# Breecher Raymond/Breecher Carl 77 - Type: Aircraft model (FAA registry) - Registry code: 05636XS - Manufacturer (registry): BREECHER RAYMOND/BREECHER CARL - Model: 77 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 ยท Reciprocating - Seats: 1 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/breecher-raymond-breecher-carl-77 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 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 (15) As reported by operators and repair stations, by the model named in the report. - [SDR 2017FA0000301](https://openairdocs.org/sdr/2017FA0000301), Jul 3, 2017: COIL. FAILED. ENGINE HAD A LOSS OF POWER, THE FIRST DROP IN POWER WAS FROM 2400 RPM TO 2100 RPM. THEN A SLIGHT RISE IN POWER THEN BACK DOWN TO 2100 RPM. AFTER ADJUSTING THE M - [SDR 2016FA0000128](https://openairdocs.org/sdr/2016FA0000128), Feb 12, 2016: PRESSURE SWITCH. LEAKING. THIS IS A NORMALLY OPEN OIL PRESSURE SWITCH. CONTACTS CLOSE AT 4 PSI TO ACTIVATE THE ENGINE HR METER. THE SWITCH CONSTRUCTION IS METAL BODY, CRIMPED ON THE PLAS - [SDR 2012FA0000046](https://openairdocs.org/sdr/2012FA0000046), Jan 13, 2012: HINGE FITTING. CRACKED. DURING AN ANNUAL, DISCOVERED A WELDED REPAIR TO A CRACK ON THE PILOT-SIDE DOOR ON THE INNER SKIN BELOW THE RIVETS THAT FASTEN THE LOWER HINGE TO THE DOOR. WHILE - [SDR AU510001777](https://openairdocs.org/sdr/AU510001777), Dec 12, 2005: SPAR. FAULTY. LT AND RT WING REAR SPARS PNO 108-100000-23 (LT) AND P/N 108-100000-24 (RT) FAULTY. EVIDENCE OF WING MOVEMENT AT SKIN INTERSECTIONS ON TOP OF EACH WING. - [SDR 2005FA0001267](https://openairdocs.org/sdr/2005FA0001267), Aug 25, 2005: MOUNT. CRACKED. THE UPGRADED ENGINE MOUNT WAS FOUND CRACKED. A PLUG USED TO RELIEVE WELDING PRESSURE AND ADD ADD LINSEED OIL APPEARS TO THE THE PROBLEM (STRESS RISER? ETC) THE - [SDR 2005FA0000184](https://openairdocs.org/sdr/2005FA0000184), Feb 14, 2005: ADAPTER. LEAKING. DOUBLER INSTALLEN IN FUEL TANK HAS NO ACCESS AND MFG CAN NOT TELL US HOW TO STOP FUEL LEAK. - [SDR 20000920SH001](https://openairdocs.org/sdr/20000920SH001), Jul 14, 2000: VENT LINE. BENT. INITIAL FLIGHT INFORMATION REVEALED RIGHT FUEL TANK WOULD RUN DRY LONG BEFORE LEFT. AFTER MANY LEAK TESTS, THE FUEL VENTS WERE SET TO FACTORY SPECS. NEXT FLIGHT - [SDR AU981005](https://openairdocs.org/sdr/AU981005), Aug 14, 1998: FORK. CRACKED. (AUS) NOSE LANDING GEAR FORK CRACKED. FOUND DURING INSPECTION IAW SB2241. - [SDR AU981004](https://openairdocs.org/sdr/AU981004), Aug 14, 1998: FORK. CRACKED. (AUS) NOSE LANDING GEAR FORK CRACKED. FOUND DURING INSPECTION IAW SB2241. - [SDR AU981003](https://openairdocs.org/sdr/AU981003), Aug 14, 1998: FORK. CRACKED. (AUS) NOSE LANDING GEAR FORK CRACKED. FOUND DURING INSPECTION IAW SB 2241. - [SDR 98ZZZX1910](https://openairdocs.org/sdr/98ZZZX1910), May 12, 1998: BOLT. FAILED. DURING THE 7,000 HOUR WING CARRY-THROUGH STRUCTURE INSPECTION AND WING BOLT REPLACEMENT, FOUND BOLT HEAD, WASHER, AND SPACER LYING IN BOTTOM OF SPAR. NOTED CORR - [SDR 96ZZZX4755](https://openairdocs.org/sdr/96ZZZX4755), Aug 21, 1996: NOSE GEAR. FAILED. AIRCRAFT LANDED, BOUNDED HARD, THEN HIT NOSE GEAR FIRST. NOSE GEAR SHEARED OFF. NO INJURIES. AIRCRAFT DAMAGE TO NOSE GEAR, PROPELLER STRIKE, AND ENGINE SUDDEN S - [SDR 95ZZZX6769](https://openairdocs.org/sdr/95ZZZX6769), Nov 21, 1995: CYLINDER. GLAZED. ENGINE INSTALLED WITH NEW MILLENNIUM CYLINDERS DURING MAJOR OVERHAUL. COMPRESSION CHECKS AFTER 100.5 HOURS REVEALED NR 1 - 52 PSI, NR 2 - 64 PSI, NR 3 - 52 PSI, - [SDR 95ZZZX5630](https://openairdocs.org/sdr/95ZZZX5630), Sep 10, 1995: ROCKER COVER. RUSTED. WHILE PERFORMING AN ANNUAL INSPECTION THE ROCKER COVERS WERE FOUND EXTREMELY RUSTY ON THE INSIDE. OWNER ADVISED HE HAD LEFT THE ENGINE HEATER PLUGGED IN ALL WIN - [SDR 95ZZZX3658](https://openairdocs.org/sdr/95ZZZX3658), Jul 5, 1995: PUSHROD. FAILED. PUSHROD FAILED AND WAS NOT MARKED WITH THE PROPER P/N PER THE A.O. 80-25-02 LYCOMING ADVISED THAT THE PROPER PUSHRODS WERE INSTALLED DURING ORIGINAL ASSEMBLY. A ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech 77](https://openairdocs.org/model/beech-77): 113 registered aircraft, registry code 1153007 - [Parker 77](https://openairdocs.org/model/parker-77): 0 registered aircraft, registry code 0564430 --- 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.