N205FR
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.
27 reports on file, 2012-05-19 – 2022-02-25.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124-1001 UPON L/H DOOR SIL REMOVAL, CORROSION FOUND ON FR68. L/H LOWER CORNER FITTING. CORRECTIVE ACTION: REMOVED AND REPLACED CORNER FITTING L/H FR68 IAW A320 SRM 51-72-11./END/
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124.0438 AFT CABIN UNDERNEATH FLOOR BOARDS, R/H SIDE AT FR68 FLOOR BEAM Y765 HAS DEEP SURFACE CORROSION CORRECTIVE ACTION: REMOVED AND REPLACED Y765 FLOOR BEAM @ FR68 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124.0428 AFT CABIN UNDERNEATH FLOOR BOARDS, L/H SIDE AT FR68 FLOOR BEAM Y765 HAS DEEP SURFACE CORROSION CORRECTIVE ACTION: REMOVED AND REPLACED Y765 FLOOR BEAM @ FR68 IAW A320 SRM 51-72-11
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124-0441. AFT CABIN UNDERNEATH FLOOR BOARDS, R/H SIDE, AT FR66 THRESHOLD FWD I/B END HAS CORROSION AT ATTACHMENT HOLE. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN R/H SIDE DOOR SILL BEAM IAW A320 SRM 53-41-14-283-002 AND SRM 51-72-11./END/
Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124.0427 AFT CABIN UNDERNEATH FLOOR BOARDS, L/H SIDE AT FR68 AFT THRESHOLD AFT OF GIRT BAR FITTING, THRESHOLD CORRODED IN CORNER AREA CORRECTIVE ACTION: REPLACED DOOR SEAL BEAM IAW A320 SRM 51-72-11
Part: FLOORBEAM — DAMAGED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124.0424 L/H AFT CABIN, BELOW FLOORBOARDS BETWEEN FR68 AND FR69, FLOOR BEAM AT Y1292 HAS A HOLE DAMAGE IN TOP SURFACE CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM STA Y1292 FR68 IAW A320 SRM 51-72-11
Part: PLATE — CRACKED (ZONE 100) · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124.0423 L/H AFT CABIN, BELOW FLOORBOARDS BETWEEN FR68 AND FR69, FRAME SHEAR PLATE CRACKED ALMOST ALL THE WAY ACROSS ABOUT 6 INCHES CORRECTIVE ACTION: REMOVED AND REPLACED SHEET (WEB) @ FR68 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R 12124.0350 FWD CABIN FLOORBEAM Y254 CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION: REMOVED AND REPLACED Y254 FLOORBEAM @FR12 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
SUPPLEMENTAL CORRECTION FOR N/R #: REFERENCE PEMCO N/R 12124.0353 FWD CABIN FLOORBEAM Y-1292 CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION: REMOVED AND REPLACED Y-1292 FLOORBEAM @ FR12 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R 12124.0347 FWD CABIN FLOORBEAM Y1292 CORRODED BETWEEN FR 12-FR-16 CORRECTIVE ACTION: REMOVED AND REPLACED Y1292 FLOORBEAM @FR12 IAW A320 SRM 21-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R 12124.0349 FWD CABIN FLOORBEAM Y503.2 CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION: REMOVED AND REPLACED Y503.2 FLOORBEAM @FR12 IAW A320 SRM 51-72-11
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R# 12124-0353. FWD CABIN FLOORBEAM Y-1292 CORRODED BETWEEN FR12-FR16. CORRECTIVE ACTION: REMOVED AND REPLACED Y-1292 FLOORBEAM @ FR12 IAW A320 SRM 51-72-11./END/
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R 12124.0348 FWD CABIN FLOORBEAM Y765 CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION: REMOVED AND REPLACED Y765 FLOORBEAM @FR12 IAW A320 SRM 51-72-11
Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,220 hrs · 17,129 cycles
DISCREPANCY: REFERENCE PEMCO N/R 12124.0421 L/H AFT CABIN, BELOW FLOORBOARDS BETWEEN FR 69 AND FR 70, SHEAR WEB PLATE HAS DEEP SURFACE CORROSION AT AFT END CORRECTIVE ACTION: REMOVED AND REPLACED SHEAR WEB @ FR 69 L/H AFT CABIN IAW A320 SRM 51-72-11
Earlier reports · 2012–2021 · 13 reports
2021
Part: BATTERY — DISCHARGED (ZONE 200) · airframe 40,162 hrs · 16,650 cycles
DISCREPANCY: REFERENCE LP162374 ITEM 1, EPSU SYSTEM FAIL FLAGGING 10WL. CORRECTIVE ACTION: REMOVED AND REPLACED 10WL EPSU BATTERY. OPS CHECK GOOD AT THIS TIME REF AMM 33-51-38-04 CONF 00 .
Part: BATTERY — DISCHARGED (ZONE 200) · airframe 40,162 hrs · 16,650 cycles
DISCREPANCY: REFERENCE LP162374 ITEM 2, EPSU SYSTEM FAIL FLAGGING 12WL. CORRECTIVE ACTION: REMOVED AND REPLACED 12WL EPSU BATTERY. OPS CHECK GOOD AT THIS TIME. REF AMM 33-51-38-04 CONF 00 .
2020
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 36,857 hrs · 15,026 cycles
OPEN FASTNER HOLE CRACK INDICATION, FR36 HOLE #9, Y+1294, AFT ORIENTATION. CORRECTIVE ACTION: CRACK REMOVED BT REPAIR CUTOUT ON TASK CARD A0-53EO-3420-TASK.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 36,857 hrs · 15,026 cycles
OPEN FASTNER HOLE CRACK INDICATION, FR36 HOLE # 7, Y+1297, AFT ORIENTATION. CORRECTIVE ACTION- CRACK REMOVED BT REPAIR CUTOUT ON TASK CARD AO-53E0-3420-TASK.
2018
Part: UNKNOWN — ODOR (CABIN) · airframe 31,348 hrs · 12,654 cycles
PILOT REPORTED A WET SOCK ODOR IN THE ACFT WHEN FIRST WALKED ON, BURNING EYES. MAINTENANCE PERFORMED TSM 05-50-00-810-831-A. PERFORMED APU INSPECTION IAW AMM 49-00-81-810-874-A, HYDRAULIC SYS INSPECTION IAW AMM 29-00-00-790-001-A, AND INSPECTED PACKS 1 & 2 . NO DEFECTS NOTED. NO FURTHER ODORS FOUND DURING APU AND PACK OPERATION. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 31,218 hrs · 12,598 cycles
DURING FLIGHT, HAD A ODOR IN THE CABIN. NR 1 PACK 1 WASS SUSPECTED. FOLLOWED QRH AND VOL. II PROCEDURES. ODOR IN AFT GALLEY MOSTLY DESCRIBED AS A ROTTEN EGG AND ACETONE TYPE ODOR. THE ODOR LEANS TO THE NR 2 ENGINE AND NR 2 PACK. NR 2 ENGINE BORESCOPED. PERFORMED TSM 71-00-00-810-802-A THRU STEP (4) NO OIL WETTING PRESENT. NR 1 AND 2 PACKS RAN WITH BOTH ENGINES AND APU, NO ODOR OR DEFECTS NOTED IAW AMM 21-58-00-710-002 A.
Part: UNKNOWN — ODOR · airframe 30,890 hrs · 12,452 cycles
CREW REPORTS STRONG ODOR AFTER TURNING ON PACKS POST TAKE OFF. CREW DECLARED EMERGENCY, DAWNED O2 MASK, FOLLOW QRH AND RETURNED TO THE FIELD AND COMPLETED AN OVERWEIGHT LANDING WITH NO OTHER ISSUES. MAINTENANCE PERFORMED TROUBLESHOOTING ON ENG 1 AND ENG 2. COMPLETED MIN IDLE CHECKS FOR TYPE 2 CAUSE OF CABIN ODORS. BORESCOPE ON BOTH ENGINES NORMAL AND NO ABNORMAL ODORS NOTED REF TSM 05-50-00-810-831-A. AIRCRAFT WAS RETURNED TO SERVICE.
2017
Part: BOTTLE — OUT OF RIG (ZONE 800) · airframe 28,502 hrs · 11,457 cycles
DEPLOY R1 DOOR SLIDE, DUE TO INABILITY TO INSTALL PIN FOR INFLATION BOTTLE. SLIDE REPLACED ON PEMCO NR 1779N176. PERFORMED OPERATIONAL TEST OF ESCAPE SLIDE DEPLOYMENT IAW AMM 25-62-00-710-051-A TIME TO FULLY DEPLOY 8.32 SECONDS.
2016
Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 21,435 hrs · 8,676 cycles
DURING C CHECK INSPECTION, NOTED THE AFT WET AREA, LT CORNER, BETWEEN FRAME 69 & 70, LATERAL SHEAR PLATE CORRODED. REPLACED THE LT LATERAL SHEAR PLATE IAW SRM 51-74-00, SRM 51-44-11 & SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 21,435 hrs · 8,676 cycles
DURING C CHECK INSPECTION, NOTED THE AFT WET AREA RT CORNER, BETWEEN FRAME 69 & 70, LATERAL SHEAR PLATE CORRODED. REPLACED AFT WET AREA RT SHEAR PLATE, AT FRAME 69 - 70 IAW SRM 51-42-11.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 21,435 hrs · 8,676 cycles
DURING C CHECK INSPECTION, NOTED EMER LIGHT ON CEILING PANEL, ABOVE SEAT ROW 21 & 22 DOES NOT ILLUMINATE ON TEST. FOUND EMER LIGHT ON CEILING PANEL, ABOVE SEAT ROW 21 & 22 DISCONNECTED. RE-CONNECTED CONNECTORS IAW AMM 33-51-02. OPERATIONS CHECKED GOOD IAW AMM 33-51-11-400-01A.
2012
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,646 hrs · 2,927 cycles
AFT F/A SWIVEL SEAT FLASHLIGHT WILL NOT ILLUMINATE. ACFT WAS OUT OF SERVICE FOR ROUTINE OVERNIGHT MX. THE FLASHLIGHT WAS R & R IAW AMM 25-65-53 PB 401. THE NEW UNIT OPERATES NORMALLY.
Part: GIRT BAR — BINDING (R2 DOOR SLIDE) · airframe 7,487 hrs · 2,871 cycles
R2 GIRT BAR FALLS OPS TEST PROCEDURE, TELESCOPIC END DOES NOT MOVE FREELY IN THE GIRT BAR. REF TASK CARD C528001-08 STEP 4.B(1) R & R R2 ESCAPE SLIDE IAW TASK 2S-62-44-000-012-A. REMOVED DEFECTIVE GIFT BAR. INSTALLED R2 ESCAPE SLIDE IAW AMM 25-62-44-400-007-A WITH SERVICEABLE GIRT BAR. PERFORMED OPS CHECK IAW AMM 32-51-00-710-00 1-A. OPS CHECK GOOD.