N700KW
Registered owner: EASTERN AIRLINES LLC, MO (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.
43 reports on file, 2018-04-22 – 2026-05-04.
Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 74,005 hrs · 31,225 cycles
LEFT ENGINE INDICATING LOW OIL QUANTITY IN FLIGHT. 20 QUARTS AT TAKEOFF, 3 QUARTS AT LANDING. DIVERSION WAS REQUIRED REQUIRED FOR INDICATION. A/C DIVERTED TO TOL.4-MAY-26 LP 43645.
Earlier reports · 2018–2025 · 42 reports
2025
Part: PRESSURE SENSOR — FAILED (HYD SYS) · airframe 73,556 hrs · 31,096 cycles
CENTER HYD SYSTEM EICAS MESSAGE
Part: HYDRAULIC SYSTEM — FALSE INDICATION (ZONE 700) · airframe 73,548 hrs · 31,093 cycles
C. HYD. SYSTEM EICAS MESSAGE
Part: PANEL — MISSING (ZONE 400) · airframe 73,471 hrs · 31,061 cycles
R/H PYLON PANEL; # 433FR MISSING ON POST FLIGHT INSPECTION.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 73,462 hrs · 31,058 cycles
R/H EMERGENCY EXIT & PAX EMERGENCY LIGHTS L996,L321,L121 & L776 INOP.
Part: SPAR — CORRODED (ZONE 600 FLAP) · airframe 73,462 hrs · 31,058 cycles
CORROSION DAMAGE HAS BEEN FOUND ON THE REAR SPAR LOWER CHORD OF THE INBOARD TRAILING EDGE FLAP ON THE RH WING. THE DAMAGE HAS BEEN CUT OUT TO REMOVE THE DAMAGED SECTION OF THE 2024-T3511 EXTRUDED TEE AND REPLACED WITH AN EQUIVALENT 2024-T3 EXTRUSION. THE REPAIR MEMBER IS SPLICED TO THE EXISTING LOWER CHORD USING 2024-T3 EXTRUDED ANGLES AT EACH END IN ACCORDANCE WITH SEMAN PERU SAC REPAIR DRAWING ED-2025-0005 (REF. 7).
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 73,462 hrs · 31,058 cycles
2 EACH EXTERNAL EMERGENCY LIGHTS NOT ILLUMINATING
Part: LIGHT — NO TEST (ZONE 200) · airframe 73,462 hrs · 31,058 cycles
BATTERY PACK FOR EMERGENCY LIGHTS L290,L291,L292 & L293 FAIL CAP TEST.
Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 73,462 hrs · 31,058 cycles
BATTERY PACK FOR EMERGENCY LIGHTS L290,L291,L292 & L293 FAILED CAP. CHECK.
Part: ACCESS PANEL — MISSING (ZONE 400) · airframe 73,462 hrs · 31,058 cycles
EXHAUST NOZZLE FWD 1 EACH ACCESS PANEL MISSING @6:00 POSITION.
Part: SKIN — SEPARATED (WING) · airframe 73,413 hrs · 31,045 cycles
FLIGHT FROM AFW TO YYZ, AFTER LANDING MECHANIC DURING POST FLIGHT INSPECTION DISCOVERED THAT THE S51MT (ATA 57 - INBOARD WING TRAINING EDGE) PANEL HAD PARTIALLY DEPARTED THE AIRCRAFT. APPEARS THE PANEL FASTENERS WERE NOT PROPERLY INSTALLED.
Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 200) · airframe 73,409 hrs · 31,043 cycles
MID GALLEY FIRE SMOKE DETECTOR SMOKE ALARMS GO OFF DURING DESCENT SAYS "FAULT"
2024
Part: FIRE WARNING — ILLUMINATED (LEFT) · airframe 72,982 hrs · 30,908 cycles
LEFT ENGINE FIRE (WARNING EICAS) INDICATION ON CLIMB OUT. PILOT COMMANDED ENGINE SHUTDOWN FOLLOWING QRH. NO ENGINE FIRE BOTTLE UTILIZED. FIRE WARNING LIGHTS EXTINGUISHED AFTER THE FIRE T- HANDEL WAS ACTIVATED. UNEVENTFUL LANDING - NO EMERGENCY EGRESS CREW ONLY NO PASSENGERS. RB211-524HT-36 ESN 13264.
Part: ENGINE — FAILED · airframe 72,958 hrs · 30,895 cycles
FAILED BSI IAW ASB RB211-72-AL 102, EO 767-72-0015 AD 2024-07-04 EASA 2024-0069.
Part: FRAME — CORRODED (BS 1562) · airframe 62,365 hrs · 35,578 cycles
SECTION 46 WEB FRAME AT STA.1562.
2023
Part: JACKSCREW — SHEARED (ZONE 400) · airframe 72,717 hrs · 30,821 cycles
FAULT FOUND DURING MAINTENANCE OF T/R REASON FOR REPORTABLE DELAY.
Part: MARKER — DISCHARGED (ZONE 200) · airframe 72,571 hrs · 30,787 cycles
DURING FUNCTIONAL CHECK EXIT MARKER AT CEILING NEAR FWD DOOR L1 DID NOT ILLUMINATE.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 72,571 hrs · 30,787 cycles
L3 & L4 EMER LIGHT INOP
2022
Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 71,719 hrs · 30,569 cycles
L3 DOOR OVER HEAD EXIT LIGHT INOP/CORRECTIVE ACTION REPAIRED BATTERY WAS SAPPED ACCOMPLISHED IAW AMM BOEING 767 CHAPTER 33-51-07.
Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 71,719 hrs · 30,569 cycles
R1 DOOR EXIT LIGHT INOP/ CORRECTIVE ACTION REPAIRED BATTERY WAS SAPPED ACCOMPLISHED IAW AMM 33-51-07
Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 71,719 hrs · 30,569 cycles
L3 EMERGENCY OVER HEAD LIGHT INOP/ CORRECTIVE ACTION REPAIRED BATTERY WAS SAPPED ACCOMPLISHED IAW AMM BOEING 767 CHAPTER 33-51-07
Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 71,719 hrs · 30,569 cycles
L1 DOOR EXIT LIGHT INOP/ CORRECTIVE ACTION REPAIRED, BATTERY WAS SAPPED ACCOMPLISHED IAW AMM 33-51-07
Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 71,719 hrs · 30,569 cycles
COCKPIT DOOR OVER HAED EXIT LIGHT INOP/ CORRECTIVE ACTION REPAIRED BATTERY WAS SAPPED ACCOMPLISHED IAW AMM 33-51-07
Part: BATTERY PACK — DEPLETED (ZONE 800) · airframe 71,719 hrs · 30,569 cycles
L3 EMERGENCY OVERHEAD LIGHT INOP
Part: BATTERY PACK — FAILED INSP (ZONE 200) · airframe 71,557 hrs · 30,527 cycles
EMERGENCY LIGHTS INOP AT ENTRY DOOR L1, L2 AND EMERGENCY EXIT DOOR L3. FOUND DURING SERVICE CHECK IN MCI
Part: LIGHT — DEPLETED (ZONE 100) · airframe 71,353 hrs · 30,474 cycles
DURING OPS CHECK EMERGENCY LIGHTS BATTERY WAS DEPLETED
Part: LIGHT — DEPLETED (ZONE 100) · airframe 71,353 hrs · 30,474 cycles
DURING OPS CHECK EMERGENCY LIGHTS BATTERY WAS DEPLETED.
2021
Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 70,622 hrs · 30,332 cycles
LAV SMOKE DETECTORS AFT LEFT, AFT REAR RIGHT, AFT REAR DO NOT TEST. TRANSFERED TO DMI 700-21-0081.
Part: NONE — NONE · airframe 70,561 hrs · 30,322 cycles
DURING WALK AROUND FOUND 1 BLOCKER DOOR DAMAGE LEFT ENGINE THRUST REVERSERS. REV INSPECTION AND ENGINE CONFIRMATION OF CONTINUED SERVICE. SUPPLIMENTAL . REMOVED AND REPLACED L/H ENGINE CORONA AND #3 BLOCKER DOOR IAW AMM 78-31-06 AND ESM 78-32-00-440-043/044. OPS CHECK GOOD.COMPONENT REPLACEMENT BLOCKER DOORS (P/N J314179 POSITION #3 S/N TVL BW4913) AND CORONA (P/N LJ37755 AND S/N AA46).
Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 70,561 hrs · 30,322 cycles
DURING WALK-AROUND FOUND 1 BLOCKER DOOR DAMAGE LEFT ENGINE TRUST REVERSERS. REV INSPECTION AND ENGINEERING CONFIRMATION OF CONTINUED SERVICE. CONFIGURATION DEVIATION LISTING APPLIED AND NEW PARTS AND HARDWARE ORDERED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,381 hrs · 30,286 cycles
FLIGHT DECK EMERGENCY LIGHT INOP. FLIGHT DECK EMERGENCY LIGHT BATTERY REPLACED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,081 hrs · 30,226 cycles
THE R4 EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE MECHANIC REMOVED AND RPLACED R4 SIDE EMERGENCY LIGHT THAT WAS FOUND LOOSE IN ADDITION TO M733 POWER BATTERY PACK PER AMM 33-51-21. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,081 hrs · 30,226 cycles
THE R2 AND R4 EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE MECHANIC REMOVED AND RPLACED THE POWER SUPPLY BATTERY PACK M733 PER AMM 33-51-21. ALSO RELIGHTED THE R4 EMERGENCY LIGHT LAMP SOCKET. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHTS) · airframe 69,941 hrs · 30,201 cycles
DURING MAINTENANCE CHECKS THE MECHANIC FOUND L1 AND R1 EXIT EMERGENCY INTERIOR LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK ON L1 & R1 ON INTERIOR LIGHTS. OPS CHECK FOUND TO BE IAW AMM 33-51-07.
Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHTS) · airframe 69,941 hrs · 30,201 cycles
DURING MAINTENANCE CHECKS THE MECHANIC FOUND L5 AND R3 EXIT EMERGENCY INTERIOR LIGHTS INOP. AIRPLANE CHARGED EMERGENCY BATTERY L3 AND R3 EXIT INTERIOR LIGHT, OPS CHECK IAW AMM 33-51-00 TO BE NORMAL.
Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHTS) · airframe 69,932 hrs · 30,198 cycles
DURING A ROUTINE MAINTENANCE THE MECHANIC FOUND L1,L3 AND L4 EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED M738 BATTERY PACKS. OPS CHECK IS NORMAL AND IAW AMM 33-15-66.
Part: DOOR — MISSING (LT NACELLE) · airframe 69,678 hrs · 30,152 cycles
DURING WALK AROUND IT WAS NOTED THE LEFT ENGINE OUTBOARD NACELLE STRUT DOOR WAS MISSING. THE FME DURING THE WALK AROUND NOTED THE MISSING DOOR IN THE LOG PAGE (LEFT ENGINE NACELLE DOOR MISSING). THIS WAS PLACED ON CDL ISSUED AND ISSUED AN MRN. MAINTENANCE MECHANIC RE-SECURED THE SENSOR TARGET BRAKE WITH NEW RIVETS. A/C WAS RETURN TO SERVICE.
2020
Part: CONTROL SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 69,631 hrs · 30,141 cycles
DURING INSPECTION N700KW WAS IN HEAVY CHECK. C-CHECK MAINTENANCE IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHT TEST CONTROL SWITCH WAS FOUND DEFECTIVE. THE CORRECTIVE ACTION TAKEN WAS TO REMOVE AND REPLACED THE CONTROL SWITCH ON P40 EMERGENCY EXIT LIGHT TEST, IAW 0767 SWPM 20-83-11 PAGE 13. PERFORMED OPERATIONS CHECK RESULTS WERE GOOD, IAW B767 AMM 33-51-06 PAGE 202.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 63,508 hrs · 28,756 cycles
EMERGENCY LIGHTS AT THE L4, R4, AND L1 DOORS. REMOVED AND REPLACED POWER SUPPLY (M736)IAW B767 AMM 33-51-01 OPS CHECK FOUND OK AND REMOVED AND REPLACED AFT R AND L DOOR SLIDE EMERGENCY 1T LAMP IAW B767 AMM 33-51-06 OPS CHECK OK
Part: FIRE DETECTOR — FALSE INDICATION (NR 2 ENGINE) · airframe 68,954 hrs · 30,012 cycles
#2 ENGINE FIRE INDICATION ON THE GROUND, AT IDLE, PRIOR TO TAKE OFF. QRH WAS FOLLOWED AND FIRE BOTTLE #1 DISCHARGED. INDICATION REMAINED SO FIRE BOTTLE #2 WAS DISCHARGED AND EMERGENCY DECLARED. AIRPORT FIRE RESCUE RESPONDED AND FOUND NO INDICATION OF FIRE. AIRCRAFT RETURNED BACK TO THE GATE. MAINTENANCE FOUND NO INDICATION OF FIRE. REMOVED AND REPLACED ZONE 2 FIRE DETECTOR ASSY (FIRELOOP) I/A/W B767 AMM 26-11-02. CONDUCTED AN OPERATION CHECK I/A/W B767 AMM 26-11-00. OPS CHECK GOOD. ALSO REMOVED AND REPLACED #2 ENGINE FIRE BOTTLE AND CARTRIDGE #1 AND FIRE BOTTLE AND CARTRIDGE #2 I/A/W B767 AMM 26-21-03. OPS CHECK GOOD.
2019
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,934 hrs · 30,004 cycles
DURING 28 DAY CHECK FOUND R/H EXIT SIGN LIGHT INOP. REMOVED AND REPLACED R/H AFT BATTERY PACK IAW B767 AMM 33-51-07. OPS CHECK NORMAL. NOTE: AIRCRAFT WAS IN MAINTENANCE CHECK AT THE TIME THE ISSUE WAS FOUND. FAA PMI HAS BEEN NOTIFIED.
Part: HELICOIL — BACKED OUT (GENERATOR) · airframe 86,211 hrs · 29,777 cycles
LOST OIL PRESSURE AND QUANTITY TO THE POINT WE HAD TO SHUTDOWN IN FLIGHT AND DIVERTED TO ALTERNATE DESTINATION. FOUND BOLTS FOR DEDICATED GENERATOR BACKED OUT AND HELICOILS ALSO BACKED OUT. REPLACED HELICOILS AS REQUIRED AND REINSTALLED GENERATOR
2018
Part: ENGINE — HOT START (LEFT) · airframe 68,127 hrs · 29,754 cycles
LEFT ENGINE HOT START 510 DEGREES WITH ONLY 17% N2 FUEL FLOW NORMAL N3 MAXIMUM AT 23%. TROUBLESHOT IAW FIM 71-05 F//T 808 AND AMM 71-00-00.