N805WA
Registered owner: CARIBBEAN SUN AIRLINES INC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| World Atlantic Airlines | Operator | on 2025-08-23 | Operator named in NTSB report |
Accident & incident history
Operated by World Atlantic Airlines (per NTSB report)
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.
23 reports on file, 2013-12-27 – 2025-09-09.
Part: A/C PACK — NO DISCREPANCY (ZONE 200) · airframe 57,062 hrs · 32,610 cycles
BURNING SMELL REPORTED AFTER FLIGHT BY FLT ATTENDANTS SUSPECTED FROM LEFT PACK PER THEM. PERFORMED INSPECTION WITH L/H AND R/H A/C PACKS AND NO DISCREPANCY FOUND AS PER MD80 AMM 21-00-00: PERFORMED INSPECTION LEFT AND RIGHT ELECTRIC SYSTEMS NO DISCREPANCY FOUND AS PER MD80 AMM 24-20-00
Part: LIGHT — BURNED OUT (ZONE 200) · airframe 56,743 hrs · 32,309 cycles
LOW LEVEL EMERGENCY LIGHTS ON SEATS ROWS 21-32 BURNED OUT
Part: ACCESS PANEL — LEAKING (ZONE 600) · airframe 56,534 hrs · 32,084 cycles
DURING POSTFLIGHT INSP FUEL LEAKAGE WAS FOUND AT RIT TANK TOP SIDE
Part: VALVE — FAILED (ZONE 700) · airframe 56,336 hrs · 31,855 cycles
AFTER TAKEOFF AND RISING LANDING GEAR, THE LANDING GEAR'S RED NOSE LIGHT WAS NOT EXTINGUISHED.
Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 56,328 hrs · 31,846 cycles
CABIN DISCREPANCY REPORT (CDR) ROW 3 AND SERVICING EMERGENCY LIGHTS NOT WORKING ROW 21, 23 ISLE PATH LIGHTING NOT WORKING EXIT LIGHT OF L1, R1 AND L2.
Part: SKIN — DENTED (ZONE 200) · airframe 56,318 hrs · 31,835 cycles
THE L/H UPPER FUSELAGE BETWEEN STA-218 AND STA-237 HAS STRUCTURAL DAMAGE.
Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 56,275 hrs · 31,790 cycles
EMERGENCY LIGHTSAT L1 AND L2DOORS ARE INOP (NOT TESTING)
Part: CONTROL MODULE — INOPERATIVE (ZONE 200) · airframe 56,275 hrs · 31,790 cycles
EMERGENCY LIGHTS AT INBOARD OVERWING EXIT DOORS L/H AND R/H ARE INOP
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 56,275 hrs · 31,790 cycles
EMERGENCY LIGHTS AT CABIN AFT DOOR INOP
Part: CONTROL MODULE — FAILED (ZONE 200) · airframe 56,233 hrs · 31,741 cycles
EMERGENCY LIGHTS FWR EXIT LEFT AND RIGHT WERE FOUND VERY DIM. AFTER TROUBLESHOOTING THE MODULE CONTROL ASSY AB5-1 WAS REPLACED. THE OPERATIONAL TEST WAS FOUND NORMAL IAW MD-80 AMM 33-53-00.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 56,206 hrs · 31,714 cycles
EMERGENCY EXIT LIGHT INOP
Earlier reports · 2013–2024 · 12 reports
2024
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,410 hrs · 31,013 cycles
ON THE L1 DOOR JAMB THE EMERGENCY LIGHT LOCATED ON THE FRAME OF THE DOOR FAIL TEST PERFORMED DURING C-CHECK. REF. TASK CARD 53-200-05-01, WO 6549 CORRECTIVE ACION: REMOVED NAD REPLACE BATTERIES PACK L1 DOOR LAP EMERGENCY LIGHT I.A.W. MD80 AMM 33-53-00. PN: 10-0119-1 LIGHT ASSY-EMERGENCY PORTABLE (V729114).
2019
Part: WIRE — BROKEN (FIRE LOOP) · airframe 52,917 hrs · 29,319 cycles
LT ENGINE LOOP A AND FIRE HANDLE INTERMITTENT ILLUMINATION DURING APPROACH WITHOUT FIRE BELL FOR THE ENGINE FIRE AND NO CAWS ALERT. OPS CHECK LT ENGINE FIRE DETECTION LOOP A FOUND TO BE NORMAL IAW AMM 26-10-00. DURING APPROACH, THE LT ENGINE DETECTION LOOP A ND LT FIRE HANDLE INTERMITTENT ILLUMINATION. WHEN TESTING LOOP A IAW QRH, ONLY TWO LOOP LIGHTS CAME ON INSTEAD OF THREE. RT ENGINE AND APU ILLUMINATED, THE LT ENGINE FIRE LOOP A LIGHT AND FIRE HANDLE LIGHT DID NOT ILLUMINATE, FIRE WARNING WAS NOT ACTIVATED IN LT ENGINE, NO CAWS, NO FIRE BELL. TEST WAS NOT SATISFACTORY. PERFORMED TROUBLESHOOTING OF THE NR 1 ENGINE FIRE DETECTION SYSTEM IAW AMM 26-10-00 WDM 26-26-31-01, 26-11-00. FOUND A BROKEN WIRE AT LOOP B OF THE LOWER PYLON DETECTOR ELEMENT THAT WAS CORRECTED. ALSO FOUND SWAPPED ELEMENT WIRES AT UPPER PYLON ELEMENT SENSOR SECURED PER WDM 26-11-00. PERFORMED OPS CHECK. OPS CHECK NORMAL IAW AMM MD-80 26-10-00. NO FAULTS NOTED.
Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 52,230 hrs · 28,919 cycles
DURING APPROACH LT ENGINE FIRE INDICATION INTERMITTENT AND THEN WENT OFF. MTX T/S ENGINE FIRE DETECTION STSYEM. FOUND LT FIRE LOOP "A" TEST SYSTEM FAILED. TRANSFERRED TO DMI 4568. IN REFRENCE TO DMI 4568: RERACKED LT ENGINE FIRE DETECTOR CONTROL UNIT AS PER AMM 26-10-03. OPS CHECK NORMAL AS PER AMM 26-10-00. THIS ACTION CLEARED DMI 4568.
2017
Part: EFIS — INOPERATIVE (FIRST OFFICERS)
FIRST OFFICER`S EFIS INSTRUMENTS INOPERATIVE AFTER TAKEOFF. STALL INDICATOR FAILURE LIGHT (AMBER) ILLUMINATED AFTER TAKEOFF.
2015
Part: HANDSET — FAILED (INTERCOM) · airframe 47,721 hrs · 26,645 cycles
FWD INTERCOM FROM COCKPIT TO F/A INOPERATIVE. R & R COCKPIT PEDESTAL HANDSET IAW MD-80 AMM 23-40-04. PERFORMED OPS CHECK IAW AMM 23-40-04, OPS CHECK NORMAL.
Part: DUCT — BROKEN (TAIL COMPARTMENT) · airframe 47,254 hrs · 26,242 cycles
AIR RETURN DUE TO INTERMITTENT INDICATION OF TAIL COMPARTMENT TEMP, HIGH. R & R BROKEN DUCT BY THE RT AUGMENTATION VALVE IAW 36-10-01, ACCOMPLISHED LEAK CHECK WITH ENGINE RUN-UP, NO LEAKS NOTED, NR002. PERFORMED PYLON EXTERNAL INSPECTION, NO DAMAGE NOTED IAW SRM 51-50-00 AND INTERNAL STRUCTURE INSPECTION IAW AMM 54-05-03, NO DEFECTS NOTED, NR004. PERFORMED INSPECTION ON INTERNAL AND SUPPORT AREA INCLUDING ELECTRICAL, PNEUMATIC AND STRUCTURAL, NO DAMAGE NOTED IAW 53-05-03.
Part: COVER — OUT OF ALIGNMENT (L2 DOOR SLIDE) · airframe 47,191 hrs · 26,180 cycles
L2 DOOR CAN NOT BE OPENED BECAUSE OF SLIDE COVER. RESCURED L-2 DOOR SLIDE COVER IAW AMM 25-62-00.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 47,112 hrs · 26,096 cycles
DURING DAILY CHECK, FOUND AFT FLOOR EMERGENCY EXIT IDENTIFIER OUT. R & R EMERGENCY BATTERY PACK AND OPS CHECK NORMAL, AFT EMERGENCY EVACUATION LIGHTS IAW MM 33-53-00.
Part: A/C PACK — UNKNOWN (BOTH) · airframe 47,000 hrs · 25,991 cycles
LOST BOTH PACKS AT 33,000 FT, COULD NOT RECOVER PACKS. PERFORMED ADJUSTMENT TEST RT TEMP CONTROL SYS, FOUND NORMAL ON GROUND IAW MM 21-60-00. PERFORMED ADJUSTMENT TEST LT TEMP CONTROL FOUND PACK IN AUTO INOPERATIVE. PERFORMED LT & RT PACK TEMPERATURE CONTROL INTEGRITY CHECK A AND OPS CHECK IAW BILL OF WORK 2655, AND MM 21-60-00, OPS CHECKED PASSED.
2014
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,914 hrs · 25,911 cycles
FOUND DURING DAILY CHECK, EMERGENCY LIGHTS OUT AT SEAT ROW 4 INOPERATIVE. R & R AND REPLACED EMERGENCY BATTERY PACK AT ROW 4 IAW AMM 33-53-00, CHECKED GOOD.
Part: BOLT — BROKEN (NR 2 WHEEL) · airframe 46,052 hrs · 25,222 cycles
DURING WALK AROUND FOUND NR 2 WHEEL WITH 2 BROKEN TIE BOLTS. R & R NR 2 WHEEL ASSY IAW 34-40-01.
2013
Part: PUMP — INOPERATIVE (FUEL BOOST)
FWD FUEL CENTER BOOST PUMP INOPERATIVE. R & R FORWARD CENTER TANK FUEL BOOST PUMP IAW AMM 28-20-07. CHECKED NORMAL.