N936XJ

Part: BUSHING — DAMAGED (ZONE 500 AILERON) · airframe 35,773 hrs · 25,173 cycles

"FOUND L/H AILERON SIDE BUSHING LUGS LABELED ""C""AND ""F"" TO BE PREVIOUSLY OVERSIZED. FABRICATED BUSHINGS FOR LH AILERON LUGSLABELED ""C"" AND ""F"" IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25."

Part: FORMER — CORRODED (ZONE 800) · airframe 35,773 hrs · 25,173 cycles

FOUND PAX DOOR FWD FORMER TO BE CORRODED. LOCATED AND DRILLED PAX DOOR FORMER IAW CRJ 900 SRM51-40-11-001-001-A01. INSTALLED SERVICEABLE PAX DOOR FORMER (P/N: 601R318031-5) IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. PERFORMED OPERATIONAL TEST OF THE PAX DOOR IAW CRJ 900 AMM 52-11-00-710-801 (A02). OPERATIONAL TEST GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,773 hrs · 25,173 cycles

FOUND PAX DOOR DD7A INTERCOSTAL TO BE CORRODED. NEW SERVICEABLE PAX DOOR DD7A INTERCOSTAL P/N : 601R318083-1 HAS BEEN LOCATED AND DRILLED IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED PAX DOOR DD7A INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: HINGE — CRACKED (ZONE 200) · airframe 35,773 hrs · 25,173 cycles

PAX DOOR HINGE FWD LUG IS CRACKED. REMOVED PAX DOOR HINGE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR HINGE PN 601R318073-5 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED PAX DOOR HINGE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. EDGE SEALED AND RESTORED FINISH IAW CRJ900 SRM 51-14-06-001-001-A01 TR 51-0071 AND 51-21-16-001-001-A01 TR 51-0068

Part: BEARING — DAMAGED (ZONE 500 AILERON) · airframe 35,773 hrs · 25,173 cycles

" LH AILERON BEARING LUG MARKED H FOUND OVERSIZED WHEN BEARING WAS REMOVED DIA IS 1.0035"" REPAIRED IAW MHIRJ REO 690-57-61-384 REV -- DATED 2025-04-22. "

Part: BEARING — DAMAGED (ZONE 500 AILERON) · airframe 35,773 hrs · 25,173 cycles

" FOUND L/H AILERON SIDE BEARING LUG LABELED ""A"" TO BE PREVIOUSLY OVERSIZED. REPAIRED IAW MHIRJ REO 690-57-61-386 REV -- DATED 2025-04-22. "

Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 35,773 hrs · 25,173 cycles

"FOUND R/H AILERON SIDE BEARING LUG LABELED ""I"" TO BE PREVIOUSLY OVER SIZED. REPAIRED IAW MHIRJ REO 690-57-61-383 REV -- DATED 2025-04-18 "

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,773 hrs · 25,173 cycles

FOUND PAX DOOR DD6 MID INTERCOSTAL TO BE CORRODED. INSTALLED SERVICEABLE INTERCOSTAL MID DD6 (PN: 601R318057-1) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,773 hrs · 25,173 cycles

FOUND FS 280 L/H CROSSBEAM TO HAVE SPOTS OF CORROSION BETWEEN BL 0 AND LBL 12. INSTALLED L/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01. REF. CRJ 900 SRM 53-11-10-201-004-A01 FOR ALTERNAT FASTENERS.

Part: WEB — CORRODED (ZONE 200) · airframe 35,773 hrs · 25,173 cycles

"FOUND R/H F.S. 280 WEB TO BE CORRODED. REMOVED CORROSION FROM R/H F.S. 280 LWR WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG. .040"", REMOVED .007"" REMAINING .033"", ALLOWABLE .005"". FABRICATED, LOCATED AND MATCH DRILLED SERVICEABLE R/H F.S. 280 LWR WEB REPAIR PARTS IAW CRJ 900 SRM 53-11-10-201-004-A01. R/H F.S. 280 LWR WEB REPAIR PARTS FABRICATED FROM 7075 T-6 .040"" PO# 5-23072. INSTALLED FS 280.00 NEW RH LOWER WEB IAW CRJ900 SRM 53-11-10-201-004-A01 STEP 5.B (4 AND 5). COMPLIED WITH REMAINING STEPS OF CRJ900 SRM 53-11-10-201-004-A01. STEP 5.B(6 THRU 10) AND 6.A."

Part: WEB — CORRODED (ZONE 200) · airframe 35,773 hrs · 25,173 cycles

"FOUND L/H F.S. 280 WEB TO BE CORRODED. REMOVED CORROSION FROM L/H F.S. 280 LWR WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG. .040"", REMOVED .009"" REMAINING .031"", ALLOWABLE .005"". FABRICATED, LOCATED AND MATCH DRILLED SERVICEABLE L/H F.S. 280 LWR WEB REPAIR PARTS IAW CRJ 900 SRM 53-11-10-201-004-A01. L/H F.S. 280 LWR WEB REPAIR PARTS FABRICATED FROM 7075 T-6 .040"" PO# 5-23072. INSTALLED FS 280.00 NEW LH LOWER WEB IAW CRJ900 SRM 53-11-10-201-004-A01 STEP 5.B (4 AND 5). COMPLIED WITH REMAINING STEPS OF CRJ900 SRM 53-11-10-201-004-A01. STEP 5.B(6 THRU 10) AND 6.A."

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,773 hrs · 25,173 cycles

FOUND FS 280 R/H CROSSBEAM TO HAVE MULTIPLE SPOTS OF CORROSION BETWEEN BL 0 AND RBL 12. UPON FURTHER EVALUATION FOUND FS 280 R/H CROSSBEAM FOUND OUT OF LIMITS IAW CRJ 900 SRM 53-00-00-101-001-A01. DUE TO 100% MATERIAL LOSS. REMOVED R/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE FS 280 R/H CROSSBEAM (PN# CC670-34094JP-2S) IAW CRJ900 SRM 51-40-11-001-001-A01. LOCATED AND DRILL HOLES COMMON TO RH FLOOR SILL AND 280 CROSSBEAM AND INSTALLED RIVETS IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED R/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01. REF. CRJ 900 SRM 53-11-10-201-004-A01 FOR ALTERNAT FASTENERS. APPLIED PAINT AND CIC REQUIRED ON FWD & AFT SIDE OF R/H FS 280 CROSSBEAM IAW CRJ900 SRM 51-25-21-001-001-A01 AND 51-21-11-001-001-A01.

Part: DOUBLER — CHAFED (ZONE 100) · airframe 35,773 hrs · 25,173 cycles

"THERE IS A CHAFE ON THE AFT LAVATORY DUMP CANNON PLUG DOUBLER. REMOVED 3 RIVETS IAW CRJ-900 SRM 51-42-06-001-001-A01 IN ORDER TO BLEND CHAFED AREA. BLENDED CHAFED AREA IAW CRJ-900 SRM 51-12-00-001-001-A01. MAX MATERIAL REMOVED WAS 0.005"".. ORIGINAL THICKNESS WAS 0.125"" WITH REMAINING THICKNESS AFTER BLENDING OF 0.120"". DOUBLER THICKNESS IS WITHIN LIMITS IAW CRJ-900 SRM 53-00-00-101-001-A01 WITH LESS THAN 10% OF MATERIAL REMOVED. UT C/W ON REWORKED AREAS OF THE AFT LAVATORY DUMP CANNON PLUG DOUBLER IAW CRJ 900 NDTM PT 1 51-20-004-270-A01 FOUND LOWEST MRT TO BE .121"" OR GREATER HFEC PERFORMED ON REWORKED AREAS OF THE AFT LAVATORY DUMP CANNON PLUG DOUBLER IAW CRJ 900 NDTM PT 1 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME REPLACED 3 RIVETS THAT WERE REMOVED FOR BLENDING IAW CRJ-900 SRM 51-42-06-001-001-A01. RECEIVED, C/W, AND ATTACHED ENDEAVOR AIR EA# CRJ953-19048, REV IR, DATED 4/11/2025. NOTES"

Part: DOUBLER — CHAFED (ZONE 400) · airframe 35,773 hrs · 25,173 cycles

"LOWER R/H TRANS COWL LATCH DOOR COAMING IS CHAFED REMOVED AND REPLACED LOWER R/H TRANS COWL LATCH DOOR COAMING IAW REO 670-54-21-1207 REV NC DATED 2014-07-30. LOCATED AND DRILLED NEW SERVICEABLE LOWER R/H TRANS COWL CHANNEL P/N CN624-2049-201 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE LOWER R/H TRANS COWL CHANNEL P/N CN624-2049-201 IAW CRJ900 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LOWER R/H TRANS COWL DOUBLER P/N CN624-2068-209 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE LOWER R/H TRANS COWL DOUBLER P/N CN624-2068-209 IAW CRJ900 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED ""CAUTION BEFORE OPENING OR CLOSING "" DECAL IAW CRJ 900 AMM 20-60-04-400-801-A01"

Part: FRAME — CORRODED (ZONE 100) · airframe 35,773 hrs · 25,173 cycles

CORROSION AT FS310 ON FRAME FROM FLOOR SUPPORT POST TO STGR 22R REPAIRED IAW CRJ 900 SRM 53-00-06-201-001-A03.

Part: NONE — NONE (NONE) · airframe 35,449 hrs · 24,901 cycles

WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL 05/2022 FOUND FITTINGS PN CC670-33563-001SB AND CC670-33562-001SB AT STR12A LH AND RH SIDES CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING AIRCRAFT FASTENER LOCATIONS REPAIRED IAW MHIRJ REO 690-53-11-1930 REV-- 1/25/2025.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,449 hrs · 24,901 cycles

WHILE PERFORMING R53595-R-R BLIND BLTS ON PRES FLR SILL DECK AT FS792-801 WE FOUND CORROSION ON THE R/H SIDE SILL DECK AT FS792 AND FS801. REPAIRED IAW MHIRJ REO 690-53-41-511 REV -- DATED 2025-01-19

Part: LUG — CRACKED (ZONE 200) · airframe 35,449 hrs · 24,901 cycles

L/H FWD EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV- DATED 2024-11-06

Part: LUG — CRACKED (ZONE 200) · airframe 35,449 hrs · 24,901 cycles

R/H AFT EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV0 DATED 2024-11-06

Part: LUG — CRACKED (DOOR FRAME) · airframe 35,449 hrs · 24,901 cycles

R/H FWD EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV-- DATED 2024-11-06

Part: CONTROLLER — FAULTED (F/O WINDSHIELD) · airframe 33,890 hrs · 23,555 cycles

DURING CRUISE FIRST OFFICER SIDE WINDSHIELD HEATER, AT THE LOWER RIGHT CORNER, BEGAN TO SMOKE AND SPARK. DEACTIVATED RH WINDSHIELD HEAT SWITCH WHICH STOPPED THE SPARKING BUT FUMES AND OCCASIONAL SMOKE CONTINUED DURING THE DESCENT AND ON THE GROUND. REMOVED AND REPLACED FIRST OFFICER SIDE WINDSHIELD IAW J/C 900-56-900-901. ALSO REPLACED THE WINDSHIELD TEMP CONTROLLER IAW AMM 30-41-06. ALL OPS AND LEAK CHECKS GOOD.

Part: LAMP — INOPERATIVE · airframe 29,943 hrs · 20,274 cycles

AFT EXTERIOR (LH & RH) EMERGENCY LIGHTS INOP. R/R AFT EXTERIOR (LH & RH) EMERGENCY LIGHT BULBS IAW CRJ 900 AMM 33-51-15. OPS CHECK GOOD. PN ON/OFF (LH & RH) # 8GH002473-08.

Part: SENSOR — INOPERATIVE · airframe 29,087 hrs · 19,573 cycles

BRAKE OVERHEAT WARNING IN FLIGHT, RAN QRH, MESSAGE CLEARED THEN CAME BACK WHEN THE GEAR WAS RETRACTED. REMOVED AND REPLACED LHOB BRAKE TEMP SENSOR IAW CRJ900 AMM 32-46-01

Part: SKIN PANEL — GOUGED · airframe 28,741 hrs · 19,291 cycles

1EA GOUGE ON R/H WING PNL 622BL IN:TM EMP#:884 BLENDED 2EA GOUGES ON R/H WING L/E PNL 622BL IAW CRJ 900 SRM 51-12-00, REPAIRED IAW ENDEAVOR AIR EA# CRJ 957-12194

Part: WIRE HARNESS — NOT SEATED · airframe 28,741 hrs · 19,291 cycles

FWD FACING AISLE EMERGENCY LIGHT IS INOPERATIVE. RESEATED CONNECTOR P339 ALL WORK DONE IAW CRJ WM 33-50-01 OP CHECK GOOD IAW CRJ 900 AMM 33-51-00

Part: FLOORBEAM — CORRODED · airframe 28,741 hrs · 19,291 cycles

LBL 27.00 FLOORBEAM CAP IS CORRODED FRAME STATION 997 TO FRAME STATION 1047 IN MULTIPLE AREAS. J/C 900-53-180-300 REPAIRED LBL 27.00 FLOORBEAM F.S. 997 TO F.S. 1047 IAW MHIRJ 690-53-61-1028. REPAIRED BLEND AREA 8 ON LBL 27.00 FLOORBREAM IAW ENDEAVOR AIR EA NO:CRJ953-12050

Part: STIFFENER — CRACKED · airframe 28,741 hrs · 19,291 cycles

PAX. DOOR POWER ASSIST MOTOR MOUNT BRACKET IS CRACKED. J/C 900-52-830-500 INSTALLED NEW POWER ASSIST MOTOR MOUNT BRACKET (STIFFENER) IAW CRJ 900 SRM 51-42-11.

Part: HINGE FITTING — GOUGED · airframe 28,741 hrs · 19,291 cycles

LH WING T/E #3 AILERON HINGE MOUNT FITTING HAS TOOLING MARK DAMAGE. J/C 900-57-590-503 REPAIRED LH WING T/E #3 AILERON HINGE MOUNT FITTING I.A.W. BOMBARDIER REO #690-57-51-231 REV-DATED 2021-09-04

Part: SKIN — GOUGED · airframe 28,741 hrs · 19,291 cycles

AFT LOWER FUSE SKIN @ F.S. 913-927 AT STR 27 HAS GOUGE. THE DAMAGE WAS REPAIRED IAW REO 670-53-00-290 REV. F.

Part: FRAME — CORRODED · airframe 28,741 hrs · 19,291 cycles

CORROSION ON LOWER FLANGE AT FRAME FS319.7 BETWEEN STGR 26L TO STGR27 JC: 900-53-140-500 IN:AV EMP#: 873 CORROSION ON LOWER FLANGE @ F.S. 319.7 BETWEEN STGR 26L TO 27L REPAIRED IAW EA CRJ953-12029.

Part: ANGLE — CORRODED · airframe 28,741 hrs · 19,291 cycles

CORROSION ON NUTPLATES AT FS 280 CRAWLWAY ANGLE SUPPORT JC: 900-53-140-500 IN:AV EMP#:873 REMOVED & REPLACED FWD CRAWLWAY ANGLE SUPPORT P/N: CC670-34095-3 IAW CRJ900 SRM'S 51-40-11, 51-43-06 & 51-42-13

Part: SEAT TRACK — GOUGED · airframe 28,741 hrs · 19,291 cycles

SEAT TRACK GOUGE AT STA 661+8.40 WL 72.50 I/B TRACK (RED DOT) R/H INSIDE. JC:900-53-900-126 IN:RR EMP#:1092 REMOVED AND REPLACED SEAL TRACK F.S. 661.00 +8.40 TO F.S. 693.00 IAW CRJ 900 SRM 51-41-02.

Part: FRAME — CORRODED · airframe 28,741 hrs · 19,291 cycles

CORROSION ON LOWER FLANGE AT FRAME FS310 BETWEEN STGR25L TO STGR26L JC:900-53-14-500 IN:AV EMP#:873 REMOVED CORROSION ON LOWER FLANGE AT FRAME 310 BTW STGR25L TO STGR26L FOUND -002" MATERIAL LOST-REF TO EA #CRJ953-11999

Part: STRINGER — CORRODED · airframe 28,741 hrs · 19,291 cycles

CORROSION ON STGR 26L FS 280+5 JC:900-53-140-500 IN:AV EMP#:873 REMOVED CORROSION ON STGR 26L FS280. FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 53-21-06. REMOVED & REPLACED NEW STGR IAW CRJ 900 SRM 51-40-11 & 51-42-06

Part: BUTTSTRAP — CORRODED · airframe 28,741 hrs · 19,291 cycles

CORROSION ON BUTTSTRAP AT FS 280 BETWEEN STGR 25L TO STGR 26L JC:900-53-140-500 IN:AV EMP#:873 REPAIRED BUTTSTRAP AT F.S. 280 BETWEEN STGR 25L TO STGR 26L IAW ENDEAVOR AIR CRJ900 EA NO: CRJ953-12172 EA REV IR

Part: BUTTSTRAP — CORRODED · airframe 28,741 hrs · 19,291 cycles

"CORROSION ON BUTTSTRAP AT FS 280 BETWEEN STGR 24L TO STGR 25L JC:900-53-140-500 IN:AV EMP#:873 REPAIRED BUTTSTRAP AT F.S. 280 BETWEEN STGR 24L TO STGR 25L IAW ENDEAVOR AIR CRJ900 EA NO: CRJ953-12173 EA REV I R

Part: ANGLE — CRACKED · airframe 28,741 hrs · 19,291 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED IN:DG EMP#:281 REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW CRJ900 SRM 52-11-04

Part: SKIN — SCRATCHED · airframe 28,741 hrs · 19,291 cycles

SCRATCH ON SKIN AT ZONE 132 MARKED RED DOT. JC:900-53-130-300 IN:RR EMP#:1092 REPAIRED 2EA, AREA AND RESTORED FINISH IAW CRJ900 EA CRJ953-11903

Part: SKIN — GOUGED · airframe 28,741 hrs · 19,291 cycles

MID CARGO DOOR LOWER AFT CORNER DAMAGED (RED DOT). JC:900-52-810-303 EMP#:1092 MID CARGO DOOR LOWER AFT CORNER REPAIRED IAW EA NO: CRJ952-11905

Part: HINGE ARM — GOUGED · airframe 28,741 hrs · 19,291 cycles

MID CARGO DOOR AFT HINGE GOUGED AND DAMAGED (RED DOT) JC:900-52-810-303 IN:RR EMP#1092 MID CARGO DOOR AFT HINGE REPAIRED IAW EA NO CRJ952-11930

Part: SKIN — DENTED · airframe 28,741 hrs · 19,291 cycles

FUSELAGE SKIN DENTED RH AND 1.0 INCHES OF AFT FS. 310.00 BETWEEN STRINGERS 20 R AND 21R JC:900-53-900-310 IN:TS EMP#:432 RE-FORM DENTED SKIN TO ORIGINAL CONTOUR ENDEAVOR AIR EA# CRJ953-11934 ROW A NO MATERIAL LOSS

Part: ELECTRICAL BOX — CRACKED · airframe 28,741 hrs · 19,291 cycles

EXT. POWER RECEPTACLE/ PLUG IN, BOX STRUCTURE CRACKED ON I/B SIDE OF RECEPTACLE. JC:900-53-130-300 IN:TB EMP#:432. REMOVED AND REPLACED AC EXTERNAL POWER RECEPTACLE BOX IAW (REO) 670-53-11-029 (CC670-33401 REF)

Part: KNOB — LOOSE (MEGAPHONE) · airframe 24,153 hrs · 15,676 cycles

MEGAPHONE VOLUME KNOB WAS LOOSE. ADJUSTED AND REATTACHED IAW AMM 25-61-14, OPS CHECKED GOOD.

Part: CONTROL UNIT — INOPERATIVE (INTERPHONE) · airframe 24,050 hrs · 15,595 cycles

MID CABIN FLIGHT ATTENDANT EMERGENCY LIGHT NOT ILLUMINATING. REMOVED & REPLACED THE INTERPHONE CONTROL UNIT IAW AMM 23-31-07. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 20 CD) · airframe 23,567 hrs · 15,249 cycles

OXYGEN MASKS AT ROW 20 CD DEPLOYED. REPACKED AND STOWED THE PAX OXYGEN MASKS IAW AMM 35-21-09.

Part: STRIKER — GOUGED (PAX DOOR SEAL) · airframe 22,809 hrs · 14,694 cycles

PASSENGER DOOR SEAL STRIKER IS GOUGED AT FWD UPPER LATCH PIN FITTING. REPAIRED THE STRIKER IAW SRM 53-21-23-201-006-A01. LEAK & OPS TESTED GOOD IAW AMM 52-00-00-790-801.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 22,809 hrs · 14,694 cycles

PAX DOOR WEB ANGLE CRACKED AT CABLE PULLEY BRACKET FOR POWER ASSIST MOTOR. REPAIRED PAX DOOR WEB ANGLE AT CABLE PULLEY BRACKET IAW SRM 52-11-04.

Part: SMOKE DETECTOR — DAMAGED (CARGO BAY) · airframe 22,809 hrs · 14,694 cycles

SMOKE DETECTOR IS DAMAGED IN AFT CARGO AREA. REMOVED AND REPLACED DAMAGED SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK TO BE ACCOMPLISHED ON W/O 1015257 2000 0002 S/N5966396 ITEM BLOCK 2.

Part: LIGHT — INOPERATIVE (MAIN CABIN) · airframe 22,653 hrs · 14,575 cycles

EMERGENCY LIGHTS SOME BULBS ARE NOT WORKING PERFORMED OPS TEST OF THE ACCENTS LIGHTS IAW CRJ900AMM 33-21-00 OPS TE ST GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

FOUND BOTH REAR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT PS38 IAW AMM 33-51-17. OPS CHECKED GOOD. NO OTHER DEFECTS NOTIED.

Part: SMOKE DETECTOR — NO TEST (FWD LAVATORY) · airframe 22,404 hrs · 14,404 cycles

FWD LAVATORY SMOKE DETECTOR NOT TESTING, NO EVIDENCE OF HALON DISCHARGE. PERFORMED AN OPS CHECK OF FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00. NO DEFECTS NOTIED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (MAIN CABIN) · airframe 22,040 hrs · 14,161 cycles

DURING FA SAFETY CHECKS, THE EMERGENCY LIGHT TEST FAILED. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW 33-51-00, OPS CHECKED NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 14) · airframe 21,354 hrs · 13,661 cycles

PAX OXYGEN MASK DEPLOYED AT ROW 14 A&B. RESTOWED THE OXYGEN MASKS IAW AMM 35-20-00-710-810. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BEARING — CRACKED (BS 797) · airframe 20,055 hrs · 12,746 cycles

LEFT AND RIGHT WING TO FUSELAGE LINKS AT BS 797 ARE CONTACTING AT UPPER AND LOWER FITTINGS AND BOTH LOWER BEARINGS ARE CRACKED. COMPLIED WITH EO'S R57189, R57190 AND R57200. OP CHECKED GOOD.

Part: STRINGER — CORRODED (BS 319-349) · airframe 20,055 hrs · 12,746 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 319 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-10-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 20,055 hrs · 12,746 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. REMOVED AND REPLACED THE SEAL STRIKER IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 20,055 hrs · 12,746 cycles

PAX DOOR SILL ANGLE IS CORRODED BETWEEN BS 310 - 349. REMOVED AND REPLACED THE LOWER DOOR SILL IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 1051-1088) · airframe 20,055 hrs · 12,746 cycles

STRINGER 25L FROM BS 1051.30 TO 1088.20 IS CORRODED. REPAIRED THE STRINGER IAW EA CRJ953-04902 REV IR.

Part: STRINGER — CORRODED (BS 364-379) · airframe 20,055 hrs · 12,746 cycles

STRINGER 23R CORRODED BETWEEN BS 364-379. REPAIRED THE STRINGER IAW EA CRJ 953-04922.

Part: FITTING — CORRODED (BS 265-280) · airframe 20,055 hrs · 12,746 cycles

RIGHT JACK SUPPORT FITTING IS CORRODED BETWEEN BS 280 - 265. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-000-A01 & 51-42-21-001-001-A01 & EA CRJ 953-04951.

Part: FLOORBEAM — CORRODED (BS 1047) · airframe 20,055 hrs · 12,746 cycles

FLOORBEAM AT BS 1047 HAS CORROSION ON TOP BETWEEN RBL 27 AND 34. REPAIRED IAW EA CRJ 953-04916.

Part: STRINGER — CORRODED (BS 333-364) · airframe 20,055 hrs · 12,746 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 319 - 349. REMOVED AND REPLACED STRINGERS IAW SRM 51-10-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 1047) · airframe 20,055 hrs · 12,746 cycles

FLOORBEAM AT BS 1047 HAS CORROSION ON TOP BETWEEN RBL 27 AND 34. REPAIRED IAW EA CRJ 953-04916.

Part: LINK — CORRODED (BS 797) · airframe 20,055 hrs · 12,746 cycles

LEFT AND RIGHT WING TO FUSELAGE LINKS AT BS 797 ARE CONTACTING AT UPPER AND LOWER FITTINGS AND BOTH LOWER BEARINGS ARE CRACKED. COMPLIED WITH ENDEAVOR AIR EO'S R57189, R57190 AND R57200. OP CHECKS GOOD.

Part: STRINGER — CORRODED (BS 1051-1088) · airframe 20,055 hrs · 12,746 cycles

STRINGER 24L FROM BS 1051.30 TO 1088.20 IS CORRODED. REPAIRED THE STRINGER IAW EA CRJ953-04897 REV IR.

Part: STRINGER — CORRODED (BS 295-310) · airframe 20,055 hrs · 12,746 cycles

STRINGER 19R HAS CORROSION BETWEEN BS 295 TO 310. REPAIRED THE STRINGER IAW EA CRJ953-04927.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 20,055 hrs · 12,746 cycles

GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED LOWER GALLEY SERVICE DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 1069-1088) · airframe 20,055 hrs · 12,746 cycles

STRINGER 23L FROM BS 1069.75 - 1088.20 IS CORRODED. REPAIRED THE STRINGER IAW EA CRJ953-04896.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,055 hrs · 12,746 cycles

INTERCOSTAL STRINGER 27R BETWEEN BS 349 - 364 CORRODED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 977-1000) · airframe 20,055 hrs · 12,746 cycles

LEFT FLOOR SUPPORT IS CORRODED FROM BS 977 TO 1000. REPAIRED THE FLOOR SUPPORT IAW EA CRJ953-04915 REV B.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,055 hrs · 12,746 cycles

INTERCOSTAL STRINGER 27L BETWEEN BS 349 - 364 CORRODED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 20,055 hrs · 12,746 cycles

STRINGER 21R IS CORRODED BETWEEN BS 319 TO 333. REMOVED AND REPLACED THE STRINGER IAW SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 & 51-24-36-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

STRINGER 21R CORRODED AT FS 364 - FS 379. REMOVED & REPLACED STRINGER 21R, FS 333-379 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 280-333) · airframe 20,055 hrs · 12,746 cycles

STRINGER 21R IS CORRODED BETWEEN BS 319 TO 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 & 51-24-36-001-001-A01.

Part: STRINGER — CORRODED (BS 349-364) · airframe 20,055 hrs · 12,746 cycles

CORROSION FOUND AROUND FASTENERS ON STR 24R BETWEEN BS 349 AND 364. REPAIRED THE STRINGER IAW EA CRJ953-04934 DATED 10-19-2016 REV IR.

Part: STRINGER — CORRODED (BS 295-310) · airframe 20,055 hrs · 12,746 cycles

STRINGER 20R HAS CORROSION BETWEEN BS 295 TO 310. REPAIRED IAW EA CRJ953-04928 REV IR.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

INTERCOSTAL PN MM670-43251-009 AND SUB FRAMES PN MM670-43253-011 AND PN MM670-43253-013 HAVE ELONGATED AND DOUBLE DRILLED HOLES AND NEED REPLACEMENT. FABRICATED INTERCOSTAL IAW EA CRJ953-04930 & SUB FRAMES IAW EA CRJ953-04935 REV A. INSTALLED INTERCOSTAL AND SUB FRAMES IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 285) · airframe 20,055 hrs · 12,746 cycles

RIGHT FLOOR SUPPORT IS CORRODED AT BS 285. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 319-349) · airframe 20,055 hrs · 12,746 cycles

INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN BS 310 - 349. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND AMM 51-80-00-140-801-A01.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 20,055 hrs · 12,746 cycles

INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN BS 310 - 349. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND AMM 51-80-00-140-801-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 20,055 hrs · 12,746 cycles

FS 280 TRANVERSE BEAM IS CORRODED AROUND SEVERAL FASTENER HOLES AND AT MACHINED EDGE AT APPROX RBL 1.5 CORROSION ON MACHINED EDGE GOES COMPLETELY THROUGH PART IN TO RADIUS. REMOVED RH FS 280 TRANSVERSE BEAM AND INSTALLED SERVICEABLE BEAM IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-42-21-001-001-A01 AND 51-21-11-001-001-A01.

Part: BEAM — CORRODED (BS 280) · airframe 20,055 hrs · 12,746 cycles

900-53-900-504; LH FS 280 TRANSVERSE BEAM IS CORRODED AROUND FASTENER HOLES AND CRACKED AT APPROX LBL 12. REMOVED THE TRANSVERSE BEAM AND INSTALLED SERVICEABLE BEAM IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-42-21-001-001-A01 AND 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 330-349) · airframe 20,055 hrs · 12,746 cycles

STRINGER 26R HAS CORROSION BETWEEN BS 330 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A011, 51-42-21-001-001-A01, 51-25-00-001-001-A01 AND 51-25-00-001-00-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,055 hrs · 12,746 cycles

RIGHT BULKHEAD WEB AT BS 280 IS CORRODED AT RBL 11 AT WL 72.5. REPLACED THE LOWER BULKHEAD WEB, IAW REO:670-53-11-594, STEPS 3-12.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 20,055 hrs · 12,746 cycles

J ANGLE IS CORRODED AT BS 280 FLOORBEAM BETWEEN LBL 12 TO RBL 12. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 20,055 hrs · 12,746 cycles

STRINGER SPLICE 26R, BS 333 HAS CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-21-11-001-001-A01 AND 51-25-00-001-001-A01.

Part: STRINGER — CORRODED (BS 342) · airframe 20,055 hrs · 12,746 cycles

STRINGER 26L, BS 342 HAS CORROSION AROUND RIVET BUCKTAIL. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 AND 51-21-11-001-001-A01.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

LT WEB AT FS 280 IS CORRODED AT LBL 11 AT WL 72.5. REPAIRED FS 280 LT WEB AT LBL 11 WL 72.5 REO 670-53-11-594 REV A STEPS 3-12. COMPLIED WITH BY REPLACING LT LOWER WEB P/N:670-53-11-594-1.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

LT WEB AT FS 280 IS CORRODED AT LBL 11 AT WL 72.5. REPAIRED FS 280 LT WEB AT LBL 11 WL 72.5 REO 670-53-11-594 REV A STEPS 3-12. COMPLIED WITH BY REPLACING LT LOWER WEB PN 670-53-11-594-1.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,055 hrs · 12,746 cycles

RIGHT BULKHEAD WEB AT BS 280 IS CORRODED, RBL 11, WL 72.5. REPLACED THE LOWER BULKHEAD WEB IAW REO:670-53-11-594, STEPS 3-12.

Part: SEAT TRACK — CORRODED (BS 573-661) · airframe 20,055 hrs · 12,746 cycles

RIGHT FWD FUSELAGE SEAT TRACK CORRODED. REMOVED, FABBED, LOCATED, DRILLED, AND INSTALLED THE SEAT TRACK IAW REO 670-53-00-343 REV M AND SRM 51-40-11-001-001-A01, AND AMM 53-00-49-400-801-A01.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 20,055 hrs · 12,746 cycles

RIGHT FLOOR SUPPORT IS CORRODED BETWEEN FS 349 TO FS 364. REPAIRED THE FLOOR SUPPORT IAW EA CRJ953-04898 REV B.

Part: ATTACH ANGLE — CORRODED (INTERCOSTAL) · airframe 20,055 hrs · 12,746 cycles

ANGLE ATTACHING TO INTERCOSTAL AT STRINGER 20R BS 349 IS CORRODED. REMOVED AND INSTALLED THE ATTACH ANGLE IAW SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 573-661) · airframe 20,055 hrs · 12,746 cycles

RIGHT FWD FUSELAGE SEAT TRACK CORRODED. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED THE SEAT TRACK IAW REO 670-53-00-343 REV M AND SRM 51-40-11-001-001-A01, AND AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (FS 743 -763) · airframe 20,055 hrs · 12,746 cycles

RIGHT FWD FUSELAGE SEAT TRACK CORRODED. REMOVED, FABRICATED, LOCATED,DRILLED, AND INSTALLED THE SEAT TRACK IAW REO 670-53-00-343 REV M AND SRM 51-40-11-001-001-A01 AND CJR 900 AMM 53-00-49-400-801-A01

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 20,055 hrs · 12,746 cycles

RIGHT FLOOR SUPPORT IS CORRODED BETWEEN BS 349 - 364. REPAIRED THE FLOOR SUPPOR IAW EA CRJ953-04898 REV B.

Part: SEAT TRACK — CORRODED (BS 670-720) · airframe 20,055 hrs · 12,746 cycles

RIGHT SEAT TRACK NR 5 FROM BS 670.85 - 720.85 CORRODED AND WORN IN SPOTS. REMOVED THE SEAT TRACK AND FABRICATED A NEW SEAT TRACK AND INSTALLED IAW AMM 53-00-49-000/-400-801-A07, SRM 51-40-11-001-001-A01, 51-31-16-001-001-A01 AND REO 670-53-00-343.

Part: THRESHOLD — CORRODED (BS 319-349) · airframe 20,055 hrs · 12,746 cycles

SERVICE DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED SERVICE DOOR CORRODED THRESHOLD WITH A NEW SERVICEABLE THRESHOLD IAW SRM 51-42-06-001-001-A01.

Part: ATTACH ANGLE — CORRODED (BS 349) · airframe 20,055 hrs · 12,746 cycles

ATTACH ANGLE TO INTERCOSTAL AT STRINGER 20R BS 349 IS CORRODED. REMOVED AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

CORROSION ON SEAT TRACK AT RBL 12 BETWEEN FS 847.00 AND FS 977.00 AT VARIOUS LOCATIONS. REMOVED AND INSTALLED NEW SEAT TRACKS AT RBL 9.00 BETWEEN FS 847.00 TO FS 977.00 IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND SRM 51-41-02-001-001-A01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

CORROSION ON SEAT TRACK AT RBL 12 BETWEEN FS 847.00 AND FS 977.00 AT VARIOUS LOCATIONS. REMOVED AND INSTALLED NEW SEAT TRACKS AT RBL 9.00 BETWEEN FS 847.00 TO FS 977.00 IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND SRM 51-41-02-001-001-A01 AND 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,055 hrs · 12,746 cycles

RT AFT FUSELAGE SEAT RAILS 8 HAS CORROSION. REMOVED DAMAGED SEAT TRACK SEGMENT. FABRICATED NEW SERVICEABLE SEAT TRACK SEGMENT AND INSTALLED NEW SERVICEABLE SEAT TRACK SEGMENT AT FS 851.03 - FS 865.00 IAW AMM 53-00-49-000-801-A07, AMM 53-00-49-400-801-A07, SRM 51-40-11-001-001-A01 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,055 hrs · 12,746 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 477 AND 669. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, REO 670-53-00-343 REV M AND AMM 53-00-49-000/400-801-A07.

Part: STIFFENER — CORRODED (BS 942-954) · airframe 20,055 hrs · 12,746 cycles

FLOORBEAM STIFFENER IS CRACKED & BENT AT RBL 12 BETWEEN BS 942 & 954. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-21-001-001-A01 AND EA CRJ95304907.

Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 20,055 hrs · 12,746 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 477 AND 669. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, REO 670-53-00-343 REV M AND AMM 53-00-49-000/400-801-A07.

Part: STIFFENER — CRACKED (BS 280) · airframe 20,055 hrs · 12,746 cycles

VERTICAL STIFFENER ON FWD SIDE OF FS 280 BEAM AT RBL 26 IS CRACKED. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-691) · airframe 20,055 hrs · 12,746 cycles

LBL 9 SEAT TRACK IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 477 AND 669. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, REO 670-53-00-343 REV M AND AMM 53-00-49-000/400-801-A07.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 20,055 hrs · 12,746 cycles

FLOORBEAM ANGLE BS 280 IS CORRODED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 20,055 hrs · 12,746 cycles

STRINGER SPLICE 25R HAS CORROSION BS 333. REMOVED AND REPLACED THE STRINGER SPLICE 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 (BS 349 - 479) · airframe 20,055 hrs · 12,746 cycles

SEAT TRACK AT RBL 9, BS IS CORRODED BETWEEN BS 349 - 379. REMOVED, FABRICATED & INSTALLED A SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000/400-801-A07, REO 670-53-00-343, SRM 51-40-11-001-001-A01, 51-21-11-001-001-A01, AND 51-21-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 743-763) · airframe 20,055 hrs · 12,746 cycles

LEFT AFT FUESLAGE SEAT TRACK CORRODED. FABRICATED & INSTALLED THE SEAT TRACKS IAW REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-866) · airframe 20,055 hrs · 12,746 cycles

LEFT AFT FUESLAGE SEAT TRACK CORRODED. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 787-747) · airframe 20,055 hrs · 12,746 cycles

LEFT AFT SEAT TRACKS CORRODED. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 565 - 677) · airframe 20,055 hrs · 12,746 cycles

LEFT FWD SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, 51-40-11-001-010-A01 & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 20,055 hrs · 12,746 cycles

CORROSION ON SEAT TRACK AT LBL 12 BETWEEN BS 847 AND 977 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-07, SRM 51-40-11-001-001-A01 AND REO 670-53-00-343 REV M.

Part: PANEL — CHAFED (RT AILERON) · airframe 20,055 hrs · 12,746 cycles

699AB IS CHAFED. RECEIVED SERVICEABLE PART. LOCATED, DRILLED AND COUNTERSUNK IAW SRM 51-40-11-001-001-A01.

Part: ANGLE — CORRODED (PASSENGER DOOR) · airframe 20,055 hrs · 12,746 cycles

PAX DOOR MID CAP ANGLE IS CORRODED BETWEEN BS 310 - 349. REMOVED CORRODED PAX DOOR MID CAP ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-40-11-001-001-A01 AND AMM 20-21-00-910-801-A01.

Part: SEAT TRACK — CORRODED (BS 847-985) · airframe 20,055 hrs · 12,746 cycles

CORROSION ON SEAT TRACK AT LBL 12 BETWEEN BS 847 AND 977 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, SRM 51-40-11-001-001-A01 AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 677-722) · airframe 20,055 hrs · 12,746 cycles

LEFT FWD SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, 51-40-11-001-010-A01 & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 613-669) · airframe 20,055 hrs · 12,746 cycles

RBL 9 FLOOR SEAT TRACK IS CORRODED AT BS 669 AND 613. REMOVED FABRICATED AND INSTALLED THE SEAT TRACK IAW REO 670-53-00-843 REV M AND AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 373-485) · airframe 20,055 hrs · 12,746 cycles

SEAT TRACK SEGMENT AT LBL 9 IS CORRODED BETWEEN BS 373 TO 379. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,227 hrs · 12,163 cycles

FLIGHT ATTENDANT REPORTS XFA JUMP SEAT FLASHLIGHT BATTERY INOPERATIVE. R & R FLASHLIGHT & HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SKIN — DENTED (TE FLAP) · airframe 17,255 hrs · 10,861 cycles

PERMANENT REPAIR OF THE RT FLAP LOWER SKIN. DENT MEASURES 1.34” X 1.29” X 0.020” DEEP & LOCATED AT APPROX FS 36.00, BETWEEN THE AFT SPAR & INTERCOSTAL SPAR. REPAIRED IAW EA CRJ957-03678.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 17,263 hrs · 10,868 cycles

COPILOT FLASHLIGHT INOPERATIVE. R & R FIRST OFFICERS EMER FLASHLIGHT BATTERY PACK IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.

Part: DETECTOR — MALFUNCTIONED (TE FLAP) · airframe 17,265 hrs · 10,870 cycles

FLAP FAIL CAUTION, FLAP FAIL 9 DEGREES, SLATS 0 DEGREES, LNG WGT 74500 & SPEED 180 KTS. R & R LHIB SKEW DETECTOR IAW AMM 27-52-45. OPERATIONS CHECKED GOOD.

Part: COVER — MISSING (CABIN) · airframe 16,517 hrs · 10,344 cycles

AFT EMER NOTICE SIGN, RED & YELLOW LIGHT FILTERS MISSING IN AFT CABIN. DEFERRED YELLOW LENS COVER IAW MEL 23-40-1N. MX NOTIFIED, PLACARD INSTALLED. REPLACED MISSING EMER LT COVER IAW AMM 33-51-07. OPERATIONS CHECKED GOOD. THIS CLEARS MEL, MM02 UPDATED & PLACARD REMOVED.

Part: LIGHT — UNSECURE (CABIN) · airframe 16,156 hrs · 10,101 cycles

PHOTO LUMINESCENT STRIP EXIT ROW 12B CAME OFF. RESECURED EMERGENCY FLOOR STRIP AT ROW 12B IAW AMM 25-60-00.

Part: HEATER — FAILED (GALLEY) · airframe 16,041 hrs · 10,020 cycles

CABIN & COCKPIT HAD STRONG ODOR OF EXHAUST FUMES DURING FLIGHT. FUMES PERSISTENT AFTER LANDING. R & R GALLEY HEATER IAW AMM 21-23-64.

Part: LENS — MISSING (EXIT SIGN) · airframe 15,191 hrs · 9,459 cycles

SERVICE DOOR EXIT LIGHT LENS COVER IS MISSING. INSTALLED EXIT SIGN LENS IAW AMM 33-51-05. PART ON BC5-0393-288, SERIAL N/A.

Part: PANEL — CHAFED (WING) · airframe 15,126 hrs · 9,417 cycles

PANEL 622CB CHAFED ON LE. DRILLED UP NEW PANEL IAW SRM 51-40-11-001-001-A01. PANEL TO BE INSTALLED ON OPERATION 192.

Part: FUSE — FAILED (BATTERY CHARGER) · airframe 15,126 hrs · 9,417 cycles

TASK CARD 900-53-140-509 FLIGHT ATTENDANT STATION G1 & G2 EMER EXIT FLOOR LEVEL LIGHTS INOPERATIVE 15. DURING TROUBLE SHOOTING FOUND FUSE F3 ON EMER BATTERY CHARGER FAILED. REPLACED FUSE IAW CMM RE 25-60-03. REMOVED & REINSTALLED EMER BATTERY CHARGER NR 1 IAW AMM 33-51-17-000-802-A02 & 33-51-17-400-802-A02. REMOVED & REINSTALLED BATTERY PACK IAW 33-51-17-000-801-A02 & 33-51-17-400-801-A02. OPERATIONS CHECKED EPSU GOOD IAW 33-51-17-710-801-A02.

Part: ACCESS PANEL — CHAFED (TE FLAP) · airframe 15,126 hrs · 9,417 cycles

RIGHT WING INBD FLAP ACCESS PANEL 684EB SHOWS CHAFE DAMAGE. CHECKED LIMITS IAW SRM 57-52-01-101-001-A01 PART OUT OF LIMITS. DRILLED NEW PANEL 684EB IAW SRM 51-40-11-001-A01.

Part: BRACKET — WORN (NR 2 COWLING) · airframe 15,126 hrs · 9,417 cycles

NUMBER 2 ENG AFT CORE COWL ALIGNMENT STANDOFF BLOCK AT 3 O'CLOCK POSITION HAS WORN ALIGNMENT FINGER. REMOVED REPAIR STRIPS FROM NR 2 CORE COWL. R & R STANDOFF ALIGNMENT BRACKET. REINSTALLED WEAR STRIPS ON NR 2 CORE COWL IAW SRM 51-42-06-001-001-A01 & AMM 54-13-00-201-A01 & SRM 54-13-00-201-006-A01.

Part: FAIRING — CHAFED (PYLON) · airframe 15,126 hrs · 9,417 cycles

RIGHT HINGE LINE FAIRING 443B CHAFED. REPLACED & DRILLED NEW SKIN HINGE FAIRING. REATTACHED STIFFENERS, PAINTED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-25-01-001-001-A01.

Part: ACCESS PANEL — CHAFED (TE FLAP VANE) · airframe 15,126 hrs · 9,417 cycles

RIGHT WING INBD FLAP VANE ACCESS PANEL 684ET SHOWS CHAFE DAMAGE. DRILLED UP NEW PANEL 684ET & INSTALLED RIVETS IAW SRN 51-42-06-001-001-A01. OLD PANEL OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. PANEL TO BE INSTALLED.

Part: ACCESS PANEL — CHAFED (TE FLAP VANE) · airframe 15,126 hrs · 9,417 cycles

LEFT WING INBD FLAP VANE ACCESS PANEL 584ET SHOWS CHAFE DAMAGE. DAMAGE FOUND TO BE OUT OF LIMITS ON PANEL 584ET IAW SRM 57-52-01-101-001-A01. LOCATED & DRILLED FASTENER HOLES IN NEW PANEL IAW SRM 51-40-11-001-001-A01. PAINTED NEW PANEL IAW SRM 51-25-01-001-001-A01.

Part: SUPPORT CHANNEL — LOOSE (FUSELAGE) · airframe 15,126 hrs · 9,417 cycles

MAIN LANDING GEAR FAIRING RT VERTICAL SUPPORT CHANNEL IS LOOSE WHERE IT SECURES TO THE LOWER SUPPORT CHANNEL DUE TO ATTACH SCREW PULLING THROUGH THE VERTICAL SUPPORT CHANNEL. REMOVED RT MLG VERTICAL SUPPORT CHANNEL. REPLACED, MATCH DRILLED & INSTALLED NEW RT MLG VERTICAL SUPPORT CHANNEL IAW SRM 51-42-21-001-01-A01 & 51-40-06-001-001-A01.

Part: HOUSING — CRACKED (E&E DOOR) · airframe 15,126 hrs · 9,417 cycles

AVIONICS BAY DOOR HANDLE HOUSING CRACKED AROUND THE HANDLE. REMOVED AVIONICS DOOR IAW AMM 52-42-00-000-801-A01. REMOVED AVIONICS DOOR HANDLE IAW 52-42-03-000-801-A01. LOCATED & DRILLED NEW HANDLE HOUSING IAW SRM 51-42-21-001-001-A01 & 51-40-11-001-001-A01. INSTALLED AVIONICS DOOR HANDLE HOUSING IAW SRM 51-42-21-001-001-A01 & 52-42-03-440-801-A01. INSTALLED AVIONICS DOOR IAW AMM 52-42-00-400-801-A01. OPERATIONS CHECKED GOOD IAW AMM 52-42-00-710-801-A01 PN OFF ON H3445-5 SN OFF ON 2026 1942.

Part: SUPPORT CHANNEL — LOOSE (FUSELAGE) · airframe 15,126 hrs · 9,417 cycles

MAIN LANDING GEAR FAIRING LT VERTICAL SUPPORT CHANNEL IS LOOSE WHERE IT SECURES TO THE LOWER SUPPORT CHANNEL. SUSPECT VERTICAL SUPPORT CHANNEL FASTENER HOLE IS WORN. PN CC670-85500-1 DWG CC 670-85500. REMOVED, DRILLED & INSTALLED NEW VERTICAL SUPPORT CHANNEL IAW SRM 51-42-21-001-001-A01 & SRM 51-40-11-001-001-A01. TORQUE WRENCH USED TC01A02-01 CAL 5-6-14 DUE 5-6-15.

Part: ACCESS PANEL — DAMAGED (TE FLAP) · airframe 15,126 hrs · 9,417 cycles

C1 RT WING INBD FLAP ACCESS PANEL 684GB SHOWS CHAFE DAMAGE. PANEL DAMAGE IS BEYOND LIMITS MATCH DRILLED NEW PANEL, PANEL WILL BE INSTALLED ON TALLY CARD 302 IAW SRM 57-52-01-101-001-A01 & 51-40-11-001-001-A01.

Part: PANEL — CHAFED (LT PYLON) · airframe 15,126 hrs · 9,417 cycles

LEFT PYLON HINGE FAIRING CHAFED. REPLACED LT PYLON HINGE FAIRING PANEL 433BB WITH NEW SKIN IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: COVER — CRACKED (CABIN) · airframe 15,126 hrs · 9,417 cycles

TASK CARD 900-53-900-107 LT & RT AFT EMER LIGHT COVERS CRACKED. R & R WITH SERVICEABLE ONES IAW CMM 33-52-07 PG 3 SECT 3 1 A & PG 4 SECT 7 B.

Part: LENS — CRACKED (CABIN) · airframe 15,126 hrs · 9,417 cycles

TASK CARD 900-53-900-308 LT & RT FWD EMER LIGHT LENS COVER CRACKED. R & R WITH SERVICEABLE ONES IAW CMM 33-52-07 PG 3 SECT 3 1 A & PG 4 SECT 7 B.

Part: VALVE — DEFECTIVE (NLG STRUT) · airframe 13,302 hrs · 8,245 cycles

GEAR DISAGREE WARNING ON EICAS, NOSE GEAR WOULD NOT LOCK IN UP POSITION, FOLLOWED CRJ900 POM NON-NORMAL. RAMP WAS CONTAMINATED, RUNWAY ONLY SLIGHTLY WITH PACKED SNOW. GEAR WAS CHECKED AFTER LANDING IN GRR & APPEARED FREE OF CONTAMINANTS. FOUND NLG STRUT FLAT VERIFIED FLUID SERVICE OF STRUT. R & R NLG STRUT AIR VLV IAW CMM 32-21-06. SERVICED NITROGEN IAW AMM 12-12-32. PERFORMED GEAR SWING IAW AMM 32-30-00, ALL CHECKED GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 13,239 hrs · 8,203 cycles

CABIN & COCKPIT FILLED WITH SMOKE AFTER APU STARTED NR 1 PACK AUTO FAIL DISPLAYED. DEFER COCKPIT TEMP CONTROL SYS IAW MEL 21-61-14. CAT C, MC ADVISED 96041. ENTERED INTO MMO2, PLACARD INSTALLED. INVESTIGATED CTRL 2481268-1 NR 1 LT AUTO PACK FAIL, SMOKE IN CABIN, DUE TO SEIZED LT ACM IAW AML 2481271-2. THIS CLEARS DTRL 2481268-1, PLACARD REMOVED FROM MMO2 MX CTRL NOTIFIED 53431.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,591 hrs · 7,793 cycles

AFT F/A FLASHLIGHT IS INOPERATIVE. R & R F/A FLASHLIGHT, IAW AMM 25-61-01.

Part: PBE — FAILED (COCKPIT) · airframe 12,201 hrs · 7,551 cycles

FLIGHT DECK PBE HAS LOST ITS VACUUM SEAL. R & R PBE SMOKE HOOD IAW JC 900-25-900-902. ACFT OK FOR SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

E/E BAY TCAS ANTENNA DOUBLER BETWEEN FS 295-310 HAS CORROSION. REMOVED AND REPLACED TCAS ANTENNA DOUBLER BETWEEN FS 293-310 E & E BAY IAW CRJ 900 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LEFT SIDE SEAT TRACK 4 CORRODED/GOUGED. REMOVED UNSERVICABLE NR 4 LEFT SIDE SEAT TRACK AND INSTALLED SERVICABLE TRACK IAW CRJ 900 AMM 53-00-43.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FS 310 FAME HAS CORROSION ON FWD SIDE BETWEEN STRINGERS 26L-25R. REMOVED CORROSION FROM FRAME 310. PART IS WITHIN LIMITS IAW CRJ 900 SRM 53-21-06 AND EO R53277.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,615 hrs · 7,180 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED AFT DRAG ANGLE IAW REO 670-52-11-072 AND REO 690-52-11-222. P/N 601R31772-55.

Part: SKIN — DAMAGED (TE FLAP) · airframe 11,615 hrs · 7,180 cycles

LEFT I/B FLAP LOWER I/B SKIN DAMAGED. REPAIRED DAMAGE IAW REO 670-57-52-160.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

RIGHT FS 280.0 LOWER WEB CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF RIGHT FS 280.0 LWR WEB IAW EO R53339.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LEFT FS 280.0 LOWER WEB CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF LEFT FS 280.00 LWR WEB IAW EO R53339.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LEFT SIDE SEAT TRACK NR 3 CORRODED/GOUGED. DOT A247 043. REMOVED AND REPLACED LEFT SIDE SEAT TRACK 3 IAW CRJ 900 AMM 53-00-49. P/N SH690-36282-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

RIGHT NR 1 FLOOR TRACK CORRODED. REMOVED AND INSTALLED RIGHT NR 1 FLOOR TRACK IAW CRJ AMM 53-00-49-400-801 PART SH670-32159-1.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FS 280.00 CROSS BEAM LOWER SIDE HAS CORROSION AREA ABOVE SERVICE LIGHT. REMOVED AND REPLACED FS 280 BEAM FWD FLOOR ANGLE SPLICE IAW CRJ 900 SRM 51-40-11. P/N CC670-34095-3S.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

SIDE SEAT TRACK STICK 4 RIGHT IS CORRODED. REMOVED AND REPLACED RIGHT NR 4 SIDE SEAT TRACK IAW CRJ 900 AMM 53-00-49. P/N SH690-36283-1.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LEFT FS 280.0 BEAM CORRODED. REMOVED AND REPLACED LEFT FS.280 BEAM IAW EO R53334. P/N CC670-34094-1S.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

SIDE SEAT TRACK STICK 2 RIGHT IS CORRODED. REMOVED AND REPLACED RIGHT 2 SIDE SEAT TRACK IAW CRJ 900 AMM 53-00-49 STEP 4A.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FORWARD OF SERVICE DOOR WEB CORRODED. REMOVED AND REPLACED FLOOR SILL AT FS 319.70 - FS 280 IAW CRJ 900 SRM 51-42-06. P/N SH670-32172-11.

Part: PANEL — CRACKED (RT PYLON) · airframe 11,615 hrs · 7,180 cycles

RIGHT PYLON UPPER AFT HINGE PANEL CRACKED AT THE AFT FASTENER. REPAIRED HINGE FAIRING PANEL IAW CRJ 900 SRM 51-40-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

RBL 12 BEAM CRACKED FWD OF FS 280.00 CROSSBEAM. REMOVED AND REPLACED RBL 12 DAMAGED SECTION IAW EO R53333.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

WHILE WORKING STRINGER 26R FS 319-333 CORROSION FOUND ON SPLICE ANGLE AT FS 333. REMOVED AND REPLACED STGR 26R SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06. P/N SH670-32429-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FS 319 FRAME HAS CORROSION BETWEEN S26L-S26R. REMOVED CORROSION FRAME 319. FRAME IS WITHIN LIMITS IAW CRJ 900 SRM 33-21-06 AND EP R53277.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 11,615 hrs · 7,180 cycles

THE FOLLOWING EMERGENCY LIGHTS STAY ON AFTER POWER CUT: LEFT FWD O/W EXTERNAL, RIGHT AFT O/W EXTERNAL, ALL FOUR OW EXIT INTERNAL, BOTH AFT O/W FLOOR EXIT INTERNAL AND AFT FACING CENTER CEILING. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY CHARGER IAW CRJ 900 AMM 33+51-17-400-802. OPS TEST OF EMERGENCY POWER SUPPLY UNIT 3 GOOD IAW CRJ 900 AMM 33-51-17-710-801. P/N 11-0049, S/N OFF 23351, S/N ON 23187.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FS 295 FRAME AFT SIDE HAS CORROSION BETWEEN STRINGERS 26L-25R. REMOVED CORROSION FROM FS 295 FRAME. PART IS WITHIN LIMITS IAW CRJ 900 SRM 53-21-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

SIDE SEAT TRACK STICK 7 RIGHT IS CORRODED. REPLACED RIGHT SIDE SEAT RAIL 7 IAW CRJ 900 AMM 53-00-49. P/N SH670-36260-5.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LBL 12 BEAM CRACKED FWD OF FS 280.00 BEAM. REMOVED AND REPLACED LBL 12 DAMAGED SECTION IAW EO R53333.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

STRINGER 26L HAS CORROSION BETWEEN FS 280-FS 295. REMOVED AND REPLACED STGR 26L FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06. SH670-31634-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

LEFT SIDE SEAT TRACK NR 7 CORRODED/GOUGED. REPLACED LEFT SIDE SEAT NR 7 TRACK IAW CRJ 900 AMM 53-00-49. P/N SH670-36230-5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

FS 349 FRAME HAS CORROSION ON AFT SIDE JUST LEFT OF S26R. REMOVED CORROSION FROM FRAME AT FS 349 PART IS WITHIN LIMITS IAW CRJ 900 SRM 53-21-106 AND EO R53277.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

SIDE SEAT TRACK STICK 5 RIGHT IS CORRODED. REPLACED RIGHT NR 5 SIDE SEAT TRACK IAW CRJ-900 AMM 53-00-49. P/N SH690-36284-1.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

RIGHT FS 280.0 BEAM CORROSION. REMOVED AND REPLACED RIGHT FS 280 BEAM IAW EO R53334. P/N CC670-34094-2S.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

STRINGER 26R BETWEEN FS 319.70-333 ATTACH RIVETS AND SURFACE EVIDENCE OF CORROSION. REMOVED AND REPLACED STGR 26R FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06. P/N SH670-31634-2.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 11,615 hrs · 7,180 cycles

E/E BAY RT/OB DIAPHRAGM BETWEEN FS 349-364 HAS CORROSION. REMOVED CORROSION FROM RIGHT O/B DIAPHRAGM PART IS WITHIN LIMITS IAW CRJ 900 SRM 55-21-23 AMD EO 53277.

Part: LIGHT — DAMAGED (CABIN) · airframe 11,291 hrs · 6,985 cycles

EMERGENCY EXIT LIGHTING STRIP BY ROW 13 IS DAMAGED. RE-SECURED EXIT MARKING STRIP AT ROW 13AB. CONDITION & SECURITY CHECKS GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 11,057 hrs · 6,848 cycles

THE 13 A/B FLOOR TRACK LOOSE. RE-INSTALLED FLOOR TRACK LIGHT IAW CRJ900 AMM 33-51-01.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 9,856 hrs · 6,077 cycles

AFTER WAITING 10 MINUTES PER MEL 26-14-1A, RETRACTED THE GEAR AND RECEIVED A GEAR DISAGREE WARNING. FOLLOWED THE EMC NON-NORM CHECKLIST AND RETURNED TO DEPARTURE. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,856 hrs · 6,077 cycles

EMERGENCY LIGHTS ON STATUS MESSAGE, OVERHEAD "EXIT" LIGHT ILLUMINATED OVER ROW 13. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROW 13 OPS TESTED IAW AMM 33-51-17 GOOD.

Part: ENGINE — CONTAMINATED

AFTER TAKEOFF, FLIGHT ATTENDANT SMELLED BURNING PLASTIC. PILOTS CONFIRMED AN ODOR. RETURN TO DEPARTURE. IDENTIFIED ODOR AS ENGINE WITH SOAP, RESIDUAL FROM ENGINE WASH ON RT ENGINE. RAN ENGINES TO 85 OIL TEMP WITH PACKS ON FULL HOT UNTIL ODOR DISSIPATED. AIRCRAFT OK FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 8,106 hrs · 5,062 cycles

FWD F/A NOTIFIED FLIGHT DECK ENROUTE, THAT THE EXIT COVER FOR THE EXIT SIGN ON THE FWD SERVICE DOOR (SMALL SIGN HALFWAY DOWN THE FRAME LT SIDE LOOKING AT DOOR) IS MISSING. INSTALLED NEW COVER FOR MISSING EXIT SIGN ON SERVICE DOOR, PN: BC5-0393-288. OK FOR SERVICE.

Part: LIGHT — DISLODGED (CABIN) · airframe 6,734 hrs · 4,185 cycles

PART OF THE FLOOR TRACK LIGHTING IN FWD GALLEY WAS DISLODGED BY CATERING. INSTALLED SERVICEABLE FLOOR TRACK IAW MM 33-51.

Part: LIGHT — UNSECURE (CABIN) · airframe 6,724 hrs · 4,179 cycles

EMERGENCY LIGHTING ON FLOOR FROM LAV NEEDS TO BE RESECURED. SECURED EMERGENCY LIGHTING FLOOR STRIP AS NEEDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 6,116 hrs · 3,812 cycles

"SMOKE" RIGHT AFTER T.O. THE FWD LAV WARNING MESSAGE CAME ON. STARTED GOING THROUGH THE NON NORMAL PROCEDURES PER THE POM AND THEN THE LIGHT WENT OUT. THERE WAS A STRONG UNNATURAL ODOR EMITTING FROM THE LAV PER FLT ATT. WHICH WE COULD ALSO SMELL IN COCKPIT. INSPECTED FWD GALLEY AND FWD LAV AREA FOR CAUSE OF SMOKE, NO DEFECTS NOTED. MDC SHOWS LAV FAN FAILED/WIRING, LOW FAN SPEED, B1 CODE 007306. DEFERRING FWD EXHAUST FAN GALLEY/LAVATORY PER MEL 21-23-1(C). C/W MX PROC. COLLARED CB CBP-2 B8.

Part: SKIN — CHAFED (BS 916 S27) · airframe 5,869 hrs · 3,673 cycles

SKIN CHAFED AT FS 916.00 STR 27 UNDER AFT BELLY FAIRING. REPAIRED SKIN DAMAGE AT ES 916, STR27 UNDER AFT BELLY FAIRING IAW MODSUM NR IS670538200021 AND REO 670-53-00-014.

Part: SKIN — DAMAGED (BS 916 S27) · airframe 5,869 hrs · 3,673 cycles

RIVET CHAFED AT ES 916.00, STR 27 UNDER AFT BELLY FAIRING. R & R DAMAGED RIVET AT ES 916, STR27 UNDER AFT BELLY FAIRING IAW MODSUM NR IS670538200021 AND REO 670-53-00-014.

Part: PANEL — CRACKED (PAX DOOR) · airframe 5,870 hrs · 3,673 cycles

PAX DOOR FWD TOP STEP SIDE PANEL ZONE 2 CRACKED. REPAIRED DISCREPANT SIDE PANEL IAW REO 670-52-11-104.

Part: PANEL — CRACKED (PAX DOOR) · airframe 5,870 hrs · 3,673 cycles

PAX DOOR, AFT TOP STEP AND MID STEP SIDE PANEL CRACKED AT ZONE 2 AND 3. CUT AWAY DAMAGE FROM PAX DOOR STEP AFT SIDE PANEL AT ZONES 2 AND 3 AND INSTALLED REPAIR ANGLES AND DOUBLER IAW REO 670-52-11-104.

Part: LIGHT — MISSING (CABIN) · airframe 5,373 hrs · 3,408 cycles

THE FLOOR EMERGENCY STRIP BY FWD GALLEY IS MISSING. REPLACED GALLEY FLOOR EMERGENCY BASE STRIP P/N PL88-900LH00.