# Hawley Richard A1B - Type: Aircraft model (FAA registry) - Registry code: 13017PN - Manufacturer (registry): HAWLEY RICHARD - Model: A1B - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/hawley-richard-a1b 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. None matched. ## Registered aircraft (1) - [N5249H](https://openairdocs.org/aircraft/N5249H): [Burton Anthony A L](https://openairdocs.org/faa-owner/BURTON%20ANTHONY%20A%20L), [San Tan Valley, AZ](https://openairdocs.org/faa-place/AZ/San%20Tan%20Valley), built 1991, S/N 1735 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB GAA18CA213](https://openairdocs.org/ntsb/GAA18CA213), Apr 13, 2018: Hawley Richard A1B (N5249H), Lincoln, CA, substantial damage. Probable cause: The pilot’s failure to maintain directional control during takeoff. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20180412003599A](https://openairdocs.org/incident/20180412003599A), Apr 12, 2018: Hawley Richard A1B (N5249H), Lincoln, CA, Destroyed. On 4/12/18 an experimental aircraft, N5249H crashed at Lincoln regional airport klhm. The pilot was taken to the hospital with some injuries but released… ## Service difficulty reports (28) As reported by operators and repair stations, by the model named in the report. - [SDR 2023F00082](https://openairdocs.org/sdr/2023F00082), Mar 15, 2023: HOSE. ABNORMAL. AFTER TAKE-OFF DURING RETRACTION OF THE LANDING GEAR DOORS REMAINED EXTENDED DUE TO LOOSE OF GREEN HYD LIQUID. -LANDING GEAR EMERGENCY EXTENSION PROCEDURE WAS A - [SDR 2023F00011](https://openairdocs.org/sdr/2023F00011), Dec 29, 2022: ACCUMULATOR. ABNORMAL. RTO + GTB: ABANDONED TAKE OFF (50KTS) HYD BLUE SYS LO PRESS. IN ACCORDANCE WITH AMM 29-12-42-000-001-A/400-001-A THE BLUE POWER ACCUMULATOR FIN 2070GM WAS REMOV - [SDR 2022F00303](https://openairdocs.org/sdr/2022F00303), Aug 8, 2022: ENGINE. BIRD INGESTION. DESCRIPTION: BIRD STRIKE ENGINE #1 RTO WAS PERFORMED AT 185 KTS SUCCESIVE EXPLOTIONS WERE EXPERIENCE AND ENGINE STALLED LATER. ACTION PERFORMED: IAW AMM 05-51-1 - [SDR FG6R202006021017](https://openairdocs.org/sdr/FG6R202006021017), Jun 1, 2020: BLADE. DEBONDED. BLADE SHANK AREA SHOWS TYPICAL PROPELLER WRINKLES IN PAINT. WHILE REMOVING THE DAMAGED PAINT, THE FIBERGLASS LAYERS UNDERNEATH WERE FOUND UN-BONDED AND FLAKING - [SDR 2017FA0000489](https://openairdocs.org/sdr/2017FA0000489), Sep 13, 2017: HINGE. BROKEN. AILERON HINGE ASSEMBLY. AILERON HINGE ASSEMBLY BROKE ON LEFT OUTBOARD AILERON CAUSING THE LEFT AILERON TO JAMB AGAINST THE WING TIP. PILOT LOST AILERON CONTROL. - [SDR 2017FA0000160](https://openairdocs.org/sdr/2017FA0000160), Apr 11, 2017: GEARSHAFT. BROKEN. MAGNETO FAILED IN FLIGHT, FLIGHT WAS MADE TO THE AIRPORT ON THE REMAINING MAGNETO. THE AFFECTED MAGNETO, OLD TYPE LONG COIL TAB, NO SPARK LADDER IN BLOCK. THE F - [SDR 2016FA0000156](https://openairdocs.org/sdr/2016FA0000156), Apr 1, 2016: STRAINER. MISINSTALLED. FUEL GASCOLATOR/STRAINER ON FIREWALL WAS FACTORY-INSTALLED BACKWARD. FUEL FROM TANKS ENTERED THE "OUT" PORT, FUEL GOING TO CARBURETOR WENT OUT THE "IN" PORT. PO - [SDR CA140730018](https://openairdocs.org/sdr/CA140730018), Jul 17, 2014: GAUGE. CRACKED. (CAN) THE FUEL GAUGES IN THIS AIRCRAFT ARE A POLYURETHANE COMPOUND KNOWN AS SUPERTHANE ETHER. ON INSPECTION THEY APPEARED TO BE CRACKING, THOUGH NO FUEL OR VAPO - [SDR CA120913008](https://openairdocs.org/sdr/CA120913008), Jul 8, 2012: HINGE. DAMAGED. (CAN) IAW PILOT`S REPORT, THE UPPER ENGINE COWLING HINGE PIN SLID FORWARD FROM THE PIANO HINGE ASSY FAR ENOUGH THAT IT MADE CONTACT WITH THE PROPELLER BLADES IN - [SDR 2012FA0000694](https://openairdocs.org/sdr/2012FA0000694), Jun 27, 2012: G SWITCH. INOPERATIVE. WHEN TESTING ELT AT ANNUAL INSPECTION, FOUND THE IMPACT SWITCH WOULD NOT WORK AT ALL. INSTALLED NEW SWITCH. - [SDR CA070921004](https://openairdocs.org/sdr/CA070921004), Sep 21, 2007: SEAL. LOOSE. (CAN) REFERENCED TO SDR NR 20070917013 AFTER FINDING COWLING SEAL LODGED IN THE CARB VENTURI. THE PILOT/OWNER OF THIS AIRCRAFT WAS REQUESTED TO CHECK THE CONDIT - [SDR CA070917013](https://openairdocs.org/sdr/CA070917013), Sep 14, 2007: SEAL. DISLODGED. (CAN) ON FINAL APPROACH THE ENGINE SUDDENLY EXPERIENCED A SEVERE LOSS OF POWER WHEN CARB HEAT WAS SELECTED. DURING INSPECTION, AFTER LANDING, A (3) INCH PIECE O - [SDR 2007FA0000863](https://openairdocs.org/sdr/2007FA0000863), Aug 14, 2007: RUDDER PEDAL. FAILED. RUDDER PEDAL OPERATION CAN LEAD TO NO BRAKE OPERATION AT FULL TRAVEL OF RUDDER. SENDING IN THIS FIELD APPROVAL REQUEST FOR A VERNIER MIXTURE CONTROL. BELIEVE TH - [SDR 2005FA0000087](https://openairdocs.org/sdr/2005FA0000087), Apr 30, 2004: WIRE. LOOSE. DURING TROUBLESHOOTING OF WIRES IN VM1000 SYSTEM, WIRE J4-13, VOLTAGE SENSE, CAME LOOSE AND SHORTED TO GROUND. THIS WIRE IS CONNECTED DIRECTLY TO BUS WITH NO CI - [SDR 2004FA0000252](https://openairdocs.org/sdr/2004FA0000252), Nov 6, 2003: AILERON. MISLOCATED. FOUND RIVET IN AILERON LEADING EDGE HAD CAUGHT CORNER OF RIB INSTEAD OF THROUGH CENTER OF RIB. CONDITION IN BOTH LEFT AND RIGHT AILERONS AT WS123. REPAIRED COND - [SDR 2003FA0001128](https://openairdocs.org/sdr/2003FA0001128), Nov 4, 2003: DUCT. CHAFED. GROOVES WORN IN ROCKER BOX OIL RETURN TUBE. AUXILLIARY HEAT AIR DUCT AT LOWER SIDE OF NR 1 CYL WAS RUBBING ON OIL RETURN TUBE. GROOVES APPEARED TO BE 30 PERCENT - [SDR 2003FA0001029](https://openairdocs.org/sdr/2003FA0001029), Oct 1, 2003: TERMINAL. BROKEN. LEFT FORWARD HORIZONTAL STABILIZER STRUT UPPER TERMINAL BROKE. BREAK OCCURED ON THE UPPER THREADED PORTION OF THE FITTING. - [SDR 2002FA0001294](https://openairdocs.org/sdr/2002FA0001294), Nov 13, 2002: LINE. SEPARATED. CENTER SUPPLY PRIMER LINE SEPARATED FROM TEE FITTING AT BACK OF ENGINE. DISCOVERED DURING ATTEMPT AT COLD ENGINE STARTING. NOTICED DIFFICULTY IN STARTING AND FU - [SDR 2002FA0001345](https://openairdocs.org/sdr/2002FA0001345), Nov 7, 2002: SCREEN. MISSING. OIL SCREEN MISSING FROM HOUSING. MISSING INSPECTORS. - [SDR 2002FA0001344](https://openairdocs.org/sdr/2002FA0001344), Nov 7, 2002: INDICATOR. SEPARATED. TRIM ARM INDICATOR CAME OFF ACTUATOR STUD AND JAMMED TRIM WHEEL. CAUSE DUE TO NO RETAINING NUT ON ACTUATOR STUD SCREW. INSTALL RETAINING NUT ON ACTURATOR STUD S - [SDR 2002FA0000579](https://openairdocs.org/sdr/2002FA0000579), Apr 19, 2002: SLIP JOINT. LEAKING. REMOVED MUFFLER/ EXHAUST DUCT ASSEMBLY INTERNAL BAFFLES MISSING, AND NR 4 CYLINDER LOWER SLIP JOINT LEAKING. - [SDR 2002FA0000578](https://openairdocs.org/sdr/2002FA0000578), Apr 19, 2002: BAFFLE. MISSING. REMOVED MUFFLER/ EXHAUST DUCT ASSEMBLY INTERNAL BAFFLES MISSING, AND NR 4 CYLINDER LOWER SLIP JOINT LEAKING. - [SDR 2001FA0000530](https://openairdocs.org/sdr/2001FA0000530), Nov 4, 2001: TIE BOLT. SHEARED. AVIAT HUSKY A1B. BROKEN TIE-ROD BOLT DISCOVERED DURING A POST-FLIGHT PILOT'S INSPECTION. THIS PART ATTACHES THE STRUT (LEFT SIDE STRUT (1 OF 3) = LOWER, ANTERIO - [SDR 2001FA0000370](https://openairdocs.org/sdr/2001FA0000370), Aug 29, 2001: TERMINAL. BROKEN. FORWARD HORIZONTAL STABILIZER STRUT UPPER TERMINAL WAS FOUND BROKEN ON PREFLIGHT. BREAK OCCURED ON .3125 (5/16) THREADED PORTION AT UPPER END OF THREADS. - [SDR 2001FA0000058](https://openairdocs.org/sdr/2001FA0000058), Mar 27, 2001: STRUT. FAILED. LANDING GEAR STRUT FAILED AT WELD DUE TO COMPLETE LACK OF WELD PENETRATION. LANDING GEAR SEPARATED FROM AIRCRAFT AT LANDING. DUE TO WELD FAILURE. - [SDR 20010510AP007](https://openairdocs.org/sdr/20010510AP007), Mar 27, 2001: ATTACH FITTING. SHEARED. TACH 80.2 HOURS LEFT MAIN GEAR ATTACHMENT(FORWARD STRUT) SHEARED OFF AT FUSELAGE ATTACHMENT POINT DURING NORMAL LANDING OF AIRCRAFT. THE WELDED AREA THAT THE LH - [SDR 20000919SH024](https://openairdocs.org/sdr/20000919SH024), Aug 4, 2000: GASKET. MISSING. FILTER ADAPTER WAS MISSING PN MS28773-08 GASKET. AN6289-8D. NUT WAS NOT TORQUED. OIL FILTER ADAPTER WAS LEAKING. (X) - [SDR 20000919SH023](https://openairdocs.org/sdr/20000919SH023), Aug 4, 2000: GASKET. MISSING. FILTER ADAPTER WAS MISSING PN MS28773-08 GASKET. (X) ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Aviat A-1B](https://openairdocs.org/model/aviat-a-1b): 361 registered aircraft, registry code 2210406 --- 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.