENDED THE DAMAGE AND FOUND TO BE WITHIN LIMITS IAW TR53-0050, 53-00-00. CLASSIFED AS MAJOR REPAIR IAW GMM 5-3.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 17,185 hrs · 11,781 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES, OPS CHECKED GOOD IAW AMM 25-60-00.

Part: LIGHT — MISSING (CABIN) · airframe 16,943 hrs · 11,600 cycles

EMERGENCY LIGHTN MISSING IN FRONT OF FORWARD LAVATORY. REPLACED EMERGENCY LIGHT IAW AMM 33=51=01. ACFT OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 16,740 hrs · 11,451 cycles

EMERGENCY LIGHT MISSING AFT OF SERVICE DOOR. INSTALLED EMERGENCY LIGHT IAW AMM 20-60-04.

Part: LIGHT — MISSING (CABIN) · airframe 16,740 hrs · 11,451 cycles

EMERGENCY LIGHT MISSING BY AFT LAV. REPLACED EMERGENCY LIGHT IAW AMM 31-51-01, ACFT OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 14,618 hrs · 10,025 cycles

SEVERAL EMERGENCY EXIT LIGHTS ARE INOPERATIVE. FOUND CONNECTORS LOOSE IAW ESPM 20-26-00 AND 20-44-00. OPS TESTED THE LIGHTS IAW AMM 33-51-00-710-801, A01.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,618 hrs · 10,025 cycles

EMERGENCY LIGHT AT RT OVERWING HAS BROKEN WIRES. CRIMPED NEW CONTACTS ON EMERGENCY LIGHT WIRES IAW ESPM 20-16-00. OPS TESTED THE LIGHTS IAW 33-51-00-710-801, A01, OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 14,618 hrs · 10,025 cycles

RBL 9, SEAT TRACK SEGMENT CORRODED BS 661+16. REMOVED AND REPLACED THE SEAT TRACK IAW GREO 670-53-00-343.

Part: BEARING — WORN (RUDDER) · airframe 14,615 hrs · 10,024 cycles

BOTH CENTER RUDDER HINGE BEARINGS ARE WORN. REPLACED THE HINGE BEARING IAW RIL 1213, REV NC.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 14,615 hrs · 10,024 cycles

INSPECTION FOUND CORROSION ON BS 333 AND RBL 9 FLOORBEAM. REPAIRED IAW IAW SRM 51-42-06-001-001-A01 AND 51-21-11-001-001-A01 AND DWG PL SH670-32167.

Part: ATTACH ANGLE — CORRODED (BS 752.5) · airframe 14,615 hrs · 10,024 cycles

DADO PANEL ATTACH ANGLE CORRODED AROUND NUTPLATE AT BS 752.5 ON LT SIDE. REMOVED AND REPLACED THE ATTACH ANGLE IAW AMM 53-00-49-000-801 AND AMM 53-00-4-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 913) · airframe 14,615 hrs · 10,024 cycles

LEFT SEAT TRACK SEGMENT FOUND CORRODED AT BS 913. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 14,602 hrs · 10,015 cycles

RIGHT SIDE SEAT TRACK FROM BS 677 - 720.85, CORRODED OUT OF LIMITS. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 14,615 hrs · 10,024 cycles

LEFT SEAT TRACK SEGMENT BS 785.15 - 847+16 FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 14,615 hrs · 10,024 cycles

LEFT SEAT TRACK SEGMENT BS 744.15 - 761.85 FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A07) AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 14,615 hrs · 10,024 cycles

LEFT SEAT TRACK SEGMENT BS 677 - 720.85 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT RAIL SEGMENT IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 14,602 hrs · 10,015 cycles

RIGHT SIDE SEAT TRACK BS 785.15 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 744) · airframe 14,615 hrs · 10,024 cycles

RIGHT SEAT TRACK SEGMENT FOUND CORRODED AT BS 744.15. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801, A01.

Part: SEAT TRACK — CORRODED (BS 453) · airframe 14,615 hrs · 10,024 cycles

RBL 9, SEAT TRACK SEGMENT BS 453 FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 14,615 hrs · 10,024 cycles

RBL 9 SEAT TRACK SEGMENT FOUND CORRODED BS 661+16. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801, CONFIG A07.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 14,608 hrs · 10,020 cycles

COCKPIT FLOOR SUPPORT ANGLE HAS CORROSION.

Part: ANGLE — CORRODED (BS 280 BULKHEAD) · airframe 14,608 hrs · 10,020 cycles

RT BS 280 BULKHEAD LOWER WEB CAP ANGLE HAS CORROSION ON FASTENER HEADS. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED IAW EA 32-2014-078.

Part: SEAT TRACK — CORRODED (BS 349-581) · airframe 14,615 hrs · 10,024 cycles

CORROSION AND SCRATCHES FOUND ON RT SEAT TRACK FROM BS 349 - 581. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: LIGHT — DETERIORATED (CABIN) · airframe 14,608 hrs · 10,020 cycles

EMERGENCY LIGHTING STAINED AND NOT PROPERLY INSTALLED THRU-OUT ACFT. FOUND ON INCOMING CHECK. R & R THE LIGHTS IAW AMM 33-51-01-000/400-801 A27.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 14,608 hrs · 10,020 cycles

RT F/S ELECTRICAL BAY FLOOR IS CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-509.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,073 hrs · 8,370 cycles

LEFT EXTERIOR AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-15 AIPC FIG 1, ITEM 22. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 12,020 hrs · 8,334 cycles

THE FWD OTBD CORNER OF THE FLOOR SILL JUST AFT OF THE SERVICE DOOR IS CORRODED FS 349, RBL 45. REPAIRED IAW REO 690-53-21-537.

Part: STRUCTURE — CORRODED (BS 295-333) · airframe 12,020 hrs · 8,334 cycles

PACKER LOCATED AT LBL9 AND FS 295, 310 AND FS 333 IS CORRODED. REMOVED 3 EA PACKERS FROM LBL9 AT FS STA 295, 310, AND 333 IAW SRM 51-42-06-001-001-A01. INSTALLED 1 PACKER AT LBL9, FS 333 IAW SRM 51-42-06-001-001. RECEIVED AND INSTALLED 2 REMAINING PACKERS AT LBL9, FS 295 AND 310 IAW SRM 51-42-06-001-001.

Part: PACKING — CORRODED (BS 333) · airframe 12,020 hrs · 8,334 cycles

PACKING LOCATED AT RBL 9 AND BS 333 IS CORRODED. REMOVED ONE PACKING IAW SRM 51-42-06-001-001-A01. INSTALLED NEW PACKING IAW SRM 51-42-06-001-001.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 12,020 hrs · 8,334 cycles

RIGHT SIDE BS 280 LOWER BULKHEAD WEB CORRODED. REPAIRED IAW REO 670-53-11-594.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 12,020 hrs · 8,334 cycles

LEFT SIDE BS 280 LOWER BULKHEAD WEB CORRODED. REPAIRED IAW REO 670-53-11-594. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 12,012 hrs · 8,329 cycles

FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT IAW SRM 57-51-06-001-001-A01 AND ATTACH ANGLE. REPAIRED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001 & DWG CC670-33052. LOCATED AND DRILLED THE REPLACEMENT TRACK IAW SRM 51-40-11-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,012 hrs · 8,329 cycles

RT BS 280 FLOORBEAM CORRODED APPROX RBL 11. REMOVED FLOORBEAM IAW SRM 51-42-00-001-001-A01 & SRM 51-42-21-001-001-A01. INSTALLED FLOORBEAM IAW SRM 51-42-06-001-001-A01 & SRM 51-42-11-001-001-A01 AND SRM 51-42-22-001-001-A01 & DWG CC670-34010. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 12,012 hrs · 8,329 cycles

FLOOR SUPPORT CRACKED ON AFT SIDE. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001 & DWG CL670-33052. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CRACKED (BS 274) · airframe 12,012 hrs · 8,329 cycles

FLOOR SUPPORT CRACKED AT APPROX FS 274, LBL 12. REPAIRED IAW REO 690-53-11-562. MAJOR REPAIR.

Part: BUTTSTRAP — CORRODED (BS 280) · airframe 12,020 hrs · 8,334 cycles

FS 280, BUTT STRAP CORRODED BETWEEN S25-26R. REPAIRED IAW AMM 53-00-47-000-A01 & 25-84-00-400-801. AND SRM 51-21-06-001-001-A01 & 51-42-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: BULKHEAD — CORRODED (COCKPIT) · airframe 12,012 hrs · 8,329 cycles

LT FLIGHT DECK BULKHEAD AT APPROX LBL 11 CORRODED. REPAIRED IAW SRM 51-21-06-001-001-A01. REPAIR CLASSIFED AS MAJOR.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 12,020 hrs · 8,334 cycles

LT BS 280 CROSSBEAM CORRODED UPPER T/E PORTION. REMOVED LT 280.00 CROSSBEAM IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. INSTALLED CROSSBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-22-001-001-A01 & 51-42-12-001-001-A01 & DWG CC670-34010.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 12,020 hrs · 8,334 cycles

FLIGHT DECK FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001 & DWG CC670-33052. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,012 hrs · 8,329 cycles

FLOOR SUPPORT AT FS 280 RBL 45 CORRODED. REPAIRED IAW SRM 53-21-43-201-002-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CRACKED (B 274) · airframe 12,012 hrs · 8,329 cycles

FLOOR SUPPORT CRACKED FS 274, RBL 12. REPAIRED IAW REO 690-53-11-562. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 12,020 hrs · 8,334 cycles

DENT RT SIDE OF PAX DOOR TOP STEP AND PAX DOOR SKIN DAMAGE AT UPPER FWD CORNER REPAIRED IAW REO 670-12-11-260 AND REO 670-52-11-260.

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHT) · airframe 12,000 hrs · 8,322 cycles

LEFT FWD WING EMERGENCY LIGHT INOPERATIVE. PROPERLY INSTALLED EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 9,876 hrs · 6,985 cycles

FORWARD FLIGHT ATTENDANT & OBSERVER LIFE VEST BAGS TORN. REMOVED AND REPLACED FLIGHT ATTENDANT & OBSERVER LIFE VESTS IAW AMM 25-61-03.

Part: SEAL — MISSING (MEDICAL KIT) · airframe 9,577 hrs · 6,753 cycles

SEAL ON EMERGENCY MEDICAL KIT IS MISSING. INSTALLED NEW SEAL IAW CRJ900 AMM 25-61-04.

Part: LIFE VEST — MISSING (CABIN) · airframe 9,950 hrs · 6,699 cycles

MISSING LIFE VEST 20B INSTALLED MISSING LIFE VEST 20B IAW CMM 25-21-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 8,803 hrs · 6,142 cycles

EMERGENCY FLOOR LIGHT STRIP DEGRADED 7 INCHES IN FRONT OF LT WARDROBE UNIT. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01. AIRCRAFT OK FOR SERVICE.

Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 8,027 hrs · 5,586 cycles

AIR RETURN L FAN VIB IN YELLOW AT FL 340 L FAN VIB INDICATIONS WERE 2.1-2.3 OIL TEMP/PRESSURE NORMAL ENTIRE FLIGHT INITIAL DESCENT AT FL 340 VIB RANGED FROM 2.3-2.8 AT 16000 N1-67.9 L FAN VIB GREEN AT 1.7 AT 10000 N1 67.3 L FAN VIB-1.5 TURNED ON COWLS-NO ICE. PERFORMED FAN BLADE TANGS LUBE OF LEFT ENGINE IAW CRJ900 AMM 72-21-02, OPS TESTED GOOD, OK FOR SVC.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 7,976 hrs · 5,552 cycles

EXIT TRACK GLOW STRIP FROM FORWARD LAV INTO GALLEY IS PARTIALLY MISSING. REMOVED & REPLACED EMERGENCY AISLE FLOOR PATH STRIP AT GALLEY IAW CRJ900 AMM 33-51-01. OK FOR CONTINUED SERVICE.

Part: O-RING — DEFECTIVE (FUEL SYSTEM) · airframe 7,215 hrs · 5,036 cycles

FUEL LEAK FOUND BY REFUELER. REMOVED AND REPLACED REFUEL/DEFUEL DUCT O-RINGS PER AMM 28-25-11, OPS CHECK GOOD, VERIFIED PARTS EFFECTIVITY. OK FOR SERVICE.

Part: UNKNOWN — FUMES (CABIN) · airframe 3,850 hrs · 2,876 cycles

F/A REPORTED SMOKE FUMES ROWS 9, 10, 11, 12. FUMES WERE EXTRACTED. PERFORMED ENGINE RUNS USING BOTH ENGINE BLEEDS IAW CRJ900 AMM 71-00-00. FOUND NO FUMES. ACFT OK FOR SERVICE.

Part: ACM — SURGES (LEFT) · airframe 3,449 hrs · 2,603 cycles

A/C 197PQ DIVERTED INTO TYS DUE TO SMOKE IN THE COCKPIT. THE SMOKE CLEARED AS ACFT BEGAN DESCENT. LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE LEFT ACM WAS SERGING AND CAUSING THE SMOKE. MAINTENANCE DEFERRED IT WITH THE INTENT TO REPLACE DUE TO NO PARTS AVAILABLE.