# TCDS 7H1: Airbus Helicopters

- Type: Type certificate data sheet
- Status: Current
- Holder: Airbus Helicopters
- Revision: 16
- Revised: January 10, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: CAR 6, CAR 10
- Registered aircraft: 22, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/7e/c6/7ec69fb890891daf3f29cb5d8dae73155e754f75eb26a2b55255449839621619
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/84AC475A3B4C670E86257C67005E3B1E.0001
- Page: https://openairdocs.org/tcds/7H1

## Models (5)

As the data sheet lists them.

- SE 3130-Alouette II
- SE 313B-Alouette II
- SA 318C-Alouette Astazou
- SA 3180-Alouette Astazou
- SA 318B-Alouette Astazou

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2 3 4 5 6 7 
Rev. No. 16 - - 14 15 - 16 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
7H1 
Revision 16 
Airbus Helicopters 
SE 3130-ALOUETTE II 
SE 313B-ALOUETTE II 
SA 3180-ALOUETTE ASTAZOU 
SA 318B-ALOUETTE ASTAZOU 
SA 318C-ALOUETTE ASTAZOU 
January 10, 2014 
 
TYPE CERTIFICATE DATA SHEET NO. 7H1 
 
This data sheet which is a part of type certificate No.  7H1 prescribes conditions and limitations under which the product for  
which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. 
 
Type Certificate Holder: Airbus Helicopters 
  Aeroport Internati onal Marseille Provence 
  13725 - Marignane - Cedex 
  France 
 
TC Holder Record: Eurocopter France changed name to Airbus Helicopters on January 1, 2014. 
 
Section I. - Model SE 3130 Alouette II, approved 14 January 1958 
  - Model SE 313B Alouette II, approved 28 August 1968 
 
 Engine Model SE 3130:  Turbomeca Ar touse 11B1, IIC, IIC1, IIC2, IIC5, IIC6 
  Model SE 313B:  Turbomeca Artouste IIC5, IIC6 
 
FUEL SPECIFICATION (Latest Amendment) REMARKS 
 FRENCH NATO USA UK  
 AIR 3405 
(TRO) 
F34  D.eng.RD 2453 
AVTUR/FA II 
 
  F35  D.eng.RD 2494 
AVTUR 
 
 AIR 3407 
(TR4) 
F40 MIL-T-5624 
(JP.4) 
D.eng.RD 2486 
AVTAG FA II 
 
  F45  D.eng.RD 2486 
AVTAG 
 
AVIATION 
FUELS 
AIR 3404 
(TR5) 
F42    
 TR.5 F44 MIL-T-5624 
(JP.5) 
D.eng.RD 2498 
AVCAT 
 
  F12 MIL-G-5572  25 hr. maximum between overhauls 
 Gasoline 
AIR 3401 
F18 
F22 
MIL-G-5572 D. eng. RD 2485 is is recommended to add 1% to 2 % 
oil, preferably mineral oil. 
 
NAVY 
7120 STM 
Gas Oil = O 
F75 MIL-F-16884 DEF STAN 31-4 Do not use below - 15°C 
FUELS 7120 STM 
Gas Oil = 20 
F76    
 
 
OTHER 
FUELS 
Automotive 
Gasoline 
DCEA/2D 
MT 80 
 
F46 
  
DEF 2401 
25 hr maximum between overhauls 
it is recommended to add 1% to 2% 
oil; preferably mineral oil. 
 Illuminating 
oil (kerosene) 
DCEA/IIC 
 
F58 
 
V V K 211 
 
DEF 2403 
Sulfur: less than 02% 
Flash point: not less than 38°C. 
Freezing point: not greater than  
-40°C.

2 of 7 7H1, Rev 16 
FUEL SPECIFICATION (Latest Amendment) REMARKS 
 FRENCH NATO USA UK  
OTHER 
FUELS 
(Cont’d) 
Automotive 
Diesel oil 
40 Dieso 
DCEA/21C 
 
F54 
 
V V F 800 
Class DF 2 
 
TS 10003 
Sulfur: less than 1% Kinematic 
viscosity at 20°C:  less than 9 cst. 
Do not use below O°C. 
 
 
ENGINE OIL SPECIFICATION (L atest Amendment) REMARKS 
 FRENCH NATO USA UK  
Normal AIR 3512 0.138 Shell Turbine oil 
9  
Esso Aviation 
oil 57  
Caltex Jet eng. 
oil heavy 
DED 2479 Refer to instruction entitled "OIL 
COLD" in paragraphs 1.6.1 and 1.6.2 
in Flight Manual 
For outside 
temperature 
below -10°C 
AIR 3515 0.135 Aeroshell 
turbine oil 3 
Esso Aviation 
utility oil F 
Caltex Jet eng. 
oil medium 
heavy 
Caltex aircraft 
instrument oil 
D.Eng.RD 
2490 
 
or 
 
DEF 2001 
 
For out-side 
temp. between 
-15°C +5°C 
   DED 2480  
 
 
 Engine Limits Maximum speed 34,000 r.p.m. 
  Maximum power 400 hp 
  Maximum tail pipe temperature (t4) 550°C for a max. of 15 min. 
  Maximum continuous tail pipe temp. 510°C 
 
 Rotor limits Maximum speed 420 r.p.m. 
  Minimum speed 280 r.p.m. 
  Constant speed, power-on flight 360 r.p.m. 
 
 Maximum Weight Model SE 3130 : 3300 lb. 
  Model SE 313B : 3500 lb. (See NOTE 8) 
 
Section II. - Model SA 3180 Alouette - Astazou, approved November 25, 1964 
 - Model SA 318B Alouette - As tazou, approved August 28, 1968 
 - Model SA 318C Alouette - As tazou, approved August 28, 1968 
 
 Engine Turbomeca As tazou IIA power unit

3 of 7 7H1, Rev 16 
FUEL SPECIFICATION (Latest Amendment) REMARKS 
 FRENCH NATO USA UK  
 AIR 3405* 
(TRO) 
F34  D.eng.RD 2453 
AVTUR/FS II 
 
  F35  D.eng.RD 2494 
AVTUR 
 
 
AVIATION 
AIR 3407* 
(TR4) 
F40 MIL-T-5624 
(JP.4) 
D.eng.RD 2454 
AVTAG FS II 
 
FUELS  F45  D.eng.RD 2486 
AVTAG 
 
 AIR 3404* 
(TR5) 
F42    
 TR.5    * F44 MIL-T-5624 
(JP.5) 
D.eng.RD 2498 
AVCAT 
 
  F12 MIL-G-5572  25 hr. maximum between overhauls 
 Gasoline * 
AIR 3401 
F18 
F22 
 
MIL-G-5572 
 
D.eng.RD 2485 
it is recommended to add 1% to 2% 
oil.  Preferably mineral oil. 
 7120 STM 
Gas Oil =O 
F75 MIL-F-16884 DEF STAN 31-4 Do not use below -15°C For the 
normal use of this fuel the AZ 156 
NAVY 
FUELS 
7120 STM 
Gas Oil =20 
F76   unit containing one of the fuel 
marked*: 
-is recommended in all cases. 
-is essential if the temperature is 
below 10°C. 
 Automotive 
Gasoline 
DCEA/2D 
MT 80 
 
F46 
  
DEF 2401 
25 hr. maximum between overhauls 
it is recommended to add 1% to 2% 
oil, preferably mineral oil. 
OTHER 
FUELS 
Illuminating oil 
(kerosene) 
DCEA/IIC 
 
F58 
 
V V K 211 
 
DEF 2403 
Sulfur: less than0.2% 
Flash point: not less than 38°C. 
Freezing point: not greater than -40°C 
 Automotive 
Diesel Oil 
40 Dieso 
DCEA/21C 
 
F54 
 
V V F 800 
Class DF 2 
 
TS 10003 
Sulfur: less than 1% Kinematic 
viscosity at 20°C less than 9 cst. 
Do not use below 0°C. 
For the normal use of this fuel the AZ 
156 unit (SNIAS S.B. 28.14) 
containing one of the fuel marked*: 
- is recommended in all cases 
- is essential if the temperature is 
below 10°C. 
 
 
ENGINE OIL SPECIFICATION (L atest Amendment) REMARKS 
 FRENCH NATO USA UK  
 AIR 3513 0.148 MIL-L-7808   
 
NORMAL 
 
AIR 3515 
 
0.135 
Aeroshell 
Turbine Oil 3. 
  
   Esso Avn. 
Utility Oil F 
D.Eng.RD 
2490 
Use of brands other than those shown 
opposite requires S.G.A.C. approval. 
   Caltex jet engine 
oil medium 
heavy 
  
 
The mixing of oils AIR 3513 and AIR 3515 is not permitted.  The system should be flushed when changing from one type to the 
other.

4 of 7 7H1, Rev 16 
 Engine Limits Engine speed : 43,500 r.p.m. held c onstant by governor (transient variations of + 1500  
  r.p.m. are permissible when applyi ng rapid collective - pitch variations) 
  Maximum takeoff power  :  523 hp. (See NOTE 6) 
  Maximum continuous power:  473 hp. (See NOTE 6) 
  Maximum tail pipe temperature for starting (30 seconds): 550°C peak value 
   630°C for period 
   not exceeding 3 seconds (between 5,000 and 10,000 r.p.m.) 
  Maximum for take off  :  525°C (See NOTE 6) 
  Maximum continuous ta il pipe temperature  :  500°C (See NOTE 6) 
 
 Rotor limits Maximum speed 420 r.p.m. 
  Minimum speed 280 r.p.m. 
  Constant speed, power-on flight 362 r.p.m. 
 
 Maximum Weight Model SA 3180 : 3300 lb. 
  Model SA 318B : 3500 lb. (See NOTE 8) 
  Model SA 318C : 3650 lb. (See NOTE 8) 
 
Section III, Data Applicable to All Models 
 
 Airspeed Limits Never Exceed Speed: 105 kt for SE 3130, SE 313B  ) See NOTE for 
   SA 3180, SA 318B  ) required placard 
   111 kt for SA 318C ) 
 
 C.G. Range (107.1) to (120.9) for SE 3130, SE 313B 
  (107.09) to (124.02) for SA 3180, SA 318B , and for SA 318C with speed limitation. 
 
 Datum 118.11 forward of rotor centroid. 
 
 Leveling Means Two leveling lugs on body structure LH lower corners and two leveling lugs on body  
  structure RH lower corners. 
 
 Number of Seats 5.  Pilot, co-pilot (51); 3 passengers (87). 
 
 Maximum baggage 220 lb. under rear seat  (86.6) (with 5 persons of 176 lb. ea. on board) or 507 lb. behind  
  pilot's and front passenger's se ats, with rear seat folded (74.8) (One pilot and one front  
  passenger on board).  (See NOTE 2 for required placard). 
 
 Fuel capacity 153 gals. (120), usable 149 gals. 
 
 Oil Capacity 2 gals. (137 for model SE 3130 and SE 313B) 
   (150 for model SA 3180, SA 318B and SA 318C) 
 
 Rotor Blade Movements For rigging information, refer to  Alouette II or Alouette Astazou Maintenance Manual,  
  as applicable. 
 
 Serial Nos. Eligible The French Government Certif icate of Airworthiness for Export endorsed as noted under 
"Import Requirements" must be submitted for each individual helicopter for which 
application for certification is made.  For applications for Standard Airworthiness 
Certificates made after May1, 2004, a review of historical records is needed to determine 
if the helicopter was delivered to and operated by the military.  If the helicopter has 
military history, the helicopter is not eligible for a Standard Airworthiness Certificate 
unless a copy of a Standard Airworthiness Certificate issued at the time of delivery to the 
military is submitted. 
                                                                
 Certification Basis CAR 10.  CAR 6 effective Janua ry 15, 1951 including Amendment 6-1 through 6-8, plus  
  Special Conditions notified by the U.S. govern ment to the Government of France in FAA  
  letter of May 28, 1957. 
  Type Certificate No.  7H1 issued January 14, 1958 
  Date of Application October 11, 1955

5 of 7 7H1, Rev 16 
The French Direction Generale de l’Aviation Civile (DGAC) originally type 
certificated this rotorcraft under its type certificate TC 1.  The FAA validated 
this product under U.S. Type Certificate Number 7H1.  Effective September 28, 
2003, the European Aviation Safety Agency (EASA) began oversight of this 
product on behalf of the DGAC. 
 
 Import Requirements  
The FAA can issue a U.S. airworthiness certificate based on a National Aviation 
Authority (NAA) Export Certificate of Airworthiness (Export C of A) signed by 
a representative of the French Generale de l’Aviation Civile (DGAC) on behalf 
of the European Community.   
 
The Export C of A should contain the following statement: “The aircraft covered 
by this certificate has been examined, tested, and found to comply with the type 
design approved under U.S. Type Certificate Number 7H1 and to be in a 
condition for safe operation.” 
 
 
 Equipment The basic required equipment as prescrib ed in the applicable airworthiness regulations  
  (see Certification Basis) must be installed in the aircraft for certification.  In addition, the  
  following item of equipment is required: 
(a) SGAC approved Alouette II or Alouette Astazou Flight Manual, as applicable. 
 
Service Information Each of the documents listed below must state that it is approved by the 
European Aviation Safety Agency (EASA) or – for approvals made before 
September 28, 2003 – by the French Generale de l’Aviation Civile (DGAC).  
Any such documents are accepted by the FAA and are considered FAA 
approved. 
 
 Service Bulletin, 
 Structural repair manuals, 
 Vendor manuals, 
 Aircraft flight manuals, and  
 Overhaul and maintenance manuals. 
 
    This applies only to the acce ptance of the type design data. 
 
 
NOTE 1: Current weight and ba lance report, including list of equipment included in certificated empty weight, and  
 loading instructions when necessary, must be provid ed for each helicopter at the time of original  
 certification.  In order to obtain the most consistent weight and balance results, all model helicopters should  
 be weighed on jackpoints rather than on skids, wheels or  floads.  When changes are made to the helicopter  
 which affect the weight and balance refer to the Flight Manual for instructions. 
 
 The certificated empt y weight and corresponding center of gravity location must include unusable fuel of 26  
 lb. (120) and undrainable oil of 2.2 lb. (162.2 for models SE 3130, SE 313B and 172.5 for models SA 3180,  
 SA 318B and SA 318C). 
 
NOTE 2: The following placards must be displayed: 
 
 (1) In full view  of the pilot: 
  (a) "This helicopter must be operated in compliance with the operating limitations specified in the  
   SGAC approved helicopter Flight Manual". 
 
  (b) "Never exceed speeds.  Variation of Vne with altitude and weight". 
   (b) (1) SE 3130 Alouette II and SA 3180 Alouette Astazou.

6 of 7 7H1, Rev 16 
 
 Altitude Sea Level 3,000 ft 6,000 ft 9,000 ft 12,000 ft 13,500 ft 
 Weight (lb) kt kt kt kt kt kt 
 3,300 105 95 85    
 3,100 105 100 90 80   
 2,900 105 105 95 85 75  
 2,700 105 105 100 90 80 75 
 2,400 105 105 105 95 85 80 
 2,200 105 105 105 100 90 85 
 
  (b) (2) SE 313B Alouette II and SA 318B Alouette Astazou. 
 
 Altitude Sea Level 3,000 ft 6,000 ft 9,000 ft 12,000 ft 13,500 ft 
 Weight (lb) kt kt kt kt kt kt 
 3,500 100 90 80    
 3,300 105 95 85    
 3,100 105 100 90 80   
 2,900 105 105 95 85 75  
 2,700 105 105 100 90 80 75 
 2,400 105 105 105 95 85 80 
 2,200 105 105 105 100 90 85 
  (b) (3) SA 318C Alouette Astazou 
 
 Altitude Sea Level 3,000 ft 6,000 ft 9,000 ft 12,000 ft  13,500 ft 
 Weight (lb) kt kt kt kt kt kt 
 3,650 111 108 95 78   
 3,500 111 108 95 78   
 3,300 111 108 95 81 67  
 3,100 111 108 96 84 73 67 
 2,900 111 108 98 88 78 73 
 2,700 111 108 100 92 84 80 
 2,400 111 108 101 95 89 85 
 
 (2) Secured to the floor in the rear right corner: 
  "Maximum baggage 220 pounds under rear seat (+86.6 in) with 5 persons of 176 pounds each on board,  
  or 507 pounds behind pilot and front passenger seats, with  rear seat folded (+74.8 in) and one pilot and  
  one front passenger on board". 
 
NOTE 3: The retirement times of critical parts are listed in Alouette II Maintenance Manual, or Alouette Astazou  
 Maintenance Manual, chapters 5, SGAC-approved. 
 
NOTE 4: These helicopters must be serviced and maintained in conformance with the following manuals, as  
 applicable, of which chapter 5 "Per iodic Inspection" is SGAC approved: 
 
 (a) Alouette II Maintenance Manual (airframe and engine) 
 (b) Alouette - Astazou Maintenance Manual (airframe and engine) 
 
NOTE 5: The Siren Sling and Air Equipm ent rescue hoist are special purpose equipment and should be operated in  
 accordance with the limitations described in CAR 8.  Information concerning operation limitations is also  
 contained in the heli copter Flight Manual. 
 
NOTE 6: Maximum certificated horsepower for this installation is limited to 400 hp due to rotor transmission  
 limitations. 
 
 For the same reason, the ma ximum permissible exhaust gas temperatures are limited to: 
 - Takeoff: 490°C (For OAT 15°C and below) and 515°C at OAT: 45°C; 
   Straight line interpretation between 15°C and 45°C. 
 - Maximum continuous : 460°C

7 of 7 7H1, Rev 16 
NOTE 7: To convert the model SE 3130 Alouette II to th e Model SA 3180 Alouette-Astazou the following assemblies 
must be installed in place of the corresponding assemblies designed for the SE 3130 Alouette II in 
accordance with Sud Aviation modification AM 817: 
 
 Assembly Drawing No. 
 - Engine Astazou II A 3180-50-50.000 
 - Oil system (engine and M.G.B.) 3180-54-10.000 
 - Engine vent 3180-50-50.010 
 - Clutch unit 3180-63-10.000 
 - Rear engine mount 3180-21-03.100 
  or 3180-21-03.200 
 - Engine controls 3180-76-13.000 
 - Fuel system 3180-52-00.000.1 
 - Main gear box 3160-62-00.000.9 
 - Main rotor shaft 3160.68.10.000.2 
 - Starter wiring installation 3180.72.22.300 
 - Spring actuator 3180-89-00.000 
 - Instrument panel installation 3180-76.50.000 
 - Firewall asse mbly 3180-59-10.000 
 - Transmission support platform 3180-27-60.000 
   (Stainless steel 
 
 Further, the following equipmen t (optional on Alouette II) must mandatorily be installed. 
 
 - Servo-unit installation 3130-73-71.000 
 
NOTE 8: (1) to convert the model SE .3130 Alouette II to the Model SE 313B or the model SA 3180 Alouette -  
  Astazou to the Model SA 318B the following modifications are required: 
  
 - High pitch stop adjusted for 15° 
 - Reinforced main rotor blades P/N 3130-11-20.000 
 - Body structure reinforced transversal bar P/N 3130-21-15.100 
 - Artouste IIC5 or IIC6 engines must be installed for model SE 3130 Alouette II only. 
 - Instruction plates P/N 3130-25-20.090, index mark s on pitch indicator P/N 3130-90-00.144, instruction  
  plates P/N 3180-76-26.011. 
 - Modification of marking helicopter 318-00-10.0 06 (Alouette-Astazou) 313B-00-00.020 (Alouette II). 
 - And the following tail rotor g ear box/tail rotor hub modifications: 
 
 Either: Reinforced tail rotor gear box P/N 3130-66-70.000 and tail rotor head P/N 3130-33-30.000.1. 
  
 or Fork type rotor hub 3180-33-00.000 and tail rotor blades P/N 3160-34-10.000.6 
  Tail rotor gear box P/N 3160-66-10.000.1 
 
 The following modifications must be embodied before floats are installed: 
 
 - Reinforced float type landing gear P/N 3130-73-54.500 
 - Hydraulic dampers on float type landing gear P/N 3130-46-10.560 
 
 (2) To convert the model SA 3180 Alouette-Astazou to the model SA 318C the following modifications are  
  required in addition to the foregoing (except instruction plates P/N 3130-25-20.090 and P/N 3180-76- 
  26.011) 
 
 - Landing gear reinforced transversal bar P/N 3180-46-10.010 or P/N 3180-46-10.015 
 - Landing gear shock strut P/N 3180-46-10.100 
 - Instruction plates P/N 3180-25-10.040 and P/N 3180-76-26.019 
 - Marking on airspeed indicator P/N 3180-90-00.006 
 
NOTE 9: Effective January 1, 2014, Eurocopter France name was changed to Airbus Helicopters. 
 
 
 
...END...
```

## ADs (26, in force first)

- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2012-23-03](https://openairdocs.org/ad/2012-23-03): Tail Rotor Drive System · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 5 more. Effective Dec 31, 2012
- [AD 2002-01-30](https://openairdocs.org/ad/2002-01-30): Main Gearbox Magnet Plug · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 7 more. Effective Feb 19, 2002
- [AD 2001-18-51](https://openairdocs.org/ad/2001-18-51): Main Gearbox Assembly · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 5 more. Effective Oct 31, 2001
- [AD 2000-05-11](https://openairdocs.org/ad/2000-05-11): Tail Rotor Blades · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 7 more. Effective Mar 24, 2000
- [AD 2000-03-06](https://openairdocs.org/ad/2000-03-06): Horizontal Stabilizer Spar Tube · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 2 more. Effective Mar 21, 2000
- [AD 99-09-16](https://openairdocs.org/ad/99-09-16): Main Rotor Blade Inspection · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 2 more. Effective May 13, 1999
- [AD 98-16-02](https://openairdocs.org/ad/98-16-02): Tail Rotor Blade · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 7 more. Effective Sep 4, 1998
- [AD 88-12-11](https://openairdocs.org/ad/88-12-11): Main Drive Shaft · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 5 more. Effective May 20, 1988
- [AD 85-07-07](https://openairdocs.org/ad/85-07-07): Control Rod · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 3 more. Effective Apr 19, 1985
- [AD 81-06-04](https://openairdocs.org/ad/81-06-04): Transmission Deck & Bellcrank Support · Airbus Helicopters SA 318B-Alouette Astazou, SA 318C-Alouette Astazou, SA.315B Alouette III and 4 more. Effective Mar 20, 1981
- [AD 75-27-05](https://openairdocs.org/ad/75-27-05): Main Rotor Blades · Airbus Helicopters SA 3180-Alouette Astazou, SA 318C-Alouette Astazou, SA.315B Alouette III and 6 more. Effective Jan 19, 1976
- [AD 75-24-14](https://openairdocs.org/ad/75-24-14): Excessive Vibration · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 7 more. Effective Oct 30, 1975
- [AD 75-16-06](https://openairdocs.org/ad/75-16-06): Tail Rotor Gear Box · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 6 more. Effective Jul 28, 1975
- [AD 67-15-04](https://openairdocs.org/ad/67-15-04): Tail Rotor Gear Box Drive Shaft · Airbus Helicopters SE 3130-Alouette II. Effective May 14, 1967
- [AD 63-19-05](https://openairdocs.org/ad/63-19-05): Main Rotor Hub · Airbus Helicopters SE 3130-Alouette II. Effective Sep 16, 1963
- [AD 63-19-06](https://openairdocs.org/ad/63-19-06): Main Rotor Shaft · Airbus Helicopters SE 3130-Alouette II. Effective Sep 13, 1963
- [AD 61-22-08](https://openairdocs.org/ad/61-22-08): Tail Rotor Gear Box Bolts · Airbus Helicopters SE 3130-Alouette II. Effective Oct 28, 1961
- [AD 61-16-07](https://openairdocs.org/ad/61-16-07): Main Rotor Hubs · Airbus Helicopters SE 3130-Alouette II. Effective Aug 5, 1961
- [AD 60-11-09](https://openairdocs.org/ad/60-11-09): Rotor Blades · Airbus Helicopters SE 3130-Alouette II
- [AD 58-14-01](https://openairdocs.org/ad/58-14-01): Rotor Blade Bonding · Airbus Helicopters SE 3130-Alouette II
- [AD 58-22-04](https://openairdocs.org/ad/58-22-04): Tail Rotor Drive Shaft · Airbus Helicopters SE 3130-Alouette II
- [AD 59-05-06](https://openairdocs.org/ad/59-05-06): Oilite Bearing Replacement · Airbus Helicopters SE 3130-Alouette II
- [AD 72-16-08](https://openairdocs.org/ad/72-16-08): Cracks in Sleeves Gear Box Oil Line · Airbus Helicopters SA 3180-Alouette Astazou, SA 318B-Alouette Astazou and SA 318C-Alouette Astazou
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 98-12-20](https://openairdocs.org/ad/98-12-20) (historical): Horizontal Stabilizer Spar Tube · Eurocopter France SA 3180-Alouette Astazou, SA 318B-Alouette Astazou, SA 318C-Alouette Astazou and 2 more. Effective Jul 14, 1998

## Registered aircraft by registry model (OpenAirDocs)

- [S N I A S SE 3130 ALOUETTE II](https://openairdocs.org/model/s-n-i-a-s-se-3130-alouette-ii): 7 aircraft (registry code 8680502)
- [S N I A S SA 318C ALOUETTE AST](https://openairdocs.org/model/s-n-i-a-s-sa-318c-alouette-ast): 4 aircraft (registry code 8680511)
- [Sud SA 318C](https://openairdocs.org/model/sud-sa-318c): 4 aircraft (registry code 8680501)
- [Sud Aviation/Eurocopter ALOUETTE II SE313B](https://openairdocs.org/model/sud-aviation-eurocopter-alouette-ii-se313b): 2 aircraft (registry code 8680507)
- [Aerospatiale SA 318C ALOUETTE AST](https://openairdocs.org/model/aerospatiale-sa-318c-alouette-ast): 1 aircraft (registry code 8680514)
- [Aerospatiale SA-318C ALOUETTE II](https://openairdocs.org/model/aerospatiale-sa-318c-alouette-ii): 1 aircraft (registry code 8680520)
- [Sud SA 313B II ALLOUETTE](https://openairdocs.org/model/sud-sa-313b-ii-allouette): 1 aircraft (registry code 8680840)
- [Sud SA 318C ALOUETTE AST](https://openairdocs.org/model/sud-sa-318c-alouette-ast): 1 aircraft (registry code 8680508)
- [Sud SE3130 ALOUETTE II](https://openairdocs.org/model/sud-se3130-alouette-ii): 1 aircraft (registry code 8680210)
- [Airbus Helicopters EC 225 LP](https://openairdocs.org/model/airbus-helicopters-ec-225-lp): 0 aircraft (registry code 8682990)
- [Airbus Helicopters SA 318C](https://openairdocs.org/model/airbus-helicopters-sa-318c): 0 aircraft (registry code 8680779)
- [Eurocopter France SA 318 C ALOUETTE](https://openairdocs.org/model/eurocopter-france-sa-318-c-alouette): 0 aircraft (registry code 868097B)
- [Eurocopter France SE 3130](https://openairdocs.org/model/eurocopter-france-se-3130): 0 aircraft (registry code 8680968)
- [Eurocopter/France SE313B](https://openairdocs.org/model/eurocopter-france-se313b): 0 aircraft (registry code 8680972)
- [S N I A S SA 3180 ALOUETTE-AST](https://openairdocs.org/model/s-n-i-a-s-sa-3180-alouette-ast): 0 aircraft (registry code 8680506)
- [Sud SE313B ALOUETTE II](https://openairdocs.org/model/sud-se313b-alouette-ii): 0 aircraft (registry code 8680823)

## STCs approved under this data sheet (45)

- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the
Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SH4672SW](https://openairdocs.org/stc/SH4672SW): Installation of P3180-9/10 upper sliding window assembly and -11/-12 lower sliding window assembly in the passenger door.. The NORDAM Group LLC
- [STC SH1792SW](https://openairdocs.org/stc/SH1792SW): Foxtronics/Tramm BTI 600 nickel cadmium battery temperature system.. FoxCart GSE, LLC
- [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC
- [STC SH406AL](https://openairdocs.org/stc/SH406AL): Installation of L2700 SA 318 skis.. Airglas Inc.
- [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models.. Technisonic Industries Limited
- [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System.. Atlantic Avionics Inc.
- [STC SH1249SW-D](https://openairdocs.org/stc/SH1249SW-D): Installation of Eastern Rotorcraft Corporation cargo hook model 2A15E.. American Eurocopter Corporation
- [STC SH1253SW-D](https://openairdocs.org/stc/SH1253SW-D): Installation of SEB 505 starter-generator to replace Labinal Starter-generator.. American Eurocopter Corporation
- [STC SH1384SW-D](https://openairdocs.org/stc/SH1384SW-D): Replace existing landing light and anti-collision light.. American Eurocopter Corporation
- [STC SH1913SW-D](https://openairdocs.org/stc/SH1913SW-D): Installation of external cargo carrier.. American Eurocopter Corporation
- [STC SH2215SW-D](https://openairdocs.org/stc/SH2215SW-D): Installation of abrasion resistant tape on main rotor blade leading edge.. American Eurocopter Corporation
- [STC SH4266SW-D](https://openairdocs.org/stc/SH4266SW-D): Alternate parts for installation of Modification AMS 2195.. American Eurocopter Corporation
- [STC SH1913SW](https://openairdocs.org/stc/SH1913SW): Installation of external cargo carrier.. American Eurocopter Corporation
- [STC SH2215SW](https://openairdocs.org/stc/SH2215SW): Installation of abrasion resistant tape on main rotor blade leading edge.. American Eurocopter Corporation
- [STC SR09001RC](https://openairdocs.org/stc/SR09001RC): Installation of Eurocopter window.. Tech-Tool Plastics Inc
- [STC SH695NW](https://openairdocs.org/stc/SH695NW): Installation of Model 2512 weighing system.. Onboard Systems
- [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International
- [STC SH437NW](https://openairdocs.org/stc/SH437NW): Installation of an electronic weighing system (for monitoring cargo weight). Measurement Systems Intl
- [STC SH130WE](https://openairdocs.org/stc/SH130WE): Installation of Nightsun SX-16C searchlight.. Spectrolab, Inc
- [STC SH694NW](https://openairdocs.org/stc/SH694NW): Installation of Model 2512 weighing system.. Onboard Weighing Systems
- [STC SH155WE](https://openairdocs.org/stc/SH155WE): Installation of battery temperature monitor system.. K S Avionics, Inc
- [STC SH540NW](https://openairdocs.org/stc/SH540NW): Installation of onboard weighing system.. Onboard Weighing Systems
- [STC SA1249SW](https://openairdocs.org/stc/SA1249SW): Eastern rotorcraft cargo hook 2A15E.. Thales Avionics, Inc.
- [STC SH1870SW](https://openairdocs.org/stc/SH1870SW): Install 315A-22-11-200 protection assembly for tail drive shaft.. Thales Avionics, Inc.
- [STC SH475AL](https://openairdocs.org/stc/SH475AL): Installation of ASC-3 maintenance platform, -4 maintenance platform step, and -5 personnel step.. Alaskan Sky-Craft Co
- [STC SH440AL](https://openairdocs.org/stc/SH440AL): Installation of cargo baskets.. Alaskan Sky-Craft Co
- [STC SH1277SW](https://openairdocs.org/stc/SH1277SW): Eastern Rotorcraft cargo hook and 'H' frame 17080-1.. Thales Avionics, Inc.
- [STC SH1-175](https://openairdocs.org/stc/SH1-175): American type rate of climb, altimeter, air speed and outside air temperature indicators.. Republic Aviaiton Corp
- [STC SH1-253](https://openairdocs.org/stc/SH1-253): Goodyear floats and United States hardware.. Republic Aviaiton Corp
- [STC SH1-315](https://openairdocs.org/stc/SH1-315): Modification of rotor swash plate.. Republic Aviaiton Corp
- [STC SH1-461](https://openairdocs.org/stc/SH1-461): Engine air inlet duct screens.. Republic Aviaiton Corp
- [STC SH1-475](https://openairdocs.org/stc/SH1-475): Purolator fuel filter element type EP-173 P/N 6656561 and gasket 6656574.. Republic Aviaiton Corp
- [STC SH1-504](https://openairdocs.org/stc/SH1-504): Cabin heating system utilizing Stewart-Warner 940F24 heater.. Republic Aviaiton Corp
- [STC SH1-527](https://openairdocs.org/stc/SH1-527): Transmission gears in transmission box assembly SE 3130 62-30-00; 81P740009 first stage sun gear, one; 81P740006 second stage sun gear, one; 81P740007 satellite gear, twelve.. Republic Aviaiton Corp
- [STC SH1-563](https://openairdocs.org/stc/SH1-563): Tail light modification.. Republic Aviaiton Corp
- [STC SH1-592](https://openairdocs.org/stc/SH1-592): American manufactured instrument panel and cabin dome lighting.. Republic Aviaiton Corp
- [STC SH1-614](https://openairdocs.org/stc/SH1-614): Anti-collision rotating beacon light.. Republic Aviaiton Corp
- [STC SH1-616](https://openairdocs.org/stc/SH1-616): Marginal weather instrument group consisting of directional gyro, gyro horizon and turn-slip indicators.. Republic Aviaiton Corp
- [STC SH1-617](https://openairdocs.org/stc/SH1-617): Grimes eyebrow instrument lights.. Republic Aviaiton Corp
- [STC SH1-618](https://openairdocs.org/stc/SH1-618): Shoulder harness for pilot and copilot.. Republic Aviaiton Corp
- [STC SH1-623](https://openairdocs.org/stc/SH1-623): American type folding 3-man troop seat.. Republic Aviaiton Corp
- [STC SH159EA](https://openairdocs.org/stc/SH159EA): Raybestos-Manhatten Ray-Bond (R) R8001 adhesive as an alternate bond for bonding of Alouette.. Republic Aviaiton Corp

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