Beech Bonanza/Debonair In-Flight Break-ups |
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1962- 2007 |
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Date |
Location |
Model |
T-storm/CU encounter |
VFR into IMC |
Partial panel |
Attempted aerobatics |
Airframe ice |
Non-convective turbulence |
Loss of control (IFR) |
Other/unknown |
NTSB ID |
NTSB comment |
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2/22/1964 |
MT |
C35 |
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1 |
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Unknown |
OVERLOAD FAILURE |
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3/1/1964 |
AL |
M35 |
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1 |
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Unknown |
SEPARATION IN FLIGHT |
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8/1/1965 |
OH |
A35 |
1 |
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CHI66A0013 |
OVERLOAD FAILURE |
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8/5/1965 |
MS |
A35 |
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1 |
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MIA66A0018 |
OVERLOAD FAILURE |
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8/31/1965 |
KS |
M35 |
1 |
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MKC66A0014 |
SEPARATION IN FLIGHT |
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9/10/1965 |
Can |
B35 |
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1 |
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CAN65C0036 |
STRUCTURAL FAILURE DUE AERODYNAMIC LOADS. |
10/8/1965 |
WI |
35 |
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1 |
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CHI66A0033 |
SEPARATION IN FLIGHT |
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12/24/1965 |
VA |
D35 |
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1 |
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NYC66A0069 |
RUDDERVATOR FAILURE CAUSED BY AERODYNAMIC OVERLOADS |
12/29/1965 |
UT |
C35 |
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1 |
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DEN66A0052 |
WINGS: WING ATTACHMENT FITTINGS,BOLTS SEPARATION IN FLIGHT |
4/19/1966 |
PA |
S35 |
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1 |
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NYC66A0119 |
WITNESS HEARD ACFT DIVE,EXPLODE;PARTS FALL OUT of OVERCST |
7/22/1966 |
MN |
C35 |
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1 |
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MKC67A0005 |
MOVABLE TAIL SURFACFS NOT RECOVERED. |
8/9/1966 |
AK |
V35 |
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1 |
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ANC67A0015 |
L.AND R.RUDDERVATORS AND L.WING SEP DUE TO OVERLOADS. |
8/10/1966 |
IL |
H35 |
1 |
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CHI67A0022 |
RUDDERVATORS FAILED DUE NEG.OVERLOAD. |
8/25/1966 |
OR |
G35 |
1 |
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SEA67A0017 |
HORIZONTAL STABILIZER, ATTACHMENTS SEPARATION IN FLIGHT |
9/11/1966 |
OR |
A35 |
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1 |
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SEA67A0022 |
RIGHT WING AND LEFT RUDDERVATOR FAILED IN FLIGHT |
9/21/1966 |
IL |
F35 |
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1 |
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CHI67A0011 |
HORIZONTAL STABILIZER, ATTACHMENTS OVERLOAD FAILURE |
11/5/1966 |
KY |
G35 |
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1 |
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CHI67A0060 |
BOTH WINGS AND EMPENNAGE SEPARATED. |
11/7/1966 |
PA |
S35 |
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1 |
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NYC67A0077 |
L WING OUTBOARD LEFT/RIGHT RUDDERVATOR SEP |
12/31/1966 |
GA |
35 |
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1 |
MIA67A0069 |
WINGS SEPARATED IN FLT |
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1/28/1967 |
CA |
B35 |
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1 |
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OAK67A0059 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
2/11/1967 |
VT |
35 |
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1 |
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NYC67A0113 |
OUTBOARD R WING FAILED POSITIVELY.TAIL ASSY SEPARATED |
3/12/1967 |
CA |
A35 |
1 |
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OAK67A0067 |
SEPARATION IN FLIGHT |
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4/14/1967 |
TX |
F35 |
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1 |
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FTW67A0102 |
LEFT WING FAILED. |
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4/21/1967 |
SD |
35 |
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1 |
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MKC67A0059 |
SEPARATION IN FLIGHT |
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7/21/1967 |
NJ |
H35 |
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1 |
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NYC68A0013 |
GENL INFLITE DISINTEGRATION. |
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8/3/1967 |
MO |
E35 |
1 |
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MKC68A0009 |
INFLIGHT STRUCTURAL DISINTEGRATION. |
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11/5/1967 |
NY |
A35 |
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1 |
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NYC68A0070 |
NON-INST RATED PLT. RT WING AND EMPENNAGE SEPARATED. |
4/11/1968 |
WY |
V35 |
1 |
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DEN68A0045 |
LT WING AND TAIL ASSY SEPARATED FROM ACFT. |
5/5/1968 |
CA |
V35 |
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1 |
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OAK68A0064 |
HORIZONTAL STABILIZER, ATTACHMENTS VERTICAL STABILIZER |
5/19/1968 |
PA |
A35 |
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1 |
NYC68A0121 |
LEADING EDGE RT WING, 40 IN PIECE OF RT AILERON SEPARATION |
7/4/1968 |
MT |
C35 |
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1 |
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SEA69A0005 |
GENERAL DISINTEGRATION IN FLT. |
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7/18/1968 |
OH |
G35 |
1 |
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CHI69A0007 |
GENERAL DISINTEGRATION OF ACFT. |
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8/4/1968 |
IA |
G35 |
1 |
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MKC69A0008 |
GENERAL DISINTEGRATION OF ACFT. |
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9/30/1968 |
KS |
V35A |
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1 |
MKC69A0018 |
BOTH WING ,ENG WITH FWD FUSELAGE SECTION, EMPENNAGE SEP |
1/20/1969 |
TX |
M35 |
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1 |
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FTW69A0049 |
GYRO INOP.IFR IN CLOUDS.WINGS/TAIL CAME OFF. |
3/30/1969 |
LA |
S35 |
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1 |
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FTW69A0067 |
WINGS FAILED OUTBD OF ATTACHMENTS. |
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4/23/1969 |
OR |
K35 |
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1 |
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SEA70A0003 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
12/9/1969 |
NV |
K35 |
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1 |
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LAX70A0034 |
SEPARATION IN FLIGHT icing conditions |
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7/19/1965 |
ID |
35 |
1 |
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SEA66A0005 |
SEPARATION IN FLIGHT |
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3/30/1970 |
CA |
P35 |
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1 |
LAX70AL062 |
OVERLOAD FAILURE |
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4/26/1970 |
GA |
P35 |
1 |
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MIA70AM086 |
PLT RCVD SVR WX WARNG.TURBC SVR TO EXTREME FCST |
7/15/1970 |
WV |
33 |
1 |
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IAD71AI005 |
BOTH WGS SEPARATED. |
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5/7/1971 |
IN |
C35 |
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1 |
CHI71AC082 |
3 OF 4 RUDDERVATOR TRIM TAB CTL CABLES SEVERELY CORRODED,FAILED. |
5/27/1971 |
KY |
P35 |
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1 |
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CHI72AC085 |
ACFT DISINTEGRATED. PLT FLT PLANNED INTO KNOWN MARGINAL WEA. |
7/2/1971 |
NC |
S35 |
1 |
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IAD72AI001 |
ACFT DISINTEGRATED. |
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10/1/1971 |
SD |
C35 |
1 |
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MKC72AK023 |
R WG,BOTH STABS AND CTL SURFACES SEPARATED IN FLT. |
11/9/1971 |
TX |
C35 |
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1 |
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FTW72AF026 |
EMPENNAGE SEPN DUE HI POS G LOAD. |
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11/22/1971 |
TX |
J35 |
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1 |
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FTW72AF029 |
FAILURE OCCURRED IN TURB ENVIRONMENT. GENL INFLT BREAKUP. |
3/30/1972 |
NE |
F35 |
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1 |
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MKC72AK058 |
EXTENSIVE IN-FLT BREAKUP |
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8/18/1972 |
BI |
D35 |
1 |
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Unknown |
R WG AND STABILIZERS FAILED |
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11/17/1972 |
TX |
B35 |
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1 |
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FTW73AFO19 |
OVERLOAD FAILURE |
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4/14/1973 |
KS |
E35 |
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1 |
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MKC73AK061 |
IN HOLDING PATTERN . LOST CTL,L WG SEPARATED IN FLT. |
4/22/1973 |
TX |
V35 |
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1 |
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FTW73AF062 |
LOST CTL IN IFR COND.BOTH WGS SEPARATED.INST RATING 3 1/2 WKS PRIOR. |
7/27/1973 |
GA |
V35A |
1 |
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MIA74AM009 |
L WING,STAB SEPD. |
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8/16/1973 |
IA |
E35 |
1 |
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MKC74AK006 |
L STAB ASSY SEPARATED |
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8/26/1973 |
TX |
35 |
1 |
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FTW74AF011 |
OUTBD R WG & BOTH STABS SEPARATED IN FLT. |
9/6/1973 |
OK |
P35 |
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1 |
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FTW74AF014 |
WINGS AND TAIL SEPRTD. |
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10/25/1973 |
CA |
35 |
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1 |
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OAK74AP018 |
LOC APCH.DIFFICULTY .OVERLOAD FAILURE L WING,SEPARATED. |
12/26/1973 |
CA |
C35 |
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1 |
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OAK74AP025 |
R WING,STABS SEPD. |
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3/10/1974 |
OK |
35 |
1 |
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FTW74AF065 |
SEPN OF L WING ASSY & EMPENNAGE. |
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4/20/1974 |
KS |
35 |
1 |
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MKC74AK062 |
GENERAL DISINTEGRATION |
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5/5/1974 |
TX |
S35 |
1 |
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FTW74AF080 |
SEPARATION IN FLIGHT |
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5/14/1974 |
MT |
35 |
1 |
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SEA74AS044 |
DISINTEGRATION INFLT. |
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6/1/1974 |
KY |
P35 |
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1 |
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NYC74AN099 |
R AND L RUDDERVATOR SEPARATED |
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6/5/1974 |
KY |
35 |
1 |
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NYC74AN102 |
R WING MAIN SPAR FRAGMENTED. |
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6/30/1974 |
OH |
N35 |
1 |
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CHI74AC100 |
WING SPAR WING ATTACH POINTS SPTD POSITIVE,REARWARDS DIRECTION. |
8/2/1974 |
AL |
M35 |
1 |
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MIA75AM012 |
WINGS,EMPENNAGE SEPD |
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8/16/1974 |
AR |
V35A |
1 |
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FTW75AF007 |
OVERLOAD FAILURE |
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9/1/1974 |
OH |
35 |
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1 |
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CHI75AC024 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
9/1/1974 |
LA |
P35 |
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1 |
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FTW75AF013 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
9/24/1974 |
TX |
M35 |
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1 |
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FTW75AF024 |
L WG FAILED JUST BFOR IMPACT. |
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12/30/1974 |
TX |
V35B |
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1 |
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FTW75AF046 |
BOTH WGS & R STAB SEPARATED IN FLT. |
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1/30/1975 |
CA |
N35 |
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1 |
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LAX75AL030 |
BOTH STABS & L WG FAILED |
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4/6/1975 |
CA |
M35 |
1 |
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LAX75AL050 |
L WG & STAB SEPARATED IN FLT |
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4/22/1975 |
TX |
V35A |
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1 |
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FTW75AF064 |
BOTH RUDDERVATORS & R WG SEPARATED |
5/30/1975 |
GA |
G35 |
1 |
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MIA75AM084 |
OVERLOAD FAILURE |
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6/22/1975 |
MN |
A35 |
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1 |
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MKC75AK063 |
GENERAL DISINTEGRATION |
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7/16/1975 |
GA |
35 |
1 |
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MIA76AM005 |
INITIAL FAIL IN LE OF R WING,SEPARATED OUTBOARD OF WHEEL WELL. |
8/1/1975 |
AL |
J35 |
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1 |
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MIA76AM012 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT. . |
10/16/1975 |
TX |
V35 |
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1 |
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FTW76AF033 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
10/24/1975 |
IL |
V35B |
1 |
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CHI76AC033 |
RUDDERVATORS AND BOTH WINGS SEPARATED |
11/28/1975 |
CA |
P35 |
1 |
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LAX76AL039 |
BOTH WINGS SEPD NR GND |
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5/28/1976 |
CA |
M35 |
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1 |
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LAX76AL080 |
OVERLOAD FAILURE |
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9/26/1976 |
MN |
P35 |
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1 |
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MKC76AK084 |
STRUCTURAL ICE. TAIL SECTION BROKE FREE IN FLIGHT. |
10/2/1976 |
AZ |
35 |
1 |
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LAX77FA001 |
ENTIRE EMPENNAGE SEPARATED. |
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1/14/1977 |
WA |
C35 |
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1 |
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SEA77FA012 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
3/5/1977 |
GA |
M35 |
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1 |
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MIA77FA042 |
EXTENSIVE IN FLIGHT BREAKUP. |
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5/5/1977 |
CA |
35 |
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1 |
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LAX77FA041 |
L WG FAILED. |
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8/18/1977 |
LA |
V35B |
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1 |
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FTW77FA070 |
OVERLOAD FAILURE FIRST FLT IN ACTUAL INSTRUMENT CONDITIONS. |
9/12/1977 |
OK |
V35A |
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1 |
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FTW77FA074 |
GENERAL DISINTEGRATION. |
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10/15/1977 |
KY |
D35 |
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1 |
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IAD78FA005 |
SEPARATION IN FLIGHT |
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10/23/1977 |
LA |
M35 |
1 |
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FTW78FA005 |
WINGS POS OVERLOAD L WING SEP DOWN L R STAB RUDVATR SEP POS |
11/17/1977 |
IN |
P35 |
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1 |
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CHI788A011 |
GENERAL DISINTEGRATION. |
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2/10/1978 |
CA |
35 |
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1 |
OAK78FA016 |
LEFT WING DISINTEGRATED IN FLIGHT. |
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4/26/1978 |
GA |
N35 |
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1 |
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MIA78FA072 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
4/29/1978 |
IA |
S35 |
|
1 |
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MKC78FA034 |
OVERLOAD FAILURE |
|
|
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5/1/1978 |
CA |
S35 |
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1 |
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LAX78FA045 |
LEFT WING & TAIL SURFACES MISSING |
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5/12/1978 |
MO |
F35 |
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1 |
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MKC78FA037 |
SEPARATION IN FLIGHT |
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6/23/1978 |
MO |
E35 |
1 |
|
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MKC78FA052 |
OVERLOAD FAILURE |
|
|
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3/17/1979 |
CA |
D35 |
|
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|
1 |
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LAX79FA034 |
OVERLOAD FAILURE |
|
|
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3/18/1979 |
CA |
A36 |
|
1 |
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LAX79FA036 |
SEPARATION IN FLIGHT |
|
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5/23/1979 |
AL |
G35 |
1 |
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MIA79FA088 |
SEPARATION IN FLIGHT |
|
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10/20/1979 |
CA |
V35B |
|
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1 |
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LAX80FA006 |
WINGS SEPARATED. |
|
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2/24/1980 |
GA |
V35 |
1 |
|
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MIA80FA037 |
OVERLOAD FAILURE |
|
|
|
5/25/1980 |
SC |
P35 |
|
1 |
|
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ATL80FA050 |
L STAB/RUDDERVATOR SEPTD. |
|
|
6/12/1980 |
CA |
35 |
|
1 |
|
|
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LAX80FA112 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
9/12/1980 |
CA |
35 |
|
|
|
|
|
|
|
1 |
LAX80FA140 |
OVERLOAD FAILURE |
|
|
|
12/30/1980 |
WI |
G35 |
|
1 |
|
|
|
|
|
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CHI81FA014 |
V-TAIL STABILIZRS & WINGS SEPD DWNWRD |
1/16/1981 |
AZ |
S35 |
|
1 |
|
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LAX81FA037 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
2/28/1981 |
NM |
A36TC |
|
1 |
|
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FTW81FA041 |
BOTH WINGS & R HRZNTL STAB SEPD UPWARD.L HRZNTL STAB BENT UP & AFT. |
3/6/1981 |
CO |
P35 |
|
|
|
|
1 |
|
|
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CHI81FA032 |
GENERAL DISINTEGRATION |
|
|
3/20/1981 |
AZ |
B35 |
|
1 |
|
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LAX81FA063 |
EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT |
4/18/1981 |
OK |
E35 |
|
1 |
|
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FTW81FA074 |
L RUDDERVATOR SEPD DWNWRD.R WING, R STAB/RUDDERVATOR SEPD UP |
2/13/1982 |
CA |
J35 |
|
1 |
|
|
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LAX82FA071 |
LEFT WING & BOTH STABILATORS SEPARATED |
7/2/1982 |
CA |
V35B |
|
|
|
|
1 |
|
|
|
LAX82FA240 |
STABILIZER REVEALED IT HAD SEPARATED DOWNWARD |
5/22/1983 |
AL |
V35B |
|
|
|
|
|
|
1 |
|
ATL83FA198 |
STABILIZERS/RUDDERVATORS, TAIL CONE, RIGHT WING TIP TANKS SEP |
8/1/1983 |
NC |
F35 |
1 |
|
|
|
|
|
|
|
ATL83AA305 |
ONE WING MISSING |
|
|
|
2/17/1984 |
VA |
V35B |
|
|
|
|
|
|
1 |
|
ATL84MA101 |
DEFORMATION L STAB UPWARD DEFORMATION R STAB |
5/26/1984 |
OK |
G35 |
|
1 |
|
|
|
|
|
|
FTW84FA242 |
SEPARATED IN-FLT AT A LOW ALT |
|
6/17/1984 |
NE |
C35 |
1 |
|
|
|
|
|
|
|
MKC84FA174 |
WRECKAGE 1 MI BY 1/4 MI. |
|
|
7/22/1984 |
FL |
A36 |
1 |
|
|
|
|
|
|
|
MIA84FA206 |
WINGS UP, VERTSTAB SEP TOP OF TAILCONE CONE SEP |
7/27/1984 |
TX |
S35 |
1 |
|
|
|
|
|
|
|
FTW84FA326 |
EVIDENCE OF PREVIOUS STABILIZER OVERLOAD |
9/26/1984 |
SC |
V35B |
|
|
|
|
|
|
|
1 |
ATL84FA298 |
RT & LT STABILIZERS & RUDDERVATOR GROSS NEGATIVE OVERLOAD |
12/6/1984 |
NC |
N35 |
|
1 |
|
|
|
|
|
|
ATL85FA050 |
FUSELAGE..OVERLOAD |
|
|
3/21/1985 |
CA |
D35 |
|
|
|
|
|
1 |
|
|
LAX85FA181 |
LEFT STABILIZER ASSEMBLY SEPARATED |
|
7/25/1985 |
OK |
H35 |
|
1 |
|
|
|
|
|
|
FTW85MA297 |
LEFT WING & BOTH RUDDERVATORS HAD SEPD FM OVERLOAD FAILURE |
3/15/1986 |
CA |
A36TC |
|
|
|
|
1 |
|
|
|
LAX86FA140 |
FAIL L SIDE CARRY THRU STRUCTURE. STRUCTURE BROKE UPWARD
(POSITIVE) |
6/4/1986 |
OK |
A36TC |
1 |
|
|
|
|
|
|
|
DEN86FA150 |
STABILIZERS FAILED NEG AND SEP BOTH WINGS THEN FAILED NEGATIVELY |
9/7/1988 |
FL |
K35 |
|
1 |
|
|
|
|
|
|
MIA88FA267 |
FUSELAGE MINUS WINGS & TAIL SPINNING FROM OVRCST |
9/18/1989 |
CA |
S35 |
|
1 |
|
|
|
|
|
|
FTW89GA170 |
OUTER 1/2 RIGHT WING SEPARATED |
|
7/12/1990 |
VA |
P35 |
1 |
|
|
|
|
|
|
|
BFO90FA063 |
LEFT WING AND RIGHT STABILATOR SEPARATED |
5/16/1991 |
TX |
V35B |
1 |
|
|
|
|
|
|
|
FTW91FA080 |
IN-FLT BREAKUP |
|
|
|
8/5/1992 |
AR |
A36 |
1 |
|
|
|
|
|
|
|
DEN92FA083 |
BROKE UP IN FLIGHT |
|
|
|
6/9/1993 |
WI |
A36 |
|
1 |
|
|
|
|
|
|
CHI93FA200 |
exceeded the design strees limits of the airplane |
10/2/1993 |
WI |
G35 |
|
|
|
|
|
|
|
1 |
CHI94FA001 |
STABS FAIL DOWN R WING SEP AT ROOT, L WING SEP 3 PCS |
11/12/1993 |
CA |
V35 |
|
1 |
|
|
|
|
|
|
LAX94FA048 |
BREAKUP ALTITUDE OF 14,000 FEET |
|
7/5/1994 |
AL |
H35 |
1 |
|
|
|
|
|
|
|
ATL94FA131 |
SPAR FRACTURE UP L RUDDERVATOR SEPARATED UPWARD |
7/12/1995 |
CA |
A36 |
|
|
|
|
|
|
|
1 |
LAX95FA249 |
STABILIZERS INITIALLY SEPARATED, FOLLOWED BY BOTH WINGS |
4/29/1996 |
GA |
V35 |
1 |
|
|
|
|
|
|
|
MIA96FA134 |
left wing and tail stabilizer had separated |
|
3/24/1997 |
FL |
V35 |
1 |
|
|
|
|
|
|
|
ATL97FA054 |
an in-flight breakup of the airplane was presumed to have
occurred |
5/12/1998 |
WV |
A36 |
|
|
|
|
1 |
|
|
|
IAD98FA054 |
stabilizer and wings downward overstress separation |
4/11/2002 |
CA |
G35 |
|
|
|
1 |
|
|
|
|
LAX02FA134 |
tail sep first, then l wing broke off. engine sep and the
passenger ejected |
4/27/2002 |
NC |
35 |
|
1 |
|
|
|
|
|
|
ATL02FA091 |
failure of the right wing due to overstress separation |
6/29/2002 |
AZ |
C35 |
|
|
|
|
|
|
|
1 |
LAX02FA210 |
R wing pos overload sep and impacted R stabilizer pilot falling
asleep |
7/5/2003 |
KY |
F35 |
|
1 |
|
|
|
|
|
|
NYC03FA148 |
in-flight breakup |
|
|
|
11/25/2003 |
OR |
S35 |
|
|
1 |
|
|
|
|
|
SEA04FA022 |
l stab sep upward and aft both wings sep up and positive |
7/18/2004 |
GA |
B36TC |
1 |
|
|
|
|
|
|
|
ATL04FA159 |
in-flight breakup |
|
|
|
2/9/2007 |
GA |
A36 |
|
|
|
|
1 |
|
|
|
ATL07FA040 |
broke up in-flight |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Totals |
48 |
55 |
4 |
2 |
13 |
6 |
9 |
11 |
|
|
|
|
|
|
Date |
Location |
Model |
Tstorm/ CU encounter |
VFR into IMC |
Partial panel |
Attempted aerobatics |
Airframe ice |
Non-convective turbulence |
Loss of control (IFR) |
Other/unknown |
NTSB ID |
NTSB comment |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Total |
148 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Model 35 |
136 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
(V-tail) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Models 33, 36 |
12 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
(Straight tail) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|