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ASCE 10-97 Suspicious Design Results STAAD

Hi Everyone,

I have the following structure modeled in STAAD and evaluated using ASCE 10-97.  After reviewing some of the results, the utilization ratios are not in agreement with the hand calculations based on the forces being applied.  I concentrate on member 881 which has an utilization of 24.5 which makes no sense.  Please advice if I have input something wrong in the design component.

CODE ASCE 1997
FYLD 4752 MEMB 881
UNB 7.8 MEMB 881
UNT 7.8 MEMB 881
MAIN 5 MEMB 881
LEG 0 MEMB 881
SSY 1 ALL
SSZ 1 ALL
NHL 0 MEMB 881
TRACK 3 MEMB 881
CHECK CODE MEMB 881
UNIT INCHES KIP
LOAD LIST 20
PRINT MEMBER FORCES GLOBAL LIST 881
SECTION 0 0.25 0.5 0.75 1 MEMB 881
PRINT MEMBER SECTION FORCES LIST 881
PRINT MEMBER STRESSES LIST 881
FINISH

 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted)
 
 MEMBER     TABLE       RESULT/   CRITICAL COND/     RATIO/     LOADING/
                          FX            MY             MZ       LOCATION
 =======================================================================
 

 *   881 ST   L25253                   (AISC SECTIONS)
                           FAIL     ASCE 3.12-1       24.572        20
                        6.59 C          0.04           0.66        3.89
 
   AXIAL CAPACITY OF SECTION =      9.422
   EULER CAPACITIES - Y AXIS, Z AXIS =     29.047,        6.860
   MOMENT CAPACITY - Y AXIS =      1.204
   MOMENT CAPACITY - Z AXIS =      0.695
   BOLT CAPACITY =  11.421  NO OF BOLTS =   1   NET SECT. FACTOR = 1.000
   SHEAR CAPACITY/ACTUAL SHEAR - Y AXIS =      5.997,        0.000
   SHEAR CAPACITY/ACTUAL SHEAR - Z AXIS =      5.997,        0.000
   ACTUAL/ALLOWABLE SLENDERNESS RATIOS =    165.444,      250.000
 
 |---------------------------------------------------------------------|
 
 
 
   ************** END OF TABULATED RESULT OF DESIGN **************
 
 
  2869. UNIT INCHES KIP
  2870. LOAD LIST 20
  2871. PRINT MEMBER FORCES GLOBAL LIST 881
    STAAD SPACE                                              -- PAGE NO.  346


 
 
   MEMBER END FORCES    STRUCTURE TYPE = SPACE
   -----------------
   ALL UNITS ARE -- KIP  INCH     (GLOBAL)
 
  MEMBER  LOAD  JT      FX        FY       FZ        MX        MY         MZ
 

 
    881   20   230     -0.03      0.00     6.59      0.00      0.00       0.00
               232     -0.03      0.00    -6.59      0.00      0.00      -0.00
 
 
   ************** END OF LATEST ANALYSIS RESULT **************
 
 
  2872. SECTION 0 0.25 0.5 0.75 1 MEMB 881
  2873. PRINT MEMBER SECTION FORCES LIST 881
    STAAD SPACE                                              -- PAGE NO.  347


 
 
   MEMBER FORCES AT INTERMEDIATE SECTIONS
   --------------------------------------
   ALL UNITS ARE -- KIP  INCH
 
 MEMB  LOAD  SEC       AXIAL   SHEAR-Y   SHEAR-Z       MOM-Y       MOM-Z
 

 
   881   20  0.25       6.59     -0.01      0.01        0.43        0.43
             0.50       6.59      0.00      0.00        0.57        0.57
             0.75       6.59      0.01     -0.01        0.43        0.43
 
 
   ************** END OF LATEST ANALYSIS RESULT **************
 
 
  2874. PRINT MEMBER STRESSES LIST 881
    STAAD SPACE                                              -- PAGE NO.  348


 
 
  MEMBER STRESSES
  ---------------
  ALL UNITS ARE KIP /SQ INCH
 
 MEMB   LD  SECT    AXIAL    BEND-Y     BEND-Z   COMBINED  SHEAR-Y  SHEAR-Z
 

 
    881   20   .0      7.3 C      0.0       0.0       7.3      0.1      0.1
              0.25     7.3 C      0.9       1.9       9.7      0.0      0.0
              0.50     7.3 C      1.2       2.6      10.5      0.0      0.0
              0.75     7.3 C      0.9       1.9       9.7      0.0      0.0
              1.0      7.3 C      0.0       0.0       7.3      0.1      0.1
 
 
   ************** END OF LATEST ANALYSIS RESULT **************


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