# TCDS A55NM: Deutsche Aircraft GmbH - Type: Type certificate data sheet - Status: Current - Holder: Deutsche Aircraft GmbH - Revision: 8 - Revised: February 10, 2022 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Registered aircraft: 21, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/49/7e/497ea6efc34bef6dcabf8880bd02379c61b1e924cb791fc0b409670c87fe2ebb - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/66D7FE17DA2D9EE3862587E500655BD6.0001 - Page: https://openairdocs.org/tcds/A55NM ## Models (1) As the data sheet lists them. - 328-300 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A55NM Revision 8 Deutsche Aircraft GmbH Dornier Model 328-300 February 10, 2022 FAA TYPE CERTIFICATE DATA SHEET NO. A55NM This data sheet which is part of Type Certificate No. A55NM prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the US Federal Aviation Regulations. Type Certificate Holder Deutsche Aircraft GmbH Sonderflughafen Oberpfaffenhofen D-82234 Wessling Germany Type Certificate Holder Record Dornier Luftfahrt GmbH transferred TC A55NM to Fairchild Dornier GmbH, effective August 8, 2000. Fairchild Dornier GmbH transferred TC A55NM to AvCraft Aerospace GmbH, effective July 28, 2003. AvCraft Aerospace GmbH transferred TC A55NM to 328 Support Services GmbH, effective June 7, 2006. 328 Support Service GmbH re-named to Deutsche Aircraft GmbH, effective October 6, 2021. 1. Model Dornier 328-300 (Transport Category Airplane) approved July 15, 1999 1.1 MTOW Increase (Mod 10) Major modification “Mod 10”, which is covered by Dornier Change Notice CN-F0053, was approved by FAA on April 17, 2000. The following data are valid for both the basic 328-300 aircraft, as well as for Mod 10 aircraft, except where specifically noted. 1.2 Flight Level 350 Option Major modification covered by Dornier Change Notice CN-F0166, was approved by FAA on March 26, 2001. The following data are valid for both the basic 328-300 aircraft, as well as for aircraft incorporating Change Notice CN-F0166, except where specifically noted. Engines 2 Pratt and Whitney of Canada Ltd. PW 306B turbofan engines. Refer to engine FAA-Type Certificate E35NE. Auxiliary Power Unit One Honeywell Model: GTCP 36-150. For details refer to AFM No. AM-AFM- 050599-ENV, Section 02-06-00, page 6. Fuel (a) Specifications: ASTM (D 1655) Jet A ASTM (D 1655) Jet A1 ASTM (D 1655) Jet A-2 IATA Kerosene Type Fuel (b) Additives: According to Dornier 328-300 Aircraft Maintenance Manual Document No. TM- AMM-010399-ENV. Oil Types of approved oils for use in PW 306B engines are: - 5 Centistoke oils (conforming to specification PWA 521, Type II). - Third generation oils. Engine Model PW306B Limits Refer to AFM No. AM-AFM-050599-ENV Page No. 1 2 3 4 5 Rev. No. 8 7 7 7 7 A55NM 2 Airspeed Limits (I.A.S.) VMO 270 KIAS from sea level to 8,000 ft increasing linearly to 300 KIAS at 10,000 ft VMO MMO 300 KIAS from 10,000 ft to 20,700 ft 0.66 from 20,700 ft to 31,000 ft VA (Maneuvering) 190 KIAS from sea level to 31,000ft. VFE (Flaps Extended) 12° 12° 200 KIAS for Basic 205 KIAS for Mod 10 20° 180 KIAS 32° 160 KIAS VLE = VLO Tire Speed 200 KIAS 210 MPH Windshield wiper operating speed 166 KIAS Datum The aircraft reference zero datum point (QE 0) is located 59.05 in. (1,500 mm) forward of the fuselage nose cone and 98.425 in. under the fuselage centerline and the aircraft buttock line. The 0% MAC datum is located 369.21in. (9.378m) aft of the reference datum (QE 0). Mean Aerodynamic Chord The MAC length is 80.20 in. (2.037 m) Leveling Means Measuring marks are provided on the aircraft for leveling. These marks are indicated by special rivets or drillings as shown and described in the Weight & Balance Manual, Document No. TM- WBM-010399-ENV. Maximum Weights For Basic Max Ramp Weight: 33841 lb. (15350 kg) Max Takeoff Weight: Max Landing Weight: Max Zero Fuel Weight: 33510 lb. (15200 kg) 31063 lb. (14090 kg) 27800 lb. (12610 kg) For Mod 10 Max Ramp Weight: 34789 lb. (15780 kg) Max Takeoff Weight: Max Landing Weight: Max Zero Fuel Weight: 34524 lb. (15660 kg) 31724 lb. (14390 kg) 28814 lb. (13070 kg) Center of Gravity Limits Refer to AFM No. AM-AFM-050599-ENV Minimum Crew 2 - Pilot and copilot Maximum Passenger Seating Capacity 33 Type of Baggage Compartment Class "D" Compartment (rear) Maximum Baggage Total of 1653 lbs (750 kg) in the rear baggage compartment - 882 lbs (400 kg) in the forward part - 771 lbs (350 kg) in the aft part - max. floor loading = 75 lb/ft2 Fuel Capacity 7970 lbs usable (gravity refueled) 7800 lbs usable (pressure refueled) 3 A55NM Oil Capacity Oil capacity per Engine MAX OIL TANK MIN OIL TANK US Gallons 2.11 0.79 Liters 8.00 3.00 Maximum Operating Altitude 31,000 ft. for basic aircraft 35,000 ft. for aircraft incorporating Change Notice CN-F0166 Control Surface Movements Wing Flaps 12°, 20°, and 32° Ailerons 28° up (+1°), 25° down (+1°) Elevator 30° up (-2°), 25° down (-1°) Stabilizer Rudder fixed 24° right (+1°), 24° left (-1°) Serial Numbers Serial Numbers for Basic: 3105 up to and including 3144, 3146, 3148 3151, 3152, 3153, 3154, 3158, 3159 Serial Numbers for Mod 10: 3145, 3147, 3149, 3150, 3155, 3156, 3157, 3160 and subsequent The following serial numbers are declared Non-TC compliant aircraft and excluded from the TCDS due to production details and known non-conformities: Former test article aircraft S/No’s.:3099, 3102 Import Requirements The FAA can issue a U.S. airworthiness certificate based on an Export Certificate of Airworthiness (Export C of A) signed by a representative of the LBA 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 conform with the Type Design approved under U.S. Type Certificate No. A55NM and to be in a condition for safe operation.’ The U.S. airworthiness certification basis for aircraft type certificated under 14 CFR Part 21, section 21.29, exported by country of manufacture is section 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated under section 21.29 exported from countries other than the country of manufacture (e.g., third party country) is section 21.183(d) or 21.185(b). Certification Basis 14 CFR part 25 Effective February 1, 1965, including Amendments 25-1 through 25-87. Additionally, Dornier elected to comply voluntarily with §25.351 as amended by Amendment 25-91. For aircraft incorporating Flight Level 350 modification (Change Notice CN- F0166), Dornier elected to comply voluntarily with §25.832 as amended by Amendment 25-94. Special Conditions: - No. ANM-99-273, “High Intensity Radiated Fields (HIRF) Protection. Exemptions: - No. 6895 for FAR 25.1435(b)(1) Hydraulic System Test - No. 6900 for FAR C36.9(e)(1) Approach Speed for Noise Equivalent Level of Safety Findings: - Use of 1g Stall Criteria (various FARs) - Rejected Takeoff and Landing Performance Criteria (FAR 25.101, 25.105, 25.109, 25.113, 25.115, 25.735, and 25.1587) - Lavatory Fire Protection (FAR 25.854(a)) - Flight crew top hatch emergency exit markings (FAR 25.811(f)) Optional Requirements complied with: - FAR 25.1419 Icing A55NM 4 Environmental Standards complied with: - FAR Part 36 effective December 1, 1969, including Amendments 36-1 through 36-21. - FAR Part 34 effective September 10, 1990, including Amendment 34-1 through 34-3. Additional Design Requirements complied with per FAR 21.21(b)(2): - Ice Contaminated Tailplane Stall (Issue Paper F-3) - Roll Control in Supercooled Large Droplet Conditions (Issue Paper S-2) Based on 14 CFR section 21.29(a) for new import TCs, or section 21.101(g) for changes to TCs, applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. The Luftfahrt-Bundesamt (LBA) originally type certificated this aircraft under its type certificate Number 2534. The FAA validated this product under U.S. Type Certificate number A55NM. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Federal Republic of Germany. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see the Certification Basis) must be installed in the aircraft. The lists of all equipment as well as optional approved equipment are contained in the document: Equipment approved for the Model Dornier 328-100 is listed in Document No. TD-34000, Equipment Register Document. Airplane Flight Manual EASA approved Airplane Flight Manual AM-AFM-050599-ENV. Service Information Each of the documents listed below that contain a statement that it is approved by the European Aviation Safety Agency (EASA) – or for approvals made before September 28, 2003 – by the LBA, are accepted by the FAA and are considered FAA approved. Additionally, the type certificate holder has contracted with 328 Design GmbH (328DO) as the EASA approved DOA holder. Approvals issued by 328DO or by the TC holder under the authority of EASA approved design organization EASA.21J.438 – or for approvals made prior to September 28, 2003 – by the TC holder under the authority of LBA approved design organization LBA.JA.002, are considered FAA approved. These approvals pertain to the design data only.  TC holder Service Bulletins, except as noted below,  Structural repair manuals  Vendor manuals referenced in TC holder Service Bulletins  Airplane flight manuals  Repair instructions. Note: Design changes that are contained in TC holder Service Bulletins and that are classified as Level 1 Major in accordance with the FAA/EASA agreed Technical Implementation Procedures for Airworthiness and Environmental Certification (TIP latest Revision), must be approved by the FAA. 5 A55NM NOTES NOTE 1. Current weight and balance report including a list of equipment included in certificated e mpty weight, and loading instructions when necess ary must be provided for each aircraft at its delivery. For further information see Weight & Balance Manual TM-WBM-010399- ENV NOTE 2. Airworthiness Limitations including structural inspections and retirement times for safe-life parts are listed in Dornier Airworthiness Limitations Document TM-ALD-010599-ALL. NOTE 3. Certification Maintenance Requirements (CMR) are listed in Document TM- CMR-010599-ALL. The CMR Document is attached as an appendix to the MRB Document TM-MRB-010599-ALL. NOTE 4. Compliance with the optional ditching requirements of FAR 25.801, FAR 25.1411, and FAR 25.1415 has not been shown. ...END... ``` ## ADs (58, first 50, in force first) - [AD 2025-15-05](https://openairdocs.org/ad/2025-15-05): Fuel · Deutsche 328-100 and 328-300. Effective Sep 3, 2025 - [AD 2025-06-08](https://openairdocs.org/ad/2025-06-08): Landing gear · Deutsche 328-100 and 328-300. Effective May 8, 2025 - [AD 2024-19-16](https://openairdocs.org/ad/2024-19-16): Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Nov 26, 2024 - [AD 2023-23-07](https://openairdocs.org/ad/2023-23-07): Flight Controls · Deutsche 328-100 and 328-300. Effective Jan 16, 2024 - [AD 2022-21-07](https://openairdocs.org/ad/2022-21-07): Placards and markings, Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Dec 15, 2022 - [AD 2020-09-13](https://openairdocs.org/ad/2020-09-13): Time Limits/Maintenance Checks · 328 Support Services 328-300. Effective Jun 22, 2020 - [AD 2018-19-13](https://openairdocs.org/ad/2018-19-13): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Oct 31, 2018 - [AD 2018-03-02](https://openairdocs.org/ad/2018-03-02): Fuselage · 328 Support Services 328-300. Effective Feb 23, 2018 - [AD 2017-21-06](https://openairdocs.org/ad/2017-21-06): Fuel · 328 Support Services 328-100 and 328-300. Effective Dec 20, 2017 - [AD 2014-03-15](https://openairdocs.org/ad/2014-03-15): Placards and Markings; and Doors. · 328 Support Services 328-100 and 328-300. Effective Apr 9, 2014 - [AD 2012-07-03](https://openairdocs.org/ad/2012-07-03): Equipment/Furnishings · 328 Support Services 328-100 and 328-300. Effective May 10, 2012 - [AD 2012-01-08](https://openairdocs.org/ad/2012-01-08): Flight Controls · 328 Support Services 328-100 and 328-300. Effective Feb 29, 2012 - [AD 2011-18-13](https://openairdocs.org/ad/2011-18-13): Wings · 328 Support Services 328-100 and 328-300. Effective Oct 25, 2011 - [AD 2011-15-07](https://openairdocs.org/ad/2011-15-07): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Aug 22, 2011 - [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010 - [AD 2009-01-06 R1](https://openairdocs.org/ad/2009-01-06-R1): Auxiliary fuel system · 328 Support Services 328-300. Effective Nov 23, 2009 - [AD 2009-18-14](https://openairdocs.org/ad/2009-18-14): Flight controls · 328 Support Services 328-100 and 328-300. Effective Oct 14, 2009 - [AD 2009-10-03](https://openairdocs.org/ad/2009-10-03): Flight controls · 328 Support Services 328-100 and 328-300. Effective May 26, 2009 - [AD 2005-13-03](https://openairdocs.org/ad/2005-13-03): Flight control systems · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005 - [AD 2005-13-04](https://openairdocs.org/ad/2005-13-04): Fuselage drain line · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005 - [AD 2005-10-06](https://openairdocs.org/ad/2005-10-06): Left- and right-hand elevator horns · 328 Support Services 328-300. Effective Jun 16, 2005 - [AD 2005-10-02](https://openairdocs.org/ad/2005-10-02): Wing leading edge · 328 Support Services 328-300. Effective Jun 15, 2005 - [AD 2005-05-11](https://openairdocs.org/ad/2005-05-11): Main landing gear (MLG) · 328 Support Services 328-300. Effective Apr 18, 2005 - [AD 2004-22-06](https://openairdocs.org/ad/2004-22-06): Metal oxide varistor (MOV) modules · 328 Support Services 328-100 and 328-300. Effective Dec 2, 2004 - [AD 2004-09-22](https://openairdocs.org/ad/2004-09-22): Ground cooling fan · 328 Support Services 328-300. Effective Jun 15, 2004 - [AD 2004-09-38](https://openairdocs.org/ad/2004-09-38): Ground spoiler assemblies · 328 Support Services 328-300. Effective Jun 15, 2004 - [AD 2004-09-12](https://openairdocs.org/ad/2004-09-12): Passenger seats · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004 - [AD 2004-09-17](https://openairdocs.org/ad/2004-09-17): Rudder spirng tab · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004 - [AD 2004-08-18](https://openairdocs.org/ad/2004-08-18): Motive Flow Check Valves · 328 Support Services 328-300. Effective Jun 1, 2004 - [AD 2004-03-16](https://openairdocs.org/ad/2004-03-16): Fire extinguisher control panels · 328 Support Services 328-300. Effective Mar 17, 2004 - [AD 2003-20-02](https://openairdocs.org/ad/2003-20-02): Anti-ice tubing · 328 Support Services 328-300. Effective Nov 4, 2003 - [AD 2003-19-03](https://openairdocs.org/ad/2003-19-03): Nose landing gear (NLG) · 328 Support Services 328-100 and 328-300. Effective Oct 27, 2003 - [AD 2003-05-08](https://openairdocs.org/ad/2003-05-08): Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) Impact Switches · 328 Support Services 328-100 and 328-300. Effective Apr 18, 2003 - [AD 2003-03-17](https://openairdocs.org/ad/2003-03-17): Aileron, Elevator, Rudder Trim Tabs, and Rudder Spring Tab Screws · 328 Support Services 328-100 and 328-300. Effective Mar 12, 2003 - [AD 2002-26-21](https://openairdocs.org/ad/2002-26-21): Electrical wire harness · 328 Support Services 328-100 and 328-300. Effective Feb 12, 2003 - [AD 2002-26-06](https://openairdocs.org/ad/2002-26-06): Airplane Flight Manual (AFM) · 328 Support Services 328-300. Effective Jan 17, 2003 - [AD 2002-16-16](https://openairdocs.org/ad/2002-16-16): Actuating cartridge on the auxiliary power unit (APU) · 328 Support Services 328-100 and 328-300. Effective Sep 23, 2002 - [AD 2002-16-13](https://openairdocs.org/ad/2002-16-13): Rudder spring tab · 328 Support Services 328-100 and 328-300. Effective Sep 20, 2002 - [AD 2002-03-15](https://openairdocs.org/ad/2002-03-15): Left- and Right-Hand Potentiometer Levers of the Aileron Flight Control System · 328 Support Services 328-100 and 328-300. Effective Mar 27, 2002 - [AD 2001-26-18](https://openairdocs.org/ad/2001-26-18): Forward Engine Mount Vibration Isolators · 328 Support Services 328-300. Effective Feb 8, 2002 - [AD 2001-13-08](https://openairdocs.org/ad/2001-13-08): Brake Assemblies · 328 Support Services 328-300. Effective Aug 1, 2001 - [AD 2001-12-04](https://openairdocs.org/ad/2001-12-04): Hydraulic Line · 328 Support Services 328-300. Effective Jul 18, 2001 - [AD 2000-26-13](https://openairdocs.org/ad/2000-26-13): Hydraulic Accumulators · 328 Support Services 328-300. Effective Jan 17, 2001 - [AD 2000-21-13](https://openairdocs.org/ad/2000-21-13): Parking Brake · 328 Support Services 328-300. Effective Nov 29, 2000 - [AD 2000-04-23](https://openairdocs.org/ad/2000-04-23): Rudder Spring Tab · 328 Support Services 328-100 and 328-300. Effective Mar 22, 2000 - [AD 98-24-27](https://openairdocs.org/ad/98-24-27): Fire Extinguisher · 328 Support Services 328-100, 328-300, A320-111 and 42 more. Effective Jan 29, 1999 - [AD 94-19-06](https://openairdocs.org/ad/94-19-06): Crew Oxygen Masks · 328 Support Services 328-100, 328-300, 500 and 17 more. Effective Oct 6, 1994 - [AD 2024-03-07](https://openairdocs.org/ad/2024-03-07) (historical): Fuel · Deutsche 328-100 and 328-300. Effective Apr 16, 2024 - [AD 2011-01-07](https://openairdocs.org/ad/2011-01-07) (historical): Flight controls · 328 Support Services 328-100 and 328-300. Effective Feb 9, 2011 - [AD 2009-21-06](https://openairdocs.org/ad/2009-21-06) (historical): Equipment/furnishings. · 328 Support Services 328-100 and 328-300. Effective Nov 20, 2009 All 58: https://openairdocs.org/tcds/A55NM/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Fairchild Dornier DORNIER 328-300](https://openairdocs.org/model/fairchild-dornier-dornier-328-300): 11 aircraft (registry code 3370601) - [Dornier 328-300](https://openairdocs.org/model/dornier-328-300): 7 aircraft (registry code 2990220) - [Dornier Luftfahrt DORNIER 328-300](https://openairdocs.org/model/dornier-luftfahrt-dornier-328-300): 2 aircraft (registry code 2996001) - [Dornier Luftfahrt 328-300](https://openairdocs.org/model/dornier-luftfahrt-328-300): 1 aircraft (registry code 2990221) - [Fairchild 328-300](https://openairdocs.org/model/fairchild-328-300): 0 aircraft (registry code 3370640) ## STCs approved under this data sheet (23) - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc. - [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC - [STC ST04508NY](https://openairdocs.org/stc/ST04508NY): Installation of ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST03654NY](https://openairdocs.org/stc/ST03654NY): Installation of Control Horn Anti-Icers. SMR Technologies Inc - [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC - [STC ST10933SC](https://openairdocs.org/stc/ST10933SC): Installation of an Executive Interior and Reduction in Maximum Zero Fuel Weight form 28,814 to 28,279 pounds.. VT DRB Aviation Consultants - [STC ST10940SC](https://openairdocs.org/stc/ST10940SC): Installation of an Executive Interior and Maximum Zero Fuel Weight limitation reduction from 28,814 pounds (13,070 kg) to 28,279 pounds (12,854 kg). VT DRB Aviation Consultants - [STC ST01181SE](https://openairdocs.org/stc/ST01181SE): Installation of increased security cockpit door. Cascade Aviation Services Inc - [STC ST04169AT](https://openairdocs.org/stc/ST04169AT): Installation of EL/M-2022A(V) 3 Multimode Surveillance Radar System (MSRS). TKC Aerospace, Inc. - [STC ST03394CH](https://openairdocs.org/stc/ST03394CH): Installation of a cabin interior alteration. TKC Aerospace, Inc. - [STC ST00664DE](https://openairdocs.org/stc/ST00664DE): Replacement of existing 33-place cabin configuration with 12 passenger executive configeratin.. Zenith Aviation Inc - [STC ST02485LA](https://openairdocs.org/stc/ST02485LA): Installation of FLIR turret, KU-Band antenna, and radome. TKC Aerospace, Inc. - [STC ST02636NY](https://openairdocs.org/stc/ST02636NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG - [STC ST02132LA](https://openairdocs.org/stc/ST02132LA): Installation of Cabin Interior Noise Reduction Kit. Aircraft Technical Development Inc. dba Aerocon Engineering Company - [STC ST00188BO](https://openairdocs.org/stc/ST00188BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit.. Pratt & Whitney Engine Services Inc. - [STC ST09993SC](https://openairdocs.org/stc/ST09993SC): Installation of interior shell, cabinetry, seats, card tables, monitors, entertainment system, system wiring, and lavatory.. AvCraft Support Services Inc. - [STC SA09496AC](https://openairdocs.org/stc/SA09496AC): Conversion of the lavatory water supply system from a gravity feed to a pressure system by adding a pump, a small hot water tank and control system and by replacing the single lever faucet with an infrared activated faucet with hot and cold capability in accordance with Fairchild Aircraft Drawing SATA380G0010, Water System Mod -- Hot/Cold, Revision B dated November 22, 1999, or later FAA approved revision.. AvCraft Aviation LLC - [STC SA09839SC](https://openairdocs.org/stc/SA09839SC): Installation of Teledyne Telelink Data Link System.. Aircraft Systems & Mfg --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.