1981 BOEING 727-225

General Specs (cont.)

Total Time:62739

Engine 1 Time:50650 HOURS

Engine 2 Time:61192 HOURS

Condition:Used

Flight Rules:N/A

Additional Classifications

Detailed Description

HP-1939UCG. 1981 Boeing B727-225F

KEY FEATURES AND MODIFICATIONS:

- Fresh 2C Inspection Delivered by Saltillo Mexico MRO Iberoamerica – Sept 2025
- AEI Cargo Door Modification including 9G Barrier, Main Deck Structural Enhancements, Floor Modifications and Splitter Locks, Side Vertical Restraints, and Smoke Detection System
- ADS-B OUT (Dual)
- TCAS II v7.1
- Digital Flight Data Recorder
- Mark VII Enhanced Ground Proximity Warning System
- IS&S Digital Air Data System (RVSM Approval)
- HT9100 FMS/GPS
- USB Ports – Cockpit and Cabin
- 406 MHz ELT
- Stage III Noise Approval
- Forward Lavatory

Avionics / Equipment

AVIONICS & EQUIPMENT
AEI Cargo Door Modification 
ADS-B OUT (Dual)
TCAS II v7.1
Digital Flight Data Recorder
Mark VII Enhanced Ground Proximity Warning System
IS&S Digital Air Data System (RSVM Approval)
HT9100 FMS/GPS
USB Ports - Cockpit and Cabin
406 MHz ELT
Stage III Noise Approval
Forward Lavatory

Airframe

TIME/CYCLES DATA
Total Hours 62,739 Hours	
Total Cycles 40,199 Cycles	
Next C Check Due 66,739 Hours	
Remaining Till Next C Check 4,000 Hours
Next C Check 2C
C Check Interval 4,000 Hours
Last C Check Date 8/2025
Total Hours Since Last C Check 0
Total Cycles Last C Check 0

OPERATIONAL WEIGHTS
Max Taxi Weight 191,000 lbs
Max Takeoff Weight 190,500 lbs
Max Landing Weight 161,000 lbs
Max Zero Fuel Weight 146,500 lbs
Basic Empty Weight 93,091 lbs
Fuel Capacity 54,000 lbs

Engines / Mods / Prop

ENGINE(S)
Engine Position 1:
Model JT8D-17
Serial 707118
Total Engine 50,650:25
Total Cycle 31,859
Limit Disk for Cycle 5,986
Due Date for AD and S/B 7/2030

Engine Position 2:
Model JT8D-17
Serial 700121
Total Engine 61,192:15
Total Cycle 41,086
Limit Disk for Cycle 6,579
Due Date for AD and S/B 7/2030

Engine Position 3:
Model JT8D-17
Serial 689903
Total Engine 37,557:32
Total Cycle 30,427
Limit Disk for Cycle 4,864
Due Date for AD and S/B 7/2030

AUXILIARY POWER UNIT
Model GTCP85-98C
Part Number 380678-1-1
Serial Number P-3596OC

LANDING GEAR
Position Nose
Part Number 65-72762-1
Serial Number 39661
Interval 16,000
Due Date 2/2030

Position Left
Part Number 65-72761-35
Serial Number DLH1154
Interval 16,000
Due Date 2/2030

Position Right
Part Number 65-72761-36
Serial Number SLS-1014W
Interval 16,000
Due Date 2/2030

Remarks

MAINTENANCE HIGHLIGHTS
Aircraft Currently Undergoing 1C Inspection at Saltillo Mexico MRO Iberoamerica - September 2025
C1-C5 Check and 10 Year Structural Inspection Complied May 2023
-17 Engines with 6,579, 5,986 and 4,864 Cycle Remaining Each
Engine HPC Inspection AD – Due July 2030
Landing Gear Overhaul – Due February 2030
Boeing MPD (MSG-3) Inspection Program
Aircraft in Active Service 
Records Available for Inspection – Panama City, Panama






Coleman Jet Solutions assumes no responsibility or liability for the accuracy of information contained herein. Specification are intended to facilitate the preliminary review of the aircraft and may not be used for any other purpose. It is the responsibility of the purchaser to conduct their own inspection of the aircraft and to verify the accuracy of the information contained herein. Aircraft is subject to prior sale, commitment, or withdrawal from the market, at any time, without notice.