N926XJ

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 36,507 hrs · 25,856 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED SERVICE DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15. OPS TEST PASS.P/N OFF/ON: 8GA411060-06

Part: ANGLE — CRACKED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR AFT WEB ANGLE IS CRACKED. COMPLETED REPAIR OF PAX DOOR AFT DRAG ANGLE IAW CRJ 900 SRM 52-11-04-201-002-A01

Part: ANGLE — CORRODED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR SUPPORT ANGLE AT DD7A FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR ANGLE AT DD7A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01

Part: RETAINER — CORRODED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR CLIP ON FWD SIDE OF SUPPORT ANGLE AT DD7A IS CORRODED LOCATED ,DRILLED AND INSTALLED NEW PAX DOOR CLIP P/N 601R318058-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: SKIN — CORRODED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR INNER SKIN IS CORRODED ON INNER SIDE AROUND NUTPLATES. ACCESSED THRU PANEL 832BL. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER SKIN AND INSTALLED NUT PLATES IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR INTERCOSTAL IS CORRODED IN UPPER RADIUS. LOCATED UNDER PANEL 832BR. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL P/N:601R31902-318 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: DOUBLER — CRACKED · airframe 33,861 hrs · 23,659 cycles

PAX DOOR FORWARD LATCH FITTING BACK-UP STRUCTURE IS CRACKED. ACCESSED THRU PANEL 832AL LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FWD LATCH FITTING BACK UP STRUCTURE IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: FLOORBEAM — CORRODED · airframe 33,861 hrs · 23,659 cycles

RH FLOOR BEAM AT FS 280 RBL 3 HAS HEAVY PITTING. REPLACED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.

Part: FLOORBEAM — CORRODED · airframe 33,861 hrs · 23,659 cycles

LH FLOOR BEAM AT FS 280 LBL 4 HAS HEAVY PITTING. INSTALLED LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01

Part: ANGLE — CORRODED · airframe 33,861 hrs · 23,659 cycles

FLOOR PANEL SUPPORT ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL9 CORRODED ACROSS ENTIRE LENGTH REMOVED AND REPLACED J ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: FLOOR SUPPORT — CORRODED · airframe 33,861 hrs · 23,659 cycles

FLOOR SUPPORT ANGLES AT LBL9 AND RBL9 AT FS278 HAVE MINOR CORROSION. INSTALLED NEW SERVICEABLE FLOOR SUPPORT ANGLES PNS: CC670-34191-1 AND CC670-34191-2 AT RBL 9 AND LBL9 FS 278 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 29,045 hrs · 19,582 cycles

LEFT SIDE AFT EMERGENCY LIGHT OUT WHILE DOING EXTERIOR LIGHT INSPECTION PER W/O 860880 (LINE CHECK). REMOVED AND REPLACED EMERGENCY EXTERIOR AFT LIGHT BULB (LEFTSIDE), IAW AMM 33-51-15. OPERATIONS CHECK GOOD, NO FURTHER DEFECT NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,969 hrs · 19,515 cycles

ROW 14 EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PS43 AT SEAT ROW 14, IAW CRJ 900 AMM 33-51-17. OPERATIONS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,672 hrs · 19,215 cycles

RIGHT REAR EMERGENCY LIGHT WIRE BROKEN. INSTALL NEW LIGHT ASSY, TESTED OK, REPLACED IAW AMM 33-51-15.

Part: COVER — DENTED (PAX DOOR) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: DENT ON COVER LOWER SIDE FWD/AFT CORNER AT PASSANGER DOOR.(PTAS)(SM) SUMMARY: COVER LOWER SIDE AFT CORNER AT PASSENGERS DOOR WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 PAR 6 AND 7, SRM 51-42-06-001-001-A01 PARAGRAPH 6 AND FWD LOWER COVER WAS ATTENDED WHIT NRC 00468

Part: ACCESS PANEL — WORN (WING) · airframe 27,548 hrs · 18,314 cycles

PARTS RACK: WEAR ON ACCESS PANELS 584GB, 595BB, 699AB, 699CB AND 699BB. (AI)(AD). WEAR ON ACCESS PANELS 584GB, 595BB, 699AB, 699CB AND 699BB WERE BLENDED OUT PER CRJ 900 SRM 51-12-00-001-001-A01 PAR. 5.B.2. ACCESS 699 BB, 699 CB, 584 GB, AND 599 BB WITH AN ORIGINAL THICKNESS OF 0.100 "AND A MINIMUM OF 0.093" THEREFORE THEY ARE WITHIN LIMITS PER.CRJ 900 SRM 57-51-01-101-A01 PER.4 TABLE 1. ACCESS 699AB WITH AN ORIGINAL THICKNESS OF 0.100 "REMAINING WITH A 0.050" REMANENT THEREFORE IT IS OUT OF LIMITS PER.CRJ 900 SRM 57-51-01-101-A01 PAR.4 TABLE 1, IT WAS REPLACED PER CRJ 900 SRM 51-40-11-001-001-A01.

Part: GROUND STUD — WORN · airframe 27,548 hrs · 18,314 cycles

AWR IN REF. EO R53582. WEAR ON LOW PRESSURE GROUND CONNECTION PLATE. (SM)(FUS). WEAR ON LOW PRESSURE GROUND CONNECTION PLATE WAS BLENDED OUT AND EVALUATED PER REO 670-53-61-1382 REV.A

Part: CANISTER — CRACKED (SLAT TRACK) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 INSIDE LH WING MAIN FUEL TANK WS 148. (SM)(AD). SUMMARY: SLAT TRACK CANISTER 1-3 INSIDE LH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV.-

Part: FLOORBEAM — CORRODED (BS 346) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

AWR; [ TASK R53520 STEP 7 ]: 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) CORROSION LEVEL 2. PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: SUPPORT — CORRODED (BS 322) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

AWR; [TASK R53520 STEP 7]: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS RELACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001-A01.

Part: SUPPORT — CORRODED (BS 346) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

AWR; [ TASK R53520 STEP 7 ]: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41 RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001-A01

Part: SUPPORT ANGLE — CORRODED (BS 329) · airframe 27,548 hrs · 18,314 cycles

AWR; [TASK R53520 STEP 7]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) CORROSION LEVEL 2. PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6C

Part: SUPPORT — CORRODED (BS 339) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

AWR; [TASK R53520 STEP 7]: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41 RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001-A01

Part: DOUBLER — CRACKED (TRAY) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CRACK ON DOUBLER OF COLLER TRAY OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT. (FUS). SUMMARY: DOUBLER OF COLLER TRAY OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 53-11-43-201-001-A01

Part: STRINGER SPLICE — CORRODED (BS 394-485) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION IN STGR 21RH AND SPLICE BTW FS=394.00 TO FS=485 (FUS)(TCI: 53-20-311). CORROSION LEVEL 2. STGR 21RH AND SPLICE BTW FS=394.00 TO FS=485 WERE REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01 ADDITIONAL PART: SH670-33252-1

Part: FLOOR SUPPORT — CORRODED (BS 1015-1051) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON FLOOR BEAM 27LBL IN STA. FS= 1015 TO FS= 1051 AT AFT BAGGAGE BAY. (CCT) (TC 100-15). SUMMARY: LEVEL CORROSION 2. FLOOR BEAM 27LBL IN STA. FS= 1015 TO FS= 1051 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ900 SRM 53-00-41-201-001-A03 FIGURE 53-00-41-995-816.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION IN INTERCOSTAL 20RH BTW FS=349.00 TO FS=364. (FUS)(TCI: 53-20-311). CORROSION LEVEL 2. INTERCOSTAL 20RH BTW FS=349.00 TO FS=364 WAS REPLACED PER CRJ900 SRM 51-42-20-001-001-A01 PAR 6.D AND CRJ900 SRM 51-42-13-001-001-A01 PAR 6.D.

Part: COAMING — WORN (CARGO DOOR) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: WEAR ON LOWER SEAL RETAINER AT AFT BAGGAGE BAY DOOR. (C2). LOWER SEAL RETAINER AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01 PAR. 6.D AND CRJ900 SRM 51-42-02-001-001-A01 PAR. 6.D AND UNDER NRC 00240.

Part: INTERCOSTAL — CORRODED (BS 333-349) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON INTERCOSTAL FS 333 TO FS 349 AND STGR 20RH AT FWD AVIONICS (E/E) (TCI: 100-06). CORROSION LEVEL 2. INTERCOSTAL FS 333 TO FS 349 AND STGR 20RH AT FWD AVIONICS WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01.

Part: BRACKET — CRACKED · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CRACK IN FWD/UPPER BRACKET CLIP TO ATTACH UPPER ACCUMULATOR IN METERING VALVE AREA AT FWD FUSELAGE. (FUS). FWD/UPPER BRACKET CLIP TO ATTACH UPPER ACCUMULATOR IN METERING VALVE AREA AT FWD FUSELAGE WERE REPLACED PER CRJ-900, SRM 51-42-21-001-001-A01 ADDITIONAL PART: CC670-75604-2

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE AT CROSSBEAM FS280 BTWN. RBL9 TO LBL9.(CPAX)(TCI :(53-10-219) CORROSION LEVEL 2. FLOOR PANEL SUPPORT ANGLE STA. FS=280 BETWEEN 9LBL/9RBL AT COCKPIT. WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6. C. AND CRJ900 SRM 51-42-20-001-001-A01 PAR. 6. C.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,548 hrs · 18,314 cycles

AWR; PER MTC REQUEST: DURING REMOVAL OF RH DRIP PAN,CRACK WAS FOUND ON CROSSBEAM FS280 BTWN. 11RBL AND 15 RBL.(CPAX) CROSSBEAM RBL WAS REPLACED PER CRJ-900, SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON SILL AT THE AFT BAGGAGE-BAY DOOR BTW FS.1000 TO FS.1047 (SM) CORROSION LEVEL 2. SILL AT THE AFT BAGGAGE-BAY DOOR BTW FS.1000 TO FS.1047 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR 6A, CRJ900 SRM 51-42-13-001-001-A01 PAR 6A AND CRJ900 SRM 51-42-20-001-001-A01 PAR 6A

Part: COAMING — WORN (CARGO DOOR) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: WEAR (3EAS) ON EDGE FRAME OF THE AFT BAGGAGE BAY DOOR CUTOUT (SM) EDGE FRAME (COAMING) OF THE AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 51-42-10-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

AWR HIDDEN DAMAGE CORROSION ON FLANGE AT CROSSBEAM FS280, BTWN 0.0 AND 09 LBL.(CPAX) CORROSION LEVEL 2. CROSSBEAM LH ON STA FS=280 WAS REPLACED PER CRJ-900,SRM 51-42-21-001-001-A01.PAR. 6. C. AND CRJ900 SRM 51-42-06-001-001-A01 PAR. 6. C.

Part: SUPPORT — CRACKED (FAIRING) · airframe 27,548 hrs · 18,314 cycles

PART RACKS: CRACK ON FWD SUPPORT ON FAIRING PANEL 196DR AT CENTER FUSELAGE.(FUS). FWD SUPPORT ON FAIRING PANEL 196DR AT CENTER FUSELAGE WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01

Part: SEAT TRACK — CORRODED (BS 693-977) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [FS= 693 TO FS= 830,9LBL/ 9RBL] [FS= 830 TO FS= 849, 9RBL] [FS= 849 TO 977, 9LBL/ 9RBL] AT PAX CABIN. (CPAX) (TCI: 53-20-233) SUMMARY:CORROSION LEVEL 2, ON FLOOR SEAT RAILS IN SECTIONS [FS= 693 TO FS= 830,9LBL/ 9RBL] [FS= 830 TO FS= 849, 9RBL] [FS= 849 TO 977, 9LBL/ 9RBL] AT PAX CABIN. THEY WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801-A07 THEY WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801-A07.

Part: SEAT TRACK — CORRODED (BS 785-847) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [FS=785 TO FS= 847+16, STGR 15LH] AT PAX CABIN. (CPAX) TCI: 53-20-233 SUMMARY:CORROSION LEVEL 2, ON SIDE SEAT RAILS IN SECTIONS [FS=785 TO FS= 847+16, STGR 15LH] AT PAX CABIN, THEY WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801-A07.

Part: RETAINER — BENT (CARGO DOOR) · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION. BENT PLATE LOWER PRESSURE SEAL RETAINER AFT CORNER AT FWD BAGGAGE BAY DOOR, ALSO BENT PLATE LOWER PRESSURE RETAINER AT CENTRAL BAGGAGE BAY DOOR (C1). PLATE LOWER PRESSURE SEAL RETAINER AFT CORNERS AT FWD BAGGAGE BAY DOOR WAS REPAIRED PER SRM 52-35-07-201-001-A01 FIG. 52-35-07-995-803 AND FIG. 52-35-07-995-804 AND PLATE LOWER PRESSURE SEAL RETAINER AT CENTER BAGGAGE BAY DOOR WAS REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6C.

Part: SEAT TRACK — CORRODED (BS 661-720) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [FS= 661+16 TO FS= 661+90, STGR 15LH] [FS= 661+90 TO FS= 720.85, STGR 15LH] AT PAX CABIN. (CPAX) (TCI: 53-20-217) SUMMARY: CORROSION LEVEL 2, ON SIDE SEAT RAILS IN SECTIONS [FS= 661+16 TO FS= 661+90, STGR 15LH] [FS= 661+90 TO FS= 720.85, STGR 15LH] AT PAX CABIN.THEY WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 ( CONFIG. A07 )

Part: SEAT TRACK — CORRODED (BS 485-693) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [FS= 485 TO FS= 581,9RBL] [FS= 581 TO 661+32, 9LBL/9RBL] [FS= 661+32 TO FS= 693, 9LBL] AT PAX CABIN. (CPAX) (TCI: 53-20-243) SUMMARY: CORROSION LEVEL 2, ON FLOOR SEAT RAILS IN SECTIONS [FS= 485 TO FS= 581,9RBL] [FS= 581 TO 661+32, 9LBL/9RBL] [FS= 661+32 TO FS= 693, 9LBL] AT PAX CABIN.THEY WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG. A07)

Part: ANGLE — CORRODED (BS 386.5) · corrosion level 2 · airframe 27,548 hrs · 18,314 cycles

INITIAL INSPECTION: CORROSION ON IMPACT ANGLE FS386.5 AND STGR 23R. FWD WASTE LAVATORY SERVICE PANEL (142BR). (FUS)(TCI:100-16) CORROSION LEVEL 2. IMPACT ANGLE BETWEEN FS386.5 AND STGR23R ON FWD WASTE LAVATORY SERVICE PANEL (142BR) WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6C

Part: LIGHT — MISSING (MAIN CABIN) · airframe 24,363 hrs · 15,927 cycles

EMERGENCY LIGHT STRIP AT THE LEFT REAR EMERGENCY EXIT WAS MISSING. REPLACED THE EMERGENCY LIGHT TRACK IAW AMM 33-51-01.

Part: SEAL — BROKEN (FWD PBE) · airframe 23,339 hrs · 15,210 cycles

FORWARD FA PBE BROKEN. RESEALED THE FWD PBE IAW AMM 25-60-00. OK FOR SERVICE

Part: AED — INOPERATIVE (MAIN CABIN) · airframe 23,160 hrs · 15,077 cycles

AED LIGHT NOT WORKING. R & R AED IAW AMM 25-61-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PBE — DAMAGED (MAIN CABIN) · airframe 23,073 hrs · 15,016 cycles

WARDROBE PBE LOST VACUUM REMOVED AND REPLACED WARDROBE PBE PN MR-10042N IAW CRJ900 AMM 35-31-06

Part: PBE — DAMAGED (MAIN CABIN) · airframe 23,073 hrs · 15,016 cycles

AFT CABIN PBE LOST ITS VACUUM REMOVED AND REPLACED AFT CABIN PBE PN OFF MR-10042N PN ON MR-10047N IAW CRJ900 35-31-06

Part: PBE — DAMAGED (MAIN CABIN) · airframe 23,073 hrs · 15,016 cycles

FWD ENTRANCE PBE LOST ITS VACUUM REMOVED AND REPLACED FWD ENTRANCE PBE PN MR-10042N IAW CRJ900 AMM 35-3 1-06

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,416 hrs · 14,548 cycles

FA REPORTED EMERGENCY LIGHTS GO OUT AFTER TEST. FOUND BATTERIES TO BE DEPLETED. SET TO CHARGE AND OPERATIONAL TEST WAS GOOD IAW AMM 25-62-00. NO FURTHER MX IS NECESSARY.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 22,374 hrs · 14,511 cycles

FOWARD FLGHT ATTENDENT EMERGENCY FLASHLIGHT SEAL BROKE. REMOVED AND REPLACED THE FWD FA EMERGENCY FLASHLIGHT LIGHT SEAL IAW AMM 25-61-02. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: SEAL — LOOSE (FLASHLIGHT) · airframe 22,159 hrs · 14,354 cycles

F/O FLIGHT DECK FLASHLIGHT SEAL IS LOOSE. REMOVED & REPLACED THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,919 hrs · 14,192 cycles

LT AND RT EXTERIOR AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-17, OPS NORMAL.

Part: STRINGER — CORRODED (BS 333-349) · airframe 21,892 hrs · 14,173 cycles

STRINGER 23R CORRODED, BS 333 TO 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 21,892 hrs · 14,173 cycles

MAIN AVIONICS DOOR HANDLE FITTING IS CRACKED AT THE BASE OF THE HANDLE. REMOVED AND REPLACED THE MAIN AVIONICS DOOR HANDLE HOUSING IAW SRM 51-42-21, AND ATTACHED THE HANDLE HOUSING MECHANISM IAW AMM 52-42-03. OPS CHECKED GOOD IAW AMM 52-42-00-710-801. "

Part: STRINGER — CORRODED (BS 364-379) · airframe 21,892 hrs · 14,173 cycles

STRINGER 21R CORRODED, BS 364 TO 379. REPAIRED THE STRINGER IAW EA CRJ953-05682, REV IR. LEAK TEST OF THE EXHAUST DUCT GOOD IAW AMM 21-23-00-790-802.

Part: CARGO TRACK — CORRODED (BS 565) · airframe 21,892 hrs · 14,173 cycles

FWD CARGO BAY BS 565, LBL 3 CARGO RING SUPPORT IS CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-42-06, 51-42-21, AND 51-42-24.

Part: FITTING — FAILED (NOSE JACK) · airframe 21,892 hrs · 14,173 cycles

WHILE PERFORMING A PERMANENT REPAIR OF NOSE JACK POINT HELICOIL FAILED NDT INSPECTION BEFORE RETAPPING THE FITTING. REMOVED AND REPLACED NOSE JACK FITTING WITH NEW IAW SRM 51-42-21.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,892 hrs · 14,173 cycles

RIGHT OVERWING, FWD EMERGENCY LIGHT WIRES BROKEN. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-15. OPS TESTED GOOD IAW AMM 33-51-15-710-801.

Part: CARGO TRACK — CORRODED (BS 565) · airframe 21,892 hrs · 14,173 cycles

FWD CARGO BAY BS 565, STRINGER 23L CARGO TRACK RING SUPPORT IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-21, AND 51-42-24.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 21,892 hrs · 14,173 cycles

LEFT WING INBD FLAP LOWER SURFACE IS DENTED 14 INCHES FROM THE INBD EDGE. REPAIRED IAW EA 957-05700, REV IR.

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 21,892 hrs · 14,173 cycles

MAIN AVIONICS DOOR AFT SURROUND, LEFT LATCH PIN INTERCOSTAL ATTACH FLANGE CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: CHANNEL — CORRODED (BS 295-310) · airframe 21,892 hrs · 14,173 cycles

TCAS ANTENNA INTERNAL CHANNEL CORRODED, BS 295 TO 310. REMOVED AND REPLACED THE TCAS ANTERNAL CHANNEL IAW SRM 51-42-06, AND SRM 51-42-21.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 21,892 hrs · 14,173 cycles

STRINGER SPLICE 25R AT BS 333 CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06.

Part: STRINGER — CORRODED (BS 295-333) · airframe 21,892 hrs · 14,173 cycles

STRINGER 23R CORRODED, BS 295 TO 333. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06.

Part: STRINGER — CORRODED (BS 295-310) · airframe 21,892 hrs · 14,173 cycles

STRINGER 24R CORRODED, BS 295 TO 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06.

Part: RISER — CRACKED (L1 DOOR) · airframe 21,892 hrs · 14,173 cycles

L1 DOOR FWD RISER CRACKED IN CORNER THIRD STEP FROM THE TOP. REPAIRED THE FWD RISER WEB IAW REO 670-52-11-104.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,892 hrs · 14,173 cycles

LEFT BS 280 FLOORBEAM HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13, & 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,892 hrs · 14,173 cycles

MAIN CABIN FLOORBEAM IS CORRODED BS 280, LBL 9 - RBL 9. REMOVED AND REPLACED IAW SRM 51-42-06, AND 51-42-21.

Part: COVER — CRACKED (WIRE HARNESS) · airframe 21,892 hrs · 14,173 cycles

MID CARGO DOOR FWD HINGE WIRE HARNESS PROTECTOR IS CRACKED. REMOVED AND REPLACED THE WIRE HARNESS PROTECTOR IAW SRM 51-41-02.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,894 hrs · 13,501 cycles

RT SIDE FWD EMERGENCY LIGHT LENS IS CRACKED JUST AFT OF SERVICE DOOR. REMOVED AND REPLACED THE LENS IAW AMM 33-51-15.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,894 hrs · 13,501 cycles

EMERGENCY LIGHT LOCATED AT SEAT 15CD IS CRACKED. REMOVED AND REPLACED THE CAP IAW A MM 33-51-01

Part: LIGHT — UNSECURE (CABIN) · airframe 19,724 hrs · 12,670 cycles

EMERGENCY ILLUMINATION ON FLOOR AT EXIT ROW 13 CABIN DOOR NOT SECURED TO FLOOR. SECURED EMER ILLUMINATION STRIP ON FLOOR AT EXIT 13 CABIN DOOR IAW AMM 33-51-01, NO FURTHER DETAILS NOTED AT THIS TIME.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 19,538 hrs · 12,551 cycles

THE FOLLOWING EMER LIGHTS ARE INOPERATIVE DS177, DS439, DS441, DS443, DS98, DS174, DS100, DS175, DS93, DS55, DS94, DS102, DS56 IAW AMM 33-51-00-710-802-A16 & 33-51-15-400-801-A08 FOR LOCATION OF DS NUMBERS. TROUBLE SHOT EMER LIGHTS SYS, DISCOVERED BATTERY PACK NR 5 CONNECTOR NOT FULLY SEATED ON JACK. INSTALLED CONNECTOR ALL THE WAY ON & PERFORMED OPERATIONAL CHECK OF EMER LIGHTS IAW AMM 33-51-00-710-802-A16. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 19,538 hrs · 12,551 cycles

ROUTINE CHECK, INTERIOR OVERHEAD EMER EXIT LIGHTS AT OVERWING EXITS ARE INOPERATIVE AS WELL AS THE RT FLOOR LEVEL LIGHTS ARE INOPERATIVE. TROUBLE SHOT EMER LIGHTS, DISCOVERED BATTERY PACK NR 5 DISCONNECT CONNECTOR NOT FULLY INSTALLED TO JACK SIDE. CONNECTED ALL THE WAY & PERFORMED OPERATIONAL CHECK OF EMER LIGHTS IAW AMM 33-51-00-710-802-A16. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

FRAME SECTOR AT FS 310 IS CORRODED, BETWEEN STRINGER 26R TO 26L. REPAIRED CORROSION IAW REO 670-53-21-799 & SRM 51-42-21-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT FLOOR SILL BETWEEN FS 280 & 319 IS CORRODED. CONTINUATION CARD 81518411 OP 99. R & R RT FLOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

PASSENGER DOOR FLOOR SILL & SILL ANGLE HAS AREAS OF CORROSION, BETWEEN FS 310 - 349. CONTINUATION CARD 81518411 OP 104. R & R PAX DOOR FLOOR SILL & ANGLE, PN SH670-31825-9S & SH670-31875-7S, IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 19,538 hrs · 12,551 cycles

CUSTOMER REQUEST INBOUND 3 PAX DOOR HAS A CRACK ON AFT SIDE BEHIND GAS SHOCK BEAM. CONTINUATION CARD 81518416 OP 36. R & R ANGLE PN 601R317745-7 & FABRICATED REPAIR DOUBLER IAW REO 670-52-11-104 REV F. REMOVED & INSTALLED TO AFT SIDE OF PAX DOOR IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK AT LBL 9, FS 379 IS CORRODED. PERFORMED CUT OUT OF CORRODED SEAT TRACK AT FS 379, LBL 9.0. REMOVED & INSTALLED NEW SECTION OF TRACK. WORK PERFORMED IAW REO 670-53-00-074 REV A DATED 2009 03 05, REO 670-53-00-343 REV M DATED 2015 10 19, SRM TASKS 53-00-49-000-801 CONFIG A07 & 53-00-49-400-801 CONF A07.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

FRAME SECTOR AT FS 295 IS CORRODED, BETWEEN STRINGER 26R - 26L. REPAIRED FRAME SECTOR CORROSION IAW REO 670-53-21-799 REV. THIS IS A MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

FRAME SECTOR AT FS 645 IS CORRODED, BELOW LT FLOOR SILL. CONTINUATION CARD 81518411 OPS 97 & 106. FRAME SECTOR WAS REPAIRED IAW SRM 53-00-06-201-001-A03, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

FS 280 IS CORRODED, FWD J ANGLE, LT BULKHEAD WEB, RT BULKHEAD, LT CROSSBEAM & RT CROSSBEAM. TRANSFERRED FROM CO 15184116 JOB 81518411. OPERATIONS 33 - 35. CONTINUATION CARD 81518411 OP 91. LT & RT FS 280 BULKHEAD WEBS REPAIRED IAW GREO 670-53-11-594. R & R LT & RT CROSSBEAMS & FWD J ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

COCKPIT FLOORBEAM AT LBL 12, JUST FWD OF FS 280.00 IS CRACKED. REPAIRED COCKPIT FLOORBEAM IAW EO R5 3263.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

TWO EACH INTERCOSTALS, BETWEEN FS 364 - 349 ARE CORRODED AT STRINGERS 27 & 26R. CONTINUATION CARD 81518411 OP 100. R & R TWO EACH INTERCOSTALS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-21-06-001-001-A01, 53-21-23-001-003-A02 & 51-42-21-001-001-A01. OPERATIONAL TEST IS GOOD AT THIS TIME.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

COCKPIT FLOORBEAM AT RBL 12, JUST FWD OF FS 280 IS CRACKED. REPAIRED COCKPIT FLOORBEAM IAW EO R5 3263.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SERVICE DOOR FLOOR SILL IS CORRODED, BETWEEN FS 319 - 349. CORROSION ON SERVICE DOOR FLOOR SILL MOUNT ANGLE WAS REPAIRED BY R & R ANGLE PN SH670-31982-1 IAW SRM 51-42-21-001-0 01-A01 & SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LATCH PIN INTERCOSTAL AT FS 364, STRINGER 27L IS CORRODED AROUND FASTENER ON ATTACHING FLANGE. NO DAMAGE ALLOWED IN AREA IAW SRM 53-21-23-101-003-A02. REPLACED LATCH PIN INTERCOSTAL PN SH670-32075-3 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

AFT CARGO DOOR FLOOR SILL IS CORRODED, BETWEEN FS 100 - 1047 & HAS TWO EACH CHAFES. ONE IS APPROX 4""L X .5""W X .010""D & THE OTHER CHAFE IS 8""L X .25""W X .005""D. AFT CARGO DOOR SILL, PN MM670-35655-003 WAS REPLACED IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 19,538 hrs · 12,551 cycles

LEFT VERTICAL STABILIZER FWD DRAG ANGLE IS CRACKED AT AFT END OF DRAG ANGLE. CRACK MEASURES APPROX 1.25"" LONG. AFT END OF FWD LT VERTICAL DRAG ANGLE WAS REPAIRED IAW GREO 690-55-31-004.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT FLOOR SILL IS CORRODED, BETWEEN FS 349 - 364. REPAIRED FLOOR SILL AT FS 349 - 364 IAW EO 953-04334 REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 5 AT STRINGER 15 HAS CORROSION, BETWEEN FS 677 - 720.85. LOCATED, DRILLED & INSTALLED NEW LT SIDE SEAT RAIL, PN SH690-36284-1, IAW AMM 53-00-49-400-801 A07 & REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 6 AT STRINGER 15 HAS CORROSION, BETWEEN FS 744 - 761. RT SIDE SEAT TRACK WAS REMOVED, FABRICATED & REPLACED IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 3 AT STRINGER 15, HAS CORROSION BETWEEN FS 565 - 661+16. LT SIDE SEAT RAIL WAS R & R WITH FABRICATED TRACK PN N126-2075 IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK AT STRINGER 15 HAS CORROSION, BETWEEN FS 379.00 - 477.40 - 2"". FABRICATED, LOCATED & INSTALLED NEW SEAT TRACK, PN SH690-32233-3 IAW REO 670-53-00-343, SRM 51-40-11-001-001-A01 & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 4 AT STRINGER 15 HAS CORROSION, BETWEEN FS 661+16 - 677. LOCATED, DRILLED & INSTALLED NEW LT SIDE SEAT TRACK SEGMENT, PN SH690-36283-1 IAW AMM 53-00-49-400-801A07 & REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 8 AT STRINGER 15 HAS CORROSION, BETWEEN FS 847+16 - 865. RT SIDE SEAT TRACK SEGMENT PN SH690-36286-3 WAS FABRICATED, R & R IAW REO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK NR 8 AT STRINGER 15 HAS CORROSION BETWEEN FS 847+16 TO FS 847+32. FABRICATED, LOCATED & INSTALLED NEW TRACK IAW REO 670-53-00-343, SRM 51-40-11-001-001-A01 & AMM 53-00-49-400-801-A07, PN SH690-36286-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK IS CORRODED AT LBL 9 & FS 379. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A11. LOCATED & DRILLED NEW TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 4 & SPLICED TRACK SEGMENT AT STRINGER 15 BETWEEN FS 661+16 TO 677 HAS AREAS OF CORROSION. RT SIDE SEAT TRACK PN SH690-36283-1 WAS FABRICATED. R & R IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK SEGMENT AT LBL 27 HAS CORROSION, BETWEEN FS 485 - 565. SEAT TRACK SEGMENT WAS REPLACED WITH FABRICATED SEGMENT IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 5 AT STRINGER 15 HAS CORROSION, BETWEEN FS 677 - 720.85. RT SIDE SEAT TRACK WAS R & R WITH FABRICATED TRACK PN SH690-36284-1 IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 7 AT STRINGER 15 HAS CORROSION, BETWEEN FS 785 - 847+16. REMOVE SEAT TRACK IAW AMM 53-00-49-000-801-A11. TRACK FABRICATED IAW REO 670-53-00-343. TRACK INSTALLED IAW AMM 53-00-49-400-801-A11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK SEGMENTS ONE EACH AT RBL 9 & LBL 9, BETWEEN FS 581 - 661+32, HAVE MULTIPLE AREAS OF CORROSION. SEAT TRACK WAS FABRICATED, R & R IAW REO 670-53-00-343 & AMM 53-31-49-101-001-A02 & 53-00-49-000 400-801-A07.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 19,538 hrs · 12,551 cycles

CUSTOMER REQUEST, INBD 3 PAX DOOR AFT WEB STIFFENER IS CRACKED, REQUIRES REPLACEMENT. PAX DOOR AFT STIFFENER WAS R & R IAW SRM 51-42-06-001-001-A01 & 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK IS CORRODED AT RBL 9 AT FS 359 - 379. LOCATED, DRILLED & INSTALLED NEW SEAT TRACK, PN SH670-32159-1, IAW SRM 51-40-11-001-001-A01 & REO 670-53-00-343 & AMM 53-00-49-400-801A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 3 AT STRINGER 15 HAS CORROSION, BETWEEN FS 565 - 661+16. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK SEGMENT, PN SH690-36282-1, IAW GREO 670-53-00-343. INSTALLED NEW SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,538 hrs · 12,551 cycles

SEAT TRACK SEGMENTS ONE EACH AT RBL 9 & LBL 9, BETWEEN FS 661+32 - 693 HAS MULTIPLE AREAS OF CORROSION. INSTALLED SEAT TRACKS IAW AMM 53-00-49-400-801-A07. FABRICATED SERVICEABLE SEAT TRACKS IAW REO 670-53-00-343.

Part: LENS — DETACHED (CABIN) · airframe 19,446 hrs · 12,482 cycles

EMERGENCY EXIT AISLE LIGHTING LENS ASSEMBLY DETACHED. R & R EMER EXIT AISLE ACCENT LENS IAW AMM 33-21-12.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 19,191 hrs · 12,315 cycles

EMERGENCY GLOW STRIP CAME UNDONE, GALLEY. SECURED EMER GLOW STRIP IAW REQUIRED. REFER TO LOG PAGE 3292345 FOR LAST FLIGHT.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,129 hrs · 12,280 cycles

CAPTAINS SIDE EMER FLASHLIGHT INOPERATIVE. R & R EMER LIGHT, CAPTAIN SIDE, IAW AMM 25-61-02. PERFORMED OPERATIONS CHECK IAW AMM 25-61-00. OPERATIONS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: STRUT — DEFECTIVE (NLG) · airframe 18,875 hrs · 12,122 cycles

AFTER TAKEOFF UPON GEAR UP SELECTION FELT VIBRATION IN NOSE WHEEL AREA, FOLLOWED BY STEERING INOPERATIVE. IMMEDIATELY AFTER LIFTOFF THEN GEAR DISAGREE WARNING, NOSE GEAR SHOWING YELLOW HASH MARKS. FOLLOWED GUIDANCE NON NORMAL CHPT 7 CHECKLIST. RETURNED, NORMAL LANDING WHEN GEAR WAS SELECTED DOWN, NOSE GEAR LOCKED IN POSITION NORMALLY. OK TO DEFER LG RETRACTION & EXTENSION SYS IAW MEL 32-30-1 IAW MOC 96247. PROCEDURES COMPLIED WITH, PLACARD INSTALLED & MM02 UPDATED. MEL 32-30-1 LG RETRACTION & EXTENSION SA 97287 REF LOG PAGE 3253663 ITEM 2 FOR STRUT REPACK, NLG. PERFORMED FUNCTIONAL RETRACTION OF LG IAW AMM 32-30-0 0-865-801. OPERATIONS CHECKED GOOD.

Part: TRIM PANEL — UNSECURE (CABIN) · airframe 18,752 hrs · 12,035 cycles

FLIGHT ATTENDANT REPORTS REFLECTIVE STRIP BY GALLEY SERVICE DOOR IS COMING OFF. SECURED SERVICE DOOR LOWER AFT SIDEWALL TRIM PANEL IAW AMM 25-26-07. ACFT OK FOR CONTINUED SERVICE.

Part: STOWAGE BOX — LEAKING (CREW O2) · airframe 18,227 hrs · 11,660 cycles

OBSERVER OXYGEN MASK HAS STEADY LEAK FROM PRESS TO TEST BUTTON. DEFERRING OBSERVER'S OXYGEN SYS IAW MEL 35-10-1. MXC NOTIFIED 96045, MMO2 UPDATED & PLACARD PLACED CAT A. R & R OBSERVER OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15. OPERATIONS CHECKED GOOD. CLEARED FROM MM02. PLACARD REMOVED MOC 96427 NOTIFIED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,186 hrs · 11,631 cycles

BULB OUT ON LOWER EMER LIGHT BELOW THE FLASHLIGHT IN MAIN DOOR ENTRY WAY. ENTERED ON TO MMO2, DEFERRED PAX DOOR EMER FLOOD LIGHT IAW MEL 33-51-1C C. MX NOTIFIED 4488 & PLACARD INSTALLED. RELAMPED PN 6100928 IAW 33-51-11. OPERATIONS CHECKED GOOD, CLEARED MEL & MX NOTIFIED 96112.

Part: LIGHT — MISSING (CABIN) · airframe 17,877 hrs · 11,406 cycles

ON THE LT SIDE OF THE GALLEY FLOOR, THE FLOOR TRACK LIGHTING STRIP IS MISSING. INSTALLED SERVICEABLE FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01. ACFT OK FOR SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 16,884 hrs · 10,673 cycles

RIGHT AFT EMER EXIT LIGHT WIRE BROKEN. REPAIRED WIRE GS844 IAW ESPM 20-16-05. PERFORMED OPERATIONS CHECK OF EXTERNAL EMER LIGHTS IAW AMM 33-51-15. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 16,160 hrs · 10,172 cycles

ON TAKEOFF RED GEAR DISAGREE, NOSE WHEEL & GEAR INDICATOR STAYED RED WHEN GEAR HANDLE WAS SELECTED UP. DEFERRED LG RETRACTION SYS IAW MEL 32-30-1. PLACARD INSTALLED. MXC 4632 NOTIFIED & MM02 UPDATED. CAT II DOWNGRADE REQUIRED TORQUE NLG AFT DOOR DRIVE BRACKET HARDWARE IAW JOB CARD 900-32-710-900. ALSO ADJUSTED PROX SENSOR PX11 IAW AMM 32-61-05-820-805. DM CLEARED, MM02 UPDATED & PLACARD REMOVED. MXC NOTIFIED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,963 hrs · 10,032 cycles

RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. ALLOWED ALL BATTERY PACKS TO CHARGE. PERFORMED OPERATIONS CHECK ON EMER LIGHTS IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,544 hrs · 9,757 cycles

EMERGENCY LIGHTS DO NOT WORK WHEN TURNED ON FOR TESTING, THEY FLICKER FOR A SECOND THEN GO OUT & STAY OUT. R & R NR 1 EMER BATTERY PACK IAW AMM 33-51-17. ALL CHECKED GOOD ACFT RETURNED TO SERVICE.

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 15,007 hrs · 9,386 cycles

ELONGATED SCREW HOLE OTBD BRACKET SECURING THE WIRE BUNDLES COMING OFF THE RT SIDE STAY. R & R BRACKET SECURING WIRE BUNDLES ON RT STAY IAW SRM 51-41-03-001-001-A01, 51-42-06-001-001-A01, STEPS 11 & 9 51-42-21-001-001-A01 STEP 10 & 8.

Part: AILERON — DAMAGED (LT WING) · airframe 15,007 hrs · 9,386 cycles

WHILE PAINTING LT AILERON FOUND COMPOSITE DAMAGE TO TE UPPER SIDE AT OTBD END. REPAIRED LT WING AILERON TE IAW REO 690-57-61-103 & THE FOLLOWING SRMS 51-25-01-001-001-A01 51-42-19-001-001-A01, 51-24-26-001-001-A01 & 51-20-008-230-A01.

Part: PANEL — CHAFED (TE FLAP) · airframe 15,007 hrs · 9,386 cycles

LEFT WING INBD FLAP PANEL 584ET IS MISSING PAINT & HAS CHAFING MARKS. DRILLED NEW VANE ACCESS PANEL IAW SRM 51-40-11-001-001-A01 & PAINTED PANEL IAW 51-25-01-001-001-A01.

Part: FIRESHIELD — BENT (RT NACELLE) · airframe 15,007 hrs · 9,386 cycles

TASK CARD 900-54-440-301 RT ENG LOWER NACELLE HAS A BEND IN THE INSIDE METAL. REPAIRED FIRE SHIELD IAW EA CRJ954-0298 STEPS 1 THRU 7.

Part: FIRESHIELD — DAMAGED (RT NACELLE) · airframe 15,007 hrs · 9,386 cycles

TASK CARD 900-54-440-301 RT ENG LOWER NACELLE HAS A HOLE IN THE INSIDE METAL. REPAIRED LWR NACELLE RT ENG FIRE SHIELD IAW EA CJ954-02511.

Part: GLOWSTRIP — DETERIORATED (PAX DOOR) · airframe 15,007 hrs · 9,386 cycles

PAX DOOR 4TH STEP AFT EMERGENCY GLOW STRIP REQUIRES REPLACEMENT DUE TO DETERIORATION, PN S7251B575. R & R GLOW STRIP ON PAX DOOR IAW AMM 20-60-04-000-801-A01 & 20-60-04-400-801-A01.

Part: FAN — FAULTY (DISPLAY) · airframe 14,624 hrs · 9,151 cycles

DISPLAY COOL CAUTION ILLUMINATED DURING FLIGHT WITH OTHER DISPLAY FAN ALREADY DEFERRED RESULTING IN A LOSS OF ALL DISPLAY COOLING. BOTH PILOTS NOTICED BURNING SMELL IN THE COCKPIT. COMPLIED WITH NON-NORMAL CHECKLIST. R & R COCKPIT DISPLAY FAN NR 2 IAW AMM 21-24-12, OPERATIONS TESTED GOOD.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 14,015 hrs · 8,745 cycles

FLOOR LIGHT STRIP LOOSE AT 1CD. INSTALLED NEW FLOOR LIGHT STRIP COVER IAW REF 33-51-01. CHECKS GOOD FOR SECURITY.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

RIGHT FLOOR SILL IS CORRODED IN NUMEROUS AREAS FROM FS 280 TO FS 319. REPAIRED RIGHT FLOOR SILL AT FS 280 IAW REO 690-53-21-420 & 670-53-21-139 & EO R53275.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

FRAME IS CORRODED AT FS 310, BETWEEN 27 &26R. REPAIRED FRAME 310 BETWEEN STRINGERS 27 AND 26R IAW EO R53272.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

FRAME 349 HAS CORROSION BETWEEN STRINGER 26R AND 25R, IN THE FWD E & E BAY. REPAIRED FRAME 349 BETWEEN STRINGERS 26R AND 25R IAW EO R53272.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

SKIN SPLICE AT FS 280 IS CORRODED BETWEEN STRINGERS 26R & 26L. REMOVED CORROSION AT FS 280.00 BUTT STRAP BETWEEN STRINGER 26R AND STRINGER 26L IAW CRJ 900 EO R53272 PAGE 5.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 25L IS CORRODED BETWEEN FS 333 & FS 319. REMOVED AND REPLACED SPLICE AT STRINGER FS 333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

RIGHT 280 BEAM CORRODED. REMOVED AND REPLACED RIGHT 280 BEAM IAW CRJ 900 SRM 51-42-06 AND 51-41-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

LEFT 280 BEAM CORRODED. REMOVED AND REPLACED RIGHT 280 BEAM IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 25R IS CORRODED AROUND FASTENERS AT FS 333. REMOVED AND REPLACED STRINGER 25R SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 26R IS CORRODED BETWEEN FS 333 & FS 349. REMOVED AND REPLACED STRINGER 26R BETWEEN FS 333 AND FS 364 IAW CRJ 900 SRM 51-42-06.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

SERVICE DOOR THRESHOLD CORRODED. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06 ON SERVICE DOOR THRESHOLD EO R53272.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,894 hrs · 7,427 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR ASSIST CABLE PULLEY BRACKET. REPAIRED CRACKED DRAG ANGLE IAW CRJ 900 SRM 52-11-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

UNDER ADG JACK PAD SKIN CRACKED. CUT AWAY DAMAGE, FAB NEW CLEAT & DOUBLER & INSTALLED CLEAT & DOUBLER AT FS 193 UNDER ADG PUMP IAW REO 670-53-11-509.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

SERVICE DOOR FLOOR ANGLE CORRODED. REMOVED AND INSTALLED NEW ANGLE IAW CRJ 900 SRM 51-42-06 AND 51-40-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

PAX DOOR THRESHOLD CORRODED. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06, PAX DOOR THRESHOLD.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

ATTACHMENT ANGLE, 2" LEFT OF STRINGER 27, IS CORRODED FROM FS 360 TO FS 364. REMOVED AND REPLACED ATTACHMENT ANGLE (LEFT I/B INTERCOSTAL) IAW CRJ 900 SRM 51-42-06. AAR SM-74.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 26R HAS CORROSION AROUND FASTENERS BETWEEN FS 295 & FS 310. REMOVED AND REPLACED STGR 26R FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-41-06. P/N SH670-31634-2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 26L IS CORRODED FROM FS 349 TO FS 340. REMOVED & REPLACED STGR FROM FS 333 TO FS 364 IAW CRJ 900 SRM 51-42-06.

Part: PANEL — CHAFED (WING) · airframe 11,894 hrs · 7,427 cycles

RS-2-20 (PANEL RACK) PANEL 584GB IS CHAFED. REMOVED & REPLACED PANEL 584GB IAW CRJ-900 SRSM 51-42-11.

Part: PANEL — CHAFED (WING) · airframe 11,894 hrs · 7,427 cycles

RS-2-22 PANEL 684EB HAS A CHAFED SPOT. REPLACED PANEL 684EB AND LOCATED AND DRILLED IAW CRJ 900 SRM 51-40-11.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

ANTENNA DOUBLER IS CORRODED BETWEEN FS 310 & FS 295, AND STRINGERS 26L & 26R. REMOVED AND REPLACED ICAS ANTENNA DOUBLER IAW CRJ 900 SRM 51-42-06.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

ATTACHMENT ANGLE, 2" RIGHT OF STRINGER 27, IS CORRODED FROM FS 349 TO FS 364. REMOVED AND REPLACED ATTACHMENT ANGLE (I/B RIGHT DIAPHRAM) IAW CRJ-900 SRM 51-42-06. AAR SM-74.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

NR 1544870, SPLICE ON STGR 26R HAS CORROSION AT FRAME 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR 26R AT FS 333 IAW CRJ 900 SRM 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

STRINGER 26L IS CORRODED FS 333 STRINGER SPLICE. REMOVED & REPLACED STGR 26L SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

CABIN LEFT SEAT TRACK NUMBER 7 - STA 813- TRACK IS CORRODED (2) PLACES. REMOVED AND REPLACED LEFT NR 7 SIDE WALL SEAT TRACK IAW CRJ 900 AMM 53-00-49. P/N SH670-36260-5.

Part: PANEL — CHAFED (WING) · airframe 11,894 hrs · 7,427 cycles

RS-2-20 (PANEL RACK) PANEL 584EB IS CHAFED. REMOVED & REPLACED PANEL 584EB IAW CRJ-900 SRM 51-42-11.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 11,894 hrs · 7,427 cycles

MID CARGO BAY DOOR LOWER FWD & AFT DOOR SKIN CHAFED. REMOVED CHAFE FROM MID CARGO BAY DOOR LOWER FWD AND AFT DOOR SKIN IAW CRJ 900 SRM 51-21-11. SEE CONTINUATION CARD FOR DETAILS.

Part: PANEL — WORN (WING) · airframe 11,894 hrs · 7,427 cycles

RS-2-22 PANEL 699AB HAS A WORN GROVE IN IT. LOCATED AND DRILLED THE REPLACEMENT PANEL 699AB P/N 601R-13-440-2 REF CRJ-900 SRM 51-40-11.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,894 hrs · 7,427 cycles

PAX DOOR FLOOR ANGLE CORRODED. REMOVED AND REPLACED PAX DOOR FLOOR ANGLE IAW CRJ 900 SRM 51-41-02. P/N SH670-31825.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 7,818 hrs · 4,929 cycles

PHOTO ILLUM STRIP MISSING IN GALLEY. REPLACED GALLEY FLOOR STRIP AS REQ IAW MM 25-33.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 599 hrs · 416 cycles

CREW INFORMED MX THAT EMERGENCY LIGHTING WAS INOP. REPLACED BATTERY CHARGER AND BATTERY PACK.

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 284 hrs · 192 cycles

GEAR EXTENSION FAILED ON APPROACH TO DTW. PERFORMED EMERGENCY LANDING GEAR EXTENSION AND LANDED IN DTW. (S)