Date:	Saturday 23 June 2012
Time:	19:55
Type:	de Havilland DH.82A Tiger Moth II
Owner/operator:	Nicholas John Baker
Registration:	N523R
MSN:	82960
Total airframe hrs:	3472 hours
Engine model:	De Havilland GIPSY MAJOR
Fatalities:	Fatalities: 0 / Occupants: 2
Aircraft damage:	Substantial
Category:	Accident
Location:	Near the intersection of Jurupa Avenue and Poplar Street, Fontana, CA -   United States of America
Phase:	En route
Nature:	Private
Departure airport:	Flabob Airport, Riverside, CA (RIR/KRIR)
Destination airport:	Cable Airport, Upland, San Bernardino County, CA (KCCB)
Investigating agency:	NTSB
Confidence Rating:	Accident investigation report completed and information captured

Narrative:
de Havilland DH.82A Tiger Moth MSN 82960 (Gipsy Major #82874): Taken on charge by the RAF as R5065 at 8 MU RAF Little Rissington, Gloucestershire 28.3.40. To 6 EFTS RAF Sywell, Northamptonshire 13.11.40. To 38 MU RAF Llandow, Glamorgan 22.10.45 for long-term storage.

Struck off charge when sold 25.1.50 to Defford Flying Club. Registered as G-ANEI (C of R R4153/1) 29.9.53 to Defford Aero Club (Worcester) Ltd, Defford [later Pershore] Worcestershire. C of A issued 28.1.55. . C of A lapsed 1.5.59; renewed 17.8.60. C of A lapsed 14.9.62. C of A renewed 15.5.64.

Registration G-ANEI cancelled 19.5.64 and re-registered (C of R R4153/2) 25.5.64 to Holding & Barnes Ltd, Ilford, Essex (aircraft based Stapleford Tawney, Abridge, Essex). A Bill of Sale dated 19.8.64 stated that aircraft had been sold 3.3.64 by Lewis J Benjamin (sole owner) to Robertson Associates, Beverley Hills, Los Angeles, CA for $900 (although the document was not notarized 17.5.66). Sold 20.8.64 to D S Green, Weybridge, Surrey (presumably as nominee); sold on to Cliff Robertson in California, USA and registration G-ANEI cancelled 25.3.65.

Ferried to Cherbourg 25.9.64 and then probably to Germany. Returned to Croydon late 1965 and shipped early 1966 to Cliff Robertson, Los Angeles, California. UK export C of A E4153 issued 16.5.66. US Registered as N523R (application dated 19.6.66) 20.6.66 to Robertson & Associates, Beverley Hills, CA (later Van Nuys, CA). C of A issued 11.8.66. Accident 12.5.67 when undershot on approach to Santa Paula Airport, CA and undercarriage struck rocks (see link #10), Repaired and returned to service.

Sold 29.4.69 and re-registered 23.5.69 to Clifford P Robertson, Los Angeles [aircraft based at Santa Paula, CA]. Used to obtain FAA Type Certificate; issued 7.2.66. C of A issued 1.10.69. Operated in film “Villa Rides” in 1968 in which it was deliberately crashed; later repaired. According to one source (see link #9) Tiger Moth N523R has had, on at least two occasions. "celebrity pilots": "...the logbooks he does have are very revealing about the aircraft’s history. Charles Lindbergh flew the plane in September 1969, and below his signature with a later date is astronaut Buzz Aldrin’s signature".

Re-registered 21.2.82 to Nicholas J Baker, Santa Barbara, CA (later Torrance, CA); Subsequently ground-looped in film “The Aviator” (1985). Later painted in 1954-era colours as G-ANEI. Fitted with Gipsy Major #8438 [5.2005]. Badly damaged in forced landing in field near intersection of Jurupa Avenue & Poplar Street, Fontana, CA 23.6.2012 following engine failure; no injuries. According to the NTSB report into the accident:

"HISTORY OF FLIGHT
On June 23, 2012, about 1955 Pacific daylight time, a DeHavilland DH 82A (Tiger Moth), N523R, nosed over following a forced landing near Fontana, California. The pilot was operating the airplane under the provisions of 14 Code of Federal Regulations Part 91. The airline transport pilot and passenger were not injured. The airplane sustained substantial damage to the aft fuselage, rudder, and upper wings during the accident sequence. The local flight departed Flabob Airport, Riverside/Rubidoux, California, about 1950, with a planned destination of Cable Airport, Upland, California. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported that the initial climb after takeoff was uneventful. He leveled the airplane for cruise once they had reached an altitude of 2,000 feet mean sea level (msl), and reduced the engine speed from 2,300 to 2,000 rpm. He then noticed an additional reduction in engine speed, accompanied by a vibration. He applied full engine throttle control, but the engine speed did not increase. With a field in view, he elected to immediately perform a forced landing. The airplane was not at a sufficient altitude for him to turn the airplane into the wind, and during the landing roll, the airplane nosed over.

=AIRPLANE INFORMATION=
Federal Aviation Administration (FAA) records revealed that the two-seat biplane was manufactured in the United Kingdom in 1940, and imported to the United States in 1965, where it was subsequently purchased by the pilot in 1987.

The airplane was equipped with a four-cylinder, air-cooled, DeHavilland Gipsy Major Series 1C Engine, serial number 8438. Maintenance records indicated that at the time of the last annual inspection, which occurred on November 1, 2011, the airframe had amassed a total of 3,472 flight hours, with the engine a total of 683 hours since overhaul in 1966. The pilot reported that the airplane had flown for 17 hours since the inspection.

=TESTS AND RESEARCH=
Examination
The airplane was recovered from the accident site, and subsequently examined by the NTSB investigator-in-charge. Examination of the engine revealed that the forward clamping bolt for the cylinder number four rocker bracket assembly had separated, allowing the assembly to partially detach from the head. As a result, the rocker arm had become displaced from the exhaust valve. The bolt head and shank was loose within the rocker cover, with its separated end located in the cylinder head assembly. Examination of the bolt revealed that it was about 8 millimeters in diameter, and had separated about 4 millimeters past its shank. The threaded bolt tip remained within the nut, with its cotter pin still in place. The bolt sustained peening damage across its entire surface, and examination of the fracture face revealed granular textured features, with a series of semicircular striations emanating from a thread fillet. The bolt head exhibited an indiscernible manufacture marking, which did not correspond to any current Military or National Aerospace Standards.

Examination of the remaining cylinders revealed an alternate rocker clamping method had been employed, which utilized three internal-wrenching hexagon drive bolts, secured with interconnecting safety wire.

=Cylinder Head Modification=
Rolls Royce Modification News Sheet, Number 1448, issued March 17, 1950, detailed a modification to the rocker bracket assembly designed to obviate failure of the clamping bolts. The modification requires performing a minor alteration to the bracket, and then installing larger, 9-millimeter diameter bolts, along with a one piece locking plate instead of the castellated nuts and cotter pins.

Logbook records dating back to 1997 revealed that the engine had undergone maintenance requiring the removal of all four cylinder heads on three occasions. The last removal occurred in January 2009, when new pistons were installed. No record was located indicating the 1448 modification had been performed, and no documentation could be found detailing the installation of the internal-wrenching hexagon drive bolts on cylinders one, two, and three.

Examination of FAA records did not reveal the existence of any airworthiness directives for this engine model, and no other instance of this type of failure was located within the FAA service difficulty report database.

FAA regulations do not require compliance with service letters, service bulletins, and modification sheets for aircraft operated under part 91.

NTSB Probable Cause=
Partial loss of engine power during cruise flight due to a failed engine cylinder rocker assembly clamping bolt. Contributing to the accident was the failure of unknown maintenance personnel to perform a modification to the assembly that would have prevented the failure".

Still on rebuild [2017]. Registration ccancelled 17.1.2018 by FAA as "expired"

1. Royal Air Force Aircraft R1000-R9999 (James J Halley, Air Britain, 1980)
2. CAA History of G-ANEI 1953-64: https://cwsprduksumbraco.blob.core.windows.net/g-info/HistoricalLedger/G-ANEI-1.pdf
3. CAA History of G-ANEI 1964-65: https://cwsprduksumbraco.blob.core.windows.net/g-info/HistoricalLedger/G-ANEI-2.pdf
4. https://air-britain.com/pdfs/production-lists/DH82.pdf
5. http://www.airhistory.org.uk/dh/p829.html
6. FAA: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N523R
7. NTSB Number WPR12LA275: https://data.ntsb.gov/Docket?ProjectID=84071
8. https://planecrashmap.com/plane/ca/N523R/
9. http://airportjournals.com/cable-airports-celebrity-tiger-moth/
10. NTSB (Accident 12.5.1967) - NTSB Identification: LAX67F0449: https://www.ntsb.gov/Pages/brief.aspx?ev_id=19228&key=0
11. https://en.wikipedia.org/wiki/Flabob_Airport
12. https://en.wikipedia.org/wiki/Cable_Airport
13. Villa Rides (1968 movie): https://www.imdb.com/title/tt0063775/?ref_=nv_sr_srsg_0
14. The Aviator (1985 movie): https://www.imdb.com/title/tt0088758/?ref_=fn_al_tt_2

Tiger Moth N523R (still marked as G-ANEI) Cable Airport Airshow 1 October 2004

Date/time	Contributor	Updates
24-Jun-2012 03:52	gerard57	Added
24-Jun-2012 06:37	RobertMB	Updated [Time, Aircraft type, Registration, Cn, Location, Nature, Source, Narrative]
21-Dec-2016 19:28	ASN Update Bot	Updated [Time, Damage, Category, Investigating agency]
27-Nov-2017 20:45	ASN Update Bot	Updated [Other fatalities, Departure airport, Destination airport, Source, Narrative]
07-Feb-2022 13:03	Dr. John Smith	Updated [Time, Operator, Other fatalities, Source, Embed code, Narrative]
07-Feb-2022 15:08	Dr. John Smith	Updated [Operator, Departure airport, Destination airport, Source, Narrative]
07-Feb-2022 15:19	Dr. John Smith	Updated [Destination airport, Source, Narrative]