N200PQ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
149 reports on file, 2011-06-27 – 2025-05-14.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK ON INTERCOSTAL BTW FS177 AND FS185 ON FWD EQUIPMENT COMPARTMENT WAS FOUND IN REF. TO NRC 0444. INTERCOSTAL BTW FS177 AND FS185 ON FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER EA CRJ953-19327 REV. IR
Part: SKIN — CRACKED · airframe 34,483 hrs · 25,575 cycles
AFTER TO REPAIR SKIN, LEADING EDGE, FIXED, SS201.55 - SS210.69, PER EA CRJ957-19084 REV.IR, CRACK WAS FOUND ON WELDING REPAIR CRACK FOUND ON WELDING REPAIR OF LEADING EDGE, FIXED, SS201.55 - SS210.69 WAS REPAIRED PER EA CRJ957-19084 REV. B
Part: SUPPORT — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK ON FWD SUPPORTS (2EAS) OF INBOARD BRAKE ACCUMULATOR WAS FOUND FWD SUPPORT OF INBOARD BRAKE ACCUMULATOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: ACCESS PANEL — CORRODED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB SETTLEMENT (STRAP) AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB WAS REPAIRED PER EA CRJ953-19313 REV IR AND WAS REPLACED PER CRJ900 SRM 51-42-10-001-001-A01
Part: CANISTER — CRACKED (ZONE 500) · airframe 34,483 hrs · 25,575 cycles
CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,483 hrs · 25,575 cycles
CORROSION ON RBL9/LBL9 SEAT TRACK BTW FS661.00+90-FS693.00. AT FLOOR STRUCTURE. DUE TO EXCESSIVE DAMAGE ON RBL9/LBL9 SEAT TRACK BTW FS 661.00 + 16 TO FS 693.00 AT FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A07)
Part: FITTING — CORRODED (ZONE 200) · airframe 34,483 hrs · 25,575 cycles
CORROSION ON FITTING (7 EAÿ½S) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE. FITTING (3 EA'S) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
Part: ACCESS PANEL — CRACKED (ZONE) · airframe 34,483 hrs · 25,575 cycles
CRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR IN REF. TO TASK CARD 900-57-510-700. CRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR WAS REPAIRED REO 670-53-82-430 REV: - -
Part: SUPPORT — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK ON AFT TRACK SUPPORT FS1047 OF THE AFT BAGGAGE BAY DOOR AFT TRACK SUPPORT (DIAPHRAGM) FS1047 OF THE AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 CRJ900 SRM 51-42-21-001-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00 AT FWD EQUIPMENT COMPARTMENT CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB RH SIDE FS193. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB RH SIDE FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
Part: SUPPORT — CRACKED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CRACK ON SUPPORT JB6, FWD CORNER AT FWD EQUIPMENT COMPARTMENT SUPPORT JB6, FWD CORNER AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 34,483 hrs · 25,575 cycles
CORROSION ON MID CAP ANGLE LOWER SURROUND STRUCTURE PASSENGER DOOR. MID CAP ANGLE LOWER SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND WAS REPLACED PER CRJ900 51-41-02-001-001-A01
Part: PANEL — CORRODED (ZONE 800) · airframe 34,483 hrs · 25,575 cycles
CRACKED AFT SIDE PANEL BTW TOP STEP AND MIDDLE STEP AT PASSENGER DOOR INTERNAL STRUCTURE (STEP SETTLEMENT AREA, UPPER & LOWER). AFT SIDE PANEL BTW TOP STEP AND MIDDLE STEP AT PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01.
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 34,483 hrs · 25,575 cycles
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
Part: SUPPORT — CORRODED (ZONE 100) · airframe 34,483 hrs · 25,575 cycles
CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB. SUMMARY: CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01
Earlier reports · 2011–2024 · 133 reports
2024
Part: BRACKET — NONE · airframe 33,605 hrs · 24,837 cycles
WHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. COMPLIED WITH MHIRJ EO SH698-75359 SNIEO S11.
Part: FLOOR SUPPORT — MISMANUFACTURED (ZONE 200) · airframe 33,605 hrs · 24,837 cycles
WHILE INCORPORATING SB 670SH-53-043 REV C, WE HAVE ENCOUNTERED MISMATCHED FACTORY PILOT HOLES @FS 843 LBL 18 COMMON TO THE LBL18 FLOOR BEAM AND PRESSURE BOX EXISTING HOLES. COMPLIED WITH MHIRJ REO 690-53-41-503 REV--10/17/2024.
Part: A/C PACK — UNKNOWN · airframe 33,605 hrs · 24,837 cycles
WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND LH AND RH STR12A FITTINGS PN CC670-33563-001SB AND CC670-33562-001SB CANNOT BE INSTALLED IAW SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING FASTENERS LOCATIONS ON THE AIRCRAFT COMPLIED WITH MHIRJ REO 690-53-11-1871 REV -- DATED 2024-10-12.
Part: LUG — CRACKED (ZONE 800) · airframe 33,605 hrs · 24,837 cycles
L/H FORWARD EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW THE AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17473 REV IR 10/15/2024.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,605 hrs · 24,837 cycles
RBL 9 SEAT TRACK FOUND TO BE CORRODED F.S. 693 TO F.S 847. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01, MODSUM IS67053000195, AND CRJ 900 AMM 53-00-49-400-801-A07.
Part: DOOR — CRACKED (ZONE 800) · airframe 33,605 hrs · 24,837 cycles
L/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17506 REV IR 10/15/2024.
Part: DOOR — CRACKED (ZONE 800) · airframe 33,605 hrs · 24,837 cycles
R/H FORWARD EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW THE AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17502 REV IR 10/12/2024.
Part: DOOR — CRACKED (ZONE 800) · airframe 33,605 hrs · 24,837 cycles
R/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17503 REV IR 10/12/2024.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,605 hrs · 24,837 cycles
LBL 9 SEAT TRACK FOUND TO BE CORRODED F.S. 693 TO F.S 847. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01, MODSUM IS67053000195, AND CRJ 900 AMM 53-00-49-400-801-A07.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,464 hrs · 23,809 cycles
AFT EMERGENCY LIGHTS ON BOTH SIDES INOP. R & R EPSU BATTERY PACK (PS38) IAW JC 33-900-701.
2021
Part: BEAM — CORRODED · airframe 27,718 hrs · 19,788 cycles
AFT CARGO COMPARTMENT, FLOOR BEAM AT LBL 27 CORRODED IN A COUPLE LOCATIONS FROM APPROX FS 1000.00 TO FS 1031.00. - REPAIRED AFT CARGO FLOORBEAM AT LBL 27 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND INSTALLED MYLAR IAW CRJ 900 SRM 51-27-19-001-001-A01.
Part: PLATE — CORRODED (PAX DOOR) · airframe 27,718 hrs · 19,788 cycles
PAX DOOR SURROUND STRUCTURE, LOWER MID CAP ANGLE CORRODED BETWEEN FS 310 AND FS 349. - REMOVED AND REPLACE PAX DOOR MID CAP ANGLE AND KICKPLATE ANGLES IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & 51-40-11-001-001-A01 & ADJUSTED PROX SWITCH IAW AMM 52-70-04-820-802-A01. WVAC EMP STAMP # 750 MTC.
Part: RETAINER — CRACKED · airframe 27,718 hrs · 19,788 cycles
WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE RETAINERS AND 1 EACH UPPER RETAINER AND PAINTED RIVET HEADS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-41-02-001-001-A01, AMM 53-07-420-802-A01, AND SRM 51-25-11-001-001-A01 LEAK CHECK GOOD.
Part: ANGLE — CORRODED (BS 310-349) · airframe 27,718 hrs · 19,788 cycles
PAX DOOR SURROUND STRUCTURE, LOWER MID CAP ANGLE CORRODED BETWEEN FS 310 AND FS 349. - REMOVED AND REPLACE PAX DOOR MID CAP ANGLE AND KICKPLATE ANGLES IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & 51-40-11-001-001-A01 & ADJUSTED PROX SWITCH IAW AMM 52-70-04-820-802-A01.
Part: PLATE — MISSING (LT PYLON) · airframe 27,718 hrs · 19,788 cycles
LH PYLON HAS 2 BOND PLATES MISSING ON TOP OF PYLON AND RH PYLON HAS ONE BOND PLATE MISSING. - INSTALLED 3 EA NEW BONDING PLATE ON L/H PYLON TOP SURFACE AND 2 EA NEW BONDING PLATE ON R/H PYLON P/N MM670-37197-007 IAW CRJ 900 SRM 51-42-13-001-001-A01. AND AMM 51-80-00-760-801-A01. CHECK BOND 6000 AND 51-80-00-910-812-A01, 51-80-00-140-804-A01. AMM.
Part: FRAME — CRACKED · airframe 27,718 hrs · 19,788 cycles
FRAME AT FS 333 BETWEEN STGR 1R AND STGR 2R CRACKED. - REPAIRED CRACKED FRAME AT FS 333 BETWEEN STR1R AND STR2R IAW ENDEAVOR EA CRJ 953-12092 REV IR DATED 9/15/21. CUT, REPAIRED, AND LEACK CHECKED POTABLE WATER LINE BTWEEN FS 333 AND FS 349 IAW CRJ 900 AMM 20-30-00-910-802-A01. LEAK CHECK GOOD. WVAC EMP # 574784
Part: YOKE — NICKED (ENGINE MOUNT) · airframe 27,718 hrs · 19,788 cycles
RIGHT ENGINE FWD YOKE MOUNT HAS SEVERAL NICKS ON THE LOWER END FWD AND AFT EDGES - REPAIRED RIGHT ENGINE FWD YOKE NICKS ON THE LOWER END FWD & AFT EDGES IAW BOMBARDIER REO#670-71-21-057, REV--, DATED 2013-09-13.
Part: RETAINER — CRACKED (CARGO DOOR SEAL) · airframe 27,718 hrs · 19,788 cycles
WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE RETAINERS AND 1 EACH UPPER RETAINER AND PAINTED RIVET HEADS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-41-02-001-001-A01, AMM 53-07-420-802-A01, AND SRM 51-25-11-001-001-A01 LEAK CHECK GOOD.
Part: RETAINER — CRACKED (CARGO DOOR SEAL) · airframe 27,718 hrs · 19,788 cycles
WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE RETAINERS AND 1 EACH UPPER RETAINER AND PAINTED RIVET HEADS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-41-02-001-001-A01, AMM 53-07-420-802-A01, AND SRM 51-25-11-001-001-A01 LEAK CHECK GOOD.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 24R CORRODED BETWEEN FS 295 TO FS 310. - INSTALLED STR 24R FS 280-333 IAW ENDEAVOR AIR EA# CRJ 953-12340.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 19R CORRODED BETWEEN FS 295 AND FS 310 - REMOVED AND REPLACED STR 19R FROM F.S. 295-310 IAW CRJ 900 SRM 51-42-21-001-001-A01 AND EA CRJ953-12283 REV IR DATED 10/15/2021. WVAC EMP STAMP # 711 MTC
Part: LONGERON — CORRODED · airframe 27,718 hrs · 19,788 cycles
LONGERON AT STR 25R F.S. 333-349 CORRODED - REMOVED & REINSTALLED INTERCOSTAL AT STRGR 25R FOR ACCESS & REMOVED & REPLACED LONGERON IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001 001-A01, 51-42-21-001-001-A01 & COMPLIED WITH EA CRJ953-12231 DATED 10/5/2021 REV IR. WVAC EMP STAMP # 774 MTC
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 23R CORRODED BETWEEN FS 295 TO FS 310. - INSTALLED STR 23R FS 280-333 IAW ENDEAVOR AIR EA# CRJ 953-12284.
Part: ANGLE — CORRODED · airframe 27,718 hrs · 19,788 cycles
GALLEY SERVICE DOOR SILL ANGLE IS CORRODED BEHIND ATTACH BRACKET FOR SCUFF PLATE. (PROTECTOR PLATE). - REMOVED & REPLACED SERVICE DOOR SILL ANGLE IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED & REINSTALLED SERVICE DOOR FITTINGS & TORQUED & SAFETIED BOLTS IAW CRJ SRM 51-41-02-001-001-A01, & CRJ 900 AMM 'S 20-21-00-910-801-A01 & 20-51-00-400-807-A01. OPS CHECK GOOD FOR CRJ 900 AMM 52-41-00-700-801-A01.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
AFT CARGO BAY SEAT TRACK AT LBL 27 BEGINNING AT APPROX FS 985.00 CORRODED. - REMOVED FABRICATED AND INSTALLED SEAT TRACK @ LBL27 FS 926-988 IAW CRJ 900 SRM 53-51-49-101-001-A02, 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07.
Part: INTERCOSTAL — CORRODED · airframe 27,718 hrs · 19,788 cycles
INTERCOSTAL AT STGR 27R CORRODED BETWEEN FS 349 AND FS 364. - REMOVED, LOCATED, DRILLED & INSTALLED NEW INTERCOSTAL AT STR 27R FS 349-364 AND R/R PROX SENSOR IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND AMM 52-70-08-000/400-801-A01. OPS GOOD. WVAC EMP STAMP # 712 MTC.
Part: INTERCOSTAL — CORRODED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STGR 20L BETWEEN FS 310 AND FS 349. - REMOVED, UNSERVICEABLE INTERCOSTAL, DRILLED & LOCATED & INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, & REINSTALLED CONNECTOR IAW CRJ 900 ESPM 20-26-31. WVAC EMP STAMP #774 MTC
Part: BRACKET — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH HYDRAULIC BRAIDED LINES BRACKET FOR LH MLG BRAKE SYSTEM IS CORRODED ABOVE MLG SIDE STAY ACTUATOR. - REMOVED & REPLACED L/H HYDRAULIC INTERFACE BRACKET AT LBL 48 IAW CRJ 900 SRM 51-41-02-001-001-A01. RECONNECTED 5 EACH MLG HYDRAULIC LINES IAW CRJ 900 AMM 20-22-00-910-801-A01. BLEED, LEAK & OPS CHECK GOOD. WVAC EMP STAMP #774 MTC
Part: CHANNEL — CRACKED · airframe 27,718 hrs · 19,788 cycles
STRAP ASSY ON PANEL 195DL IS CRACKED. - DRILLED, LOCATED, INSTALLED & MODIFIED C-CHANNEL IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-40-11-001-001-A01, & BOMBARDIER IS 670538200021.
Part: ANGLE — CORRODED · airframe 27,718 hrs · 19,788 cycles
FRAME ON INNER PAX DOOR STRUCTURE @ FS 327 HAS EVIDENCE OF CORROSION. - REMOVED & REPLACED 327 FRAME & ATTACHING ANGLE ON INNER PAX DOOR IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP STAMP #774 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
AFT CARGO BAY SEAT TRACK AT RBL9 BEGINNING AT APPROX. FS 985.00 CORRODED. - REMOVED SEAT TRACK, FABRICATED SEAT TRACK & INSTALLED SERVICEABLE SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 & 51-40-11-001-001-A01 & AMM 53-00-49-000/400-801-A07. WVAC EMP STAMP # 774 MTC.
Part: INTERCOSTAL — CORRODED · airframe 27,718 hrs · 19,788 cycles
SERVICE DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED BETWEEN FS 295 AND FS 333 AT STGR 20R. - REMOVED INTERCOSTAL AT RBL27 FOR ACCESS & INSTALLED, REMOVED & INTERCOSTAL AT 20R IAW CRJ 900 SRMS 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 & INSTALLED SCREWS IAW CRJ 900 SRM 51-41-02-001-001-A01. WVAC EMP STAMP
Part: SKIN — CORRODED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR INNER SKIN CORRODED AND DENTED IN MULTIPLE LOCATIONS (MARKED WITH TAPE). - REMOVED PAX DOOR INNER SKIN , LOCATED & DRILLED NEW SKIN & INSTALLED NEW SERVICEABLE SKIN IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-14-001-001-A01, 51-42-15-001-001-A01, 51-42-22-001-001-A01, 51-23-00-001-001-A01. WVAC EMP STAMP #774 MTC
Part: FRAME — CORRODED · airframe 27,718 hrs · 19,788 cycles
FRAME ON INNER PAX DOOR STRUCTURE @ FS 327 HAS EVIDENCE OF CORROSION. - REMOVED & REPLACED 327 FRAME & ATTACHING ANGLE ON INNER PAX DOOR IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP STAMP #774 MTC
Part: RIB — BENT · airframe 27,718 hrs · 19,788 cycles
LH AILERON, "RIBLET" IN CTR HINGE BENT. - REPLACED RIBLET IAW SRM 57-02-21-001-001-A01 AND PAINTED RIVETS IAW SRM 51-21-10-001-001-A01.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER AT STGR 25L CORRODED FROM FS 319 TO FS 349. - REPAIRED IAW ENDEAVOR EA CRJ 953-12200 REV IR DATED 10/19/2021.
Part: CUP — CORRODED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR TOP STAIR PANEL, FEED THROUGH CUP AND FWD "C" CLIP CORRODED. - REMOVED TOP STAIR PANEL IAW CRJ 900 SRM 51-92-13-001-001-A01. DRILLED NEW PARTS IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED TOP STAIR PANEL IAW CRJ 900 SRM 51-42-13-001-001-A01. WVAC EMP #56689
Part: FITTING — CORRODED · airframe 27,718 hrs · 19,788 cycles
GALLEY SERVICE DOOR BOTTOM SEAL STRIKER HAS CORROSION AROUND SCREW HOLES. - REMOVED & REPLACED STRIKER SEAL IAW CRJ SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 53-21-23-001-002-A01.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 20R CORRODED BETWEEN FS 295 TO FS 310. - REMOVED UNSERVICEABLE STRINGER 20R, DRILLED, LOCATED & INSTALLED NEW SERVICEABLE STRINGER IAW CRJ 900 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-40-11-001-001-A01. WVAC EMP STAMP #774 MTC
Part: FITTING — CORRODED · airframe 27,718 hrs · 19,788 cycles
GALLEY SERVICE DOOR SILL PROTECTOR FITTINGS (4 EACH) CORRODED REMOVED UNDER OP #145, 146. - LOCATED & DRILLED 4EACH SILL PROTECTOR FITTINGS IAW CRJ 900 SRM 51-SRM'S 51-40-11-001-001-A01 & 51-42-21-001-001-A01. WVAC EMP STAMP #774 MTC
Part: RETAINING CLIP — CORRODED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR TOP STAIR PANEL, FEED THROUGH CUP AND FWD "C" CLIP CORRODED. - REMOVED TOP STAIR PANEL IAW CRJ 900 SRM 51-92-13-001-001-A01. DRILLED NEW PARTS IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED TOP STAIR PANEL IAW CRJ 900 SRM 51-42-13-001-001-A01. WVAC EMP #56689
Part: FRAME — CORRODED · airframe 27,718 hrs · 19,788 cycles
FRAME AT FS 295 CORRODED BETWEEN STGR 25L AND STGR 25R. - REPAIRED FRAME AT FS 295 IAW CRJ 900 SRM'S 53-00-06-201-006-A01 & 51-40-11-001-001-A01.
Part: FITTING — GOUGED · airframe 27,718 hrs · 19,788 cycles
LH AILERON OB CTR HINGE NODE HAS LARGE GOUGE ON BOTTOM RADIUS. - REPAIRED IAW BOMBARDIER REO 670-57-61-107 REV B DATED 2019-01-14. WVAC EMP STAMP #774 MTC
Part: FITTING — GOUGED · airframe 27,718 hrs · 19,788 cycles
LH AILERON OB PCU LINK ATTACH NODE HAS A LARGE GOUGE ON THE BOTTOM RADIUS. - REPAIRED IAW BOMBARDIER REO 670-57-61-107 REV B DATED 2019-01-14. WVAC EMP STAMP #774 MTC
Part: BEAM — CORRODED · airframe 27,718 hrs · 19,788 cycles
AFT CARGO BAY FLOOR BEAM @ LBL 9 CORRODED IN SEVERAL AREAS FROM APPROX FS 1000.00 TO AFT OF FS 1047.00. - REPAIRED IAW CRJ 900 SRM 53-00-41-201-001-A03.
Part: ANGLE — CORRODED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR SURROUND STRUCTURE, LOWER SILL ANGLE CORRODED BETWEEN FS 310 AND FS 349. - LOWER SILL ANGLE IDENTIFIED AS PART #SH670-31875-7. FOUND PART CORRODED BEYOND REPAIR AND REQUIRES REPLACEMENT IAW CRJ 900 SRM 51-77-00-001-001-A01. REMOVED AND REPLACED LOWER SILL ANGLE, KICKPLATE PT #SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. RESORTRED PAINT FINISH TO REWORKED AREA IAW CRJ 900 SRM 51-25-16-001-001-A01. WVAC EMP #460661
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
SEAT TRACK HAS MULTIPLE AREAS OF CORROSION AT RBL 9 FS 849.00+49 TO FS 977.00. - FOUND SEAT TRACK AT RBL 9 FS 849.00+49-FS 977.00 TO BE OUT OF REPAIRABLE LIMITS IAW CRJ 900 SRM 53-31-49-001-001-A02. REMOVED SEAT TRACK AT RBL 9 FS 849.00+49-FS 977 IAW CRJ 900 AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01. INSTALLED NEWLY FABRICATED SEAT TRACK AT RBL 9 FS 849.00+49-FS 977.00 IAW CRJ 900 AMM 53-00-49-400-801-A07. WVAC EMP STAMP # 712 MTC.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 26R CORRODED BETWEEN FS 294-FS 310 - DAMAGE OUT OF TOLERANCE IAW SRM 53-21-03-101-002-A04. DRILLED NEW STR IAW SRM 51-40-11-001-001-A01 INSTALLED STR AND STR SPLICE IAW 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 WVAC EMP # 56689
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
R/H SIDE SEAT RAIL FS 744-752 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED RH SIDE SEAT RAIL AT FS 744-FS 752 AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07. WVAC EMP # 56689
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
R/H SIDE SEAT RAIL FS 379-485 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED RH SEAT RAIL IAW CRJ 900 AMM 53-00-49-00-801, SRM RAIL OUT OF LIMITS PER SRM 53-21-49-101-001-A01 AND INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801-A07 WVAC EMP # 56689
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
STRINGER 25R CORRODED BETWEEN FS 319 TO 333. - REMOVED STRINGER 25R AND 3EA CLIPS, 2EA STANDOFFS AT FS 280.00 TO FS 333, LOCATED AND DRILLED NEW STR 25R AND INSTALLED NEW STRINGER 25R PN:SH670-31212-2U, AND SAME SERVICEABLE 3EA CLIPS AND 2EA STANDOFFS, IAW CRJ 900 SRM 51-42-06-001-001-A01,AND 51-40-11-001-001-A01. WVAC EMP #56689
Part: SPLICE ANGLE — CORRODED · airframe 27,718 hrs · 19,788 cycles
FS 280 CROSSBEAM LOWER SPLICE ANGLE CORRODED AND BLOWN UP HOLES. - FOUND SPLICE ANGLE TO BE OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01, LOCATED, DRILLED & INSTALLED & PAINTED SERVIEABLE SPLICE ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-25-00-001-001-A01. WVAC EMP STAMP # 774 MTC
Part: STRINGER — CRACKED · airframe 27,718 hrs · 19,788 cycles
STR 3L AT FS 280 IS CRACKED - COMPLIED WITH ENDEAVOR AIR E.O. R53568 REV 5. REFERENCE JOB 81520045, OP 5344 FOR COMPLETION OF THIS TASK. WVAC EMP # 583111
Part: JOINT — CORRODED · airframe 27,718 hrs · 19,788 cycles
JOINT ANGLE/SPLICE AT STR 25R FS 333 CORRODED. - LOCATED, DRILLED & REPLACED JOINT ANGLE SPLICE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-00-001-001-A01, 51-14-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS 744-752 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED AND REPLACED LH SIDE SEAT RAIL FS 744 - FS 752 IAW CRJ 900 AMM 53-00-49-000/400-801-A07. WVAC EMP STAMP #776 MTC
Part: ANGLE — CORRODED · airframe 27,718 hrs · 19,788 cycles
FWD WING TO FUSELAGE. FAIRING (191BB/191CB) MID SUPPORT FRAME HAS CORROSION ON ATTACHMENT ANGLE APPROXIMATELY LBL 6 FS 661+90. - REMOVED AND REPLACED ATTACH ANGLE AT FS 661+90 LH SIDE ON MID SUPPORT FRAME IAW CRJ 900 SRM 51-42-11-001-001-A01 AND 51-42-15-001-001-A01. WVAC EMP STAMP # 776 MTC
Part: BEAM — CRACKED · airframe 27,718 hrs · 19,788 cycles
PAX DOOR, AFT GAS SPRING BEAM CRACKED - REMOVED AND REPLACED PAX DOOR, AFT GAS SPRING BEAM WITH A NEW PART P/N 601R318011-1 IAW CRJ SRM 51-42-06-001-001-A01 WVAC EMP STAMP # 712 MTC
Part: CROSSBEAM — CORRODED · airframe 27,718 hrs · 19,788 cycles
FS 280 RH CROSSBEAM CORRODED. - REMOVED AND REPLACED FS 280 RH CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND 51-42-22-001-001-A01 AND 51-42-22-001-001-A01. WVAC EMP STAMP # 776 MTC.
Part: CROSSBEAM — CORRODED · airframe 27,718 hrs · 19,788 cycles
FS 280 LH CROSSBEAM CORRODED. - REMOVED AND REPLACED FS 280 LH CROSSBEAM IAW CRJ 900 SRM
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
R/H SIDE SEAT RAIL 581-661+16 HAS CORROSION ON MULTIPLE SPOTS - REMOVED UNSERVICEABLE SEAT TRACKS, FABRICATED NEW SEAT TRACK, & INSTALLED NEWLY FABRICATED SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 & CRJ 900 AMM 53-00-49-000/400-801-A07. INSTALLED AND TIGHT-ENED SCREWS ON SEAT RAIL AT FS 597 AND FS 661 IAW CRJ 900 AND REMOVED ORANGE TAPE, AMM 53-0-49-400-801(CONFIG A07)
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
SEAT TRACK AT RBL9 FS 661+8.4 TO FS 693 HAS MULTIPLE AREAS OF CORROSION. - FOUND SEAT TRACK CORROSION AT BL9 FS 661+8.4 TO FS 693 TO BE OUT OF ALLOWABLE LIMITS IAW CRJ 900 SRM 53-41-49-101-001-A02. FABRICATED NEW SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 & 51-40-11-001-001-A0 REMOVED CORRODED SEAT TRACK AT RBL9 FS 661+8.4 - FS 693 AND INSTALLED NEW FABRICATED TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A7.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
L/H SIDE SEAT RAIL FS 913-969 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED LH SIDE SEAT RAIL AT F.S. 913-F.S.969 IAW CRJ900 AMM 53-00-49-000-801-A19. FABRICATED NEW SEAT RAIL IAW CRJ900 SRM 53-00-49-201-002-A01.INSTALLED NEW FABRICATED SEAT RAIL LH SIDE FS913-FS969 IAW CRJ900 AMM 53-00-49-400-801-A19. WVAC EMP STAMP # 712 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
SEAT TRACK HAS MULTIPLE AREAS OF CORROSION AT RBL 9 FS 834.00 TO FS 849.00+48. - FABRICATED SEAT TRACK & INSTALLED SERVICEABLE SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01, 51-40-11-001-001-A01, & CRJ 900 AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS677-720 HAS CORROSION ON MULTIPLE SPOTS. - INSTALLED LH SIDE SEAT TRACK AT FS 677 TO 720 IAW CRJ 900 AMM 53-00-49-400-801(CONFIG A07). WVAC EMP STAMP #750 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS379-485 HAS CORROSION ON MULTIPLE SPOTS. - INSTALLED L/H SIDE SEAT RAIL FROM FS 379 TO 485 IAW CRJ 900 AMM 53-00-49-400-801(CONFIG A07) WVAC EMP STAMP #750 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
RH SIDE SEAT RAIL 677-720 HAS CORROSION ON MULTIPLE SPOTS. - INSTALLED RH SIDE SEAT RAIL AT FS 677 TO 720 IAW CRJ 900 AMM 53-00-44-400-801(CONFIG A07). WVAC EMP STAMP #774 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
SEAT TRACK AT LBL 9 FS 581- FS 661+8.4 HAS MULTIPLE AREAS OF CORROSION - INSTALLED SEAT TRACK AT LBL9 FS581 TO FS661+8.4 IAW CRJ 900 AMM 53-00-49-400-801 (CONFIG A07). WVAC EMP STAMP #781 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS847+16-913 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED & REPLACED L/H SEAT TRACK FS 847+16 - FS 913 IAW CRJ 900 AMM 53-00-49-000/400-801-A19 AND FABRICATED SEAT TRACK CRJ 900 SRM 53-00-49-201-002-A01. WVAC EMP STAMP #774 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS485 TO FS581 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED AND REPLACED SEAT TRACK AND FABBED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A19 AND CRJ 900 SRM 53-00-49-201-A01. WVAC EMP STAMP #774 MTC
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
LH SIDE SEAT RAIL FS661+16-677 HAS CORROSION ON MULTIPLE SPOTS. - REMOVED & REPLACED L/H SIDE SEAT RAIL 661+16-677 AND FABRICATED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A19 AND CRJ 900 SRM 53-00-49-201-002-A01 & SRM 51-40-11-001-001-A01. WVAC EMP STAMP #774 MTC
Part: FRAME — CRACKED (BS 333 S2R) · airframe 27,717 hrs · 19,788 cycles
FRAME, FS333.00, S1R-S2R, PN SH670-31356-5, CL600-2D24, FOUND CRACKED IN THE UPPER SECTOR OF THE FRAME AT FS333.00 BETWEEN S1R AND S2R. THE CRACK MEASURES 2.50â IN LENGTH. THE FRAME IS FORMED FROM 0.050" 7075-T62 AL ALLOY.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
RH SIDE SEAT RAIL FS485-581 HAS CORROSION ON MULTIPLE SPOTS. - FABRICATED NEW SEAT RAIL AT RH SIDE FS 485-581 IAW CRJ 900 SRM 53-00-49-201-002-A01 AND INSTALLED ON THE RIGHT SIDE AT FS 485 TO FS 581 IAW CRJ 900 AMM 53-00-49-400-801-A19.
Part: STRINGER — CORRODED · airframe 27,718 hrs · 19,788 cycles
FS 485.00 HAS CORROSION AT STGR 26LH. - REMOVED CORROSION AT FS 485 BETWEEN ST 25L TO 26R IAW CRJ 900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS AND FOUND TO BE WITHIN LIMITS IAW CRJ 900 SRM 53-31-06-101-003-A04. MATERIAL REMOVED .004". NOMINAL THICKNESS .050" CRJ 900 SRM 51-42-06-001-001-A01. APPLIED PROTECTIVE TREATMENT AND PAINT BLENDED AREAS IAW CRJ 900 SRM 51-25-06-001-001-A01 AND 51-23-16-001-001-A01. WVAC EMP #587140
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
SEAT TRACK AT LBL 9 FS 485-FS 581 HAS MULTIPLE AREAS OF CORROSION. - INSTALL SEAT TRACK PN: SH690-33405-1 AT LBL 9 FS 485 TO FS 581 IAW CRJ 900 AMM 53-00-49-400-801-A19.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
RH SIDE SEAT RAIL FS661+16-677 HAS CORROSION ON MULTIPLE SPOTS. - INSTALLED NEW RH SIDE SEAT RAIL FS661+16-677 IAW CRJ 900 AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED · airframe 27,718 hrs · 19,788 cycles
FLOOR SEAT TRACK AT RBL 9 CORRODED BETWEEN FS 349 TO FS 485 - REMOVED & REPLACED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 349 TO FS 485 IAW CRJ 900 AMM 53-00-49-000/400-801. WVAC EMP STAMP #712 MTC
2018
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,845 hrs · 16,697 cycles
AFT OVERBOARD EMERGENCY CALL LIGHT INOP. VERIFIED MID-CABIN (RED) EMG LIGHT VERY DIM. ITEM DEFERRED IAW MEL 23-40-1K (B). ENTERED IN MM02 MXC NOTIFIED 98765.***REPLACED MID CABIN OVERWING EXIT LOCATING AFT SIGN IAW AMM 33-51-07. OPS CK GOOD. REMOVE D FROM MM02. PLACARD REMOVED. MXC NOTIFIED #95974
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,802 hrs · 15,926 cycles
OVERHEAD EMERGENCY EXIT ROW SIGN LENS WAS MISSING. SECURE THE EMERGENCY LIGHT LENS.
Part: DOOR SILL — GOUGED (AFT CARGO) · airframe 22,196 hrs · 15,446 cycles
AFT CARGO DOOR CUTOUT LOWER SILL, AFT HALF HAS LIGHT MULTIPLE GOUGES. REPAIRED THE CARGO LOWER DOOR SILL IAW EA 953-6505, REV A. PERFORMED A VRMC CHECK IAW AMM 52-00-00-790-801, NO LEAKS NOTED.
Part: STRINGER — CORRODED (BS 280-319.7) · airframe 22,196 hrs · 15,446 cycles
STRINGER 25R HAS CORROSION BETWEEN BS 319.7 AND 280, IN THE FWD E&E BAY. REPAIRED THE STRINGER IAW EA CRJ953-06533.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,196 hrs · 15,446 cycles
PASSENGER DOOR, AFT WEB DRAG ANGLE IS CRACKED. REPAIRED THE DRAG ANGLE IAW SRM 52-11-04, AND 51-12-10.
Part: GUARD — CRACKED (MLG WHEEL WELL) · airframe 22,196 hrs · 15,446 cycles
LEFT MLG WHEEL WELL FWD LOWER GRAVEL GUARD PANEL IS CRACKED. REPLACED THE LEFT MLG WHEEL WELL FWD LOWER GRAVEL GUARD IAW AMM 20-21-00.
Part: ELT — INOPERATIVE (ELT BAY) · airframe 22,170 hrs · 15,429 cycles
ELT WIRE BROKEN. R&R ELT MAIN ASSY AND BATTERY IAW AMM 25-62-02 AND JOB CARD 25-360-720. PERFROMED OPS CHECK PER J/C 25-220-700. OPS CHECK GOOD. P/N OFF:452-0133 S/N OFF: 361732-079 P/N OFF:453-5000 S/N OFF170-08575.
Part: OXYGEN MASK — DAMAGED (SEAT 1BA) · airframe 22,161 hrs · 15,423 cycles
LEFT CABIN OXYGEN MASK AT SEAT 1BA IS DAMAGED. INSTALLED A NEW OXYGEN MASK IAW AMM 32-21-09-400-801-A01.
Part: OXYGEN MASK — DAMAGED (CABIN) · airframe 22,161 hrs · 15,423 cycles
RT SIDE CABIN O2 MASKS AT SEATS 4DC, 8DC, AND 10DC HAVE 2 EA MASKS DAMAGED. REMOVED AND INSTALLED SERVICABLE RT SIDE CABIN O2 MASK AT SEATS 4DC, 8DC AND 10DC, OPS TEST GOOD IAW AMM35-21-09-400-801-A01 AND 35-20-00-710-803-A01.
Part: OXYGEN MASK — DAMAGED (RT SIDE CABIN) · airframe 22,161 hrs · 15,423 cycles
RH SIDE CABIN 02 MASK DAMAGED. REMOVED AND REPLACED RH SIDE CABIN O2 MASK, OPS CHECKED GOOD IAW CRJ-900 AMM 35-21-09-400-801-A01 AND 35-20-00-710-803-A01.
2017
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 20,837 hrs · 14,397 cycles
TCAS DOUBLER AT FS 295.00 - 310.00 CORRODED. REMOVED CORRODED DOUBLER, LOCATED AND DRILLED NEW TCAS DOUBLER IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE TCAS DOUBLER IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01 & DWG #SH670-32364. INSTALLED TCAS ANTENNA BETWEEN FS 295 - 310 IAW AMM 34-43-07-400-801 A03.
Part: FRAME — CORRODED (FUSELAGE) · airframe 20,837 hrs · 14,397 cycles
CORROSION AT FS 349.00 25R-26R. COMPLIED WITH REMOVED CORROSION AND RESTORED FINISH PER EC/TC REO 670-53-21-1308.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 20,837 hrs · 14,397 cycles
CORROSION ON SPLICE AT FS 333.00 26L. REMOVED CORROSION AND RESTORED FINISH OF AREAS WITHIN LIMITS PER ECTC REO 670-53-21-1308. REPLACED SPLICES AT FS 333-349 26L+26R PER SRM 51-42-06-001-001-A01, DWG SH670-32420 AND SRM 51-40-11-001-001-A01.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,590 hrs · 13,563 cycles
FWD UPPER LT GALLEY LIGHT NEEDS RELAMPING. RELAMPED BULB IN FWD UPPER LT ENTRY EMERGENCY LIGHT IAW AMM 33-51-00-710-801.
Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 19,194 hrs · 13,288 cycles
PILOT REPORTED CAPTAIN'S OXYGEN MASK WILL NOT INFLATE HARNESS. MX REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TESTED GOOD. AIRCRAFT OK FOR SERVICE.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 17,512 hrs · 12,119 cycles
AFTER TAKEOFF, RECEIVED RT BLEED DUCT WARNING MESSAGE. ACFT RETURNED TO DEPARTURE. TROUBLESHOT SYS IAW FIM 36-21-03. COULD NOT DUPLICATE FAULT. OPS CHECK GOOD, ACFT OK FOR SERVICE.
2015
Part: SKIN — DAMAGED (BS 295-310) · airframe 16,699 hrs · 11,550 cycles
BURN ON SKIN BETWEEN BS 295- 310 AND STIRNGERS 25-26R. DRILLED THROUGH BURN IN SKIN USING .0128" DRILL BIT AND DEBURRED NEW HOLE IN SKIN. WORK DONE REF SRM 53-00-00, TR 53-0050. PERFORMED ET INSPECTION OF THE REWORKED AREA IAW NDTM 51-20-006. NO CRACKS NOTED. PERFORMED ET CONDUCTIVITY INSPECTION OF THE REWORKED AREA IAW NDTM 53-00-000-252-A01. MEASURED CONDUCTIVITY IS 34 PERCENT IACS AT 60HZ. INSTALLED SOLID FASTENER AND WASHER IN NEW HOLE IAW SRM 53-00-00, TR 53-0050, THIS IS A PERMANENT REPAIR.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 14,962 hrs · 10,343 cycles
DURING REMOVAL OF LOWER SILL ANGLE FOUND LOWER MOUNTAIN ANGLE TO BE CORRODED AT SERVICE DOOR ENTRANCE. R & R LOWER ANGLE MOUNT TO SERVICE DOOR OPENING IAW SRM 51-42-06-001-001-A01.
2014
Part: BULKHEAD — CORRODED (BS 280) · airframe 14,962 hrs · 10,343 cycles
LT BULKEHAD WEB AT BS 280 HAS LIGHT CORROSION. REMOVED THE CORROSION IAW SRM 53-11-10-201-003-A01. BLENDED AREA ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH EC/TC REO 670-53-11-594 AMD GREO 670-53-11-594, REV.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 14,962 hrs · 10,343 cycles
RIGHT BULKHEAD WEB AT BS 280 HAS LIGHT CORROSION. REMOVED THE CORROSION IAW SRM 53-11-10-201-003, A01, 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV.
Part: FLOOR SUPPORT — CRACKED · airframe 14,962 hrs · 10,343 cycles
RIGHT FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01, AND DWG CC670-33052, REV E.
Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 14,962 hrs · 10,343 cycles
FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-40-06-001-001-A01, AND DWG CC670-33052, REV E.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,962 hrs · 10,343 cycles
LT BS 280 FLOORBEAM IS CRACKED AT LBL 9 . REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: ANGLE — CORRODED · airframe 14,962 hrs · 10,343 cycles
LOWER SILL ANGLE HAS CORROSION AT SERVICE DOOR ENTRANCE. LOWER SILL ANGLE CORROSION IS BEYOND ALLOWABLE LIMITS IAW SRM 53-21-33-101-002-A01. R & R LOWER SILL ANGLE ON SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31986.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,962 hrs · 10,343 cycles
INTERCOSTAL HAS CORROSION BETWEEN BS 349-364 STRINGER 27L. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. 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 DWG SH670-32050, REV J.
Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 14,962 hrs · 10,343 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 785.15 - 830. DAMAGE IS BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A07, AND AMM 53-00-49-400-801 A07.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 14,962 hrs · 10,343 cycles
RIGHT FLOOR SEAT TRACK HAS CORROSION JUST AFT OF BS 349, RBL 9. DAMAGE BEYOND ALLOABLE LIMITS IAW SRM 53-21-49-101-001-A01. R & R CORRODED SEAT TRACK BETWEEN BS 350-485 IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 14,962 hrs · 10,343 cycles
RIGHT FLOOR SUPPORT HAS CORROSION BETWEEN BS 280-310 RBL 45. CORROSION BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-390, REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 & DWG SH670-32170.
Part: STRUCTURE — CORRODED (BS 333) · airframe 14,962 hrs · 10,343 cycles
PACKER CORRODED AT FS 333, RBL 9. CORROISON BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01.
Part: FRAME — CORRODED (BS 310) · airframe 14,965 hrs · 10,345 cycles
FS 310 FRAME HAS CORROSION FROM STR 26L-25R. REMOVED CORRROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-06-101-002-A02. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-06-101-002. REPAIRED FRAME FS 310 IAW REO 670-53-21-799 BY COMPLING WITH EC/TC REO 670-53-21-799. COMPLIED WITH REO 670-53-21-799, 51-20-006.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 14,962 hrs · 10,343 cycles
FLOOR SEAT TRACK AT RBL 9 BS 661+16 - 693 HAS CORROSION. DAMAGE IS BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,962 hrs · 10,343 cycles
INTERCOSTAL HAS CORROSION BETWEEN BS 349-364, STR 27R. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. 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.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 14,962 hrs · 10,343 cycles
RT SIDE SEAT TRACK HAS CORROSION FROM BS 744.15 - 761.85. DAMAGE IS BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-A01, CONFIG A07, AND AMM TASK 53-00-49-400-801, A07.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,962 hrs · 10,343 cycles
ANGLE ATTACHED TO BS 280 FLOORBEAM FOR COCKPIT FLOOR HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. R & R IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 14,962 hrs · 10,343 cycles
RT FLOOR SUPPORT HAS CORROSION AT FS 349, RBL 45. REPAIRED IAW IAW SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 14,962 hrs · 10,343 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 785.15- 830.40. DAMAGE IS BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-013, REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-A01, CONFIG A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 14,962 hrs · 10,343 cycles
LEFT SIDE SEAT TRACK HAS CORROSION FROM BS 744.45 - 761.85. DAMAGE IS BEYOND ALLOWABLE LIMITS OF GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND IAW AMM 53-00-49-400-801-A07.
Part: MEGAPHONE — DAMAGED (CABIN) · airframe 14,364 hrs · 9,922 cycles
MEGAPHONE BATTERY CASE DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,207 hrs · 9,812 cycles
RIGHT FUSELAGE AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT FUSELAGE AFT EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-15.
2013
Part: GROUND WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 11,996 hrs · 8,373 cycles
LEFT OVERWING AFT EMERGENCY EXIT LIGHT INOPERATIVE. FOUND GROUND WIRE OF AFT LT OVERWING EXTERNAL EMERGENCY LIGHT PULLED OUT OF PIN CONTACT. INSTALLED SERVICEABLE PIN CONTACT ON TO GROUND WIRE OF AFT LT OVERWING EXTERNAL EMERGENCY LIGHT IAW ESPM 20-16-00. OPS TESTED GOOD.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,912 hrs · 8,318 cycles
PHOTOLUMINESCENT STRIP MISSING AT RT FWD EMERGENCY EXIT. INSTALLED PHOTOMOINESCENT STRIP MISSING AT RT FWD EMERGENCY EXIT IAW AMM 33-51-01.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 11,497 hrs · 8,033 cycles
F/A REPORTS REAR MEGAPHONE INOPERATIVE, VOLUME CONTROL SPINS FREELY WITH NO STOP. R & R MEGAPHONE AFT IAW AMM 25-61-14.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 10,694 hrs · 7,550 cycles
FLIGHT ATTENDANT REPORTS FORWARD FLASHLIGHT NOT TESTING. REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY AND OPERATIONS CHECKED GOOD PER CRJ-900 CMM 25-60-11.
Part: SENSOR — MALFUNCTIONED (ANTI-ICE SYS) · airframe 10,597 hrs · 7,475 cycles
RIGHT WING ANTI ICE CAUTION MESSAGE WITH WING ANTI-ICE ON. REMOVED AND REPLACED RIGHT INBOARD WING TEMPERTURE SENSOR AND OPERATIONS CHECKED GOOD PER CRJ-900 AMM 30-12-06.
Part: ANTENNA — FAULTY (WEATHER RADAR) · airframe 10,597 hrs · 7,475 cycles
RADAR QUIT WORKING ON APPROACH. IT TURNED BACK ON AFTER LANDING. REMOVED AND REPLACED WEATHER RADAR RECEIVE TRANSMITTER ANTENNA IAW CRJ900 AMM 34-41-01. OPERATIONS CKECKS GOOD.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 10,581 hrs · 7,463 cycles
LIGHTNING DAMAGE AT AT FS 571 S-10R AND AT FS 603 S-10R BEYOND MAXIMUM BLENDOUT LIMITS. CUTOUT TO 1.115" AND 0.6355" RESPECTIVELY. REPAIRED IAW EA CRJ953-01455 AND CORRESPONDING DER SIGNED 8110-3.
Part: SIGN — MISSING (CABIN) · airframe 10,293 hrs · 7,277 cycles
EXIT SIGN MISSING ROW 12. SECURE CENTER AISLE OVERHEAD EXIT ROW IAW CRJ900 AMM 33-51-00, OK FOR SERVICE.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 10,124 hrs · 7,155 cycles
SEAT 11A LIFE VEST BAG TORN. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03.
Part: LIFE VEST — MISSING (CABIN) · airframe 10,047 hrs · 15,324 cycles
LIFE VEST SEATS 11A AND 11B MISSING. PASSENGER LIFE VEST STRAPS MISSING AT SEATS 11A AND 11B. (P/N 1003118-009) INSTALLED LIFE VESTS IAW AMM 25-61-03. DEFERRED PASSENGER LIFE VESTS AT SEATS 11A AND 11B IAW MEL 25-64-01 PER MOC. DO NOT OCCUPY SEAT" COVERS AND PLACARD INSTALLED.
2012
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,951 hrs · 6,289 cycles
RBL 12 FLOORBEAM CRACKED FORWARD OF FS 280 IS CRACKED. REPAIRED IAW REO 690-53-11-407.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,951 hrs · 6,289 cycles
LBL 12 FLOORBEAM CRACKED FORWARD OF FS 280 IS CRACKED. REPAIRED IAW REO 690-53-11-407.
Part: CONTAINER — TORN (LIFE VEST) · airframe 8,951 hrs · 6,289 cycles
FORWARD FLIGHT ATTENDANTS LIFE VEST BAG TORN. REMOVED AND REPLACED FLIGHT ATTENDANTS LIFE VEST IAW AMM 25-61-03.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,762 hrs · 5,376 cycles
WORKING DM# 58045 NR 3 LT EXT OVERWING EMERGENCY LIGHT INOP. WORKING DM# 58045. REMOVED AND REPLACED NR 4 BATTERY PACK IAW CRJ900 AMM 33-51-17. OPS CHECK GOOD, OK FOR SVC. DM CLEARED PLACARD REMOVED. PART EFFECTIVITY VERIFIED.
2011
Part: BUSHING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 7,467 hrs · 5,209 cycles
THE HORIZONTAL HINGE PIN BUSHING AND HINGE PIN WERE FOUND CORRODED. REPAIRED IAW BOMBARDIER REO 690-55-11-006 REV C.
Part: HINGE PIN — CORRODED (HORIZ STAB) · airframe 7,467 hrs · 5,209 cycles
DURING A 3FH8 INSPECTION DAMAGE WAS FOUND TO THE HORIZONTAL STAB HINGE FITTING (RT O/B). HEAVY CORROSION (RUST) WAS FOUND ON THE HINGE PIN BUSHING AND HINGE PIN. IT APPEARS AS IF THE HINGE PIN AND BUSHING HAVE SEIZED TOGETHER AND AS THE STABILIZER WAS ACTUATED IN FLIGHT THE ANTI-ROTATION TAB OF THE PIN AND BUSHING HAVE GOUGED THE ANTI-ROTATION TANG OF THE HINGE FITTING. THE ANTI-ROTATION TANG IS 1 & 3/16" LONG AND 7/32" DEEP, THE GOUGED AREA IS 7/8" LONG AND IS 7/32" DEEP AT ITS MAXIMUM POINT. REPAIRED RT HORIZONTAL STAB ANTI ROTATION TAB IAW REO 690-55-11-005. GOOD FOR 5000FH FROM TIME OF REPAIR. SEE REO 690-55-11-005 FOR EXTENSIONS AS NEEDED. REINSPECT TABS AT EVERY SUBSEQUENT 2000FH.
Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 6,929 hrs · 4,796 cycles
GEAR DISAGREE REMOVED & REPLACED LANDING GEAR SELECTOR VALVE PER FIM 32-31-00 REF CRJ 900 AMM 32-32-10, VERIFIED PART EFFECTIVITY. GEAR DID NOT COME DOWN ON ITS OWN, EMERGENCY EXTENSION HANDLE WAS PULLED FOR SUCCESSFUL GEAR EXTENSION.
Part: ANTI-ICE VALVE — MALFUNCTIONED (LEFT) · airframe 6,377 hrs · 4,433 cycles
LT BLEED CAUTION MSG/SLATS HALF SPEED. REMOVED AND REPLACED ANTI ICE COWL VALVE IAW AMM 30-22-01 OP/C GOOD.