N298PQ
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.
70 reports on file, 2014-12-31 – 2023-12-26.
Part: HINGE — CORRODED (PAX DOOR STEP) · airframe 22,324 hrs · 16,877 cycles
PAX DOOR TOP FOLDING STEP HINGE IS CORRODED. REMOVED CORRODED HINGE, LOCATED AND DRILLED NEW HINGE IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW HINGE AS NEEDED IAW CRJ 900 AMM 52-11-04-400-801 STEP (4) (A) (3 & 4). HINGE PN# CC670-31981-3.
Part: BRACKET — CRACKED (PAX DOOR) · airframe 22,324 hrs · 16,877 cycles
PAX DOOR AFT GAS SPRING BRACKET CRACKED. REMOVED PAX DOOR AFT GAS SPRING BRACKET P/N 601R318011-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. INSTALLED AFT GAS SPRING BRACKET WITH P/N 601R318011-1 AT PAX DOOR IAW CRJ900 SRM 51-42-06-001-001-A01.
Part: HANDLE — CRACKED (ZONE 800) · airframe 22,324 hrs · 16,877 cycles
PAX DOOR INNER HAND LEVER (P/N 600-31887-15) CRACKED. EVAL. PAX DOOR INNER HAND LEVER (P/N 600-31887-15) FOUND TO BE CRACK ORDER REPLACEMENT HANDLE IAW CRJ900 IPC 52-11-02 FIG 5 ITEM 242REMOVED INNER HANDLE ASSEMBLY IAW CRJ-900 AMM 52-11-02-000-809 (CONFIG. A02). LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER HANDLE AS REQUIRED IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-43-00-001-001-A01. INSTALLED NEW PAX DOOR INNER HANDLE PN 600-31887-15 IAW CRJ900 AMM 52-11-02-400-809-A02.OPS TEST GOOD IAW CRJ 900 AMM 52-11-00-710-801-A01.) FOUND TO BE CRACK ORDER REPLACEMENT HANDLE IAW CRJ900 IPC 52-11-02 FIG 5 ITEM 242REMOVED INNER HANDLE ASSEMBLY IAW CRJ-900 AMM 52-11-02-000-809 (CONFIG. A02). LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER HANDLE AS REQUIRED IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-43-00-001-001-A01. INSTALLED NEW PAX DOOR INNER HANDLE PN 600-31887-15 IAW CRJ900 AMM 52-11-02-400-809-A02.OPS TEST GOOD IAW CRJ 900 AMM 52-11-00-710-801-A01.
Part: STRINGER — CORRODED (UNKNOWN) · airframe 22,324 hrs · 16,877 cycles
FOUND CORROSION ON STGR 20R BETWEEN F.S 379-394 REMOVED DAMAGED STR 20R BETWEEN FS 349 TO FS 477 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW STR 20R BETWEEN FS 349 TO FS 477 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW STR 20R BETWEEN FS 349 TO FS 477 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 P/N SH670-31405-2S REMOVED STRINGER CLEATS FROM STA 349-454 AT STRINGER 20R TO ACCESS THE REMOVAL OF THE STRINGER AND REMOVED THE SKIN RIVETS IAW CRJ900 SRM 51-42-06-001-001-A01 INSTALLED STRINGER CLEATS BETWEEN FS349 AND FS454 AT STR20R IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED SUPPORT ANGLE FOR ACCESS LOCATED AT STR 20R AND BETWEEN FS 437 TO FS 453 IAW CRJ-900 SRM 51-42-13-001-001-A01 INSTALLED SAME SERVICEABLE SUPPORT ANGLE LOCATED AT STR 20R AND BETWEEN FS 437 TO FS 453 IAW CRJ-900 SRM 51-42-13-001-001-A01
Part: ANGLE — CORRODED (UNKNOWN) · airframe 22,324 hrs · 16,877 cycles
"PASSENGER DOOR SURROUND STRUCTURE, MID CAP ANGLE IS CORRODED. REMOVED PASSENGER DOOR SURROUND STRUCTURE, MID CAP ANGLE P/N SH670-31825-9 IAW CRJ900 SRM 51-41-02-001-001-A01.AND LOCATED, DRILLED , AND INSTALLED PASSENGER DOOR MID CAP ANGLE P/N SH670-31825-9 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND 51-41-02-001-001-A01. "
Part: FLOOR SUPPORT — CRACKED (BS 169) · airframe 22,324 hrs · 16,877 cycles
"FWD EQUIPMENT COMPARTMENT RH FLOOR CRACKED AT FS 169. PERFORMED REPAIR TYPE 2, ON R/H SIDE OF FWD EQUIPMENT COMPARTMENT IAW CRJ-900 SRM 52-11-43-201-001-A01, STEP 4.A(2)(G -K), DOUBLER PO# 5-5403, 0.040ÿ½, CLEAT PO# W89584, 0.032ÿ½. INSTALLED DOUBLER PO# 5-5403, 0.040"", AND CLEAT PO# W89584, 0.032"". IAW CRJ-900 SRM 53-11-43-201-001-A01 STEPS L-N. INSTALLED PLACARD 600-90862-1 IAW CRJ-900 SRM 51-42-06-001-001-A01."
Part: FLOOR PANEL — CRACKED (UNKNOWN) · airframe 22,324 hrs · 16,877 cycles
FWD EQUIPMENT COMPARTMENT LH FLOOR CRACKED AT FS 193.00. REPAIRED IAW CRJ900 SRM 53-11-43-201-001-A01.
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 22,324 hrs · 16,877 cycles
LH AFT DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED. : REMOVED LH AFT DRAG ANGLE FROM VERTICAL STABILIZER IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, & 51-42-22-001-001-A01. AND FIT, DRILLED AND TRANSFERED HOLES INTO NEW ANGLE IAW CRJ900 SRM 51-40-11-001-001-A01.AND THEN COUNTERSUNK AND INSTALLED NEW AFT DRAG ANGLE P/N AV670-21186-003, ON VERTICAL STABILIZER IAW CRJ-900 51-42-10-001-001-A01, 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.AS WELL AS SEALED AND PAINTED IAW CRJ-900 SRM 51-22-00-001-001-A01 51-25-01-001-001-A01
Part: ANGLE — CRACKED (UNKNOWN) · airframe 22,324 hrs · 16,877 cycles
LH FWD DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED. PERFORMED PERMANENT REPAIR OF LH FWD DRAG ANGLE ON VERTICAL STAB IAW CRJ900 SRM TASK 55-31-00-201-001-A01.
Earlier reports · 2014–2020 · 61 reports
2020
Part: ACCESS PANEL — WORN (WING) · airframe 15,120 hrs · 10,586 cycles
"PART RACKS:WEAR ON ACCESS PANEL 521AT, 622DB, 622CB, 584JB,584EB, 584LB, 684GB, 684JB,684EB,584AB AND 584GB. (SM) ""SUMMARY: OF NRC. 00246. WEAR ON ACCCESS PANELS 521AT, 622DB, 622CB, 584JB, 584LB, 684GB, 684JB,584AB AND 584GB WERE MEASURED AND FOUND WITHIN LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01. WEAR ON ACCESS PANEL 584EB AND ACCESS PANEL 684EB WERE MEASURE AND FOUND OUT OF LIMITS PER CR "
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS=310 BTW STGR 25LH / 25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY: ON NRC. 00266 CORROSION LEVEL 2. FRAME FS=310 BTW STGR 25RH/25LH WAS REPAIRED PER EA NO: CRJ953-10346 REV. IR "
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS=295 BTW STGR 25LH / 25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). ""SUMMARY: ON NRC. 00264 CORROSION LEVEL 2. FRAME FS=295 BTW STGR 25LH / 25RH WAS REPAIRED PER CRJ-900 EA CRJ953-10345 REV. IR "
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: DAMAGE FLOOR PANELS 282FRF, 281CLF, 281GLF AND 281DLF AT AFTER CARGO COMPARTMENT. " "SUMMARY: FLOOR PANEL 281CLF P/N: BA670-31684-7 WAS VERIFIED AND REPLACED PER CRJ 900 IPC 53-00-47 ITEM 55A, FLOOR PANEL 282FRF P/N: BA670-31683-7 WAS VERIFIED AND REPLACED PER CRJ 900 IPC 53-00-47 ITEM 40B, FLOOR PANEL 281GLF AND 281DLF AT AFTER CARGO COMPARTMENT WERE REPAIRED PER CRJ 900 CMM ATA 53 COMCMM-030 REV. T "
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: DELAMINATED FLOOR PANEL 281BLF AT AFTER CARGO COMPARTMENT. " "SUMMARY: FLOOR PANEL 281BLF AT AFT BAGGAGE BAY ARE OUT OF LIMITS WITH DIMENSION 152IN^2 PER CRJ 900 CMM ATA 53 COMCMM-030 REV. T PAR. 8.0 THEREFORE WAS REPLACED PER CRJ 900 AMM 53-00-47 "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON INTERCOSTAL BTW STGR 20RH AND FS=349 / FS=319 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). ""SUMMARY: INTERCOSTAL BTW STGR 20RH AND FS=349 / FS=319 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON INTERCOSTAL (2EAS) BTW FS=349 / FS=364 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). " "SUMMARY: ON NRC. 00275 CORROSION LEVEL 2. INTERCOSTAL (2EAS) BTW FS=349 / FS=364 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 " SH670-32075-3
Part: RUB STRIP — TORN (VERTICAL STAB) · airframe 15,120 hrs · 10,586 cycles
"PART RACKS : TORN AND LOOSE TEFLON STRIP AT VERTICAL STABILIZER ACCESS PANEL NBR , 326DL , AND 326DR ( SM ) " "SUMMARY: NEW STRIPS, RUBBER, UPPER VISOR ACCESS PANEL 326DL AND 326DRWERE INSTALLED PER CRJ/900 SRM 51-42-06-001-001-A01. "
Part: GRILL — CRACKED (CARGO BAY) · airframe 15,120 hrs · 10,586 cycles
"PART RACKS: CRACKED CHIMNEY GRILLS (3 E/A) AT FWD CARGO COMPARTMENT. " "SUMMARY: OF NRC:00421; CHIMNEY GRILLS (2 E/A´S) WERE VERIFIED AND REPLACED PER CRJ-900 IPC 53-32-31-01 ITEM: 270 P/N: A843021-501 AND ITEM: 300 P/N: A843021-505, AND CRACKED CHIMNEY GRILL (1 E/A) ITEM:330 P/N:A843021-507 WAS REPAIRED PER REO 670-53-32-004 REV. -D REPAIR 1. "
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: DELAMINATED FLOOR PANEL 252DRF AT PAX CABIN. " "SUMMARY: FLOOR PANEL 252DRF AT AFT BAGGAGE BAY ARE OUT OF LIMITS WITH DIMENSION 149IN^2 PER CRJ 900 CMM ATA 53 COMCMM-030 REV. T PAR. 8.0 THEREFORE WAS REPLACED PER CRJ900 AMM 53-00-47-400-802. A14 "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STGR 26RH BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304) ""SUMMARY OF NRC:00262 CORROSION LEVEL:2 ON STGR 26RH BTW FS=280 / FS=333, STRG 26 RH BTW FS=280 / FS=333 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01. "
Part: COVER — DENTED (PAX DOOR) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: DENT ON FWD/AFT LOWER CORNERS AT PASSENGER DOOR (PTAS). " "FWD/AFT LOWER CORNERS AT PASSENGER DOOR WERE REPLACED PER CRJ-900 SRM51-42-10-001-001-A01 "600-31902-288
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS=319 BTW STGR 25LH / 24RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY OF NRC 00267 CORROSION LEVEL 2:FRAME FS=319 BTW STGR 25LH / 23RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ/900 SRM 53-00-06-201-006-A01 FIG. 53-00-06-995-825 AND 51-42-06-001-001-A01 "
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS=349 BTW STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). " "SUMMARY: FRAME FS=349 BTW STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. "
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: OF NRC:00213 CORROSION LEVEL 2. ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. ANGLE MOUNTING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: STRIKER — NICKED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: NICK ON EDGE TO FS169.00 STRUCTURE NEAR TO WL79.50 AT LH FWD EQUIPMENT (FUS) " "SUMMARY: ON NRC. 00155 SEAL STRIKER WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. "
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON DOUBLER BTW FS=295 / FS=310 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY ON NRC 00265: CORROSION LEVEL 2. DOUBLER BTW FS=295 / FS=310 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER 51-42-06-001-001-A01 "
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CRACK IN BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE. (FUS) (SM) " "SUMMARY: ON NRC. 00010 BOX AT A/C EXTERNAL POWER RECEPTACLE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: STRIKER — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: ON NRC. 00212 STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: STRIKER — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: ON NRC. 00212 STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON ANGLES (4 E/A) OF SUPPORTS PROTECTORPLATE LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. ""SUMMARY: ON NRC. 00214 ANGLES (4 E/A) OF SUPPORTS PROTECTOR PLATE LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY OF NRC 00263: DUE CORROSION LEVEL 2 ON STGR 27 BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT IT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6C AND SRM 51-42-21-001-001-A01 PAR. 6C "
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS=333 / FS=364 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305) " "SUMMARY OF NRC 00273: DUE CORROSION LEVEL 2 ON STGR 27 BTW FS=333 / FS=364 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT IT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 "
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"AWR: HIDDEN DAMAGE; AFTER REMOVAL THE FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON CROSSBEAM FS280 BTW BL0/RBL12 IN REF NRC: 00198 (SM) ""SUMMARY OF NRC 00306: DUE CORROSION LEVEL 2 ON CROSSBEAM FS280 BTW BL0/RBL12 IT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, 51-42-13-001-0001-A01 AND 51-42-21-001-001-A01 "
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"AWR: HIDDEN DAMAGE; AFTER REMOVAL THE FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON CROSSBEAM FS280 BTW BL0/LBL12 IN REF NRC: 00198 (SM) " "SUMMARY OF NRC 00304: DUE CORROSION LEVEL 2 ON CROSSBEAM FS280 BTW BL0/LBL12 IT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, 51-42-13-001-0001-A01 AND 51-42-21-001-001-A01 "
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON STGR 21RH BTW FS=333 / FS=379 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305) ""SUMMARY OF NRC:00280 CORROSION LEVEL:2 ON STGR 21RH BTW FS=333 / FS=379 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT, STRINGER 21 RH FS=333 / FS=379 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. "
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=379.00 / FS=699.40 AND STGR 15LH (CPAX) (SM) (TCI:53-20-217). " "SUMMARY: ON NRC. 00201 CORROSION LEVEL 2. SIDE SEAT RAILS BTW FS=379.00 / FS=699.40 AND STGR 15LH WERE REPLACED PER CRJ/900 AMM 53-00-49 (CONFIG 12) "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND LBL 9. (CPAX) (SM) (TCI:53-20-245). ""FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND LBL 9 WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12). "
Part: LENS — ERODED (NAV LIGHT) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION : EROSION ON NAVIGATION LIGHT LENS AT LH WING ( AI) " "SUMMARY OF NRC S/N 00059: NAVIGATION LIGHT LENS AT LH WING WAS REPLACED PER CRJ-900 A.M.M 57-32-39. TOOL USED TORQUE P/N: QDRIVER4 S/N:1018403869 D/D:01-MAY-20 C/N:2474 "
Part: STRIKER — WORN (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: WEAR ON FWD/CENTER SEAL STRIKER AT MIDDLE BAGGAGEBAY DOOR CUT OUT (CCD) " "SUMMARY: ON NRC. 00130, STRIKER AT MIDDLE BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01 PAR 6.A AND CRJ/900 SRM 51-42-06-001-001-A01 PAR 6.A "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15RH (CPAX) (SM) (TCI:53-20-233). " "SUMMARY: ON NRC. 00200, CORROSION LEVEL 2. SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15RH, WERE REPLACED PER CRJ/900 AMM 53-00-49-400-801 (CONF. A12) "
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15LH (CPAX) (SM) (TCI:53-20-233). " "SUMMARY OF NRC 00199, CORROSION LEVEL 2: NEW SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15LH, WERE REPLACED PER CRJ/900 AMM 53-00-49 CONFIG. (A12) "
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CRACK ON EGDE TO THE SUPPORT OF THE JUNCTION BOX 6 AT RH FWD EQUIPMENT (FUS) " "SUMMARY: ON NRC. 00156 SUPPORT OF THE JUNCTION BOX 6 AT RH FWD EQUIPMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND RBL 9. (CPAX) (SM) (TCI:53-20-245). ""SUMMARY: ON NRC 00206 CORROSION LEVEL 2. FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND RBL 9 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801(CONF. A12). "
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND RBL 9. (CPAX) (SM) (TCI:53-20-243). ""SUMMARY OF NRC 00204 CORROSION LEVEL 2:SEAT RAILS BTW FS=349.00 / FS=477.40 AND RBL 9.WERE REPLACED PER CRJ 900 AMM 53-00-49 (CONF.A12) "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL BTW FS=485 / FS=533 AND LBL 27. (CPAX) (SM) (TCI:53-20-245). " "SUMMARY OF NRC 00207 CORROSION LEVEL2:FLOOR SEAT RAIL BTW FS=485 / FS=533 AND LBL 27.WAS REPACED PER CRJ-900 AMM 53-00-49 (CONFIG.A12) "
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND LBL 9. (CPAX) (SM) (TCI:53-20-243). " "SUMMARY OF NRC 00203 CORROSION LEVEL 2:FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND LBL 9.WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG.A12) "
Part: PLATE — BENT (CARGO DOOR) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: BENT AND WEAR ON LOWER PLATES AT FWD/CENTER BAGGAGE BAY DOOR (CCD) " "SUMMARY: ON NRC. 00129 LOWER PLATES AT FWD/CENTER BAGGAGE BAY DOOR WERE REPLACED PER CRJ-900 AMM 52-35-07-400-802 (CONF. 02) "
Part: RETAINER — BENT (CARGO DOOR) · airframe 15,120 hrs · 10,586 cycles
"INITIAL INSPECTION: WEAR ON LOWER PRESSURE SEAL RETAINERS FWD/AFT CORNER AT FWD/CENTRAL BAGGAGE BAY DOOR (CCD) ""LOWER (PRESSURE SEAL) RETAINERS AT FWD AND CENTRAL BAGGAGE BAY DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
2017
Part: OXYGEN MASK — BROKEN (CABIN) · airframe 9,790 hrs · 6,723 cycles
FLIGHT ATTENDANT O2 MASK BROKEN. GAVE MASK TO FA AS REQUIRED.
Part: ACM — FAILED (RIGHT) · airframe 9,428 hrs · 6,468 cycles
FA REPORTED A BURNING ODOR IN THE CABIN. RT PACK AUTOFAIL MESSAGE. SMOKE/HAZE THROUGHOUT CABIN. SHUTDOWN THE RT PACK AND APU. FOUND THE RT PACK FAILED. REMOVED AND REPLACED THE RT ACM IAW 21-51-08. OPS CHECKED GOOD.
Part: LIGHT — BROKEN (ROW 13B) · airframe 9,423 hrs · 6,462 cycles
EMERGENCY LIGHT AT 13B BROKEN. REMOVED AND REISTALLED THE EMERGENCY LIGHT IAW AMM 33-51-01. NO OTHER DEFECTS AT THIS TIME.
Part: FLASHLIGHT — MISINSTALLED (MAIN CABIN) · airframe 9,058 hrs · 6,194 cycles
FORWARD FLIGHT ATTENDANTS FLASHLIGHT IS INSTALLED BACKWARDS MAKING PREFLIGHT CHECK IMPOSSIBLE. REPLACED THE FLASHLIGHT WITH SERVICEABLE UNIT OK FOR SERVICE IAW AMM 25-61-02-400-801, CONFIG A-10.
Part: FLASHLIGHT — INOPERATIVE (GALLEY) · airframe 8,853 hrs · 6,042 cycles
FLASHLIGHT BY GALLEY DOOR INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-00.
Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 7,697 hrs · 5,261 cycles
FLASHLIGHT AT SERVICE DOOR ENTRY IS INOP. PERFORMED OPS TEST OF FLASHLIGHT IN ENTRANCE COMPARTMENT AND FOUND BATTERY TO BE DISCONNECTED. RE-PERFORMED OPS CHECK IAW AMM TR 25-0788, 25-61-00. OPS CHECK GOOD AFTER CONNECTION.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,697 hrs · 5,261 cycles
RT FS280 BULKHEAD LOWER WEB CORRODED AT THE RT FLOOR SILL. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10. REPAIRED RT FS280 BULKHEAD LOWER WEB IAW REO 670-53-11-594 REV A.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 7,697 hrs · 5,261 cycles
RT FLOOR SILL CORRODED AT THE FS280 CROSSBEAM. REPAIRED RT FLOOR SILL AT FS 280 CROSSBEAM IAW REO 670-53-21-139 REV A.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,697 hrs · 5,261 cycles
FS280 CROSSBEAM UPPER FLANGE CORRODED AT THE R/H FLOOR SILL. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED RT 280 CROSSBEAM IAW SRM 51-42-06 AND REO 670-53-11-594 REV A.
Part: WEB — CRACKED (PAX DOOR) · airframe 7,697 hrs · 5,261 cycles
PAX DOOR 2ND STEP FROM THE TOP AFT SIDE OF THE SKIN IN THE RADIUS AREA IS CRACKED A250-013. REPAIRED CRACKED ON AFT RISER WEB IAW SRM 52-11-04, TR 52-0025.
Part: PBE — UNSERVICEABLE (CABIN) · airframe 7,697 hrs · 5,261 cycles
FWD LT ATTEND SEAT PBE BAG VACUUM SEAL BROKEN. REMOVED & REPLACED FWD LT F/A PBE IAW AMM 35-31-06-000-801/ 35-31-06-400-801.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,697 hrs · 5,261 cycles
PAX DOOR AFT SIDE JUST ABOVE THE PULLEY ASSY ON THE DRAG ANGLE AREA IS CRACKED. REPAIRED IAW SRM 52-11-04 TR 52-0026.
2016
Part: STRAP — DETACHED (FLASHLIGHT) · airframe 7,368 hrs · 5,024 cycles
FWD FA FLASHLIGHT STRAP NOT ATTACHED. SECURED FLASHLIGHT STRAP NEAR FWD FA SEAT AS REQUIRED.
Part: COOLING FAN — FAULTY (COCKPIT) · airframe 6,218 hrs · 4,198 cycles
DISPLAY COOL CAUTION CAME ON IN FLIGHT, COULD SMELL AN ELEC SMELL PRIOR & QUICKLY DISSIPATED. CHECKLIST PERFORMED & IT WENT OUT. DEFERRED DISPLAY COOLING FAN NR 1, BREAKER CBP1-U2 DEACTIVATED IAW MEL 21-24-2. DISPLAY CHECK VLV VERIFIED OPERATIVE IAW MX PROCEDURES. INFORMED FLIGHT CREW OF NEW PROCEDURES TO USE IAW MEL 21-24-2. PLACARD INSTALLED & MM02 UPDATED. R & R DISPLAY COOL FAN COCKPIT IAW AMM 21-24-12. OPERATIONS CHECKED GOOD. REMOVED FROM MM02. THIS CLEARS MM02 3317672-1. PLACARD REMOVED.
Part: LIGHT — MISSING (CABIN) · airframe 6,083 hrs · 4,109 cycles
EMERGENCY FLOOR TRACK LIGHT MISSING AT 13B. INSTALLED FLOOR TRACK LIGHT IAW AMM 33-51-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 5,654 hrs · 3,822 cycles
FLOOR LUMINESCENT TAPE IN FRONT OF SEAT 12B CAME UP. SECURED FLOOR TRACK LIGHTING IN FRONT OF SEAT 12B, REF 33-51-01.
Part: FLAP — MALFUNCTIONED (WING) · airframe 5,310 hrs · 3,605 cycles
WHILE AT FLAPS 8, WHEN FLAPS 20 SELECTED, FLAPS FAILED, CAUTION MSG ABNORMAL. CHECKLIST COMPLETED. COMPLETED FLAPS OPERATIONAL CHECK IAW AMM 27-52-00. OPERATIONS CHECKED GOOD. COMPLETED GVI NO DEFECTS NOTED AT THIS TIME.
2015
Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 4,663 hrs · 3,186 cycles
EN-ROUTE HYD 3 HI TEMP CAUTION POSTED, RAN NON-NORMAL CHECKLIST, SYS 3 PSI DROPPED TO 0 PRIOR TO LANDING. TURNED 3A 3B ON IAW NON-NORMAL CHECKLIST & PSI BACK TO NORMAL. R & R NR 3 HYD RESERVOIR IAW AMM 29-12-30. OPERATIONS & LEAK CHECKED GOOD AT THIS TIME. HYD PRESS & TEMP REMAINED ON NORMAL RANGE. SEE NON-ROUTINE CARD 532062 FOR WORK PERFORMED. ACFT OF FOR SERVICE AT THIS TIME, PN ON OFF 960450-1 SN OFF 807 SN ON 0028.
Part: UNKNOWN — ODOR (CABIN) · airframe 3,710 hrs · 2,506 cycles
ON DESCENT, THROUGH 3700 FEET, BOTH FLIGHT ATTENDANTS & SEVERAL FWD PAXS NOTED A STRONG BURNING SMELL FROM ROW 12, FWD TO THE GALLEY. NO INDICATIONS IN THE COCKPIT & NO ABNORMAL CONDITIONS WERE NOTED BY THE FLIGHT ATTENDANT`S. FLIGHT ATTENDANT`S REPORT THAT OVEN COFFEE POTS FWD LAVATORY & GALLEYS WHERE NOT THE SOURCE. COMPLETED ABNORMAL SMELL IN PAX CABIN INSPECTION, NO DEFECTS NOTED AT THIS TIME IAW AMM 21-22-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 3,286 hrs · 2,207 cycles
FLASHLIGHT AT SERVICE DOOR IS NOT BLINKING. DEFERRED AFT FLASHLIGHT IAW MEL 25-61-4A ENTERED INTO MMO2 & PLACARD INSTALLED. REPLACED GALLEY FLASHLIGHT BATTERY IAW AMM 25-60-00. PLACARD REMOVED, THIS CLEAR MEL 25-61-4A & CLEARED FROM MMO2.
Part: FLASHLIGHT — NONE (CABIN) · airframe 3,181 hrs · 2,138 cycles
CREW REPORTED FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. NO DEFECTS NOTED. OPERATIONS CHECKED GOOD IAW 25-60-02.
2014
Part: LIGHT — UNSECURE (CABIN) · airframe 2,685 hrs · 1,787 cycles
EMERGENCY LIGHT IN GALLEY UNSECURE. SECURED THE LIGHT.