# Morris Motors DH82A - Type: Aircraft model (FAA registry) - Registry code: 2802711 - Manufacturer (registry): MORRIS MOTORS LTD - Model: DH82A - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A5PC](https://openairdocs.org/tcds/A5PC) (OpenAirDocs) - Holder: Williams Harry E. - Registered aircraft: 0 - Page: https://openairdocs.org/model/morris-motors-dh82a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2014-24-01](https://openairdocs.org/ad/2014-24-01): Fuselage, Wing Attach Fittings · de Havilland D.H.83 Fox Moth, D.H.82A Tiger Moth and DH 82A. Effective Jan 6, 2015 - [AD 2014-17-09](https://openairdocs.org/ad/2014-17-09): Fuselage, Wing Attach Fittings · Williams Harry E. D.H.83 Fox Moth, D.H.82A Tiger Moth and DH 82A. Effective Sep 18, 2014 ## Information bulletins (advisory) (2) - [SAIB CE-17-21](https://openairdocs.org/saib/CE-17-21): Wing and Aileron; De Havilland DH60, DH82A, and DH83 Wing Spars Produced by the Croydon Aircraft Company of New Zealand. Issued Aug 18, 2017 - [SAIB ACE-98-39](https://openairdocs.org/saib/ACE-98-39): . Issued Jul 6, 1998 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (4) As reported by operators and repair stations, by the model named in the report. - [SDR QXEA2013091001346](https://openairdocs.org/sdr/QXEA2013091001346), Aug 17, 2013: SEAT TRACK. CORRODED. CORROSION FOUND ON RT INBD SEAT TRACK AT FS 373.15. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-0 - [SDR QXEA2013022100398](https://openairdocs.org/sdr/QXEA2013022100398), Feb 21, 2013: FRAME. CORRODED. FRAME FLANGES AT FR 176 STR 32-30P HAVE CORROSION. REMOVED 1 EA RIVET TO FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01, 53-00-00-02-09 REV 12 AND DISPLACED W - [SDR 2012FA0000512](https://openairdocs.org/sdr/2012FA0000512), Jul 26, 2012: BOLT. SEPARATED. BOLT SEPARATED DUE TO HEAVY CORROSION. - [SDR QXEA2011083000767](https://openairdocs.org/sdr/QXEA2011083000767), Aug 26, 2011: STRINGER. CORRODED. STRINGER 30S IS CORRODED, FRAME 1.00 TO 19.4. REMOVED CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3888, MINIMUM REMAINING THICKNESS .057", CONFIRMED CRACK FR ## STCs that may be installed (OpenAirDocs) (9) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA00192LA](https://openairdocs.org/stc/SA00192LA): Replacement of BTH AG4 impluse and nonimpulse magnetos with Slick Magnetos on Gipsy I, Gipsy II, and Gipsy III model engines and Gipsy major series 1 through 10MK2 model engines. Moth Aircraft Company - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. Electronics International Inc - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Electronics International Inc ## PMA parts (OpenAirDocs) (12) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145563422120260806152349.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026 - [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143338250420260806152441.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026 - [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Dehavilland DH82A](https://openairdocs.org/model/dehavilland-dh82a): 8 registered aircraft, registry code 2800101 - [Dehavilland-Schildberg DH 82A](https://openairdocs.org/model/dehavilland-schildberg-dh-82a): 1 registered aircraft, registry code 2801001 - [Dehavilland/Oliver DH-82A](https://openairdocs.org/model/dehavilland-oliver-dh-82a): 0 registered aircraft, registry code 2801003 --- 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.