In the dropdown menu below you will find the detailed specifications for this specific Gulfstream IV.
Aircraft remains in service until June 30th, 2023
This aircraft will remain in service by the Royal Netherlands Airforce until June 30th, 2023. The expected increase of flight hours and cycles is 100 flight hours and 50 cycles.
Gulfstream IV specifications PDF (Updated April 4th, 2023)
Aircraft specification sheet
Aircraft Identification
AIRCRAFT IDENTIFICATION
Manufacturer:
Gulfstream Aerospace
Type and Model:
GIV
Construction / Line Number:
-
Serial Number:
1009
Date of Manufacture:
December 29th , 1986
Current Registration:
V-11
Current Operator:
RNLAF
Current Owner:
RNLAF
Aircraft Operating Limitation:
CAT II
Certificate of airworthiness
CERTIFICATION OF AIRWORTHINESS
Issuing Authority:
Netherlands Ministry of Defence
Number:
1415
Date of Issue:
December 22th , 1995
Last Validated:
-
Expiry Date:
-
Category:
A
Airframe
AIRFRAME STATUS (1)
Total Airframe Hours
17125.9 Hrs
Total Cycles (Landings):
9445 Cycles
Last Major Overhaul Accomplished:
(Hrs / Cycles / Date)
17033,3 Hrs / 9369 Cycles
December 9th , 2022
Time Since Last Major Overhaul:
(Hrs / Cycles / Date)
92,6 Hrs / 76 Cycles / 116 days
Next Major Overhaul:
August 31st , 2023
Time to Next Major Overhaul:
149 days
Average Cost of Major Overhaul:
€500.000
Current Major Overhaul Facility:
Gulfstream Aerospace Corporation
AIRFRAME MAINTENANCE PROGRAM (1)
Airworthiness Authority Approval:
FAA/ MLA
Check Type
Time Between
Overhaul
Time Since Last Check
Next Scheduled Check due
Cost
Hours/Cycles/
Calendar
Hours/Cycles/ Calendar
Hours/Cycles/
Calendar
'A' or Equivalent
150 / 300 Hours
150 Cycles
'B' or Equivalent
'C' or Equivalent
12 Months
August 31st , 2023
'D' or Equivalent
ADDITIONAL STRUCTURAL INSPECTIONS
Programme Type
MRIP
Ageing Aircraft Programme:
Not applicable.
Corrosion Prevention & Control Programme:
Included in airframe maintenance program
Supplemental Structural Inspections:
Included in airframe maintenance program
(1) Data is subject to change.
Engines
TITLED or INSTALLED ENGINES (1)
Engine Type and Model:
Rolls Royce Tay Mark 611-8
No 1
No 2
No 3
No 4
Serial Number:
16123 (2)
16124(2)
N/A
N/A
Total Time:
16687.3 Hrs
16687.3 Hrs
N/A
N/A
Total Cycles:
9307 Cycles
9307 Cycles
N/A
N/A
Last OH Accomplished
(Hrs / Cycles / Date)
14408,9 Hrs
7914 Cycles
August 10th , 2017
14408,9 Hrs
7914 Cycles
August 10th , 2017
N/A
N/A
Time Since OH/Shop Visit
2278.4 Hrs
2278.4 Hrs
N/A
N/A
Time to Overhaul/Shop Visit:
See HSI 4000 Hrs Frequency
See HSI 4000 Hrs Frequency
N/A
N/A
Time to Engine Calender Life
120 Months
September 14th , 2027
120 Months
September 14th , 2027
N/A
N/A
Cycles to Engine Limiter:
Not applicable
Not applicable
N/A
N/A
Engine Cycles Limiter:
Not applicable
Not applicable
N/A
N/A
Time Since HSI:
67 Months
67 Months
N/A
N/A
‘HSI Frequency (Hrs):
4000 / 8000 Hrs
Remaining:
1721.6 / 5721.6 Hrs
4000 / 8000 Hrs
Remaining:
1721.6 / 5721.6 Hrs
N/A
N/A
Engine Build Standard / TBO (Hrs):
E25NE (Tay TC)
E25NE (Tay TC)
N/A
N/A
Current Overhaul Facility:
Rolls Royce
Rolls Royce
N/A
N/A
Average Cost HSI:
N/A
N/A
Average Cost Shop Visit:
N/A
N/A
AUXILIARY POWER UNIT (APU) (1)
Manufacturer:
Honeywell
Type and Model:
GTCP 36-150(G)
Serial Number:
P-396C
Total Time:
5156 Hrs
Total Cycles:
10020 Cycles
Time Since Overhaul:
Not applicable
Cycles Since Overhaul:
Not applicable
Average Time/Cycles between Removals:
2500 Hours
Current Overhaul Facility:
Gulfstream Aerospace
(1) Data is subject to change.
(2) Serial Number is subject to change.
Landing Gears
LANDING GEARS (1)
Current Overhaul Facility: Gulfstream Aerospace
Nose Gear
Centre Gear
Part Number
1159L40004-27
Part Number
Not applicable
Serial Number
MA0115
Serial Number
Not applicable
Time Since Overhaul
326 Cycles
Time Since Overhaul
Not applicable
TBO
5.000 Cycles
Time Between Overhaul
Not applicable
Scrap Life
20.000 Cycles
Remaining
10500 Cycles
Scrap Life
Not applicable
Average Overhaul Cost
Average Overhaul Cost
Not applicable
Main Gear
Left Hand
Right Hand
Part Number
1159L40001-21
1159L40001-22
Serial Number
MA0259
MA0258
Time Since Overhaul
326 Cycles
326 Cycles
Time Between Overhaul
5.000 Cycles
5.000 Cycles
Scrap Life
20.000 Cycles
Remaining:
19600 Cycles
20.000 Cycles
Remaining:
14700 Cycles
Average Overhaul Cost
(1) Data is subject to change.
Interior configuration
Passenger Seating
Total Seats Certified:
19
Current Passenger Seating:
12
Present Configuration F / J /Y
Toilets:
2
Galleys:
1
Other (Specialist) Configuration Details
(1) Data is subject to change.
Principal operating weights
PRINCIPAL OPERATING WEIGHTS (1)
Maximum Taxi Weight:
75.000 lbs
Maximum Take-Off Weight:
74.600 lbs
Maximum Landing Weight:
66.000 lbs
Zero Fuel Weight:
49.000 lbs
Operating Weight:
42.064 lbs
Empty Weight:
41.259 lbs
Last Weighing:
43.884,2 lbs
Weighing Interval:
As Needed
(1) Data is subject to change.
Fuel data
FUEL DATA
Fuel Capacity:
29.500 lbs
Auxiliary Fuel:
Not applicable
Principal radio and avionics equipment
PRINCIPAL RADIO AND AVIONICS EQUIPMENT (1) (2)
Equipment
Quantity
Manufacturer
Model/Part No.
ATA Chapter 22 – Auto Flight
Flight Guidance Computer
2
Honeywell
7003974-907
Auto Pilot System (Performance Computer)
2
Honeywell
7004609-940
Flight Management System (ATA 34)
2
Honeywell
7018879-03046
ATA Chapter 23 – Communications
PA Amplifier
1
Honeywell
M2060E
HF Transceiver
2
Rockwell Collins
822-0102-001
VHF Transceiver
2
Rockwell Collins
822-1116-001
SELCAL Decoder
1
Terra Corp.
800-0012-105
ATA Chapter 31 – Indicating and Recording
Flight Data Recorder
1
L3 Communications
S800-2000-00
Flight Data Acquisition Unit
1
Teledyne
2231230-14-A-1
Accelerometer
1
Patriot Sensors
3001-01-111
Cockpit Voice Recorder (ATA 23)
1
L3 Communications
2100-1225-22
Airborne Data Loader (ATA 34)
1
Sensata Technologies Inc.
G7228-01
ATA Chapter 34 – Navigation
Air Data Computer
2
Honeywell
7000700-964
EGPWS Computer
1
Allied Signal
965-0976-003-226-226
Inertial Reference Unit
3
Honeywell
HG1075AE04
Navigation Receiver
2
Rockwell Collins
622-7194-201
DME
2
Rockwell Collins
622-7309-101
Radio Altimeter
2
Honeywell
7001840-922
Weather Radar
2
Honeywell
7006921-415
TCAS Computer
1
Honeywell
7517900-55020
ATC Transponder
2
Rockwell Collins
622-9210-501
ADF Receiver
2
Rockwell Collins
622-7382-101
(1) Data is subject to change.
(2) Serial Number is subject to change.
Other specifications
AIRSTAIRS
Are Forward / Aft Air stairs Fitted:
Forward
ACCIDENTS/INCIDENTS/REPAIRS & MODIFICATIONS (1) (2)
Number of significant accident/incidents:
1x off runway, NWS incident
Number of major repairs or modification:
LH/RH T-box corrosion repair
LH/RH Horizontal corrosion repair
ANY PERIOD OF STORAGE DETAILS
Period of aircraft/engines storage:
Not applicable
Location:
Period(s):
From:
To:
Does the aircraft have a complete technical history from manufacture?
Yes
Are all records and documentation in order and up dated on a regular basis?
Yes
Is there are any reason why the aircraft should or could not be sold or transferred to another operator with regard to the content and quality of the technical records?
No
(1) Data is subject to change.
(2) Serial Number is subject to change.
